supercritical carbon dioxide brayton cycle for power...
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Supercritical Carbon Dioxide Brayton cycle for power generation:
Major R & D efforts and directions
Pradip DuttaDepartment of Mechanical EngineeringDepartment of Mechanical Engineering
Indian Institute of Science, Bangalore, India
Green Power - Challenges & Innovation, NTPC Energy Technology Research Alliance (NETRA) June 08– June 09, 2017
Major advantages of CSP in Indian context
What is concentrating solar power (CSP)?
• Concentrated energy → heat up a fluid → produce steam → activate turbines → electricity
• PV : Directly converts sunlight into electricity
Major advantages of CSP in Indian context
• High conversion efficiency possible• Possibility of thermal storage, hybridization• Scalability; grid compatibility• Easy to establish indigenous manufacturing• Vast indigenous experience in thermal power technology
Main components of a CSP plant
SOLAR FIELD POWER PLANT
Parabolic Trough Technology
Compact Linear FrenselReflector Technology
Power Tower Technology
Different collector technologies
Conventional Steam based Solar Thermal Plant
C
Thermal Storage
Boiler /
D
4
Steam turbine2
3
Solar field
B
Pump 2
Boiler / Heat Exchanger
Pump 1A
1
Condenser
De-aerator
Pump 3
5
6
7
Conventional Steam based Solar Thermal Plant
C
Thermal Storage
Boiler /
D
4
Steam turbine2
3
Solar field
B
Pump 2
Boiler / Heat Exchanger
Pump 1A
1
Condenser
De-aerator
Pump 3
5
6
7
Line Focus & Single Axis Tracking Point Focus & Dual Axis Tracking
Parabolic DishParabolic Trough
Present Collector Technology Options
Solar TowerLinear Fresnel
•High capital expenditure (bulky power block)•Water intensive •Expansion into two-phase region, leading to blade corrosion; water treatment issuesLow thermal efficiency (2 phase heat addition;
Problems and Limitations of Steam-based Rankine Cycle Power Plants
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corrosion; water treatment issues•Low thermal efficiency (2 phase heat addition; limitation of turbine inlet temperature) •Not easily scalable: Viable for large scale only (> 50 MW)
CSP cost Arithmetic
Solar field cost ~ 60%
Solar field Power Plant
Aim: decrease cost (low cost structure, tracking, optics, coating materials)
Aim: increasecycle efficiency
coating materials)
Develop new cycles, new engines
Develop “disruptive” technologies
Resources
High insolationModerate insolation
Potential Technology innovations for distributed CSP
1) High Efficiency CO2 Brayton cycles (100 kW – 5 MW)Supercritical CO2 Brayton cycle: >50% cycle efficiency even at 700°C receiver temperature
• also being developed for next generation nuclear power plantsplants
2) Organic Rankine Cycle (ORC) systems (25 kW -1 MW)Challenge: scale down penalty
Brief Description of Brayton cycle
Closed Brayton cycle
Constant pressure heat addition andrejection.
Efficiency of Brayton cycle dependsonly on pressure ratio
Closed cycle gas turbines are simple,
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Closed cycle gas turbines are simple,compact, less expensive and have shorterconstruction periods:
→ Better overall economics.
Simple Recuperated Closed Brayton Cycle
T-S, Recuperated Closed Brayton Cycle
CO2 Brayton Cycles: New concept
power generation =20 kW compressor OD=1.5 cm
Sandia National Labs
Supercritical
Transcritical (2-phase heat rejection)
Transcritical (1-phase heat rejection)
Sub-critical (1-phase
Supercritical CO2 Brayton: >50% cycle η even at 700ºC
Smaller vol. flow rates, low compression work, compact power block
Sub-critical (1-phase heat rejection)
S-CO2 Thermodynamic Cycle
Supercritical CO2 (S-CO2)
Major advantages:• Very high cycle efficiency (~50%)• Compact power block• Dry cooling (waterless operation)
Heat source temp: 500-700°C
Heliostat field Schematic of S-CO2 Power Plant with Solar Field
Turbine
Regenerator
Compressor Air Pre Cooler
3
4 6
1
2
5
5Air inlet
Air exit
High Pressure
Low PressureReceiver
Solar Heat Input
Heliostat Field
• Dry cooling (waterless operation)• Versatile (solar, waste heat, nuclear)
Relative sizes of Steam and SCO2 turbine
Performance studies of Brayton cycles
1
10
100
1000
0 200 400 600 800 1000 1200
Pre
