SANDIA NATIONAL LAB · 2013. 5. 13. · material testing in h 2 gas - sandia national lab i. moro,...
Transcript of SANDIA NATIONAL LAB · 2013. 5. 13. · material testing in h 2 gas - sandia national lab i. moro,...
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MATERIAL TESTING IN H2 GAS
-
SANDIA NATIONAL LAB
I. Moro, L. Briottet, P. Lemoine
| PAGE 1 CEA | 10 AVRIL 2012
APRIL 9-10, 2013
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MATERIAL TESTING UNDER
HYDROGEN GAS AT CEA/LITEN
OVERVIEW
| PAGE 2
CEA | 10 AVRIL 2012
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MATERIAL TESTING IN GASEOUS H2
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Uniaxial loading under H2
< 350 bar and < 300°C
Disc/tube test under H2/He
< 1000 bar - Impurities
H2/D2 gas permeation tests
< 5 bar and < 300°C
Permeation cell
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PRESSURE VESSEL
+
SERVO-HYDRAULIC
TEST FRAME
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CEA | 10 AVRIL 2012
• MTS servo-hydraulic test frame (250 kN)
• Custom vessel
• Frontal opening
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PRESSURE VESSEL : OVERVIEW
| PAGE 5 SNL | APRIL 10 2013
Alignment device
External
load cell
Heating
Vacuum pump Gas management
MTS servo-hydraulic
test frame
Ventilation flow H2 sensor
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| PAGE 6 SNL | APRIL 10 2013
PRESSURE VESSEL : OVERVIEW
Specific device to screw
the door at nominal
torque without
damaging the load line
Specific design to allow
thermal expansion while
remaining aligned
Device for pressure
vessel alignment
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PRESSURE VESSEL : TESTS UNDER HIGH PRESSURE H2
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Pressure vessel
Maximum volume available
5,5L
+ use of dedicated tool to
reduce the gas volume
Max pressure (MPa) 35
T (°C) RT - 300
Test frame
Device maximum load 50 kN
Displacement ~100 mm
Min displacement rate
µm/s ~1
Fatigue test R > 0
Frequency Tested < 10Hz
under H2
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PRESSURE VESSEL : CROSS SECTION
Water cooling
Front door
Moving rod
Stud
Furnace
Gas-tight ducting
for instrumentation
Seals
Material vessel
SS 316L
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PRESSURE VESSEL : CROSS SECTION
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| PAGE 10 SNL | APRIL 10 2013
PRESSURE VESSEL : SEALS
3 O-ring
dynamic
seals
Monitoring
Pumping
Security alert
Static seals
Kalrez seals
(perfluoroelastomer)
SS S-type seals
(temperature)
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| PAGE 11 SNL | APRIL 10 2013
PRESSURE VESSEL : TRANSDUCERS
Strain gages COD or extensometers
CTOD gage
Load cell
Signal drift during long term tests under hydrogen pressure (> few hours)
Not stabilised after 2 days under 30 MPa H2
Slow drift : not critical for cyclic loadings
WOL test (with in-situ precracking) not possible
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PRESSURE VESSEL : LOAD CELL
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0
0,6
1,2
1,8
9,6 9,7 9,8 9,9
Forc
e (
kN)
Déformation (%)
cellule extérieure
cellule in-situ
External load cell (100kN) : friction between rod and seals estimated < 300 N
=> detrimental for tests below ~10 kN
Development of an internal 50kN load cell (strain gages protected from H2 gas)
no drift
very sensitive to alignment and clamping
External cell
Internal cell
Strain
Load
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H2, N2
Remote control and monitoring
Pneumatic valves
H20 et 02 sensors : not effective for low ppm (< 10 ppm)
Hygrometer : capacitance principle using a gold/alumina oxide probe
Trace Oxygen Analyser : Micro fuel cell (electrochemical galvanic device)
Tests under H2 : N60 purity gas
Always the same procedure including :[Vacuum / N2] (x 3) before H2 inlet
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PRESSURE VESSEL : GAS MANAGEMENT
Servo-hydraulic device
remote control
