Advanced ORC Architectures for Waste Heat Recovery at IIT Madras

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Potential of a Transcritical Regenerative Series Two Stage
Organic Rankine Cycle for Dual Source Waste Heat Recovery
Anandu Surendran
Satyanarayanan Seshadri Ph.D
Energy and Emissions Lab
Department of Applied Mechanics
Indian Institute of Technology| Madras
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
Existing ORC architectures
Proposed architecture
Heat source and modelling conditions
Parameter studies
Optimization and comparison
Conclusion and future works
Contents
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
 
Existing ORC solutions
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
 
 
Pre-heated single stage ORC
Dual-loop ORC
 
Series Two stage ORC (STORC)
 
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
Parallel 
Two stage ORC (PTORC)
 
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
 
 
More often multiple heat sources exist concurrently
Existing complex architectures are less economical
All existing architectures are of lower thermal efficiency
Inability to fully utilize all the heat sources when multiples heat sources are present
Why advanced ORC architectures for more than one heat
source ?
What could be done?
ORC
System
What is being proposed?
An advanced ORC layout: Trans-critical Regenerative Series Two Stage
Organic Rankine Cycle (TR-STORC)
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
              TR-STORC layout
   
         
 
T-s diagram of TR-STORC
Novel architecture that combines supercritical evaporation in high
pressure (HP) stage and  partial evaporation in low pressure (LP)
stage
 Utilizes the  superheat of exhaust vapour from HP turbine in the
regenerator to fully evaporate the working fluid in LP stage and boost
power output
2.9 MW natural gas engine
Used as stationary power generation units in steel plants and other
process industries
Heat Sources from a Gas Engine
Engine jacket cooling water
Engine lubrication oil cooling
First stage air intake intercooler
Engine exhaust gases
Engine generator radiated heat
Heat from second stage intercooler
Heat source: Stationary IC Engine
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
Exhaust gases
Hot water
First three are recovered as hot water on a 70/90°C flow return basis
Primary heat source : 
Exhaust gases 
(Tp= 432°C, mp=16,528 kg/h)
Secondary heat source : 
Hot water 
(Ts= 90°C, ms=50,400 kg/h)
Working fluid : Cyclopentane
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
 Cycle parameters
All processes are at steady state
Pressure drop and heat transfer from the pipelines is neglected
Changes in kinetic and potential energy of the working fluid is negligible
All heat exchangers are counter flow type
Both LP and HP turbine stages have same isentropic efficiency
MATLAB model integrated with REFPROP
Discretized heat exchanger model with N=50 in HP evaporator for
capturing the cooling curve and pinch point location
N=30 for condenser and LP evaporator
Mass flow rate in HP and LP loops are calculated iteratively
Search technique to find the optimum vapor fraction in LP evaporator
outlet
Modelling equations and procedure
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
Influence of HP evaporation pressure and vapor outlet temperature
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
At lower HP evaporator pressures, lower values of vapor outlet
temperatures lead to maximum work output
For higher HP stage pressures ,the optimum vapor fraction is higher for a
given vapour outlet temperature
Influence of HP evaporation pressure and vapor outlet temperature
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
U
p
 remains almost constant with vapour outlet temperature
The peaks in U
s
 correspond to maximum mass flow rates in the pre-heater section of
LP evaporator
The variation in thermal efficiency is a direct result of the variation in net power
output and heat source utilization rates
Influence of LP evaporation temperature (pressure)
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
At lower values of T
3
,  higher utilization of secondary heat is seen
At lower values of T
3
, the thermal efficiency of the LP stage decreases resulting in
lower power outputs
An intermediate value of T
3 
 exists that maximizes the net power output of the TR-
STORC.
Cycle optimization : Parameters and Constraints
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
The maximum operating temperature of the working fluid is set as the upper limit on the
vapor outlet temperature
Condenser pressure is kept above atmospheric pressure to prevent air leakage into the
system
Volumetric flow ratios (VFR) of both HP and LP turbines are constrained within 50 so
that single stage turbines with can be used (Invernizzi
et al.
, 2007)
The cooling limit on the primary heat source is set to 373K to prevent acid droplet
formation
Genetic Algorithm (GA) with net power output as the objective function
Compared with an optimized STORC and pre-heated ORC for various cases
Optimization results : At engine design point
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
TR-STORC delivers the highest power output which is 16% higher than STORC and 23% than
pre-heated ORC
TR-STORC also has the highest thermal efficiency, 6% higher than pre-heated ORC and 25%
higher than STORC
U
s
 increased by 2.6 times than pre-heated ORC
Comparable mass flow rates and UA requirements with STORC
Optimization results : Influence of heat source temperatures and
heat content
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
14%-20% more power output than STORC
As the secondary heat source temperature increases, the relative increase in power
output of TR-STORC and STORC exceeds that of pre-heated
For the heat ratios investigated, TR-STORC delivers 4.8-5.5% increased power output
than STORC.
Tp= 673K , Ts= 363K
 
