1989 archive...5.3 steam generator tube/tubes failure. 5.4 end plug fails to close after refuelling....
TRANSCRIPT
PROBABILISTIC SAFETY ASSESSMENT OF
NARORA ATOMIC POWER PROJECTby
A. K. Babar, R. K. Saraf, A. Kakodkar Reactor Engineering Division
andV. V. S. Sanyasi Rao
Health Physics Division
1989
B.A
.R.C
. - 14
45
B.A.R.C. - 1445
GOVERNMENT OF INDIA ATOMIC ENERGY COMMISSION
PROBABILISTIC SAFETY ASSESSMENT OF NARORA ATOMIC POWER PROJECT
byA.K. Babar, R.K. Saraf and A. Kakodkar
Reactor Engineering Divisionand
V.V.S. Sanyasi Rao Health Physics Division
BHABHA ATOMIC RESEARCH CENTRE BOMBAY, INDIA
1989
INIS Subject Category s E34.00
Descriptors
NARORA-1 REACTOR NARORA-2 REACTOR REACTOR SAFETY PROBABILISTIC ESTIMATION FAILURE MODE ANALYSIS REACTOR ACCIDENTS MONTE CARLO METHOD FAULT TREE ANALYSIS RELIABILITY FAILURESREACTOR COOLING SYSTEMSPUMPSFEED WATERECCMODERATORSVALVESPIPESCALANDRIAS CONDENSATES HEAT EXCHANGERS COMPRESSORS POWER SUPPLIES REACTOR SHUTDOWN LEAKSCONTAINMENT
EBDBABILISIIC-SAEEJDL-ASSESSHEHIOE
NARDRA ATOMIC POWER PROJPCT
ABSTRACT
Various safety studies on Pressurised Water. and Boiling Water reactors have been conducted. However, a detailed report on probabilistic safety assessment(PSA) of PHWRs is not available. PSA level T results of thestandardised 235 MWe PHWR under construction at Narora are presented herein. Fault Tree analysis of various initiating events(IEs), safety systems haa been completed. Event Tree analysis has been performed for. all the dominating IEs to identify the accident sequences and a list of thedominating accident sequences is included. Analysis has been carried out using Monte Carlo simulation to propagate the uncertainties in failure rate data. Further, uncertainty analysis ic extended to obtain distributions for the accident sequences and core damage frequency. Some noteworthy results of the study apart from the various design modifications incorporated during the design phase are : .
i) The accident sequences resulting from station blackout are dominant contributors to the core damage frequency.
ii) Class-IV transients, small break LOCA are significantIEs. Main steam line break is likely to induce (staeam S-Uc"4' generator tube ruptures.
iii) Moderator circulation, fire fighting system, secondary steam relief are relatively important in core damage frequency reductions.
iv) Under accidental situations human errors are likely to be associated with valving in shutdown cooling and fire fighting systems.
(i>
LEOEHDIE -Initiating Event
ESF -Engineered Safety Function
ML -Medium LOCA
SL -Small LOCA
Class JV -Main( Grid & Station) Power Supply
Class III -Emergency(DG) Power Supply
FW -Feed Water
MSLB -Main Steam Line Break
APWS -Active Process Water System
NAHPPWS -Non-active High Pressure Process Water System
ECI -Emergency Coolant Injection
ECR -Emergency Coolant Recirculation
RBI -Reactor Building Isolation
RBC -Reactor Building Cooling
RT -Reactor Trip
SLHS -Small LOCA Handling System
FFS -Fire Fighting System
SSR -Secondary Steam Relief
AFWS -Auxiliary Feed Water System
SDC -Shutdown Cooling System
(ii)
EAPWS -Emergency Active Process Water System
ЯЕ -Human Error
CCF -Common Cause Failure
PROBABILISTIC SAPETT ASSESSMEt QZ
HARQBA ATOMIC POWER project
<¥4Л»PPCIIOH
Probabiliatic Safety AsaeasaentCPSA) in the context of Nuclear Power Plants(NPPs) is associated with the nodels that predict the offsite radiological release resuiting from the potential reactor accidents. In its entirety, it comprises the following levels:
1.Identification of accident sequences and quantitative estimates of the frequency of each i.e System Analysis
2. Radiological release to the environment associated with each class of accident sequence i.e. Containment Analysis
3. Analysis of the off-site consequences of the releasei.e. Consequence Analysis
It is intended to obtain a fullscope probabilistic model of a standardised 235MWe Pressurised Heavy Water Reactor (PHWR) which would be uséd in the safety and operational analysis of the reactor. The model would be a risk management tool to meet the following objectives.
a. Determining the core damage frequency using a set of internal Initiating Events(IEs) and external IEs like loss of off-site.power
b. Identification and quantification of the dominating! accident sequences, uncertainities and spécifié contributers to system failures to establish their teat: and procurement procedures
c. Identifying design and operational weaknesses
d. Supporting decisions on safety issues
e. Developing test and maintenance schedules anddetersuning allowable outage times to assist in the establishment of criteria for Technical Specifications
f. Correlating accident »equences to release categories
g. Consequence modelling and risk estimation
Narora Atomic Power Project(KAPP) is a 235 KVe PHVR under construction and would be a standardised design for the forthcoming similar projects under construction or being planned. A PSA study of KAPP was undertakeri to identify the dominating accident sequences relevant to PHWR design, quantify the same using System Reliability Models like Fault Tree etc. to fulfill the various objectives and perform a design evaluation to improve Safety and Reliability and possibly think in terms of an Inherently Safe Reactor. This report presents the results of Level-I PSA carried out for HAPP in terms of the following information.
a. Identification of dominating Initiating Events
b. Reliability analysis of various IEs and the Engineered Safety Functions(ESFs) using Fault Tree methods.
c. Identification of accident sequences leading to core damage using Event Tree methods
d. Quantification of accident sequences to obtain dominating accident sequences leading to fixing the reliability requirements of various systems in reducing the risk
e. Uncertainty analysis and error propagation to account for the variability in component failure data, accident sequence and core damage frequency etc.
3LimiIAIXHC ITS
Many iapoctant studies.exaaplea [13,t2] have been perforeed on the use of PSA In case of Light Water Reactors(LWRs), however, a detailed study is yet to appear for a PHVR. In order to Identify the IEs applicable to a PHWR, it would be worthwhile to list the different design features. The PHWR is a heavy water cooled, heavy water ■oderated, natural uraniun fuelled reactor which utilises the pressure tube concept. The pressure tubes containing the fuel run horizontally through the reactor core. Each pressure tube is isolated and insulated froa the heavy water aoderator by a concentric calandria tube and a gas annulus. The aoderator is operated at low teaperature and pressure. The reactivity control and shutdown aechanisas reside in the low pressure aoderator, thus siaplifying their design, construction and áaintenance and eliainating virtually, the possibility of their ejection in an accident situation. In the standardised design, two fast acting, independent, diverse shutdown systeas are provided and on a reactor trip, the aoderator is not duaped. Thus, in case of loss of coolant accidents, the cool.aoderator can act as a heat sink.
The IEs can be generally classified into the following aain groups:
1. Decrease in reactor coolant inventory
2. Increase in reactor coolant inventory
3. Decrease in reactor coolant system flow rate
4. Decrease in heat renoval by secondary systea
5. Increase in heat renoval by secondary systea
6. Reactivity and power distribution anoaalies
7» Anticipated transients without scranUTWS)
8. Radioactive releasee from a sub-system or component
9. Others
Annex. 2 of Safety Guide SGD11[3] gives a list of IEs generally analysed for the application of a licence for LVR in U.S.A. A number of IEs listed below were added to account for the design differences between PHWRs and LWRa.
1. Leakage from the seal plug after refuelling (group 1)
2. Bleed valve stuck open(l)
3. Failure of a limited number of tubes in any heat exchanger other than steam generator in PBT systea(1)
4. Failure of coolant channel including its end fitting(l)
5. Feed valve stuck open(2)
6. Bleed valve stuck closed(2)
7. Bleed isolation valve closed(2)
8. Flow blockage in any coolant channel assembly/any feeder(3)
9. Failure of reactor moderator flow(6)
10. Failure at any location of moderator system piping(6)
11. Failure of fuelling machine when off the reactor and full of irradiated fuel(8)
A composite list incorporating the IEs given in reference [3] and those enumerated above was prepared and is given below.
1.0 Increase in heat removal by .Bccondarv_gygl:em
1.1 Feed water system malfunction that results in decrease in feed water temperature.
1.2 Feed water system naifunction that resulta in an increase in feed water flow.
1.3 Steam Pressure Regulator(Regulating eyeten)nalfunction or failure that results in increasing stean flow.
1.4 Inadvertant opening of a relief valve resulting in stean flow increase.
1.5 Spectra of steam system piping failures inside and outside containment.
2.0 Decrease in heat removal bv the secondary system2.1 Boiler pressure control(BPC) system nalfunction
resulting in decrease in stean flow.
2.2 Loss of external electrical load.
2.3 Turbine trips
2.4 Inadvertant closure of main steam isolation valve.
2.5 Loss of condenser vaccun.
2.6 Class IV power failure i.e. coincident loss of station as well as grid supply.
2.7 Loss of nornal feed flow.
2.0 Feed water piping break3.0 Decieftge .in reactor coolant .aydten flow ifttu
3.1 Single and multiple reactor coolant pump trips.
3.2 Coolant punp shaft seizure.
3.3 Coolant punp shaft breakage.
3.4 Flow blockage in any reactor fuel channel assembly.
3.5 Failure of all mechanical seals on PHT pump(s).
4.0 Increase in reactor coolant inventory.
4.1 Feed valve stuck open.
4.2 Bleed valve stuck closed.
4.3 Bleed isolation valve closed by mistake by the operator.
3.0 Decrease in reactor спо1аП^ inventory.
5.1 Inadvertant opening of a relief valve in PHT system.
5.2 Feed water tube or insturment tube breakage.
5.3 Steam generator tube/tubes failure.
5.4 End plug fails to close after refuelling.
5.5 PBT header and piping failure.
5.6 Bleed valves stuck open.
5.7 Feed isolating valve closed by operator's mistake.
5.8 Pressure tube failure( followed by calandria tube failure releasing PHT coolant to the moderator.
5.9 Failure of large number of tubes in any heat exchanger( other than steam generator) in PHT system( bleed cooler, gland cooler, shutdown cooler).
5.10 Failure of end fitting of any channel assembly followed by the failure of lattice tube of end shield through which the end fitting runs.
5.11 Failure of mechanical joint between pump cover and pump casing of main coolant pumps.
5.12 Massive failure of a pump cover/casing of main coolant pump.
6.0 Eeactivitv_and power distribution anamollaa.
6.1 Uncontrolled withdrawal of control rod( Reactivitycontrol nechanien) assembly from a sub-critical or low power start up condition( assuming the mostunfavourable conditions of the core and reactor coolant system).
6.2 Uncontrolled withdrawal of control rod assembly at a particular power( assuming the most unfavourable reactivity conditions of the core and the reactor coolant system) that yields the most severe result( low power to full power).
6.3 Chemical control( composition) system malfunction that results in a decrease in boron concentration in reactor coolant.
6.4 Fuel bundle ejection accident.
6.5 Failure of reactor moderator flow.
6.6 Failure at any location of any pipe of reactor moderator system.
6.7 Drop of a load on reactivity mechanisms.
7.0 EftflioacUve release, f roa, ft .cubs va tea pi component.7.1 Tritium leakage.
7.2 Radioactive gas waste system leak or failure.
7.3 Radioactive liquid waste system leak or failure.
7.4 Postulated radioactive releases due to liquid tank failures.
7.5 Design basis fuel handling accident.
7.6 Accidental dropping of spent fusl casks( during transfer of fuel to reprocessing plants).
7.7 Failure of fuelling machine when off-reactorcontaining full complement of irradiated fuel.
7.8 Failure of containment dousing(a) A douse has occured prior to accident.(b) Dousing system is unavailable following accident.
7.9 Containment and associated system failure.
7.10 One door open of air lock or transfer chamber most critical for radioactive release from containment and seals on second door deflated( its impact, for example, when PHT system is leaking or has broken).
7.11 Failure to close any containment isolation device.
8.0 Anticipated transients.without scram( Dual failures).
8.1
8.2
8.3
8.4
8.5
8.6
8.7
Inadvertant withdrawl of control rod( like 6.1 and 6.2 plus faulure of trips).
Loss of feed water.
Loss of class IV power.
Loss of electrical load.
Loss of condenser vaccum.
Turbine trip.
Closure of main steam line isolation valve.
9.0 Others•
9.1 Failure of instrument air.
9.2 Design basis fire.
9.3 Design basis earthquake.
9.4 Degraded operation of containment atmosphere cooling equipment( coupled with PHT failure).
9.5 Leaking containment( coupled with radioactive release from any other systems).
9.6 Turbine overspeed protection faulure.
9.7 Turbine break up.
9.8 Design basis tornado.
9.9 Failure of steam generator support.
9.10 Massive failure of station cooling water tunnel/discharge duct.
Based on the analytical study of the causes and consequences, the following events are considered important for further studies.
1. PHT header and piping failure(group 1)
2. Steam generator tube(s) failure(l)
3. Coolant channel failure(s)(1)
4. Spectrum of steam system piping failure inside and outside containment(5)
5. Loss of normal feed flow(4)
6. Feed water pipe breaks(4)
7. Class XV failure i.e. coincident loss of station as well as grid supply(4)
8. Compressed air failure
9. Fuelling machine induced LOCAs(l)
10. Leakage from the seal plug after refuèlling(1)
11. Loss of regulation
12. Flow blockagè in any coolant channel aaaenbly/feederO)
13. Process water system failure(9)
14. Single and multiple reactor coolant pump failure(s)(3)
15. Failure of a limited number of tubes in any heat exchanger other than the steam generator in PUT system(1)
16. Failure of moderator flow(6)
17. Turbine trips(4)
As can be inferred from the list above, the effect of internally generated missiles, man induced events( air craft crashes) and natural phenomena on the reactor and its associated systems is not considered in this analysis. In addition some events like ATWS are not considered due. to two independent fast acting and diverse shutdown systems in PHWRs. Turbine trip is covered by other events( partly by class IV failure and partly by IRV opening and/or secondary steam relief). Failure of moderator flow is not important as an initiating event. However moderator system is important in those situations where core cooling ' is impaired due to failure of other means of cooling. The remaining events are analysed regarding their frequency and possible impact on the core depending upon the operability states of the various ESFs provided, in the subsequent sections.
3..RSLIABHiII3LAHAbySISIt is important to differentiate between different
categories of systems from the reliability viewpoint. IEs are associated with failure in Process Systems which are active during normal functioning of the reactor e.g. Reactor Regulating System, Primary Heat Transport, fuel etc. where as ESFs are Protective and Containment Systems which are not active during the normal reactor operation but act following failure of a process system to limit the
11consequences thereof. Apart from these, there are support systems e.q. Station Electric Supply, Compressed Air which are active durinq normal operation and are also essential in the functioning of the ESFs.
Since process systems play an active role in plant operation, any process equipment failure would be immediately annunciated. But in case of protective and containment systems, being normally standby, there may be component failures which will be unrevealed till there is a demand on the system to function or it is tested. As a result a safety system will remain in a failed condition over the period of time from the occurrence of the failure till it is revealed by the test and repairs are effected. A process system failure during this interval would result in a dual failure. Thus, an accident sequence would arise if a process failure is coupled with the unavailability of one or more ESFs.
3,1,.RELIABILITY-CRITERIABased on the system definitions above, the reliability
index of process systems or lEs has been computed in terms of frequency i.e. the probable number of failures per year while for the safety systems, the. term unavailability or probability of failure on demand has been used which is the probable fraction of the time during which the system is not available. The unavailability is further related to component failure rates and test frequencies by the following equation
UnavailabilitysFailure rate(yr_1)*Failure- duration(Yrs)
where the failure duration is assumed to be equal to half of the time between tests since the failure at any time between tests is equally probable. Unless mentioned otherwise, the test interval used in the analysis is assumed as one month. Small variations in the test intervals are not considered whereas, if it varies by an order or more, an exact computation is used. In addition, the contributions due to scheduled and breakdown maintenances are also incorporated. The distribution of downtime is assumed as lognormal, with a median duration of
24 hours and a maintenance action rate of once in six months.
3.Jg.IMbPRE RATE DATAThe input data required for reliability analysis
comprises of the following
i) Component Failure Rate Data
ii) Component Maintenance Data
iii) Human Error Rate(HER) Data
iv) Common Cause Failure(CCF) DATA
The confidence in reliability analysis is determined to a large extent by the accuracy in failure rate data of the constituent components. It would be ideal to use data based on our operational experience but this is presently not adequate. The other alternative is to use data from established sources[4] which may not be always applicable due to variations in design, quality, operating environment etc. Bayesian techniques have been used to obtain better estimates by using the limited information based on RAPS experience and WASH-1400 as prior for a number of components like DCs, Transformers etc. The Kolmogorov- Smirnov test of hypothesis applied to the posterior confirmed its lognormal distribution. The Bayesian analysis of DCs is shown in Table 1.
3.3-C. CAPSE. EAIMRESThe common cause failures are dependent, multiple
failures arising from a common initiating cause. The main categories of CCFs considered in the analysis are
i) Design Errors
ii) Manufacturing Errors
iii) Test and Maintenance Errors13
iv) Effect of External Environnent
As far as practicable, care is exercised to 3se«p the process and safety systens independent of each other and safety systens anong themselves to nininise the incidence of CCFs. Special qualification procedures where applicable, have been adopted for the components to viths-4nd the connon causes such as earthquake, accelerated environment following an accident like LOCA etc. $-factor rtel has been used for the analysis of CCFs and the plant specifics have been incorporated.
3.4 SAFETY AMD-RELIABILITY ANALYSIS
Fault Tree Analysis has been extensively used and safety and reliability analysis of various IEs and ESFs applicable to NAPP has been performed to obtain both1 the probabilities of failure on demand as well as spurious failure rates. This helped in the design evaluations and also, ill decision making regarding safety issues. Sone design modifications as a result of the analysis are outlined here.
i) Reliability inprovenent in the design of interlocks and D,0 condensate lines in the Reactor Building Isolation System to effectively isolate the containment.
ii) Design modifications in ECCS to account for the interdependence of various stages of injection,identification of components to assist in improved procurement and test procedures
iii) Comparative evaluation of designs for secondaryshutdown system to obtain optimum configuration from the viewpoint of simplified design resulting in high availability, reduced test and maintenance efforts and adequate safety
iv) Provision of isolating valves in the interface of moderator circulation system with liquid poison addition systems to reduce the frequency of loss of moderator
These modifications( Table 2), interalia, have been implemented to improve the system reliabilities contributing to an overall risk reduction. The results of reliability analysis of the various ESFs are ahown in Table ЗА. The frequency of failure in respect of various IEs is shown in Table 3B. In order to account for the variability in data, an Uncertainty Analysis has been carried out assuming a lognormal distribution for the failure data and error factors as listed in [4]. The details of Fault Trees and other calculations of the reliability analysis are given [5] and these are also included in the appendix. A distribution is obtained for the Top Event using a Computer Program based on Monte Carlo simulation and the 5th, 50th(median) and 95-i:h percentile points are obtained, for various reliability indices. The data on HER and human responses to accident situations is inadequate in our context. However, components prone to human errors and their effect on system functioning have been identified in the analysis e.g. the valves in Feed Vater System.
4 ACCIDENT SEQUENCE IDENTIFICATION
In view of the 'Defense in Depth* approach applied in the design of reactor systems, an accident situation arises only when an IE is coupled with the unavailability of one or more ESFs. Thus a dual or multiple failure is necessary for an accident to occur. These dual or multiple failures are known as Accident Sequences in PSA parlance. The significance of accident sequences can be understood from the definition of risk as follows:
Risk *• Probability of occurrence*Consequences
In a HPP, the probability of occurrence signifies the probability of all the accident sequences and the consequences are measured in terms of radioactivity releases. Thus risk from a NPP
IS
• IProbability of accident sequence*Consequences All accident sequencesand the overall risk can be quantified if we can identify all the accident sequences and evaluate their consequences. In level I PSA, the requirement is to identify all the accident sequences and relate them to component failures and human errors. In the present study, accident sequences relevent to NAPP have been identified' using Event Tree methodology. Event Trees for all the dominating IEs have been drawn the details of which are given in the following sections.
4 1 ACCIDENT..SE •10 > iCE-QBABIIFICAIIQN
The accident sequence as identified by the Event Tree may be expressed as follows.
; Accident Sequence-Initiating Event * ESF(s) Failure
Obviously, in an accident sequence there are other terms implying the success of other systems; however these
i can be ignored since the success probabilities are approximately 1.0. In terms of probabilities, the accident sequence probability may be written as
P ” PIE*PESF1*PESF2*.....
where PIEis the frequency of the Initiating Event and p_ is the probability of failure on demand or the unavailability of that particular ESF obtained from the respective Fault Trees. In order to obtain correct accident sequence probability, the correct probabilities of the individual factors must be used, incorporating any dependency among the factors. Thus various system probabilities are treated as conditional probabilities and expressed as
PESF1 " PESF1/IE and PESF2 " PESF2/ESF1.IE
where PESFi/ie denotes the probability of ESF1 failure given that the initiating évent has occurred and so on. A simple multiplication of the probabilities can only be used
when the various factors are independent. The dependencies, if any, are included in the discussion on the individual Event Trees.
4.2 L0SS QFCQQLANT ACCIDENT(LOCA1 JEELS.
The different locations in a PHWR PBT piping where XiOCAs can occur are shown in figure 1. Unlike in PVRs and BWRs the diameter of the largest piping in PHWRs is much smaller, thereby limiting the radioactivity discharge rate in case of LOCAs. The coolant activity discharged into the containment is smaller due to the smaller PBT inventory in PBVRs. Depending upon the ESFs required to act upon, LOCAs can be divided into
1. Large LOCA-e.g. PBT header rupture
2. Medium LOCA'-e.g Endfitting failure, Feeder rupture etc.
3. Small LOCA- Instrument tube rupture, SG tube rupture etc.
Small LOCAs(the break area ~<0.1\ of 2A, A being the area of the largest diameter piping) handling is within the capability of pressurising pimps to start with and depending upon the storage tank very .low level( which. definitely is indicated) small LOCA handling systems can take care of the situation. For breaks at some locations like pressure tube and steam generator tube, the recirculation phase of small LOCAs may not be actuated as no water gets collected in the FM vault. This may lead to ECCS injection/recircUlation. Bowever, there is sufficient time available for the operator to take action and manually control the course of the initiating event. If there are clad damages, these are limited and significant release of activity is not expected. The various scenarios that follow depending upon the break location and the progress of the IE depending upon the operation of the ESFs is discussed in detail in the subsequent pages.
Large LOCAs are characterised by break areas greater than 10\ of 2A. These lead to fast depressurisation of the PBT which leads to subsequent ECCS injection and
recirculation. Because of the speed with which the IE propagates, operator actions are not expected/anticipated and accordingly all the ESFs that have to be operated axe designed to cut in automatically. Because of the fast depressurisation and subsequent low PHT pressure ECCS cuts in and continues to provide cooling such that core damage if at all is limited. The course of the IE with the associated ESFs is discussed in detail in the later pages.
Medium LOCAs (figure 4),break area between say 0.1\ of 2A and ~10\ of 2A, are characterised by a slow rate of depressurisation of the PHT system, especially in the lower end of the break sizes of the medium LOCA breaksize spectrum. Because of this the reactor remains at full power after the LOCA occurs for a sufficient period(**1 to 2 minutes) adding a good amount of thermal energy to the system. In addition, the ECCS flow may not be enough, during the initial phases and a sustained low flow condition(stagnation) in the fuel channels is expected which can lead to singificant clad damage. (In case Reactor Building does not get pressurised to initiate crash cooling of the boilers to allow continued ECCS flow through the core,(it is essential that depressurisation of the PHT system by blowing of the secondary side of the boilers be carried out manually by the operator) If this operator action is not carried out there cçn be significant clad damage. In NAPP a provision has been made to convert this type of situation into large LOCA by opening a pair of parallel valves during the light water injection phase.
