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Page 1: Optimizing Turbomachinery Controls Symposium... · Optimizing Turbomachinery Controls Symposium ... • Steam Turbine Control ... • While turbo-compressors & turbines can last >

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OptimizingTurbomachinery

ControlsSymposium

Houston, TXJune 2013

OptimizingTurbomachinery

ControlsSymposium

Houston, TXJune 2013

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China

Des Moines

Amsterdam

Abu Dhabi

Italy

Australia Brazil Moscow

CCC Global FacilitiesCCC Global Facilities

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Mission StatementMission StatementCCC collaborates with customers to deliver reliable solutions for critical turbo machinery control applications that result in tangible economic benefits.

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Participant IntroductionsParticipant Introductions

Any specific objectives for this session?

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Agenda – Day 1Agenda – Day 1

• Optimizing Turbomachinery Control / Financial impact • Compressor Classifications• Turbocompressor Control Techniques

– Measuring Distance from Surge– Auxiliary Equipment Selection– Specialized Antisurge Control Response– Performance (Process) Control Integration– Stand-alone Compressor Simulation– Using Recycle for Process Control

• Working with Turbocompressor Networks– Parallel Compressor Loadsharing

• Base-loading, Equal Flow, Equidistant Techniques

• TrainView Web Workshop – Attendee Operation

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Agenda – Day 2Agenda – Day 2

• Steam Turbine Control– Turbine Start-up & Shutdown Automation– Speed & Extraction Control Techniques and Demo

• Application Examples– LNG Liquefaction – Refrigeration Compressors– NGL Fractionation Facilities & Bayu Undan Example– Ammonia-Urea Unit Applications

• Process Control vs. Safety Shutdown Systems– System Availability and Fault Tolerance – API Standards Update

• Tips for Specification Writing

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Machinery

Process

Controls

Turbomachinery Controls

Turbomachinery Controls

AntisurgePerformance

SpeedExtraction

LoadsharingQuench

Flare

Centrifugal CompressorsAxial Compressors

Steam TurbinesGas TurbinesHot Gas Expanders

Cryogenic ExpandersPower Recovery Trains

LNGOffshore

FPSONGLGTL

Gas Transmission

PTAOlefinsRefiningAmmoniaMethanol Air Separation

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Major Challenges in System Design

Major Challenges in System Design

• Accurately Representing Compressor Operation:– Variable process conditions– Variable gas composition– Lack of flow elements in some sections

• Control Element Selection & Sizing– Valve selection & sizing– Transmitter range specification– Recycle piping arrangement– Designing for recycle cooling/quench

• High Speed Response:– Flat performance curves (especially near surge)– Desire for operating stability & efficiency– Desire to maximize the operating envelope

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Major Challenges in System Design

Major Challenges in System Design

• Dealing with Control Loop Interaction– Antisurge to antisurge decoupling– Antisurge to performance control decoupling– Coordinated mode switching between machines

• Loadsharing for Compressor Networks– Parallel, Series, & Compound arrangements

• Integrating Multiple Limiting Variables– Compressor limits– Driver limits– Process limits

• Maximizing Overall System Availability– Providing reliable control system redundancy– Effectively dealing with field equipment faults

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FinancialImpact ofOptimizing

TurbomachineryControl Systems

FinancialImpact ofOptimizing

TurbomachineryControl Systems

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Lifecycle CostsLifecycle Costs30-year life cycle costs for a 20,000 HP compressor

* Costs in constant dollars

Source: “Experiences in Analysis and Monitoring Compressor Performance”Ben Duggan & Steve LockeE.I. du Pont, Old Hickory, Tennessee24th Turbomachinery Symposium

Maintenance Cost$4.5 Million

Initial Cost $1.5 Million

Energy Cost$180 Million

97% of total costs

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Lifecycle CostsLifecycle Costs

Source: “Experiences in Analysis and Monitoring Compressor Performance”Ben Duggan & Steve LockeE.I. du Pont, Old Hickory, TennesseePresented at the 24th Annual Turbomachinery Symposium

30-year costs per a 1,000 HP

What can we control?

0.0

5.0

10.0

15.0

Initial Cost Maintenance Energy Lost Production

$ Millions

?

ControllableUncontrollable

* Costs in constant dollars

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Machinery Controls -Retrofit Economics

Machinery Controls -Retrofit Economics

• While turbo-compressors & turbines can last > 30 years, control systems can be obsolete < 10 years

• Newer control systems can offer:– Better performance & integration capabilities– Improved machinery protection– Better system availability

• More reliable digital electronic components• Improved system redundancy schemes• Improved self-diagnostic capabilities• Integrated predictive maintenance tools

• ROI can be extremely attractive due to the potential for: – Increases in process throughput– Increased “insurance” against catastrophic failures– Energy savings

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Compressor Types &

Classifications

Compressor Types &

Classifications

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Reciprocating (Piston) Air Compressors (aka Recips)

Reciprocating (Piston) Air Compressors (aka Recips)

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Rotary Screw Air Compressors

Rotary Screw Air Compressors

• Also Positive Displacement Machines • Normally 200HP to 1000HP

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Centrifugal CompressorsCentrifugal Compressors

• Widespread use, many applications• Gas is accelerated outwards by rotating impeller• Can be built for operation as low as 5 psi, or operation

as high as 10,000 psi (35 kPa - 55,000 kPa)• Sizes range from 200 HP to 95,000 HP

Single Case Compressor Centrifugal ImpellerImpellers

Diffusers

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Compressor inlet nozzle

Thrust bearing

Journal bearing

Shaft and labyrinth seal

Impeller inlet labyrinth seals

Discharge volutes

Impellers

Drive coupling

Casing (horizontally split

flange) Compressor discharge nozzle

Cross Section of Horizontal SplitCross Section of Horizontal Split

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Horizontal-Split Turbocompressor

Horizontal-Split Turbocompressor

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Centrifugal Plant Air Package

Centrifugal Plant Air Package

Inlet Air Filters

Inlet Guide Vanes

Auxiliary Lube Oil Pump

After Cooler

Controls

Electric Motor Drive

InterCoolers

Gear Box

Driver Shaft

ImpellersOil Reservoir

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Multi-Section with Bull GearMulti-Section with Bull Gear

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Compressor volute

Pinion shafts

2nd Stage impeller

Drive coupling

Labyrinth seals

Main drive gear

Inlet guide vanes

Bull-Gear Driven MachineBull-Gear Driven Machine

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Barrel-Type CentrifugalBarrel-Type Centrifugal

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Barrel-Type CentrifugalBarrel-Type Centrifugal

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Axial CompressorsAxial Compressors

