Tutorial: Fundamentals of Supercritical...
Transcript of Tutorial: Fundamentals of Supercritical...
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Tutorial: Fundamentals of Supercritical CO2
Grant Musgrove Aaron M. Rimpel
Jason C. Wilkes, Ph.D.
Southwest Research Institute
March 28, 2016
© Southwest Research Institute 2015
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Abstract The recent interest to use supercritical CO2 (sCO2) in power cycle
applications over the past decade has resulted in a large amount of literature that focuses on specific areas related to sCO2 power cycles in great detail. Such focus areas are demonstration test facilities, heat exchangers, turbomachinery, materials, and fluid properties of CO2 and CO2 mixtures, to name a few. As work related to sCO2 power cycles continues, more technical depth will be emphasized in each focus area, whereas those unfamiliar with the topic are left to undertake the large task of understanding fundamentals on their own.
The following content provides an introductory tutorial on sCO2 used in power cycle applications, aimed at those who are unfamiliar or only somewhat familiar to the topic. The tutorial includes a brief review of CO2 and its current industrial uses, a primer on thermodynamic power cycles, an overview of supercritical CO2 power cycle applications and machinery design considerations, and a summary of some of the current research and future trends.
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This tutorial provides an introduction to sCO2 in power cycle applications
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sCO2 loop hardware
Supercritical CO2 (sCO2)
Power cycle applications
Research and future trends
Fossil Fuel
Ship-board Propulsion
Geothermal[6-1] [6-2]
[6-3]
[6-4]
[6-5]
Concentrated Solar Power
Pcrit = 7.37 MPa (1070 psi)Tcrit = 31
C (88
F)
Supercritical region
Two-phase region
CO2
7.37 MPa
31
C
Increasing isobars
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CO2 General Information
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Spring
Autumn
Image source [1-1]
CO2 is a gas at atmospheric conditions with a concentration of ≈ 400 ppm
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combustion
fossilization
volcanic activity
respiration respiration
phot
osyn
thes
is
respiration in decomposers
non-energy uses, oil+gas production
byproducts, etc.
Carbon compounds in dead matter
(biomass)
Organic compounds in animals
Organic compounds in plants
Carbon in fossil fuels
Carbon compounds in geological formations
feeding
CO2 in atmosphere
Image source [1-3]
There are both industrial and natural contributors and consumers of CO2 in our atmosphere
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9 Source: “U.S. Climate Action Report 2014”
Fossil fuel combustion is the largest industrial contributor to CO2 production
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Transportation (petroleum) and electricity generation (coal) majority contributors of CO2
Source: “U.S. Climate Action Report 2014”
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International regulations are continually reducing CO2 emissions in vehicles
11 Source: International Council on Clean Transportation, Policy Update 2014
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Food & beverage
Fire extin-guishers
Welding (shield gas)
Agriculture
Oil & gas production (more info with sCO2)
Various image sources [1-4]
CO2 Industrial Applications
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What is Supercritical CO2?
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CO2 is supercritical if the pressure and temperature are greater than the critical values
REFPROP (2007), EOS CO2: Span & Wagner (1996)
Supercritical region
Two-phase region
7.37 MPa (1,070 psi)
31°C (88°F)
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Video of Supercritical CO2
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Image source: [2-2]
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Air
Air
GT TIT
pp T
hC
∂∂
= CO2
Supercritical region
CO2
Fluids operating near their critical point have dramatic changes in enthalpy
REFPROP (2007)
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CO2 density sharply decreases near the critical point
REFPROP (2007)
Supercritical region
10%
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CO2 density sharply decreases near the critical point
REFPROP (2007)
Supercritical region
30% ∆ρ = 10%
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CO2 density decreases near the critical point
REFPROP (2007)
Supercritical region
70% ∆ρ = 30%
∆ρ = 10%
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CO2 speed of sound decreases through the critical point
CO2
REFPROP (2007)
Supercritical region
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Supercritical region
Air
Water
CO2 viscosity decreases through the critical point
1 µPa-s = 10-6 kg/m/s REFPROP (2007)
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10
100
1000
100 200 300 400 500 600 700 800 900 1000
Thermal Conductivity
[mW/m/K]
Density [kg/m3]
CO2 thermal conductivity is enhanced near the critical region
305K 307K
309K
350K
Critical density
REFPROP (2007)
Water
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10
100
1000
100 200 300 400 500 600 700 800 900 1000
Thermal Conductivity
[mW/m/K]
Density [kg/m3]
CO2 thermal conductivity is enhanced near the critical region
305K 307K
309K
350K
Critical density
REFPROP (2007)
Water
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Power Cycle Basics
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Power Cycle Basics Overview
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Carnot – “the standard”
Brayton – gas cycle
Rankine – vapor cycle
Differences between ideal and actual cycles Improvements to simple cycle
Also…
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Carnot Cycle Processes
(1-2) Isothermal heat addition (2-3) Isentropic expansion (3-4) Isothermal heat rejection (4-1) Isentropic compression
Not practical to build Most efficient heat
engine
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Qout Qin
Wturb
Tem
pera
ture
Entropy
Qout
Qin
TH
TL
1
2
3
4
1 2
3 4
S1 = S4 S2 = S3
ηth,Carnot = 1 – TL/TH
TL : Limited by available sink
TH : Limited by materials
Comp. Comp. Turb. Turb.