4.2.1 LARGE BREAK LOCA
The ET for the initiating event large LOCA is as shown in figure 2. It is important to note that the void coefficent of reactivity is positive in a PHWR and this warrants a fast shutdown in the present case. Since the moderator is not dumped on a reactor trip, the presence of a large volume of moderator which is cooled by an independent circuit of pumps and heat exchangers acts as an ultimate heat sink. Various studies [6],[7] indicate that no fuel melting is likely to occur even il ECCS fails on LOCA. Thus fuel melting in a PHWR can be postulated to occur when there is a breach in the moderator circuit in
conjunction with LOCA and ECI failure. Thus, the probability of failure in caee of accident sequences 2 and 7 would be further multiplied by the probability of loss of moderator. The other accident sequences are related to the failure of containment functions e.g. reactor building isolation« reactor building cooling etc. It is recognised that RBI system is extremely important in case of activity leaks and as mentioned in section 3« care <.«s been exercised in engineering reliability into the system. Further, double containment is provided to check activity leakages. RBC function is performed by i) Suppression Pool which is a passive system and ii) Fan Cooling Units. In Indian PHWRs, all high enthalpy systems including PHT are located in.a volume called V1 which is connected to rest of the volume V2 of the containment by means of a vent system via the suppression pool water. Any leakage from volume V to V2 which are seperated by leak tight walls and floors may marginally affect the efficacy of suppression pool, for which the probability is low. The vapour suppression pool would absorb about 25 to 30% of the energy released from PET system and also trap a significant part of the activity. The RB coolers located within the containment bring down the pressure following the accident.
.SMALL..BREAK LOCA •Small Break LOCA, as mentioned before, is defined as
the break corresponding to upto 0.1% of the double ended or about 1/2* in the PHT, which is more likely due to an instrumentation tubing etc. and is within the Pressurising Pump capability. Here, consideration is given only to those breaks which result in spillages in FM Vault/Boiler Room area. Steam generator tube breaks and pressure tube ruptures are considered seperately. Due to the high stored energy and significant decay heat for the first few minutes, it is essential that pressurising pumps operate for about half an hour of the event.. Since these pumps are on class IV, the failure of class IV supply in this duration would affect the core cooling capabilities. Even though the FM pumps start in case of class IV failure, the flow delivered by these pumps would not be adequate to meet the core cooling requirements, resulting in a significant rise in clad temperature. Since the system goes on loosing
inventory, the pressure falls and ECCS would be actuated eventually. But till such time, due to inadequate coolinq, some clad damage might have already occurred.
However, a Small LOCA Handling System(SLHS) has been provided in NAPP wherein, on sensing a low level in the storage tank and at PHT pressure greater than 55Kg/cm2, D20 is injected into the PHT storage tank from the ECCS accumulators and subsequently, the spillage is recirculated to allow enough time for operator action to detect and plug the leak. Even with class IV power available, failure of SLHS is also likely to lead to the same situation as described above. However, if small LOCA injection occurs and recirculation fails, the situation is less severe as the stored heat from the fuel has been removed and the clad temperatures are low. In this situation, high pressure ECCS injection is not possible as the D20 in the accummulators got already transferred to the storage tank. The efficacy of SLHS in situations where a small break may propagate into a medium break is also questionable since’ the accummulator water would not be available for emergency coolant injection. It may be worthwhile under the circumstances to transfer initially D20 from outside tank and subsequently from the D20 accummulators. This would ensure availability of ECCS during injection phase. The event tree for small break LOCA is shown in figure 3.
4.2.3 STEAM GENERATOR TUBE RUPTORE
Upon the rupture of a steam generator tube, there will be an increase in the affected SG water level with a decrease in the D20 storage tank level. Unlike in RAPS and MAPS boiler level control action is on the individual boiler level and steam flow rate from the boiler. The level controller, thus, tries to maintain the boiler level. However, as the PHT system is loosing water, the storage tank level dips to very low value and this initiates a reactor trip.
As the system pressure is greater than 55Kg/cm2 and D20 storage tank level is low, small leak handling system gets actuated. The D20 required for this system is drawn initially from the ECCS D20 accumulators. When the level in
these is low, a D20 storage tank outside the reactor building provides the required makeup water. This can continue until the D20 in the 3211-TK-1 gets exhausted.Before this water is exhausted, the leaky SG should be identified and isolated. The positive indication for SG tube leak is high activity in feed water(or steam). As the steam activity is continuously monitored, it is possible, by operator action, to isolate the leaky steam generator.
If the leaky SG is not promptly isolated, the PHT system starts loosing water and hence pressure. ECCS accumulators, being empty, are of no use. Due to reduced cooling, the clad temperatures start increasing(due to decay heat). Eventually light water injection will start and stabilize the system with light water recirculation. This IE is thus, more or less identical to the small break LOCA in terms of the effects on the core and PHT but may lead to a large scale contamination in the turbine building etc.
4L-2 ^-PRESSURE. TUBE ^CORRESPONDING CALANDRIA TUBE RUPTURE
The PHWR comprises a large number(306 at NAPP) of pressure tubes, each about 5.43 meters long having 83mm diameter and each is surrounded by a concentric calandria tube. A large inventory thus enhances the probability of failure and as described in figure 1, this would be a case of LOCA inside the core. Based on the operating experience of Canadian and Indian PHVRs, a failure rate < 1.0*10’4/year per pressure tube is obtained(which is corroborated by the failure data usually used in the pipe rupture calculations). With respect to the break size, effects on the PHT system, the pressure tube failure is equivalent to a medium LOCA. However, a significant difference exists in the present case since the failure may induce large reactivity effects due to dilution of borated moderator with PHT heavy water in addition to the positive reactivity effects due to crash cooling, voiding etc. The fast reactivity changes would be compensated by the simultaneous actuation of both the primary and secondary shutdown systems and the slower dilution of moderator can be overcome if the Automatic Liquid Poison Addition
System(ALPAS) is effective in injecting the boron into the moderator. The efficacy of ALPAS in the prevailing conditions needs be confirmed.
4-.-2_. 5-MAIN STEAM LINE BREAK
This IE is somewhat identical to the Design Basis Accident(DBA-Large LOCA). However« the energy released into the containment, the subsequent pressure peak and temperature rise would all be in the secondary containment which is not designed for pressure retention and this is vented to the atmosphere by the opening of the blowout panels. The probability of this IE is also expected to be greater than large break LOCA. The effect on PHT system in terms of depressurisation would be very fast, due to crash cooling but the pressure would be restored if there is no leakage in the primary system through SG tubes. The event tree for steam line break without any steam generator tube failures is shown in figure 5A. Boiler inventory would also deplete fast due to crash cooling and Fire Water System(FFS) would have to be actuated by the operator when the Boiler pressure falls to about 3.7Kg/cm2(Both the boiler feed pumps may trip due to overspeeding and AFWS may not be able to provide adequate cooling). The reactor cooling may continue in this mode or SDC system may be valved in. In case FFS is not available, a fast operator action is warranted to bring in SDC system Within about 20 minutes before the boilers dryout. If SDC fails under these circumstances, it would result in core damage. In case ECCS fails, 20-25% voiding is expected resulting in an uncertainty in the effectiveness of the thermosyphoning process to cool the core and may cause clad.damage. If FFS also fails, a large scale clad damage is expected though the presence of moderator may prevent a core melt.
The reaction forces coupled with a high pressure differential across the SG tubes, may induce multiple failures in SG tubes and the event tree for this is as detailed in figure 5. Thus MSLB may result in medium/large LOCA too and it is essential to qualify the SG tubes for such impact loading.
4.3 FEED WATER SYSTEM РАТТ.ПИЕ
Thé event tree for this IE ie shown in figure 6.Feed Water System failure can be due to a) failure of boiler feed pumps(BFPs) or b) rupture of feed pipe. IN case of failure of BFPs reactor trips on high PHT pressure or low steam generator level. Auxiliary BFPs start on auto. Reactor can be cooled down further, if it is warranted, by the SDC pumps.
Feed Water pipe break downstream of the check valves near the SGs leads to a situation where the break can neither be isolated nor auxiliary feed to the SGs be supplied. This leads to a complete blowdown of the affected SG. This is likely to induce SG tube failures due to thermal shock as well as loading of the tubes due to vapor bubble formation and collapse on the secondary side of.SG . However, the length of the piping( and hence the probability) that results in such failures is small. This SG can, by operator action, be isolated on the primary side(due to continuous monitoring of steam activity in the individual boilers).
Feed water pipe breaks upstream of the check valves near the SGs can be isolated(The check valve acts as an isolater on one side of the break). Even if the break cannot be isolated from the otherside this situation does not lead to loss of SG inventory. If the operator valves in the auxiliary feed line, normal cooldown of the PHT can be resorted to and later SDC system can be valved in. If the auxiliary feed line cannot be valved in, secondary steam relief is required and SDC system has to be valved in for entering into a stable state. In case SDC system cannot be valved in Fire Water injection to Boilers is required. If Fire Water System also fails, cooldown of PHT is not possible.
If secondary steam relief is not realised, PHT gets pressurised and this will lead to either PRV opening (and hence LOCA) or pressure tube rupture.
1...4 CLASS IV-POWER SUPPLY FAILUREClass IV is the nain supply provided both by the grid
and generated by the station. This IE is significant in our context due to high frequency of class IV failure. Based on the operating experience, it is observed that the frequency is > 1.0/year which is relatively high since it is usually 0.1 to 0.3/year in many other countries. Interdependence( common cause failure) of station supply on grid fluctuations and vice-versa is a significant factor in determining the frequency. At NAPP in the Northern Grid, the frequency may be of the order of 2/year.
The ET and the various ESFs required to mitigate the effects of the transient are as shown in figure 7. The Secondary Steam Relief(SSR) is provided by a redundant configuration comprising steam discharge valves(SDVs) and boiler relief valves and the probability of failure of this system would be low. On class IV failure, secondary cooling is provided by auxiliary feed water system which is further backed up by the FFS driven by three dedicated diesel pumps. In case of loss of all secondary cooling, SG holdup would last for about 20 minutes and by this time, the. shutdown cooling system must be valvèd in. Similar criteria is applicable to valving in of FFS in case AFWS is not available.
Accident sequence 14( fig. 7)is critical which depicts the failure of both class IV and class III leading to the situation of Station Blackout. The station batteries are usually rated for a duration of 20 to 30 minutes and this sets a limit to the available time within which the power supply must be restored. The probability of restoring the supplies in 30 minutes is low. NUREG-1032 of USNRC quotes a median value of restoring time for offsite power as 0.5 hours and repairing time of DG as 8 hours. In case of an extended Blackout, it would result in a critical situation since AFWS, SDC would not be available. Also, the supply to control and protective systems(class I) would be lost, resulting in a total loss of minitoring and indication of the plant status. It may be essential to crash cool the primary which would result in large scale
voiding in the system. However, with secondary cooling available, provided by the PFS, thermosyphoning may be effective. The reliability of FFS is thus crucial for mitigating the station blackout situation. In addition, FFS is essentially a low pressure system and manual actions are involved in valving in of the same. In case of a station blackout, which is definitely an unusual situation,the stress on the operator is likely to be high and the time available is also "half an hour. Hence the probability of human error would be significant and the same is considered as 10’2 . However, sicne FFS is the only safety system available, the chances of recovery would be high and this system could be valved in after some delay.
A ._5_- COMPRES SEP AIR SUPPLY SYSTEM FAILURES
The compressed air is an important support system required in instrumentation and control for valve operations, pneumatic process monitoring components etc. The system comprises mainly of compressors and dryers and dry air is supplied to a common header through air receivers which act also as air reservoirs for 5 to 10 minutes. In the reactor building, three air receivers have been provided to provide triplicated lines for air supply to safety system components. These air receivers further act as reservoirs and in case of losa of compressed air supply from the compressors, the capacity would be available for 10 to 15 minutes. Utmost care is exercised in safety system design wherein, the air operated devices would assume fail safe operation and no continuous air supply would be required for further operation. In case where failure of compressed air may lead to unsafe situations, local air receivers have been provided to mitigate the sitiation. Thus, the reliability of compressed air system would be adequate if the local air receivers are properly maintained so that they act as proper standby components. It would be essential to provide pressure gauges in the local air receivers and institute periodic maintenance. At this level of operation, compressed air system failures may not affect the reactor safety.
A. fi- PPEL HAUDLING ГА1ЫтЕа
During refuelling operations! «Fuelling Machine is a part of the PHT systea and foras an extended boundary. Various failure nodes arising froa the FM operations are considered as followsa). Fuelling Machine On Reactor
In this operation, there is hydraulic connection between the nagazine and the reactor end fitting. All the DjO leaving the aagazine has to return to the priaary systea through the coolant channel. Thus, any breach in the FM D20 circuit would result in LOCA. However, based on the reliability analysis, the contribution of this interface LOCA is negligible,b) Fuelling Machine Park
In this node, FM is in the transit between the reactor and the fuel transfer port and could be carrying spent fuel bundles in the aagazine. A failure in the D20 control systea would result in spent fuel bundles in the aagazine not getting cooled.
The other possibility nay be that the seal plug and sheild plugs are.not seated properly after the refuelling operation and the FM is renoved froa the channel after the leak detection test fails to diagnose the leak. This aay result in the ejection of seal and shield plug leading to endfitting failure and ejection of áll the fuel bundles froa the channel.c).On Fuel Transfer
Xn this node the FM is claaped to the fuel transport and there is a hydraulic connection between the aachine and the fuel transfer port. Failure of D20 control systea would result in fuel bundles being deprived of the cooling.
The frequency of fuel handling failure is estiaated as 1.0*10°/year resulting in radioactivity leaks into the containaent. This IE would be significant only when the RBI systea fails. Thus, the probability of this accident sequence is less than 1.0*1 O'*8/year.
■4.? LOSS OF REGULATION
26
The regulating system is designed to control the reactivity changes and thereby, providing a control on reactor power and preventing any flux peaking etc. The loss of regulation Accident(LORA) amounts to withdrawl of control and absorber rods used for reactivity control. The regulating system is based on triplicated instrumentation channels and the movement of any rod is controlled by the individual servo motors. Thus failure of the servo motor would affect a single rod only. In case of a failure in any regulating channel, the same is rejected and the control is transferred to an operating healthy channel. Thus, a single channel faulure coupled with the failure of the transfer circuit would result in loss of regulation in a single control channel amounting to about 5mK. In case of the failure in all the regulating channels, due to a ■ common cause, it is a LORA involving about 16mX reactivity ; insertion. However, the design of the reactor ' regulating system limits the reactivity addition rate to a maximum of 0.03mK/sec per control group. Thus, in all cases of LORA involving control and absorber rods, the maximum rate of reactivity insertion would be limited to 0.06mK/sec. Also, each of the two reactor shutdown Systems have enough depth and speed to terminate all reactivity insertions. However, reacticvity insertions would lead to high pressure in the PHT system. If the pressure relief system is not available, the situation may lead to pressure tube and calandria tube: failure. This would result in the crash cooling of PHT system. Positive reactivity introduced may exceed the worth of the shutdown systems and the efficacy of ALPAS would also be questionable. The frequency of this accident sequence would, however, be "I.0*10’*/year.
4.8 FLOW BLOCKAGE IlLAHY. CQPLAHT-ASSEMBLY.
Operating heat fluxes, even in maximum rated channel, are such that there is sufficient burnout margin. In fact flows upto ”18\ of the rated flows[5] in the channels can be tolerated without any fuel damage. Bence flow reductions even of sufficient magnitude do not pose any problem.
Ofcourse these result in high channel teaperature «rich causes a setback of the reactor. Thus only flow blockages( or severe flow reductions) are of concern. These can be due to suspended objects of 'considerable size in the PHT system. Normally objects left in the PHT system during construction can be detected during commissioning. Water chemistry in PHWRs is well controlled and this minimises corrosion and thus buildup of suspended particles. During refuelling operations, some paddings etc. can get dislodged from the fuel bundle. These are unlikely to lead to full channel blockage. Broken parts from rotating components, like pumps, can also cause some kind of flow blockage. Similarly parts of valve bodies, which if they get dislodged and get deposited elsewhere,, can be a cause for flow blockage. However in the operating PHWRs in the world, there is not even a single event of this type reported so far(eventhough partial blockages have been reported). If flow blockage occurs, there is no safety system to take care of. However, moderator can act as a heat sink and the damage is limited to the affected channel only.
4.9 ACTIVE. PROCESS..WATER SYSTEMAPW system failures of short duration are unlikely to
have any impact on the safety of the reactor. In case of failures of long duration, the reactor automatically trips as this system affects the cooling of thd PHT pump motor, moderator pump motor etc. If emergency APW system gets valved in, moderator cooling can be maintained.
To keep the PHT system solid( to compensate for the shrinkages) the pressurising pumps have to cut in and continue to operate while the auxiliary feed water system continues to cool the PHT system.If the pressurising pumps do not cut in, D O injection of ECCS can occur. If AFWS does not cool the primary, this might lead to high PHT pressure and consequent IRV opening which if fails to close again is a LOCA situation.
In case emergency APW system fails, moderator cooling is affected, the remaining accident scenario remains unaltered i.e. AFWS operation to remove the decay heat, pressurising pumps/D^O injection to keep the PHT solid. If
all these systems operated as intended, the situation is stable. If the pressurising pumps and the DO injection fail to come, there may be voiding in PHT system and if the voiding is substantial clad failures may occur. In case auxiliary feed water system does not come in, PHT gets pressurised and this leads to IRV opening and hence LOCA. The event tree for this IE is shown in figure 8.
Д.-ДО HOH~ACTIYE HIGH PRESSURE PROCESS WATER SYSTEMThe event tree for this IE is shown in figure 9. If
the loss of NAHPPW system is of short duration, it does not affect the safety of the reactor or its associated safety systems. If this failure is of significant duration, systems like DCs are affected due to the nonavailability of jacket cooling water system. Under this situation, class IV failure of significant duration will result in a condition similar to Station Blackout.
In case class IV is available, as the main and auxiliary boiler feed pump cooling is affected, secondary steam relief is required to depressurize the PHT system or else IRV may open, close, open again to relieve the excess PHT pressure and this may ultimately result in LOCA. If SSR is avilable, to keep the PHT solid, auxiliary main feed( pressurising pump operation) is required. In case this is not available, SDC can be valved in which if fails to cut in, is likely to lead, to fuel overheating and subsequent clad failures. If SDC cuts in, the consequences will be less. If auxiliary main feed is available, and SDC is available, a stable state is reached. If SDC does not come, fire water has to bè injected into the boiler to continue cooling of PHT. However, it is not certain whether enough : cooling of PHT system is provided and this may result in some clad failures. If fire water does not get injected, PHT gets pressurised and IRV opening may take place and this is going to be a delayed LOCA.
з.-SYSTEM DEPENDENCIESAs mentioned before, various ESFs have been designed
to operate independently- both among themselves and also, with respect to the IE. However, some form of dependency has been observed. Normally, it is expected that various components and equipments are designed to operate in the accelerated environmental conditions generated by the IE. In case of LOCA, an environment of high temperature, pressure, radiation and humidity prevails in the containment and various components e.g. pump seals, pump motors, junction boxes, coolers etc. are susceptible to it. Further, the presence of moderator as a heat sink is very important in case of PHWRs to prevent fuel failures' if ECCS fails büt the efficacy of the system need be ensured when a significant amount of energy is added into the moderator. The reliability of the moderator pumps, flange joints etc. will be affected in such cases. The effects of such common causes have been incorporated in the accident sequence quantification. In addition, intersystem dependencies have been considered in developing the event trees. Effect of the failure of the support systems on subsequent progression of the event trees have been incorporated( eg. DCs are not considered in NAHPPW system initiating event ET) where ever found necessary.
fi-PQUIHAXINfi, ACCIDENT.SEQUENCESThe overall number of accident sequences identified
through Event Tree analysis is very large as described in the previous section. However, based on the probabilistic and analytical assessment of the consequences of the accident sequences; a relatively small number of accident sequences which contribute to activity release in to the containment are presented in the table 4. These accident sequences( excluding those resulting in coolant activity only i.e. sequences 2,3,16 and 19) are expected to result in core damage and are designated as Dominating Accident Sequences. The extent of core damage is not assessed at this stage and the same will be the next phase of this study wherein, the consequences in terms of the effect on the core, radioactivity released, effect on the containment and its failure modes etc. would be discussed. As mentioned
before, the presence of moderator in the core prevents fuel eelting in case of LOCA and unavailability of the emergency core cooling systems. Thus, all accident sequences originating from LOCAs, MSLB and others resulting ultimately in LOCA would cause fuel failures only if the moderator is not available as a heat sink. Thus, accident sequences resulting form station blackout(9 and 10) and from active process water failure which provides cooling to moderator heat exchangers, contribute to fuel failures as such and in all other cases, the frequencies would be multiplied by the probability of loss of moderator as a heat sink. The frequency of core damage, thus calculated, is 1.5*10'S/year. The major contrubution is from station blackout related events( A decision has been taken to incorporate a third DC which reduces the emergency power supply unavailability by a factor of 3, leading to a core damage frequency of '5*10"e/year). An uncertainty analysis has been carried out for all the dominating accident sequences( table 5) and the error factors are further propagated to obtain a distribution for the frequency of the core damage as shown in the table 6.
7 ACCIDENT- SEQUENCES-SENSITIVE TQ..HUMAN ERRORThe boiler feed water system is backed up by the AFWS
which automatically cuts in when main feed pumps trip or class IV failure occurs. As a result of TMI studies and recommendations, emergency feed water is provided to boilers from the fire fighting system. This is essentially a low pressure system and thus, would necessitate a crash cooling on the secondary side to reduce the pressure and prevent a SG dryout before fire water is injected into the boilers. Thus, in nccident sequences involving loss of main and auxiliary feed water, a reasonably fast operator action(20 t 30 mts) is warranted to provide secondary cooling. Funner, SDC too is a low temperature system and is reliable if valved in when PHT temperature is <150°C. In case all the secondary cooling is impaired, a crash cooldown of the PHT is essential to valve in SDC. This is a high stress situation and the available time is short and the information available to the operator also may not be adequate resulting in a high human error probability. In fact, so far, training is with respect to failures in
various process systens only which oust be extended to accident sequences.
8 relative importance of initiatingSYSTEMS
¡Vis i»цз^шр. mmAccident sequences are related to the IEs and the ESF
failures which are further expressed in terns of the component failures and the human errors. This provides a measure to reduce the core damage frequency. The dominating XEs considered for the analysis have been explained in section 2 and the ETs were constructed for these IEs to obtain all the accident sequences and then the dominating accident sequences. The contribution of the various IEs to the dominating accident sequences is shown in the table 7. In case of an ESF, the importance function is expressed in terms of the core damage frequency reduction worth and is defined as the ratio
IAir_dominatinq_jequences_not containing a particular ESFCA11 dominating accident sequences
which, in other terms, is a measure of the effect of the reliability improvement in the particular ESF as shown in the table 8.
The authors are indebted to Dr. R.N. Kulkarni of Atomic Energy Regulatory Board for his immense help in preparing the required computer programs fox carrying out the uncertainty evaluations. Thanks are also due to the various system designers at NFC for useful discussions. The various comments received on the draft version of this report from the organisations BARC,HPC and AERB were appreciated and have appropriately been considered in this version.
1. WASH-1400, Reactor Safety study, USNRC(1975)
2. Gernan Risk Study
3. Safety Series no.S0-SG-D11,Safety Guides -General Design Safety Principles for NPPs, IAEA, Vienna
4. National Reliability Evaluation Progran(NREP)<1982)
5. NAPP Safety Report Voluae XX*6. CANDO Safety Research -A Status Report, Second Annual
Conference, Canadian Nuclear Society, June,1981, Hancox, W.T.
