HAL Id: jpa-00226599
https://hal.archives-ouvertes.fr/jpa-00226599
Submitted on 1 Jan 1987
HAL is a multi-disciplinary open access archive for the deposit and dissemination of sci- entific research documents, whether they are pub- lished or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers.
L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignement et de recherche français ou étrangers, des laboratoires publics ou privés.
HYDROGEN EMBRITTLEMENT IN Al-Li-Cu-Mg ALLOYS (8090-T651)
F. Binsfeld, M. Habashi, J. Galland, J. Fidelle, D. Miannay, P. Rofidal
To cite this version:
F. Binsfeld, M. Habashi, J. Galland, J. Fidelle, D. Miannay, et al.. HYDROGEN EMBRITTLEMENT
IN Al-Li-Cu-Mg ALLOYS (8090-T651). Journal de Physique Colloques, 1987, 48 (C3), pp.C3-587-
C3-596. �10.1051/jphyscol:1987368�. �jpa-00226599�
JOURNAL DE PHYSIQUE
Colloque C3, suppl6ment au n09, Tome 48, septembre 1987
HYDROGEN EMBRITTLEMENT IN Al-Li-Cu-Mg ALLOYS (8090-T651)
F. BINSFELD, M. HABASHI, J. GALLAND, J.P. FIDELLE*, D. MIANNAY*
and P. ROFIDAL*
Ecole Centrale des Arts et Manufactures, F-92295 Ch.Eitenay-Malabry Cedex, France
* C E A , B.P. 511, F-75752 Paris Cedex 15, France
ABSTRACT
This paper describes the hydrogen embrittlement (HE) o f an A1-Li a l l o y aged a t 190°C and with d i f f e r e n t durations o f ageing (10, 15, 20 and 30 hr).
Two techniques were employed t o measure HE : a) cathodic p o l a r i z a t i o n i n a molten s a l t s bath with -3 VIAg on t e n s i l e specimens ; b ) gaseous hydrogenation on disks. Hydrogen charging was achieved a t 190°C. The r e s u l t s show t h a t HE i s important when the a1 1 oy i s i n the over-aged condition.
INTRODUCTION
A1-Li a l l o y s have gathered strong i n t e r e s t especially i n t h e a i r c r a f t industry. Compared t o conventional high-strengh a1 umini um a1 loys o f the 2000 or 7000 series, i t i s known t h a t A1-Li a l l o y s o f f e r a 10% increase i n Young's modulus along w i t h a 10% decrease i n s p e c i f i c weight, thus making them rather competitive t o new non-metal 1 i c materi a1 s 1 i ke carbon f i b r e reinforced '
composi tes. Moreover, t h e i r mechanical properties are equivalent t o those o f conventional high-strength A1
.
a1 loys.I n t h e binary Al-Li a l l o y system, t h e 6
'
(A13Li) p a r t i c l e s which p r e c i p i t a t e throughout t h e matrix are responsible f o r strengthening. I n the A1-Li-Cu-Mg a l l o y s apart from the6
I , semi coherent, S t (AlzCuMg) and TI(A12CuLi) phases p r e c i p i t a t e during a r t i f i c i a l ageing treatment. 6
'
i s a metastable phase' which forms as spherical p a r t i c l e s which remain coherent w i t h the matrix ( 1 ). During p l a s t i c deformation, these p a r t i c l e s may be cut by moving dislocations such t h a t f u r t h e r deformation along the same s l i p plane i s favoured ; s l i p becomes coplanar (2, 3) and leads t o poor toughness and ducti 1 i ty. The s l i p cop1 anari t y gives ri se t o stress concentrations a t g r a i n boundaries i nduci ng intergranul ar f a i 1 ures (4). The growth r a t e o f6
dependsArticle published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphyscol:1987368
JOURNAL DE PHYSIQUE
o n vacancy c o n c e n t r a t i o n which i n t u r n i s a f f e c t e d by high s o l u t i o n t r e a t m e n t t e m p e r a t u r e f o l 1 owed by c o l d
water
quenched (51.