• Gas flows in direction of rotating shaft• Can be built for lower pressures only

– (10 to 100 psi discharge pressures)

• Very efficient for high flow applications• Not as common as centrifugals

RotorBlades

Casing

StatorBlades

Stator BladesRotor Blades Shaft

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Axial Compressor InternalsAxial Compressor Internals

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Compressor outlet nozzle

Rotor blades

Labyrinth sealsBlade actuator

linkage

Compressor rotor

Compressor inlet nozzle Thrust bearing

Adjustable stator blades

Axial-Hybrid CompressorAxial-Hybrid Compressor

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Single-Section, Three-Stage Single-Case, Two-Section, Six-Stage

Two-Case, Two-Section, Six-Stage

Series Network

Parallel Network

Compressor System Classifications

Compressor System Classifications

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Compressor Control

Solutions

Compressor Control

Solutions

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Critical Success FactorsCritical Success Factors

• Prevent unnecessary process trips and downtime

• Minimize effect and duration of process disturbances

• Prevent surge, overspeed, overheating, and associated damage

• Automate startup and shutdown

1. Reliability

2. Efficient Operation

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Critical Success FactorsCritical Success Factors

• Maximize process throughput

• Minimize setpoint deviation

• Optimize loadsharing

• Minimize antisurge recycle or blow-off

• Operate at lowest energy level

1. Reliability

2. Efficient Operation

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Critical Success FactorsCritical Success Factors

• Prevent unnecessary process trips and downtime

• Minimize effect and duration of process disturbances

• Prevent surge, overspeed, overheating, and associated damage

• Automate startup and shutdown

1. Reliability

2. Efficient Operation

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Cost of the Problem Middle East LNG Project

Cost of the Problem Middle East LNG Project

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Critical Success FactorsCritical Success Factors

• Maximize process throughput

• Minimize setpoint deviation

• Optimize loadsharing

• Minimize antisurge recycle or blow-off

• Operate at lowest energy level

1. Reliability

2. Efficient Operation

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Increased ProductionIncreased ProductionEthylene Plant Example / Charge-Gas Compressor

– Every 0.1 bar (1.5 psi) increase in 3rd stage Pd provides annual production increase of approx. 1.5 %

– An average reduction of 0.1 bar (1.5 psi) in 1st Stage Ps (coil outlet pressure) provides an estimated 1% increase in Yield

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Increased ProductionIncreased Production• Steel Mill Example

– Hot Metal production is directly proportional to the mass flow of “wind to the furnace”

– Loss of flow during stove-filling procedures in the range of .5 to 1.5% of total flow (...production)

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Developing the Compressor Curve

Developing the Compressor Curve

Pd Discharge Pressure (P2)Pc Differential Pressure (Pd - Ps) or (P2 - P1) Rc Pressure Ratio (Pd/Ps) or (P2/P1) Hp Polytropic HeadRc

Qs, normalQs, massQs, vol

Compressor curve for a specific

speed N1

Rprocess,1

Q1

Rc1

Rprocess,2

Q2

Rc2

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s

c

2, volume

Adding Control Margins

Process Limit

Power Limit

Maximum Speed

Actual Available Operating Zone

Stonewall or Choke LimitStable Zone of

Operation

Minimum Speed

Surge Limit

s

c

2, volume

Integrating Multiple Limiting Variables

Integrating Multiple Limiting Variables

Adding Control Margins

Process Limit

Power Limit

Maximum Speed

Stonewall or Choke Limit

Minimum Speed

Surge Limit

Your turbomachinery control system must move smoothly in and out of compressor and driver limits while providing effective process control and stability

Stable Zone of Operation

Actual Available Operating Zone

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What is Surge?What is Surge?

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Surge DescriptionSurge Description

• Flow reverses in 20 to 50 milliseconds

• Complete surge cycle in 300ms to 3 seconds

• Compressor vibrates

• Temperature rises

• “Whooshing” noise

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Consequences of SurgeConsequences of Surge

• Rapid flow and pressure oscillations

• Exponential temperature increase

• Process instability & lower efficiency

• Potential machine damage• Trips may occur• Conventional instruments and

operators may fail to recognize surge

TIME (sec.)

1 2 3

TIME (sec.)1 2 3

FLOW

PRESSURE

TEMPERATURE

TIME (sec.)1 2 3

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Consequences of SurgeConsequences of Surge

Damage on axial compressor ‐ rotor →

Damage on axial← compressor – stator 

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• Pressure drops and forward flow is reestablished

• Compressor reaches surge point A• At this point the potential energy in the vessel

exceeds the capability of the compressor

Qs, vol

Pd

• As pressure builds, resistance goes up, operating point “draws” the perf curve

• Because Pv > Pd(max) , the flow reverses

Pd = Compressor discharge pressurePv = Vessel pressure

Developing the Surge CycleDeveloping the Surge Cycle

Pd

Pv

B A

CD

• From A to B….20 - 50 ms…….. Drop into surge• From C to D....20 - 120 ms…… Jump out of surge• A-B-C-D-A….0.3 - 3 seconds…… Surge cycle

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Factors Leading to SurgeFactors Leading to Surge

• Machine/Process startup and shutdown• Operation at reduced throughput• Operation at heavy throughput with:

– Process upsets / Load changes – Operator errors– Gas composition changes– Cooler problems– Filter or strainer problems– Driver problems / Power loss / Trips

• Surge is not limited to times of reduced throughput, it can and does occur under full operation

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Surge VideosSurge Videos

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Calculating Distance from

Surge

Calculating Distance from

Surge

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Distance from SurgeDistance from Surge

Fact:– The more inaccuracy in the measurement of distance to surge,

the farther we’ll need to stay from the surge limit to ensure reliable operation

Challenge:– The compressor surge limit moves with compressor inlet

conditions: Temperature, Pressure, and gas composition

– The antisurge system should provide a distance to surge calculation that is invariant of any change in inlet conditions

– This will lead more reliable surge protection while reducing the required surge control margin:

• Larger turndown range on the compressor

• Reduced energy consumption during low load conditions

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OEM Provided Coordinate Systems

OEM Provided Coordinate Systems

• Typical compressor maps include: (Qs, Hp), (Qs, Rc), or (Qs, Pd) coordinates, where:

Qs = Suction flow / can be expressed as actual or standardized volumetric flow

Hp = Polytropic Head

Rc = Compressor Ratio (pd / ps)

pd = Discharge pressure of the compressor

ps = Suction pressure of the compressor

ks = Exponent for isentropic compression

• These maps are defined for (1) specific set of inlet conditions: Ps, Ts, MW & ks