7. Safety Research for CANDO Reactors, IAEA. Technical Connittee Meeting on Theraal Reactor Safety Research, Moscow, Dec,1981, Hancox, W.T.
8. Application of PSA in licensing of PHVR, Tareny E.M.,Presented at the XAEA-AERB workshop on Safety Analysis held at Bombay,5-16 May,1986.
TABLE It BAYESIAN ANALYSIS OF DEMAND FAULURE8 DATA ON DG8 AT RAPS
PRIOR POSTEROIR
Vos O.Ol 0.0433
A • _ 0.03 0.03330 SO
X • 0.09 0.6260 95
M -З.Э2 -2.93
0 0.673 0.943
SAFETY SYSTEM
AVERAGE FAILURE RATE/
UNAVAILABILITY
MAJORITYCONTRIBUTORS
CRITICAL COMPONENTS
AND CONTRIBUTIONREMARKS/
RECOMMENDATIONS
MODIFIEDVALUES
EMERGENCY CORE COOUNG SYSTEM
«x tÓ3/dLIGHT WATER. MX
4.5 X 1Ö3
RECIRCULATION17X1Ï3
RUPTURE DISC 2 * Ml MV-52 1 X mlMV-24 1 к Ml
MV-31 1 X ÎÔ
CHANGE M RO DESIGN PR. REDUNDANCY IN MVs. ENVRNMENTAL OUALFICATION OF MVsAND PIMPS.
2.5 xM3
REACTOR BUILDING ISOLATION
8.x 10/d BYPASS LINE4 X 10"3/ 4 CONDENSATE RETURN LINE4 X 10^/ d ;
DAMPERS 7314 0M5 ORDM6 - 2x10vd teach)VALVES-Ixl^/d (..chi
INTERLOCKING THEOPENING OF 734 DM-13 ANO OM-14 WITH THE aOSURE OF DM5 i DM«. REDUNDANCY M CONDENSATE RETURN UNES
<1xM3
ELECTRICAL POWERsupply ¡missii
Щ CLASSE1-2/yr.SxlïVd
CCF DUE TO OFSIGN,MAlNTENA4a FIÆL OH SYSTEM ETC
DGs - 3x1? (CCF) 'INDEPENDENCE AND STAGGARO MAINTENANCE.
3x1?
MODERATOR SYSTEM9 DROP N LEVEL ñ) CALENORIA
ISOLATION
2V.
9xW3/d
SHM t REG. ROO COOLMG SYSTEM ACTUATION CIRCUIT
LARGE NO. OF BELLOW SEAL VALVESMVs » 3 x lôV d (each)
MONITORING OF MV ACTUATION CIRCUIT COMPONENTS.
SxM3
REACTOR PROTECTION SYSTEM
INSTRUMENTEDREÜEF VALVES
2x10/d
<10/d
MSTRUMENT ATION CHANNELS CCF
INSTRUMENTATION CHANNELS CCF
REDUNDANCY M ТИР PARAMETER AM)SHUTDOWN DEVICES. .
?
TABLE SAFETY SYSTEMS MAIN FAILURE MODES & MODIFICATIONS
TABLE ЗАi FAILURE PROBABILITIES OF SAFETY SYSTEMS
8.No SAFETY SYSTEM DEMAND FAILUREPROBABILITY
ERRORFACTOR
1 Emergency coreCooling 3.5*10'3 2.0
2 Reactor BuildingIsolation 2.0*10'* ¡2.4
3 Emergency PowerSupply 3.0M0'3 1.Э
4 Reactor BuildingCoolers l.OMO'3 3.0
S Reactor Protection 2.0*10'* 4.06 Auxiliary Feed
Water 1.0*10'3 1.8 •7 Fire Fighting l.OMO"3 3.08 Small LOCA
Handling 2.0M0"2 3.09 Moderator System 3.0M0"3
TABLE ЭВ: FAILURE FREQUENCY OF INITIATING EVENTS
S .NO INITIATINGEVENT
FAILUREFREQUENCY(уr"1)
ERRORFACTOR
1 Large Break LOCA 1.0*10"4 102 Medium Break LOCA 1.0*10"2 33 Small Break LOCA 1.0*10"2 34 • Class-IV Power
Supply 1.0 25 Feed Water System 0.5 1.76 Main Steam Line
Break 3.0*10° 37 Active Process
Water System 1.0 1.58 Non-active High
Pressure Process Water System 0.2 2.1
9 Compressed AirSystem 2.6 1.3
10 Moderator Level 2.0 1.211 Steam Generator
Tube Rupture 1.6*10° 3
37TABLE 4i DOMINANT ACCIDENT SEQUENCES - CONSEQUENCES
S.NO ACCIDENT SEQUENCE FREQUENCY(умг"1)
CONSEQUENCES/REMARKS ¡IE E8Fe(Fa1L«d>
1 ML ECR 2.0*10"5 Clad failures expected. May lead to delayed RB pressurisation depending up on the extent of MU reaction.
2 ML RBC 1.0*10’S RB remains pressurised, high leak rates expected. No core damage
3 ML . RBI 1.0*10 5 All coolant activity released to environment. No core damage
4 ML ECI 1.5*10*5 Significant clad damage expect -ed leading to MU reaction &H generation resulting in contain -ment pressurisation. Fuel melting not expected due to presence of moderator.
S SL SLHSI 1.0*10*4 Uill lead to clad failures.MU expected when ECI comes in contact with clad at high T.H generated may lead to conr tSinment pressurisation.
b SL RT 1.0»10*e Even SLHS may not be available since the same signal is used for both. Significant clad damage(Studles required)
7 SL CLASS-IV 1.0*10*5A
Voiding occurs. SignificantClad failures expected.
в CLASSIV
CLASS'-! 11 <1.0*10"3 If exceeds 0.5 hours results in clad damage.Recovery of off site power considered here.
9 CLASSIV
CLASS-11IfFF8 1.0*10*®
m
PHT pressure singal not available. Spring loaded RVs open. Otherwise pr. tube rupture. NO ESFs effective to cool the core hence core melting likely.
10 CLASS CLASS-1II,HE 1.0*10*' Same as above11 CLASS
IVCLASS-1II|SSR <1.0*10*7 Same consequences as above.
12 CLASSIV
SSR <1.0*10*4 May result in №.. All otherESFs including moderator are available. It will result in significant clad damage.
TABLE 4 continued fron previous page
S.NO ACCIDENT SEQUENCE FREQUENCY(year’1) CONSEQUENCES/REMARKS
IE E8Fs(Fa1Led)13 FW 88R <3.0*10*5 ML. All ESFo Including aodera-
tor systea are available.14 FW AFUS &
HE(10‘2)3.0*10’e Saae as above.
13 FW AFWSf8DC i HE(0.9> 4.3O10’7 ML,
But ECC8 nay not be effective since crash cooling is not available.
16 MSLB 3.0*10’3 All coolant activity released Into the sec. containment. High leak rates expected.
17 MSLB ECR 6.0*10 e Clad damage evulvalent to ML/LL depending upon the number of tubes falling. All activityInto the sec. containment.
18 MSLB EC1 4.3*10’® Significant clad damage.19 MSLB FF3 & HE 3.0*10’7 LOCA through 1RV. Only coolant
activity released.20 APU EAPWS 1.0*10 * Some clad damage may occur.21 APW EAPWB & EC1 1.0*10‘7 Clad damage, heavy voiding of
PHT expected.22 APU EAPWS i AFUS 1.0*10 7 ML. No moderator cooling.23 NA
HPPW8 CLASB-1V2.0*10’* Same as station blackout.
24 NAHPPWS SSR
<2.0*10’® ML through 1RV. No crash cooling since SSR Is not available.
23 NAHPPWS SDC & FF8
2.0*10’7 LOCA through IRV
TABLE S» DOMINANT ACCIDENT SEQUENCES - UNCERTAINTY ANALYSIS
8.No Accident Sequence Medianrrequency<Yr"1)
ErrorFactor
1 ML & ECR 6.0*10"® 3.34 ML & ECI 4.3*10"® 3.35 SL & SLHI 3.0*10"7 3.66 SL & RT 3.0*10"® 4.7'7 SL & Class IV 3.0*10"® 4.7В Station Blackout 9.0*10"7 2.29 Blackout & FF8 1.0*10"® 3.9
11 Blackout & SSR 1.0*10"7 6.012 Class IV & SSR 3.0*10"7 3.713 FW & SSR 1.3*10"7 3.714 FWyAFWS & HE(.Ol) 1.3*10"® 3.4IS FW,AFWS,SDC S.HEC.9) 1.4*10"® 3.417 MSLB & ECR l.B*10"® 3.318 MSLB & ECI 1.4*10"® 3.320 APW & EAPW8 3.0*10"® 3.021 APW,EAPWS & ECI 3.0*10"10 3.622 APW,EAPWS & AFW 3.0*10"® 4.823 NAHPPWS & Class IV 6.0*10"7 3.624 NAHPPWS & SSR 6.0*10"® 3.723 NAHPPWS,8DC & FFS 6.0*10"10 3.4
* This corresponds to extended station blackout
\ 40\
TABLE 61 PERCENTILES OF THE CORE DAMAGE FREQUENCY
PERCENTAGE FREQUENCY
3 7.01*10"®10 8.21*10"®13 9.19*10"®20 1.00*10"*23 1.09*10’*30 1.17*10"*33 1.2DM0"*40 1.33*10"*43 1.43*10"*30 1.34*10"*33 1.66*10"*60 1.80*10"*63 1.93*10"*70 2.11*10"*73 2.30*10"*80 2.37*10"*83 2.93*10"*90 3.47*10"*93 4.48*10"*
TABLE 7 s COHTIRBUTIOH OF IES TO DOMINATING ACCIDENTSEQUENCES
S.NO IE \Contribution
1 ML 3.442 FW 5.453 MSLB 1.034 SL 10.925 APW 2.636 NAHPPW 1.207 CLASS-IV 75.11
TABLE 8: CORE DAMAGE FREQUENCY REDUCTION VORTH OF ESF
S.NO ESF CMFRW
1 SSR 0.822 SLHI 0.903 ECR 0.974 ECI 0.985 EAPWS 0.976 RT 0.9997 AFWS 0.9788 FFS 0.679 SDC 0.99910 CLASS-IV 0.9811 Mod. System 0.40
LOCA IESim raras
INSIDETHECORE
Pressure TubeRuptures
1INLET OUTLETSIDE SIDE
Inlet Header Break Pimp outlet Pipe BreakPuap Suction Piping BreakInlet Feeder Rupture
- Outlet-Header Break- Boiler Inlet Pipe Break- Outlet Feeder Pipe Break
FIG 1: VARIOUS TYPES OF LOCA mrmiHG EVENTS IN PHNRS
OUTSIDETHECOBS
ZUPHT
INTERFACE
Bleed Valves Stuck Open IKV OpenBreak in Bleed System Piping Break in Relief System Piping Feed System Pipe Break Shutdown Cooling System Pipe Break Gland System Pipe Break Fuelling Hachine Interface Failure
IE RT EP ECI RBI RBC ECR
23
45
67
8 9
1011
12*10"Z/yr
1*10'В/уг
2*10’’°/yr
1*10'7/yr
2e1O",0/yr
1.5*10 /уг
1.5*10'®Ууг
1.5*10*’,,/уг <10'? /уг
410 /уг
FIG 2: EVENT TREE FOLLOWING LARGE BREAK LOCA
IE PS RT SLHSI SLHSR
0‘*/yr
--------- 1
Class-IV
1
23
45
6
fWj/yr1*10 /уг
2*10"*/yr1*10's/yr
I^IO'^/yr
SLHSI Snail LOCA Handling Systen Injection SLHSR Small LOCA Handling Systea Recirculation
FIG 3 : EVENT TREE F0LL0MIN6 SMALL BREAK LOCA
IE RT 1 £P ECI RBI RBC 11 BCR
101112
2*10“*/уг 1*10" /уг2М0_;/уг1*10*5/уг2*10"*/уг 1.5*10"*/уг1•S*10"*/yr 1.5*10’5/уг1.5*10"J/yr
<Ю"1 /уг <10 * /уг
Пв 4: EVENT TREE ПЗШМ1Ж MEDIUM BREAK LOCA
3*10°/yr
6*10’*/уг 3«10"*/yr
6*10’9/уг
4.5*10*-/yr
ECÏ Eaezgency Cooling Injection RB? Reactor Building IsolationECR Energency Cooling Recirculation
FIG 5: EVENT TREE FOLUMNG NAIM STEM! UNE BREAK INDUCING STEAK GENERATOR TUBE FAILURE
1
3«10°yr10’*
1.5*10’3
10-2
10,-3 4ю-1
T24 3.0*10 e/jr5 3.0*10’?/yr6 3.0*10’I/yr7 3.0*10’Г/тг8 4.5*10*"/yr9 4.5*10’J/yr10 4.5*10’"/yr11 4.5*10"*Vy*121314
4.5*10 ¡J/yr 4.5*10 « /ух 4.5*10’B/yr
FIG 54: EVENT TREE F0LUM1NG MAIN STEM LINE BREAK (WITH N0 STEM GBCRÀT0R TUBE FAILURE)
SSR 1 AFNS HE 1 « 1 HE FFS J
BE Huaan Error
FIG G: EVENT TREE РОШЯПЖ FEED MATER SYSTEM FAILURE
1234 5*10*2*/ir5 5*10“e/yr
6 5*10"*/yr
7 5*10**/yr
IE RT EP SSR APRS HE FFS
1/уг
* 11 SX
-3J 0.1 1«
10-э
10-Э
10-2
<10
3*10-з
234
567
8 91011 1213 <10:/yr14 З*10*3/уг
15 3*10”*/yr16 3*10,/yr17 3*10’;/yt18 <10"T/ÿr
10"*/yr
10"?/yr 10 I/yr 10”5/yr
10"!/yr 10_J/yr
HE Human Error SSR Secondary Steam Relief FFS Fire Fighting System EP Electirc Power
FIG 7: EVENT TREE FOLLOMING CLASS-IV PONER FAILURE
IE EARNS 1 PP 1 FMP AFNS ECI
123
45
6789
10
10"*/уг
10"*/уг
io:i;/rrЮ J"/уг
5*10"*/уг
5*10-;/уг 5*10 7/ух
РР Pressurising Pumps E&PffS Emergency Active Process Vater System FNP IN/C Pumps HPIS Higt) Pressure Injection System
FIG 8: EV0ÍT TREE FOUMIMG ACTIVE IP PROCESS KATER SYSTEM FAILURE
PS SSR РМР
1
23 2*10'*/yr4 2*10*’/yr
5 2*10~®/уг
6 2*10'П/УГ
7 <2*10*S/yr
8 2*10'4/yr
PS Class IV Povex Supply
FIG 3: EVENT WEE FOUMING NON-АСТПЕ IF PROCESS МАШSYSTEN FAILURE
Cl
APPENDIXSYSTEM RELIABILITIES
52
53
i.iimPDUCTiOH
The objective o£ Nuclear Power Plant (NPP) Safety ia to ensure and demonstrate that the risk from the plant to public and plant personnel is acceptably low. Risk of occurrence of an accident is defined in terms of probability of occurrence of an accident and its consequences in terms of the radioactivity released. The probability of failure in various systems which nay lead to accident situations or affect the sequence of events during accident conditions are evaluated in this appendix.
Although no quantitative risk criterion is specified, a general requirement is that the probability of malfunctions . be limited to small values, decreasing as the severity of consequences increases, so that overall risk remains acceptably low. The following criteria are applied during all stages of design.a. The design, construction and operation of all
components,systems and structures and particularly those essential to the safety of the reactor shall follow the best applicable codes,standards or practice to engineer reliability and safety into the systems,
bi The safety systems shall be independënt of each other and also of the process systems.
c. Each safety system shall be readily testable and shall be tested at a frequency which demonstrates that itsunavailability target is met. As a guide line, a target unavailability of. 10"3 yr/yr is assigned to each safety system. Such reliability goals not only provide targets for equipment design but also for component testing andmaintenance schedules. It is essential that these values be adhered to during the life time of reactor. A deviation could indicate aging of the plant.
2-SYSTEM RELIABILITY METHODOLOGY 8. ASSOMPTIONS
This section summarizes the nethodology of calculation and reliability of process and safety systens whose failure could lead to unsafe situations.
2Л DPLQGI
The computations are based on Fault Tree models. A fault tree is a deductive model which starts with the definition of most undesired event (the system failure) known as the Top Event and proceeds downward till all the combinations of events leading to the top event are identified in terms of failures of basic components. Various stages in the tree are coupled through logic gates.
2b. 2L ASSPHPTIQWS
1) It is generally assumed that the failure rates are constant and the components are utilised during their useful life period only. Equipments are replaced well before the onset of wearout period and early failures are detected during the installation and commissioning phases. The variability in failure rates is treated as lognormal.
2) The number of test operations performed do not cause any significant changes in the failure rates.
3) Piping failures in literature are reported in terms of a)failure per foot-year or b)failure per section-year. Aa any piping system consists of both long piping as well as a good number of sections, an averaging procedure is used in arriving at piping contribution. The total failure rate for per-foot and per-section basis is calculated and geometric mean of the two is assumed to represent the effective piping failure rate.The details of the analyses of the various process and
safety systems of NAPP that were carried out are presented below. A brief system description is also presented herein, however, the details are provided in NAPP safety report volumeI. .
3 PHT SYSTEM PRESSDRE В ш
h failure in PHT envelope would range fron the inlet header rupture to leakage in an inetrunent tubing. A large LOCA is a well studied and defined event and various ESFs are generally designed to cope with this situation. However, various safety studies and operational experience indicate that snail LOCA is highly probable. In addition, a PHWR has large nunber of pressure and feeder pipes which contribute to the probability of failure significantly. In NAPP seperate ESFs have also been providied to cope with the small and nedium sized breaks in the PHT pressure boundary. The major initiating events which lead to a LOCA arei. Rupture.of primary piping including the headers
ii. Rupture of feeder or coolant tubesiii. Opening of Relief valves spuriously or due to a transient
and subsequent failure to closeiv. Rupture of instrument or SG tubing
The response of the various ESFs to LOCA initiating events depends upon both the location and break size and based on these considerations, different LOCAs are categorised as follows:1. Large LOCA > 4я diameter or >10% of double ended inlet header
break area(2A).2. Medium LOCA 1/2 to 4" diameter or 0.1 to 10% of 2A break.3. Small LOCA upto 1/2" diameter or upto 0.1% of 2A break.
3.1 Reliability Analysis
Failures in piping systems are known to have occurred due to a variety of reasons such as design deficiencies, wrong selection of materials, inherent cracks present in the materials, wrong maufacturing, welding or erection procedures, corrosion and mal-opeartion during service. Failures are further grouped into two basic categories -Rupture (catastrophic) and Leakage (non-catastrophic). In a piping which is accessible during operation, non-catastrophic failures would be detected by visual examination or non-destructive testing. In NAPP these have been taken care of by high standards of design and material selection,stringent process control and inspection during manufacturing and installation followed by preservice testing and inservice inspection. Further due to use of ductile
FJQ Ъ'± XRV OPE.N S^FKXISTO OL_OSH.
57materials leakage would most probably precede catastrophic pipe failure. However, this is not always true and some tines a fault/crack may be so oriented as to manifest the failure in a catastrophic manner only. Apart from pipe rupture, a stuck open relief valve will also constitute LOCA. This has been separately anlysed as shown in the fault tree(Figure 3.1).
3.2 Failure Rate Data
The details ol failure rate data are included in [11] which also gives information regarding causes of failure in piping.
3,.3-ReguUB
Using the data as described before,the frequency of failure of various categories of LOCA are as follows:
-4 /yearLarge LOCA »Medium LOCA Small LOCA >The probability of inadvertent opening of relief valve and
failing to close is obtained as 1 x 10“2/year.
« 1 x 10"2/year 1 x 10"2/year
4. REGULATING SYSTEMIn case of any unsafe failure in the regulating system, the
reactor protective system would operate to mitigate an unwarranted situation. Thus the failures included in the failure analysis of this system are those which contribute to a spurious reactor trip. The system is triplicated and eventhough the signal processing part which is based on microprocessor systems is identical to all the channels, channel В is different from both A and C in that it controls the operation of two regulating rods where as both A and C are associated with a single rodeach.
A channel failure results in loss of control on a single regulating rod which can be obviated if the transfer circuit operates and transfers the control to an operating channel.Thus a channel failure occurs when the signal fails and the
transfer circuit also fails to transfer. This is shown In the Fault Tree(Figure 4.1). Failure of two channels is considered to lead to system failure in this analysis.
Ch
<5<hs/*
¡JkXIRGSZSTSH FAXIÆS
ffi/Y’r.
1 1CHARHZLFAXLORS
CHARRO.FAXLORS
CHARHELFAXLORS
F1 ^U J
^До-os/yt
IL
12-5/Гт
Ices/tr
Г—~L
(Л2Кт
<fTIWW ГЖПД1И»
<5satoÍ
<!r ^ ^ trshr 1 2 SXORAL
'JmtVytSERVO SSSVO XSXOHJU.
czscoz* ¿•7/УтД ¿y
£
ff*PROCZBSZRe
^hft
HXOXRORXCBELTA *
«A/Y»
Aff <!> <i> <6 <> 6 <i> <i>CFO DID OXO oac ISO. ARA RISC ООИ
Aie. 0/r CARD
óBTD1
t ;fig, q-iREGULATING SYSTEM FAILURE
:X
mM
en00
59The failure rate data for this systea is obtained fron
[8]. The application К factors in the analysis correspond to an ambient of about 40°C and a general ground based environment and a quality factor value 5 for MIL-e83 grade B1 components. The aean time to repair(MTTR) is assumed to be 24 hours, which is conservative. Also the common cause failures such as power supply fluctuations have been taken into consideration. The failure frequency of the regulating system is 0.3 per year.
5 MODERATOR SYSTEM
Moderator serves as an ultimate heat sink in the 'event of a dual failure involving LOCA and loss of emergency core cooling system. As major fuel failures can be averted for extended periods due to presence of moderator(upto full level in calandria)[4], it is essential to ensure that this systea is reliable. It would be seen that a) the frequency of a leak in the system that affects the moderator level is low and b) in case such an incident occurs it is possible to isolate the moderator system so as to stop the leak.
5.-1 SYtttcm DescriptionModerator system consists of two independent loops
connected to the calandria vessel. Each loop consists of a set of two pumps, a heat exchanger and associated piping and valves. There is a standby pump which can be started when any of the operating pumps in any loop fails. For the full power operation of the reactor it is essential to ensure that both the loops are operating. This system also caters to absorber; regulating and shim rods. Required quality of the moderator is maintained by the purification system, which takes continuously moderator from the system, purifies it and returns it back to the main moderator circuit. To keep the required reactivity level of the system, poison concentration in the moderator is controlled by the poison addition system and purification system. Moderator purity is monitored by the sampling station.
3.2 Reliability Analvalw
As the system is a continuously operating system, the frequency of moderator system failure leading to a decrease in level is a measure of the reliability of the system. As maintaining moderator level in calandria has an impact on fuel safety in accident situations, the probability of failure to isolate the moderator also serves as another index of reliability. In this analysis these two are considered.
S.a.ABgUBPtlongThe analysis is carried out under the following
assumptions.1. For heat exchanger tubes only rupture is considered to lead
to moderator level drop. It is assumed that leakages do not affect the moderator level much.
2. For large diameter piping, leakages in addition to .rupture are also considered as these can result in significant losses from the system. To take care of this the upper bound failure rate of rupture is used.
3. For the bellow seal valves only failure modes resulting in external leakage are considered.
4. A single pump seal leakage, it was observed in reference [12], results only in a loss of «15 litres per minute. Even if all the pump seals leak simultaneously, the total leak rate is «65 litres per minute. Based on a rough estimate[12], it is found that there is about one hour time available for moderator level to reach the calandria isolation limit in the event of all five pump seals simultaneously leaking. Operator action, to isolate the leaking pumps, is highily probable during this one hour. Hence pump seal leakages in moderator system are not considered to lead to a significant level drop in the calandria. The length of small and large diameter piping considered here is shown in table 5.1.
