development status of a rapid-cold-start, on-board, microchannel steam reformer · 2004-06-04 · 2...

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1 6/1/04 DOE Hydrogen, Fuel Cells & Infrastructure Technologies Program 2004 Peer Review Meeting Greg A. Whyatt May 25, 2004 Team Members: Kriston Brooks, Jim Davis, Chris Fischer, Dave King, Larry Pederson, Susie Stenkamp, Ward Tegrotenhuis This presentation does not contain any proprietary or confidential information. Development Status of a Rapid-Cold-Start, On-Board, Microchannel Steam Reformer Development Status of a Development Status of a Rapid-Cold-Start, On-Board, Rapid-Cold-Start, On-Board, Microchannel Microchannel Steam Reformer Steam Reformer

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Page 1: Development Status of a Rapid-Cold-Start, On-Board, Microchannel Steam Reformer · 2004-06-04 · 2 6/1/04 Objectives Utilize microchannel steam reformer and vaporizer to demonstrate

16/1/04

DOE Hydrogen, Fuel Cells & Infrastructure TechnologiesProgram 2004 Peer Review Meeting

Greg A. Whyatt

May 25, 2004

Team Members: Kriston Brooks, Jim Davis, Chris Fischer, Dave King,Larry Pederson, Susie Stenkamp, Ward Tegrotenhuis

This presentation does not contain any proprietary or confidential information.

Development Status of aRapid-Cold-Start, On-Board,

Microchannel Steam Reformer

Development Status of aDevelopment Status of aRapid-Cold-Start, On-Board,Rapid-Cold-Start, On-Board,

MicrochannelMicrochannel Steam Reformer Steam Reformer

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26/1/04

ObjectivesObjectivesObjectives

Utilize microchannel steam reformer and vaporizer todemonstrate rapid cold start of the steam reforming sub-system.

Develop a prototype microchannel-steam-reforming fuelprocessor at ~2 kWe scale that will meet DOE performancetargets when scaled up to 50 kWe.

Develop reactors, vaporizers, recuperative heat exchangers, andcondensers broadly applicable to other fuel processing options.

Engage industrial partner(s) to facilitate application of technologyto full-scale fuel processing systems.

Performance

Criteria

2004 Projected

Performance

2004 Demo

TargetCold (20C) Start Time 12 sec, reformer only <60 s to 90%

Start up Energy <7 MJ (a) 2 MJ

Power Density 2300 W/L (a) 700 W/L

Efficiency 78% 78%

(a) based on individual components only, excludes tube, duct, insulation etc.

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36/1/04

BudgetBudgetBudget

Continuing Project, $119K of Carryover Funding

FY04 Funding Level $700K, allocated:$400K funding for reforming activities (this presentation)

$300K for WGS development (poster session)

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46/1/04

Technical Barriers and TargetsTechnical Barriers and TargetsTechnical Barriers and Targets

Fuel-Flexible Fuel Processor Technical Barriers AddressedI. Fuel Processor Startup/Transient Operation

M. Fuel Processor System Integration and Efficiency

Key DOE Technical Targets Addressed:Cold (20°C) Startup Time

2004 target <60 seconds to 90% traction power

Ultimate target <30 seconds to 90% traction power

Warm Transient Response2004 target <5 sec (10% to 90% or 90% to 10%)

Ultimate target <1 sec (10% to 90% or 90% to 10%)

Start-up Energy2004 target <2 MJ at 50 kWe

Ultimate target <2 MJ at 50 kWe

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56/1/04

Approach to Developing Fast Start AbilityApproach to Developing Fast Start AbilityApproach to Developing Fast Start Ability

Use micro-channel steam reformer and water vaporizer tominimize thermal mass.

Configure reactor and vaporizer as thin panels to minimizecombustion side pressure drop, allowing high combustionflow.

Assemble reforming subsystem test unit and demonstraterapid cold start.

Transition to high temperature reforming to further reducereformer mass, minimizing startup energy.