The s t r e n g t h enhancement d u r i n g room t e m p e r a t u r e a g e i n g a p p e a r st o
be duet o
t h e p r e c i p i t a t i o n o f6 '
phase. Subsequent a r t i f i c i a l a g e i n g g i v e s r i s e
t o a
g r a i n boundary REZ, ( P r e c i p i t a t i o n F r e e Zone) i n d i c a t i n g t h a t $ p r e c i p i t a t i o n i s dependent upon t h e p r e s e n c e o f e x c e s s v a c a n c i e s (5). The P.F.Z. grows accordingt o
t 1 / 3 1 aw, where t i s t h e ageing time a t a given ageing t e m p e r a t u r e ( 6 ) . Attempts t o improve t o u g h n e s s o f A1-Li a 1 l o y s have been -based on t h e change i n g r a i n s t r u c t u r e t o i n f l u e n c e t h e f r a c t u r e process. A d d i t i o n o f manganese i s known a s a g r a i n - r e f i n e r b u t a s an improvementt o
g r o s s i n t e r g r a n u l a r f a i l u r e (7).Zirconium a d d i t i o n of l e s s t h a n 0.2% forms
p '
(A13Zr) p r e c i p i t a t i o n which g i v e s r i s eto
g r a i n--ref i nement, i n h i b i t i o n o f r e c r y s t a l 1 i s a t i o n and d e c r e a s i n g s h e a r e d6 '
p a r t i c l e s by t h e moving d i s l o c a t i o n s (8). However, zirconium g i v e s h i g h l y t e x t u r e d s t r u c t u r e s ( 5 ) i n A1-Li a l l o y s .The Cu and Mg p r e c i p i t a t e heterogeneous1 y d u r i n g a r t i f i c i a l ageing
as
S ' (A1 2CuMg) and TI (A1 2CuLi ).
The n u c l e a t i o nsites
o f t h e s e p r e c i p i t a t e s a r e d i s l o c a t i o n s formed d u r i n g quenching, d i s l o c a t i o n s i n t r o d u c e d d u r i n g s t r e t c h i n g and low-angle s u b g r a i n boundaries. Grain boundary p r e c i p i t a t i o n o f6
(AlLi ) and complex A1-CU-Mg phases occur d u r i n g a r t i f i c i a l ageing ( 9 ) . a s t r e t c h b e f o r e a r t i f i c i a l a g e i n g i n c r e a s e s t h e r a t e of ageing and t h e n i n c r e a s e s t h e y i e l d s t r e n g t h and t h e u l t i m a t e t e n s i l e s t r e n g t h b u t r e d u c e s t h e e l o n g a t i o nt o
f r a c t u r e . For each chemical composition of A1-Li a l l o y , t h e r e i sa
s p e c i f i c ageing h e a t t r e a t m e n t c o n d i t i o n (peak aged c o n d i t i o n ) a t which t h e mechanical p r o p e r t i e s a r e optimum. In t h e under-aged c o n d i t i o n , t h e deformation i s l o c a l i z e d w i t h i n s l i p bands w h i l e a t t h e peak c o n d i t i o n t h e deformation i s homogeneous and duet o
t h e i n c r e a s e d volume f r a c t i o n o f S 1 t h r o u g h o u t t h e matrix. In t h e overaged c o n d i t i o n , t h e p r e c i p i t a t i o n o f 'S'i s
a t once w i t h i n t h e m a t r i x and i n t h e sub-grain boundaries ( 9 ) .On t h e o t h e r hand, conventional h i g h - s t r e n g t h aluminium a l l o y s such
as
A1-Zn-Mg, Al-Zn-Mg-Cu and A1-Mg s u f f e r a r e v e r s i b l e hydrogen e m b r i t t l e m e n t whereas A1-Cu and al-Cu-Mg a p p e a rt o
be r e s i s t a n tt o
hydrogen i n t r o d u c e d e i t h e r by c a t h o d i c c h a r g i n g o r by exposureto
water c o n t a i n i n g environments (10).To t h e b e s t o f
our
knowledge, A1 -Li-Mg-Cu-Zr (8090 a l l o y ) has not been s t u d i e dso
f a r . In t h i s paper, hydrogen e m b r i t t l e m e n t of 8090-
T651 was t h e n i n v e s t i g a t e d .EXPERIMENTAL
The chemical composition and t h e t h i c k n e s s t of t h e a l l o y s s t u d i e d i n t h i s i n v e s t i g a t i o n a r e given i n t a b l e I .