5. For diaphragm valves in moderator and associated systems failure rate data available from MAPS operation[13] have been used, details of which are shown in table 5.2. As failure information on bellow seal valves is not available, about one third of diaphragm valve failure rate is assumed to be
61applicable to these valves.
The failure data used in this analysis is shown in table5.3. A fault tree for the moderator level drop and failure to isolate moderator in calandria have been constructed and shown in figures 5.1 and 5.2.
5.4 Résulta
With the above assumptions, using the data shown in table5.3, the frequency of moderator leve.l drop has been calculated and this turns out to be 2.0/year. Th« probability of failure to isolate the moderator in calandria turns out to be 5.0*10‘3.
Table 5.1 Details of Piping of Moderator ayates
System Lineno
Length in Metres
Number of Sections
Mpdmtpi .CirculationSesteaa)Piping & Tubing All lines 152.7 59
(diameter >3") b)Piping & Tubing 3211.8 14.0 18
(diameter<3a) 3211.9&Ins >Shim Regulating RodCooling System
Tubing
All 3240 42.5 13(diameter >3")
Liquid- PpjgpD-.Sya tealines3481-1,2,1 76.5 15
(diameter<3a) Semolina circuit
12,13 & 1610.0 1
(diameterO* )Bmificatlpn Circuit;
(diameter <3a)3221-1&2 (100\ length) Remaining all 3221 lines 50% length (The portion beyond MVs uptoIX is not considered
•
Table 5.2:Diaphragm Valve failure data MAPS 1 Operation
Description Value
Number of Valves 486
Number of Diaphragm Replacements
83
Percentage of failures assumed to lead to major External leak
50%;
Period of operation(years) 3.25
Failure Rate(per year) 0.03
Table 5.3; Failure Rate Data
Item(Failure Mode) Failure RateElPC/Xufce
{Rupture/1eakage) i) <3"diameter
ii)>3"diameter
HfiAlk Exchanger(Tube rupture)
£ШШ (Seal leakage)
Manual Valvea(External leakage)
MQtOI Operated Valves i) External leakage
ii) Failure to operate
&ÍX Operated Valves i) External leakage
ii) Failure to operate
Check ValvesExternal leakage
Control ValvesExternal leakage
Ilansis. joints
3.0*10"*/section-year 2.0*10^*/foot-year 3.0*10"*/section-year 2.0*10“3/foot-year
8.8* 10'® /tube-year'
0.108/year 3.0*10"2/year
3.3*103?/year 1.0*10’ /demand
6.0*103?/year 1.0*10" /demand
2.6*10"3/year
6.0*10’’/year 1.0*10"2/year
/;
V39 MV28 V38 CBS>
V37 V42 V34 . »43( BS> <BS)
»46<B8>
»17 MV2.1fV4. . . . ,MV16
M»1.HV3. . . . .H»13
HV27 »29 MV33 t BS> ( BS> < BS> в
FIS. 61 FAULT TREE FOR 'DROP IN MODERATOR LEVEL
C3
IO
ra
ИОВЕНАЗОВ CIRCaUkXZO« STSTZH
0-3/Yf à
i i —1Í VALVES 1
:jPOMP BEAT
! t '
ù
О О О О О ÖCV60 CV61 V40 V39 va V9
(BS> <BS) (BS) <BS>
ЛI
Ä
; рш» i ¡ 1 ! ‘ POMP
? г ;I POUF j POMP VALVES
3-e 1 4 ¡ 9£ ^ A A A Ai
vaoо Ó 6 ó ó ó óV4 V5 MV1S HV16 V24 V25
<BS> (BS>
FIG. ( A) FAULT TREE FOR " DROP IN MODERATOR LEVEL“
)
■ LIQUID POZSOii II STSTSM I
0-27/tf. 7b\
HV26 VI V38ÓV310 Ó Ó Ó ÓV24 V36 V37 V39 V2
!Ovs»
SHZM JUm RBCTUI.ATIWG BOD COOLIBO SYSTEM
09S/Yt 7ü\
' ABSDEBER I ! ABSORBER ¡ ! ABSORBER 1 j ABSORBER! ROD Al ROD A2 ROD A3 ROD A4
AЛ\I
л\
■ HAIN SYSTEM Ij Valves j
; REGULATING ; ! ROD Rl !
REGULATINGj ROD R2
SHIM ROD SI
Л ' i . Л¡Aл\ A
ÔÔÔÔÔÔÔÔ ¡ i i : ¡A. .^4
vil V12 V13 V14 V23 V29( as> <bs> <33> (bs> <bs>
и и и и и WV37 VI V2 V7 V14 V9 VIO V13
< BS) < BS) < BS) C BS> (BS> CBS) ( BS)
SHIM ROD 52
лЛ».4_i
HG. S-l í В, C ) FAULT TREE FOR “ DROP IN MODERATOR LEVEL“
09
. CALENDRIA ISOLATION FAILURE
5 >10if
-a
Ó Ó 1о3211 3211 3211 3211MV2 MV3 CV60 CV61
FIG. 5.2 FAULT TREE FOR " CALANDRIA.'lSOLATION FAILURE"
09
69
6 FEED WATER SYSTEM
Feed water is essential for heat renoval fron Prinary Beat Transport System(PHTS) when the reactor is operating or shutdown. Beat removal fron PATS is acconplished by nain feed water system(MFWS) when the reactor is operating while auxiliary feed water system caters to conditions of MFWS nonavailability and during reactor shutdown. The nonavailability of MFWS results in high PBT pressure and consequent reactor trip where AFWS nonavailability results in loss of heat renoval capábility fron FHTS and thus has safety inplication. In this section an evaluation of the frequency of MFWS failure and the demand failure probability of AFWS are presented.
^I Svsten Description
Feed water system consists of three 50\ main boiler feed pumps which take suction fron the deaerator storage tank and supply water to the four stean generators after passing through & drain cooler and a set of heaters. The flow to each of the SGs is regulated through a small and a large control valve each of which has a standby to take care of any maintenance of the operating valve. Only two main boiler feed punps are enough to supply the required feed to the SGs: However, when any of the operating pumps trips, the standby comes automatically. Even when the standby does not start, operation of the reactor at reduced power is possible and this requires operator action. This operation at reduced power is not considered as it demands operator attention and alertness within the first few seconds of the standby pump failure when any of the operating punps trips. The level in the deaerator tank is naintained by a nain condensate extraction pump(CEP) which has a backup. The condensate pump discharge is preconditioned to deaerator water temperature through three LP heaters. One of the two AFWS punps starts automatically when the main boiler feed punps trip and supply water to the SGs for heat removal. Both MFWS and AFWS share some common piping. In addition AFWS has an independent line which feeds water directly to the SGs.
fi.2 Reliability Analvala
In carrying out the reliability analysis the following assumptions were made1. Only one of the two HP heaters is sufficient for normal
reactor operation.2.Two out of the three LP heaters are enough for normal
reactor operation.3. Auxiliary condensate extraction pumps are not considered
here as these do not have any safety implication. This is due to the adequate capacity of the deaerator storage tanlt which is fed by these pumps.
4. Valves in feed control station associated with each of the SGs are not considered as closure of these valves affects only one SG and this might lead to a reduction in power. Simultaneous closure of the valves in all the four feed control stations is remote. However, these are susceptible to common cause failure due to common power supply.
5. Only major leaks from flange joints(mainly from condensate éystem) are considered to affect the system performace.Based on the above assumption, fault trees for the main
feed water system failure and auxiliary feed water system unavailability have been drawn and are shown in the figures 6.1 and 6.2 respectively. The details of 'the piping are considered in this analysis are shown in table 6.1. The failure data used in this analysis are presented in table 6.2.
The frequency of MFWS failure and the demand failure probability of AFWS have been calculated using the fault trees(fig.6.1 and 6.2) and using the data shown in table 6.2 and these trun out to be 0.5/year and 1.0*10"3/D respectively.
71TABLE 6.1: DETAILS ОТ PIPING OF FEED WATER SYSTEMS
SYSTEM Length In meters(s ixe)
Number of sections
Number of flange Joints
Condensât» System 201.64 33 ,37(die > 3")
Feed System1. Independent 131.3 37 -
piping (día > 3">
to heater no.6)11 » Common piping 169.6 62 -
(dis > 3")Steam piping 308.8 12 -
(día > 3“)
¡/
72
TABLE А.2* FalLurff Rat» Data
ltam(Fa1Lure moda) Failure rataPumpa(Including motor)
1. Falls to Start 1.0*10"3/D11. Falls to run 3.0*10"5/hr
Haatar1. Shall Leak 1.0MCTe/hr
11. Tube rupture (1000 tubes) 0.01/year
Motorised Valve1. Falls to remain
open 1.0*10"4/D11. Failure to open 1.0*10_3/D
111. Failure to operate 3.S*10"3/DManual Valve
1. Falls to remainopen 1.0*10"4/D
11. Failure to close 0.036*10"®/hr 2.7*10"'/hr111. Stuck closed
Level Switch1. Failure to operate 1.0*10"4/D
<3.0*10"‘/hr)1.0*10"4/D<3.0*10"7/hr>
Pressure Switch1. Failure to operate
Hand Switch1. Falls to transfer 1.0*10"5/D
Limit Switch1. Failure to operate 3.0*10"4/D
Relay1. Falls to energise 1.0*10’4/D
11. Failure of NC by opening given no 3.0*10"®/hr
<1.0*10"5/D>switch operation111. Failure of NO
contact to close when energised 3.0*10"7/hr
1v. Failure of NCcontact by opening or coll openingor short 1.0*10 7/hr
TABLE 6«2i Continuad
ItamtFalLura moda) Failure rataPiping ruptura
1. (día < 3"> 3.0*10 уsec-year2.0*10"J/ft-year
1. (día > З") 3.0*10“*/sec-year2.0*10"*/ft-year
Strainer1. Plugged 1.0*10“*/hr
Expanalon joint 4.0*10“3/DControl valva 1.0*10'3/DFlow element
1. All modes 0.243*10 e/hrHuman error 1.0*10"3/DFlange joints 1.0*10“‘/hrCheck valve 3.0*10“’/hrCircuit breaker 1.0*10“3/D
1.0*10“®/hr
j LOSS OF MAIN FEED WATERA0'5/Yr
I • ~=Tt
l
соыФЕ.ы%>чте.* •
SvSTE. FAXUOtlE. PUMPS j i PIPINGI I
jHEATERSA ? ? I
! : ! ! i .t
Л/521
ASSE
DESIGNEDOBS
DESIGNED
«,-4r
PUMP RECIRC. PIPING
FIG. 6.1 LOSS OF MAIN FEED WATER
ЛСТОДХХОЯ-]LOGIC !
'
/'S . . V J
PGMF OPERATING FAILURE
POMP DEMAND FAZLORE
ьо Ó' О-
•ОSTR1 EJ3 VI V22 vai
<SUCTION) <DISCHARGE) CHECE VALVE
FIG. 6. la LOSS OF CONDENSATE SYSTEM
XX.
oí
6 TUBE
ЯВРТОВЕ
4
Ô
ISOLAT! OB FAXLOHS
ЛI
HEATERS
ó - óV33 FAILS OPERATOR V32 FAILS TO CLOSE ERROR TO OPEN
Aо
1f ЛiLP 'HEATER 1 ! LP
HEATER 3. LP i! HEATER 2 .?
▼26 FAILS TO CLOSE
r\V35 FAILS TO OPEN
ÔÓ
й
О
V34 FAILS TO CLOSE
ÓV36 FAILS TO CLOSE
Г-'îLS- 80
FIG. 6.1a (Ci) LOSS OF CONDENSATE HEATERS
i
OPERATORERROR
PI
TRIPPED POMP 1¿s
STOCK CLOSED
к\^,t HS1076
HUMAS ERROR
f ?Г-'svees
—\Ô
svaee
FIG. 6.1o (Cz Cs) FAILURE OF CONDENSATE SYSTEM
■M•M
POMPS ¡2 хю-^Г
} d)CIO~A/VvPOMP
FA1L08E I Л "! Ixio'VyV
àCLASS ZV
POSER SUPPLY
НА1МТЕЫАНСЗ
TTi.¿xiO’fc/d
P6 FAILURE TO START
“■O-58/Гг I
OPERATING POMP FAZLORE
A A
\ПюгтACTUATION О
POMP
0-27/Yi
A
PSMAZNTENANCE
Â
PS! FAZLOREI
<л/гЬ
?4MAZNTENANCE
00-23/Гг i 1
j P4 ” i ! ps/61 FAZLORE FAZLORE ! FAZLOREA ■
!
ñ|>
- 4 ?4MAZNTENANCE
*6 iFAZLORE Í
A/"N
PS LSÓ
OVERLOADRELAY
FIG. б. I (FI) LOSS OF MAIN FEED WATER PUMPS ■MЭЭ
4..*
¿•8iuö4Av^—A
5 ïMAINTESASCS SPURIOUS
HSA3SB Hsaxss HEATERб HEATER63
5
VALVES
XHEATER
S
A A A ¿T*<ToMV MV 164 166
6ISOLATIOMFAZLOREz
6 Ъ 6 ъHEATER 6 HEATER 6 OPERATOR LS PREMATURE DORM FAILS ERROR CLOSURE
ó ó ' ó ó Ъ
OPERATOR LS MV-163 FAILSFAULTS TO OPES
MV-166 PAILS TO CLOSE
MV—167 FAILS TO CLOSE
FIG. 6.1 <F21L0SS OF MAIN FEED WATER HEATERSсэ
rOsS“OsS
VALVE OPERATOR LS PROTECTION MV FAILS В PASS FAILSFAILS ERROR FAULT ON P-б TO OPEN TO OPEN.
FIG. -6.1 (F5) FAILURE OF MAIN FEED WATER PUMPS.
oo
LOSÉ OF AUXILIES!feed gaaot
! 1х|о"3/Уi '■
FIG. 62 LOSS OF AUXILIARY FEED WATER
00
i VALVES
2?COMMON PIPING
VALVES • INDIVIDUAL PIPING
CV229 STOCK CLOSED
ó4
VALVES
VI06 HUMAN EKROR.
гФ<IO-*/4
V107 HUMAN ERROR
VI12 HUMAN ERROR
MV-183
ЛMV-184
Ô ÓCHECKVALVE
MV-183
FIG. 62 (Аг) LOSS OF AUXILIARY FEED WATER
' - .s.$
• i
•I
09 .
ACTOATOR
ил
Ш)сР/4 Лсл
л/А!
HOMAN ERROR SWITCH
6 ó Ъ IОP4 СВ
CONTACTP5 CB
CONTACTP6 CB
CONTACTVALVE FAILS TO REMAIN OPEN
CB CONTACTSo ö 74
V104
HS746 LOP
13-4x10-3/4
Д
оLIMITSWITCH
óHUMANERROR
FIG.. 6.2 (Аз) LOSS OF AUXILIARY FEED WATER
CoCO
7- PROCESS WATER SYSTEM
Process water system liAce electrical power supply system, is & support system. It does not directly affect the safety of the reactor but it affects the performance of the safety systems. Hence it is essential that this system be highly reliable to prevent the dependent failures of the process/safety systems. In this respect the failure frequency of the process water systems (which lead to reactor shutdown and has a bearing on the ultimate heat sink of the reactor) and the demand failure probabilities of emergency process water systems (which affect the safety systems) are analysed.
7.1 System Description
Process Vater Systems are designed to remove heat from various process systems, like moderator system( through moderator heat exchangers), shutdown cooling systems(' through shutdown coolers), safety systems like ECCS( through ECCS heat exchangers) and service systems like class III power( DC jacket cooling). To cater to the various active and nonactive systems, the process water systems are classified as:1. Active High Pressure Process Water System(AHPPWS)2. Active Low Pressure Process Water System(ALPPWS)3. Non-active High Pressure Process Water System(NAHPPWS)4. Non-active Low Pressure Process Water System(NALPPWS)
Out of these the NALPPWS being a non-safety related system( in the sense that it does not cater to any safety system) is not considered here. AHPPWS and ALPPWS systems are not normally active. But as these systems cool active systems like PHT pump gland cooling, moderator cooling, these are likely to contain some activity in case of leaks from the active systems. These active systems, are further cooled by active process water cooling system(APWCS) which mixes with the NAHPPWS before going to induced draft cooling tower(IDCT) for heat removal.
85^The flow requirements of these systems during normal
reactor operation and shutdown operation are different except for NAHPPW system. In case of ALPPWS and APVCS shutdown requirement is less than normal and it is met by seperate emergency pumps primed by class ITT power. In case of AHPPVS, shutdown requirement is more than normal requirement and the same type of pumps with a more number of pumps running! on class III) meet the emergency requirement. In case of NAHPPWS normal and shutdown requirements are the same and these are met. by the same type and number of pumps.
1.2 Reliability AnalvaljThe fllowing assumptions are made in carrying the analysis.
1. In Active Process Water Cooling System there is one standby pump for both the units. It is assumed that the demand on the standby does not arise simultaneously for both the units.
2. In Emergency Active Process Water Cooling System it is assumed that the number of pumps required are always four.(When the standby cooling system operates the pumps required are four)The piping data giving the piping details inside and
outside RB for large( > Э* dia) and small ( <3" dia) piping are given in table 7.1. The failure data used for this analysis is shown in table 7.2.
7.3 ResultaFault trees (figures 7.1 to 7.4),.' as it was mentioned
earlier, were drawn for Dthe frequency of process water system failure and 2) the probability of failure on demand of 2a) emergency active process water system and 2b) emergency nonactive cooling systems. Using the fault trees and utilising the piping data in table 7.1 and failure data in table 7.2 calculations have been done and these turn out to be 2.5/year ,4.5*10"*/D and 1.0*10"4/D for 1,2a),and 2b) respectively. The contributions of piping to the failure frequency are shown in table 7.3.
TABLE 7.1: PIPING DETAILS
Inaide Reactor Building Outside Reactor Building
Spatem Length No. of Ro.of Length No. of No. ofin Sectiona Flange in Sections Flangemeterá jointe meterá joints
AHPPWSdie < 3- 377.0 61 50 - - -die > 3- 221.0 4.8 46 103.0 10 8ALPPWSdia 4 3a - - - - - -dia > 3B 43.0 6 - 2748.0 176 153
RAHPPVS -dia < 3a 13.5 4 60.0 2 -dia > 3- 630.0 - 42 38 1010.0 37 24
APCWSdia < 3* - - - 67.0 22 22dia > 3* — — 515.0 75 50
TABLE 7.2 : FAILURE RATE DATA
Iten(Failure node) Failure rate
Punps(Including notor)i. Fails to Start 1.0*10'3/D
ii. Fails to run 3.0*10”3/hrHeat Exchanger
8.0*10’®/tube-yrii. Tube ruptureMotorised Valve
i. Fails to renainopen i.omo’Vd
ii. Internal leakage 3.0*10’®/hr(Catastrophic)
iii. Failure to operate 3.5*10”3/DManual Valve
i. Fails to renainopen 1.0*10”4/D
ii. Failure to close 0.056*10”*/hrCircuit breaker
1.0*10’®/hri. Spurious transferii. Failure to transfer 1.0*10"3/DStrainer
i. Plugged 1.0*10"S/hr4.0*10’3/D
Hunan error 3.0*10"3/DExpansion joint 4.0*10"3/D-
1.0*10"5/hrFlange joints 0.3*10"2/yr
TABLE 7.2: Continued
Iten(Failure node) Failure rate
Piping rupturei. (dia < 3") 3.0*10"4/sec-year
2.0M0"4 /ft-yeari. (dia > 3a) 3.0*10"5/sec-year
Check valve2.0*10"5/ft-year
i. Internal leakage (Catastrophic)
ii. Failure to senain
3.0*10"T/hr
openPressure Switch
1.0*10"4/D
i. Failure to operate
Linit Switch
i.o*io"4/d(3.0*10"’/hr)
i. Failure to operate Tank
3.0*10"4/0
i. Rupture 1.5*10"9/hrClass III Power Supply 5.8*10"3/yrClass IV Power Supply 1.0 to 2.0/yr
TABLE 7.3:PIPING FAILURE FREQUENCY
Systea Inside RB Outside RB
Active Process Water systemDia <3- 0.067/year
Uia >3- 0.16/year 0.56/year(Inclusive (Inclusiveof joints) of joihts)
Active Process Water Cooling SystemDia <3- 1.7*10"2/yearDia >3* - 8.75*10"3/yearNon-active HighPressure ProcessWater SystemDia <3- 3.3* 10°/year 4.9*10"3/yearDia >3" 7.1*10'3/year 9.0*10"3/year
АРИ SYSTEMГ«/*
I3xi0's/YrTANKS !
I 13/Yv
4>
COMMONPART
XT
АНРРИSYSTEM
ЧО-^/Yr 7X10"^ /fr.
1
~ Xù'Wrr jO-7/YrACTUATION .< \*. »• HXs
LOGIC PIPINGX
\x-CLASS ZV
POSER SUPPLYUli
Xл
/г'ДЗ
SJ1202
X,w'
EJ 1209Ó
V1213Лч_
V1202
XНК
TOBE•fr FOR. THE STANDBY HEAT EXCHANGER
\/ALVES HAVE TO EE OPENED AND HENCE TKE ÎÆMAND FAVLURE P?DEAft\HTV FOR VAM-VES ENTER .
Г i
ALPPSSYSTEM
/Д2
1 1 X 1 1Í7131Í ! HX1 I 7131
HX27131HX3
7131HX4
7131HXS
7131HX6
7131HX7
/А1
COо
FIG. ACTIVE PROCESS WATER SYSTEM FAILURE.
SIGNAL
i POMPSj PIPING &
VALVES
i 17133 jPI ! 7133
P27133P3
7133P4
7133P5
А л^Т А' А
0+ Ö Ô!1
О (ÿV1202 V1004 STR POMP CB CHECK
1202 VALVE
we lNCLU*Deb IN COMMON PIPING t FOR. STANt>b7 PUMP ALSO
PAVE TO CHANGE STATE.
FIG, T-.HAV ACTIVE HIGH PRESSURE PROCESS WATER SYSTEM FAILURE. CO
EJlOO1 EJ 1215 STR1201
V1208 MV1021 + HAND SWITCH
POHP CB HV1021LS
77V120Ô
LS
* THESE HAVE TO CHANGE STATS FOR- STAN'Db'V PUMP OPERATION AND A U SO CHANGE STATE \WHEN THE OPERATING PUMP TRIPS .
НОМАМERROR
FIG. 7.KA2) FAILURE OF ALPPW SYSTEM
БДРВSYSTEM
LEAKAGE OPERATORERROR
EJ1202
EJ1207
V1213 V1202
FIG. ?,2 FAILURE OF EMERGENCY ACTIVE PROCESS WATER SYSTEM.
ЕАНРРвSYSTEMw*
с \**-
PIPING & VALVES
lixio
2POMPS ACTUATION
LOGIC2-2X10
•1----------- 1 1 ___u,
7133PI
7133P2
7133P3
7133P4
7133PS
¿__iA
A
XwPOMP
X■ i
SIGNAL
ъ
V1202 V1O04ОSTR1202
V1003 CH. V.
Ъ
CB
"ÔHUMANERROR
FIG. V--2 (EA1) FAILURE OF EAHPPW SYSTEM
V1002 VI211
(УVALVES
ЕА .LPPff SYSTEM
< IXio-4/У
5
7131 P3
74s
Ъ
HS HUMAN ERROR
ÔCBs
ЛPUMP
7131 P4
Ï&
àSTR1203
1*10PUMPS ACTUATION
& LOGIC
1f \KJ
V1001 CH. V.
FIGURE- 7.21EA2) FAILURE OF EALPPW SYSTEM.
оPOMPOP.
