thermodynamic and economic evaluation of a small-scale organic rankine cycle integrated with a...
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Thermodynamic and economic evaluation ofa small-scale organic Rankine cycle integratedwith a concentrating solar collector
Milad Ashouri1, Fatemeh Razi Astaraei1*, Roghaye Ghasempour1, M.H. Ahmadi1
and Michel Feidt21Renewable Energies and Environmental Department, Faculty of New Science andTechnologies, University of Tehran, Tehran, Iran; 2Laboratoire d’Energetique et deMecanique Theorique et Appliquee, ENSEM, 2, Avenue de laForetde Haye, 60604,Vandoeuvre 54518, France
*Corresponding author:
AbstractRecently, distributed power systems especially with renewable sources have shown an increasing demand
all over the world and have been a technical viable solution to demand growth for electricity. Among
these, solar-thermal power plants show a trustworthy source for electricity generation especially for rural
areas where small-scale plants are needed. Organic Rankine cycle (ORC) is a suitable power cycle for
electricity generation from low-grade heat and has shown a good compatibility with parabolic trough
solar collectors (PTCs). In this study, a PTC integrated with an ORC is being studied thermodynamically
and economically for small-scale electricity generation up to 100 kW electricity. Four schematics of the
cycle including the recuperation and superheating are examined. Effect of superheating and recuperating
was investigated on the thermal efficiency and costs of the system. A parametric study shows the effect of
key parameters such as turbine inlet temperature and pressure on the characteristics of the system such as
net work, thermal efficiency, oil temperature, overall heat transfer coefficient and heat transfer area of
shell-and-tube heat exchangers and also on costs of the system. Results show the dependence of the system
efficiency and system costs on the operating pressure of heat exchangers. Existence of the Recuperator
seems quite effective on increasing the cycle efficiency and, in some cases, lowering the total costs due to
lowering the condenser load. A comparison of different working fluids including benzene, butane,
pentane, isopentane, R123 and R245fa have been done to cover a wide range of operating pressures and
temperatures. Results show that benzene has the best thermodynamic performance among other fluids
followed by pentane, isopentane, R123, R245fa and butane. Also, benzene has the highest total cost
among other fluids followed by pentane, isopentane, butane, R123 and R245fa. This paper helps to
evaluate a solar ORC power plant both thermodynamically and economically.
Keywords: organic Rankine cycle; efficiency; solar collector; economic evaluation
Received 3 January 2015; revised 23 July 2015; accepted 24 July 2015
1 INTRODUCTION
Thermodynamics cycles have been put under investigation by
various authors. Ahmadi et al. [1] studied an Atkinson engine
and optimized the performance of the system using genetic algo-
rithm. Among these thermodynamic cycles, solar powered cycles
have been received much attention. Ahmadi et al. [2] optimized
a solar multi-step irreversible Brayton cycle based on normalized
power and thermal efficiency. They also designed a solar dish
Stirling for maximized thermal efficiency and power and also
performed a thermo-economic maximization to consider eco-
nomic parameters [3, 4]. Among these, organic Rankine cycles
(ORCs) have received much attention during last decade. This
cycle obeys the fundamental rules of conventional Rankine
cycles working with water in common plants but has some
advantages over water Rankine cycle which made it popular.