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66/1/04

Project SafetyProject SafetyProject Safety

Training of staff on laboratory-specific hazards is assuredby limiting access via IOPS (Integrated Operations System)

Test plans reviewed/approved by safety and facility staff.

The microchannel architecture has low internal volume,which minimizes flammable gas inventory.

Steam reforming is endothermic no runaway reactions

A single relay shutdown switch included in all experiments.

Automated shutdown and alarm capability included forunattended operation.

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76/1/04

FY 2000

Designed and built

10 kWe SR with integrated HX network

FY2001

10 kWe reactor testing

First “low dP” vaporizers

Modular test stand established

FY 2002

Modular Test Stand Testing

SR fuel flexibility, durability testing

Full-scale low dP vaporizers delivered

FY 1999

Fast SR kinetics

observed in a

microchannel reactor

Reforming ReactorHT WGS Reactor

LT WGS Reactor

Combustor

Reformate Recuperator

ReformingDevelopment Timeline

ReformingDevelopment Timeline

FY 2003

Investigate high temperature

reforming kinetics and sulfur

tolerance. Fabrication of first

low-dP reforming reactor.

FY 2004

Low-dP Gas-Gas Recuperator

Low-dP reforming and rapid

cold start demonstration.

Recuperator/mixer provided

for ANL 10 kWe ATR.

First low-dP vaporizer prototype

Reforming Test Stand for capacities up to 2 kWe.

Low-dP steam

generator for 50kWe ATR system.

ANL FASTERRecuperator

First Microchannel steam reformer

Low DP TestSystem Micro-channel

Hardware

Low DP Test System

High Temperature Reformer withWGS reactors

10kWe Reforming System

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86/1/04

Changes Made to Achieve Fast StartChanges Made to Achieve Fast StartChanges Made to Achieve Fast Start

Low dP configuration is used on reactor andvaporizer. Allows increased combustion gas flow.

Fuel is directly injected into steam. This eliminates themass and thermal transient associated with the fuel vaporizer.

High temperature air recuperator eliminated.Previously located between the reformer and vaporizer, the recuperatorwas eliminated to prevent the thermal mass from affecting the start-uptransient behavior.

The low-temperature air recuperator has beenenlarged to retain efficiency. The low-temperaturerecuperator does not need to reach operating temperature in order toachieve full reformate production.

Combustion is now non-catalytic and spark ignited.Provides lower pressure drop and faster startup.

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

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96/1/04

Advantages of Low-dP Reformer(compared to previous configuration)

Advantages of Low-Advantages of Low-dPdP Reformer Reformer(compared to previous configuration)(compared to previous configuration)

Low pressure drop (~1” H2O) at steady statereduces parasitic power drain associated with airmovement. During startup, high gas flow does notproduce excessive pressure drop.

Elimination of metal header eliminates lagbetween ignition and heat delivery to reaction channelson combustion side.

Initial heat delivery is uniform across allreaction channels – reduces transient time to achievequality reformate during cold start.

Higher inlet combustion temperaturescan be tolerated without excessive metal temperatures –efficiency and startup energy advantages.

Low-dP Reformer

Previous Configuration

Technical Accomplishments/ProgressTechnical Accomplishments/Progress

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106/1/04

Low-dP Reformer –Tolerance of Higher Inlet Temperatures

Low-Low-dPdP Reformer Reformer ––Tolerance of Higher Inlet TemperaturesTolerance of Higher Inlet Temperatures

By controllingh(rxn)>h(air) metaltemperature can be heldnear reformingtemperature, allowinghigher gas inlettemperature.