Wnet = Wturb - Wcomp
Wcomp
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∫ ⋅
−
dST
QQ outin
∫ ⋅
−
dVP
WW outin
Thermodynamics Aside… 1st Law
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∫ ⋅dVP
Pres
sure
, P
Volume, V
1
2 3
4
∫ ⋅dST
Tem
pera
ture
, T
Entropy, S
1
2
3
4
Net Mechanical Work Produced
Net Heat Utilized =
=
= C
T
P
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Brayton Cycle (Ideal) Processes
(1-2) Isentropic compression (2-3) Const. pres. heat addition (3-4) Isentropic expansion (4-1) Const. pres. heat reject.
Open- or closed-loop
51
ηth,Brayton = 1 – PR(1-k)/k
Comp. Turb.
HP-HE
LP-HE
Qin
Qout
Wnet
1
2 3
4
Tem
pera
ture
, T
Entropy, S
1
2
3
4
Qout
Qin
Tem
pera
ture
, T
Entropy, S
Tmax
Tmin
PR, k : ηth
Optimal PR for net work
Closed-loop
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Rankine Cycle (Ideal) Processes
(1-2) Isentropic compression (2-3) Const. pres. heat addition (3-4) Isentropic expansion (4-1) Const. pres. heat reject.
Same processes as Brayton; different hardware
Phase changes E.g., steam cycle
52
Turb.
Boiler
Condenser
Qin
Qout
WT,out
1
2 3
4
Pump WP,in
Tem
pera
ture
, T
Entropy, S
Qin
Qout
Liquid
Gas
Liquid+ Vapor
1
2
3
4
ηth = 1 – Qin/Qout
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Ideal vs. Actual Processes
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1-2, 3-4: Irreversibilities
2-3, 4-1: Pressure losses
Brayton Rankine
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Power Cycle Variations
Regeneration Intercooling Reheating Recompression
What is supercritical power cycle?
54
…
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Brayton Cycle + Regeneration
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T4 < T2
Regenerator = counter-flow HE (a.k.a. recuperator)
Effectiveness: ε = (h5-h2)/(h4-h2)
Figure reference: Cengel and Boles (2002)
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Intercooling & Reheating… Two Sides of the Same Coin
56
Minimize compressor work input
Increase fluid density
Intercooling
Maximize turbine work output
Decrease fluid density
Reheating
Multi-stage intercooling
Multi-stage reheating
Approach isothermal conditions
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Multi-Stage Intercooling & Reheating
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Multi-stage reheat
Multi-stage intercool
Approximates Ericsson cycle
≈ Isothermal expansion
≈ Isothermal compression
ηth,Ericsson = ηth,Carnot Figure reference: Cengel and Boles (2002)
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Brayton Cycle + Regeneration + Intercooling + Reheating
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Figure reference: Cengel and Boles (2002)
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60 Source: Ludington (2009)
Regeneration vs. Recompression in Brayton Cycle
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Rankine Cycle + Reheating
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Multi-stage reheat
Figure reference: Cengel and Boles (2002)
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What is a Supercritical Power Cycle?