First, this cycle can work under low temperatures and pressures
in comparison to conventional Rankine cycle and shows a better
International Journal of Low-Carbon Technologies 2015, 0, 1–12# The Author 2015. Published by Oxford University Press.This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/), whichpermits unrestricted reuse, distribution, and reproduction in any medium, provided the original work is properly cited.doi:10.1093/ijlct/ctv025 1 of 12
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performance than water especially from low-grade heat sources
because its working fluids include a variety of hydrocarbons and
refrigerants and according to the range of accessible heat source
temperatures and pressures, different outputs can be derived by
using suitable working fluids, second, it can work without feed-
water heaters and multi-stage turbines which makes it simple
and low cost. Among these, solar parabolic trough collectors are
a huge source of thermal energy but with a low-grade heat
which makes it only suitable for some kilowatts to few megawatts
electricity generation, also it shows a reliable means for electri-
city generation especially in rural areas or near factories to meet
their demand without the need for connection to grid which
may be expensive. As mentioned before, the organic fluids used
in ORCs are divided into hydrocarbons and refrigerants, some
of them are dry fluids which mean they have a positive slope
T–S diagram in the saturation vapor region. This makes it pos-
sible for some organic fluids to work properly without super-
heating to a great extent and cause no damage to turbine. As
shown in this study, a comparison of different dry organic fluids
with and without superheating and recuperation has been done
to show the variations in cycle efficiency and performance of
the system which help us make a decision to choose the system
conditions according to our needs. The ORC has been put
under investigation by many authors. Le et al. [5] performed a
thermodynamic analysis and optimization of a supercritical
ORC driven by low-grade heat. Two cases of basic and regenera-
tive ORC were investigated. Results showed that R1234ze has the
best performance. Rayegan and Tao [6] developed a procedure
to select the working fluids in a solar ORC plant and found that
11 working fluids are suitable in solar ORCs that under low- or
medium-temperature solar collectors. Wang et al. [7] presented
a detailed analysis of ORC coupled with solar collector with a
thermal storage system during a whole day. McMahan [8]
designed and optimized a solar-thermal ORC with various
working fluids. Quoilin et al. [9] presented an optimization and
sizing procedure of heat exchangers in a small-scale solar-driven
ORC by pinch and pressure drop and optimized it by turbine
input pressure and evaporator temperature. Ferrara et al. [10]
compared different organic fluids in a 20 kWe solar plant and
chose acetone as the best organic fluid choice with supercritical
pressure. Le et al. [11] performed a thermodynamic and eco-
nomic analysis of a subcritical ORC using zeotropic working
fluids and water temperature at 1508C as a hot source. Pentane
showed the best exergetic performance and the lowest levelized
cost of electricity. The best maximized exergy efficiency cor-
responds to the working fluid mixture with the smallest
temperature glide. Under exergy efficiency maximization, pure
fluid-based ORCs present higher thermodynamic performances.
Wang et al. [12] performed a multi-objective optimization of
ORC with waste heat using the exergy efficiency and total capital
costs of the system as the objectives. The turbine inlet tempera-
ture, turbine inlet pressure, pinch and approach points of the
heat exchangers were introduced to be the key parameters of the
system for performing the optimization. Al-Sulaiman [13] pre-
sented an exergy analysis of a parabolic trough solar collector on
a steam Rankine cycle and an ORC bottoming cycle as the con-
denser. Result showed that the main sources of destruction are
trough collectors and the vapor generator. Also, the bottoming
cycle increased the exergy efficiency compared with a steam
Rankine cycle without the bottoming cycle. Each of the afore-
mentioned works in the literature focused on one type of ORCs.
In this study, four schematics of the cycle have been chosen to
study with respect to both thermodynamic and economics to
give a better evaluation of the solar ORC power plants. A
small-scale ORC driven by a parabolic trough solar collector was
simulated using a commercial software [14] interacting with
MATLAB for doing the energy balance of the system and sizing
procedure of heat exchangers for the system described.
2 THERMODYNAMIC MODEL
Schematics of solar ORC is presented in Figure 1. Also, the
process in T–S diagram is shown in Figure 2.
ORC fluid is pumped through economizer and is heated to
its saturation temperature. Then it enters evaporator in which
the two-phase mixture is transformed to pure vapor in constant
temperature, the third heat exchanger superheats the fluid and
raise the temperature in a constant pressure. Vapor in state 6
enters the turbine and delivers the power, because of the high
energy content of vapor in state 7, we can reuse its energy by
entering the fluid to a Recuperator to preheat the incoming sub-
cooled fluid before entering the economizer. The working fluid
enters the condenser at state 7 and is cooled to its saturated
liquid. Then, the pump raises its pressure to economizer pres-
sure and the cycle completes. The basic relations used in the
model are as follows [15].
Mass balance equation:
X
_mi ¼X
_mo ð1Þ
where _mi is the inlet mass flow rate (in kg/s) and _mo is the outlet
mass flow rate (in kg/s).
Energy balance equation:
Q�W ¼X
_moho �X
_mihi ð2Þ
where Q indicates heat (in kW), W work (in kW) and h is en-
thalpy of hot fluid (in kJ/kg).
Vapor generator (including economizer (Eco), evaporator
(Eva) and superheater (SH)):
QVG ¼ UAEcoDTLMTD;Eco þ UAEvaDTLMTD;Eva
þ UASHDTLMTD;SH ð3Þ
where UA is product of heat transfer coefficient and heat transfer
area (in kW/8C), where U refers to overall heat transfer coeffi-
cient (in W/m K) and TLMTD is logarithmic mean temperature
difference.