T a b l e I : Chemical composition and t h i c k n e s s of t h e a l l o y s s t u d i e d ( w t % ) .
...
I
LiI
MgI
CuI
ZrI
S iI
TiI
Fe I N a , p p m l t , m m l1
2.71
1.11
1 . 31
0.091
0.021
0.021
0.021
31
0 . 81 1
2.91
1.11
1 . 31
0.091
0.021
0.021
0.021
31
1 . 61
The experimental m a t e r i a l was suppl i e d by CEGEDUR PECHINEY i n t h e form of 0.8 and 1.6
nun
r o l l e d p l a t e i n t h e s o l u t i o n t r e a t e d (535OC d u r i n g I h r and t h e n c o l d w a t e r quenched) and 3% s t r e t c h e d , c o n d i t i o n T-351. Hydrogen charging was achieved by two methods :1 ) C a t h o d i c a l l y on t e n s i l e specimens having 1.6 m m t h i c k n e s s i n a molten s a l t s bath ( 1 1 ) a t 190°C d u r i n g 10, 15, 20 and 30 h r and a t d i f f e r e n t c a t h o d i c p o t e n t i a l s : -1 .5, -2.0, -2.5 and -3.0 V/Ag. A f t e r hydrogenation, o u t g a s i n g was a c h i e v e d , and QH was measured a t 520°C and 1000°C. Uncharged and hydrogen c a t h o d i c a l l y charged specimens
were
t e n s i l e t e s t e d a t room t e m p e r a t u r e , u s i n g a s t r a i n r a t e o f 2 . 7 . 1 0 - ~ s - ~ t o s t u d y t h e e f f e c t o f hydrogen c h a r g i n g on t e n s i l e p r o p e r t i e s . Reference specimenswere
t h o s e aged a t 1 90°C i n f u r n a c e d u r i n g 10, 15, 20 and 30 h r .2 ) Gaseous hydrogen on d i s k s having 0 . 8
mm
t h i c k n e s s . The d e t a i l s of t h i s methodwere
d e s c r i b e d elsewhere (12). The r e f e r e n c e g a z was helium. The f o l l owing procedureswere
achieved :a ) i n c r e a s i n g t h e r a t e of hydrogen p r e s s u r e A P/ A t from 0.007 t o 188
-4
M%hi&&ternal hydrogen). The a l l o y was i n T651 c o n d i t i o n ;
b) thermal hydrogen o r helium charging on both s i d e s a t 1 90°C, d u r i n g 20 h r . Gas p r e s s u r e was 400 Pa ( i n t e r n a l hydrogen) ;
c ) c a t h o d i c a l l y hydrogen c h a r g i n g a t 190°C d u r i n g 2 0 h r and w i t h -3V/Ag ( i n t e r n a l hydrogen).