Thin panel allowsconduction to reducemetal temperaturegradient, allowing highergas temperatures withoutexcessively high metaltemperatures.

reforming reaction zone

reforming

reaction zone

reforming reaction zone

h(air)

h(rxn)

k(metal)

convective heating

conduction

conduction

hot gas

hot gas

Cross Section of Low-dP Reformer

(reforming flow is into the plane of the diagram)

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

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116/1/04

Initial Fast-Start Test SystemInitial Fast-Start Test SystemInitial Fast-Start Test System

Quencher forstartup exhaust

AirRecuperator

Exhaust

Air Inlet

Startup Air Inlet

Preheated Air Duct

Insulated Gap

Gaseous Fuel

Inlet123456

7

Spark Ignition (not visible)

1 = location of mixer for mixing gaseous fuel into startup air stream2 = location of combustion chamber (inside duct)3 = location of panel reactor (inside duct)4 = microchannel recuperator, heated by steam during startup5 = location of water vaporizer (inside duct)6 = exhaust duct carrying gases exiting the water vaporizer7 = injection point for fuel to be reformed (atomizes liquid into steam)

Recuperator Bypass valve

Vaporizer

Reformer

Air

Recuperator

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126/1/04

Fast Cold Start – Reformate FlowFast Cold Start Fast Cold Start –– ReformateReformate Flow Flow

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

0

2

4

6

8

10

12

14

0 5 10 15 20 25 30 35 40 45 50 55 60

Elapsed Time From Ignition on Combustion Side, Seconds

Start

water/fuel at

t = 3 sec

~Full Reformate flow

at t = 12 sec

Reduce Fuel

Feed at t = 15-16

sec

Ignition at

time=0

Refo

rmate

Flo

w, d

ry S

LP

Mcomposition measured inprevious fast start test

H2 72.3%

CO 6.1%

CO2 19.1%

CH4 0.24%

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136/1/04

Fast Start – Combustion Side TemperatureFast Start Fast Start –– Combustion Side Temperature Combustion Side Temperature

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

Combustion Gas Average Temperatures

(each value is the average of 8 TCs)

0

100

200

300

400

500

600

700

800

900

1000

1100

0 5 10 15 20 25 30 35 40 45 50 55 60

Elapsed Time (sec)

Start

water/fuel at

t = 3 sec

Reformate flow

at t = 12 sec

Reduce Fuel

Feed at t = 15-

16 sec

Tem

pera

ture

, °C

Inlet to Reactor

Reactor Outlet/Inlet to Vaporizer

Vaporizer Outlet

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146/1/04

Fast Start - Reforming Side TemperaturesFast Start - Reforming Side TemperaturesFast Start - Reforming Side Temperatures

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

Tem

pera

ture

, °C

Reforming Reaction Side Temperatures

0

100

200

300

400

500

600

700

800

900

1000

1100

0 5 10 15 20 25 30 35 40 45 50 55 60

Time (sec)

TC-109 (R1 Steam/Fuel In)

TC-110 (Vap_Steam Out)

TC-111 (SR In)

TC-112 (SR Out_Reformate)

TC-113 (R1_Reformate Out)

Start

water/fuel

at t = 3 sec

Superheated

Steam to SR

at t = 20 sec

Reformate

Flow at ~full

rate, t = 12 sec

Reduce Fuel

Feed at t = 15-

16 sec

Steam @ 7 sec,

superheat

@11sec

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156/1/04

Start-up Strategy: Initially high steam rateStart-up Strategy: Initially high steam rateStart-up Strategy: Initially high steam rate

At startup, heat from the refomerexhaust is used to make greater thannormal (6-8X) quantities of steam.

High steam flows heat the reformaterecuperator (and WGS / PROX reactoronce integrated.)

Steam heating minimizes pressure dropon exhaust gas stream (compared tousing exhaust gas directly).

High steam flows provide high S:C ratioat reformer, reducing CO content in thereformate. Low CO reduces demand forWGS activity during startup.

Equilibrium CO concentrations

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

30-sec transient

sample

6.1% CO >650°C

Target Startup

S:C Range

steady-state

4.5% CO

@663°C

mo

l% C

O, D

ry B

asis

650°C

750°C

875°C

0%

2%

4%

6%

8%

10%

12%

14%

16%

18%

20%

0 3 6 9 12 15 18 21 24 27 30S:C Ratio

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166/1/04

Preliminary Estimate of Warm up time forWGS/PROX

PreliminaryPreliminary Estimate of Warm up time for Estimate of Warm up time forWGS/PROXWGS/PROX

Input Values/Assumptions

Heat using heat capacity of high-steam (S:C=24:1) reformate.(neglect heat of reaction in WGS and PROX, heat on air side ofWGS/PROX and condensation in initial operation).

