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U N C L A S S I F I E D Chemical Hydrogen Rate Modeling, Validation, and System Demonstration DOE Fuel Cell Technologies Program Annual Merit Review, EERE: Hydrogen, Fuel Cells and Infrastructure Technologies Program Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken, Biswajit Paik, and Jose I. Tafoya, Project ID: st007_semelsberger_2013_O This presentation does not contain any proprietary, confidential, or otherwise restricted information

Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

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Page 1: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Chemical Hydrogen Rate Modeling, Validation, and System Demonstration

DOE Fuel Cell Technologies Program Annual Merit Review, EERE: Hydrogen, Fuel Cells and Infrastructure Technologies Program

Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson

LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken, Biswajit Paik, and Jose I. Tafoya,

Project ID: st007_semelsberger_2013_O

This presentation does not contain any proprietary, confidential, or otherwise restricted information

Page 2: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

LANL Project Overview

Timeline • Project Start Date: Feb FY09 • Project End Date: FY14 • Percent Complete: 65%

2

Budget •Total Project Funding: $4.7M

•DOE Share: $4.7M • Funding:

•2012: $900K •2013: $880K

Barriers • Barriers Addressed

A. System Weight and Volume B. System Cost C. Efficiency D. Durability/Operability E. Charging/Discharging Rates F. Codes and Standards G. Materials of Construction H. Balance of Plant Components J. Thermal Management K. System Life-Cycle Assessments S. By-Product/Spent Material Removal

Project Timeline Phase 1 Phase 2 Phase 3

2009 2010 2011 2011 2012 2013 2014 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2

Page 3: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Relevance

• Provide a validated modeling framework to the Energy Research Community (e.g., H2A)

• Provide an internally consistent operating envelop for materials comparison wrt • System/Component mass, volume, and cost • System performance

• Provide component scaling as a function of chemical hydrogen storage media

and application

• Provide materials operating envelop required to meet DOE 2017 targets

• Identify and advance engineering solutions to address material-based non-idealities

• Identify, advance, and validate primary system level components

3

Page 4: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 4

System Architect Section

Page 5: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Overall HSECoE Objectives

5

1. Validate chemical hydrogen storage system model

2. Determine viable chemical hydrogen storage material properties

3. Develop and demonstrate “advanced” (non-prototypical) engineering concepts

Page 6: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

HSECoE Phase 1-3 Objectives

6

Phase 1: • Identify Essential System Components • Develop Preliminary System Designs & Model Framework

Phase 2: • Validate System Components • Refine System Models and System Designs

Phase 3: • Validate Integrated System Components • Validate and Refine System Level Models and System Design

Page 7: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Ammonia Borane System Designs

7

Exothermic Model 50 wt. % Slurry-Phase AB

Feed Pump (P-1)

Borazine/Ammonia

Filter (FT-2)

Fuel Cell

Reactor (RX-1)

Volume Displacement Tank (TNK-1)

Phase Separator Ballast Tank

(PS-1)

Fill Station Fill & Drain

Ports

STR-1

P

PS

T

P

Rupture Disk@ 2 bar(INS-01)

L

Ammonia Filter (FT-3)

Flapper Doors

STR-2

1" P

last

ic

1" P

last

ic

½” SS ½” SS

½” SS

Reactor Heater (H-1)

½” S

S

PRV @ 5 bar(V-4)

INS-08

INS-07

PRV @ 30 bar(V-2)

T

INS-06

INS-04

V-5

INS-09

INS-10

V-3

INS-11

½” SS

½” S

S

3/8" SS

3/8" SS

½” SS

Recycle Pump (P-2)

T

INS-05

Rupture Disk@ 2 bar (INS-03)

L

INS-02

1" Plastic

Feed Pump Motor (M-1)

Reactor Stirrer Motor (M-3)(Optional)

Recycle Pump Motor (M-2)

FinnedDrain Vessel

(TNK-2)

CoalescingFilter (FT-1)

Gas Radiator(RD-2) Pusher Fan

Motor (M-4)

Pusher Fan Motor (M-5)

Liquid Radiator(RD-2)

Particulate Filter (FT-4)

T

V-1

MM

SS

C

3/8"

SS

½” SS

½” SS

C

CC

C

M

S

P

T

Operator Interface

Valve Controller

Safety Feature

Pressure Transducer

Temperature Sensor

Rupture Disk

Pressure Relief Valve

Control Valve

Pressure Control Valve

Multiport Valve

Control Logic Line

Fresh Feed Line

Spent Slurry Line

Hydrogen Product

Legend

Ballast Tank (5L)

Borazine/Ammonia/Particulate Filter +

Ballast (FT-2)

Fuel Cell

Reactor (RX-1)

Volume Displacement Tank (TNK-1)

Phase Separator Ballast Tank

(PS-1)

Fill Station Fill & Drain

Ports

P

S

PS

T

P

Rupture Disk@ 2 bar(INS-01)

L

Flapper Doors

1" P

last

ic

1" P

last

ic

½” SS

Reactor Heater (H-1)

½” S

S

PRV @ 5 bar(V-4)

INS-08

INS-07

PRV @ 30 bar(V-2)

T

INS-06

INS-04

V-5

INS-09

INS-10

V-3

INS-11

½” SS

½” S

S

3/8" Al

3/8" Al

T

INS-05

Rupture Disk@ 2 bar (INS-03)

L

INS-02

1" Plastic

Pusher Fan Motor (M-5)

Gas & Liquid Radiators(RD-1/2)

T

V-1

MM

S

C

3/8"