 
 
 
 
Baseline : Pre-heated single
stage ORC
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
Summary and
 Conclusions
A two stage cycle architecture that improves on the existing STORC architecture by
combining supercritical heating in the HP stage and partial evaporation and
regeneration in the LP stage is proposed
2.9MW Stationary gas engine  is selected as the heat source
Results are compared with optimized pre-heated ORC and STORC
The main conclusions are:
For a 2.9MW natural gas engine, TR-STORC delivers 
16% and 23% higher power
output than STORC and pre-heated ORC respectively
U
s
 increased by 2.6 times than pre-heated ORC
TR-STORC has 6% and 25& higher thermal efficiency than pre-heated ORC and STORC
TR-STORC presents excellent exergetic performance for dual source heat recovery
over STORC and pre-heated ORC
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
Future works and leads
 Experimental validation of heat exchanger loop – using throttle valves (in
progress at IIT M)
Experimental validation – using expanders
Study of supercritical nature of refrigerants, siloxanes and other alkanes
Other possibilities
WHR for petroleum refineries with multiple heat streams
Combined solar+ geothermal applications
Single heat source applications such as geothermal by temperature splitting
Compete against supercritical CO2 systems at higher source temperatures
Thank you..
Energy and Emissions Lab
Indian Institute of Technology (IIT), Madras
 
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
Anandu Surendran
Research Scholar (Ph.D)
FMB #121
Energy and Emissions Lab
Fluid Mechanics Division
Department of Applied Mechanics , IIT M
Email:
 
anandusurendran@smail.iitm.ac.in
Ph no: 9446525291, 7550160214
Dr. Satyanarayanan Seshadri
Assistant Professor
FMB #201
Fluid Mechanics Division
Department of Applied Mechanics , IIT M
Email: 
satya@iitm.ac.in
Ph no: 044-2257-4078, 9845068998
Contact details
Indian Institute of Technology | Madras
Energy and Emissions Lab | Department of Applied Mechanics
At design point
Pressure ratio across HP turbine : 68 bar to 2.2 bar approx : 31
Pressure ratio across LP turbine : 2.2 bar to 1.2 bar approx : 1.8
Pressure limit: 80 bar
Appendix
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
L. Shi, G. Shu, H. Tian, and S. Deng, “A review of modified Organic Rankine cycles (ORCs) for internal
combustion engine waste heat recovery (ICE-WHR),” 
Renew. Sustain. Energy Rev.
, vol. 92, pp. 95–110,
Sep. 2018.
I. Vaja and A. Gambarotta, “Internal Combustion Engine ( ICE ) bottoming with Organic Rankine Cycles (
ORCs ),” 
Energy
, vol. 35, no. 2, pp. 1084–1093, 2010.
G. Shu, L. Liu, H. Tian, H. Wei, and G. Yu, “Parametric and working fluid analysis of a dual-loop organic
Rankine cycle (DORC) used in engine waste heat recovery,” 
Appl. Energy
, vol. 113, 2014.
G. Manente, A. Lazzaretto, and E. Bonamico, “Design guidelines for the choice between single and dual
pressure layouts in organic Rankine cycle (ORC) systems,” 
Energy
, vol. 123, pp. 413–431, 2017.
J. Li, Z. Ge, Y. Duan, and Z. Yang, “Design and performance analyses for a novel organic Rankine cycle
with supercritical-subcritical heat absorption process coupling,” 
Appl. Energy
, vol. 235, pp. 1400–1414,
Feb. 2019.
S. Rech, S. Zandarin, A. Lazzaretto, and C. A. Frangopoulos, “Design and off-design models of single and
two-stage ORC systems on board a LNG carrier for the search of the optimal performance and control
strategy,” 
Appl. Energy
, vol. 204, pp. 221–241, Oct. 2017.
T. Chen, W. Zhuge, Y. Zhang, and L. Zhang, “A novel cascade organic Rankine cycle (ORC) system for
waste heat recovery of truck diesel engines,” 
Energy Convers. Manag.
, vol. 138, pp. 210–223, 2017.
T. Li, Z. Zhang, J. Lu, J. Yang, and Y. Hu, “Two-stage evaporation strategy to improve system
performance for organic Rankine cycle,” 
Appl. Energy
, vol. 150, pp. 323–334, 2015.
S. Lecompte, H. Huisseune, M. Van Den Broek, and M. De Paepe, “Methodical thermodynamic analysis
and regression models of organic Rankine cycle architectures for waste heat recovery,” 
Energy
, vol. 87,
pp. 60–76, 2015.
U. Larsen, L. Pierobon, F. Haglind, and C. Gabrielii, “Design and optimisation of organic Rankine cycles
for waste heat recovery in marine applications using the principles of natural selection,” 
Energy
, vol. 55,
pp. 803–812, 2013.
C. Invernizzi, P. Iora, and P. Silva, “Bottoming micro-Rankine cycles for micro-gas turbines,” vol. 27, pp.
100–110, 2007.
References
Indian Institute of Technology | Madras
5
th
 International Seminar on ORC Power Systems | Athens, Greece
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Presentation of a novel Trans-critical Regenerative Series Two-Stage Organic Rankine Cycle (TR-STORC) by researchers Anandu Surendran and Satyanarayanan Seshadri at the 5th International Seminar on ORC Power Systems in Athens. The TR-STORC layout combines supercritical evaporation in the high-pressure stage with partial evaporation in the low-pressure stage, utilizing exhaust vapor superheat to maximize power output. Detailed discussions on existing ORC architectures, proposed solutions, optimization strategies, and future research directions were also presented.