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Turbine (Tur) isentropic efficiency:
hTur ¼WTur;a
WTur;s
¼hi � ho;a
hi � ho;s
; ð4Þ
WTur;a ¼ m6h6 �m7h7 ð5Þ
where hTur is efficiency of the turpine, ho;s is isentropic enthalpy
of hot fluid and ho;a is actual enthalpy of hot fluid.
Condenser (Cd):
_QCd ¼ _m8h8 � _m1h1 ¼ UACdDTLMTD;Cd ð6Þ
Pump isentropic efficiency:
hpump ¼Wpump;s
Wpump;a
ð7Þ
Net output work of the system:
Wnet ¼ WTur;a �Wpump;a ð8Þ
Thermal efficiency ðhThÞ of the system:
hTh ¼Wnet
Qin
ð9Þ
In this study, turbine isentropic efficiency and mechanical effi-
ciency was supposed to be 80 and 99%, respectively, as a logical
supposition. A single-stage refrigerant turbine was used because
delivering small amounts of work up to 100 kWe was considered
[16]. The Recuperator model effectiveness was fixed to 80%
corresponding to the medium technology design [17] with a
minimum pinch of 58C and a maximum pressure drop of 3%.
A centrifugal ORC pump with an 85% isentropic efficiency was
selected. Also, a reciprocating pump was selected for oil circula-
tion through the collectors. The vapor generator consists of
three phases, first of them makes the quality of vapor equal to
zero (x ¼ 0), second one evaporates the fluid to its saturated
vapor in constant pressure (x ¼ 1) and the third part heats the
Figure 1. Schematic diagram of a solar ORC with superheater and recuperator.
Figure 2. T–S diagram for the ORC process (benzene).
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saturated vapor to some degree and makes it superheated. For
the sake of simplicity, the same system conditions described
above were taken into account for all the working fluids. The
three phases described are shown in Figure 3. The vapor gener-
ator and condenser use multi-pipe shell-and-tube heat exchan-
gers for relative low cost and commercial availability. The
working fluids are in the tube side and the shell side conveys the
oil and water in the vapor generator and condenser, respectively.
The schematic of a shell-and-tube heat exchanger is shown in
Figure 3.
Water-cooled condenser is used in the cycle with inlet water
temperature of 158C, minimum pinch of 58C was selected. It
is assumed that the outlet state of working fluid from the con-
denser is saturated. The condenser consists of two phases,
de-superheating region and condensation region which are
shown in Figure 4.
2.1 Single-phase regionIt is assumed that the flow is fully developed in the heat exchan-
gers and the condition is steady state. Also, heat losses to
ambient are neglected. The governing equations in the single-
phase region of heat exchangers in the tube side are as follows:
Re ¼rul
m; ð10Þ
where Re is the Reynolds number, u is the velocity (m/s) of the
organic fluid in the tube and is defined as
u ¼_m
rS; ð11Þ
l is defined as the characteristic length and, for a tube, is defined
as its inner diameter Di. Density (r, in kg/m3) dynamic viscosity
(m, in Pa s) and Prandtl number are found from fluid mean tem-
perature. S is the cross-sectional area of tubes (in m2)
The Stanton number is given by
St ¼ ERe�0:205Pr�0:505; ð12Þ
where
E ¼ 0:0225 expð�0:0225 ln ðPrÞ2Þ; ð13Þ
The convective heat transfer coefficient (a, in W/m2 C) for the
inner tube is defined as [18]
ai ¼ rucSt; ð14Þ
Figure 3. Temperature profile in vapor generator and schematic for a multi-pipe shell-and-tube heat exchanger.
Figure 4. Temperature profile in condenser.
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where c is the heat capacity of the fluid, St is Stanton number.
For calculating the heat transfer coefficient across bundle of
tubes (shell side), the Nusselt number is given as
Nu ¼ aRemc Pr0:34FN; ð15Þ
where
Rec ¼rumDo
m; ð16Þ
where a, m and FN are constants related to Reynolds number.
The velocity um is calculated at the minimum cross-flow area in
the bundle as
um ¼_mORC
LwNtr; ð17Þ
where Nt is the number of tubes in a row, L is the length of tube
experiencing the cross-flow and w is dependent to the arrange-
ment of tubes in the bundle [18].