Al

½” SS

½” SS

C

C

M

S

P

T

Operator Interface

Valve Controller

Safety Feature

Pressure Transducer

Temperature Sensor

Rupture Disk

Pressure Relief Valve

Control Valve

Pressure Control Valve

Multiport Valve

Control Logic Line

Fresh Feed Line

Spent Slurry Line

Hydrogen Product

Legend

Recirculation Pump (P-3) Recirc Pump

Motor (M-2)

Feed Pump (P-1) Recycle Pump (P-2)Pump/ReactorMotor (M-1)

End of Phase 1

Current

Projected

Primary Unit Operations • Volume Displacement Tank • Reactor • Gas-Liquid Separator • Ballast Tank • Heat Exchangers • H2 Purification • Recycle Loop

Page 8: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 8

Exothermic Model

FOCUS AREAS

System Mass System Volume

Projected

Current

End of Phase 1

50 wt. % Fluid-Phase Ammonia Borane

50 wt.% Ammonia Borane Spider Charts

Page 9: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Projected Improvements for Ammonia Borane Slurry System

9

Phase

1: 50

wt.%

AB

Phase

2: 50

wt.%

AB

Projec

ted: 5

0 wt.%

AB

Projec

ted: 6

0 wt.%

AB

Projec

ted: 7

0 wt.%

AB

40

50

60

70

80

90

100

110

120

130

Gravimetric Volumetric

Material ImprovementsEngineering Improvements

Per

cent

age

of D

OE

201

7 V

olum

etric

or G

ravi

met

ric T

arge

ts

Phase 1 to Phase 2 (Current)

• Phase 2 Component Validation Results

• Higher fidelity System Models and System Designs

Phase 2 (Current) to Projected

• Component Integration

• Component Performance Enhancements

Engineering Improvements

Material Improvements 60 wt.% AB slurry (~ 8.7 wt. % H2) will meet both the DOE 2017 gravimetric and volumetric targets

Page 10: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Alane Slurry System Designs

10

Endothermic Model 50 wt. % Alane Slurry

Feed Pump

Radiator

Fuel Cell

Reactor/PreheaterLiquid Flow Thru Reactor

Radiator

H2 Flow Thru Reactor

Recuperator

H2 Clean-Up System

Displacement Tank

Fill Station Feed Line

Fill Station Product Line Vibrator Rupture

Disk/TRD

Phase Separator/

Ballast Tank

Rupture Disk/TRD

P T

P T

P P P

T

P

T

L

End of Phase 1

Current

Projected

Notable Differences • Recycle Loop replaced with Recuperator • Eliminated one Heat Exchanger/Radiator • Reduced H2 Purification

Page 11: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 11

50 wt. % Alane Spider Charts

Endothermic Model

FOCUS AREAS

System Mass System Volume

Projected

Current

End of Phase 1

Page 12: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Projected Improvements for Alane Slurry System

12

Phase

1: 50

wt.%

Alan

e

Phase

2: 50

wt.%

Alan

e

Projec

ted: 5

0 wt.%

Alan

e

Projec

ted: 6

0 wt.%

Alan

e

Projec

ted: 7

0 wt.%

Alan

e

40

50

60

70

80

90

100

110

120

130 Volumetric Gravimetric

Per

cent

age

of D

OE

201

7 V

olum

etric

or G

ravi

met

ric T

arge

ts

Material ImprovementsEngineering Improvements

Phase 1 to Phase 2 (Current)

• Phase 2 Component Validation Results

• Reduction of H2 Purification and Heat Exchangers

• Higher fidelity System Models and System Designs

Phase 2 (Current) to Projected

• Similar approaches as those taken for the AB system

Engineering Improvements

Material Improvements Alane slurry loadings greater than 70 wt.% (~ 8.4 wt.% H2) are expected to meet the DOE 2017 mass and volumetric targets

Page 13: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

System Architect Accomplishments/Highlights

Chemical Hydrogen Storage System Architect & Fluid-Phase System Designer

Developed and assessed endothermic and exothermic system designs and models

Identified material operating limitations for the on-board production of hydrogen

Performed component validation tests (e.g., GLS, VDT, H2 purification, reactors, etc.,)

Refined system level models and designs from Phase 2 component validation efforts

Identified system engineering improvements for system mass, system volume,

system cost, component manufacturability, system complexity, and system performance

13

Page 14: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 14

LANL Technical Section 1. Reactors and Reaction Characteristics

• LANL Objectives and Relevance • Accomplishments

2. Hydrogen Purification • LANL Objectives and Relevance • Accomplishments

Page 15: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 15

• Data Collected

• Temperature • Gas phase analyses (impurities and hydrogen) • Reactor performance (conversions, selectivities,etc.,) • Material performance and limitations

• Materials Tested • Slurry AB (exothermic) • Slurry Alane (endothermic) • Liquid MPAB (exothermic)

• Reactors Tested

• Auger (slurry alane and slurry AB) • Helical reactors (MPAB) • Packed-bed (MPAB)

1. To demonstrate the reactive transport of slurry-phase chemical hydrogen storage materials

2. To collect the highest quality kinetics data for model validation

Model Validity

Model Breadth

System Performance

Objectives: Reactor Design and Reaction Characteristics

Page 16: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Approaches

16

Three different reactors were examined with liquid phase MPAB In-house built auger reactor was examined with slurry phase ALANE and AB

Slurry Phase Reactor

Liquid Phase Reactors Technical Limitation: Reactant slugging Our Method: Design reactors that prevent or minimize reactant slugging 2013 Goals: Design, build and test helical and packed-bed reactors with liquid-phase MPAB coupled with gas-phase analyses