  • ORC Power Systems
  • Waste Heat Recovery
  • IIT Madras
  • Advanced Architectures

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  1. Indian Institute of Technology | Madras Potential of a Transcritical Regenerative Series Two Stage Organic Rankine Cycle for Dual Source Waste Heat Recovery Anandu Surendran Satyanarayanan Seshadri Ph.D Energy and Emissions Lab Department of Applied Mechanics Indian Institute of Technology| Madras 5th International Seminar on ORC Power Systems | Athens, Greece

  2. Indian Institute of Technology | Madras Contents Existing ORC architectures Proposed architecture Heat source and modelling conditions Parameter studies Optimization and comparison Conclusion and future works 5th International Seminar on ORC Power Systems | Athens, Greece

  3. Indian Institute of Technology | Madras Existing ORC solutions Pre-heated single stage ORC Dual-loop ORC 5th International Seminar on ORC Power Systems | Athens, Greece

  4. Indian Institute of Technology | Madras Parallel Two stage ORC (PTORC) Series Two stage ORC (STORC) 5th International Seminar on ORC Power Systems | Athens, Greece

  5. Indian Institute of Technology | Madras Why advanced ORC architectures for more than one heat source ? More often multiple heat sources exist concurrently Existing complex architectures are less economical All existing architectures are of lower thermal efficiency Inability to fully utilize all the heat sources when multiples heat sources are present What could be done? Supercritical evaporation Partial evaporation Stream splitting ORC System Reducing heat exchanger requirements Utilizing superheat after expansion 5th International Seminar on ORC Power Systems | Athens, Greece

  6. Indian Institute of Technology | Madras What is being proposed? An advanced ORC layout: Trans-critical Regenerative Series Two Stage Organic Rankine Cycle (TR-STORC) Novel architecture that combines supercritical evaporation in high pressure (HP) stage and partial evaporation in low pressure (LP) stage Utilizes the superheat of exhaust vapour from HP turbine in the regenerator to fully evaporate the working fluid in LP stage and boost power output TR-STORC layout T-s diagram of TR-STORC 5th International Seminar on ORC Power Systems | Athens, Greece