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Tem
pera
ture
, T
Entropy, S
Supercritical region
Tcrit
Pcrit
Liquid region
Gas region
Liquid + vapor region
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sCO2 Power Cycles
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Why sCO2 for Power Cycles?
64
Property Effect High density near C.P.
• Reduced compressor work, large Wnet • Allow more-compact turbomachinery to achieve same
power • Less complex – e.g., fewer compressor and turbine stages,
may not need intercooling Near-ambient Tcrit
• Good availability for most temperature sinks and sources
Abundant • Low cost Familiar • Experience with standard materials
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CO2 Critical Point Comparison
65 REFPROP (2007)
Critical Pressure
Critical Temperature
(3626)
(2901)
(2176)
(1450)
(725)
(psi) MPa 25
20
15
10
5
0 0 200 400 600 800 1000
(360) (720) (1080) (1440) (1800)
H2O
SO2
R134a
CO2
Air
He
Ambient
(R)
K
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CO2 Cost Comparison*
66
*Based on market pricing for laboratory-grade substance
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The sCO2 power cycle can provide efficiencies near a steam cycle for less $/kWh
67 Source: Wright (2011) and Dostal (2004)
HeSteam
He
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Relative Size of Components
68
Adapted from Dostal (2004)
5 m Steam turbine: 55 stages / 250 MW
Mitsubishi Heavy Industries (with casing)
Helium turbine: 17 stages / 333 MW (167 MWe) X.L. Yan, L.M. Lidsky (MIT) (without casing)
sCO2 turbine: 4 stages / 450 MW (300 MWe) (without casing)
Note: Compressors are comparable in size
1 m
Source: Wright (2011)
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Example: 10 MWe Turbine Comparison
69 Source: Persichilli et al. (2012)
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sCO2 in Power Cycle Applications
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Supercritical CO2 in Power Cycle Applications
119
Nuclear
Fossil Fuel
Ship-board Propulsion
Geothermal [6-1] [6-2]
[6-3]
[6-4]
[6-5]
Concentrated Solar Power
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“Typical” sCO2 Cycle Conditions Application Organization Motivation Size [MWe] Temperature
[C] Pressure
[bar] Nuclear DOE-NE Efficiency, Size 300 - 1000 400 - 800 350
Fossil Fuel DOE-FE Efficiency, Water Reduction
500 - 1000 550 - 1200 150 - 350
Concentrated Solar Power
DOE-EE Efficiency, Size, Water Reduction
10 - 100 500 - 800 350
Shipboard Propulsion
DOE-NNSA Size, Efficiency 10, 100 400 - 800 350
Shipboard House Power
ONR Size, Efficiency < 1, 1, 10 230 - 650 150 - 350
Waste Heat Recovery
DOE-EE ONR
Size, Efficiency, Simple Cycles
1, 10, 100 < 230; 230-650 15 - 350
Geothermal DOE-EERE Efficiency, Working fluid
1, 10, 50 100 - 300 150
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Heat Source Operating Temperature Range & Efficiency
121
Assumptions (Turbomachinery Eff (MC 85%, RC 87%, T 90%), Wright (2011)
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Nuclear
Fossil Fuel
Ship-board Propulsion
Geothermal [6-1] [6-2]
[6-3]
[6-4]
[6-5]
Concentrated Solar Power
Supercritical CO2 in Power Cycle Applications
122
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Concentrated Solar Power (CSP) The Sun-Motor (1903)
• Steam Cycle • Pasadena, CA • Delivered 1400 GPM of water
Solar One (1982) • 10 MWe water-steam solar
power tower facility • Barstow, CA • Achieved 96% availability
during hours of sunshine Solar Two (1995)
• Incorporated a highly efficient (~99%) molten-salt receiver and thermal energy storage system into Solar One.