Extrapolate recuperator inlet temps to 875°C reforming temperature.

Heat recuperator with bypass valve open, close when WGS inletreaches 400°C, then control WGS inlet to 400°C.

Simplified heat transfer model for each component.

0

100

200

300

400

500

600

700

800

900

1000

0 20 40 60 80

time, seconds

Te

mp

era

ture

, C

__

Recup in

Recup out

WGS, avg

PROX, avg

Bypass

Closes

WGS SS temp

PROX SS

temp

With WGS/PROX reaction heatsources, system should reachoperating temperature in < 60 s.

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

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176/1/04

Development Path For Startup ApproachDevelopment Path For Startup ApproachDevelopment Path For Startup Approach

Key improvement will be to reduce the air flow requiredduring startup compared to initial prototype.

Transition to high temperature reforming. Reduces thermal mass ofreformer by >3X.

Incorporate improvements in fabrication. Reduces mass of reformer panelby ~40%.

Utilize higher temperature combustion gas. Air flow reduced by up to afactor of 3 at 1500°C.

Continue to deliver sufficient heat to produce high startup steamrate. Limits extent of air flow reduction.

Reductions in air flow will reduce pressure drops and electricalpower demand for blower.

50 kWe Startup Air Flow Target 450 – 600 scfm, withpressure drop of 5 to 10 inches water.

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186/1/04

Thermal Mass Energy Estimates(thermal mass defines lower limit on startup energy)Thermal Mass Energy EstimatesThermal Mass Energy Estimates(thermal mass defines lower limit on startup energy)(thermal mass defines lower limit on startup energy)

50 kWe Projections for Thermal Mass Energy Requirement by Component

MassAvg

Operating

Temp

Duty

Required to

heat from

ambient

Device [kg] [oC] [MJ]

Inconel 600 Steam Reformer (low-dP) (a) 5.5 875 2.09

Water Vaporizer (low dP) (b) 7.4 300 1.04

Air-Air Preheater (low dP) (b) 24.7 100 0.97

Reformate Recuperator (c) 1.8 554 0.48

WGS (differential) (d) 9.0 343 1.50

PROX (c) 6.6 200 0.90

Total 6.97

(c ) estimated based on preliminary design

(a) projected based on current low dP design, temperature dependence demonstrated in earlier

reactor design and demonstrated ability to reduce reduced bonding edge metal.

(b) linear extrapolation of 2 kWe prototype weight by power level. Actual weight may be less

when scaled up to 50 kWe.

(d) based on linear scaling of core design for 2 kWe prototype to 50 kWe plus header and edge

metal contributions

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

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196/1/04

Mileage Penalty Due to Start-up EnergyMileage Penalty Due to Start-up EnergyMileage Penalty Due to Start-up Energy

Target of 2 MJ, minimizes effect on fuel mileage.

Insulating high temperature components so that only thefirst start each day is “cold” reduces impact.

(a) Reference: Magbuhat, S., J. R. Long, California Air Resources Board, El Monte CA 91731: Improving California’s Motor Vehicle EmissionsInventory Activity Estimates Through the Use of Data Logger-Equipped Vehicles. Presented at the 6th On-Road Vehicle Emissions Workshop,San Diego, CA, March 18-20, 1996.

Technical Accomplishments/Progress:Technical Accomplishments/Progress:

CARB Real-World Study(a)

46 miles/day,

assumption: one cold start/day

0

20

40

60

80

100

120

0 5 10 15 20 25 30 35 40 45 50

Start-up Energy, MJ

100 mpg warm80 mpg warm60 mpg warm

Ac

tua

l M

ile

ag

e (

mp

g)

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206/1/04

Warm Transient ResponseWarm Transient ResponseWarm Transient Response

Very short residencetime within reformerenables rapidtransient response.