  7. Indian Institute of Technology | Madras Heat source: Stationary IC Engine 2.9 MW natural gas engine Used as stationary power generation units in steel plants and other process industries Heat Sources from a Gas Engine Engine jacket cooling water Engine lubrication oil cooling First stage air intake intercooler Engine exhaust gases Engine generator radiated heat Heat from second stage intercooler Exhaust gases Hot water First three are recovered as hot water on a 70/90 C flow return basis Primary heat source : Exhaust gases (Tp= 432 C, mp=16,528 kg/h) Secondary heat source : Hot water (Ts= 90 C, ms=50,400 kg/h) Working fluid : Cyclopentane 5th International Seminar on ORC Power Systems | Athens, Greece

  8. Indian Institute of Technology | Madras Cycle parameters Parameter Value Tevap,HP (K) Tevap,LP (K) Tcond (K) e (%) p (%) PP (kPa) TP, outmin (K) Tsink, in (K) Tsink, out (K) 20 T pinch HP evaporator 10 T pinch LP evaporator 10 T pinch condenser Isentropic expander efficiency 70 Isentropic pump efficiency 80 Primary heat carrier pressure 101.325 Primary heat source cooling limit 373 Inlet temperature cooling water 298 Outlet temperature cooling water 303 All processes are at steady state Pressure drop and heat transfer from the pipelines is neglected Changes in kinetic and potential energy of the working fluid is negligible All heat exchangers are counter flow type Both LP and HP turbine stages have same isentropic efficiency MATLAB model integrated with REFPROP 5th International Seminar on ORC Power Systems | Athens, Greece

  9. Indian Institute of Technology | Madras Modelling equations and procedure W = (W = + W /Q - ) LP (W - W ) net exp, W HP exp, pump, HP pump, LP th net total U U VFR VFR p = = Q (Q /Q + /V V = V = HP evap P, all Q )/Q s LP evap LP pre - heater S, all HP 6 5 /V LP 7 3" Discretized heat exchanger model with N=50 in HP evaporator for capturing the cooling curve and pinch point location N=30 for condenser and LP evaporator Mass flow rate in HP and LP loops are calculated iteratively Search technique to find the optimum vapor fraction in LP evaporator outlet 5th International Seminar on ORC Power Systems | Athens, Greece

  10. Indian Institute of Technology | Madras Influence of HP evaporation pressure and vapor outlet temperature 5.0MPa 5.5MPa 6.0MPa 6.5MPa 7.0MPa 7.5MPa 0.64 416 0.62 414 0.60 412 Optimum vapor fraction q 0.58 410 Wnet (kW) 0.56 408 0.54 406 0.52 404 5.0MPa 5.5MPa 6.0MPa 6.5MPa 7.0MPa 7.5MPa 0.50 402 400 0.48 398 0.46 396 0.44 550 560 570 580 590 600 550 560 Vapor outlet temperature (K) 570 580 590 600 Vapor outlet temperature (K) At lower HP evaporator pressures, lower values of vapor outlet temperatures lead to maximum work output For higher HP stage pressures ,the optimum vapor fraction is higher for a given vapour outlet temperature 5th International Seminar on ORC Power Systems | Athens, Greece

  11. Indian Institute of Technology | Madras Influence of HP evaporation pressure and vapor outlet temperature 17 90 30 Secondary heat source utilizaiton rate Us (%) 5.0MPa 5.5MPa 6.0MPa 6.5MPa 7.0MPa 7.5MPa 5.0MPa (Up) 7.5MPa (Up) 5.0MPa (Us) 7.5MPa (Us) Primary heat source utilizaiton rate Up (%) 88 28 Thermal efficiency (%) 16 86 26 84 24 15 82 22 14 80 20 550 560 570 580 590 600 550 560 Vapor outlet temperature (K) 570 580 590 600 Vapor outlet temperature (K) Up remains almost constant with vapour outlet temperature The peaks in Us correspond to maximum mass flow rates in the pre-heater section of LP evaporator The variation in thermal efficiency is a direct result of the variation in net power output and heat source utilization rates 5th International Seminar on ORC Power Systems | Athens, Greece