Tn
t h e two l a s t c o n d i t i o n s e i t h e r he1 ium ( b ) or/and hydrogen g a s ( c )were
usedtochieve f a i l u r e .All t h e f a i l u r e s
were
c a r r i e d o u t a t 20°C. F r a c t u r e s u r f a c e swere
examined using a scanning e l e c t r o n microscope.JOURNAL DE PHYSIQUE
EXPERIMENTAL RESULTS
1 ) C a t h o d i c a l l y hydrogen c h a r g i n g
F i g u r e 1 shows t h a t t h e outgased QH i s an i n c r e a s i n g f u n c t i o n
as
t h e a p p l i e d c a t h o d i c p o t e n t i a l l e v e l and t h e t i m e o f hydrogen c h a r g i n g a r e i n c r e a s e d whatever t h e o u t g a s i n g t e m p e r a t u r e i s 520°C o r i s 1 000°C. However, QH measureda t
1000°C i s h i g h e r t h a n t h a t o b t a i n e d a t 520°C showing t h a t m o l e c u l a r hydrogen t r a p p i n goccurs
and i n c r e a s e s with t h e s e v e r i t y o f hydrogen c h a r g i n g c o n d i t i o n . QH p r i o rt o
hydrogen c h a r g i n g i s measureda t
520°C t o be a b o u t 5 ppm f o rt
= 1 . 6m
and a b o u t 1 0 ppm f o r t = 0.8nun,
and i s duet o
quenching t h e a l l o y from 535°C i n c o l d water.F i g u r e 2 shows t h e v a r i a t i o n of t h e y i e l d s t r e n g t h
Re
a s a f u n c t i o n o f hydrogen c h a r g i n g t i m e i n t h e molten s a l t s bath a t f r e e p o t e n t i a l and a t -3V/Ag, and a s a f u n c t i o n o f a g e i n g time when t h e ageing t r e a t m e n t i s achieved i n t h e f u r n a c e with o r w i t h o u t vacuum. The y i e l d s t r e n g t his
independent on t h e a g e i n g t i m e and on t h e c a t h o d i c p o t e n t i a l l e v e l and dxceeds t h o s e duet o
a g e i n g h e a t t r e a t m e n t i n f u r n a c e d u r i n g v a r i o u s t i m e s ; t h e i rRe
a c h i e v e s a maximum f o r 15 h r ageing.Maximum t e n s i l e s t r e n g t h Rm v a r i a t i o n a s a f u n c t i o n of a g e i n g t i m e i s very s e n s i t i v e t o t h e ageing h e a t t r e a t m e n t c o n d i t i o n , f i g u r e 3 . However, Rm v a l u e s measured i n t h e molten s a l t s b a t h a r e higher t h a n t h a t o b t a i n e d when u s i n g t h e f u r n a c e t o a c h i e v e t h e ageing h e a t t r e a t m e n t . Independently o f t h e h e a t t r e a t m e n t c o n d i t i o n , t h e maximum
stress
Rm i s a l s o maximum f o r 1 5 h r ageing.D u c t i l i t y l o s s
F
% due t o hydrogen c h a r g i n g i s a b o u t 20% f o r a g e i n g t i m e v a r y i n g f r o m l O t o 2 0 h r , f i g u r e 4 . % d r a s t i c a l l y i n c r e a s e s u p t o 75% f o r a 30 h r a g e i n g time.2 ) Gaseous hydrogen c h a r g i n g
For a1 1
test
c o n d i t i o n s , t h e d i s k s c e n t r a l p a r t (under p r e s s u r e ) b r e a k s i n t o numerous 1 i t t l e p i e c e s , f i g u r e 5 , i n d i c a t i n g t h e m a t e r i a l b r i t t l e c o n d i t i o n .we
have t o remember t h a t t h e r e t a i n e d QH p r i o r gaseous hydrogen c h a r g i n g was measured t o be a b o u t 1 0 ppm. P a r t l y f o r t h i s r e a s o n and c e r t a i n l y duet o
t h e e f f e c t i v e n e s s o f s u r f a c e o x i d e s , no s i g n i f i c a n t e m b r i t t l i n g e f f e c t o f hydrogen could be evidenced, f i g u r e 6 .DISCUSSION
The results show that we have introduced high concentrations of hydrogen in A1 -Li alloy by using the molten s a l t s b a t h technique a t the optimum ageing temperature. To the best of our knowledge, no attempt has been done t o measure the hydrogen diffusion coefficient DH in A1-Li alloys
a t
190°C. However, NAKASHIMA and coll. (13) have measured DH in binary A1-Li system as a function of Li percentage and of temperature. Their results show great scattering and DH is
estimatedas
about 1o - ~
cm2. s-1 in the temperature range 1 80t o
480°C, i ndependentl y of Li%. I n our conditions, hydrogenmay
diffusea t
a distance d from the surface of the metal equal t o about 85 t o 150pm
for charging time vary'ing from 10 t o 30 h r respectively and according t o t h e relation : d 5.