The convective heat transfer coefficient in the shell side is
therefore defined as:
ao ¼kNu
Do
ð18Þ
2.2 Two-phase regionFor calculating the boiling heat transfer coefficient in the vapor
generator and condenser, it is necessary to notice the significant
changes of fluid properties during phase change. The heat trans-
fer in the tubes is divided into small parts of constant properties
to gain more realistic results. The coefficient in the saturated
boiling region is the sum of convective and nucleate components
[18, 19] as follows:
ai ¼ anuc þ aconv; ð19Þ
where
aconv ¼ 0:023FcKL
Di
Re0:8L Pr0:4
L ð20Þ
and
anuc ¼ 0:00122K0:79L C0:45
L r0:49L
s0:5m0:29L ðlrGÞ
0:24
( )
ScðTw�TsÞ0:24ðpw� psÞ
0:75;
ð21Þ
where subscripts L and G accounts for the liquid and gas phase.
Fc and Sc are convective–correction factor and suppression
factor, respectively. The Reynolds number is calculated on the
assumption of liquid flowing in the tube.
ReL ¼ð1� xÞGDi
mL
; ð22Þ
PrL ¼CLmL
kL; ð23Þ
where x is the vapor quality (in %) of flow and G is the mass
velocity (in kg/m2 s) of the fluid defined as
G ¼_mORC
S; ð24Þ
where _mORC is the mass flow rate of organic fluid and S is the
tube flow area.
2.3 Condensation regionThe condensate in the condenser is assumed to form annular
flow and the coefficient is calculated based on the method of
Boyko [20] as described below.
The fluid is assumed to be liquid flow in the tube. The ReL(Eq. 22, when x ¼ 0) and PrL are used in the calculation of
Nusselt number. The equation becomes
aL ¼ 0:023KL
Di
Re0:8L Pr0:4
L ; ð25Þ
where K is the thermal conductivity (in W/ m C).
The convective heat transfer in the condenser is given as:
ai ¼aL
21þ
ffiffiffiffiffiffi
rLrG
r� �
: ð26Þ
Finally, the overall heat transfer coefficient is [18]:
1
U¼
1
ao
þ Ro þ1
ai
þ Ri
� �
Do
Di
þyw
kw
Do
Di
; ð27Þ
where the subscripts i and o refers to inside and outsider of
tubes, respectively, and yw refers to wall thickness of tubes. Also,
Rf is the fouling factor resistance.
2.3 Working fluidsSix fluids were chosen including two refrigerants R123 and
R245fa and four hydrocarbons benzene, isopentane, pentane
and butane to cover a wide range of working temperatures and
pressures. Properties of these fluids are shown in Table 1. One of
the major concerns of organic fluids is their safety, global
warming potential (GWP) relative to CO2, ozone depletion po-
tential (ODP) relative to R11 and atmospheric lifetime [22].
2.4 Collector modelIn this study, a parabolic trough solar collector was chosen as the
heat source. THERMINOL VP-1 was selected as the working
fluid [24] and its characteristics are shown in Table 2. Design
point collector nominal optical efficiency of the collector was
selected 0.82 according to Eq. (30).
hopt ¼ rmirror � hshadowing � hgeometry � hunaccounted ð28Þ
Site latitude, altitude and hour of the day were considered 358,
1420 m and 12 (solar time), respectively, according to Tehran.
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Other input characteristics of solar collector and ORC system
are presented in Table 3.
3 ECONOMIC MODEL
The economic model developed here is based on capital cost
equations of various components in the solar ORC model. For
all equipment, there is a strong dependence on material and op-
erating pressure. The method of accounting for changes in oper-
ating pressures is covered through the use of the pressure factor.
Also, the change in the material of construction is covered
through the use of the material factor. The total cost of the
system is the summation all components.
Ctot ¼ CVG þ Ctur þ CRec þ CCd þ Cpump þ CSolarpump
þ CSolarCollector; ð29Þ
The purchased cost for vapor generator is given by [21]:
CVG ¼ CoVG bVG
1 þ bVG2 FVGm FVGp
� �
; ð30Þ
where bVG1 and bVG
2 are constants of heat exchanger type. FVGm is
the material factor for stainless steel and FVGp is the pressure
factor for operating pressure of heat exchanger. The coefficients
used in the model are represented in Table 4.