Technical Limitation: Reactor fouling and reactant slugging Our Method: Design reactors that prevent or minimize reactant slugging and mitigate reactor fouling 2013 Goals: Design, build and test auger reactor for slurry-phase alane and slurry phase AB coupled with gas-phase analyses

Prevent reactant slugging & mitigate reactor fouling

Prevent reactant slugging O B PB

Page 17: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 17

Methoxypropyl Amine Borane (MPAB) (exothermic liquid)

H2N BH3O

HB

NBH

N

BHN

O

O

O

+ 2H2 +

Page 18: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 18

MPAB Accomplishments

MPAB Reactor Tests Composition:

• Neat methoxy propyl amine borane: 3.9 wt. % H2

Reactors Tested: • Helical reactors • packed-bed reactor

• Downward flow • Liquid flow rates = 0.5-1.5 mL/min • Reactor Set-point Temperatures = 50-225 °C

Operating Conditions

Liquid Exothermic Material

Prepared by Ben L. Davis and Brian D. Rekken

O B PB

Page 19: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 19

MPAB Accomplishments

60 80 100 120 140 160 180 200 220 2400

10

20

30

40

50

60

70

80

90

100

Con

vers

ion

(H2 b

ased

)

T (oC)

τliquid = 7.0 min (Rev B) τliquid = 12.5 min (Rev B) τliquid = 20.4 min (Rev B)

Liquid Exothermic Material

1. Successful demonstration of MPAB dehydrogenation as a function of reactor type, space-times and temperatures

2. Full conversion of MPAB was not observed over the temperatures, space-times, or reactors investigated

3. Borazine, and ammonia were below detectable limits (100 ppm) and only trace amounts of diborane (~200 ppm)

4. MPAB conversion was limited to less than 66% because of the increased partial pressure of MPAB for temperatures greater than 180 °C

Key Results

Re 66% v BMPAB max

X ≈

Reactant Slugging

Reactor Fouling

Trace Impurities

Research findings provided to materials researcher Ben L. Davis

Page 20: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 20

Slurry ALANE (endothermic slurry)

( ) ( )3 2 slurry slurry

AlH Al 1.5H∆→ +

3 rxnkJH +11

mol AlH∆ ≈

2.% .%wt H 10 wt≈

Page 21: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 21

Slurry ALANE Accomplishments Alane Slurry Composition:

• 20 wt. % Alane (ATK): 2.00 wt. % H2 • As-received ATK Alane • AR 200 Silicon Oil (200 cP) • TritonTM X-15 (0.025 g X-15/g Alane)

Reactor Volume Heated

Reactor Length

(mL) (cm)

Auger-1 7.4 19.1

Typical Operating Conditions

• Auger Speed: 40 rpm • Horizontal Flow • Reactor Temp: 125-275 °C • Feed Flow Rates: 0.55-1.09 mL/min

Auger Slurry Reactor

Stirred Settled

Prepared by T.A. Semelsberger

Note: alane slurry composition was ”uncatalyzed”

Page 22: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 22

Slurry ALANE Accomplishments

100 120 140 160 180 200 220 240 260 280

0

20

40

60

80

100

120

Ala

ne C

onve

rsio

n (%

)

Temp (C)

τliquid = 6.8 min τliquid = 13.5 min

1. Successful demonstration of slurry ALANE dehydrogenation as a function of space-time and temperature with auger reactor

2. Full conversion of ALANE can be achieved

3. Ti doped ALANE and/or ALANE activation will be required to lower the dehydrogenation temperature

4. Decomposition of silicon oil was observed for reactor set point temperatures greater than 225 °C and is the determinant factor for observed alane conversions greater than 1

Key Results

100%@ 270augerAlane avgmax

X T C≈ ≈

Reactant Slugging

Reactor Fouling Impurities

Page 23: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 23

Slurry ALANE Accomplishments

6( ) , 3.7 10 , 90.75aE

RTa

kJk T Ae A x Emol

− = = =

0.5( )Alane alaneapparentr k T C− =

100 125 150 175 200 225 250

0

50

100

150

200

250

Mod

el P

redi

cted

H2 F

low

(scc

m)

Avg Reactor Temp (C)

Model Predicted H2 Flow Observed H2 Flow

0.0 0.2 0.4 0.6 0.8 1.00.0

0.2

0.4

0.6

0.8

1.0

Mod

el P

redi

cted

Ala

ne C

onve

rsio

n

Observed Alane Conversion

√ Model predictions agree with experiment

Note: rate expression regressed with apparent kinetics for as-received alane collected with auger reactor

Rate expression provided to System Modeler, Kriston Brooks

Page 24: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 24

Slurry AB (exothermic slurry)

3 3 x y z 2 3 3 6 2 6NH BH B N H +2.35H + NH3+ B N H + B H∆→

rxnkJH -49

mol AB∆ ≈ 2.% 15.2 .%

ABwt H wt≈

Page 25: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 25

Slurry AB Accomplishments AB Slurry Composition:

• 20 wt. % AB: 3.05 wt. % H2 • AR 20 Silicon Oil (20 cP) • TritonTM X-15 (0.025 g X-15/g AB)

Reactor Volume Heated

Reactor Length

(mL) (cm)

Auger-1 7.4 19.1

Typical Operating Conditions

• Auger Speed: 40 rpm • Horizontal Flow • Reactor Temp: 125-275 °C • Feed Flow Rates: 0.55-1.09 mL/min

