Addressing Hydrogen Embrittlement in the SAE J2579 Fuel Cell Vehicle Tank Standard
description
Transcript of Addressing Hydrogen Embrittlement in the SAE J2579 Fuel Cell Vehicle Tank Standard
Addressing Hydrogen Embrittlement in the SAE J2579 Fuel Cell Vehicle Tank
Standard
Brian SomerdaySandia National Laboratories
Livermore, CA, USA
Christine SloaneSloaneSolutions, LLC
Kewadin, MI, USA
International Conference on Hydrogen Safety ICHS 2011San Francisco, CA, USA
September 14, 2011
Sandia is a multiprogram laboratory operated by Sandia Corporation, a Lockheed Martin Company, for the United States Department of Energy under contract DE-AC04-94AL85000
SAE J2579 focuses on safety qualification of vessel in Compressed Hydrogen Storage
System of FCVs
•Compressed Hydrogen Storage System (CHSS) boundary defined by interfaces that isolate stored high pressure H2
•All containment vessel designs include metal components (e.g., composite vessels have boss and liner)
ContainmentVessel
ContainerIsolation
Valve
FillCheckValve
ExcessflowReceptacle
with check
Full SystemIsolation
LowPressure
Regulator
PRVPRV
HighPressure
Regulator
Hydrogen Fuel Handling System
Compressed HydrogenStorage System
PRD
ServiceDefuel Shufoff
vent
ContainmentVessel
ContainerIsolation
Valve
FillCheckValve
ExcessflowReceptacle
with check
Full SystemIsolation
LowPressure
Regulator
PRVPRV
HighPressure
Regulator
Hydrogen Fuel Handling System
Compressed HydrogenStorage System
PRD
ServiceDefuel Shufoff
vent
Barthélémy, 1st ESSHS, 2006
a
Number of pressure cycles, N
crack in H2
crack in N2
Safety qualification of vessel must consider hydrogen embrittlement of metal
componentsHydrogen embrittlement accelerates fatigue cracking
Nf = Ninitiation + Ngrowth
H2
H2
H2
H2
p
a
H2
H2
H2
Vessel safety qualification typically conducted by either engineering analysis or performance
testing
•Design qualification in SAE standards based on performance testing
p
Ri
Ro
at
stress analysis: K = p[f(a, t ,Ro, Ri)]
crack growth law: da/dN = C(K)m
engineeringanalysis
pressure
p
Number of pressure cycles, N
performancetesting
Nf
Vessel safety qualification in SAE J2579 is based on performance
testing
•These performance tests do not evaluate “durability” under H2 gas pressure cycling, i.e., hydrogen embrittlement
Pneumatic test (H2) Hydraulic test
Durability Performance Verification Test
cb
Proo
f Pr
essu
re
5% cy -40Ca
5% cy +50Cb
40%cy 15-25Cc
150%NWP
+55oC +55oC a
Pres
sure
time
BurstBP0 <20%
Leak
/ P
erm
eatio
n>
30 h
rs
a Fuel/defuel cycles @-40oC with initial system equilibration @ -40oC, 5 cycles with +20oC fuel; 5 cycles with <-35oC fuelb Fuel/defuel cycles @+50oC with initial system equilibration @+50oC, 5 cycles with <-35oC fuelc Fuel/defuel cycles @15-25oC with service (maintenance) defuel rate, 50 cycles
5% cy +50C5% cy -40C40%cy 15-25C
Leak
/ P
erm
eatio
n>
30 h
rs
180%NWP
125%NWP115%NWP80%NWP
ab
Expected-Service Performance Verification Test
500 cy = light duty1000 cy = heavy duty
cb
Proo
f Pr
essu
re
5% cy -40Ca
5% cy +50Cb
40%cy 15-25Cc
150%NWP
+55oC +55oC a
Pres
sure
time
BurstBP0 <20%
Leak
/ P
erm
eatio
n>
30 h
rs
a Fuel/defuel cycles @-40oC with initial system equilibration @ -40oC, 5 cycles with +20oC fuel; 5 cycles with <-35oC fuelb Fuel/defuel cycles @+50oC with initial system equilibration @+50oC, 5 cycles with <-35oC fuelc Fuel/defuel cycles @15-25oC with service (maintenance) defuel rate, 50 cycles
5% cy +50C5% cy -40C40%cy 15-25C
Leak
/ P
erm
eatio
n>
30 h
rs
180%NWP
125%NWP115%NWP80%NWP
ab
Expected-Service Performance Verification Test
500 cy = light duty1000 cy = heavy duty
Pres
sure
Dam
age
Dro
p
time
BP0 <20%
ResidualStrength
Chem
ical
s
48 hr
N cycles15C-25C
chemicalexposure 150% NWP
burst
125%NWP
180%NWP
1000 hr+85oC
M cycles-40oC
M cycles+85oC, 95%RH
10cycles
15-25oCProo
f Pre
ssur
e
80%NWP
N cycles•3500 cycles passenger light-duty• 7000 cycles commercial, heavy-dutyM cycles• 1000 cycles passenger light-duty• 2000 cycles commercial, heavy-duty
Pres
sure
Dam
age
Dro
p
time
BP0 <20%
ResidualStrength
Chem
ical
s
48 hr
N cycles15C-25C
chemicalexposure 150% NWP
burst
125%NWP
180%NWP
1000 hr+85oC
M cycles-40oC
M cycles+85oC, 95%RH