ssu
re (b
ar)
Enthalpy (kJ/kg)
1TN
2′TN 3′TN
4′TN6TN
5TN1S
2′S 3′S
4′S6S
5S
308 K 873 K
1SN
2′SN 3′SN
4′SN6SN
5SN
Transcritical (TN)
Supercritical (S)
Subcritical (SN)
Turbine
Regenerator
Boiler
1
5
2
3
6
4
iHTFoHTF
850
950
3′SN3′TN3′S873 K
P-h diagram
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CompressorGas cooler
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Parametric studies•Turbine expansion ratio•Low side pressure•Heat source temp. range
Outcome of studies• Cycle efficiency• Heat recovery• Flow rates• Entropy generation• Optimization
Working fluids studied• Air, CO2
250
350
450
550
650
750
850
0.5 1 1.5 2 2.5 3 3.5 4
Tem
per
atu
re (K
)
Entropy (kJ/kg K)
1SN
2′SN
6SN
5SN4′SN
1TN
2′TN 6TN
5TN
4′TN
1S
2′S6S
5S
4′S
308 K
T-s diagram
Thermal Efficiency and its optimization
15
20
25
30
35
Ov
era
ll th
erm
al e
ffic
ien
cy (%
)
Turbine inlet temp = 873 K
p1= 1 bar
p1= 85 bar
p1= 75 bar
p1= 70 bar
p1= 40 bar
Air, p1 = 1 bar
1
10
100
1000
Pre
ssu
re (b
ar)
1TN
2′TN 3′TN
4′TN6TN
5TN1S
2′S 3′S
4′S6S
5S
308 K 873 K
1SN
2′SN 3′SN
4′SN6SN
5SNTurbine eff= 75 %
Compressor eff= 80 %
Subrcritical CO2
Transrcritical CO2
supercritical CO2
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SN-CO2 cycle, TN-CO2 cycle, ∆ S-CO2 cycle,Key Conclusions
• S-CO2 performs the best.
• Ratio of regenerator heat recovery to externally supplied ~3
• Hence, proper design of regenerator a major challenge
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1 2 3 4 5
Expansion ratio
Turbine inlet temp = 873 K1
0 200 400 600 800 1000 1200
Enthalpy (kJ/kg)
1SN 4′SN6SN
[1] Garg et al , Supercritical carbon dioxide Brayton cycle for concentrated solar power, J. Supercritical Fluids, 2013[2] Garg et al., Comparison of CO2 and Steam in Transcritical Rankine Cycles for Concentrated Solar Power, Energy Procedia, 2014
CO2 vs Steam
350
450
550
650
750
850
950
Tem
per
atu
re (
K)
2′TC
5TC
3′TC
(873 K)
3′
4′
2′
4
2
4′TC
iHTF
oHTF
350
450
550
650
750
850
950
1050
1150
Tem
per
atu
re (
K)
3′ (873 K)
3′
4′2′
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1
iHTF
o
CO2 Transcritical Condensing cycle Supercritical Steam cycle
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250
350
0.5 1 1.5 2 2.5 3Entropy (kJ/kg K)
1TC
2′TC
300 K
2
1
6TC
250
350
0 2 4 6 8 10
Entropy (kJ/kg K)
12′ 300 K
4′
oHTF
• More heat source temperature required for the same turbine inlet temperature for steam.• Easier choice of Heat transfer fluid (HTF) for CO2 .
S-CO2 has potential to replace steam in
Conventional power plant
Solar thermal power plant
Nuclear power plant
• Year 2012: US DOE awarded 10 MWe S-CO2 R&D solar plant to a consortium consisting of NREL, Sandia, Abengoa Solar, Echogen Power Systems, U. of Wisconsin and EPRI.• US Department of Energy's S-CO2 initiatives: $44 million proposed in 2016 Budget for R&D
International status: Recent highlights
S-CO2 to replace steam in
Conventional power plant
Solar thermal power plant
Nuclear power plant
Challenges of S-CO2
PCHE etched Plates
Development of turbo expander, compressor & generator
High speed equipments
Compact turbine
Development of Recuperator (PCHE)
Thermal hydraulic Design,
Mechanical Design
Fabrication Aspects
Metallic materials suitable for long term operation at
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PCHE Channels
PCHE Block Section
Metallic materials suitable for long term operation at high temperature in CO2 environment
Materials available for temperatures less than 550 0C.
Compatibility of materials with heat transfer fluid of solar plant
Fabrication aspects:
First chemically etching flow channels into plates
CO2 Brayton: Critical thermal challenges
• High T high P receivers for CO2.
• Heat exchangers: Regenerator, pre-cooler
• High T thermal energy storage system : molten salt, PCM,
particles?
• Ideally, receivers and storage systems would need an integrated • Ideally, receivers and storage systems would need an integrated
approach in design
Test loop at Sandia National Labs (for Nuclear)
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S-CO2 test loop at IISc(for Solar)
Supercritical CO2 Brayton Cycle test loop at IISc
CAD Layout • High side temperature: 550°C
• High side pressure: 140 bar.