1 ~6xlQ-6/d
I/StuL__i
Л
EMERGENCY NAHPPW COOLING SYSTEM
IXIO■-+U
~ 4*\о~ь/а
ФI ЭЯ2
/ЕЯ2
О oPUMP DISCHARGE ACTUATION
DEMAND VALVE MVIOOI LOGIC
ЛCB
] i-6xiEAPWC NAHPFWS COMMONSYSTEM PUMPS PART
X
7134 PI 7134 P2 ACTUATION IDCTLOGIC
( ОOPERATOR ERROR TO
ACTIVATE PRELUBRICATION
* FOR n°n operating pump
o~s/d
POWERSUPPLY
FIGURE- 1-3 FAILURE OF E NAHPPWC SYSTEM
PI
PUMPPONCTION
FIGURE-
\d44
POMPDEMAND
ACTUATIONLOGIC
DISCHARGEVALVE
?.3(EN1) FAILURE OF E APWC SYSTEM
-з,I«io Ht
HOa-tCTZVZ COOLING SYSTEM
ГО-3/Yr.ЛРЯС
SYSTEM
JïMftrNAH?FW SYSTEM
Л А т
I 1 i 1HE'S О V
PIPING CLASS ZVPOMPS
POWER SUPPLY Ф
NALFPWSYSTEM
PIPING
6 ■ 6 Ó Ó Ó Ó ÓШС1 ISOLATING HE2 HZ3 ИМ HZS HEB HS7
2 VALVES -DO- -DO- -DO- -DO- -DO- -DO-
P1 P»
Л6 5 ó ó ó ó ó
SP.XSZPSIGNAL
DISC».VALVE
CB LFO POMP STB DISCH. VALVE • OP. FAILS TO CLOSE
óÔ
ACSiam.
àFOHP
DEMAND
óPDMPOP.
Ó 5 óDISCH.VALVE
DISCH.VALVE
STBAINSB
COOMOHPABX
Л
ACTOATIOHLOGIC
ъIDCT
* Ifc \S OSb«jm«d demand О»» 1*»« gbxindW ^UYn^. "iS Ykct SÁ-rriu¿a**<-0 ч-С
jar boTW 1h€ Unib .
3LOP СЭ
F16. 7-4 FAILURE OF NONACTIVE СООШС SYSTEM СО09
НАНРРЯ
0.2иО.«4ЖР—TÍci
О ‘-*<55-2 Xlûs/yf.
CLASS ZIZ POOER SUPPLY
5CBot.
3-6>lO~4 /y-f.PDHPS
■IbùtA-hr.
PIPZNG
TU
PUMPOP.
ACTUATIONLOGZC
P-l
"5 JMVlOOl CB
DEMAND
"ff
POMPDEMAND
^ APPL\CAB ^ SfANt> Рим P ONL>/ .
OPERATOR ERROR TO ACTZVATE PRELUBRICATION
FIGURE- 9.Í.IWFAILURE OF NAHPPW SYSTEM
100
fl-COMPRESSED AIR SYSTEM
The Compressed Air System comprises of six compressors and three dryers for both the units along with the associated air receivers,valves and piping. During normal reactor operation,three compressors are connected to one common header and the other three to another common header. The headers in turn are associated with a dryer each and in case of failure or maintenance of any operating dryer, the third dryer, can be valved in. Two compressors in each unit are 'ON1 during normal operation, one being on class TV and the other on class ITT and the third compressor is rtandby on class III. It is usually a unitised operation with tie up valves V-1030 and V-1029 kept normally closed.
a.J-BgHafcültY„&nalygia
The loss of compressed air situation arises when the air pressure falls below 7kg/cm2(g) in the common header. The details of reliability analysis are shown in the fault tree(Figure 8.1). The failure modes for loss of instrument air are as follows:a) Two out of three compressors trip or one of the running compressors fails and the standby compressor fails to start on demand or fails to run. The running compressor would be able to maintain the air pressure above the limit for about 10 mts. The tie line valves must be opened within the duration manually.b) Failure of one of the dryers coupled with the standby dryer
either under maintenance or failure 'on demand* or failure in operation during the maintenance period of the first dryer.c) Failure in piping.
8,2 fflUme Rflte-Pflfca
The Air compressors may fail due to the failure in any of the following components.
101i. Suction filter
ii. Compressor or the Motoriii. Inter cooleriv. After cooler
V. Inter connecting piping, tubing etc. vi. Air receivers including the relief valve instrumentation
tubing, piping etc.In case of the Air drying plant, various components leading
to dryer failure are:i. Regeneration system components,eg RV-1726,V-1689/V-1688 or
V-1692/V-1693, blowers etc.ii. Prefilters and associated valves,postfilters and
asssociàted valves,iii. Piping.However,the reliability analysis is based on the failure data obtained from RAPS [14] wherein the availability figures for LP and HP compressors and dryers are included as total subsystems. The fault tree is also not developed down to the component level due to the same reason. Based on RAPS data, following failure data has been used in the analysis.
Compressors: Availability - 90\Failure rate - 3/yrMaint, down time - 15 days/yr
Dryers: Availability - 90\Failure rate - 2/yrMaintenance down time - 15 days/yr
Class III Emergency Operation of Compressed Air System( Instrument Air)
During class IV power supply failure loads are automatically brought down and handled by class III power supply,wherein only one compressor is 'ON' (one which was working on class IV switches over to class III,ie CP2) and CP3 will remain as standby. Similarly air drying plant DR1 will switch over to class III and there will not be any standby drying plant during class III operation assuming unitised mode. These conditions have been explicitly shown in fault tree (Figure 8.2).
FIG. 8.1
COMPRESSED AIR SYSTEM FAILURE(INSTRUMENT AIR CL IV)
>=* 2/YyU »7«IO'2
AIRCOMPRESSORS
1 4-5/Yr. i
? 10 ORSER
RUNNING
ъ
STANDB7
1 0-5OPERATION О MAINTENANCE
PIPING COMPRESSOR
Д
¿1Л
¿if"; ó 6 ó
CflFAILS
CP2FAILS
СРЭ FAILS ON DEMAND
CP3FAILS
RUNNING Ó
1 1CPI CP2 CP3
CP2 UNDER MAINTENANCE
FIG. 8.1 (A) COMPRESSED AIR SYSTEM FAILURE оGO
FAILS ON FAILSDEMAND
DR1 DK2 UNDERFAILS MAINTENANCE
FIG. .8-1 (B) COMPRESSED AIR SYSTEM FAILURE
COrWÍESSCD air SrSTCT F*IL'JQ£ lINSTeur.£W AIR OASS Ш)
( CLASS IV VRAILURg Г
”77 777 10
1.0 X 10'-3 VO0-’ óDA 1 PYPTtir
г.о ж 1cr2^Lwr* * » Д- *“3
FAILURE COMPRESSORS CLASS III FAILURE
5CP 2 FAILURE
CP 3
? ó ó óСРЭ CP 3 CP 3
FAILS 04 OERANO FAILS IPtOER I1AINTENANC£ rls« 8-? COHPflESSEO AIR SYSTP1 FAILUAC ( IICTRUPIEMT AIR CLASS III )
L.3 RcBUlta106
The frequency of compressed air failure in the unitised mode of operation is 2*6/yr and the probability of failure on demand of class III instrument air system is 1.0*10‘4/D.
Д-ELECTRICAL,POWER SUPPLY SYSTEM
The electrical supply system which provides power to all station loads, is an important safety system since it is essential for the satisfactory operation of various other safety related systems. The system is broadly classified into ‘four different categories of power supplies depending upon the reliability, continuity and availability of the power supply requirements. These are termed as -Class I, Class II, Class III and Class IV supplies. Class IV and Class III are the basic normal and emergency power sources respectively for long term operation.
9.1_, Class IV Power Supply
This forms the main source of power to all the station electrical loads under normal operating conditions of the unit. There are two diverse and independent sources of Class IV power, one from the 220KV grid through a 220/6.9KV start-up transformer and other from the station generator through a 16.5/6.9XV unit transformer. The two sources are interconnected(at 6.6KV level)' in such a way that in case of loss of power from any of them, power supply can be maintained by a fast automatic transfer of loads to the other healthy source.
9.1.1__Reliability. Anataaia
The failure of Class IV supply is not unsafe, however, it is an important initiating event since a number of process systems connected on Class IV supply e.g. PHT pumps. Main BFP etc. trip and DCs are the main source of supply to emergency loads on Class III till it is restored.
The frequency of Class IV supply failure is the iaportant parameter which, coupled with the unavailability of Class lit supply, would yield the frequency of Station Blackout after about 30 mts. of loss of both the supplies. The reliability analysis of Class IV is shown in the fault tree of figure 9.1. The dominant failure modes are*.1.Failure of grid supply when station generator or unit transformer is down due to maintenance
2. Failure of station supply when components of grid supply are down
3. Simultaneous failure of both the sources of Class IV supplyThe frequency of Class IV failure has been worked out using
Markov Techniques[9]. It is important to note that it would be essential to consider both the effects of grid fluctuations on the performance of reactor and vice versa - any transient leading to reactor trip and subsequently, disturbing the grid stability. Both the situations would lead to a Class IV failure.
9^2 -_CLASS III POWER SUPPLY SYSTEM
During normal operation, Class III buses are supplied from6.6 KV class IV buses. When Class IV is not available, the loads on Class IV are automatically dropped to enable the DCs to start and subsequently, pick up in sequence after DCs are at rated speed. The transfer is affected through the Emergency Transfer System. The sequence of pick up is chosen with reference to the urgency and importance of each load. Normally more load is connected to Class III buses than that could be handled by a single DG. This is permissible as the DG rating is higher than ¿he nominal during the first two hours of operation. In the event a single DG only starts the sequence of load picking is stopped at a condition where the operating DG is not overloaded. The system is considered safe even if only one DG is in operation and the priority loads are connected. The tripping of isolating CBs and the closing of CB in series with the DG is done by interlock circuits and their availability have been considered in the analysis.
3^1 RflllftbllltY Analvala108
The details of reliability analysis are shown in the Fault Tree of figure 9.2. The major failure modes of Class III unavailability area. Independent failures
Since the emergency power supply system comprises of 2(100\) DCs, availability of any one of them would, as mentioned before, be adequate. Thus, failure of both DCs on demand would be the failure criterion. The contribution from the bus and the CB associated with each DG is also included. The operation of the CB is through interlock circuits whose contribution is associated with the CB.b. Test and Maintenance
Testing and Maintenance of components contribute to the system unavailability due to reduced redundancy during the test or maintenance period and is also a function of corresponding intervals. Test contribution would, however, be negligible, к downtime of 7 days/year has been assumed for a DG in the calculations. Thus, the maintenance contribution ■ 2*7*(Qd+Q0)/365 where Qd is the probability of faiure on demand and Qq is the probability of failure in operation during the mission time( assumed to be 24 hours) when the other DG is under maintenance.
9.3 Common Cause Failures
Common Cause Failures(CCFs) are multiple failures which are dependent and caused by a single initiating cause. Various factors contributing to CCFs in DCs may be listed as follows:a. Design and Fabrication deficiencies e.g. fuel oil blockage,
water in fuel oil, common service water supplies and D.C. supplies,
b. Operator errors in test and maintenance,c. External Environmental Effects e.g. rise in room ambient
temperature.
109In case physical diversity and fire barriers are provided, the effects of CCFs emanating from the external environment e.g. fire, change in room ambient temperature etc. would be reduced. Since the maintenance of two DCs is independent and staggered, the contribution due to human error in test and maintenance is significantly reduced. It has been bbserved[10] that lach of detailed procedures,checking the restorability after test and maintenance are dominant causes of CCF due to human error in test and maintenance. Other factors contributing to CCFs area.fuel oil blockage or water in the fuel oil system,
b. lack of water chemistry control in the engine jacket water causing corrosion
c. service water system or DC power unavailability,d. loss of start air pressure etc.
The overall contribution due to CCFs is quite dominating and is estimated as 1,0*10°
Э.l-Overloading EffectsOn Class IV failure, all the loads connected to Class III
buses are dropped. When DCs start and pick up speed, the loads are sequentially picked up in accordance with the emergency transfer logic. In case a CB associated with any Class III load fails to trip, the corresponding load would not be dropped and the DC may be overloaded and because of the intertie, the other DG could also trip. But the DGs are designed for a minimum of 10V overload and no single load exceeds this capacity. Thus, at least two CBs must fail to open to cause any overloading of DG. The probability of this failure is I.OMO*4.
9.5. ClftBS—U .SuREly
Class II is the uninterrupted supply required for the important systems like reactor protective,regulating systems etc. The Class II buses are normally fed from Class III through ACVRs and the MG sets and during nonavailability of Class III,through Class I, i.e. DC batteries, for a period of about 30 minutes. Thus, the contribution of batteries will be significant only in case of short term availability requirements. Apart from this Class II buses are also directly connected to the respective Class III buses.
CLASS ZV SUPPLY <6.6 KV> FAILURE
A 4 Ht.
i
521 513 5241 5241 BOS GRID GENI 522 5241 BOSSUT1 СВЭ CB34 CB33 F/G/R UT1 CB16 E/D/H
FIG. 9.1 CLASS -IV SUPPLY FAILURE
5231-7
FIG. 9.2 CLASS-Ш SUPPLY FAILURE
113
Э^5.1 Reliability AnalviHw
The details of reliability analysis are included in the Fault Tree of figure ).3 and are identical to the analysis as in f 1.
IQ FIRE WATER SYSTEM
In NAPP a system of constantly pressurised and readily available water supply system has been arranged to tackle' the type of fire where wit.er can be effective. The ¿yatem comprises storage of water, pumps and piping network terminating with hydrants and sprinklers at various locations in the plant premises. Besides this, fire water system acts as an emergency backup toa. Feed water systemt in the event of auxiliary boiler feed
water system failureb. Active process water andc. Process water cooling system
1Q..J—Syflten .Dfig.crlptlpn
The main source of fire water is the storage available in the natural draft cooling tower basins and the cooling water tunnel connecting the basins with the cooling water pump house. The fire water pumps are common for both units 1 and 2. One electric motor driven pump and three dedicated diesel engine driven pumps have been provided for this purpose.
10.2 Reliability AnalygiaReliability analysis is done for the on demand, failure
probability of fire water system as backup system to process systems with the following assumptions.
i. Two pumps out of three diesel engine driven pumps should be available.
114il. At a time backup ayates la required for one unit only
iii. Piping failure in any part of the fire water ayates, if not iaolated, can affect the aupply to the proceaa ayatesa.
Total pipe failure of thia ayates and the failure of the puspa ( two) are the contributing factora for the fire water ayates unavailability. The detaila of the analyaia are shown in the fault tree(Figure 10.1). The failure data used for the reliability calculationa is given in table 10.1. The calculated value of desand failure probability of thia ayates ia 1.0*10‘3/D
TABLE 10.1 : FAILURE RATE DATA
S .No Conponent Failure Rate
1 Pump 1.0*10'3/Da
2 Circuit Breaker 1.0*10*J/D3 Check Valve 1.0*10’4/D4 Pressure Switch 1.0*10'4/d5 Manual Valve 1.0*10"4/D6 Diesel Engine 3.0*10°/D7 Pipe Rupture 3.0*10'5/sec-yr
(dia >3") / 2.0*10‘5/ft-yr
äVlOOl CH. V.
<55*10-4-PIPING MS
VALVES
JL 3xio“4иCCF DE* s
7141 P2 7141 P3
fire baserS7STBIS7
10r3/d
PUMPS1?1X10-4-
CCFPOMPS
DOMESTICBASER
7141 P4 7141 P9
-éxio*
-¿r¿r ¿ ¿T-ó'1'"TT Ó-* ó <r<r¿r¿r <f
BBCIRCO— PS POWER POMP Viooe RECIRCO- CB DE PS POMP V1032V1002 CB ___ г л'т'тлм г.тмв тгАТТ.пиК FAILURE CH. V.
LATION LINE SUPPLYPOMP
FAILUREVlOOe RECIRCO- CB DE PS PUMP
LÄSION LINE FAILURE FAILURE
FIG. ю.1 FIRE WATER SYSTEM FAILURE
11711 REACTOR SHUTDOWN ЗТГГЕМЗ
The reactor shutdown system(RSS) is designed to automatically shutdown the reactor to prevent any damage to the plant which might subsequently lead to the release of radioactivity. It is Imperative that the RSS minimised the probability of failure of both the fuel structure and the primary system boundar/ under various conditions of operation, transients and the various postulated accident conditions. In order to achieve this, redundancies and diversities are incorporated into the design. To a large extent,, every initiating event is monitored using diverse process parameters so that the reactor shutdown function is not impaired even in the event of common cause failure of the redundant units.
.H-Л Sygtea-SsgcyiptignThe reactor shutdown system comprises of:
13.1.1 Instrumentât J^r.Process monitoring Instrumentation is used to monitor the
various process parameters like pressure, temperature, flow, radiation etc. In general, all the state variables which depict the operating environment of the fuel integrity and PHT pressure boundary, are instrumented to generate signals to be used by RSS. Limits on these parameters are so decided that under any abnormal conditions, no damage occurs taking into account the severest effect of CCF of RSS insturmentation. All the trip parameters are categorised into a) Absolute and b) Conditional trips and are arranged in triplicated channels.
11.1.2 TllF-tofllgTrip logic processes the information received from instrument channels, performs the necessary logic using 2 out of 3 coincidence scheme and provides signal to the clutch coils of the primary shutdown system( also called mechanical shutoff sysmtem or MSS). The function is performed by relay logic which operates on 48V D.C. Three seperate and independent sources of
power are used for the three channels, in view of the single failure criteria. Fourteen shutoff rods are divided into two groups of seven rods, each group of clutch coils fed from seperate 90V D.C. sources with a backup.
..1.1.. 1.«3 Shutdown devlcci
Shutdown devices ultimately trip the rector by introducing adequate amount of negative reactivity. The system has diverse, redundant provisions in the form of a. Mechanical Shutoff cods
This comprises vertical tubular cadmium rod .elements distrubuted in fourteen locations over the entire core with independent winch type drive mechanism for rod. These rods are held parked on the top of the core with the help of rope drum, electromagnetic clutch and irreversible worm and worm wheel drive. Upon receipt of shutdown signal the electromagnetic clutches are deenergised and the shutdown rods fall by gravity to bring about a quick reactor shutdown. Compression springs installed on the shutdown rods ensure the initial acceleration and a dashpot assembly absorbs the kinetic energy at the end of travel. A single failure in the primary shutdown system would not constitute a system failure under all conditions, b. Liquid poison injection
The system comprises of 12 tubes passing through the core and is divided into four banks of three rods each. Each bank has an associated poison (borated D20) tank and a Helium pressure tank and is independent of the others. The high pressure gas tank(TK-6) is connected to the liquid poison tank(TK-4) through fast acting solenoid valves. In order to reduce the probability of spurious injection, two SVs are connected in series. These valves are normally closed and opened whenever the shutdown system is required to act. All other SVs in the pressure balancing line or the Helium recirculation line are open during normal operation and closed on demand. Since three of the four banks provide sufficient reactivity depth for the reactor shutdown, nonavailability of one bank is not unsafe.
119The signal for the operation of nechahical shutoff rods is
derived fron the procees nonitoring instrunentation whereas, the liquid poison injection in addition to selective process parameters is also actuated when two or more shutoff rods fail to enter the calandria in a stipulated tine after the reactor trip. The two shutdown nechanisns aré independent and based on diverse node of operation and thus, are not anenable to CCF.
Safety Analysis
The RSS conprises of a nunber of trip paraneters which are actuated, depending upon the nature of the initiating eyent or the fault situation. However, it can be assuned that at least two parameters will be actuated for every initiating event. The details of the safety analysis are shown in the fault tree(Figure 11.1). The CCF block in the instrumentation includes common causes affecting both the paraneters because of whoch a low value of 0( p«\CMF/A«0.01} has been assuned. The safetyanalysis is carried out on the basis of the following assumptions.a. Test interval is fortnightlyb. Unsafe failure rate of the channel is 1.0*10's per hourc. Short failure of the switching diodes in the trip logic is
not unsafed. CCF of trip relays is due to welding of the contacts in the
ladder network for which a 0 of 0.01 has been assuned.e. Based on CIRUS experience[15], the probability of failure for
a shutoff rod is 2.0*10~5 per demand which for the present analysis, is assumed as 6.0*10~s per denand to account for the design differences.
The MSS reliability would then be 14C2 (6*10“5 )2 or 3.3*10’7 per denand. Hovever, taking into account all types of failures the reliability of nechanical shutdown rods have been taken as less than 10’4 per denand.
The details of the safety analysis of the liquid poison system are as shown in the fault tree(Figure 11.1). The analysis is critically dependent upon the assumption that one bank is redundant since the two nain injection valves are in series and any one of these failing to open would lead to failure of the poison injection in one bank. All the other solenoid valves which change state on denand are redundant. The probability of
RSS UNSAFE FAILURE
Л2*ю' S
. D E FИи*10Г5/Йг P ' JZjuo'Vd
F16. 11.1 REACTOR SHUTSOWIN SYSTEM FAILURE /оо
§Сн
R&S SP URI COB FU LUKE
Л0*/*'•У
POZSOS 2HJECTX0B SYSTEM
■ist \
TH'tr
1S. 0.RODS
INSTRUMENTS
А O’14/tV
'T
¿r*
CLUTCH CLUTCH D E FOPES
ihr
sacxuF HAzaSUPPLY
Tr•32/Yr
90 V DC
ОЭ/ïrCLUTCHSHORT~s
тцw
DIODE !03*10 "/Hr OPES-b
FIG. 1^2
REACTOR SHVJtdown SYSTEM SPURIOUS FAILURE
121
NO POISON INJECTION
5*10• \T
42Í2*5*io"s
SV16 svi SV2 SV17FIG. 11.3SAFETY ANALYSIS OF NAPP POISON INJECTION SYSTEM
123failure of a bank ie 2.5M0'3 is, thus, governed by the series valves and that of all the banks is 4.0M0"5, because 2 out of 4 banks aust fail on clenand.Xfifit—and—Maintenance Contribution; The test contribution froa main injection valves is negligible due to series configuration. The maintenance contribution, assuming 24 hours down time for maintehance action once in six months is
^Maintenance -4*3«V<24*2)/(Í*720) "4.0*«-*
where P0 is the probability of failure of a bank.Common Cause Failures; The analysis of CCFs for secondary shutdown system is associated with the common failures of the valves in the redundant banks of the system. Since all SVs are energised and their status displayed in the control room, the probability of any operator error during test and maintenance is considered negligible. The contribution due to design and environment is shown in the fault tree(Figure 11.3).
11.3 Reliability Analysis
The reliability analysis is associated with the spurious reactor trips due to failure in the RSS. It is assumed that the accidental dropping of a single shutoff rod or poison injection in a single bank of tubes will cause a reactor trip and also, the switching of backup supply(90V) is faster' than disengaging time period for a shutoff rod clutch. The details of the reliability anlysis are shown in the fault tree(Figure 11.2)
11.4 ResultaThe probability of unsafe failure of the reactor shutdown
system is conservatively estimated as 2*10~s/demand, the majority contribution being from CCF in instrument channels.
12 EMERGENCY CORE COOLING SYSTEM
124Eaergency Cor« Cooling Syetem(ECCS) is designed to reaove
the decay heat fron the fuel following a loss of coolant accident(LOCA) and provide means of transferring decay heat to the ultimate heat sink under all credible nodes of failure of the primary heat transport 8ystem(PHTS). Two different, systems are employed, one for handling large and medium LOCA and a second system for handling Small LOCA. In this section a safety analysis of the ECCS for large and medium LOCAs is presented. Spurious injection of ECCS is, however, not considered as it. is not possible due to the presence of check valves in the ECCS lines whose opening is governed by a positive differential pressure between ECCS and PHTS(which does not exist under normal operating conditions) when the signal is spuriously actuated.
i
J2-1 Svatca .DgacrlptlonECCS consists of (a) a heavy water accumulator (b) a light
water accumulator and (c) a recirculation system and associated piping and valves. Upon the occurence of LOCA conditions as
sensed by low inlet header pressure signal and/or differential pressure signal, signal for injection is initiated. Depending upon whether the injection is type I or II or til, the appropriate valves are operated and heavy water injection takes place. As soon as the heavy water in the heavy water accumulator gets exhausted and the system pressure falls below 32 Kg/Cm2, light water tank gets pressurised and provides core cooling after rupturing the rupture disk which normally isolates the light water tank from the PHTS. After water in this tank gets exhausted, as sensed by the low level sensor, the two out of four recirculation pumps( which are already started when the LOCA signal is generated) take suction initially from an overhead storage tank and later from the supression pool and cool the core. In type I injection depressurisation of PHTS is done during light water injection/recirculation mode by opening MV~.38 and MV-39. Prior to light water recirculation, the recirculation pump discharge passes through MV-52 back to pump suction. However, during recirculation MV-52 is closed.