The base cost of vapor generator CoVG is the cost of equipment
made from carbon steel at ambient working pressure and is
defined as
logCoVG ¼ kVG1 þ kVG2 log AVG þ kVG3 ðlogAVGÞ
2; ð31Þ
where kVG1 , kVG2 and kVG3 are constants of heat exchanger type.
Also, AVG is the calculated heat transfer area for vapor generator.
Also, FVGp is given by
log FVGp ¼ cVG1 þ cVG2 log pVG þ cVG3 ðlog pVGÞ2; ð32Þ
where cVG1 , cVG2 and cVG3 are constants of heat exchanger type and
pVG is the operating pressure of organic fluid in bar.
The cost of turbine is expressed as:
Ctur ¼ FbmC0tur; ð33Þ
where Fbm is the bare module factor and is related to turbine
type and material (stainless steel steam turbine). C0tur is the base
cost for turbine expressed as:
log CoTur ¼ kTur
1þ kTur2 log Wtur þ kTur3 ðlogWturÞ
2; ð34Þ
where Wtur is the turbine shaft power in kW. The cost functions
for recuperator and condenser are similar to vapor generator
with different heat transfer area and operating pressure as
Table 2. Thermal oil properties [24].
Substance Min/max
temperature
(8C)
Density
(kg/m3)
Specific
heat
(kJ/kg C)
Thermal
conductivity
(w/m C)
THERMINOL
VP-1
12.78/398.9 1067.6 1.532 0.1368
Table 3. Collector model parameters.
Parameter Value
rmirror 0.94
�shadowing 0.98
�geometry 0.93
�unaccounted 0.96
Receiver tube outer diameter 70 mm
Reflector aperture width 1 m
Reflector row pitch/aperture width 2.5
Reflector cleanliness factor 0.95
Receiver tube emissivity 0.14
Receiver glass envelope emissivity 0.86
Convective heat transfer coefficient outside glass envelope 56.78 w/m28C
Mass flow rate of thermal oil 4.5 kg/s
Minimum allowable pinch point temperature difference
(for vapor generator, condenser and recuperator)
58C
Mass flow rate of ORC fluid 0.5 kg/s
Table 1.Working fluid properties [22, 23].
Substance Physical data Tbpa (8C)
Tcrb (8C) Pcr
c (bar)
Molar mass
(kg/kmol)
Safety
data
ASHRAE
34 safety
group
Environmental
data
atmospheric
lifetimed
/GWP/ODP
Benzene 80.08 288.9 48.94 78.108 – –
pentane 36.06 196.55 33.70 72.149 A3 –
R123 27.823 183.68 36.618 152.93 B1 1.3/77/0.02
Isopentane 27.83 187.2 33.78 72.149 A3 –/20/0
R245fa 15.14 154.01 36.51 134.05 B1 7.6/1030/0
Butane 20.49 151.98 37.96 58.122 A3 –
aNormal boiling point.bCritical temperature.cCritical pressure.dTime in which the organic fluids remain in the atmosphere (year).
Table 4. Coefficients of cost estimation equations.
Component K1 K2 K3 B1 B2 Fm
Vapor generator 2.7652 0.7282 0.0783 1.74 1.55 2.8
Recuperator 2.7652 0.7282 0.0783 1.74 1.55 2.8
Condenser 2.7652 0.7282 0.0783 1.74 1.55 2.8
Turbine 3.4092 20.5104 0.0030 0 1 3.6
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follows:
CCd ¼ CoCd bCd
1 þ bCd2 FCdm FCdp
� �
; ð35Þ
log CoCd ¼ kCd1 þ kCd2 log ACd þ kCd3 ðlog ACdÞ
2; ð36Þ
log FCdp ¼ cCd1 þ cCd2 log pCd þ cCd3 ðlog pCdÞ2; ð37Þ
CRec ¼ CoRec bRec
1 þ bRe2 FRecm FRecp
� �
; ð38Þ
log CoRec ¼ kRec1 þ kRec2 log ARec þ kRec3 ðlog ARecÞ
2; ð39Þ
log FRecp ¼ cRec1 þ cRec2 log pRec þ cRec3 ðlog pRecÞ
2: ð40Þ
The ORC pump uses a centrifugal pump and its cost is defined
as:
CORCpump ¼ CoORCpump
�
bORCpump2
þ bORCpump2 FORCpump
m FORCpumpp
�
; ð41Þ
where
log CoORCpump ¼ k
ORCpump1 þ k
ORCpump2 log WORCpump
þ kORCpump3 ðlog WORCpumpÞ
2: ð42Þ
bORCpump1 , b
ORCpump2 are the constants for centrifugal pump.