10cycles
15-25oCProo
f Pre
ssur
e
80%NWP
N cycles•3500 cycles passenger light-duty• 7000 cycles commercial, heavy-dutyM cycles• 1000 cycles passenger light-duty• 2000 cycles commercial, heavy-duty
Logic flow for addressing hydrogen embrittlement through performance testing in
SAE J2579
•Recent activity focused on Appendix C.14 and Appendix C.15
Metals in vessel are 6061 Al or high-nickel 316 stainless steel?(SAE J2579 Appendix B.2.3)
Metals in vessel meet acceptance criteria from materials testing in H2?(SAE J2579 Appendix C.15)
Vessel qualified using existing expected-service (pneumatic) and durability (hydraulic) performance tests (SAE J2579 Section 5.2.2)
YES NO
Vessel qualified using existing performance tests (SAE J2579 Section 5.2.2) AND new (more extreme) H2 gas cycling test (SAE J2579 Appendix C.14)
NO
YES
Logic flow for addressing hydrogen embrittlement through performance testing in
SAE J2579
•Tests in Appendix C.15 determine whether material has unrestricted (i.e., not design specific) hydrogen compatibility
Metals in vessel are 6061 Al or high-nickel 316 stainless steel?(SAE J2579 Appendix B.2.3)
Metals in vessel meet acceptance criteria from materials testing in H2?(SAE J2579 Appendix C.15)
Vessel qualified using existing expected-service (pneumatic) and durability (hydraulic) performance tests (SAE J2579 Section 5.2.2)
YES NO
Vessel qualified using existing performance tests (SAE J2579 Section 5.2.2) AND new (more extreme) H2 gas cycling test (SAE J2579 Appendix C.14)
NO
YES
Appendix C.15 materials test:slow strain rate tensile test
HH
HH
HH
H2
H2H2
H2
H2 H2
OR
•Issues addressed:–Acceptance criterion established as RAH2/RAair > 0.7
–Test conducted in H2 gas or with “precharged” H
–Test temperature(s)
RA
Appendix C.15 materials test:fatigue crack initiation test
stress (S)
cycles to failure (Nf ~ Ninitiation)
• Issues addressed:–R ratio, i.e., ratio of Smin to Smax
–Stress-cycle frequency (f)
–Test temperature(s)
–Acceptance criterion, e.g., Nf(H2)/Nf(air) ~ 1air
H2
Appendix C.15 materials test:“long crack” growth test
da/dN
K
H2
H2
H2
H2H2
H2
H2H
HH
load
aH2
H2
H2
H2H2
H2
H2H
HH
load
a
air
H2
• Issues addressed:–Load-cycle frequency
–Test temperature(s)
–Acceptance criterion?
Load-cycle frequency must be specified for fatigue tests conducted in H2 gas
Magnitude of accelerated fatigue cracking in H2 gas depends on load-cycle frequency
A.H. Priest, British Steel, 1983
Logic flow for addressing hydrogen embrittlement through performance testing in
SAE J2579
•Performance test in Appendix C.14 evaluates design-specific hydrogen compatibility
Metals in vessel are 6061 Al or high-nickel 316 stainless steel?(SAE J2579 Appendix B.2.3)
Metals in vessel meet acceptance criteria from materials testing in H2?(SAE J2579 Appendix C.15)
Vessel qualified using existing expected-service (pneumatic) and durability (hydraulic) performance tests (SAE J2579 Section 5.2.2)
YES NO
Vessel qualified using existing performance tests (SAE J2579 Section 5.2.2) AND new (more extreme) H2 gas cycling test (SAE J2579 Appendix C.14)
NO
YES
Performance test in Appendix C.14 intended to account for H2-accelerated fatigue
cracking
• Issues addressed:–Pressure-cycle profile
–Test temperature
–Number of cyclesH2 pressure
Number of pressure cycles, N
125% NWP
rise time > 5 min hold time > 2 min
p
H2
H2
H2
H2
H2
H2H2
fillermaterial a
2 MPa
SAE working group on hydrogen embrittlement represents international
effort
• SAE J2579 Appendix B.2.3• SAE J2579 Appendix C.15• SAE J2579 Appendix C.14
JapanJARIAIST/HYDROGENIUS
EuropeAdam OpelBMWRobert BoschLinde
USAGMSandia National Laboratories
Summary
•Vehicle tank standard SAE J2579 describes safety qualification for Compressed Hydrogen Storage System
•Safety qualification based on performance testing–Hydraulic long-term durability test does not account for
hydrogen embrittlement
•New tests developed for SAE J2579 to evaluate hydrogen compatibility of vessel designs–Material-level testing determines whether material has
unrestricted (i.e., not design specific) hydrogen compatibility
–Component-level testing evaluates design-specific hydrogen compatibility