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November 3, 2004 04-73007/M-15301.ppt 1 Air, Water and Thermal Management for PEM Fuel Cell Systems Honeywell Engines, Systems & Services Torrance, Ca

Air, Water and Thermal Management for PEM Fuel Cell Systems

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November 3, 200404-73007/M-15301.ppt

1

Air, Water and Thermal Management for PEM Fuel

Cell Systems

Honeywell Engines, Systems & ServicesTorrance, Ca

November 3, 200404-73007/M-15301.ppt

2

AgendaAgenda

• Select PEM Fuel Cell Subsystems• PEM Fuel Cell Air Management• PEM Fuel Cell Thermal and Water Management

November 3, 200404-73007/M-15301.ppt

3

Select PEM Fuel Cell SubsystemsSelect PEM Fuel Cell SubsystemsSelect PEM Fuel Cell Subsystems

Fuel

Cell

Stack

Water Separator & Condenser

PumpR

adiator

Thermal Management

Water Pump

Water

MOTORT CAMBIENTAMBIENT

CONTROLLER 300 VDC

VARIABLEVANE

Water ManagementAir Management

November 3, 200404-73007/M-15301.ppt

4

Fuel Cell Turbocompressor ConceptFuel Cell Turbocompressor ConceptFuel Cell Turbocompressor Concept• Contamination free air flow to fuel cell

• Compliant foil air bearings (no lubricants) • Low production cost potential • Zero Maintenance• Reliable - one moving part• Lightweight/Compact - <15 kg/<15 liters• Efficient

• 75% compressor• 80% expander/turbine

• High temperature capable expander/turbine• Variable geometry turbine maximizes system

efficiency• Maximizes energy recovery and maintains fuel

cell stack pressure• Modular

November 3, 200404-73007/M-15301.ppt

5

Foil Air BearingsFoil Air BearingsFoil Air Bearings• Developed by Honeywell• Over 30 years of proven performance• High-speed efficiency• Compact • No maintenance • Up to 80k hours of

continuous operation • 50k start/stops• Low life-cycle costs

Foil Air Bearing Technology Provides Long Operating Life without Oil Lubrication

Foil Air Bearing Technology Provides Long Operating Life without Oil Lubrication

November 3, 200404-73007/M-15301.ppt

6

Foil Air Bearing Turbomachinery AdvancesFoil Air Bearing Turbomachinery AdvancesFoil Air Bearing Turbomachinery Advances250 K ThrustTurbopump(Launch Vehicle)

Impr

ovin

g-

Mat

eria

ls, M

anuf

actu

ring

Tech

niqu

es, T

oolin

g,O

pera

ting

Tem

pera

ture

, Loa

d C

apac

ityD

ampi

ng, T

est R

igs

DC-10First ProductionProgram With HighReliability Demonstrated

727Successful

Pilot Program

First GeneralAviation Unit

Improved 3-WheelDesign with HigherCapacity Bearings

A-7EFirst MilitaryBootstrap Retrofit

F-18High Efficiency and Reliability Innovative Design Improves Starting

M1A1/A2 Battle Tank NBC

F-16Modified F-18Unit

F-22 VCS

Turbogenerator

Cruise Missile

LH2/LOXTurbopump

1986A310MD-11B757/767

1970’s

First FlightUnit

1965

Honeywell is a Leader in Foil Air Bearing Turbomachinery TechnologyHoneywell is a Leader in Foil Air Bearing Turbomachinery Technology

1980’s

1990’s

2000

November 3, 200404-73007/M-15301.ppt

7

Fuel Cell Turbocompressor HistoryFuel Cell Turbocompressor HistoryFuel Cell Turbocompressor History

2 Bootstrap Turbocompressors (Full and Partial Flow Sizes)

TEPCO 5MWPhosphoric Acid

Fuel Cell Power Plant1981

Demonstration of Motor Driven Turbocompressor w/Mixed Flow Compressor and

Variable Nozzle Turbine DoE 50kW PEM Fuel Cell System

for Light Duty Vehicle2001

Demonstration of Motor Driven Turbocompressor

w/315degC Temperature Capability Turbine in

DoE/Honeywell 50kW PEM Fuel Cell System

2001

Motor Driven Turbocompressor DoE 50kW PEM Fuel Cell System

for Light Duty Vehicle2003

Demonstration of MotorDriven Turbocompressor

DoE 50kW PEM Fuel Cell Systemfor Light Duty Vehicle

1997

Motor Driven Turbocompressor PEM Fuel Cell System for Unmanned Aerial Vehicle2003

Honeywell is a Leader in Foil Air Bearing Turbomachinery for Fuel CellsHoneywell is a Leader in Foil Air Bearing Turbomachinery for Fuel Cells

