high temperature anode recycle blower for solid oxide fuel cell · 2018-12-11 · doe award...
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Ultra High Temperature Anode Recycle Blower for Solid Oxide Fuel Cell
Department of Energy Award No.
DE-FE0031148
Prepared for DOE Kickoff Meeting
By Mohawk Innovative Technology, Inc.
Principal Investigator: Hooshang Heshmat, PhDDOE Program Manager: Jason T. Lewis, Program Director
DE-FOA-0001735“Solid Oxide Fuel Cell Prototype System Testing and Core Technology Development”
Dec 1 2017
Project Team
MITI• Hooshang Heshmat, PhD
• Principal Investigator
• Jose Luis Cordova, PhD• PM/Thermal Management
• James F. Walton II• Rotordynamics
• Garrett M. Davis• Aerodynamic Design
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Team Background
MITI Specializes in High-Speed, High-Temperature Oil-Free Rotating Machinery Technology
• Blowers
• Compressors
• Turbo-alternators
• Gas-Turbine Engines
• Flywheel Energy Storage
• And more
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MITI’s Completely Oil Free Blower & Compressor Technology
4
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
Fuel Cell Anode Recycle Blower
1.5 kW
80,000 rpm
Water Treatment Aerator
80 kW
60,000 rpm
Mohawk Innovative TechnologyDOE Award DE-FE0031148
MITI’s Compliant Foil Bearings Gen-VCompletely OIL FREE Technology• High Load & High Temperature• Sizes from 6 to 200 mm Diameter• DN to over 6 Million• Speeds greater than 700,000 RPM
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Project Overall Objective• Develop ultra-high
temperature anode recycle blower (UHT-ARCB) prototype that uses uncooled Solid Oxide Fuel Cell (SOFC) anode gas• Demonstrate successful operation of
UHT-ARCB• Demonstrate that design can achieve
TRL5• Determine fabrication methods to
achieve commercial cost of < $110 per SOFC kWe
• Increase Efficiency and Reduce BOP• Recycle anode off-gas• Reduce external water supply used for
fuel reforming• Elimination of heat exchangers• Reduce BOP footprint
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Leverage Precursor 180oC SOFC ARC
• Developed a 180oC Anode Recycle Blower for 100 kWe SOFC• DOE Award No.: DE-FE0027895
• The prototype is currently undergoing performance testing
• Eventual goal of that program is to test in an actual 100 kWe SOFC demonstrator by FuelCell Energy, Inc. (FCE)
• All the know-how obtained, particularly with regard to design for manufacturability and cost for commercialization will be leveraged.
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Advantage of UHT-ARCB vs. 180oC ARCB
• Current plan is to use 180oC ARCB under development.• This requires use of
two heat exchangers (HX) to reduce gas temperature
• This represents around 6 kW of thermal losses
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Advantage of UHT-ARCB vs. 180oC ARCB
• Benefits of using UHT-ARCB• Reduced BOP by elimination of HXs and supporting
piping, insulation.
• Reduced pressure drop
• Reduced thermal losses by ~6kW
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Technical Approach
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Project Structure• Task 1: Project management and planning
• Report Preparation
• Kickoff and Annual Review Meetings
• Task 2: Definition of requirements
• Task 3: Design Proof-of-Concept System• Preliminary design
• Detailed design and analysis
• Task 4: Hardware Fabrication and Assembly• Checkout tests
• Task 5: UHB-RCB Testing• Dynamic and high temperature test data
• Task 6: Final report and assessment of outcomes
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Task 2: Definition of Requirements
• Operating conditions specified with input from FuelCell Energy Inc. • For this program, FCE has
provided specifications and operating regimes at no-cost.
• Three operating regimes to consider • Start Up Transient
• Nominal Operation
• Rated Operation
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Property Nominal Rated Start-Up
Temperature T [oC] 621 650 700
Inlet Pressure P [kPa] 103.9 103.9 103.9
Mass Flow m [kg/s] 0.033 0.036 0.22
Pressure Increase DP [kPa] 7.2 8.7 Unspecified
Operating Regime
Units
Anode Recycle Gas Composition:• Mixture of Water Vapor, Methane, Carbon Dioxide,
Carbon Monoxide, Hydrogen
Task 2: Design Considerations
• Net Power Input < 3 kW• Oil-Free Foil Bearing Design
• No Lubricant Contamination• Low Power Loss Bearings
• Process gas (CH4) for secondary gas path
• Process gas for housing cooling, with option for forced water/glycol loop necessary
• Economical Design• Low Capital Cost• Low Maintenance Cost• Low Operating Cost
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Task 3: Design Process
Oil-Free System Design Elements
• Motor/Power Electronics
• Fluid/Thermodynamic Analysis
• Aerodynamic Design
• Rotor-Dynamic Analysis
• Foil Bearing Design
• Thermal Management
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Task 3: General Layout
180oC Precursor Anode RCB UHT-RCB
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Task 3: Aerodynamic Design Summary
Preliminary Sizing Results
• Type = Centrifugal
• Diameter = 75 mm
• Operating Speed Range• 55 krpm < N < 80 krpm
• Adiabatic Efficiency > 70%
• Material: Rene 41
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Task 3: Aerodynamic Design Performance
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108
110
112
114
116
118
0.02 0.025 0.03 0.035 0.04
Dis
char
ge p
ress
ure
[kP
a]
Mass flow rate [kg/s]
Predicted Discharge Pressure