Auger Slurry Reactor

Prepared by Ewa Rӧnnebro

Stirred Flocculated

Page 26: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

1. Successful demonstration of slurry AB dehydrogenation as a function of space-time and temperature with auger reactor

2. Full conversion of MPAB can be achieved but was not observed over the temperatures and space-times investigated

3. Maximum impurities observed during operation

26

Slurry AB Accomplishments

86%@ 212augerAB avgmax

X T C≈ ≈

( )3

145

max3.0%%

T

NHn

n

= ≈

( )168

max2.8%%

T

borazinen

n=

( )168

max1.0%%

T

diboranen

n=

Reactant Slugging

Reactor Fouling Impurities

Key Results

Auger reactor performed equally well for both ENDOTHERMIC and EXOTHERMIC media types

Page 27: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 27

LANL Technical Section 2. Hydrogen Purification

• LANL Objectives and Relevance • Accomplishments

Page 28: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Borazine Adsorption Approaches

28

> 15 different adsorbents were screened for borazine adsorption capacity

Technical Limitation: Borazine and ammonia are known fuel cell impurities generated from ammonia borane

Our Methods: 1. Develop and screen for potential borazine adsorbents 2. Implement ammonia adsorbent (UTRC) with down-selected

borazine adsorbent (LANL) to demonstrate hydrogen purification

2013 Goals: 1. Down select borazine adsorbent with the highest borazine

adsorption capacity 2. Demonstrate ammonia and borazine that is co-fed can be

scrubbed to produce fuel-cell grade hydrogen

Adsorbents

Static Adsorption

Dynamic Adsorption

(Downselect adsorbents)

• Pre-treatment • Temperature • Chemical Modification • Concentration

Page 29: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 29

ACN-210-15 Down Selected ACN-210-15

Borazine Adsorption Accomplishments

Key Results 1. ACN-210-15 demonstrated the highest borazine

adsorption capacity around 40% (Pamb) & 80% (P = 5 bar)

ACN-210-15> AX-21> Y-zeolite > ZSM-5 > Oxides

Note: Chemically modified substrates did not show marked improvements over the as-received analogs

2. ACN-210-15 is an off-the-shelf carbon adsorbent

requiring no special pretreatments or handling

3. ACN-210-15 is a woven felt that is ideally suited for vibration prone environments because ACN-210-15 is not friable

4. Adsorption capacity decreases with increasing temperature

Page 30: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

1. Borazine has a higher chemical affinity toward MnCl2 than ammonia has toward ACN-210-15

• Ammonia adsorption capacity in ACN-210-15 ~ 1%

• Borazine adsorption capacity in MnCl2 ~ 6%

2. Adsorbent bed configuration is important

30

Ammonia and Borazine Adsorption Accomplishments

Ammonia and borazine can be scrubbed to produce fuel-cell grade hydrogen

Borazine should be scrubbed prior to Ammonia

Key Results

We have identified potential scrubbing technologies that can reduce the current requirement of 6.8 kg of ACN-210-15

Ammonia Adsorbent

Page 31: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 31

Summary: 2013 Accomplishments • Successfully demonstrated flow reactor tests with quantification on slurry ALANE, slurry

AMMONIA BORANE, and liquid MPAB

• Full conversion of “uncatalyzed” ALANE can be achieved for temperatures greater than 270

C

• Improvements in ALANE dehydrogenation kinetics were observed with the use of dopants and solvents (reviewer only slides)

• No impurities were detected during ALANE dehydrogenation

• Trace amounts of diborane were detected during MPAB dehydrogenation

• AMMONIA BORANE produced borazine, diborane, and ammonia impurities

• Reactant slugging and reactor fouling were mitigated through our in-house designed and built reactors

• In-house built auger reactor performed equally well for both slurry ALANE and slurry AMMONIA BORANE compositions

• ACN-210-15 demonstrated the highest borazine adsorption capacity

• Demonstrated that ammonia and borazine can be scrubbed to produce fuel-cell grade hydrogen

Page 32: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 32

LANL Future Work

1. Slurry AB Compositions (exothermic)

• Perform kinetics/reactor tests with increased AB loadings (30-50 wt. %); develop rate expression

2. Slurry Alane Compositions (endothermic)

• Perform kinetics/reactor tests with increased alane loadings (40- 60 wt.%); develop rate expression

• Extend alane kinetics/reactor tests to include different solvents (e.g., DEGB) and dopants (e.g., Ti)

3. Liquid MPAB (exothermic)

• Redesign reactor to address material limitation

4. Borazine Scrubbing • Examine non-adsorbent based borazine scrubbing technologies

Page 33: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Collaborations

33

External Collaborators Effort Contact H2 Codes and Standards General Guidance C. Padro (LANL)

Chemical Hydrogen Storage Researchers Materials Research J. Wegrzyn (BNL) T. Baker (U. Ottawa) B. Davis (LANL)

H2 Production & Delivery Tech Team WTT Analyses M. Pastor (DOE) B. James

LANL Fuel Cell Team General Guidance Fuel Cell Impurities

T. Rockward (LANL)

R. Borup (LANL)

H2 Safety Panel General Guidance/Concerns S. Weiner

SSAWG Technical Collaboration G. Ordaz (DOE)

H2 Storage Tech Team General Guidance Ned Stetson (DOE)