• Assume isentropic process (no changes in gas composition or in system entropy)

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Limitations of OEM Coordinate SystemsLimitations of OEM

Coordinate Systems• These coordinates are NOT invariant to suction

conditions as shown

• For control purposes we want the SLL to be presented by a single curve for a fixed geometry compressor

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Distance From Surge is a Moving Target

Distance From Surge is a Moving Target

• Most all process compressors will also have to operate in off-design conditions

• Automatic antisurge control must be able to operate under varying operating conditions:– Suction Temperature

– Suction Pressure

– Gas Composition

– Rotational SpeedDesign Nitrogen Off-gasMW MW MWPs Ps PsTs Ts Tsks ks ks

hr

qr2

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Distance From Surge is a Moving Target

Distance From Surge is a Moving Target

• A map based on polytropic head & volumetric flow coordinates is much closer to invariant when inlet conditions change, however:– There are no Hp transmitters

available

– Gas analyzers are generally slow & unreliable for use in continuous control

– Multiple analyzing points would be necessary to calculate Zs and Zavg

hr

qr2

Design Nitrogen Off-gasMW MW MWPs Ps PsTs Ts Tsks ks ks

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Developing Invariant Coordinates

Developing Invariant Coordinates

Cp = Specific Heat at Constant PressureCv = Specific Heat at Constant Volume

p = Polytropic EfficiencyΔPo,s = Differential Pressure across orifice plate

at Suction

Where:Zs,d = Compressibility in Suction, Discharge

Zavg = Average Compressibility =Ts = Suction TemperatureRc = Compression Ratio = Pd = Discharge PressurePs = Suction Pressure

R = = Gas Constant

MW = Molecular WeightRu = Universal Gas Constant

Zs Zd+2

Pd

Ps

Equations for Polytropic Head & Volumetric Flow2 :

Equations for Polytropic Head & Volumetric Flow2 :

1 cR×savg R TZHp

PP

os

sQs

2

×s sR TZ

RuMW

= -kk p

1 Cp

Cvk = Specific Heat Ratio =

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Invariant CoordinatesInvariant Coordinates

Reduce each equation by a factor A:

A s sR TZ

Qs

A.

q2s,red

Pos

Ps2 s sR TZ

s sR TZHp

A

Rc 1 hp, red

.avg sR TZ

s sR TZ

From experience, we know that the ratio of Zavg/Zs varies negligibly. Assuming it to be constant over the compressor operating range:

q2 Pos

Pss,redh Rc

1p,red

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Calculation Calculation

The relationship between pressure & temperature in polytropic compression theory leads to a

practical way to measure :

Calculating improves system accuracy when:- Gas composition varies- Compressor efficiency changes (air compressors)

Ps

Pd

Ts

Td =

Solving for :

log

log

Ts

Td

Ps

Pd

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Working with Invariant Coordinates

Working with Invariant Coordinates

Compressor map drawn in reduced coordinates

OPL (Operating Point Line)

Reduced coordinates define a performance map which:

• Is invariant to changing inlet conditions

• Has one surge limit point for a given rotational speed and compressor geometry

• Permits calculation of the operating point without obtaining molecular weight and compressibility measurements

2Slope =

h

qOPL

p,red

s,red

Operating Point

hr

qr2

=q2 Pos

Pss,redh = Rc

s - 1sp,red

Surge Point

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Distance From Surge Calculation

Distance From Surge Calculation

Performance Curve

Operating Point

hr

qr2

Variable Ss defines the angular distance from the operating point to the surge point

The controller continuously calculates:

The ratio of the slope of the Surge Limit Line & the slope of the Operating Point line:

SlopeOPLSs =

SlopeSLL

The distance between the operating point and the surge limit:

d = 1 - Ss

OPL (Operating Point Line)

SLL (Surge Limit Line)

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CCC A/S Controller DeviationCCC A/S Controller Deviation

The controller calculates deviation from the SCL as:

DEV = d - b1

Where:d = 1 – SSb1 = the relative distance

between the SLL & the SCL

DEV represents the distance between the operating point and the surge control line

hr

qr2

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• The surge parameter is defined as: S f

qsr

r op 1

2(h )

,

• The function f1 returns the value of qr2 on the

SLL for input hr

• Non-linearity in the Surge Limit Line can be accommodated using a function based on a piecewise characterization of either map axis

Building the Surge Limit LineBuilding the Surge Limit Line

hr

hr

qr2SLL qr

2

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NOT invariant coordinates (Hp, Qs)

Advantage of Invariant Coordinates / Illustration (1)

Advantage of Invariant Coordinates / Illustration (1)

Invariant coordinates (hr, qr2)

Where:Hp = Polytropic headQs = Volumetric suction flowQr

2 = Reduced flow squaredhr = Reduced head

Choose the right coordinates for each antisurge application

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Advantage of Invariant Coordinates / Illustration (2)

Advantage of Invariant Coordinates / Illustration (2)

Invariant Coordinates

1500 2000 2500 3000 3500 4000 4500 50005

10

15

20

25

30

35

40Actual Surge Plot

Vol. Inlet Flow - ACFM [ACMH]

Dis

. Pre

ssur

e P

sig

1 1 1 1 1 12 2

22 2 2

3

3

33

3

3

44

44

44

5

55

5

5

5

6

6

6

6

6

6

-.4 -.2 0 .2 .4 .6 .8 1 1.2 1.4-.4

-.2

0

.2

.4

.6

.8

1

1.2Surge Points - Mode fA 65

Reduced Flow [none]

Red

uced

Hea

d

11

11

11

22

2

22

2

3

3

33

33

4

4

4

4

4

4

5

5

5

5

5

5

6

6

6

6

6

6

Curve 1: MW = 4.62; Ps = 6.033 kg/cm2 aCurve 2: MW = 5.90; Ps = 6.800 kg/cm2 aCurve 3: MW = 7.90; Ps = 14.900 kg/cm2 aCurve 4: MW = 8.20; Ps = 6.800 kg/cm2 aCurve 5: MW = 9.70; Ps = 14.900 kg/cm2 aCurve 6: MW = 10.8; Ps = 14.900 kg/cm2 a

Hydrogen Recycle CompressorVariant Coordinates

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Surge TestingSurge Testing

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Surge Testing:a Daily RoutineSurge Testing:

a Daily Routine

0 5 10 15 20 25 30 35 40.2

.25

.3

.35

.4

.45

.5

.55

.6

.65

“High Speed Recording of Inlet Flow”

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Why Surge Test?Why Surge Test?