Gas remote
control
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Sample preparation :
- traction / LCF : surface roughness
- crack growth / toughness : precrack under air
Gas management procedure to ensure gas purity
N2 pressure at testing pressure to check tightness
H2 pressure
Tests using MTS (MPT or specific procedure)
After testing : H2 sweeping out, N2 inlet, vacuum, 1 bar N2
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PRESSURE VESSEL : TEST PROCEDURE
Servo-hydraulic device
remote control
Gas remote
control
P
External load = f(P)
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Shut down all
electrical power
in test room
H2 sweeping out
N2 inlet
Max venting flow rate
in the room
Automated safety procedure
Remote control – No access under H2
Automatised gas management procedure
Security camera
Min venting flow rate
| PAGE 15 SNL | APRIL 10 2013
PRESSURE VESSEL : SAFETY ISSUES
Seal tightness control
H2 and O2 sensors
2 H2 thresholds
10 % Inferior flammability limit in air
20 % Inferior flammability limit in air
MTS Gas
management
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MAIN DISADVANTAGES Test in temperature : thermal inertia
Test preparation : ~3 hours, alignment
Gas purity analysis
Pressure below 35 MPa / Low P accuracy below 2 bar
FUTURE IMPROVEMENTS
Gas purity analysis
Extensometer with strain gages : signal drift LVDT ?
Crack initiation detection from small defect (calibrated hole)
Towards 100 MPa ?
| PAGE 16 SNL | APRIL 10 2013
PRESSURE VESSEL : SUMMARY
MAIN ADVANTAGES Available volume (+ use of tools to reduce gas
volume) / instrumentation
Remote gas management
“Fast” atmosphere switches
Reliable : 6 years old – No major trouble
Precise measurement from low to high loads
Load cell : no drift under H2
Alignment : ~ straight crack fronts
crack front
SENT specimen
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DISK PRESSURE TESTS
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CEA | 10 AVRIL 2012
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DISC PRESSURE TEST : SET-UP
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H2
He
Compressed air
H2O
Remote control
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DISK PRESSURE TESTS : OVERVIEW
Remote control
H2, He : Up to 100MPa, Tmax = 100°C 2 cells
Pressure rate: up to 1000 bar/min
above 0,1 bar/min
Controlled pressure rate
Working with impure gas (dedicated cell)
O2
H2O (bubbler up to 100°C) (from few ppm to 5000 ppm) Including long time steps
| PAGE 19 SNL | APRIL 10 2013
Room T H2O 100°C
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DISK PRESSURE TESTS
SEALS
O-ring (elastomer) at high rates
Indium at low rates
| PAGE 20 SNL | APRIL 10 2013
WATER CONTENT CONTROL
Dedicated H2 + H2O gas bottle
Using bubbler
Measuring P and T
Assuming saturated gas
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TUBE PRESSURE TESTS
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DEVICE ADAPTED TO TUBE PRESSURE TESTS
Long time range tests
under H2 pressure (few months)
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DISC PRESSURE TESTS
Advantages
Low volume
Easier to proceed
Dedicated cell for impure gas
Fast gas switches (few seconds)
Closer to service-life loadings
| PAGE 22 SNL | APRIL 10 2013
Improvements
Measuring in-situ deflection
Developing tests under fatigue (cycling pressure) with
/ without defects
Disadvantages
Less instrumented
More difficult to analyze
mechanically (use of FEM)
Boundary conditions
Small thickness
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H2/D2 GAS PERMEATION DEVICE
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20°C < T < 300°C
Pabs < 5 bar
Mass spectrometer
• Diffusion coefficient
• Solubility
• Traps (binding energy)
• Oxide layer
Developments
Permeation under tensile loading
Influence of hydrostatic stress gradient
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THANK YOU
I. Moro, L. Briottet, P. Lemoine
| PAGE 24 CEA | 10 AVRIL 2012
APRIL 9-10, 2013