Nominal
Rated
Start-up
Specs
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MarginFlexible Target
Task 3: Aerodynamic Design Performance
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1
1.5
2
2.5
0.02 0.025 0.03 0.035 0.04
Po
we
r [k
W]
Mass flow rate [kg/s]
UHT Predicted Performance
Mixture
Air (heated)
Air (room temp)
Start-up,80 krpm
Rated, 65 krpm
Nominal, 55 krpm
Mohawk Innovative TechnologyDOE Award DE-FE0031148
Task 3: Aerodynamic Design Performance
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0.3
0.4
0.5
0.6
0.7
0.8
0 0.01 0.02 0.03 0.04 0.05 0.06
Ad
iab
atic
eff
icie
ncy
Mass flow rate [kg/s]
(Mixture) Predicted Adiabatic Efficiency
Nominal, 55 krpm
Rated, 65 krpm
Start-up, 80 krpm
Mohawk Innovative TechnologyDOE Award DE-FE0031148
Task 3: Motor Selection
Permanent Magnet Motor
• Encapsulated Samarium Cobalt
• Permits Larger Air Gap
• Higher Efficiency
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3 kW design based on previous 1.5 kW version
DOE Award DE-FE0031148
Task 3: Preliminary Rotordynamic Analysis
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Mode 1(Rigid Body)
7604 rpm
Mode 2(Rigid Body)
8296 rpm
Mode 3(1st Bend)
173,763 rpm
DOE Award DE-FE0031148
Task 3: Secondary Flow and Cooling Scheme
• A 100 kW fuel cell stack uses 3.14 g/sec of fresh CH4.• Available CH4
Conditions: Ti ~ 20oC, Pi~ 205 kPa
• The CH4 can be used in the secondary flow for thermal management.
• Available CH4 flow can remove up to up to 1.2 kW thermal an maintain motor in a safe temperature zone.
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Task 3: Work in Progress
•Complete Preliminary Layout
•Detailed Design• Rotating Components• Housing• Bearings• Thermal Management
•Manufacturing & Assembly Drawings
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Task 4: Hardware Fabrication and Integration
• Fabricate and Instrument Prototype• Vibration/Displacement Probes
• Thermocouples/Pressure Transducers
• Preliminary and Checkout Tests• Validate Instrumentation
Operation
• Verify Motor/Controller Operation
• Confirm Rotor Lift-Off Speed
• Leak Check
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Task 5: UHT-ARCB Testing
•Demonstrate ability to achieve full design speed
•Measure flow rate and pressure/temperature rise with room temperature air and high temperature (up to 700oC) similitude gas and map performance characteristics
•Compare measured and design performance
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Task 6: Assessment of Outcomes
• Objectives:• Compare results to requirements
• Assess scalability of technology• Explore design scalability up to flows for SOFCs with power output in
the 10 MWe range and higher
• Assess economic performance and compare to cost target of $110 per SOFC generated kWe• Estimated cost for 1 MW load meets or is less than the targeted cost
of $40 per SOFC generated kWe
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Task 6: Cost Considerations and Scalability
Projected Cost After Product Development:
• Estimated Cost for First 10 Units• 3 kW: $12k - $15k / unit• 50 kW: $40k - $60k / unit
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Project Schedule
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Oct Nov Dec Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec Jan Feb MarTask 1: Project Management and
Planning
Task 1.1: Report Preparation
Task 1.2: Meetings and
PresentationsTask 2: Definition of
RequirementsTask 3: Design of Proof of Concept
System
Task 3.1: Preliminary Design
Task 3.3: Detailed Design
Task 4: Hardware Fabrication and
Integration
Task 5: Blower Performance Test
Task 6: Assesment of Outcome
and Plan Forward
2019
TasksQ1 Q2 Q3 Q4 Q5 Q6
20182017
`
Kick-off Meeting
Communication with FCE
Hardware Complete
End of Testing
Final ReportQuartery Prog. Reports
Milestones
Quarterly Reports
Annual Merit
Reveiew
Detailed Design Review
Preliminary Design Review
DOE Award DE-FE0031148
Project Budget
Total Estimated Cost: $ 373,819.00•80% Government Share: $ 299,055.00•20% Recipient Share: $ 74,764.00
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Risk Management
Main Risks Identified (R) and Planned Mitigation Strategies (M):• R: Thermal management: CH4 cooling scheme may be insufficient
• M: Additional closed loop water/glycol (with stock radiator and pump)
• R: Schedule of long lead items: Motor Magnet procurement may cause prototype fabrication delay• M: Handle motor set component procurement as a critical path step.
• M: Secure quotes from multiple vendors
• R: Prototype Fabrication Cost: Initial prototype low-volume cost may be high.• M: Minimize part count
• M: Casting of as many parts as possible
• M: Material substitution where thermally possible
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Technology Readiness Level
• TRL Definitions• TRL 5 - System/subsystem/component validation in relevant
environment:
• TRL 6 - System/subsystem model or prototyping demonstration in a relevant end-to-end environment
• Prototype will be a high TRL 5 at end of Phase I
• Will achieve TRL 6 at end of an eventual Phase II
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Status Summary
• Design Requirement Reviewed
• Preliminary Design and Layout Underway
• Detailed Design to Begin in Feb 2018
• Manufacturing to Begin Apr 2018
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MITI
1037 Watervliet-Shaker Rd
Albany, NY 12205
Thank You For Your Attention!w
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