• Maximizing operating envelope– Validating predicted compressor maps– Establishing accurate surge limit (or safe operating

point near surge)

• Field-testing compressor responses in process conditions through field devices– Actual transmitter field calibrations– Actual flow element installation– Actual process gas (in some cases)

• Determining signature of surge for proper configuration of surge detection system

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Why Surge Test?Why Surge Test?

• Testing surge control system response in difficult process conditions– Ensuring system is capable of preventing surge

and breaking surge cycle (if necessary)

• Field performance data available for future benchmarking– Can the machine develop enough head?– Can the compressor operate over the complete

range needed?

• Preventing unexpected surprises after commissioning

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Surge DetectionSurge Detection

Pressure and Flow Variations During a Typical Surge Cycle

100%

100%

0%

0%

Pd

Po

20 to 50 milli-seconds

1 TO 2 SECONDS

• Surge signature should be recorded during commissioning

• Rates of change for flow and pressure transmitters should be calculated

• Thresholds should be configured slightly more conservatively than the actual rates of change during surge

• Surge is detected when the actual rates of change exceed the configured thresholds

• The following methods have been used:

– Rapid drop in flow– Rapid drop in pressure– Rapid increase in temperature– Rapid drop in flow & pressure

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Typical CCC Surge TestTypical CCC Surge Test

• Procedure typically takes place with the compressor “off-process” or in nearly full recycle

• CCC engineer starts with predicted surge limit & default surge control margin

• Antisurge valve held in manual in partially open position

Operating Point

hr

qr2

Predicted Surge Limit Line

b1

Default Surge Control Line

Initial State

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Typical CCC Surge TestTypical CCC Surge Test

• The surge limit line (SLL) is moved to the right in a safe distance from the predicted surge limit

• The antisurge control margin (b1) is then set to “0” (no margin)

• The antisurge valve is slowly closed, moving the operating point to the temporary SCL/SLL (see next slide)

Operating Point

hr

qr2

“Safe” Surge Limit Line

K

Temporary Surge Control Line

b1= 0

Test Preparation

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Typical CCC Surge TestTypical CCC Surge Test• Antisurge controller is

placed in AUTO • CCC engineer slowly

decreases “K” thereby increasing the slope of the SCL/SLL

• The operating point follows the SCL/SLL moving ever closer to the actual surge limit

• This action is repeated in small steps, letting the process stabilize between movements

Operating Point

hr

qr2

“Safe” Surge Limit Line

-K

Temporary Surge Control Line

b1= 0

Moving Towards Surge

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Typical CCC Surge TestTypical CCC Surge Test

• At the actual surge point, a sudden drop in flow will occur

• Recycle TripTM and Safety OnTM work to break the surge cycle and reestablish stable control in a safe operating region

• Established K value (slope of the SLL) is evaluated in relation to existing data

hr

qr2

Confirmed Surge Limit Line

Surge Point

Touching Surge

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Typical CCC Surge TestTypical CCC Surge Test

• Test data is adjusted as necessary and entered into the antisurge control parameter set

• CCC engineer then enters a new surge control margin (b1) appropriate for ongoing operation of the controller

• Safety OnTM is then resetmoving the SLL back to the newly established and now field tested position

Operating Point

hr

qr2

b2

Re-establish Safe Margin

New Surge Control Line

Setting the controller

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Surge Test /Compressor Simulation

Surge Test /Compressor Simulation

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Example: Export Compressor Test

Example: Export Compressor Test

4000 6000 8000 10000 12000 14000 16000 18000 200001.8

2

2.2

2.4

2.6

2.8

3

3.2

3.4Qs vs Rc

Qs in AM^3/hr

Rc=

Pd/

Ps

*

*

*

*

*

*

1

2

3

4

5

6

Predicted Curve

Train A Tested CurveTrain B Tested Curve

• In this example, (2) “identical” compressors were surge tested during CCC system commissioning

• The predicted surge limit on Train A turned out to be significantly to the left of the predicted curve

• Thus, the test identified the potential for a wider operating range to be established on Train A

*

1

2

3

4

5

6

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Is Surge Testing Required?Is Surge Testing Required?

• Adequate set-up of the antisurge system without surge testing during commissioning is achievable in most cases, however:

- Our experience indicates that there are often significant differences between predicted compressor performance documentation (maps) and field test data collected

• Field service engineers should perform testing only with coordination & cooperation of the complete commissioning team

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FactorsAffecting

Surge Control Margin

FactorsAffecting

Surge Control Margin

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The Approach to Surge is FastThe Approach to Surge is Fast

• Performance curves are almost invariably flat near surge

• Even small changes in compression ratio cause large changes in flow

• Suction or discharge pressure controller will accelerate the operating point in the direction of surge

Rc

Qs100%

0

100%

0

100%

0

1 SEC.

Pd

PoA C

D

B

RcA CB

Pressure SP

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Factors Affecting Surge Control Margin

Factors Affecting Surge Control Margin

Larger Surge Control Margin– Inability to surge test– Less then ideal piping

configuration – High noise-to-signal ratio on

system inputs– Compromised recycle valve

response– Possible large process

disturbances– Flat curves

Smaller Control Margin– Surge testing with varying speeds

and process gas conditions– Ideal piping configuration– Clean and repeatable transmitter

signals– Fast & accurate recycle valve

response– NO large process disturbances– Steep performance curves

SCL 1

SLLSCL 2

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Influence of Controller Execution Time

Influence of Controller Execution Time

Analog controller

SLLSCL

100%

0%

Controlleroutput

100%

0%

A leading engineering firm was contracted to evaluate the effect of controller execution rates on system response• A dynamic controller-in-the-loop

simulation was built• An antisurge control application

was selected• Digital controllers were compared

to an analog controller• Analog controller tuned for

minimum overshoot• Digital controllers got the same

tuning parameters• All trials use the same

disturbance: closure of discharge block valve

Operatingpoint

Time

Time

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Analog vs. Digital Controller at 2 Executions per Second

Analog vs. Digital Controller at 2 Executions per Second

•201

1 C

ompr

esso

r C

ontr

ols

Cor

pora

tionAnalog controller

SLLSCL

100%

0%

100%

0%

SLLSCL

100%

0%

Controlleroutput

100%

0%

Operatingpoint

Digital controller(2 executions per second)

Time

Time

Time

Time

• Compressor surged• Large process upset would have resulted

Tuning same as analog controller

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Analog vs. Digital Controller at 10 Executions per SecondAnalog vs. Digital Controller at 10 Executions per Second

•201

1 C

ompr

esso

r C

ontr

ols

Cor

pora

tion

SLLSCL

0%

100%

0%Tuning same as analog controller

SLLSCL

100%

0%

100%

0%

Time

Time

• Compressor almost surged• Control system would have to be set up with bigger

surge control marginAnalog controller Digital controller

(10 executions per second)