Argonne National Laboratory Independent Analyses R. Ahluwalia

HSECoE Collaborators Effort Contact

UTRC

Ammonia Scrubbing B. van Hassel Simulink® Modeling J. Miguel Pasini

Gas-Liquid Separator Randy McGee

PNNL MOR E. Ronnebro System Modeling K. Brooks BOP K. Simmons

NREL Vehicle Modeling M. Thornton

SRNL Slurry Mixing David Tamburello

Ford FMEA Mike Veenstra

Page 34: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Acknowledgements

Ned Stetson and Jessie Adams

34

Page 35: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Backup Slides

35

Page 36: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

HSECoE Partners

36

Page 37: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Supporting Information

42

Page 38: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

SMART Milestones Chemical Hydrogen Storage Team

Component Lead S*M*A*R*T Milestone Status 20 Mar 2013 Projected Outcome

Materials Development LANL

Report on ability to develop a 40wt% liquid AB material (6.4wt%H2) having viscosity less than 1500cP pre- and post-dehydrogenation and kinetics comparable to the neat.

Developed a 3.9 wt.% H2 liquid phase chemical hydrogen storage media that is liquid both pre- and post-reaction with kinetics similar to that of solid AB, preliminary impurities profile looks promising because of the significantly reduced or eliminated impurities production, viscosities all well below 1500cP

Investigations will continue into new solvent chemistries which are anticipated to meet the metric while minimizing fuel-cell impurities

Materials Development PNNL

Report on ability to develop a 40wt. % slurry AB material having viscosity less than 1500cP pre- and post-dehydrogenation and kinetics comparable to the neat.

45wt% AB achieved before reaction 617cP, Yield stress 48 Pa after dehydrogenation 442cP, yield stress 3.7Pa Met Target

Reactor LANL

Report on ability to develop a flow through reactor capable of discharging 0.8 g/s H2 from a 40 wt.% AB fluid-phase composition having a mass of no more than 2 kg and a volume of no more than 1 liter.

Reactor performance and Kinetics collected for • Liquid exothermic material (3.9 wt.% H2-MPAB) • Slurry exothermic material (20 wt.% AB slurry) • Slurry endothermic material (20 wt.% Alane)

Data will be provided to Kriston to incorporate into system-level model

Reactor performance tests kinetics will be performed on • 35-50 wt% AB slurries • 40-60 wt.% Alane slurries Note: Alternative reactor designs and operation will be performed to maximize reactor efficiency Data will be provided to Kriston to incorporate into system-level model

HX/Radiator PNNL Report on ability to develop/identify a radiator/HX capable of cooling the effluent from 525K to 360K having a mass less than 1.15 kg and a volume less than 10.9 liters

Radiator volume – 1.5L, mass 1.44kg, Validated models show a decrease in fins spacing will achieve the mass of 1.15kg mass and the required heat transfer meeting the metrics.

Met Target

GLS UTRC

Report on ability to develop a GLS capable of handling 720 mL/min liquid phase and 600 L/min of H2 @ STP (40 wt% AB @ 2.35 Eq H2 and max H2 flow of 0.8 g/s H2) fluid having a viscosity less than 1500cp with resulting in a gas with less than 100ppm aerosol having a mass less than 5.4 kg and volume less than 19 liters.

Mass 5.8 kg (above 5.4 kg metric) Volume 2.7 L (far below 19 L metric).

Exceeded volume target, but just over the mass target. Demonstrate operation meeting metrics utilizing spent fuel simulant.

Borazine Scrubber LANL

Report on ability to develop a borazine scrubber with a minimum replacement interval of 1800 miles of driving resulting in a minimum outlet borazine concentration of 0.1 ppm (inlet concentration = 4,000 ppm) having a maximum mass of 3.95 kg and maximum volume less of 3.6 liters.

An activated carbon borazine scrubber has been demonstrated yielding <0.1 ppm exit borazine concentration having: Mass = 6.8 kg (need significant reduction) Volume = 5.9 L (need reduction but not as critical as mass)

Alternative non-adsorbent based strategies are being explored to reduce the mass and volume of the scrubber.

Ammonia Scrubber UTRC

Report on ability to develop an ammonia scrubber with a minimum replacement interval of 1800 miles of driving resulting in a minimum ammonia outlet concentration of 0.1 ppm (inlet concentration = 500 ppm )having a maximum mass of 1.2 kg and a maximum volume of 1.6 liters.

Mass 1.1 kg (surpass 1.2 kg metric) Volume 1.6 L (meets 1.6 L metric) Met Target

BoP PNNL Report on ability to Identify BoP materials suitable for the Chemical Hydrogen system having a system mass no more than 41 kg and a system volume no more than 57 liters.

Mass = 60kg Volume = 61 L (really close to meeting volume target)

Critical reductions in mass: • borazine scrubber • pump mass • GLS mass • via parts consolidation/elimination/new technology Note: in meeting the mass target, we will also meet the volume target

System Design PNNL Report on ability to identify a system design having a mass less than 97 kg and a volume less than 118 liters meeting the all of the HSECoE drive cycles.

50%AB/Si oil : Media Mass = 97kg Media Volume = 86.5 L System Mass = 137 kg System Volume = 148 L

Alternate components and designs are being investigated but a higher density slurry (70w% AB or similar) will be required to meet the metric.

Efficiency Analysis NREL

Calculate and model the well-to-powerplant (WTPP) efficiency for two chemical hydride (CH) storage system designs and compare results relative to the 60% technical target.