kORCpump2 , k
ORCpump2 and k
ORCpump3 are constants of pump type
and WORCpump is the pump shaft work. The FORCpumpm is the ma-
terial factor for stainless steel pump and FORCpumpp is defined as:
log FORCpumpp ¼ c
ORCpump1 þ c
ORCpump2 log PORCpump
þ cORCpump3 ðlog PORCpumpÞ
2; ð43Þ
where pORCpump is the operating pressure of pump in bar. Also,
cORCpump2 , c
ORCpump2 and c
ORCpump3 are constants of pump type.
The cost of solar pump is defined similar to ORC pump with
different type (reciprocal pump) given as:
CSolarpump ¼ CoSolarpump
�
bSolarpump1
þ bSolarpump2 FSolarpump
m FSolarpumpp
�
; ð44Þ
log CoSolarpump ¼ k
Solarpump1 þ k
Solarpump2 log WSolarpump
þ kSolarpump3 ðlog WSolarpumpÞ
2; ð45Þ
log FSolarpumpp ¼ cSolarpump
1þ c
Solarpump2 log PSolarpump
þ cSolarpump3 ðlog PSolarpumpÞ
2: ð46Þ
The cost of solar field is the summation of its components in-
cluding reflector, receiver, heat transfer fluid (thermal oil),
structure and miscellaneous (material and equipment) expressed
as:
CSolarfield ¼ CReflector þ CReceiver þ CHTF þ CStr þ CMisc: ð47Þ
The cost of solar collectors is a strong function of aperture area
of collectors. The cost data for parabolic trough solar collector
were extracted from the Thermoflow software [14] and were
used in the model.
4 RESULTS AND DISCUSSION
4.1 Thermodynamic analysis resultsTable 5 shows the ORC fluids and min/max pressures and tem-
peratures which were used in the modeling as the base case with
the existence of recuperator and superheater.
Table 6 summarizes the results for six working fluids with
four schematics, simple Rankine cycle without regenerator and
superheater, with superheating, with regenerating and with both
of them. Table 6 shows that the existence of recuperator has a
more effective role on increasing the system efficiency compared
with superheating. According to Figure 5, superheating can raise
the system efficiency to some extent for all working fluids
because the energy content of working fluid is raised, but it also
increases the temperature difference in the collectors which
requires more reflective area for collectors. This behavior is
based on the reason that dry behavior of organic fluids causes
the average temperature of heat rejection to increase together
with the average temperature of heat addition. Table 6 shows a
comparison of different schematics for all working fluids. It is
revealed that existence of recuperator plays an important role in
Table 5. ORC fluids and their temperatures and pressures at turbine input
and condenser output as the base case.
ORC fluid PT (bar) TT (8C) PC (bar) TC (8C)
Benzene 26.82 287 0.20 35.28
Pentane 25 190 1 35.67
R123 30 180 1.3 35
Isopentane 30 185 1.28 34.76
R245fa 23 140 2.11 35
Butane 25.02 137 3.30 35.17
Table 6. Net electrical efficiency for different working fluids (percent).
Working fluids Simple
Rankine
cycle
Addition of
superheater
Addition of
recuperator
Addition of
superheater and
recuperator
Benzene 22.28 22.61 24.19 26.55
Pentane 15.49 15.5 17.86 18.73
R123 15.21 15.47 15.95 16.86
Isopentane 15.12 15.17 17.37 18
R245fa 12.07 12.18 12.74 13.53
Butane 12 12.1 12.62 13.37
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increasing efficiency, this is because of dry behavior of organic
fluids which their positive slope of T–S diagram causes the
outlet state of turbine to be in superheated region. A lot of
energy could be recuperated from vapor at turbine outlet and
transported to incoming fluid before entering vapor generator
by means of a recuperator. Not only existence of recuperator
decreases the amount of heat addition to working fluids in heat
exchangers, but it also decreases the condenser load to a great
extent. This is effective on lowering the heat transfer area of con-
denser and solar collector which contributes to lower total cost
for entire system. Results of modeling different organic fluids are
shown in Table 6.
As can be seen in Table 6 among these six working fluids,
benzene shows the best performance for these conditions
described. Figures 6 and 7 show the effect of turbine inlet pres-
sure on the efficiency and work output.