Direct liquid fuelinjection reducestransient responsecompared toseparate fuelvaporizer. (~2second downwardtransientdemonstrated).

Transient with Direct Fuel Injection Into Steam

Technical Accomplishments/ProgressTechnical Accomplishments/Progress

0

1

2

3

4

5

6

7

-10 0 10 20 30

Time, sec

Refo

rmate

Flo

w, slp

m_

Fuel Shut Off to

Reformer at time = 0

Reformate Flow Drops

In ~2 Seconds

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216/1/04

Previously DemonstratedReformer Productivity vs Temperature

(All fuels at 3:1 S:C, CH4 conv. is % approach to equil., Inconel 625 reformer)

Previously DemonstratedPreviously DemonstratedReformer Productivity Reformer Productivity vsvs Temperature Temperature

(All fuels at 3:1 S:C, CH(All fuels at 3:1 S:C, CH44 convconv. is % approach to equil., . is % approach to equil., InconelInconel 625 reformer) 625 reformer)

0

200

400

600

800

1000

1200

1400

1600

1800

2000

600 650 700 750 800 850 900 950

Reformate Temperature [oC]

Es

tim

ate

d P

ow

er

Ou

tpu

t [W

e]

Methane, 96.37%- 98.66% Conv.

Isooctane, 99.73%-99.80% Conv.

Benchmark, 99.78%-99.92% Conv.

Benchmark, >99.995% Conv.

A 50 kWe reactor core

would be ~2.1 L at 100%

Conversion, Benchmark

Stability of catalyst productivity verified by measuring the conversion at areference condition before and after generation of the data for each curve.

Inconel 625High-TemperatureReformer

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226/1/04

Extrapolation of Recent Single ChannelPropane Reforming Test Results

(3:1S:C, capacity evaluated at 99.7 to 99.8% conversion)

Extrapolation of Recent Single ChannelExtrapolation of Recent Single ChannelPropane Reforming Test ResultsPropane Reforming Test Results

(3:1S:C, capacity evaluated at 99.7 to 99.8% conversion)(3:1S:C, capacity evaluated at 99.7 to 99.8% conversion)

0

1000

2000

3000

4000

5000

6000

600 650 700 750 800 850 900 950

Reformate Temperature [oC]

Es

tim

ate

d P

ow

er

Ou

tpu

t [W

e]

Methane, 96.37%- 98.66% Conv.

Isooctane, 99.73%-99.80% Conv.

Benchmark, 99.78%-99.92% Conv.

Benchmark, 100% Conv.

propane single channel

Potential Gain If Recent Single Channel Result

Were Scaled to High Temp Reactor

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236/1/04

Removal of H2S from ReformateRemoval of HRemoval of H22S from S from ReformateReformate

The presence of H2O and CO in the reformate stream make it difficult toachieve sub-ppm H2S levels at WGS inlet conditions using ZnO.

There is no advantage in using a differential temperature approach whenremoving H2S with ZnO ahead of WGS reactor.

Preferred approach with ZnO is to substantially cool the reformate, removesulfur at minimum temperature, then reheat.

CuY Zeolite can reduce sulfur levels from 25ppm to <150 ppb at ambienttemperature. Material is not suitable at WGS temperature.

Testing performed on sulfur removal from simulatedreformate stream using ZnO and CuY Zeolite.Conclusions from testing include:

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246/1/04

Comparison to DOE Performance TargetsComparison to DOE Performance TargetsComparison to DOE Performance Targets

Attribute Units 2004 Status 2004 Demo Criteria Ultimate Target

Transient sec~2, 100% to 10%

~5, 10% to 90%

<5, 10% to 90% and

90% to 10%

<1, 10% to 90% and

90% to 10%

Start-up Time

(+20°C)sec

12 sec at reformer ,

estimate <60 sec for full

fuel processor

<60 to 90% traction

power

<2 to 10%,

<30 to 90%

Start-up MJ/50kWe >7.0 (a) <2 <2

Efficiency % 78 (b) 78 >80

Power density W/L 2307 (c) 700 2,000

Durability hours 1000+2000h and >50

stop/starts

5,000h and 20,000

startsSulfur

Toleranceppb (d)

<50 out from 30 ppm

in

<10 out from 30

ppm inTurndown ratio >10:1 20:1 >50:1(a) value is based on thermal mass of individual components and represents a minimum value.