Alane 24.7% WTPP efficiency AB 16.5% WTPP efficiency Met Target

Page 39: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Reactor Development and Performance

TTR Meeting Detroit, Michigan March 20-21, 2013

LANL TEAM Troy A. Semelsberger, Jose .I. Tafoya, Ben. L. Davis, and Brian. D. Rekken

T.A. Semelsberger

Page 40: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Status and Progress

Materials Tested in Batch Reactor

45

• 20 wt.% ATK Alane DEGBE-uncatalyzed

• 20 wt.% ATK Alane Julabo H350-uncatalyzed

• 20 wt.% ATK Alane DEGBE/LiH/Ti-catalyzed

• 20 wt.% ATK Alane Julabo H350/LiH/Ti-catalyzed

• 20 wt.% Slurry AB/Silicon Oil

• 20 wt.% Liquid AB/Iolilyte

Temperature Profile: Step 1: tiso = 60 min @ T = 25 °C Step 2: Tr = 1 °C/min with Tf = 140 °C Step 3: tiso = 2800 min @ T = 140 °C

Page 41: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 46

Batch Reactor Screening of Ammonia Borane and Alane

Objectives: 1. Solvent Effects 2. Catalytic Effects

Page 42: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 47

3 21.5 AlH Al H∆→ + 2.% .%wt H 10 wt≈3 rxn

kJH +11mol AlH

∆ ≈

• LiH and Ti improve kinetics of alane dehydrogenation in DEBE, but not in H350

• Solvent choice has a greater impact on alane dehydrogenation rate than LiH and Ti

• Dehydrogenation onset temperatures remain relatively unchanged wrt solvent or LiH/Ti

Alane Batch Reactor Results

90onsetT C≈

Page 43: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 48

3 3 x y z 2 3 3 6 2 6NH BH B N H +2.35H + NH3+ B N H + B H∆→2.% 15.2 .%

ABwt H wt≈

rxnkJH -49

mol AB∆ ≈

• AB Slurry demonstrated a three step process consistent with prior observations

• AB/Iolilyte two-step process coupled with chemical incompatibility with iolilyte

• Dehydrogenation onset temperatures are approximately the same

55onsetT C≈

AB Batch Reactor Results

Page 44: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Status and Progress

2. Flow Reactor Experiments

49

1. Batch Reactor Testing • AB Slurry • Alane Slurry • AB-IL

2. Flow Reactor Testing

• MPAB (liquid exothermic material) • Helical Reactor (O) • Helical Reactor (A) • Packed-bed Reactor (PB)

• AB Slurry (exothermic material) • Auger Reactor

• Alane Slurry (endothermic material) • Auger Reactor

Page 45: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 50

Alane Slurry Reactor Tests

Slurry Composition: • 20 wt. % Alane (ATK): 2.00 wt. % H2 • AR 200 Silicon Oil (200 cP) • TritonTM X-15 (0.025 g X-15/g AB)

TritonTM X-15

Stirred Settled

Prepared by T.A. Semelsberger

Page 46: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 51

0

25

50

75

100

125

150

175

200

225

250

275

300

0 50 100 150 200 250 300 350 400 450

Tem

pera

ture

(oC)

Time (minutes)

Reactor InletReactor SetpointReactor OutletAvg Reactor Temp

Alane = 1.09 mL/min Alane = 0.55 mL/min

20 wt.% Alane-07 • Auger Reactor (Volume = 7.4 mL) • Reactor Tstpt = 125-275°C • Feed Flow Rates:

• 1.09 mL/min (6.8 min) • 0.55 mL/min (13.5 min)

Alane flow-reactor experiment was well behaved and stable

No observable endothermic temperature profiles

Alane Auger Reactor Results

Page 47: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 52

100 120 140 160 180 200 220 240 260 280

0

20

40

60

80

100

120

Con

vers

ion

(%)

Temp (C)

τliquid = 6.8 min τliquid = 13.5 min

20 wt.% Alane-07 • Auger Reactor (Volume = 7.4 mL) • Reactor Tstpt = 125-275°C • Feed Flow Rates:

• 1.09 mL/min (6.8 min) • 0.55 mL/min (13.5 min)

Alane Auger Reactor Results

100 120 140 160 180 200 220 240 260 280

0

50

100

150

200

250

300

H2

Flow

(scc

m)

Temp (C)

τliquid = 6.8 min τliquid = 13.5 min

Conversion and hydrogen flow rate increase with increasing temperature

Conversions greater than 100% were observed because of the decomposition of silicon oil and/or the chemical reaction of silicon oil with aluminum/alane…resulting in an increase in the observed hydrogen production

2

100%

300

Alane max

H max

X

F sccm

Page 48: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 53

0

25

50

75

100

125

150

175

200

225

250

275

0

10

20

30

40

50

60

70

80

90

100

110

0 30 60 90 120 150 180 210 240 270 300 330 360 390 420

Avg

Reac

tor T

empe

ratu

re (o

C)

Mol

e Pe

rcen

t (%

)

Time (minutes)

[H2]

[tracer]

Sum H2 + tracer

Avg Reactor Temp

Alane = 1.09 mL/min Alane = 0.55 mL/min

20 wt.% Alane-07 • Auger Reactor (Volume = 7.4 mL) • Reactor Tstpt = 125-275°C • Feed Flow Rates:

• 1.09 mL/min (6.8 min) • 0.55 mL/min (13.5 min)

Alane Auger Reactor Results

Hydrogen mole percentage tracks nicely with temperature

The mole percentage totals sum to approximately 100%

180 min t 330 min≤ ≤

Page 49: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 54

0

1

2

3

4

5

6

7

8

9

10

0

10

20

30

40

50

60

70

80

90

100

110

0 30 60 90 120 150 180 210 240 270 300 330 360 390 420

Impu

rity:

Abs

orba

nce

Mol

e Pe

rcen

t (%

)

Time (minutes)

[H2][tracer]Sum H2 + tracerIR: TracerIR Impurity

Alane = 1.09 mL/min Alane = 0.55 mL/min

20 wt.% Alane-07 • Auger Reactor (Volume = 7.4 mL) • Reactor Tstpt = 125-275°C • Feed Flow Rates:

• 1.09 mL/min (6.8 min) • 0.55 mL/min (13.5 min)

Alane Auger Reactor Results

The only impurity observed was due to thermal decomposition of the silicon oil used as the carrier

Maximum temperature of this alane composition is around Tavg ~210 °C

Page 50: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 55

Summary: 20 wt.% Alane Slurry Reactor Results

• Successful demonstration of a 20 wt. % alane slurry dehydrogenation as a function of temperature and space-time

• Full conversion of slurry alane was observed over the temperatures, and space-times investigated

• Maximum conversion observed was XMPAB ~100% @ τliquid = 6.8min and T = 260-275°C with in-house built auger reactor

• The only impurity observed during alane dehydrogenation was the degradation of the carrier (Reactor Tstpt = 225°C, Tavg = 210°C)

• The reaction was stable, clean and facile

• Improvements in the reaction kinetics can be accomplished by the use of dopants and alternative solvents

Slurry Endothermic Material

Page 51: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Borazine Adsorption

56

5.4 Å

Borazine

Relevance: To develop and demonstrate hydrogen purification technologies that produce fuel-cell grade hydrogen meeting DOE purity targets

Component Partner S*M*A*R*T Milestone

Borazine Scrubber LANL

Report on ability to develop a borazine scrubber with a minimum replacment interval of 1800 miles of driving resulting in a minimum outlet borazine concentration of 0.1 ppm (inlet concentration = 4,000 ppm) having a maximum mass of 3.95 kg and maximum volume less of 3.6 liters.

Borazine is a known fuel cell impurity that requires scrubbing

Page 52: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Screen adsorbents for borazine adsorption capacities at RT under static adsorption conditions

Adsorbents dried under Ar flow at 200 C for 2 hr Adsorbents kept under sealed borazine gas environment for

several days Mass gain is measured to estimate the borazine adsorption

capacity under the static adsorption Downselect adsorbents to determine the dynamic adsorption capacities of borazine Dynamic adsorption mimics closely the situation where impurity gases (produced by the decomposition of AB-based H2 storage system) flow through the adsorbent (s)

57

Adsorbents

Static Adsorption

Dynamic Adsorption

(Downselect adsorbents)

• Pre-treatment • Temperature • Chemical Modification • Pressure • Concentration

Approach

Page 53: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

Borazine Adsorbents

Sample group Sample name/ID Form Surface acidity (Si/Al)

Surface area (m2/g)

Av. Particle size (μm)

Y-zeolite CBV720 CBV300

H NH4

15 2.55

780 925

<461 <461

ZSM-5 (as-received)

CBV28014 CBV3024 CBV8014 CBV5524G

H H H NH4

140 15 40 25

400 400 425 425

<461 <461 <461 <548

ZSM-5 (modified)

Cu/Zn on CBV3024E Cu/Zn on CBV5524G

NH4

25

270

<653

Activated carbon

ACN-210-15 AX-21 DMAP impregnated in AX-21

Felt Porous particle Porous particle

1500 1500

Oxides

BASF-K3-110 Al2O3 SiO2 ZnO

58

Page 54: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

59

11.36

3.77 5.54 5.99 4.45 5.31

40.54

21.98

5.12

0

6

12

18

24

30

36

42

48

Y-Zeolite,CBV720, H,S.A=780 ,Si/Al=15

Y-Zeolite,CBV300, NH4,

S.A.=925,Si/Al=2.55

ZSM-5,CBV28014, H,

S.A.=400,Si/Al=140

ZSM-5,CBV8014, H,

S.A.=425,Si/Al=40

ZSM-5,CBV3024,H,

S.A.=400,Si/Al=15

ZSM-5,CBV5524G,

NH4,S.A.=425,Si/Al=25

Act. C,ACN-210-15,

S.A.=1500

Act. C,AX-21

S.A.=1500

BASF-K3-110

Adso

rptio

n Ca

paci

ty %

Downselected Adsorbents:

Y-zeolite (CBV720) ZSM-5 (CBV28014, CBV8014) Activated carbon (ACN-210-15, AX-21)

Borazine Adsorption: Dynamic Conditions

T = 298K P = amb Flow Rate =40 sccm [borazine] =

(%) adsorbate

adsorbent

mAdsorption Capacity 100m

= ⋅

Page 55: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

60

9.52 11.36

13.46

5.67 5.54 7.65

6.13 5.99 6.4

30.59

40.54 38.92

21.6 21.98 21.7

0

5

10

15

20

25

30

35

40

45

50

Dry

As-re

ceive

d

Wet Dry

As-re

ceive

d

Wet Dry

As-re

ceive

d

Wet Dry

As-…

Wet Dry

As-re

ceive

d

Wet

Adso

rptio

n Ca

paci

ty %

Y-zeolite CBV720

ZSM-5 CBV28014

ZSM-5 CBV8014 ACN-210-15 AX-21

Humidifying Conditions: samples were exposed to a saturated water stream for two hours prior to adsorption experiments

• Zeolites and AX-21 demonstrated only slight differences in borazine adsorption capacities as a function of pre-treatment