123
Image source: [6-7]
Image source: [6-6]
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CSP – Improvement Opportunities
124
Advanced power cycles • Supercritical steam
Rankine • High temperature
air Brayton • Supercritical CO2
Cooling • 650 gal H20/MWh • Dry-cooling technology
is needed in most desert venues for CSP
− 43°C Dry bulb • Printed circuit heat
exchangers may provide a solution
• Supercritical CO2
Image source: [6-1]
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sCO2 CSP Process Diagram
125
Dual-shaft, tower receiver sCO2 Brayton Cycle solar thermal power system with thermal energy storage, Zhiwen and Turchi (2011)
Heliostats
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CSP Efficiencies vs. Power Cycle
126
Data from Stekli (2009)
0%
20%
40%
60%
80%
100%
0 250 500 750 1000 1250 1500
Cycle Efficiency
Cycle Temperature [°C]
Commercial Lab/Pilot
Concept Demonstration
Subcritical H2O Air Brayton
Air Brayton CC
Supercritical H2O
Supercritical CO2 Supercritical CO2 CC
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The transient challenges of a concentrated solar power plant are significant
01020304050
12:00 AM 6:00 AM 12:00 PM 6:00 PM 12:00 AM
Ambient Temperature °C
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Optimal Cycle Configuration with varying Compressor Inlet Temperature
• SAM modeling of typical sites shows an annual average compressor inlet temperature to be 37-38ºC assuming 15ºC approach temperature in the cooler
• Cycle Modeling – Optimal flow split
• 22-33% • Heavily dependent on CIT
– Optimal PR • Varies with use of
intercooling
– Intercooled cycles are more efficient on hot days, and less efficient on cool days
128
35 40 45 50 5545
46
47
48
49
50
51
Cyc
le E
ffici
ency
[%]
Comparison of Recompression Cycles:Flow Split and Pressure Ratio at Best Efficiency Points
35 40 45 50 5520
25
30
35
Flow
Spl
it [%
]
35 40 45 50 55
Compressor Inlet Temp [ ° C]
2.5
3
3.5
Pre
ssur
e R
atio
[-]
A
A
A
B
B
B
Average Annual Inlet Temp/ Design Point
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Wide-Range Impeller Requirements
• Range Requirements at Optimal Efficiency Condition (without using range reduction techniques)
– Compressor > 55% – Recompressor > 37%
• Control Strategies – Alter flow split and pressure ratio to
reduce compressor requirements – Control compressor inlet temperature – Employ inlet guide vanes
129
0102030405060708090
0.0 0.2 0.4
Poly
trop
ic H
ead,
kJ/
kg
Volume Flow, m3/s
Main Compressor - No Intercooling
Recompressor - No Intercooling
Main Compressor - Intercooled
Recompressor - Intercooled
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CSP Compressor Inlet Variation and Turbomachinery Performance
132
Figure 5: Comparison of Operating Range and Pressure Ratio Requirements [Modified from Japikse[5]]
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Conceptual 10 MWe Integrally Geared Compressor Applied to Recuperated Brayton Cycle
Expanders
Compressors
Re-Compressors
Main Oil Pump
Shaft to Generator
Generator
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IGC Offers Compact Configuration for this Application
Generator
Turbine Gea
rbox
R
e-C
ompr
esso
r C
ompr
esso
r
Generator G
earb
ox
Compressor Re-
Compressor G
earb
ox
Turbines
Typical IGC Package
Conventional Turbomachinery Train
• An IGC package incorporates all the key elements of a conventional train in a much more compact package
• Compressor, re-compressor, turbine and gearbox are assembled in a single compact core. • The second gearbox, additional couplings and housings in the conventional train can be eliminated • Simple IGC package can potentially reduce costs by up to 35% • Reduced mechanical complexity improved reliability and reduced maintenance
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Nuclear
Fossil Fuel
Ship-board Propulsion
Geothermal [6-1] [6-2]
[6-3]
[6-4]
[6-5]
Concentrated Solar Power
Supercritical CO2 in Power Cycle Applications
135
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Rankine Cycle Application: Nuclear Power Generation
136
Image source: [6-8]
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sCO2 for Nuclear Applications (550°C-700°C, 34 MPa)
137
Image source: [6-4]
Image source: [6-9]
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Proposed Nuclear sCO2 Cycles Direct Cycle
• No primary and secondary Na loops
• Lower Void Reactivity
Indirect Cycle
• Primary Na loop • Smaller core
size
138 Kato et al. (2007)
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Nuclear Plant Efficiency vs. Cycle Prop.