• Nominal flow rate of C02: 11 Kg/min.
• Two stage heating 100 +45 kW
To be integrated with solar receiver
Actual loop
S-CO2 Solar Receiver Configurations
Directly heated, closed-loop supercritical CO2 Brayton
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Indirectly heated, closed-loop supercritical CO2 Brayton
Possible Solar Receivers
Cavity
Volumetric
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Tubular
Volumetric
Falling Particle
Some Existing Receiver Designs
Pressurised air receiver REFOS - Volumetric Pressurised air receiver HiTREC, DLR, 1995
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Pressurised air receiver REFOS - Volumetric cavity receiver, 1996
Pressurised air receiver HiTREC, DLR, 1995
Direct Steam Generation,
Ivanpah 2014
Molten Salt, Solar Two, California,
1999
S-CO2 Receivers : Major Issues & Challenges
Tubular Receiver
Volumetric Receiver
Falling Particle Receiver
High tube wall thickness, limitation
on allowable heat flux, high losses
Window sealing and cooling, Structural failure of absorber
Particle flow control and additional heat exchanger design
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Common Issues
Coatings : Durability at high
temperature, compatibility
with s-CO2
Response to transients and
provision of inbuilt storage
Reduction in strength of
materials at high temperature
High and uneven thermal
expansion
Falling Particle Receiver
Falling particle receiver at Sandia National Lab Conceptual design of a s-CO2 falling particle receiver
•High temperature heat transfer to working fluid•Efficient absorption; no flux limitation as in tubular•Possibility of cost effective storage (e.g. sand particles)•Scalable• Specific heat : 1.5-2 kJ/kg.K; density ~ 3000 kg/m3.
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Concept 1: Straight Tubular receiver
Integrated optical-thermal modelRay Trace Model with Receiver Concept
Prototype of High Temperature CO2 Receiver (Sandia, , IISc, IITB) CSP 1
Ray Trace Model with Heliostat Field and Target
Bladed receiver design tested at SandiaBladed Panel Receiver
Flat Panel Receiver
Prototype manufacturing at Sandia
Concept 2: Helical coil cavity receiver
Irradiation Entering Cavity
Small scale model (~1 kWth) tested with compressed air and Fresnel lens test rig at IISc
Prototype of High Temperature High CO2 Receiver (Sandia, , IISc, IITB) CSP 1
Temperature distribution using air
Scaled up prototype (~10 kWth) being developed; On-sun test rig with 32 m2 Schefflerdish close to S-CO2 loop
Flux characterization using PHLUX method: Approx flux ~10 kW
Small scale module; Testing and
S-CO2 Volumetric Solar Receiver (BHEL, IISc) CSP Core 2
Development of CFD tools for volumetric receiver •Discrete Ordinates Method (DOM) for radiation heat transfer modelling coupled with FVM in ANSYS Fluent
QUARTZ GLASS – Successful demonstration with compressed air, no failure due to thermal effects
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Small scale module; Testing and validation for radiation properties, window material and sealing qualifications
Summary:1. Quartz based ceramic closed volumetric air receiver
successfully demonstrated2. Scalability of design to larger scales, higher pressures
with s-CO2 identified as potential challenges
Indirect heating of s-CO2 using ceramic based Air-s-CO2 HEX with inbuilt storage being exploredcurrently
Modeling and Experimental Evaluation of Air–Ceramic Heat Transfer and Thermal Storage Dynamics
Experimental setup and test sample
Mullite, hexagonal channels with a wall thickness of 1 mm, geometric porosity 40 %
Flow rate ~ 0.0038 kg/sT1- T5: K-type thermocouplesMass of sample: 0.450 kg
CHARGING Inlet ~873 KDISCHARGING Inlet ~300 K
SampleDensity
(kg/m3)
Specific
heat
(J/kgK)
Thermal
Conductivit
y
(W/mK)
Mullite
(3Al2O3 2SiO2)3130 1000 1.25
Chromite
(FeCr2O4)3750 1200 1.4
Numerical Simulation was performed using ANSYS Fluent to study the effects of the following parameters on heat storage
:
Channel shapes
•Square
•Hexagon
Flow rates (kg/s)
•0.001, 0.0015
•0.002
Individual Channel area (mm2)
•4, 16, 36, 64
0.001 kg/s, 300 seconds, square 4 mm2
Sample Temp Distribution
Conclusions
• New thermodynamic cycles required for addressing CSP performance issues under different design conditions
• s-CO2 is a promising working fluid for high temperature application: but issues with materials, thermophysicalproperties, heat exchanger design, high peed properties, heat exchanger design, high peed torbomachinery
• Receiver design for high pressure and high temperature very crucial
• Challenges in Recuperator heat exchanger design and mnufacuring - PCHE
Thank you
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