  12. Indian Institute of Technology | Madras Influence of LP evaporation temperature (pressure) 410 Utilization rate of secondary heat source Us (%) 580K/ 5.0 MPa 580K/ 6.0 MPa 580K/5.0MPa 580K/6.0MPa 55 18 405 50 400 Net work output (kW) 45 16 Thermal efficiency (%) 40 395 35 390 14 30 385 25 580K/ 5.0 MPa 600K/ 5.0 MPa 580K/ 6.0 MPa 600K/ 6.0 MPa 12 380 20 375 15 10 370 10 320 325 330 335 340 345 350 320 325 330 335 340 345 350 LP evaporation temperature (K) LP evaporation temperature (K) At lower values of T3, higher utilization of secondary heat is seen At lower values of T3, the thermal efficiency of the LP stage decreases resulting in lower power outputs An intermediate value of T3 exists that maximizes the net power output of the TR- STORC. 5th International Seminar on ORC Power Systems | Athens, Greece

  13. Indian Institute of Technology | Madras Cycle optimization : Parameters and Constraints Parameter Value T6 T3 560-600K 323K (Ts,in - Tevap,LP)K 1.1 Pc- 8MPa 313K-333K PHP evap Tcond Constraints Pcond VFR HP turbine 1.20 bar <= 50 VFR LP turbine <= 50 Degree of sub cooling 5K Tp,out min 373K GA parameters Population size 20 Maximum generations 15 Function tolerance 0.01kW The maximum operating temperature of the working fluid is set as the upper limit on the vapor outlet temperature Condenser pressure is kept above atmospheric pressure to prevent air leakage into the system Volumetric flow ratios (VFR) of both HP and LP turbines are constrained within 50 so that single stage turbines with can be used (Invernizziet al., 2007) The cooling limit on the primary heat source is set to 373K to prevent acid droplet formation Genetic Algorithm (GA) with net power output as the objective function Compared with an optimized STORC and pre-heated ORC for various cases 5th International Seminar on ORC Power Systems | Athens, Greece

  14. Indian Institute of Technology | Madras Optimization results : At engine design point Parameters Pre-heated ORC STORC TR-STORC Wnet (kW) I (%) ex(%) Up (%) Us (%) mwf(kg/s) Tevap,LP (K) Tevap,HP (K) Pevap,HP (MPa) VFRLP VFRHP UA (kW/K) W/UA 280 14.4 14.2 81.5 5.20 3.50 - 460 2.18 - 21.6 117 2.46 297 12.2 15.0 81.6 18.4 4.85 344 460 2.18 1.6 13.5 147 2.02 344 15.3 17.4 81.6 13.3 4.84 347 582 6.83 1.7 45.2 149 2.31 TR-STORC delivers the highest power output which is 16% higher than STORC and 23% than pre-heated ORC TR-STORC also has the highest thermal efficiency, 6% higher than pre-heated ORC and 25% higher than STORC Us increased by 2.6 times than pre-heated ORC Comparable mass flow rates and UA requirements with STORC 5th International Seminar on ORC Power Systems | Athens, Greece

  15. Indian Institute of Technology | Madras Optimization results : Influence of heat source temperatures and heat content 60 673K TR-STORC 673K STORC 773K TR-STORC 773K STORC 18 TR-STORC STORC 16 50 14 Tp= 673K , Ts= 363K 40 12 (%) (%) 10 30 8 20 6 10 4 2 0 0.2 0.4 0.6 0.8 Heat ratio 1.0 1.2 1.4 1.6 360 365 Secondary heat source temperature Ts,in (K) (W = STORC power, 370 375 380 385 390 395 - W )/W 100 Baseline : Pre-heated single stage ORC net, STORC net, preORC net, preORC 14%-20% more power output than STORC As the secondary heat source temperature increases, the relative increase in power output of TR-STORC and STORC exceeds that of pre-heated For the heat ratios investigated, TR-STORC delivers 4.8-5.5% increased power output than STORC. 5th International Seminar on ORC Power Systems | Athens, Greece

  16. Indian Institute of Technology | Madras Summary and Conclusions A two stage cycle architecture that improves on the existing STORC architecture by combining supercritical heating in the HP stage and partial evaporation and regeneration in the LP stage is proposed 2.9MW Stationary gas engine is selected as the heat source Results are compared with optimized pre-heated ORC and STORC The main conclusions are: For a 2.9MW natural gas engine, TR-STORC delivers 16% and 23% higher power output than STORC and pre-heated ORC respectively Us increased by 2.6 times than pre-heated ORC TR-STORC has 6% and 25& higher thermal efficiency than pre-heated ORC and STORC TR-STORC presents excellent exergetic performance for dual source heat recovery over STORC and pre-heated ORC 5th International Seminar on ORC Power Systems | Athens, Greece

