technology readiness of 5th and 6th generation compliant-v002
TRANSCRIPT
Technology Readiness of 5th and 6thGeneration Compliant Foil Bearing for
10 MWE S‐CO2 Turbomachinery SystemsH. Heshmat, J. F. Walton‡ and J. L. Cordova
The 6th International Supercritical CO2 Power Cycles SymposiumMarch 27 ‐ 29, 2018, Pittsburgh, Pennsylvania
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‡ Presenting Author
Overview• Objectives • Background• Technology• Summary and Conclusions
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MITI Oil‐Free Turbomachinery ‐ Compressors
3
Hydrogen Pipeline Compressor
200 kW
Hydrogen Blower
1 kW
Fuel Cell Compressor
12 kW
Air Cycle Machine
30 kW
120,000 rpm360,000 rpm 60,000 rpm120,000 rpm
MITI Oil‐Free Turbomachinery ‐ Energy
4
60 kWe
Flywheel Electromechanical Battery
8 kWe
180,000 rpm
Gas Turbine Generator ORC Turbogenerator
65 kWe
30,000 rpm60,000 rpm
Objectives
• Identify Turbomachinery Concepts Capable Of Operating Efficiently With s‐CO2
• Identify Key Enabling Bearing Technology• Oil‐Free Compliant Foil Bearings• Use s‐CO2 Process Fluid for Hydrodynamics and Thermal Management• Scalable For Multi‐Megawatt Turbomachinery Applications from kW to 100s of MW
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Preliminary Cycle Analysis for Net 10 MW System
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Sink Source
Low T Recuperator
High T Recuperator
7.9 MPa
18.4 MPa
18.1 MPa750°C128 kg/s
60 krpmP = 11 MWe
8.0 MPa
Re‐CompressorMain Compressor
18.3 MPa
Preliminary 1st Order Aero Analysis
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Turbine Rotor Concept
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53.3 cm (21 inch)
35.6 cm (14 inch)
5 MW Turbo‐Compressor (2x)
Compressor Inlet
Compressor Discharge
Turbine Inlet
Turbine Discharge
Journal Bearings
Thrust Bearings
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50‐80 krpm
General Bearing Characteristics
0 Speed or Reynolds No.0
20
40
60
80
100
RigidIncompressible
Fluid FilmBearing
Compressible FluidFilm Bearing
IncompressibleFluid
CompressibleFluid/Gas
Rolling ElementBearing
Speed
815
175150
Fluid Film
Rolling Element
Compliant Foil
Active Magnetic
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Foil Bearing Fundamental Mechanisms
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KHydro
KStruct
BHydro
BStruct
Coating
MiTi Korolon Coated Foil Bearings Demonstrated with Different Process Fluids
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Air, H2, He(H2+H2O)
R134a, 245fa,R1233zd & R1234yf,
s-CO2
2-Phase Flow
Complexities of Mechanisms
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Extent of Bearing pad surface compliancy10° (leading edge) 350° (trailing end)
0.0 0.2 0.4 0.6 0.8 1.0
Normalized Foil Compliancy Matrix
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..
.
.