140 Kato et al. (2007)
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Advantages of CO2 Cycle vs. Helium Cycle in Nuclear Applications
Pro Con Smaller turbomachinery than steam or helium
Helium preferred to CO2 as a reactor coolant for cooling capability and inertness
CO2 Brayton cycles are more efficient than helium at medium reactor temperatures
CO2 requires a larger reactor than helium or an indirect cycle
CO2 is 10× cheaper than Helium New technology
141
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Fossil Fuel [6-1] [6-2]
Supercritical CO2 in Power Cycle Applications
142
Nuclear Ship-board Propulsion
Geothermal [6-3]
[6-4]
[6-5]
Concentrated Solar Power
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Oxy-Fuel Combustion
143
Conventional Combustion
Air2 2(78% N , 21% O )
(Solar Turbines 2012)Fuel
Oxy-Fuel Combustion
Fuel 2H O
2O 2CO
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Direct Oxy-Fuel Combustion
144
Power Out
NG
CO2 Compressor
Oxy Combustor
CO2 Turbine
HRSG Steam
Rankine Cycle
Steam Turbine
Generator
Generator
Condenser
Water
Electricity
Electricity
O2
CO2 CO2
CO2
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Indirect Oxy-Fuel Combustion
145
Zero Emission Oxy-Coal Power Plant with Supercritical CO2 Cycle, Johnson et al. (2012)
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Ship-board Propulsion
[6-5]
Nuclear
Fossil Fuel
Geothermal [6-1] [6-2]
[6-3]
[6-4]
Concentrated Solar Power
Supercritical CO2 in Power Cycle Applications
146
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Ship-board Propulsion Nuclear sCO2 cycles? Improved power to weight Rapid startup Bottoming cycles
147 Source: Dostal (2004)
Image source: [6-10]
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Nuclear
Fossil Fuel
Ship-board Propulsion
[6-1] [6-2]
[6-4]
[6-5]
Concentrated Solar Power
Supercritical CO2 in Power Cycle Applications
148
Geothermal [6-3]
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Geothermal Low Temperature Heat Source
• T ≈ 210°C, P ≈ 100 bar
149 Pruess (May 19, 2010)
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Other sCO2 Power Cycle Applications
150
Waste Heat Recovery
Non-Concentrated Solar Power
Zhang (2005)
Image source: [6-11] Combined Heat & Power
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Waste Heat Recovery (Bottoming)
Rankine Cycle Description 1. Liquid CO2 is pumped to supercritical pressure 2. sCO2 accepts waste heat at recuperator and
waste heat exchanger 3. High energy sCO2 is expanded at turbo-
alternator producing power 4. Expanded sCO2 is cooled at recuperator and
condensed to a liquid at condenser
151
1
2
3
4
Image source: [6-11]
Image source: [6-12]
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sCO2 Rankine Cycle in Non-Concentrated Solar Power NCSP (Trans-critical Rankine) Tt = 180°C
• ηe,exp = 8.75%-9.45% Photovoltaic
• ηe,exp = 8.2%
152
Zhang (2007)
Zhang (2005)
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sCO2 Rankine Cycle in Combined Heat and Power (CHP) Electrical efficiency
• Higher than ordinary steam CHP • Cascaded s-CO2 plant performed best
153 Moroz (2014)
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sCO2 as a Refrigerant
154
Image source: [6-13] Image source: [6-14]
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sCO2 vs R-22 in Refrigeration
155 Brown (2002)
Employed MCHEs Summary
• CO2 COP vs. R-22 − 42% Lower at 27.8°C − 57% Lower at 40.6°C
• Majority of entropy generation in CO2 cycle was in the expansion device
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sCO2 in Heat Pumps
sCO2 replaced as a refrigerant in domestic heat pump hot water heater in Japan. • COP = 8, 90°C (194°F) • Compared to COPtyp=4-5
156
EcoCute Heat Pump (2007)
h e
e
Q WCOPW
+=
Image source: [6-14]
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157
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sCO2 Power Cycle
Research Efforts