12^2_Reliability Analvnla125
In carrying the reliability analysis, the following assumptions were made.
1. Only one of the two sets of (Э each) pressure sensors located on the two inlet headers is considered, as only one set is actuated depending upon the break location. Several seconds would elapse before the other set is actuated.
2. Only one of the two sets of (3 each) differential presauretransmitters between the inlet and outlet headers isconsidered as only one set is actuated depending upon the break location.
3. Pressure relief valves located in the gas lines of thepressurizing tanks for heavy water and light wateraccumulators are not considered in the analysis, as the gas pressure in the pressurizing tanks is monitored all the time.
4. In the recirculation loop P2 is considered as a backup for P1 and P4 is considered as a back up for P3 eventhough any of the pumps(excluding P1) can act as a back up for any other pump.
5. A monthly checking time is assumed. However, theinstrumentation located on the headers, which is normally not accessible, is assumed to be tested once in six months. Based on the above assumptions, a fault tree for the ECCS
failure has been constructed for type I and type II injections(figure 12.1 and 12.2). Since type III injection is similar to type II injection, the fault tree drawn for type II is also applicable for type III.
As the valves under test condition are provided with an override when LOCA occurs, testing does not contribute to ECCS inavailability. The failure data that was used in carrying out his analysis is shown in table 12.1. The data for components ike motor operated valves includes contribution of the actuator ircuit as well.
From the fault trees, shown in figures 12.1 and 12.2, the rrobability of failure of the ECCS system on demand during any /ре of injection is 3.5*10 3/demand.
126
«
J2,3 bona Term Operation of ECCS Pumpa
Since the demand on the continuous operation of ECCS is envisaged, in the event of a large or medium LOCA, for at least a period of two months, the long term reliability requirements of the ECCS recirculation system must be ensured. For the analysis of long term operation ECCS pumps are considered at a four unit system with one operating and three standby. Operation of one ECC pump is considered to be adequate during this period. It is also assumed in the analysis that there are no pumps under maintenance at the beginning of long term operation. This is justified because the most probable state of operation of the system is the operation of the first and the second of the four pumps during the initial period. Five cases (to study the effect of break down maintenance duration,if necessary) as detailed in table 12.2 are considered.
A computer program using Markov Approach [9], that was developed,for continuously operating systems, is used for carrying^out this analysis. The five casesCshown in Table 12.2) are analysed using the program and the results are shown in the same table. Since the pumps are located in the annular region, they are not subjected to extreme environment. However to take cognisance of the stresses due to operation for longer duration the 95th percentile value of the pump failure rate as given in reference [1] is used. From the results of the analysis( figure 12.Э) it can be seen that thé probability of failure for long term decay heat removal with no repair of ECC pumps for a mission time of two months would be 2*10~* per mission with a pump failure rate of 2*10~4/hr and 1*10° per mission with a pump failure rate of 3.0*10'4/hr. To illustrate the sensitivity of the unreliability to the failure rate of the pump during operation, calculations for a set of failure rates have been done and the results are shown in fig.12.3.
Л2.Л, Соадоп.Сйиас FflilureaRedundant óyeteme are susceptible to common cause failures
due to cosnonness in designf operating conditions, environnent, test and naintenance and human error. As indications/alaras are provided to monitor the status of systens/conponents inportant to safety, the likelihood of CCFs is reduced during test and naintenance. In instrumentation common errors due to improper calibration are not out of place here. The provision for physical separation of systems, like pumps is essential to ensure that malfunctioning of one pump does not affect the performance of the other pumps. In this analysis common cause contributions are conservatively estimated to see the susceptibility of the system to CCFs. As can be seen from the fault trees the CCFs considered are in 1)instrumentation 2)valves 3)pumps and 4)strainers(choking due to inadequate quality or peeling of paints on suppression pool liner)..
128
Table 12.1:Failure Rate Data
sNo.
Conponent Mode FailureRate(per hour)
Probability of Failure on Demand
1 Pressure/Level 1.0M0’6 1.0*10”4Transmitter,DifferentialTransmitter •
2 Indicating Alarm 2.0*10”®Meters or FIA All modes 4.0*10”®
Incipient 0.648*10”®3 Motorised Valve 3.5*10”?4 Solenoid Valve i.o*io”t5 Check valve Failure to Opei i - i.o*io”:
Leakage 3.0*10’7 1.0*10"46 Relay 1.0*10”47 Time Delay Relay Premature
Transfer 1.0*10”4Fails to
Transfer 6.0*10”®8 i.Failure of NC
Contact by Opening 1.0*10”7 4.0*10”5given not energis« idii.Short acrossNo/NC Contact 1.0*10”® 4.0*10"®ill.Failure of N0Contact to close 3.0*10”7 1.0*10"4Given energised
9 Flow Transmitter No 0/P for I/P 0.258*10”®(IEEE-500) Incipient 0.053*10”®
10 Flow Element No output 0.216*10"®Incipient 0.245*10:6
11 Strainer 1.0*10'3 4.0*10 112 Pump 1.0*10"313 Circuit Breaker Spurious Trip 1.0*10 s 4.0*10”3
Failure toTransfer 1.0*10 3
14 Rupture Disc • fi _ 3(Diaphragm) 6.0*10 e 2.0*10 3
15 Relief Valve Failure to _ *Close given 2.0*10 3Open
1
129
Table 12.2:Unreliability versus Tine (For Various Repair Times)
Repair Time* 7 Hours 24 Hours 36 Hours 48 Hours NoP'::pairOperating Time!
15 Days 0.94M0"9 3.18*10"9 9.32*10"9 1.89*10*7 5.12*10"®
1 Month 1.93MO'9 7.15*10"® 2.26*10"7 5.01*10~7 7.5 8 * 10" 9
2 Months З.ЭЗМО'9 1.31*10*7 4.93*10"7 1.13*10"® 1.0U*10"3
3 Months 5.92*10"9 2.30*10"7 7.59*10"7 1.75*10"® 4.39*10"3
ECOS ТУРЕ 1 INJECTION
I 3-5* lo3/d
U-pJ
?
s ъ
DESIGN TESTS.MAINT.
<5 Ъ
DESIGN EHVIRO——NHENT
FIG. tt-l FAILURE OF ECOS (TYPE 1 INJECTION)
FIG. 1X-1 ( X ) FAILURE OF ECCS (TYPE 1 INJECTION)
CO
PT—114 DPIA-52 DFIA 52-1 Í PT—117) <.D?ZA-53> < DPI—53 —11
RZLAÏS DFIA-ie-1 DPI—18< DPIA—17—1) t DPI—17)
DPT—83 C DPT—80>
R-3T75
R—4002
* APPLICABLE T0 TYPE Л &Ж INJECTIONS ONLY
FIG. .CL-1 (Y) FAILURE OF ECCS (TYPE 1 INJECTION) COro
LEVELINDICATION
¿10-6 [---- Ti'i
MV-15. 16
~io^~F л
ГBELAYS
LT- LIS- LIS— 143 63 63-
VALVES
7\
ACTUATION
à
\_/ О- О- ъ ЛX )'—'
--1U
ra
R-3764
a-3627
a-3670
a-6261
MV 15 MV 16 IЛ
В-3671-3
8-3674
MV—3.4
~JO‘S X—Аtt
IVALVES
1ACTUATION
j
А! tЛU)
IоMV3
ъ
MV4 I~Х л л л Л л
-U KJ w' •_а- н- а- а- а-3692-33638-1 3692 3636 3865
FÏG. 12.1 (Zi 2г Zá FAILURE OF ECOS (TYPE 1 INJECTION)
R- R- R- R- R- R- R- R- R-3778—2 3778 3873-3 3653 3653-2 3668 3775 3668-23638-2
FIG. 12.1 (Z 4) FAILURE OF EGGS (TYPE 1 INJECTION)гоOk
R- R- R- R- R- R-3638 3638-1 3876 3873-3 3662 3873
R- R- R- 3900 3870-63665-3
FIG.i. 12.. 1 (24 Zs ) FAILURE OF ECCS (TYPE 1 INJECTION) a»
¿Л
6 ^^5R- R- R-3629 3784-4 3668-4
FIG. 11-K26)
MV-7.8
~10'5
VALVES
■7Г
0^ACTUATION
S
MV 7 MV8à
Ó Ó ОR-3668
R-3907
R-3665-4
---------i
OR-3827-6
FIG. 1-11.1(28)
R-Эбе5
R-3665—2
R-3670-5
R-3666-3
R-3870
R- R- R- R- 3781 3616 3623 376-4
FIG. 4.1X1 (Z 9 Zio ) FAILURE OF ECCS (TYPE 1 INJECTION) ca-4*
VALVES
T
В
6R-3976
-5~I0
ZZ1ACTUATION
ОR-3784-5
FIG^_1X1{Z11) E. С. C. S.
R-3665-5
CO00
ôMVl MV2
10-5
ЛZL
6" 5 ~5 о 5 5R- R-3900 3830
R-3630
R-3778-3
R-3775-2
R-3778
FIG. 12--1(213) E. С- C- S.
ъ
R-3775
FIG. 12/1 (Zw) FAILURE OF ECCS (TYPE 1 INJECTION)
140
MV-31 <MV134)
r_- 10-3
c5MV31
(5R-3666-4
ОR-3668
1I ACTUATION
Z
X
Ъ ■ ó 5 5 Ъ~Ъ
R- 3767-4
R- 3767
R- 3764-4
R-3784
R-3629-5
R-3629
FIG. -1rl(Zl7) E. С. C. S.
<гVZ3
LIGHT BAIES XKjBCTioa
25*«0"*
!w«>o~»!-ie*5Mv-3.6 !
À
ÖV44
l0'4 : -io*5! JJV—7»e I
* I• tÀ
diî
HV-24
IA
:ао«иг» 1ючо~*'O l*"'31
< MV—134)8S
>10'UV13 V14
OSS2CB TESTAMAINT.
DESIGN SKTZBO-
FIG. 1.12.*2 FAILURE OF ECCS (TYPE 2 INJECTION]
äOJ
[Г и1 С: L
о8-Э641
FIG. .12..2 (Z 12) FAILURE OF ECOS (TYPE 2 INJECTION)
зсн
i MV—7,В
VALVES ACTUATION
3907 3Ô53 3653-33827-63665—4 3775 3775—4 3668 3668-2
FIG. .12.2 (Zœ) FAILURE OF ECOS (TYPE 2 INJECTION) 144
MIS
SIO
N
145
о
146
13 SMALL LEAK HANDLING SYSTEM
Snail leak handling system(SLH8) is designed to senove the decay heat from the fuel following a small LOCA and provide means of transferring the decay heat to the ultimate heat sink under this type of failure of the primary heat transport(PHT) system.
■U-l-Syatem Dcacriptipn
SLHS provides for sufficient D20 transfer to PHT storage tank for making up of losses from PHT system. This system' is actuated by the low storage tank level signal when the system pressure is >55Kg/cm*. This signal causes an automatic reactor trip also. Initially about 15 tonnes of 020 is transferred to the PHT storage tank from the ECCS D20 accumulator and later, when this gets exhausted, a 00 storage tank, 3211-TK-l, loacated outside the reactor building is used for supplying the necessary 02)0 by means of the pumps,ЗЗЭ5-Р7 and P8, provided for thi4 purpose.
During the , recirculation phase, either of the vault collection pumps 3491-PI or P2 takes suction from the sump collction area and pump the 'spilled 020 to the storage after conditioning(i.e purification and heat removal) it. The pressurising pumps or the PM pumps maintain the PHT ay., zem pressure and inventory at the controller set point. This of operation can be continued until leak is identified and plugged.
11.2 Reliability AnalYflla
Reliability analysis is done for on demand failure of SLHS and the details are shown in the fault tree(Figure 13.1). The failure rate data used for reliability calculation is given in table 13.1. The calculated value of the probability of failure on demand of this system is 2.0*10 *.
TABLE i:i.1 : FAILURE RATE DATA
S.No Component Failure rate
1 Level Transmitter 1.0*10’4/D2 Pressure Switch 1.040"4/D3 Control Valv-ï 1.040“3/D4 Pimp fails to
start on Demand 1.0M0"3/D5 Circuit. Breaker 1.0*10’3/D6 Husaan error 1.0*10“3/D7 Check Valve
(he »vy reverse leakage)
3.0*10”3/D*
ß Motorised ValveFails to close 1.0*10"3/DStuck closed 1.0*10’4/D
9 Strainer-Choking 4.0*10”4/D10 Heat Exchanger 8.0*10”e/tube-yr11 Level Switch 1.0»10"4/D12 Piping Rupture 3. OMO”5 /sec-yr
(dia > 3*) 2.0*10~S/ft-yr
* Upper bound (95 percentile value)
SLHS OEMANO FAILURE
i 2^ю*г/<1
И‘2ХКГ> 11-2x10гЗRECIRCULATION
SYSTEM
АMAKEUPSYSTEM
5V"
PIPING
<Дю"3 ^Ю-а^1СГ3^4х1о-*
▼99 MV ИР STRНЕ 104 105 4
PUMPS
¿Г▼100
21X10"^ • СН. ▼. HS НЕ
]зхю*+; ю-3ó <¿>▼ 107 HP
Р7
-А
ре
Ï7Г*PUMP+
HS НЕ+СЭ
ACTUATIONLOGIC
X’io'-5
Ó о О0 <6▼ 103 LT PS CP124 ACTU—CH.P. ATION SIGNAL
FÍG. . -13.1 S L H S DEMAND FAILURE
, RECIRCULATION j SYSTEM̂=É --z
4 ¡ I0-5 1 Î3»io-i !io"3C ó !|0-3 JS3HO"4 ho
( ] j STRAINER ; O O O
V97 !_________i HEAT EX- VSB MV2 vee LSHE Uxio“7Û CHANGER HS CH. V.
STBS МУ99
FIG. -13*1(BJ S*UHS. FAiiajm:
T?''MV94 HS HE
150и comí O.HvK' ISQLMIQH SYSTEMS
Reactor Containment ia necessary to restrict the release of radioactivity to the environment during normal as well as accidental conditions of reactor operation. Containment isolation during these conditions is achieved by closing the various inlet and exhaust paths for liquids as well as ventilation air. The reliability of the system has to be assesed to make sure that the design would meet the requirements imposed by all modes of operation.
11 ■ 1J3ygiem,-PeagiAp.tipn
NAPP reactor containment has been divided into two zones i) Primary Containment consisting of PHT system, Moderator system etc. and ii) Secondary containment consisting of Boiler Room and Dome Region, annular region between two walls of reactor building and main and emergency airlock housing. Under, normal operating conditions the atmosphere in the primary containment and in the secondary containment is maintained at a -ve pressure w.r.t. the external atmosphere with the help of ventilation exhaust fan units continuously running on Class TIT so as to avoid any ground level leakage from the reactor through the openings. Also, the pressure in the primary containment is maintained -ve w.r.to that in the secondary containment so as to avoid leakage from the Primary to the Secondary containment since the former one houses all nuclear systems.
The instrumentation logic used for; containment isolation system actuation comprises of the following triplicated monitoring channels.a) Reactor Building Pressure- This is monitored using two
differential pressuure switches and a PIA. This signal is effective only when the reactor coolant temperature at the outlet header is >101° C.
b) Reactor Building Exhaust Activity- This is monitored by Gross Gamma Monitors in the ventilation exhaust duct.
с) PHT Pressure- The PHT Pressure low signal coincident withPHT temperature >101°C.The signals from these three sets of sensors are wired in
the primary and secondary containment isolation logic circuit.In addition to the closure of dampers in the primary and
secondary containment intake and exhaust ducts, the follwing functions are governed by the containment isolation logic so as to ensure complete isolation of the radioactive atmosphere form normal atmosphere.
i) Isolation of D20 Vapor Recovery System ii) Isolation of Dryer room ventilation system
11.2.Reliability.Analygla
The details of reliability anaysis are shown in the fault trees of fig 14.1 & 2. Safety analysis deals with unsafefailures whereas spurious failures would result in the closure of a damper during normal reactor operation leading to RB pressurisation. Even though three signals could affect RB isolation, no credit is taken of these redundant parameters since it is realised that all may not be actuated for various accident situations.
The details of basic component failures resulting in the system failures are included in the fault trees. Due considerations are given to the particular modes of component failures. The failure rate data used in the analysis are shown in table 14.1.
14.3 Analysis of Common Cause Failures
The Containment Isolation System comprises of two subsystems i) Instrumentation for actuation and ii) Dampers for isolation. Redundancies have been provided in both. The actuation signals are provided by the triplicated instrumentation for
a) Primary containment Pressure high and PHT temperature>101°C
151
152b) High Activity in the Prinary Exhaust Ductc) PHT pressure low and PHT temperature >101°C.
In case of initiating events like LOCA, it is expected that all the three diverse parameters would be affected and thus i making the probability of any CC7 negligible. In case of accidental situation( e.g. Fuel Handling Accidents) leading to high activity, Containment Isolation would be affected by b) only. Activity monitoring is based on GM Counters wherein diagnostic systems are provided to monitor the performance of radiation monitors. This would reduce the duration of.unsafe failures significantly and hence the contribution of CCF too. In case of Ventilation Dampers, the majority of failure modes( e.g. Solenoid, Air Failures etc.) are safe, and spring failures only would be unsafe. The contribution to CCF would again be insignificant. However, an overall CCF contribution of 1*10~4/d has been assumed.
TABI.E 14.1: -FAILURE RATE DATA
COMEÛNENT FAILURE RATE1. Solenoid Valves/MV
Failure to operate 1.0*10'J/DFailure to remain open 1.0*10‘:/D
2. Pressure Switch 1.0*10” /D3. Circuit Breaker
Failure to transfer t 1.0*10"J/DSpurious Trip 1.0*10'®/hr
1.0*10’®/hr4. Buses(all modes)3. Relays
Failure to operate 1.0*10’*/DCoil Failure open or short 1.0*10’B/hrFailure of NC contacts by)
opening) 1.0*10"7/hr6 . Time Delay Relay
(Birne.allie Type)Premature Trinsler 1.0*10"*/DFails to Transfer 6.0*10‘!/hr
7. Dampers Failure ta operate 1.0*10"3/D8. Instriimen^atjon-gsneral 1.0*10"e/hrFailure to opereta9. Indicating Alarm Meters
All modes 4.0*10 */hr 2.0*10"’/hrCatastrophic
10. RTD Element 3.0*10”6/hr11. DP Transmitter 3.0*10*®/hrAll modes
Catastrophic 1.0*10”6/hr12. CM Counter 14.*10"®/hr
5.0*10"!/hrAll modesCatastrophic
13. Temperature Transmitter 1.5*10";/D14. Activity Transmitter 2.0*10"3/D
ЯЭ C0NTAINKH3JT5ИIH tPHIMARÏ»
¿1 1-5X10’® ino"^ l1 6m
rS
DAKFEaS ANO SOLENOIDS
CCP
OX
-4X1^4
IÎ02
15*7xi er* ia-uur* Ixi0"*lCONTAINMENT ACTIVITY PHT
Ó O Ó 6RI 160 R1061 67314 QIA-2
OPS
d»tt Ï
12я0~^ ! 2л I О"3ом ♦
SOLENOIDON «
SOLENOID
7> 5
8946 R-Z
Ö<^~b
63335PA-31
63335PA-32
015
Ï
01 3491 MV Г2.002 730 DM 4, 503 7314 DM 287,28804 7172 MV 8. 5805 7172 MV 9.59bô 7312 MV 26,3507 730 MV 28,3108 730 MV 29,3309 730 MV 30,320Ю 7312 DM 29,3001 7312 DM 32,33012 7312 DM 35,36DO 7312 DM 38,39014 7314 DM IODO 7314 DM 2/4
FIG. 1*1 PRIMARY CONTAINMENT ISOLATION FAILURE СЛ
PATH A
ÏО
SB COUTAIHMEMT SPORIOOS ISOLATION :
I в.бжю-^УНг.PÄIMAHT
CONTAZBMSRT
4-4чо*/н«Г! ffffg мхшвг СОЯТДХвМЕЯТ
: Sxiq-Vht.А
i ACTO ATI ON I LOGIC !
-¡6-£xJ0%r. p
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ÔЯ1160 _ 1 OIA-2 ВМ6 R—Y 6333» 633333
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Л Л FIG. 14. 2 SPURIOUS ISOLATION OF CONTAINMENT
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POWERSUPPL?
A
,PRESSURE i LOGIC
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PRESSURE PHTPRESSURE
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1 ACTUATIONLOGIC
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COMBINATION
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FIS. ±4-Z(0I PRIMARY CONTAINMENT ISOLATION FAILURE
сл03
157JA REACTOR BÜILDING C00I.ER8
The reactor building is divided into two areas a) primary containment and b) secondary containment. The primary containment is further divided into two volumes -volume V1 and V2 . Volume V1 contains all high enthalpy 020 systems which includes mainly the pump room, fuelling machine vault and pressure relief chambers. V2 consists of all areas which are normally accessible during reactor operation. These two are seperated by suppression pool and associated vent system. In the event of RB getting pressurised during an accident,’ the depressurisation is affected in three stages: i) fast depressuristion to limit the peak pressure by suppression pool which removes about 25\ of the total energy, ii) RB coolers which take about 2 hours to lower the pressure further and finally iii) filtration and controlled discharge through the stack( under favourable atmospheric conditions) which slowly normalises the primary containment.
There are six coolers each in FM vault, South and North, and another five in the pump room which are required to be operational under post accident condition to bring down the pressure in the primary containment. Half of these are normally 'ON' during the reactor operation and the remaining half come into operation on increase in pressure. Accident analysis is done considering the availability of only 50\ of these coolers. Thus, only half the number will be adequate for the successful depressurisation of RB in the stipulated period and the operational reliability of RB coolers would be adequate under the operating or accident conditions. However, each half of the coolers is associated with a DG, nonavailability of any DG will incapacitate 50\ of the coolers. The probability of failure of this mode of operation, assuming the probability of failure on demand of a RB cooler as 3.6*10~Э, would be 1.0*10 Э. Another common cause factor for RB coolers is non-active high pressure process water system used for all the coolers. However, the probability of NAHPPWS failing in short duration of about 8 hours would be negligible. Thus, the probability of failure of RB coolers is considered as 1.0*10~3/d.
15816 REFEREHCES
1. WASH-1400, Appendix III & IV(NUREG-G751014), Reactor Safety Study, USNRC,1975
2. IEEE-500, 19773. HAA-SR-MEHO-12420,Volume II, "Piqua Nuclear Power Facility
Availability Evaluation Report'4. Heat Transfer and Thermcihydraulic Studies Related to the
Moderator Heat Sink in a CANDO Plant, Roqers,J.T,Currie,T.C.