Time

Time

Controlleroutput

Operatingpoint

SLLSCL

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Analog vs. Digital Controller at 25 Executions per SecondAnalog vs. Digital Controller at 25 Executions per Second

•201

1 C

ompr

esso

r C

ontr

ols

Cor

pora

tion

SLLSCL

100%

0%

100%

0%

Time

TimeTuning same as analog controller

SLLSCL

100%

0%

100%

0%

Time

Time

Controlleroutput

Operatingpoint

• Response of CCC digital controller nearly identical to the analog controller

• Adding specialized response algorithms to PI control will allow even smaller surge margins

Analog controller Digital controller(25 executions per second)

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PipingLayout

Considerations

PipingLayout

Considerations

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Piping Layout ConsiderationsPiping Layout Considerations• Piping layout significantly influences controllability• The primary objective of the antisurge controller is to

protect the compressor against surge• This is achieved by lowering the resistance to

compressor flow through opening the antisurge valve• Dead-time & lag-time should be minimized• This is achieved by minimizing the volume between

three flanges:– Discharge flange of

the compressor– Recycle valve flange– Check valve flange

volume to be minimized

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Using a Single Antisurge ValveUsing a Single Antisurge Valve

Section 1 Section 2

• In order to protect section 1 the antisurge valve needs to be opened• The volume between compressor discharge, check valve and antisurge

valve determines the dead time and lag time in the system• Large volume significantly decreases the effectiveness of the antisurge

protectionResults:

– Poor surge protection– Large surge margins– Energy waste– Process trips because of surge

Large volume

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Sharing Recycle CoolersSharing Recycle Coolers

• The piping configuration for section 2 is excellent for surge protection• Minimum volume between the three flanges• The piping configuration for section 1 is not ideal as there is a large

volume of process gas to be de-pressurized

Results:- Poor surge protection- Large surge margins- Potential energy waste- Potential process trips due to surge

Large volume

Small volume

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Improving Control ResponseImproving Control Response

• Compressor 1 has ideal piping for surge protection as the volume between the three flanges is minimized

Minimum volume

• The piping layout for Compressor 2 is common but not optimum from an antisurge system response point of view - The cooler creates additional volume and decreases the effectiveness of the antisurge control system

Increased volume due to

cooler

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Optimum Surge ProtectionOptimum Surge Protection

• This compressor has ideal piping configuration for surge protection as the process volume is minimized between the three flanges for all sections

Minimum Volume

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Which Piping Configuration Would you Choose?

Which Piping Configuration Would you Choose?

• Configuration #1 has minimum volume between the flanges and is the best layout for antisurge control reaction time

• Configuration #2 requires one less cooler less / capital investment is lower and cooler maintenance costs are reduced

• Configuration #2 will require bigger surge control margins

Piping Configuration #1

Piping Configuration #2

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Specialized Control

Response

Specialized Control

Response

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Coping with the High Speed of Approaching Surge

Coping with the High Speed of Approaching Surge

• Maximize speed of response– Transmitters– Valves– System volumes– Controllers

• Utilize specialized control responses– “Predictive” response algorithms– Automated open loop (Recycle TripTM)– Adaptive surge control line– Control loop decoupling

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Basic AntisurgeControl SystemBasic AntisurgeControl System

• The antisurge controller UIC-1 protects the compressor against surge by opening the recycle valve

• Opening of the recycle valve lowers the resistance felt by the compressor, reducing Rc and increasing flow

This takes the compressor away from surge

Rc

qr2

Rprocess

Rprocess+valve

FT PdTPsT1 1 1

UIC1

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The Surge Control Line (SCL)The Surge Control Line (SCL)

• When the operating point crosses the SCL, PI control will open the antisurge valve

• PI control will give adequate protection for small disturbances

A

Rc

B

SLL = Surge Limit Line

SCL = Surge Control Line

qr2

• PI control is tuned to provide stable control during steady state operation on the SCL

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The Recycle Trip® Line (RTL)The Recycle Trip® Line (RTL)

• Disturbance arrives - the operating point moves past the SCL initiating Proportional & Integral (PI) control action

SLL = Surge Limit LineRTL= Recycle Trip® Line

SCL = Surge Control Line

Output to Valve

Time

• If the operating point hits the RTL, the conclusion is:– We are close to surge– The PI controller was too

slow to catch the disturbance

– Move the valve now!

Recycle Trip® Response

PI Control Response

Rc

Q2

OP

• An open loop response is triggered to open the antisurge valve at maximum actuator speed

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The Recycle Trip® Line (RTL)The Recycle Trip® Line (RTL)

• For large, short duration disturbances a fixed ramp out of the open loop response may hold the antisurge valve open too long– Could result in an unnecessary loss of process flow– Antisurge controller should utilize its distance from surge

calculation to accelerate the exponential decay

Output to Valve

Time

PI Control ResponseRecycle Trip® Response

• After the operating point moves back to the safe side of RTL, the open-loop function should be ramped out– PI controller will stabilize the

operating point on the SCL until normal process flow in re-established

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Output to Valve

Time

PI Control Response

Total Response

PI Control Recycle Trip®

Action

+To antisurge valve

• Total response of the controller is the sum of thePI control and the Recycle Trip® action

Benefits:– Wider operating envelope is created

due to reduced SCL margin requirement

– Energy savings due to smaller required surge margins

– Surge can be prevented for virtually any disturbance

The Recycle Trip® Line (RTL)The Recycle Trip® Line (RTL)

Recycle Trip® Response

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Improving the Accuracy of Recycle Trip®

Improving the Accuracy of Recycle Trip®

• Open loop response is the fastest way to get the antisurge valve open– But, open loop control lacks the accuracy needed to precisely

position the antisurge valve

• By definition, open loop corrections of a fixed magnitude are often either too big or too small for any specific disturbance– The rate of change of the position of the compressor operating

point has been proven to be an excellent predictor of the strength of the disturbance

– This derivative calculation can be used to adjust the magnitude of the open loop response

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d(Ss)dt

C = C1Td

Output to valve

Time

where:• C = Actual step to the valve• C1 = Constant - also defines

maximum step• Td = Scaling constant• d(Ss)/dt = Rate of change of the

operating point

Medium disturbance

PI ControlRecycle Trip®

Total

Large disturbanceOutput to valve

Time

PI Control

Recycle Trip®

Total

Recycle Trip® Based on Derivative of Ss

Recycle Trip® Based on Derivative of Ss

Benefits:• Maximum protection

– No surge– No compressor damage

• Minimum process disturbance– No process trips

Recycle Trip®

Response Calculation:

100%

0%

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CCC’s Derivative Response Algo

CCC’s Derivative Response Algo

A

Rc

B

• When the operating point moves quickly towards the SCL, the rate of change (dS/dT) is used to dynamically increase the surge control margin

• PI controller reacts earlier• Smaller steady state surge

control margins can be used without sacrificing reliability

Q2

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Additional surge margin

Benefits of Safety On® response:- Continuous surging is avoided- Operators are alarmed about surge

The Safety On® ResponseThe Safety On® Response

Compressor can surge due to:– Transmitter calibration shift– Sticky antisurge valve or

actuator– Partially blocked antisurge

valve or recycle line– Unusually large process upset

• If Operating Point crosses theSafety On® Line the compressor is in surgeRc

qr2

SLL - Surge Limit LineRTL - Recycle Trip® LineSCL - Surge Control Line

• The Safety On® response shifts the SCL and the RTL to the right

New SCL

New RTL

• Additional safety or surge margin is added

• PI control and Recycle Trip® will stabilize the machine on the new SCL

SOL - Safety On® Line

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Automated Fallback StrategiesAutomated Fallback Strategies

• Statistically over 75% of control loop problems originate from field devices

• The antisurge system should have fallback strategies to handle transmitter failures problems

• System should continuously monitor input validity • Input problems/failures should initiate a fallback mode

of operation without a machine/process trip

Benefits:– Nuisance Trip Avoidance– Latent Failure Alarm– Increased Machine & Process Availability

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Compressor Performance

Control

Compressor Performance

Control

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Performance ControlPerformance Control

• Also called:– Throughput control– Capacity control– Process control

• Matches the compressor throughput to current process requirements

• Typical Main Process Variables:– Suction pressure– Discharge pressure– Net flow to the user

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PIC - SP

• Compressor operates in point A

Pd

qr2

Shaft power

qr2

Curve 1

ARprocess + Rvalve

• Required power in point A is P1

Curve 1P1

• Pressure is controlled by blow-off

• Point B represents the point that would deliver the pressure for Rprocess

Curve 2

Rprocess

B

• Required power in point B is P2

Curve 2

P2

• Power loss is P1 - P2

• Qloss represents energy waste

Qloss

Performance Control by Blow-off or Recycle

Performance Control by Blow-off or Recycle

Notes:• Most inefficient control

method• Regularly found in plant air

systems• Rare in other systems• Not recommended• Curve 2 represents:

• Lower speed on variable speed systems

• IGVs closed on variable geometry compressors

• Inlet valve throttled on fixed speed compressors

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Performance Control by Discharge Throttling

Performance Control by Discharge Throttling

• Compressor operates in point A

Pd

qr2

Shaft power

qr2

Curve 1

ARprocess + Rvalve

• Required power is P1

Curve 1P1

• Pressure is controlled by pressure drop over valve

PIC - SP

Pressure loss across valve

• Opening of valve would reduce resistance to Rprocess

Rprocess

• Lower resistance would require less speed and power

Curve 2

Curve 2

P2

• Power loss is P1 - P2

Notes:• Extremely inefficient (consumes

approximately the same power for every load)

• Rarely used• Not recommended• Curve 2 represents:

• Lower speed on variable speed systems

• IGVs closed on variable geometry compressors

• Inlet valve throttled on fixed speed compressors

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• Inlet valve manipulates suction pressure

Pd

qr2

Shaft power

qr2 • Changing suction pressure

generates a family of curves

Suction valve open

Suction valve throttled

• Pressure is controlled by inlet valve position

PIC - SP

• Compressor operates in point A for given Rprocess

ARprocess

• Required power is P1

P1

Performance Control by Suction ThrottlingPerformance Control by Suction Throttling

Notes:• Common on electric motor

machines• Much more efficient than

discharge throttling• Power consumed changes

proportional to the load• Throttle losses are across

suction valve

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• Change of guide vanes angle a results in different compressor geometry

Pd

qr2

Shaft power

qr2

• Different geometry means different performance curve

aminaOP

amax

• Pressure is controlled by inlet guide vane position

PIC - SP

• Compressor operates in point A for given Rprocess

A

Rprocess

• Required power is P1

P1

Performance Control by Adjustable Guide Vanes

Performance Control by Adjustable Guide Vanes

Notes:• Improved turndown• More efficient than suction

throttling • Power consumed is

proportional to the load• Power loss on inlet throttling

is eliminated

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• Changing speed generates a family of curves

Pd

qr2

Shaft power

qr2

Nmin

NOP

Nmax

• Pressure is controlled by speed of rotation

PIC - SP

• Compressor operates in point A for given Rprocess

A

Rprocess

• Required power is P1P1

Performance Control by Speed Variation

Performance Control by Speed Variation

P1

PI1

SI1

Notes:• Most efficient: (Power » f(N)3) • Steam turbine, gas turbine or

variable speed electric motor• Typically capital investment

higher than with other systems• No throttle losses

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Control Loop Interaction

Control Loop Interaction

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Control Loop InteractionsControl Loop Interactions

• An optimized turbomachinery control system should incorporate all continuous control aspects of the machine

• Each continuous control loop interacts with other “local” and active control loops

• Interactions can negatively affect:– Machinery protection– Process stability & protection– Energy efficiency

• A common, less than optimum solution– Performance (process) control in DCS– Independent turbine speed governor– Independent antisurge control system

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Antisurge & Process Controllers will Interact

Antisurge & Process Controllers will Interact

• The antisurge controller and the process controller(s) manipulate the same variable:– The operating point of the compressor

• Multiple control loops on a single PV will interact when both loops are active– The control action of each controller affects the other

• The controllers have different and sometimes conflicting objectives

• Interaction with the A/S system begins on the surge control line where control stability is most important

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Common Methods of Coping with Loop Interactions

Common Methods of Coping with Loop Interactions

• De-tune the loops to minimize interactionResult - poor pressure control, large surge control margins and poor surge protection

• Put one loop on manual, so interaction is not possible. Operators will usually put the antisurge control in manualResult - no surge protection and often partially open antisurge valve

• Decouple the interactionsResult – loop stability, minimized setpoint deviation, more effective surge protection, and smaller surge control margins

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Interacting Process & Antisurge Loops

Interacting Process & Antisurge Loops

PIC-SP

• The disturbance and the PIC control response moves the operating point toward surge

A

Q2

Rc

• As Rc rises, the PIC works to reduce throughput through inlet throttling or asking for lower speed