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Development of a High Efficiency Hot Gas Turbo-expander and Low Cost Heat Exchangers for Optimized CSP SCO2 Operation J. Jeffrey Moore, Ph.D. Klaus Brun, Ph.D. Pablo Bueno, Ph.D. Stefan Cich Neal Evans Kevin Hoopes Southwest Research Institute C.J. Kalra, Ph.D., Doug Hofer, Ph.D. Thomas Farineau General Electric John Davis Lalit Chordia Thar Energy Brian Morris Joseph McDonald Ken Kimball Bechtel Marine
159
Taken from SunShot Subprogram Review: Concentrating Solar Power (Sunshot Grand Challenge Summit Anaheim, CA, May 19-22, 2014)
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Project Objectives To develop a novel, high-efficiency supercritical sCO2 turbo-expander
optimized for the highly transient solar power plant duty cycle profile. – This MW-scale design advances the state-of-the-art of sCO2 turbo-expanders
from TRL3 to TRL6. To optimize compact heat exchangers for sCO2 applications to drastically
reduce their manufacturing costs. The turbo-expander and heat exchanger will be tested in a 1-MWe test
loop fabricated to demonstrate component performance and endurance. Turbine is designed for 10 MW output in order to achieve industrial scale The scalable sCO2 expander design and improved heat exchanger address
and close two critical technology gaps required for an optimized CSP sCO2 power plant
Provide a major stepping stone on the pathway to achieving CSP power at $0.06/kW-hr levelized cost of electricity (LCOE), increasing energy conversion efficiency to greater than 50% and reducing total power block cost to below $1,200/kW installed.
160
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Work has been divided into three phases that emulate development process from TRL3 to TRL6 Phase I – Turbomachinery, HX, and flow loop
design (17 months) Phase II – Component fabrication and test
loop commissioning (12 months) Phase III – Performance and endurance testing
(6 months)
Project Approach
161
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Recuperator Prototypes – 5 and 50 kW
164
DMLS: • Expensive and slow to build • Highly automated • High pressure drop • Tested to 5000 psi
Laser Welded Construction: • Undergoing flow tests • Exceeded design predictions for
HTC • Held 2500 psi @ 600°F
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A novel turboexpander has been designed to meet the requirements of the sCO2 power with these targets:
• ~14MW shaft power • >700C inlet temp • >85% aero efficiency
TURBOEXPANDER DESIGN
CFD Analysis
DGS Face Pressure Distribution from CFD
Multi-stage Axial Turbine
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10 MW SCO2 Turbine Concept
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Test Loop Design
168
SwRI B278
Heater
sCO2 Pump
Compressor
Cooler
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Mechanical Test Configuration
169
Pipe Section Color Pump to heater Dark blue
LT heater to recuperator Yellow Recuperator to HT heater Orange
HT heater to expander Red
Expander to recuperator Dark green
Recuperator to existing Light green
Existing facility piping White Existing facility piping
(unused) Dark gray
Existing piping to pump Light blue
Recuperator
Expander Silencer Air dyno.
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Test heat exchanger prototypes Heat exchanger design nearing completion Complete Turbomachinery Design Procure long lead items for expander and test
loop Finalize test loop design
Future Work
170
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DOE sCO2 Test Program
Research compression loop • Turbomachinery performance
Brayton cycle loop • Different configurations possible
− Recuperation, Recompression, Reheat • Small-scale proof-of-technology plant • Small-scale components
− Different than hardware for commercial scale
171
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DOE sCO2 Test Program Turbomachinery
172
100 mm
Source: Wright (2011)
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sCO2 Brayton Cycle Test Loop
173 Source: Wright (2011)
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sCO2 Brayton Cycle Test Loop
174 Source: Wright (2011)
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sCO2 Brayton Cycle Performance with Regeneration Config.