5. Reliability of Piping in LWRs, Bush,S.H, Proceedings of IAEA Symposium on Reliability Problems of Reactor Pressure Components, Vienna, October,1977
6. NAPP-1/01560/86/B/8914, Reliability Analysis of NAPPProcess, Safety and Balance of Plant Systems
7. NREP Data Base8. MTL-HDBK-217C, Handbook for Reliability Prediction of
Electronic Equipment9. MAPP Safety Report, Volume II
10. Reliability of Emergency. A.C. Power Systems at NPPs, Battle,R.E., Nuclear Safety, Volume 26,1985
11. Dhruva Pipe Rupture Analysis12. Management of Leak in Moderator System, NAPP/32000/87/B/5916
dated August,!,. 198713. MAPP Moderator System Performance Report14. RAPS/09Ó00/0M/87/S/27 from Shri D.K Banerjee, 0S,RPS15. Operating Expérience of Protection and Safety System Of
CIRUS, DAE Symposium on Power Plant Safety and Reliability
KEY I/O NUMBER WINDOW N0 CRIO FUNCTION
1 W3-20 C3 CHANNEL K ECO WATER TANK LEVO. LOW
2 W3-23 ce CHANNEL L ICC WATER TANK LEVEL LOW
3 W3-28 04 CHANNEL U ECC WATER TANK LEVEL LOW
IJ.3 W3-J0 C5.C«C4
MV71/MV79 CLOSURE INITIATED ECC TANKS EMPTY
4.5.67 W3-32E5.E4E5.E4 ECC PUMPS BFF PRESS. LOW
M W3-33 E6.E8 ECC SUMP LEVEL LOW
I. 2.3,10,II, 12.13
W3-34
C3.CBC4.D5C4Æ3C3
ECC WATER 3432 TK1/TKJ TROUBLE
1.2.3 W3-39 C5.C6C4
MV72//UV80 CLOSURE (ЫШАТШECC TANKS EMPTY
15.32 W3-41 87 DOUSING TANK EMPTY
16 W3-42 D2 ECC HEAT EXCHANGERDISCHARGE TEMP. HI
\ 17.18 ' 19.20
W3-43 B3.C2C2.C2 ECC GAS 3432 TK2 TROUBLE
KEY 1 l/Q NUMBER WINDOW NO CRIO FUNCTION
28 et 0021 ce 3432 MV75 NOT CLOSE ECC IUPRD.Cl 0329 3432 CH.K ECC 40VDC FAILURECl 0330 3432 CH.L ECC 40VDC FAILURECJ 0331 3432 СН.Ы EEC 40 VOC FAILURE
15,32 Cl 0331 W3-41 07 3432 LauiBK oousme tvik empty
Cl 0512 3432 REMOTE HS OFF. NORMAL
3 Cl 0515 W3-2B C4 3432 L23M ECC WATER TANKLVL LOW
2 et este W3—23 06 3432 L23L ECC WATER TANKLVL LOW
1 Cl 0517 WJ—20 ce 3432 L23K ECC WATER TANKLVL LOW
1.2.3 Cl 0327 W3-39 C5.C6.C4 3432 UV80 CLOS IUPNO-TXS EMPTY
1.2.3 Cl 0528 W3-30 C5.C6.C4 3432 wn CLOS IMPNO-TKS EMPTY
o,e,7 Cl 0329 W3-32E3.E4E5.E4 3432 ECC PUMP 01 FF, PRESS LO
17 Cl 0533 W3-4J B3 3432 CPI ECC AIR DRIER TROUBLE
18 Ci 0534 W3-43 C2 3432 T24 ECC GAS TANK TEMP LO20 Cl 0535 W3-4J C2 3432 P22M ECC GAS TANK PRESS LO19 Cl 0538 W3-4J C2 3432 P22K ECC GAS TANK PRESS U3
20 * Cl 0337 W3-43 C2 3432 Р22Ы ECC GAS TAMC PRESS H19 et 0338 W3-43 C2 3432 P22K ECC CAS TM« PRESS ИЮ CI 0339 W3-34 05 3432 T216 ECC «ATER HTR. TEMP. H11 Cl 0340 W3-34 C4 3432 T25M ECC «ATER TXI TEMP. H12 Cl 0541 W3-34 CS 3432 T25K ECC WAHR TK3 TEMP. H11 Cl 0542 W3-34 C4 3432 T25U ECC WATER TXI TUP. Ш12 Cl 0543 C3 3432 T23K ECC WATER TX3 TEMP. LO13 Cl 034- WJ-J4 C3 J*J2 P20 ECC VATER TK PRESS. H3 Cl 0345 W3-34 C4 3432 123Ы ECC WATER TAM( LVL LO2 Cl 034« W3-34 ce 3432 U3L CCC WATER TANK LVL Ш1 Cl 0347 W3-34 CS 3432 L23K OX WATER TANK LVL LO16 Cl 034« W3-42 02 3432 Т1Э ECC HX OUTLET TEMP. H
9 Cl 0349 W3-33 E6 3432 L12 ECC SUMP LEVEL LO8 Cl 0330 W3-33 E6 3432 L11 ECC SUMP LEVEL LO9 Cl 0331 W3-33 E6 3432 LI 2 ECC SUMP LEVEL HI8 Cl 0332 W3-33 E6 3432 LI 1 ECC SUMP LEVEL H|29 Cl 0834 03 3432 V139 OPEN P1/P2 NOT RUN
23,26 Cl 0841 EUE1 3432 HXQI ECC FLOW PATH MPRÛ.27 CI 0842 £2 3432 HX01 BYPASSED ECC IMPRO
KEY I/oNUMBER
WINDOWNUMBER CRIO FUNCTION
1
30 AI 1351 05 3432 П140 ECC PI SEAL ТЕ IP
л Al 1557 03 3432 ТТ1Д0 ECC P2 SEAL ТЕ IP
30 AI 1565 03 3432 TTI31 PMI STATOR WOO TEMP.
31 Al 1624 03 3432 TTI4I PM2 STATOR WDG TEMP.
30 AJ 1626 03 3432 TT137 PM1 UP INSIDE 6RG. TEMP.
31 Al 1627 D3 3432 17147 PM2 UP INSIDE BRG. TEMP.
30 Al 1633 D3 3432 TT138 PM1 UP OUTSID BRG. TEMP.
31 Al 1634 D3 3432 TT148 PM2 UP OUTSID BRG. TEMP.
30 Al 1635 D3 3432 TT139 PMI LWR. BRO. TEMP.
J1 Al 1636 D3 3432 TT149 PM2 LWR. BRG. TEMP.
REV. NO./ REV. NO.
DATE / DATA DESCRIPTION / REVIZIA BY / DE
DRAWN BY/ OESENAT
PREPARED BY/ INT0CMI7
VERIFIED BY/ VERIFCAT
APPROVED BY/ APROBAT
DATE/DATA
S.ENE / T.CICERONE G.LEACH , J.THOMSONLi rv'
RENEL-CENTRALA NUCCEAROELECTRI :a cernavooa
OPERATIONAL FLOWSHEETEMERGENCY CORE COOLING HP ECC & SERVICE BUILDING
NOTES:’2'«.UM. TE-207K.I..M. TE—209K.L.M, <ЯЕ SPARE RTD'» WHOSE CHANNELS ARE WIRED TO THEIR
-.MSfECRVE PANELS IN THE CONTROL ROOM (51-32в,\ ex^Rnal FRECE JACKETS ARE NOT
,'2?ÏMÎF,Î5-Y WSTALLED. ïJSJ5*0 COLLECTION SYSTEM I-FS-3J810-PI
ORIO A2. A3. B2, B3.4-™E ACTUATORS of THIS Pv. are NORMALLY DETACHED
EJCEPT DURING TESTING. TO IMPROVE THE RELLABILTT'OF THE CHECK VALVES.-FOR DETAILS OF ECC INITIATION LOGIC WHICH ACTUATES
KMCES •(COUPLEXjr AS A SUBNOTE SEE OM 3432. -INSTRUMENT TESTING FACILITIES ARE OMITTED FOR
CLARITY. SEE 1-FS-34320-P3.-ALL MVs AND PVi HAVE OPEN AND CLOSE UMIT
SWITCHES FOR INDICATION PURPOSES: IE. EMI. LIGHTS. ETC. -THE VALVES ARE SHOWN IN POISED STATE.
UNLESS OTHERWISE SPECIFIED ALL EQUIPMENT ON THIS FLOWSHECT ARE PREFIXED BY 1-3432. AND INSTRUMENTS. SOLENOID. REGULATING AND CONTROL VALVES. PREFIXED BY 1-83432
WINDOW ALARMS
DEVICE EPS POWER SUPPLY DEVICE POWER SUPPL? CLASSUV3I assoo-Pim-cBiu ÜÑ39 3S32-MCC21A/F002 «UV30 92900^U70-€nOJ UV40 ЗЭК-ИСС20СД002 DWV4I Э2вОО-Рив»-СвЮЗ WV49 5532-UCC2IA/FÜ0J tikA/42 92900>PL70-C8203 UV46 SS32-MCC20C/FD03 1.UV43 азвоо-рив-ceio* MV59 5532-MCC2I A/RA01 UUV44 92e00-Pt70-CB204 MV60 5S32-MCC20C/RA01 U
■1МЯШ-....Ы.Д-ИЯ1 WV61 (11 UV80 4S2S00-PL70-C8202 | UV62 SS32-MCC20C/RA01 11
W63 SS32-MCC2IA/RAÛ3 itMV64 SS32-MCC2CC/RA03 IIMV65 S532-MCC21A/RA04 uWV66 IIW71 ssJi-ucc2iVRMI i aUV72 SS32-MCC20C/RB0I u
VÏ47(94KPlj(g))
D,0 (RD2) ZERO AIR GAP
TANK (СШЕПОИ TANK)
TK5 cue)37L
SAMPLEPOINT
E-*«~V120
BOILER ROOM
®/ТД>, TT-204K /^\TE-205K|(COMPLEX) (^J(NOTEI) ¡
TT—204L /^4TE-20SLl>4_J(N0TE1) I
OTE-20SMI (NOTE I) J
©,©
, TT-204L 1 (COMPLEX)
i TT-204M I (COMPLEX)
ГЛТЕ-214К1 (COMPLEX) IJ(NOTEI) I
РГ-ЗМ_____(COMPLEX)
"rttoF i7m'RS3¡Pa*5ídT_i i TT-208K /~NTE-207K I
J (COMPLEX) V^/(NOTEI) I
¡„©sk.ossS',1!DRAIN TO DjO
TT-208M /^>.TE-207M I COLLECTION SYS. > I 417 (COMPLEX)^(NOTEl) | ¿-ге-ЗЗвТО-PI ,
KEY cTimíl спей ВЖ! FUNCTION12ЯЗЕ W3-I CH.K MSSVi OPENING IMPENDING
u W3-2 пл CH.K (PI/P2) HEADER PRESS LOW
3 W3-3 C1 CHANNEL К REACTOR BUILDING PRESSURE EXCEEDS Э.ЗКРо
COMPLEX W3-4 CH.L MSSVs OPENING IMPENDING*.s W3-3 Г2.П CH.L (P1/P2) HEADER PRESS. LOW
в________ 1
w3-e ClCHANNEL L REACTOR BUILDING PRESSURE EXCEEDS 3.5KPo(g)
ЕП5ЕЗ W3—7 CH.U MSSVs OPENING IMPENDING7.8 1 W3-B Г6.Г4 CH.M (P1/P2) HEADER PRESS. LOW
9 W3-9 ci CHANNa M REACTOR BUILDING PRESSURE EXCEEDS 3¿KPo
10 W3-10 01 CH.K MODERATOR LEVEL HIGH11 W3-II Cl CHANNEL K F/M ROOM(R108)TEMP.H!GH
12 W3-12 01 CHANNa K F/M ROCM(R 107)TEMP.HIGF13 W3-13 01 CH.L MODERATOR LEVa HIGH14 W3-U Dl CHANNEL L F/M ROOM(R108)TEMP.H1GHIS W3-15 Dl CHANNEL L F/U RO0U(R107)TEMP.HIGH
16 W3-1B Dl CH.U MODERATOR LEVa HIGH17 W3-17 Dt CHANNa U F/U ROOU(R108)TEMP.HIG^IB W3-1B Dl CHANNa M F/M ROOM(R1D7)TEMP.HIGI
19.20 W3—19 B1.C1 CH.K BOILER ROOM TEMP. HIGH
21.22 W3—21 F1.F3 CHANNa К (P201/P202) H.T.LOOP ISOLATION INTTUTED
23,24 W3-22 B1.C1 CH.L BOILER ROOM TEMP. HIGH
2SJ6 W3-24 F2.F3 CHANNa L (P201/P202) H.T. LOOP ISOLATION INITIATED
27J8 W3-25 Bl.CI CH.M BOILER ROOM TEMP. HIGH
29.30 W3-271
FB/4 CHANNa Ы (P201/P202) H.T. LOOP ISOLATOR MITIATED
COMPLEX 1W3-28 ODD- CIRCUIT INJECTION IMPENDINGW3-29 ECC ODO CIRCUIT BLOCKED
IW3-3I MAIN STEAM SAFETY VALVE OPEN1W3-35 MSSV INSTRUMENT AIR PRESS- LOW
32.3433.35 W3-36 C2
C3 RUPTURE DISC LEVEL LOW
COMPLEX W3-37 EVEN CIRCUIT INJECTION IMPENDINGIW3-3B ECC EVEN CIRCUIT BLOCKEDIW3-40
Ri:!7 гл : ^TT-208K TE-2Û9KI T
Cl? ICOMPlfxIv ; (NOTED r-il
CONTACT ALARMS
KEY
1i GRID FUNCTION
COMPLEX 3432 CH.K ECC 40V DC FAILURE3432 CH.L ECC 40V DC FAILURE
О 0331 3432 CH.M ECC 40V DC FAILURE
COMPLEX Cl 0332 W3-1 3432 CH.K MSSV OPENING IMPEND-
COMPLEX Cl 0333 W3-4 3432 CH.L MSSV OPENING IMPEND.
COMPLEX W3-7 3432 CH.M MSSV OPENING IMPEND.'21.22 W3-21 F1.F3 3432 CH.K HT LOOP ISÛL IMPEND.125.26 Cl 0336 W3-24 F2.F3 3432 CH.L HT LOOP ISOL IMPEND-¡28.30 a 0337 W3-27 F6.F4 3432 CH.M HT LOOP ISOL. IMPEND.11.2 Í D 0338 W3-2 F1.F3 3432 PI/2K CH.K HT PRESSURE LOW
¡4.5 Cl 0339 W3-5 F2.F3 3432 P1/2L CH.L HT PRESSURE LOW
(7.6 CI 0340 W3-8 F6.F4 3432 P1/2M CH.M HT PRESSURE LOW
Ь Cl 0341 W3-3 Cl 3432 P3K RB PRESSURE>3.5KPq-6 Cl 0342 W3-6 Cl 3432 P3L RB PRESSUR£>3.5KPo
'9 Cl 0343 W3-9 Cl 3432 P3U RB PRESSURE>3.5KPo1--i D 0344 W3-3B 3432 ECC EVEN CCT BLOCKED
Cl 0345 W3—40 3432 HT INTERCONNECT VALVES FAIL
a 0346 W3-31 3432 MSSV OPEN
Cl 0347 W3-20 3432 ECC OOD CCT BLOCKEDTO ci 0348 W3-10 DI 3432 L203K MODERATOR L£VEL HIGH
13 Cl 034fl W3-13 DI 3432 U03L MODERATOR LEVEL HIGH
16 Cl 0350 W3-16 d 3432 L203M MODERATOR L£Va HIGH
COMPLEX Cl 0513 W3-37 3432 ECC EVEN CCT INJ. IMPEND.
COMPLEX a 0514 W3-2B 3432 ECC ООО CCT INJ. IMPEND.
27.28 О 051B W3-25 B1.CI 3432 CH.M BOILER ROOM TEMP. HIGH
23.24 O 0519 W3-22 BI.CI 3432 CHJ. BOILER ROOM TEMP. HICK
19.20 Cl 0520 W3-19 81,Cl 3432 CHJ< BOILER ROOM TEMP. HIGH
IB Cl 0521 W3-1B 01 3432 CH.M F/U ROOM fR107) TEMP. HIGH
13 Cl 0522 W3-15 DI 3432 CH.L F/M ROOM (R107) TEMP. HIGH
12 d 0523 W3-12 DI 3432 CH.K F/M ROOM ÍR1071 TEMP. HIGH
17 0 0524 W3-17 01 3432 CH.M F/M ROOM (R108) TEMP. HIGH
T4 D 0525 W3—14 DI 3432 CH.L F/M ROOM ÍR10B1 TEMP. HIGH
11 Cl 0526 W3-11I Cl 3432 CH.K F/M ROOM (R108) TEMP HIGH
O 0530 W3-35 3432 CH.M MSSV INST. AIR PRESS. LOW
CI 0531 W3-35 3432 CH.K MSSV INST. AIR PRESS LOW
CI 0532 W3-35 3432 CH.L MSSV INST. AIR PRESS LOW
32 O 0837 W3-36 C2 3432 L219K RDI LVU LOW
33 Cl 0838 W3-36 Ci 1 3432 L216K RD2 LVL LOW
34 Cl 0839 W3-36 C2 1 3432 L219M ROI LVL LOW.
35 Cl 0840 W3-36 C5 3432 L218U RD2 LVL LOW
ANALOG ALARMS
KEY I/ONUMBER
WINDOWNo. ORID FUNCTION
20 AI 1331 W3—19 CI 3432 Т21ЭК BOILER ROOM TEMP.33 AI 1361 W3-36 L “J 3432 L218K RD2 LVL LOW
35 AJ1362 W3-36 ~ C5 3432 L21BU RD2 LVL LOW
32 AI 1363 W3-36 C2 3432 L219K RDI LVL LOW
34 AI 1364 W3-36 C2 3432 L219U RDI LVL LOW
19 AI 1575 W3-19 Bl 3432 T204K BOILER ROOM TEMP.
23 AI 1616 W3-22 81 3432 T204L BOILER ROOM TEMP.
27 AI 1817 W3-25 01 3432 T204M BOILER ROOM TEMP.
11 AI 1620 W3-11 Ct 3432 T206K F/M ROOM (R108) TEMP.
14 AI 1821 W3-14 Dl 3432 T208L F/M ROOM (RI 08) TEMP.17 AI 1822 W3-17 Dl 3432 T206M F/U ROOM (R108) TEMP.
10 ГЖГШГТНП 01 3432 L203K MODERATOR LEVa
12 ижшлзяи Dl 3432 T208K F/M ROOM (RI07) TEMP.
15 Al 1631 W3-15 Dl 3432 T20BL F/M ROOM (R107) TEMP.
18 гетто гип 01 3432 T208M F/M ROOM (R107) TEMP.
13 Dl 3432 L203L MODERATOR LEVEL
24 remiragti CI 3432 T2I3L BOILER ROOM TEMP.
3 AI 2757 W3-3 CI 3432 РТЭК REAC. BLDG. PRESS
6 AI 2771 W3-6 Cl 3432 PT3L REAC. BLOG. PRESS
9 Al 2777 W3—9 CI 3432 PT3U REAC. BLDG. PRESS
16 AI 3156 W3-18 El 3432 L203M MODERATOR LEVEL
26 AI 3157 W3—25 CI 3432 T213M BOILER ROOM TEMP.
REV. NO./ REV. NO.
DATE / DATA DESCRIPTION / REVIZIA B? / DE
DRAWN BY/ DESENAT
» PREPARED B?/ NTOCMfT
VERIFIED BY/ VERinCAT
APPROVED B?/ APTO BAT
DATE/DATA
S.ENE T.CIClilONE G.LEACH . J.THOMSON-mW-í-'hi..
------------
RENEL-CENTRALA NUClEAROELECTRICA CERNAVODA
OPERATIONAL FLOWSHEETEMERGENCY CORE COOLING REACTOR BUILDING
1—FS—34320—P2 1 REV. A
В
D
CGC HT LOW PReSSURC LOOP
H.r. «AKR 331г-НП...
С/') НЖЬг гаи MAIN >саг-- TRANSPORT STSTCNi-rs-xiioo-Pipv_.j ру..е(А.С.) <А.0.>
TRW SPECIAL SATETY SYSTEM Test CIRCUITS COMRM TEST SOURCE i-rs-Mooe-pA-<$>-- <яО—é800»-Y._
PT..InjRGtI V/Í.VC
PI.. PT-u рт-гк PT-1L PT-ZL PT-IN PT-?M >T-«0l-K »т-г«-« »T-?oi-t •т-гое-L ►т-го1-и рт-гог-N3312-+CA0CR MDR 1 NOR 3 nor г H0R 6 NDR « H» 8 H0R 1 NOR з nor г HOR ft NOR 4 HD« ВPV..I PVIItl PVWl PVILI PVZLI PVIMI PV8MI PVZOIKI ругогте! PVZOILt pvzoai PV20IMI ругогн!n.Jt PVItt ругкг PV1L2 PV2L2 РУИС pv?«e ругоисг ругогкг PVZOlL? Pv20a2 pv?oi>e рчгог*еSV..I SV1KI ski ID ал 1M1 гмт гош гогмт ?01D ?cai zoiMi гогитSV..2 SVIKt гкг 1L2 аг IN? гиг гош гогкг SOIL? 202L? гоис гогиг
75I2-S„ -308V3 iS® -tf' 'И' IP -ip T -и® -w ■w -?p -Я4^ TO1-rS-MOOO-P« Ф»ID G4 ❖ÎRI0 G4 »10 C4 Ф»10 AI «t« ФjRID 0 <§>»10 G4 Ф»18 C4 <>:stD C4 »18 A* »ID А868000VALVE VIB VI7 VK v?f V3? V3I №0 VI* vra V27 V34 V33<Î> FROMI-FS-33I00-P1 75"grTd itЖ io s ILг: GtIB П an il Án St. ОGRID В 75“»18 0VA VIK V2K VIL va. VIM V2M VZOIK угоас V?0IL V202L V20IN V? огиPRV HtVIE (>**at PRV1L рта. Р«У1И PRVEN PRVROU рнугогк ravzoiL PRV208L PRVÎOIH ряугдги
mm R008 ROW ROW ROW R007 R007 ROW ROW МП non R007 R007
!;«l» tUPn.v|-
mœcVN.VCS
I « I ~l - И IПИЮЯЕДДД^ЧТВ-.» !Иь44|Я|135Д1ДЬ!ЛЕгТ!ПЕЗДИ ES3 Lr^ill íJ-?H.nКПТРШ
»м ВД кг+л ш ЕЯ ИД|К77*УДТ7ТД1Т7ГДдсдитапгцтдчтатдPtfr-»- Д fTSRiy ¿МЧУ-А L иктк. I то I ТО I IKI Ii?-S-MS0-vs I «si-уэ Г451-уг I
ЕСС WATER TANK LEVEL
cicvATi» у• 1¿r" ! "то 43KRAT0R HAIM CIRCUIT l-fX-32UD-Pl CRIO A?
CGC MODERATOR LEVEL LOOP
K L HLi-гоэ. LT-гож LT-гах LT-гознГ!.. ri-гож п-гозЕ ri-гожrcv. reveo» rev? ох reveo»
ругоз.i PV2UK1 PV20XI PV?f»lругв.э ругозкэ ругохэ ругожзSVZQI.I зугвж! SVZOXl sv?o»iSV209.3 svetoo SV20X3 SV203Q
VA уго»| veoxt V?0»lVS угожг vsox? VB03WVC угажз гекиэ VîeJHJ
" " VD угож4 V20X4 угоэм
« угожз VÎIOIS угоэмз73ie-s •SW V3 -307 V3 •304 V3
^ 1-rS-Klli-PI ф Otli п Q ИЮ n ^ ИЮ n
Ф l-VÏ-iP||»-PI ^ сто HI •O' «о нг •O »10 HT.
yps TO^ l-fS-32lli-Pt 4} ИЮ ¡7 ^ ИЮ 17 ^ И10 ni
OJUIDCtut
EGG SUMP LEVEL L-12
[мй*Зга,**143‘-¥г
NOTE1 ALL EOUIPTCNT LOCATED IN S-0I9
3-VALYE »CAKR73I2-S43C.VTГ " ÂTr * “î
I SUPPLY »
Ь
* L ИРГ-Х РТ-ЭИ
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LEGEND :
— THREE WAY VALVE (MANUAL CON TROLE D) REV. NO./
REV. NO.DATE / DATA DESCRIPTION / REWIA Of / oi -
DRAWN BY/ DESE NAT
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ST AND STARTING A/R S)rs - эгз50 - яг
11
1 X
7177-V006►Ч--
1-FS-71770-P2 7177,GRID E6 V009
7131-V23I
7131-V227-:-c—О
l-FS-71310-P3 GRID CIO
. ихтз
1-PS-7 1310-P3 GRID cm
Tl-10fc9 11-1000
7131-VBSB О
u \Xj m" 1
г- 0 ©I-FS-5230O-P1
GRID C7
WATER TANKгип7
\
./ TI-3091 T T-3090
О ©
I-FS-7J3I0-РЭ GRID CIO
■O' ©TI-3009 TT-3000
HX303
l-rS-5230O-P3 GRID C7
NOTE:1. UNLCSS OTHERWISC SPCCIFIED ALL EQUIPMENTS
AND VALVES ON THIS FLOWSHEET ARE PREFIXED BY 5237. AND ALL INSTRUMENTS. SOLENOID. REGULATING AND CONTROL VALVES. PREFIXED BY 65237.