According to Figure 6 there is an optimum pressure in each
temperature for fluids, the reason for this behavior lies in the
h– s diagram of working fluids, when outlet pressure of turbine
is fixed and input pressure rise, the enthalpy difference between
two pressures goes through a maximum which is due to the con-
stant pressure curves in h– s diagram of fluids [8].
Figure 7 shows the effect of turbine inlet pressure on work
output, the more pressure increases the more work produces.
But, on the other hand, the work consumed by pump to gener-
ate the required pressure also increases. As mentioned above, en-
thalpy difference across the turbine goes through a maximum
which plays a more important role in determining the network
output. Overall results are shown in Figure 7. Also a noticeable
interpretation from Figures 7 and 8 is that R123 produces less
power than butane in all working pressures but has a more
thermal efficiency. This is because butane needs more heat to
evaporate and reach the desired condition with the same mass
flow rate.
Figure 8 shows the multiplication of overall heat transfer
coefficient and heat transfer area (UA) in three regions of vapor
generator, including economizer, evaporator and superheater.
Also, Figure 9 shows the heat transfer rate in these regions,
respectively. When turbine input pressure increases with fixed
turbine back pressure, the amount of heat addition to econo-
mizer increases so as to make the sub-cooled fluid to be satu-
rated liquid (as shown in Figure 9) which leads to an increase in
UA. With rising the pressure, the enthalpy difference (latent heat
of evaporation) in two-phase area on the T–S diagram decreases
(see Figure 2) leading to a decrease in the amount of heat add-
ition in evaporator (as shown in Figure 9). On the other hand,
Figure 6. Effect of varying generator pressure on efficiency of the system.
Figure 7. Effect of generator pressure on net output work.Figure 5. Effect of superheating in different working fluids with regenerator.
Figure 8. Effect of generator pressure on characteristics of vapor generator
(benzene).
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because of increasing the evaporation temperature with increas-
ing the pressure in evaporator, the UA of evaporator increases
due to decreased DTLMTD in evaporator. With the raised pres-
sures, the same amount of superheating is obtained with less
heat addition to organic fluid as shown on Figure 9 leading to a
decreased UA in superheater. Results are shown in Figures 8 and
9 for benzene. Also, the summation of heat transfers in sub-
sections of vapor generator is shown in Figure 9. Because the
outlet temperature of vapor generator is constant, the variation in
generator pressure does not affect the outlet temperature of heat
source as shown in Figure 8, but the inlet temperature of collector
rises to a little amount with increasing the generator pressure.
This is because of the fact that increasing the generator pressure
will reduce the overall required heat of vapor generator. Also,
Figure 10 shows the variation in generator pressure on pinch
values. As can be seen, increasing the working pressure, at first
stages, do not affect the pinch value because of constant generator
temperature, but increasing the pressure eventually causes the
pinch value to decrease to a minimum allowable value.
From Figures 11 and 12, it appears that rising the turbine
inlet pressure will decrease the required reflective area in solar
field. This is due to the fact that rising the pressure causes the
overall heat duty in vapor generator to fall (according to
Figure 9) and this will reduce the required reflective area in solar
field.
Figure 13 shows the variation in UA of collector against gen-
erator pressure. UA of collector is an indicator for heat loss in
the absorber tube. Therefore, with increasing the pressure,
according to a slight increase in collector inlet temperature, the
heat losses decrease and therefore the UA is subject to a small
decrement as shown in the figure.
4.2 Economic analysis resultFigure 14 shows the column charts for each working fluid with
different schematic and their corresponding efficiencies and
costs. As can be seen, for benzene, isopentane and pentane, the
total capital cost of the plant with recuperator is the lowest al-
though it has an extra equipment (recuperator) compared with
the simple plant and the plant with superheater. The reason is
that the existence of pecuperator lowers the load of condenser by
lowering the enthalpy of inlet fluid to condenser. Also, by
Figure 9. Effect of turbine inlet pressure on characteristics of vapor generator
(benzene).
Figure 10. Effect of generator pressure on pinch temperature difference of vapor
generator for different fluids.
Figure 11. Effect of turbine inlet pressure on solar collectors’ reflective area
(benzene, R123 and R245fa).
Figure 12. Effect of generator pressure on solar collectors’ reflective area
(Pentane, Isopentane and Butane).