• Interaction starts at B as the antisurge controller starts to operate

• PIC continues to push the OP towards surge, along the resistance curve

• At B, the a/s controller begins to open the a/s valve reducing Rc and increasing flow

B

The resultant vector from these 2 forces will look something like this:

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Control Loop DecouplingControl Loop Decoupling

• Loop interaction:– Causes instability– Increases the risk of surge– Increases setpoint deviation– Increases safe margin

requirement

PIC-SPA

Q2

Rc

C

B

• Using loop decoupling, the a/s controller asks the process controller to simultaneously increase speed or open the inlet device

• The combination of the decoupled process control output and the a/s valve opening provides a much more directly counteractive response to the direction of the disturbance

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Single Compressor SimulationSingle Compressor Simulation

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UIC1

UIC2

PIC1

SIC1

Loop Decoupling for Multiple Antisurge Controllers

Loop Decoupling for Multiple Antisurge Controllers

Disturbance comes from the discharge side• Pd,2 increases• Ps,2 remains constant• Rc,2 increases• Section 2 moves towards surge

Antisurge controller UIC-2 will open the recycle valve to protect Section 2 against surge

• Pd,2 decreases• Ps,2 increases• Rc,2 decreases• Section 2 moves away from surge

Rc,2

qr,22

R

R

Disturbance

Section 1 Section 2

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UIC1

UIC2

PIC1

SIC1

Loop Decoupling for Multiple Antisurge Controllers

Loop Decoupling for Multiple Antisurge Controllers

Opening the recycle valve on Section 2 causes Ps,2 to increase / Result:

• Pd,1 increases• Rc,1 increases• Section 1 moves towards surge

UIC-1 will open its recycle valve to protect Section 1 against surge

• Pd,1 decreases• Ps,1 increases• Rc,1 decreases• Section 1 moves away from surge

Rc,1

qr,12

R

R

Section 1 Section 2

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UIC1

UIC2

PIC1

SIC1

Loop Decoupling for Multiple Antisurge Controllers

Loop Decoupling for Multiple Antisurge Controllers

Opening of recycle valve on Section 1 caused Pd,1 to decrease / Result:

• Ps,2 decreases• Rc,2 increases• Section 2 moves towards surge

• The system is oscillating• Slowing down controller

tuning could lead to:- Increased risk of surge

• Compressor damage• Process trips

- Larger surge margins• Energy waste

Section 1 Section 2

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Loop Decoupling for Multiple Antisurge Controllers

Loop Decoupling for Multiple Antisurge Controllers

• Interacting antisurge control loops need to communicate in real time to coordinate their control actions

• When UIC-2 opens the recycle valve:- Section 2 will be protected against surge- Section 1 will be driven towards surge

• How much Section 1 is driven towards surge depends on how much the recycle valve on Section 2 is opened

• The output of UIC-2 is sent to UIC-1 to inform UIC-1 about the disturbance • The same applies when Section 1 antisurge valve is opened first

The decoupling signal should be conditional, based upon a/s deviation

Section 1 Section 2

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Advanced Loop DecouplingAdvanced Loop Decoupling

• Control functions should be integrated for coordinated mode switching required during start-up, shutdown, & trip scenarios

• Decoupling is required to avoid negative interactions between antisurge & pressure control loops

• Decoupling is required between antisurge control loops to prevent instability & excess recycle

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Recycling for Capacity Control

Recycling for Capacity Control

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Capacity Control & Recycle Valve Selection

Capacity Control & Recycle Valve Selection

• Designers have the choice of using the antisurge control valves or dedicated recycle valves for capacity control – Advantages of dedicated valves include:

• Process control selection criteria can be separated from the antisurge valve selection criteria

• Low-noise trim & erosion resistant trim can be applied to the capacity control valves only

• Can be considered a redundant valve arrangement• Opening of the a/s valves can be alarmed as

“abnormal operation”– Advantages of using the A/S valve(s) include:

• Reduced space requirements • Reduced weight (offshore issue)• Reduced installation costs (valves & piping)

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Use of Common Recycle Valve for Capacity Control

Use of Common Recycle Valve for Capacity Control

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Adding the “S” Control Line to the Compressor Map

Adding the “S” Control Line to the Compressor Map

XIC uses a low-select on the DEV calculation(s) of the associated A/S controllers

Q2

RcSLL SCL XCL

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Hot & Cold Recycle ValvesHot & Cold Recycle Valves

• “S” Controllers used on cold recycle lines/valves for capacity control requirements– Low noise & anti-corrosion trim can be added to these valves

• Hot recycle used for short bursts of flow when UIC control line is crossed & for extra “trip Cv” as needed– Operating point will settle out on the cold recycle line during

low-load conditions

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Loadsharing for Compressor Networks

Loadsharing for Compressor Networks

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Control System Objectivesfor Parallel Compressors

Control System Objectivesfor Parallel Compressors

• Maintain precise control of the primary process variable (pressure or flow)

• Provide integrated and bumpless limiting variable control including surge control

• Optimally divide the load between the compressors in the network, while:– Minimizing the possibility of machine trips due to

surge, vibration, over-speed, etc.– Maximizing production throughput– Minimizing energy consumption– Minimizing disturbances of starting and stopping

individual compressors

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Operators select desired speed setpoint for the base-load machine

Base Loadingfor Parallel Compressor Operation

Base Loadingfor Parallel Compressor Operation

SIC1

SIC2

UIC1

PIC1

UIC2

~

SwingMachine

Base Loaded Machine

Setpoint

Process

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Base Loadingfor Parallel Compressor Operation

Base Loadingfor Parallel Compressor Operation

Rc,1

qr,12

Rc,2

qr,22

Compressor 1 Compressor 2

• Compressors operate at same Rc since suction and discharge are common

PIC-SP

Swing machine Base machine

• Base compressor is fully loaded and runs without recycle while the other(s) absorb the load swings

QC,2= QP,2

• Swing compressor can be running with recycle

QP,1

Where:QP = Flow to processQC= Total compressor flowQC - QP = Recycle flow

• Load could be re-divided to eliminate recycle

QP,1 QP,2QC,1

QP,1 + QP,2 = QP,1 + QP,2

Notes:- Base loading can lead to inefficient operation- Base loading increases the risk of surging the swing

compressor as it will take the worst of any disturbance- Base loading requires frequent operator intervention- Base loading is NOT recommended

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“Equal Flow” Controlfor Parallel Compressor Operation

“Equal Flow” Controlfor Parallel Compressor Operation

• Process control action is independent of the antisurge control• Higher capital cost due to extra flow measurement devices (FMD)• Higher energy costs due to permanent pressure loss across FMDs