Foil Bearing Film Pressure and Height
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Comparison of Rigid vs Compliant Bearingsat 60,000 rpm
0
250
500
750
1,000
1,250
1,500
1,750
2,000
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
Maxim
um Loa
d (lbs)
Eccentricity Ratio
Foil Bearing Compressible
Rigid BearingCompressilbe
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s‐CO2 Foil Bearing Characteristics
‐6.00E+06
‐4.00E+06
‐2.00E+06
0.00E+00
2.00E+06
4.00E+06
6.00E+06
8.00E+06
1.00E+07
1.20E+07
0.0
0.5
1.0
1.5
2.0
2.5
0.00 0.20 0.40 0.60 0.80 1.00
Stiffne
ss (lb/in)
Min Film
(mils) &
Pow
er (H
P)
Eccentricity Ratio
2.5 Inch Diameter Foil Bearing Performance vs Eccentricity ratio at 60 krpm
HN (mils) P (HP) KXX KXY KYX KYY
Power Loss
Stiffness
Min. Film Height
Film Pressure, Load and Stiffness With
Turbulence
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Load PerformanceDynamic Characteristics
Foil Bearing for 100 MW Scale
‐5.00E+06
0.00E+00
5.00E+06
1.00E+07
1.50E+07
0 2,000 4,000 6,000 8,000 10,000
Stiffne
ss (lb/in)
Speed (rpm)
3150 lb Turbine Speed Dependent SCO2 Foil Bearing Stiffness
KXX KXY KYX KYY
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Scalability of Foil Bearings from 1 to 100s MWe
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20
KorolonTM 1350A coated foil after 50 thermal cycles and bend testing
YSZ coated foil fractured after thermal cycling and bend testing
Representative sets of thermal cycles for thin foils
Bend Testing After 815°CThermal Cycling
815°C
95°C
Korolon
YSZ
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MiTi Bomb Setup to Expose Korolon Coated Foils to SCO2 at >675oC and >80 Bar
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Korolon Coated Bearing Foil Before & After Exposure to SCO2
Pretest Bend Posttest Bend
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Post Exposure Tribological Test
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MiTi Korolon™ Coated Foil Sample After Exposure to 650°C SCO2 and 500 Start/Stop Cycles
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Measured High Temperature Foil Bearing Performance
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Thermal Performance of Foil Bearing Gen IV
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Bearing Len x Diam = 100 x 75 mm2
26
5+ Hour Elevated Temperature Test
Time (Minutes)0 50 100 150 200 250 300 350
Tem
pera
ture
(C)
0
200
400
600
800
1000
Spee
d (k
rpm
)
0
5
10
15
20
25
30
35
Bearing Chamber
Bearing Inboard
Speed
Bearing Free End
20269‐T16R3ABCD
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High Temperature Foil Bearing
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870°C
815°C
Bearing Housing and Foil Temperatures
Bearing Shell Temperatures Bearing Foil Temperatures
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Foil Bearing Generations/Classes
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Summary & Conclusions• s‐CO2 Turbomachinery is Compact and Operates at High‐Speed • High Temperature s‐CO2 Environment Restricts Use of Conventional Bearing Technologies and Lubricant Systems
• Compliant Foil Gas Bearings Are an Enabling Technology • Preliminary Testing Shows Korolon Coated 6th Generation Foil Bearings Have Capabilities to Meet Needs for s‐CO2 Systems From kW to 300 MW
• High Temperature Testing to 870°C• High Load Capacity• High Speed with Low Power Loss
• Further Verification and Demonstration of Korolon Coated Foil Bearing Performance and Durability in High Temperature s‐CO2 is Underway
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Acknowledgements
• U. S. Department of Energy under Award No. DE‐SC0015811. • The authors particularly acknowledge the support of Mr. Brian K. Robinson at DOE.
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Thank you!
Backup
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Compressibility of s‐CO2
0.001
0.01
0.1
1
10
10 100 1000 10000 100000
Bearing Num
ber/Co
mpressibility
Ambient Pressure (psia)
Compressibility of Gas
Air_72F CO2_90F CO2_800F CO2_1200F
Threshold P Threshold‐L 7.9 MPa
~15 MPa
Incompressible
Compressible
Supercritical CO2
7.9 MPa
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Λ 6 ⁄ ⁄
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Bearing Requirements/Environment ‐ Scaling
Power Pressure Temperature Weight Speed(MW) (MPa) (°C) (kg) (rpm)1 7.8 ‐ 30 650 ‐ 750 1‐2 120,00010 7.8 ‐ 30 650 ‐ 750 100 50,000100 7.8 ‐ 30 650 ‐ 750 1500 10,000300 7.8 ‐ 30 650 ‐ 750 >5,000 5,400
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MITI Oil‐Free Bearings and Seals
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Thrust Foil Bearing
15‐250 mm
80 psi / 650°C
Foil Face Seal
25‐1300 mm
>80 psid / 650°C
Foil RadialSeal
20‐250 mm
>100 psid / 870°C
6‐150 mm
100 psi / 870°C
Journal FoilBearing
Startup/Shutdown Cycles0 50000 100000 150000 200000
Coe
ffici
ent o
f Fric
tion
0.0
0.1
0.2
0.3
0.4
0.5
Run
ning
Coe
ffici
ent o
f Fric
tion
0.000
0.005
0.010
0.015
0.020
0.025
Korolon Coated Foil Bearing Life Test
38
Friction During Shutdown
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Friction During Operation