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increasing the enthalpy of inlet fluid to vapor generator, it
decreases the reflective area required by solar collectors and con-
tribute to the lower cost of the overall plant. The plant with both
the superheater and recuperator has the highest efficiency but
with higher capital cost for all working fluids. Detailed results
are shown for each fluid according to Table 5 input parameters.
Figures 15 and 16 shows the detailed estimated costs of
various components including heat exchangers, pumps, turbine
and solar field against turbine inlet pressure for benzene. As can
be seen in the figures, turbine pressure is an effective parameter
on the total cost of the system. According to Figure 15, vapor
generator, recuperator and refrigerant pump show an increasing
trend with pressure because of increasing heat transfer surface
area in heat exchangers and pressure rise in the pump. On the
other hand, condenser cost decreases as the pressure increases.
This is due to the single-phase region in the condenser (see
Figure 4). With increasing pressure, the output temperature of
recuperator falls, due to improved heat transfer, and surface area
of condenser falls leading to a decreased costs. According to
Figure 16, solar pump cost remains approximately constant
because of its weak relation to turbine pressure. Other compo-
nents show a decreasing trend. This is due to the fact that asFigure 13. Effect of generator pressure on UA of solar collector (for benzene in
vapor generator).
Figure 14. Column charts indicating output work, thermal efficiency and total costs for each working fluid with different schematics.
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operating pressure of heat exchangers goes up, overall tempera-
ture rise in the collector falls resulting in a decrease in reflector
surface. As it appears from Figures 16 and 17, the receiver and
reflector accounts for the main portion of solar field total price.
The relatively slight decrease in the receiver and reflector cost is
due to the small reduction in aperture surface as mentioned
above.
Figure 18 shows that solar field constitutes the main portion
of total cost of the system (≏40–45% of the total cost). Also,
with increasing pressure, the total cost of ORC equipment rises
due to the increased heat transfer areas in the heat exchangers
but the solar field shows a decreasing trend due to decreasing
aperture area of collectors which has the dominant effect among
other costs in the solar field.
Figure 19 shows the variation in total cost of the system and
thermal efficiency against turbine inlet pressure on the condition
that other parameters remain constant. According to Figure 19,
increasing the turbine inlet pressure causes the total cost of the
plant to increase. But the efficiency goes up at first and then
decreases. Therefore, choosing the suitable operating pressure is
a tradeoff between thermal efficiency and cost of the system.
However, as the efficiency does not change dramatically (,1%)
the lower pressures are more desirable due to low costs.
5 CONCLUSION
In this study, an ORC engine coupled with a parabolic trough
solar collector was investigated thermodynamically and
Figure 15. Cost variation of ORC components versus turbine pressure
(benzene).
Figure 16. Cost variation of solar field components versus turbine pressure.
Figure 17. Cost variation of reflector and receiver versus turbine pressure.
Figure 18. Total cost of ORC and solar field versus turbine pressure.
Figure 19. Total cost of the solar ORC system and thermal efficiency against
turbine inlet pressure (benzene).
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economically for small-scale power generation. Six working
fluids were examined in cycle with different working tempera-
tures and pressures. Also, four schematics of ORC engine includ-
ing simple cycle, regenerative cycle, superheating cycle and both
superheating and regenerating cycle were compared. A
shell-and-tube heat exchanger consisting of three regions
(economizer, evaporator and superheater) was used as a vapor
generator. Sizing of heat exchangers was performed in order to
obtain capital costs of heat exchangers. The effect of key para-
meters such as turbine inlet pressure and temperature on cycle
efficiency, power output, oil temperature, current UA of heat
exchangers and costs of the equipment were investigated. Results
show that, among these fluids, benzene has the best performance
in terms of efficiency (26.55%) but with the highest total system
cost (≏76 0000 USD) followed by pentane, R123, isopentane,
butane and R245fa. Butane has the lowest efficiency (13.37%)
and R245fa has the lowest total cost of 34 000 USD. Th perform-
ance evaluation reveals that existence of recuperator is vital
because it increases the thermal efficiency by recovering the heat
from turbine outlet and lowering the loads of condenser and
solar collectors. Also, in some cases, recuperator causes the low-
ering of total cost of the system compared with simple cycle as a
result of lowering the condenser and solar collector loads. The
best schematic was found to be the cycle with recuperator and
superheater but with the cost of higher total cost. The paramet-
ric study reveals that turbine inlet pressure has an important
effect on thermal efficiency and total cost of the system.
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