SIC1

SIC2

UIC1

PIC1

UIC2

FIC

1

FIC2

SPProcess

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“Equal Flow” Controlfor Parallel Compressor Operation

“Equal Flow” Controlfor Parallel Compressor Operation

• Compressor 2 can operate with recycle while Compressor 1 has turn down

• Compressors operate at same Rc since suction and discharge are common

• Bias relays only work under a single set of conditions with matching compressor maps

Rc,1

qr,12

Rc,2

qr,22

PIC-SP

QP,1 QP,2

Equal flow Equal flowQP,1 = QP,2

Compressor 1 Compressor 2

where:QP = Flow to processQC= Total compressor flowQC - QP = Recycle flow

• Experience has shown that even identical compressors may differ by up to 20% in performance and surge limit mapping

Notes:• Requires additional capital investment in FMDs• Requires additional energy due to permanent

pressure loss across FMDs• Poor pressure control due to positive feedback in

control system (see next)• Equal flow division is NOT recommended

QC,2

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Q2

Rc

N1

N2

N3

• In a classic cascade control scheme, the slave controller needs to be tuned 4-5 times faster than the master controller

• In steady state operation, the machine is operating at the intersection of its:• Resistance Curve• Speed Curve • PIC-1 Setpoint• FIC-1 Setpoint

R1

PIC-SP

FIC-SP

OUTRSP

OUTRSP

Master Slave

• The Master Pressure Controller (PIC-1) provides the remote setpoint for Flow Controller (FIC-1), which sets the speed setpoint for SIC-1

A

PIC1

FIC1

SIC1

“Equal Flow” ControlDynamic Control Problem

“Equal Flow” ControlDynamic Control Problem

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Q2

Rc

N1

N2

N3

A

R1

FIC-SP

R2

BC

D

Scenario: A process disturbance causes the resistance curve to move from R1 to R2 , shifting operating point to B

• Since the PIC-1 loop gain is slow, its output (FIC-1’s setpoint) moves slowly

• FIC-1 reacts quickly trying to maintain its setpoint, speeding up the machine to point C at speed N2

• PIC-1 slowly reduces FIC-1’s setpoint and the primary process control variable (pressure) setpoint is finally restored at speed N3

• The control system response actually amplifies the disturbance

Notes:• Can cause significant

instability near surge

• Results in unnecessary process setpoint deviation

• Traditional pressure to flow cascade systemsare NOT recommended

OUTRSP

OUTRSP

Master Slave

PIC1

FIC1

SIC1

PIC-SP

“Equal Flow” ControlDynamic Control Problem (cont.)

“Equal Flow” ControlDynamic Control Problem (cont.)

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Equidistant LoadsharingEquidistant Loadsharing

• LSICs get their PV from their companion A/S controller and their setpoint from the MPIC

• All controllers should coordinate their control responses in real-time

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Equidistant LoadsharingEquidistant Loadsharing

• Machines operate at same Rc

PIC-SP

• The DEV is a dimensionless number representing the relative distance between the operating point and the SCL

0.10.2

0.3

DEV = 00.1

0.20.3

• Machines are kept at the same DEV which may correspond to different speeds and flow rates

DEV1 DEV2

• Recycle will only start when all machines are on their SCL• Since DEV is dimensionless, all sorts and sizes of machines can

be operated together: large, small, ST & motor driven

SCL = Surge Control LineRc,1

qr,12

Rc,2

qr,22

Compressor 1 Compressor 2

Dev1 = Dev2Q1 = Q2N1 = N2

Notes:• Maximum system turndown without recycle or blow-off• Minimizes the risk of surge since all machines’ (recycle valves)

absorb part of the disturbance• Automatically adapts to different types of compressors• CCC patented algorithm

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Loadsharing Overview (Simplified)

Loadsharing Overview (Simplified)

PID

+

Analog Inputs

+

DEV

To antisurge valve To performance control element

PV

PV

SP

DEV DEV

DEV

DEV from other loadsharing controllers

SP

POC SP

POC PV

PrimaryResponse

Load Balancing

Average

PrimaryResponse

fA Mode

PI(One Sided)

RTPI

LoopDecoupling

Loop Decoupling

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MPIC

1

To performance control element

The Primary ResponseThe Primary Response• Master controller (MPIC) controls the

main Process Variable (PV) via its PID control block

• The output of the MPIC PID goes to the primary response block in the loadsharing controller

• In the primary response block, the controller checks if the machine is close to the SCL:– Yes: don’t reduce compressor

throughput– No: reduce compressor throughput

as necessary• Apply loadsharing gain M0

PV PID

• The primary loop gain of MPIC goes directly to the performance control element via the primary response block Primary

Response

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The Primary ResponseThe Primary Response• In order to check if the machine is

close to the SCL, the LSIC primary response block needs the A/S DEV

• The DEV is reported by the UIC• When the machine is close to the

SCL, MPIC output changes will be redirected from the LSIC to the UIC

• When DEV < or = 0, further reduction of machine throughput is handled through modulation of the antisurge valve

MPIC

1PIDPV

PrimaryResponse

DEV

To antisurge valve

PrimaryResponse

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Load Balancing ResponseLoad Balancing Response

• In order to maintain equal distance from surge, each compressor needs to be kept at the same antisurge DEV

• The antisurge controller reports its current DEV to the load balancing block in the loadsharing controller

• This reported DEV becomes the Process Variable (PV) for the load balancing PID loop in the LSIC

• The loadsharing controller also reports this DEV to the MPIC

PID

PrimaryResponse

DEV

Load Balancing

PV

DEV

PV

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Load Balancing ResponseLoad Balancing Response

• The MPIC sends the average DEV to all LSICs as the set point for all load balancing blocks

• The load balancing block works to carefully balance the DEVs on all running compressors

• Its output is added to the total output to the performance control element

PID

PrimaryResponse

DEV

Load Balancing

Average

To performance control element

PV

DEV

SP

PV

DEV from other LSICs

• Other loadsharing controllers also report their DEV to the master controller to be averaged

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Loadsharing Overview (Simplified)

Loadsharing Overview (Simplified)

PID

+

Analog Inputs

+

DEV

To antisurge valve To performance control element

PV

PV

SP

DEV DEV

DEV

DEV from other loadsharing controllers

SP

POC SP

POC PV

PrimaryResponse

Load Balancing

Average

PrimaryResponse

fA Mode

PI(One Sided)

RTPI

LoopDecoupling

Loop Decoupling

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TrainView Web Workshop: Parallel Compressor Simulation

TrainView Web Workshop: Parallel Compressor Simulation