REV. NO./ REV. NO.
DATE /OAU DESCRIPTION / REVUIA 8Y / OE
DRAWN 8Г/ DCÄNAT
PREPARED ВТ/ MTOCUST
VERIFICO ВТ/ VER1FCAT /
“’^ЖтвТ/ DATE/DATA
bf J . ROSU 1. DOCARU р/ ГЕРЕНА94.12.27
f y/f Í - CENTMUrttaClEAR$LECTRtc\ ÇERNAYOOA
OPERA f¡ONAborto ГГ SHEET
RAW WATER COOLING SYSTEMI - FS - 58370 - PI I REV. A
8
DIESEL 6 U!L DING
.J5Z2>40д 6-ш- 40/;____ш
-Ä:
-Vnew
! ^ V ¿90 • ¿40/-б-À/ ^ g
№¿$10 ММ á-----1-П. j_ - T SUM
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S.237 TK<ômm
L.O
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\ \ ///P/9
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-(xr^h-(Xf4J-
♦ 52Ï7OV4067/C90 г -*•
5237^üi—A-¿гзУом/^-х- —и
1 —1¿ ¿ 4= л
7/Ç9O-GZ0/- С*-Л/ ^ ^
5Zb70 V/0/4
\i5¿37 ГК 2.ft/run.
LO4X1-//ûô€
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т_А ЫОГ£А Y.S¿110
S-U/-PO/____ •
SU70/2OS ►Хл
52370/206
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7/690
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52370/306
7/4ŸO
7/£?0- 6/0/-£'/l/ ^ ^
52270 V/03_^5 г 370 У/04
^ J52370
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ïySE____'C__^237 ГК/ '
V_________ ô/rl/nj
LO—tXh
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h/orsô5¿ПО //05A
f
YS fi fi / coo/my moc/a/e
52370 //06
I
в
ог-
5238-ТК101(over По»)
LS-U04
II
______ I
нхюгА нхюгв
! оГТ--1
is- рт- юш 1047
16RK270 ENGINE
CNGINCDRIVCNPUHP
©
óPI-1004©
ENGINEDRIVENPUMP
|-гх-згз8о-Р] GRID ЕЗ
l-rS-52380-P4 GRID 03
<©
г
DUrr AND STANDBY
PUMP AND HCATCRS
vi30 J-|
-*\s-
CODLING MODULE
TT-1078 Г1-1079e оh VII6
VI17-o- 4rcvioi
V188^H Vlg^
VISO VI2I /TN
4>^i--- кэ-—i—0\ZSZ3—\sr~TV|22^ PMI3
V125 V|26 , HTB1‘I /<Г\cÿ]--- кэ-—r-r^^í—( t-4-
V127 РМИ
© ÔT T-1076 TI-1077
гг-ювг Ti-1083
© OTT-1095 TI-1096
© OИХ101
TT-1084 11-1085
© O
HX103
y VI08
ГТ-1080 Tl-1081© oV13I 4
в
l-rs-S2370-PI GRID C6
D
1-г5-згзво-Р4GRID Dl
V151
V7/ 1-Г$-52Э80-Р1 GRID El
MOTORS POWER SUPPLY CLASS
PM13 5433-MCC3I-A6 IIIPM14 S433-MCC3I-B2 IIIHTRI3 S433-HCC31-A3 IIIHTR14 5433-MCC31-M4 111
LEGEND:HIGH TEMP. CIRCUIT
LGV TEMP. CIRCUIT
NOTES:1. UNLESS OTHERWISE specified ALL
EQUIPMENT AND VALVES on THISflowsheet are prefixed by згэе,AND ALL INSTRUMENTS. SOLENOID. REGULATING AND CONTROL VALVES. PREFIXED BY 65238.
2. VALVE VI54 IS NORMALLY closed VITH a 3nn HOLE DRILLED THROUGH THE GATE. OPERATIONAL TLÓYTSHEEt У
GLYCOL WATER COOLING SYSTEM11 - FS - 52380 - PI REV. A
8
I
в
D
(over flow) V853-ÍXb
5238-TK201
V254note e
HEADER TANK
X «“X
ilrzizl
11 r O f-li г , VCCJ VCCO: i---------^----<]--- r-
j ....../^K /éK 1 [S L.-J .«i --•••■t
V227^HX202A( нхгогв!
16RK270 ENGINE
ENGINE , ^ DRIVEN I ' 'PUMP
IS- PT- 2010 204 7
ÔPI-2004
eCNGINCnqi\/rNpuhp"
-41 GRID E5
ФФ
e-2101.
DUTY AND STANDBY PUMP AND HEATERS
V230 H
-4Л>-
CDQLING MODULE
TT-2078 11-2079
© о
V2I7—О— ч
V2I6 V22B^-| V229^-|
V220 V22I HTBg3-cÿ]--- <ь—r-{5ZSZ3—(GV222 PM23
PM24
TCV201
© ÔГТ-2076 11-2077
TT-2002 T1-2083 wю© O
T T-2095 TI-209&
© OHX20I
TT-2004 TI-2005
© O
HX203
VV208
V2O0ЧХЪ
T T-2080 TI-2081
© O
V231 H
Я
I-FS-52370-P2 GRID C5
l-rS-52380-P4 y GRID
l-rS-523B0-P4 GRID DI
MOTORS POVER SUPPLY CLASS
PM23 5433-МСС32-Л6 IIIРИ24 5433-MCC32-B2 IIIНТЙ23 5433-MCC32-A6 IIIHTR24 5433-MCC32-L1 III
^V25l
\y7GRID El
LEGEND:HIGH TEMP CIRCUIT
LÜV TEMP. CIRCUIT
NOTES:1. UNLESS OTHERWISE SPECIFIED ALL
EQUIPMENT AND VALVES ON THIS FLOWSHEET ARE PREFIXED BY 5238. AND ALL INSTRUMENTS. SOLENOID, REGULATING AND CONTROL VALVES. PREFIXED BY 65230.
2. VALVE V254 IS NORMALLY CLOSED WITH A 3nn HOLE DRILLED TROUGH THE GATE
REV. NOy REV. NO.
DATE / OATA DESCRIPTION / REVIZIA BY / DE
REN it.
DRAWN BY/DESE NAT
PREPARED BY/INTOCUIT
VERmCO BY/ VEWCAT ■"я®/" ОЛТЕ/
OATAI. DOGARU P./n.aAíia I
i ч ■Г“ Ä—* ' Г1Ж 1 94.12.«
/CERNAVODAOPERATIONAL'FLOWSHEET /
GLYCOL WATER COOLING SYSTEMI - FS - 52380 - P2 I REV. A
8
5238-TK301(ovrr flow)
/"V,,..
D
V354V
note гд
LS *3106
HX302A нхзогв
16RK270 ENGINE
ENGINE , DRIVEN ( r ' PUMP
IS- PT- 3010 30-17
f] 0 0?
ÔPI-3004
гENGINEDRIVENPUMP
GRID ES
<«> 1-г$-5гзво-Р4GRID D3
l-rS-523BD-P4 GRID D1
"TV330
MOTORS PQVGR SUPPLY CLASS
PM33 5433-MCC45-A6 IIIPM34 5433-MCC45-B2 IIIHTR33 5433-MCC45-A3 IIIHTR34 5433-MCC45-J1 III
COOLING MÜDULE
TI-307B П-3079e оJ;v3,6
V3I7—t>b-
узгв^н узгф
V320 V321 НГЙЗЗ
-c^a--- <}-—i—ESZ5Z3—(fV322 РМЭЗ
V325 V326 нгя34-Dÿ]----<Ь--1—HN/N/4!--( ç
V327 РН34
TCV30I
© ОТ Т-3076 TI-3077
тт-зовг Ti-3083е ог!á¡n J
т т - 3095
0
V3C8ЧХУ
HX30I
TI-3096
O
ГГ-30В4 T1-3085
0 O
rI--l0B0 T1-3081
0 O
УЗЗГЧ
l-FS-52350-PI GRID E6
w
V3SI
GRID El
LEGEND:-------------- - HIGH TEMP. CIRCUIT
-------------- - LOW TEMP. CIRCUIT
NOTES:1. UNLESS OTHERWISE SPECIFIED ALL
EQUIPMENT AND VALVES ON THIS flowsheet are PREFIXED BY 523& AND ALL INSTRUMENTS. SOLENOID. Rrr,ULAT|NG AND CONTROL VALVES. PREFIXED BY 65238.
2. VAI VE V334 IS NORMALLY CLOSED VI III A 3nn HOLE DRILLED TROUGH THE GATE
REV. NO./REV. NO.
DATE /DATA DESCRIPTION / REVIZIA BY / OE
DRAWN BY/OESOUT
CU
PREPARED BY/INtOCUIT
ndi”SLVCRtntO ВГ/
VCRIFICAT
ÜJtçlSMgfc
R E N^E L^CKNTRALA-ffU£LEAROEU:CTRIfA CERNA YODA
BY/ DATE/ J DATA
94.12.27
OPERA TIONA E~FLO ITS НЕЕ ÏGLYCOL WATER COOLING SYSTEM
I REV. A1 - FS - 55380 - P3
8
VA
NOTE *I. 1M.CSS QTHCRVISC arenco 4L соинчснт AMO VAL ves fM TfOS n.QVS»CCr A« PffCriXCO IT K3tL mi 4L WSTRUCNTS.sacMiia irccu.«r»« mi соигво. val ves.АЯСПХСО IT 65гэ&г. vALve v«3A is tcmM.LT anco
vim a jm* Ю.С muí i touch ГК CATC
э. val ve vas is rat ami uex o- «.reo.то PRCPARC SQ.UTOL
TOTQVS POVte SCPPLT CLASSp*n 54ЭЭ-ИССЭ1 >L4 IIIPH? IIIртэ Э4ЭЗ'ЙСС46-А6 IIIPH44 S433*>CC46.|? IIIHf*4J ■.433-*CC46-AJ 111НГР44 Л4ЭЗ-»СС46.Л III
•or. N0/nv. wo.
04 IT /041» •остлом / t» /
10
л ш è ш ь • \OPEMVKBiL riOWSHSKTGLYCOL WATER COOUNG SYSTl
1 - rs - згзво - 1 »CV11
pt-»ой
VII5
X-
cГСУЮЗ
1-Г9-52Э80-Р4
/ \/ N / \/ \
HX-401
\ / \ /\ /\ /
■O'-1075
■e TT-1074
TT-1072
1^7> [fâ
rci
HAND OPERAICD □IL PRIMING PUMP
=n^-PUVII?
-X-VIIO -X-VIII
E/D OIL PUMPS
ES-193A0 рн\г_чДз ‘ <i—TR)—[/1——Г~
VI07 VI08 ¿____ VI09
rs-l93B
LUBE OIL PRIMINGpijhps
Zho-hV104 V103
-D^O-VI06
РИИduplexriLTCRS
ГТ-1070 Г1-1071
VI32
s4»s
f1 iPT-\a96
HIW{t -j iLO
1 PI-1097
9 Ф .VI33
-r\s-TLCXCONN.ГГ2
COOLING MODULE
GENERATOR BEARING LUBE GIL SYSTEMi--------------------------------------
I LS-1113
-1112
IIII IS-52390-P3
'.RID B2
DRAIN
16RK270ENGINE
l-ES-52390-P5 GRID B&
-<5>-X — v viol
OIL FILLNORMALLY DISCONNECTED
!-Jvil3
II
HTRII
TS-I042B
HTR12
—©
—e
—о —©
PS-1003
PS-1004
PI-1001
PT-1050
TS-1042A
MOTORS POWER SUPPLY CLASS
PMH 5433-KCC3I-A4 III
PMI2 5433-MCC3I-A3 MlHTRII 5433-MCC3I-AI III
HTR12 5433-MCC3I-A2 III
5231-PM15 5433-MCC3I-B3 III523I-PM16 5433-MCC31-B4 III
NOTEI. UNLESS OTHERWISE specified ALL
EQUIPMENT AND VALVES ON THIS FLOWSHEET ARE PREFIXED BY 5239, AND ALL INSTRUMENTS. SOLENOIDl REGULATING AND CONTROL VALVES. PREFIXED BY 65839.
LEGENDFLOW GLASS
REV. NO./ REV. NO.
DATE / DATA DESCRIPTION / RÇWA 8Y
DRAWN by/ OESENAT
PREPARED BY/ INTOCUIT
VERIFIED «Г/ VERJFCAT ^ |АРяЬED^BY/
yf. M^TCANU 1. DOOARUA«,
R E N E L - CENTRAUXMjCLEAHbiha,STRICA cé&N*4V
OPERA TfOUAb-ltOWSHEET
LUBE OIL SYSTEMI - FS - 52390 - PI —1 REV
1
1 2 4 5 6
MAIN DIESEL VENTILATION AND COMBUSTION AIR SERVICE
1 2 4 5
7 8 9 10 11
MOTORS POVCR SU»*PLV CLASS
ПО? 54ЭЭ-НССЭ1-С6 ш
ГЭ09 S43D-KC4S-J4 ill
П0Э 54зэ-ны:з1-сз шГ10А з«зз-к:сз1-С4 ш
ГЭ03 54ЭЭ-НСС«3-СЭ IIIГЭОА Э4ЭЭ-МСС4Э-С4 шггоэ з«зэ*мссзг>сз шггоА Э4зз-мссэг-с4 IIIГАОЭ Э433-ИСС46-СЭ HIT ADA 3*ЭЗ-ИСС*0*С4 шгго9 34зэ-мссзгчэ шГАОВ 3433-HCC46-J4 IIIrioi V»33-»CC3WHI ш
ггш з4зэ-нссэг-н| III
Г 301 3433-ИСС43-С1 шГ 401 34ЭЗ-МСС40-С1 III
пог Э43з-*<сзьиг III
ггог 3433-*CC32'H2 ш
гзог 34ЭЭ*МСС43-01 ш
ГАог Э4ЭЗ-ИСС46-С1 ш
Г'
rPflo I}"2'
LEGENDr - TAN
ВГ - Г IRC OAHPCR AT - AIR fILTC« l - PNCUHATIC lOUVCR DA»*»CR
NOTC1. UNLESS OTMCRV1SC SPCCITICD ALL
tQUJWCHl ANO VALVES OH THIS rLOVSKCT ARC RRCriXCO Bt T352. AMO ALL INSTRUMENTS. SOICKIIO. RC0U.ATIN0 ANO CONTROL VALVfJ. RRCffKCP Ft 67Э5г.
i
L..
CRANK CASE EXHAUST SYSTEM
OCttwnON / М>1фл л
Шггммшзящщшнётшшкя^зтшя^яс^г^твгашшУ№Ж2Шг~ш1)&йелшлкат
К ff Г L - CSHTfUUr *4сиЛЙф1£СГ*Сл &Ot^färrVIfAL_J*6WSH8tír •
тгг\шт km АЯСЪонъиягю* smj7
в
V005 Ц.\
PI-1
о—*Ч—' V006
l-rs-751E0'P4 GRID ВЗ
-CÍ3-VDD4
О
Vi
7512-VHO
ТО 5237-PV103 Г®-к
l-FS-52370-Pl SI
cïo-VI09
65237-SV103 Ж
V101 _-<J----------СЛЗ—*■
V105
TO 5237-PVID4
l-rS-52370-PI S’
✓ 104 Г
м vilo
65237-SV104 Ж
VI02 _-О-----1Ж}—•-
vio6
ТО 5237-PV103[Щ.l-rS-52370-Pl S’
—cSa-Vlll65237-SVI05 ^пГ
VI03 т-К}---0<Н
V107
l-rS-52370-Pl SI
ТО 5237-PV106
ELчЛИ
V112
65237-SV106 VI08
V4I4V413 -т-—c>f—сЗ<ь А side
ТО LOUVERS ОГ S DG N0.4
V214V213 -г—i>—СЖЬ Д side
—вТО LOUVCRS or SDG N0.2
V3I4V313 т—t>—ок}- А side
В ТО LOUVERS ОГ SDG N0.3
v„3 V"4
—1>+—[><]- A side
VI15 V116
—1>—tXb В side TO LOUVERS 0Г SDG N0.1
W
TO 5237-PV303(El-rs-52370-Pl JÖL—Зь-Л
V309
65237-SV303
TK305
1-FS-52370-PÏ
TO 5237-PV304
[Щ-cía-
2;
V30IЬ<ь- -Ä-H
V305
V310
65237-SV304
TK306 V302
-XJ— -cïo—»-V306
l-rs-52370-Pl S’
TO 5237-PV305
EL V3ii
65237-SV305
TK307
l-rs-52370-PI
TO 5237-PV3067306 I-
*4
V
-PI-cikj-icV312 308
V303 -p
J-Xb—t><bV307
65237-SV306
V304 _
-*à-—t><bV30B
I-FS-52370-P2TO 5237-PV203 I— ----------tÄj-f
m 1 ve°9¥65237-SV203
TK205 V20I
J-о— ч>кьV205
65237-SV204
l-rs-52370-P2 S’ TO 5237-PV204 I-------------- i>k}—El 1 vs,° TK
206
V206
TO 5237-PV205Ш]I-rs-52370-P2 S’
Ä-fVlll65237-SV205
TK207 V203
-хъ- -okyV207
I-rs-52370-P2 TC
TO 5237-PV206 p-DÍJ-
V2I2
65237-SV206
TK208 V204-o—
-Ä-
V208
l-FS-52370-P2 H TO 5237-PV403 I-----------------E>k—Г
bl| ^65237-SV403
TK405
l-rS-58370-P2
TO 5237-PV404V404 r~
*4-ÄH
V4I0
65237-SV404
TK406
l-FS-52370-P2 H
TD 5237-PV4D5 |-----------------i>k}—El 1 ^
65237-SV405
TK407
Ж
l-rS-52370-P2 S’
TO 5237-PV406 Г-
<4-{Ль
V412
65237-SV406
TK408
Ж
V40I -p-Kj-—[>кь—<V405
V402 —-XJ-—t><J—<-
V406
V403 -p-хь—okh-4-V407
V404 _-X}-—Ыо—•-V408
NOTEI. UNLESS OTHERWISE SPECIFIED ALL
EQUIPMENT AND VALVES ON THIS FLOWSHEET ARE PREFIXED BY 5235. AND ALL INSTRUMENTS. SOLENOID. REGULATING AND CONTROL VALVES, PREFIXED BY 65235.
REV. NOy REV. ЫО.DATE /DATA DESCRIPTION / RCVMIA BY / DE
DRAWN BY/ I PREPARED BY/DE SENAT . 1 INTOCMIT VERIFIED BY/
VERtrjCAT v jpp^^n/ date/DATA
M.jMUNTEANU L 1. DOGARU H.' p.^li/hia
94.13.27Lc. /ik
OPERA TlONAlr-FbÓYtSHEETSDG INSTRUMENT AIR SYSTEM
-1,11 - FS - 52350 - P3 REV. A
0
R
¿LAPSED ÎÜŒT
LO
15
25
35
tí
45
50
55
55
SC
SSQ. STEPS
и
1 **
2 "J «4 **
5 **
tttt
10
11
Ш1Ш1РТ1Ж *r~t
Sheet 3 oí 1
CLASS III tefl" LOAD SÈMES, V KITE Щ DCs 0» TBS EUS
Cl.III KC's aa П 25,* '■Lighting, Cliss l, Class II \T190-Chiller û'rc. tap (3)
a.III ItCCs on TZ 27, CD 225 ?
LOSS OF i 1Г (ШЕР)___1220IV 00 M 3fÍr Ih)
4321-itu. Ond. txtr. Pimp
3432-ECC tap^3432-ECC Рщf 3411-End Shield Cooling Pimp
3411-End Shield Coding Panp
352S-F/V Pressurising tap7131-Sill Ser. Viter Pmp-1
7131-Siii See. Viter Рапр-З
7131-Sail Ser. Viter Pinop-3
7121-Sin Sot. Viter Pmp-1■лi:
LOSS OF CL IV S LOCA CMEXTS
1220 IV (1000 iV afterWSun 140 IV (9S.il IS)
Includes Solentor Ponj Motor. One Class l bit tecу issuatd dischtrged.3 PlOpS oui oí 3 required
1000 IV (Ц0 kV öfter lb) 1000 tv (210 tV after W
I1
ПЯ1.К 1
ИЕШЕЯШ CUSS III Ш LOAD SEOUMC! HIM ПЮ DCs QH THE BUS
ELAPSED TIME SEQ. STEPS Ltà DESCRIPTIF COKTBDL LOSS Of a IV (RATED) LOSS OF Cl !Y S LOCA COHMEXTS
10 12 3341-Shutdom Cooling Pop OFF-OR 4 Reset (Bot Runpl №(203! Inhibit Run an shutdom cool ¿.80 13 7134-Recirc. Cooling Ровр-1 OFF-STST-OR
r
Run 125B № (ISIS №) Run I75C (128c ■ Onlf one pump per bur to run
85 147134-Secirc. Cooling Ьвр-З 1 Reset (tot Run) f Reset (Rot Run) 4
85 15 7134-Recirc. Cooling Рщ-3 Run 1250№(i:SSU) Run 1753 13 (12So ■■
90 IS 7134-Rtcik. Cooling fuap-l
ûfF-SràûR ÜReset (tot Run) Reset (Xu! Run) -
100 17 u 7190-Chiller Circ. Pmp (3) OFF-SmOR Reset (Rot Run) Reset (Xc! R’un) 3 Pumps out of 8 re.].
105 18 tt 7190-Chiller Onit-CH.09 OPP-MW Run 50SU (456.3 tí) Run 500 tí (45S.3 tí!
115 19 it 7190-Chiller Onit-CB.il 0FF-0R§ Run 509 № (456.3 it) Run 500 tí (45S.3 tí) Operates 501 of time, tod 228kR
125 20 tt 3331-8. ft feed Pimp OFF-Ш Ш Run 447 tí (283 tím Run 417 tí (283 tí!
135 21 tt 7512-Instiiir Compressor
1 * -0FP-A0ljjjSTBY-Ç5x Run 220 tí (190 tíj)
Run 320 tí ¡190 tí! Operates 501 of time.
140 22 tt 7512-Instiir Coapressor
1-OPP-AU$STBT-08'
1
Reset (Rot Run) |’i, Reset (Rot Run)
.'¡'И1:'! I jf 4
~1
■VIEiCc-J
ms:1.
2.3.4.5. S. 7.
iced
IssiLve
?■ IOpeating tods are shoo is ршлthesis. vLosses of ISO tí should be added to detenine the sixe of the №. final пшвЬег to be mimed bp MSALDJ. The rated tods shorn are the ootor shaft output. >The elapsed tine is after the К CB closes. iLoad sequence mist he coupleted vithin ISO seconds ftm receijfefif LOCLIY afoul.** indicates loads пЦ one К on to bus in case ofjfrSOt,In case of 2-100t SGs/Odd sequence till be аррИсаЬЩ to bod v uith Mtot rariatfjj&of HCC tods.
s.iDiidir. ншт
Odd. Sif