November 3, 200404-73007/M-15301.ppt

8

DOE Fuel Cell TurbocompressorsDOE Fuel Cell TurbocompressorsDOE Fuel Cell Turbocompressors•Phases 1, 2 and 3 designs; programs complete

•Contamination free, zero maintenance compliant foil air bearings

•Lightweight/Compact - < 15 kg/< 15 liters•Reliable - One moving part•Low production cost potential•Performance

•70% Compressor, 2.5-3.0:1 pressure ratio @ ~85 gr/sec

•80% Variable nozzle expander/turbine, 2.5-3.0:1 pressure ratio @ ~85 gr/sec

•~5kw operation with turbine assist, 3.0 pressure ratio @ ~85gr/sec

•Up to 9kw available @ 2.5:1 pressure ratio and 85gr/sec for fuel cell system transient/startup without turbine assist

Phase 1

Phase 2

Phase 3

Phase 3 Motor Controller

November 3, 200404-73007/M-15301.ppt

9

DOE Fuel Cell TurbocompressorsDOE Fuel Cell TurbocompressorsDOE Fuel Cell Turbocompressors•Phase 4, program to complete 2005

•Enhanced design for 50-80kW systems•Contamination free, zero maintenance compliant foil air bearings

•Lightweight/Compact - 15 kg/15 liters •Reliable - One moving part•Low production cost potential•Estimated Performance

•72% Compressor, 2.5:1 pressure ratio @ ~100gr/sec

•80% Variable nozzle expander/turbine, 2.5:1 pressure ratio @ ~100gr/sec

•~6kw operation with turbine assist, 2.5:1 pressure ratio @ ~100gr/sec

•Up to 15kw available @ 2.5:1 pressure ratio and ~100gr/sec for fuel cell system transient/startup

November 3, 200404-73007/M-15301.ppt

10

Future Turbocompressor DirectionFuture Turbocompressor Direction• By year 2010

• Improve performance•80% efficient compressor•85% efficient turbine

• Continue to investigate manufacturing costs •$400/unit @ 100,000 units/year

November 3, 200404-73007/M-15301.ppt

11

Development of a Thermal and Water Management

(TWM) System for PEM Fuel Cells

November 3, 200404-73007/M-15301.ppt

12

Program ScheduleProgram Schedule• Water and Thermal Management System Concept

Analysis: Nov. 2003 - June 2004– Down-select concept systems from various options– Focused on 50 kW FC Power System– Concept Design Review: June 15, 2004

• Requirement changed to 80 kW from 50 kW

• Water and Thermal Management System Detailed System Analysis: July 2004 - Dec. 2004– Generate component and system specifications

• Water and Thermal Management System Component Hardware Development / Testing: 2005

• Water and Thermal Management System System Integration and Demonstration: 2006

November 3, 200404-73007/M-15301.ppt

13

Concept System AnalysisConcept System Analysis

• Four concepts of cathode humidification are being compared for sizing and performance evaluation– Cathode Recycle - Membrane Humidifier– Adsorbent Wheel - Porous Plate Humidifier

• Current system evaluation priority (Critical To Quality)– Size: 5 (most critical)– Reliability: 4– Cost: 3– Power consumption: 2– Weight : 1

• System and component costs are to be established after detailed system analysis

November 3, 200404-73007/M-15301.ppt

14

Cathode Humidification AlternativesCathode Humidification Alternatives

Goal: Provide cathode inlet humidification using moisture in the cathode exhaust while avoiding bulk condensation.

•• Cathode Recycle SystemCathode Recycle System mixes cathode exhaust gases with mixes cathode exhaust gases with compressed air sent to the cathode inlet to accomplish the goal.compressed air sent to the cathode inlet to accomplish the goal.

•• Porous Plate Humidification SystemPorous Plate Humidification System transfers water through a transfers water through a porous metal plate through capillary action. Condensation and porous metal plate through capillary action. Condensation and evaporation are also concurrently involved in this step.evaporation are also concurrently involved in this step.

•• Membrane Humidification SystemMembrane Humidification System is a vapor to vapor device that is a vapor to vapor device that transfers water vapor across a barrier to accomplish the goal.transfers water vapor across a barrier to accomplish the goal.

•• Adsorbent Wheel SystemAdsorbent Wheel System moves concentrated water vapor from moves concentrated water vapor from cathode exhaust to cathode inlet. cathode exhaust to cathode inlet.