That i s t o say hydrogen may diffuse up t o or behind lithium depletion zone (14) ( S 100pm),
which i s far beyond the oxide thickness (032pm)
(14).
As mentionned above, S1 phase i s initiated on dislocations sites. Knowing that internal hydrogen promotes dislocations density (1 5, 1 6 ) , the probabil i ty of S' formation i s then more important in the presence of hydrogen than without hydrogen. Tensile stresses are increased when the A1 -Li a1 loy i s cathodical ly hydrogen charged. This increase does depend on hydrogen concentration, namely the polarisqtion time a t 190°C. Table I1 gives the percentage increase in t e n s i l e properties due
t o
hydrogen charging for two durations 15 and 30 h r . The reference alloy i s taken as t h a t heat treated in furnace under vacuum.Table I I : Relative variation in the mechanical properties due to time of hydrogen charging (ageing time) a t -3.0 V/Ag.
...
I t, hr I
A Re%I
A R ~ %I
F%*I
1----_--1__---_--_1---I--- I
1 1 5 1 6 1 5 1 2 3
1
\
301
1151
191
751
The effect of internal hydrogen on the mechanical properties i s very important when the alloy i s in an overaged condition (190°C, 30 hr).klithout internal hydrogen and ageing heat treatment, the fai 1 ure surfaces show ductile rupture with f l a t surfaces containing s l i p lines, figure 7a. Figure 7b
shows
t h a twhen
the alloy i s aged heat treatmenta t
190°C during 30 hr in theC3-592 JOURNAL DE PHYSIQUE
f u r n a c e under vacuum,
a
mixed r u p t u r e t y p e o c c u r s . Deep c r a c k s i n t h e s u b - g r a i n b o u n d a r i e s and many t e a r i n g s t h r o u g h o u t t h e m a t r i x a r e observed.T h i s r e s u l t p o i n t s o u t t h a t c o a r s e d
6'
p a r t i c l e s ( 8 ) and S ' p h a s e w i t h i n t h e m a t r i x ( 9 ) and a l s o , S ' ( ~ 1 2CuMg) ( 9 ) , T2 ( A 1 2 C u ~ i ) ( 1 7) and A16(Fe, Cu) ( 1 8 ) p a r t i c l e s may b e p r e s e n t i n t h e sub-grain boundaries. With i n t e r n a l hydrogen and a t 500pm
from t h e s u r f a c e , t h e r u p t u r e t y p e changes from i n t e r g r a n u l a r (10 h r ) t o mixed ( i n t e r+
t r a n s c r i s t a l l i n e ) (1 5 and 2 0 h r ) and f i n a l l y becomes i n t e r g r a n u l a r ( 3 0 h r ) , f i g u r e 8. However, a t 100pm
from t h e s u r f a c e , t h e f a i l u r e h a s an i n t e r g r a n u l a r f e a t u r e , i n d e p e n d e n t l y o f t i m e of ageing. The l a s t r e s u l t s prove t h a t hydrogen has d i f f u s e d and e m b r i t t l e d t h e metal a t a d i s t a n c e e q u a l t o o r g r e a t e r than 100pm
from t h e m e t a l l i c s u r f a c e . The s u r f a c e o x i d e s i s t h e n overcome d u r i n g c a t h o d i c c h a r g i n g i n molten s a l t s b a t h . T h i s i snot