178 Source: Conboy et al. (2012)
Maximum Case: Total Turbine Work, 92 kW
Improve with larger scale: • Windage losses • Thermal losses • Seal leakage
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DOE sCO2 Test Program Summary
Major milestones • Test loops operational • Demonstrate process stability/control
Areas for future development • Heat exchanger performance • Larger scale test bed
− Utilize commercial-scale hardware − Demonstrate more-realistic (better) performance
• CO2 mixtures
179
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Printed Circuit Heat Exchanger (PCHE)
180 Heatric PCHE
Le Pierres (2011)
sCO2 test loop used by Sandia/ Barber-Nicholls
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Heat Exchanger Testing (Bechtel) 150 kW 8000 lbm/hr sCO2
2500 psi
181 Nehrbauer (2011)
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Tokyo Institute of Technology (TIT)
182 (Kato et al., 2007)
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Corrosion Loop at Tokyo Institute of Technology
186
316 SS, 12% Cr alloy, 200-600°C, 10 Mpa CO2, Kato et al. (2007)
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Other sCO2 Corrosion Test Facilities
MIT - 650°C, 22 MPa • Steels
UW - 650°C, 27 MPa • Steels
French Alternative Energies and Atomic Energy Commission - 550°C, 25 MPa • Steels
MDO Labs – 54.4°C, 12.4 MPa • Elastomers, engineering plastics, rubbers,
etc.
187
Guoping (2009)
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Geothermal Research
188
Schematic of EGS with sCO2 Pruess (May 18, 2010)
Explore the feasibility of operating enhanced geothermal systems (EGS) with CO2 as heat transmission fluid
Collaboration between LBNL (Pruess), UC Berkeley (Glaser), Central Research Institute of the Electric Power Industry, Japan (Kaieda) and Kyoto University (Ueda) • UC Berkeley: laboratory testing of CO2 heat extraction • Japan: inject brine-CO2 mixtures into Ogachi HDR site (T ≈ 210°C, P ≈ 100 bar) • LBNL: model reactive chemistry induced by brine-CO2 injection
Ogachi, Japan – HDR Site Pruess (May 19, 2010)
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sCO2 Critical Flow (Univ. Wisconsin)
189
(Anderson, 2009)
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Future Trends for
sCO2 Power Cycles
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Future trends and research needs
Rotordynamics Analysis of rotor-dynamic cross-coupling coefficients for sCO2
Heat Exchangers Improved heat transfer correlations near the critical region for varying geometries Improve resolution of local heat transfer measurements Heat exchanger durability – studying effects of material, fabrication, channel geometry, fouling, corrosion, and maintenance
Materials Long term corrosion testing (10,000 hrs) Corrosion of diffusion-bonded materials (PCHE HX) Coatings to limit/delay corrosion Corrosion tests under stress
Pulsation analysis Development of transient pipe flow analysis models for sCO2
Intermediate-scale is needed to demonstrate commercial viability of full-scale technologies (i.e. 10 Mwe)
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Detailed models of turbo machinery Improved transient analysis – surge, shutdown events
Fluid properties Mixture of sCO2 and other fluids Physical property testing of CO2 mixtures at extreme conditions with significantly reduced uncertainties (i.e. < 1%)
Control System and Simulation
Future trends and research needs
10 MW Scale Pilot Plant
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Summary
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195
Both supercritical power cycles and the use of sCO2 are not new concepts
sCO2 is used in a variety of industries as a solvent
sCO2 is desirable for power cycles because of its near-critical fluid properties
Supercritical region
CO2
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0.00
0.25
0.50
0.75
1.00
1.25
1.50
0 10000 20000 30000
Impeller Dia.[m]
Shaft Speed [rpm] 196
sCO2 power cycles can be applied to many heat sources and have a small footprint
The near ambient critical temperature of CO2 allows it to be matched with a variety of thermal heat sources
The combination of favorable property variation and high fluid density of sCO2 allows small footprint of machinery
Concentrated Solar Power
Nuclear
Fossil Fuel
Ship-board Propulsion
Geothermal
PR = 1.4AirS-CO2
AirS-CO2
PR = 2.0
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197
The near future goal is to improve understanding and develop commercial-scale power
International sCO2 power cycle research is ongoing
More research is needed sCO2 power cycle applications
Power production test loops
Machinery component test loops Fluid property testing
Materials corrosion test facilities
Intermediate scale (10MW) demonstration
Materials testing at high temperature, pressure and stress
Property testing with sCO2 mixtures
Rotordynamics with sCO2
sCO2 heat transfer and heat exchangers
More detailed dynamic simulation and control systems
Questions?