  17. Indian Institute of Technology | Madras Future works and leads Experimental validation of heat exchanger loop using throttle valves (in progress at IIT M) Experimental validation using expanders Study of supercritical nature of refrigerants, siloxanes and other alkanes Other possibilities WHR for petroleum refineries with multiple heat streams Combined solar+ geothermal applications Single heat source applications such as geothermal by temperature splitting Compete against supercritical CO2 systems at higher source temperatures 5th International Seminar on ORC Power Systems | Athens, Greece

  18. Indian Institute of Technology | Madras Thank you.. Energy and Emissions Lab Indian Institute of Technology (IIT), Madras 5th International Seminar on ORC Power Systems | Athens, Greece

  19. Indian Institute of Technology | Madras Contact details Anandu Surendran Research Scholar (Ph.D) FMB #121 Energy and Emissions Lab Fluid Mechanics Division Department of Applied Mechanics , IIT M Email: anandusurendran@smail.iitm.ac.in Ph no: 9446525291, 7550160214 Dr. Satyanarayanan Seshadri Assistant Professor FMB #201 Fluid Mechanics Division Department of Applied Mechanics , IIT M Email: satya@iitm.ac.in Ph no: 044-2257-4078, 9845068998 Energy and Emissions Lab | Department of Applied Mechanics

  20. Indian Institute of Technology | Madras Appendix At design point Pressure ratio across HP turbine : 68 bar to 2.2 bar approx : 31 Pressure ratio across LP turbine : 2.2 bar to 1.2 bar approx : 1.8 Pressure limit: 80 bar 5th International Seminar on ORC Power Systems | Athens, Greece

  21. Indian Institute of Technology | Madras References L. Shi, G. Shu, H. Tian, and S. Deng, A review of modified Organic Rankine cycles (ORCs) for internal combustion engine waste heat recovery (ICE-WHR), Renew. Sustain. Energy Rev., vol. 92, pp. 95 110, Sep. 2018. I. Vaja and A. Gambarotta, Internal Combustion Engine ( ICE ) bottoming with Organic Rankine Cycles ( ORCs ), Energy, vol. 35, no. 2, pp. 1084 1093, 2010. G. Shu, L. Liu, H. Tian, H. Wei, and G. Yu, Parametric and working fluid analysis of a dual-loop organic Rankine cycle (DORC) used in engine waste heat recovery, Appl. Energy, vol. 113, 2014. G. Manente, A. Lazzaretto, and E. Bonamico, Design guidelines for the choice between single and dual pressure layouts in organic Rankine cycle (ORC) systems, Energy, vol. 123, pp. 413 431, 2017. J. Li, Z. Ge, Y. Duan, and Z. Yang, Design and performance analyses for a novel organic Rankine cycle with supercritical-subcritical heat absorption process coupling, Appl. Energy, vol. 235, pp. 1400 1414, Feb. 2019. S. Rech, S. Zandarin, A. Lazzaretto, and C. A. Frangopoulos, Design and off-design models of single and two-stage ORC systems on board a LNG carrier for the search of the optimal performance and control strategy, Appl. Energy, vol. 204, pp. 221 241, Oct. 2017. T. Chen, W. Zhuge, Y. Zhang, and L. Zhang, A novel cascade organic Rankine cycle (ORC) system for waste heat recovery of truck diesel engines, Energy Convers. Manag., vol. 138, pp. 210 223, 2017. T. Li, Z. Zhang, J. Lu, J. Yang, and Y. Hu, Two-stage evaporation strategy to improve system performance for organic Rankine cycle, Appl. Energy, vol. 150, pp. 323 334, 2015. S. Lecompte, H. Huisseune, M. Van Den Broek, and M. De Paepe, Methodical thermodynamic analysis and regression models of organic Rankine cycle architectures for waste heat recovery, Energy, vol. 87, pp. 60 76, 2015. U. Larsen, L. Pierobon, F. Haglind, and C. Gabrielii, Design and optimisation of organic Rankine cycles for waste heat recovery in marine applications using the principles of natural selection, Energy, vol. 55, pp. 803 812, 2013. C. Invernizzi, P. Iora, and P. Silva, Bottoming micro-Rankine cycles for micro-gas turbines, vol. 27, pp. 100 110, 2007. 5th International Seminar on ORC Power Systems | Athens, Greece

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