t h e c a s e w h i l e gaseous hydrogen charging. However t h e r e s t r i c t e d number o f d i s k s l e f t a v a i l a b l e d i d n o t allow t h e n e c e s s a r y i n v e s t i g a t i o n o f t h e p r e s s u r e i n c r e a s e r a t e i n f l u e n c e . T h e r e f o r e , t h e s c a r c etests
on d i s k s hydrogen charged by t h i s t e c h n i q u e a r e i n c o n c l u s i v e b u t oughtt o
b e resumedmore
c o n s i s t e n t l y,
e s p e c i a l 1 y w i t h t h i c k e r d i s k s .CONCLUSION
I n t h i s work
we
have i n v e s t i g a t e d t h e hydrogen e r n b r i t t l e m e n t o f an A1-Li a1 l o y (8090). The r e s u l t s o b t a i n e d l e a d t o t h e f o l l o w i n g c o n c l u s i o n s :1 ) Using t h e molten s a l t s b a t h t e c h n i q u e and c a t h o d i c a l l y hydrogen c h a r g e d t h e 8090
-
T351 a1 l o y a t t h e peak t e m p e r a t u r e (1 90°C). The outgased q u a n t i t y of hydrogen i s an i n c r e a s i n g f u n c t i o nas
t h e t i m e of c h a r g i n g ( a g e i n g t i m e ) and c a t h o d i c p o t e n t i a l l e v e l i n c r e a s e . Molecular hydrogen t r a p p i n g i s p o i n t e d out.2) Hydrogen may promote d i s l o c a t i o n s d e n s i t y which a r e t h e i n i t i a t i o n s i t e s o f S ' phase. T e n s i l e
stresses
and d u c t i l i t y l o s s a r e t h e n i n c r e a s e d . The e f f e c t of hydrogen i s i m p o r t a n t when t h e a l l o y i s i n t h e overaged c o n d i t i o n .3 ) Hydrogen promotes a l s o i n t e r g r a n u l a r f a i l u r e , e s p e c i a l 1 y i n t h e overaged c o n d i t i o n . P r e c i p i t a t i o n o f S ' , T2 and A16(Fe, Cu) p a r t i c i e s i n t h e s u b - g r a i n b o u n d a r i e s may i n t e r a c t w i t h hydrogen atoms and t h e embri t t l e m e n t i
s
favoured.REFERENCES
( 1 ) 5. NOBLE, G.E. THOMSON
-
Metal S c i . J. 5, 114, (1 971).( 2 ) T.H. SANDERS, E.A. STARKE
-
Acta M e t a l l . 30, 927, (1982).( 3 ) 8. NgBLE, S.J. HARRIS, K . DINSDALE
-
Metal S c i . J . 16, 425, (1982).(4) T.H. SANDERS
-
Proc. 1 s t I n t . A1-Li Conf., p. 63, M e t a l l . Soc. AIME, (1981).(5) H.M. FLOWER, P.J. GREGSON, C.N.J. TITE, A.K. MUKHOPADHYAY
-
P ~ o c . Al-A1 loys, t h e i r physical and mechanical p r o p e r t i e s-
E d i t o r s E.A. STARKE J r and T.H. SANDERS J r , U n i v e r s i t y o f V i r g i n i a , C h a r l o t t e s v i l l e , USA, June (1986), p . 743.( 6 ) I.M. LIFSHITZ, V.V. SLYOZOV
-
J. Phys. Chem. S o l i d s , 19, 35, (1961).(7) K. DINSDALE, S.J. HARRIS, B. NOBLE
-
I b i d . 4, p. 101.(8) P.J.E. BISCHLER, J.W. MARTIN
-
I b i d . 5, p. 963.(9) S.J. HARRIS, B. NOBLE, K. DINSDALE, M. PRIDHAM
-
I b i d . 5, p. 755.(10) G.M. SCAMANS - Proc. Hydrogen E f f e c t s i n Metals, e d i t e d by I.M. BERNSTEIN and A.W. THOMPSON, The M e t a l l . Soc. o f AIME, Carnegie-Mellon U n i v e r s i t y , PIH, PENNSYLVANIA (1980), p. 467.