(c) based on individual components. Specific power estimated to be 909 We/kg on same basis. Does not include connecting duct and tubing

instrumentation and insulation.

(b) calculated based on 0.95*(LHV H2 out)/(LHV combustion fuel feed +LHV reforming fuel feed) The derating factor of 0.95 is considered very

conservative for low dP system.

(d) Ability to provide <150 ppb reformate from 25 ppm reformate demonstrated at ambient. Issues remain with operation on 30 ppm fuel in

reformer and removal ahead of WGS reactor.

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256/1/04

Delivered Microchannel Recuperator forANL FASTER ATR Reformer

Delivered Delivered MicrochannelMicrochannel RecuperatorRecuperator for forANL FASTER ATR ReformerANL FASTER ATR Reformer

Preheats air and steam while coolingreformate to WGS temperature

Includes a mixer to uniformly mix air into thereformate during startup to assist in heatingWGS catalyst.

Micro-Channel Recuperator

Effectiveness = 0.85

duty=3.6 kW

Pressure Drop:

side 1 dP + side 2 dP <0.4 psi

Reformate from ATR

4.9 g/s

775°C

Composition (mole fraction):

0.318 H2

0.097 CO

0.087 CO2

0.259 N 2

0.239 H 2O

Incoming Air and Steam

4.2 g/s

92°C

Composition (mole fraction):

0.469 Air

0.531 Steam

(fully vaporized)

Air and Steam to ATR

675°C

Reformate to Mixer

376°C

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266/1/04

Interactions and CollaborationsInteractions and CollaborationsInteractions and Collaborations

Delivered Recuperator/Mixer for 10 kWe FASTER autothermal reformerbeing developed at ANL.

Providing micro-channel low-dP vaporizer to support testing ofCatalytica 3 kWe steam reforming system.

Working with the Gas Technology Institute and Cleaver Brooks todemonstrate HX technology in boiler economizer application.

Micro-technology Intellectual property licensed to Velocys for specificfields of use, recent velocys activities

Velocys and ConocoPhillips, the largest U.S. refiner, have formed a joint venture todevelop and commercialize a low-cost, modular hydrogen production process basedon microtechnology.

The U.S. Department of Energy has selected the team of Velocys, Dow ChemicalCompany and Pacific Northwest National Laboratory to apply microchannel processtechnology to the production of ethylene and other olefins.

PNNL has collaborated with Oregon State Univeristy to form the Micro-Products Breakthrough Institute

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Reviewer Comments from FY2003Reviewer Comments from FY2003Reviewer Comments from FY2003

“Why stop at 2 kWe? The goal should be to design for 50kWe system.”Response: Testing at smaller scale reduces cost associated with

component development. Due to the nature of the microchannelapproach, scaling is straight forward. A full scale water vaporizerwas delivered to McDermott for inclusion in their demonstration.

“Weight reduction issues by applying material other thanstainless steel should be addressed”Response: Currently pursuing high temperature Inconel reforming

approach. This is expected to reduce reformer mass by ~4X. Alsoimprovements in fabrication technique have eliminated unnecessarymetal and reduced total reformer metal by ~40%. Additional workusing light weight metals such as aluminum and titanium will bepursued as needed to support fuel processor development.

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286/1/04

Future WorkFuture WorkFuture Work

Assemble Inconel low-dP reforming reactor systemDemonstrate fast cold start and steady operation at 900°C

Demonstrate ability to utilize very high temp combustion gas

Demonstrate reduction in fast start fuel consumption

Integrate with WGS reactor at 2 kWe scaleDemonstrate rapid start with reformer/WGS including ability torapidly steam heat the WGS reactor

Evaluate the startup time, energy, and CO content vs time for thissystem.