Borazine Adsorption: Pre-treatment Effects

T = 298K P = amb Flow Rate = 40 sccm [borazine] =

Drying Conditions: Dried @ 350 C for > 12 hr under Ar flow

Note: Chemically modified ACN did not show marked improvements in borazine adsorption or

polymerization capacities

• ACN-210-15 demonstrated improved adsorption capacity as a function of humidification

• Down selected for further study

Page 56: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

61

ACN-210-15

AX-21

30 C 80 C 150 C

Borazine Adsorption: Temperature Effects

Adsorption capacity as a fcn of temperature

(%) adsorbate

adsorbent

mAdsorption Capacity 100m

= ⋅

Borazine breakthrough curves for ACN-210-15

(%)Temperature Adsorption Capacity↑ = ↓

as-received adsorbents

as-received adsorbents

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U N C L A S S I F I E D

30.59

0.45

40.54

4.31 38.92

5.92

0

10

20

30

40

50

Dry As-received

Wet

Adso

rptio

n Ca

pacit

y %

40.54

4.31

35.34

4.66

14.51

0.68

0

10

20

30

40

50

30 C 80 C 150 C

Adso

rptio

n Ca

pacit

y %

62

Adsorption capacity as a fcn of sample pre-treatment Adsorption capacity as a fcn of temperature

Borazine adsorption capacity with ACN-210-15

(%) adsorbate

adsorbent

mAdsorption Capacity 100m

= ⋅

(%)Temperature Adsorption Capacity↑ = ↓( ) ( ) ( ) as received wet dried− ≈ >

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U N C L A S S I F I E D 63

Adsorbents Borazine Adsorbent: ACN-210-15 Ammonia Adsorbent: MnCl2 /IRH-33 (UTRC supplied) Approach Competitive adsorption: NH3 and borazine co-fed into (i) ACN-210-15 (ii) MnCl2 / IRH-33 Combining adsorption beds in series:

Co-feed NH3 and borazine through the borazine and ammonia adsorption beds connected in series

Ammonia Bed

Borazine Bed

Ammonia-Borazine Competitive Adsorption

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U N C L A S S I F I E D

64

0

0.2

0.4

0.6

0.8

1

0 50 100 150

C/C 0

Time(min)

t0

NH3 870 ppm

t1

Borazine 730 ppm

t1

ACN-210-15

ACN-

210-

15

( ) 1

0

t

BorazineAds Capacity 40%≈

( ) 0

0 33

t

BorazineAds Capacity %≈

Borazine Adsorption Capacity: ACN-210-15

( ) 1

0 1

t

AmmoniaAds Capacity %≈

( ) 0

0 0.3

t

AmmoniaAds Capacity %≈

Ammonia Adsorption Capacity: ACN-210-15

Ammonia has a low adsorption capacity in ACN-210-15

Competitive Adsorption ACN-210-15

Page 60: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

0

0.2

0.4

0.6

0.8

1

0 100 200 300 400

C/C

0

Time(min)

65

t1 t1 Borazine 966 ppm

NH3 918 ppm

t0 t0

( ) 1

0 6

t

BorazineAds Capacity %≈

( ) 0

0 5

t

BorazineAds Capacity %≈

Borazine Adsorption Capacity: MnCl2/IRH-33

( ) 1

0 6

t

AmmoniaAds Capacity %≈

( ) 0

0 3

t

AmmoniaAds Capacity %≈

Ammonia Adsorption Capacity: MnCl2/IRH-33 Mn

Cl2/I

RH-3

3

Ammonia and Borazine have comparable chemical affinities in MnCl2/IRH-33

Order of beds should be ACN-210-15 followed by MnCl2/IRH-33

MnCl2/IRH-33

Competitive Adsorption MnCl2/IRH-33

Page 61: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D

500150025003500 Wavenumber (cm-1)

66

0

0.2

0.4

0.6

0.8

1

0 50 100 150C/

C 0

Time(min)

Ammonia

Borazine

MnCl

2/IRH

-33

ACN-

210-

15

Demonstrated that ammonia and borazine can be scrubbed to produce fuel-cell grade hydrogen

:23 30

Adsorbed MassesBorazine mgAmmonia mg

≈≈

( ) 1

0 40

t

BorazineAds Capacity %≈

( ) 0

0 33

t

BorazineAds Capacity %≈

Borazine Adsorption Capacity

( ) 1

0 10

t

AmmoniaAds Capacity %≈

( ) 0

0 7

t

AmmoniaAds Capacity %≈

Ammonia Adsorption Capacity

t1 t1

t0 t0

Purification of Ammonia & Borazine

Page 62: Chemical Hydrogen Rate Modeling, Validation, and System ...Washington, DC May 13-17, 2013 Technology Team Lead: Ned Stetson LANL Team Troy A. Semelsberger, Ben L. Davis, Brian D.Rekken,

U N C L A S S I F I E D 67

Conclusions

• ACN-210-15 demonstrated the highest borazine adsorption capacity at ~ 40%

ACN-210-15> AX-21> Y-zeolite > ZSM-5 > Oxides

Note: Chemically modified substrates did not show marked improvements over the as-received analogs

• ACN-210-15 is an off-the-shelf carbon adsorbent requiring no special pretreatments or handling

• ACN-210-15 is a woven felt that is ideally suited for vibration prone environments because ACN-210-15 is not friable

• Adsorption capacity decreases with increasing temperature

• Borazine has higher chemical affinity toward MnCl2 than ammonia has for ACN-210-20

Purification order is important: borazine needs to be scrubbed prior to ammonia