( 1 1 ) A. ELKHOLY, J. GALLAND, P. AZOU, P. BASTIEN
-
C.R. Acad. Sci., 284, s 6 r i e C, (1977), p. 363.(12) J.P. FIDELLE
-
"Hydrogen embrittlement t e s t i n g " ASTM STP 543, 31 (1974), p. 243.(13) M. NAKASHIMA, M. SAEKI, Y. ARATONO, E. TACHIKAWA
-
Journal o f Nuclear M a t e r i a l s , 116, (1983), p. 141.(14) F. DEEREVE, Ph. MEYER, N. THORNE
-
Pertes en 1 i t h i u m des a l l i a g e s A1-Li-X, Rapport i n t e r n e de PECHINEY, mars ( 1 986).(15) J. EASTMAN, T. MATSUMOTO, N. NARITA, F. HEUBAUM, H.K. BIRNBAUM
-
Conf.Proc. on "Hydrogen i n Metals" E d i t e d by I. M. BERNSTEIN, A.W. THOMPSON Carnegie
-
Me1 l o n U n i v e r s i t y , P i t t s b u r g h , Pennsylvania, U.S.A. (1980), p. 397.(16) K.S. SHIN, C.G. PARK, M. MESH11
-
I b i d 15, p.209.( I T ) F.S. LIN, S.B. CHAKRABORTTY, E.A. STARKE J r
-
Met. Trans. 13A (1982), p. 401.(18) N.J. OWEN, D.J. FIELD, E.P. BUTLER
-
I b i d . 4, p. 1217.JOURNAL DE PHYSIQUE
Figure 1 : V a r i a t i o n of Q 5 2 0 ' ~ and 1000
B
C desorded a t as a f u n c t i o n of c a t h o d i c p o t e n t i a l l e v e l and of hydrogen charging (ageing time) ; hydrogen charging temperature = 19O0C.0 1151 (0lDITlOl DLIW sun ur* s I, 11w~cl + mna sun urn AT -1 114 (1W.O
.
N U T S "1- .IW 1I)O.O0 ,mu([ "IT"ILY(IWC1
I , h r
F i g u r e 3 : V a r i a t i o n of maximum t r u e s t r e s s a s a f u n c t i o n of e i t h e r t h e hydrogen charging time ( w i t h and w i t h o u t c a t h o d i c p o l a r i z a t i o n ) o r a g e i n g time : peak temperature = 190°C.
t . h r
Figure 2 : V a r i a t i o n of y i e l d s t r e n g t h a s a f u n c t i o n of e i t h e r t h e hydrogen charging time (with and without c a t h o d i c p o l a r i z a t i o n ) o r ageing time ; peak temperature = 190°C.
Figure 4 : V a r i a t i o n of maximum s t r a i n a s a f u n c t i o n of e i t h e r t h e hydrogen charging time (with and without c a t h o d i c p o l a r i z a t i o n ) o r ageing time ; peak temperature = 190°C.
F i g u r e 5 : View of a d i s k f a i l u r e by i n c r e a s i n g hydrogen gas- 1 p r e s s u r e a t 0.1 MPa.min
.
1
F i g u r e 6 : Disk f a i l u r e p r e s s u r e of hydrogen o r helium gas v e r s u s t h e f a t e of i n c r e a s i n g of t h e g a s and of p r i o r i n t e r n a l hydrogen c h a r g i n g : i s t s e r i e s c o r r e s p o n d s t o n a t u r a l a g e i n g u n t i l 1985, 2nd s e r i e s c o r r e s p o n d s t o n a t u r a l a g e i n g u n t i l 1986.
F i g u r e 7a : S u r f a c e f a i l u r e b y t e n s i l e Figure 7b : Surface failure by tensile t e s t a t room t e m p e r a t u r e o f t e s t a t room t e m p e r a t u r e of 8090-~351 a l l o y . 8090 a l l o y aged a t 190°C
d u r i n g 30 h r .
JOURNAL DE PHYSIQUE H CHARGING T I M E ( - 3 V / A g , 1 9 0 ° C )
F i g u r e 8 : V a r i a t i o n of t h e t y p e of r u p t u r e i n 8090 a l l o y c a t h o d i c a l l y h y d r o g e n a t e d
(-3V/Ag) a s a f u n c t i o n of lo hr time of h y d r o g e n a t i o n
and t h e d e p t h from t h e specimen s u r f a c e ; peak t e m p e r a t u r e = 190°c.