November 3, 200404-73007/M-15301.ppt

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Cathode Recycle System AnalysisCathode Recycle System Analysis

• Need water injection to achieve 60% RH (80 °C) at cathode inlet

• Cathode recycle compressor becomes redundant

PEMFC

AirCE

Recycle Compressor

Water Separator & Condenser

Pump

RadiatorCoolant Loop

Water Pump

Pre-cooler

Water Tank

November 3, 200404-73007/M-15301.ppt

16

Water Injection System SchematicWater Injection System Schematic

• Removed cathode recycle compressor and established a water injection baseline system

– No need for pre-cooler because of cooling from water evaporation latent heat

– Able to hit 50% and 90% RH but with low cathode inlet temperatures

PEMFC

AirCE Water Separator & Condenser

Pump

Radiator

Coolant Loop

Water Pump

Water Tank

November 3, 200404-73007/M-15301.ppt

17

Porous Plate Humidifier SystemPorous Plate Humidifier System

• Material properties tested: permeability and capillary pressure

• System sizing based on analysis of plate model• Water phase change will occur and need sub-ambient

pre-cooling for hot day / high power operations

AirCE

Porous Metal Foam Humidifier

vent

Water Separator

Pump

Radiator

Coolant Loop

Pre-cooler

PEM

FC

November 3, 200404-73007/M-15301.ppt

18

Membrane Humidifier System AnalysisMembrane Humidifier System Analysis• Able to achieve 60% RH (80 °C) with a reasonable

sized humidifier • Need pre-cooler & fan• Need to remove liquid water from cathode exhaust

before entering membrane humidifier– Liquid water inhibits membrane performance– Water trap or evaporative heater could be used

Membrane Humidifier

AirCE

vent

Water Trap

Pump

Radiator

Coolant LoopPre-cooler

PEM

FC

November 3, 200404-73007/M-15301.ppt

19

Adsorbent Wheel SystemAdsorbent Wheel System• Able to achieve 60% RH (80 °C) with a reasonable sized

wheel• Prototype tested with hot dry air at 170 °C and 22 psig

– should work without pre-cooler and fan

• Reliabilities of seals, moving parts, and motor need improvement

Adsorbent Wheel

AirCE

Pump

Radiator

Coolant Loop PEM

FC

November 3, 200404-73007/M-15301.ppt

20

Quality Function DeploymentQuality Function Deployment

Weight factor: Weighted SumBaseline 11.4

Plate 8.7Membrane 12.4

Wheel 12.5

• Two systems (Membrane Humidifier and Adsorbent Wheel) are to be further analyzed at different fuel cell power levels (25% and 10%) at ambient temperatures

November 3, 200404-73007/M-15301.ppt

21

Radiator Trade StudyRadiator Trade Study

• Preliminary radiator thermal performance trade study– Conventional “automotive” design– Conventional “aerospace” design– Advanced microchannel design

• Purpose– evaluate radiator size/weight vs. system power consumption– explore design options

• Thermal performance analysis is per following problem statement Heat rejection rate = 55 kW

Hot flow: Glycol/water (50/50)Flow Rate: 40 gpm

Tin: 167 °F ( 75 °C )∆T: 35 °C

Cold flow: AirT_in_air: 104 °F ( 40 °C )

November 3, 200404-73007/M-15301.ppt

22

Radiator Design and Power ConsumptionRadiator Design and Power ConsumptionHoneywell Automotive Radiator Designs

400

500

600

700

800

900

1000

1100

1200

1300

1400

0.5 1 1.5 2 2.5 3Power Consumption, kW

Vol

ume,

in3

/ Are

a, in

2

0

5

10

15

20

25

Wei

ght (

wet

), lb

AreaVolumeWeight

Coolant loop design and optimization should focus on ~ 1.5 to 2.0 kW power consumption (pump + fan)

November 3, 200404-73007/M-15301.ppt

23

Go Forward PlanGo Forward Plan• For an 80 kW FC system, conduct component design

– Adsorbent Wheel and Membrane Humidifier systems– Steady state loads at 100%, 25%, and 10% of 80 kW– Ambient temperature: 40° C and 20 ° C– Hybrid radiator design: Honeywell automotive + aerospace R&D

• Start test stand design and setup– Establish demonstration test plan and define test requirement– Design test stand and instrumentation

• Development opportunities– Adsorbent Wheel: product development (motor, seals, etc.)– Membrane Humidifier: lower cost / higher temperature resistance material

replacing Nafion

November 3, 200404-73007/M-15301.ppt

24

A Big Thank You!

U.S. Department of EnergyFuel Cell System Developers

For your encouragement and support

November 3, 200404-73007/M-15301.ppt

25

GUS ORDONEZPLATFORM LEADER - DEFENSE AND SPACE

Torrance, CAPhone: 310-512-2556

E-mail: [email protected]

MARK K. GEEFUEL CELL TURBOCOMPRESSORS

Torrance, CAPhone: 310-512-3606

E-mail: [email protected]

CHUNG LIUFUEL CELL THERMAL AND WATER MANAGEMENT

Torrance, CAPhone: 310-512-4328

E-mail: [email protected]