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HAL Id: jpa-00222119

https://hal.archives-ouvertes.fr/jpa-00222119

Submitted on 1 Jan 1982

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STUDY OF FRACTURE IN Cu-Al-Ni SHAPE MEMORY BICRYSTALS

S. Miyazaki, Tadashi Kawai, K. Otsuka

To cite this version:

S. Miyazaki, Tadashi Kawai, K. Otsuka. STUDY OF FRACTURE IN Cu-Al-Ni SHAPE MEMORY BICRYSTALS. Journal de Physique Colloques, 1982, 43 (C4), pp.C4-813-C4-818.

�10.1051/jphyscol:19824133�. �jpa-00222119�

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S T U D Y O F F R A C T U R E I N C u - A i - N i S H A P E MEMORY B I C R Y S T A L S

S. M i y a z a k i , T. Kawai and K. Otsuka

I n s t i t u t e of Materials Science, University of Tsukuba, Sakura-mura, Ibaraki- ken 305, Japan

(Accepted 9 August 1982)

Abstract.

-

The intergranular fracture in Cu-based shape memory alloys is most hazardous for the application of these alloys. In order to clarify the cause of the fracture, the fracture behavior of severaI Cu-Al-Ni bicrystals with different orientation relationships have been examined by tensile tests.

From these results, it has been shown that the cause of the intergranular fracture lies in the stress concentration a t grain boundaries due to the large elastic anisotropy and/or due to the difference in transformation strain a t the boundaries.

Introduction. - Among many shape memory alloys, Cu-based !3 phase alloys are receiving most attention for commercial use because of reasons of economy. A se- rious problem in applying these alloys, however, is that the fracture stress and ductility of these alloys are low in the polycrystalline state because of their inter- granular fracture. This brittleness was once suggested to be due to the large elastic anisotropy of !3 phase alloys (1,2). More recently the present authors re- ported that it would be the case, based on the result of the tensile tests of a few Cu-Al-Ni bicrystals ( 3 ) . In order to justify the above proposition and to investi- gate another cause of the intergranular fracture of these alloys, the fracture be- havior of other bicrystals with different orientation relationships have also been examined in the present study.

Experimegtal Procedure and Some Preliminary Considerations.

-

( Specimens and tensile tests ) The ingots of Cu-14.6A1-4.ONi(wt%) and Cu-14.2A1-4.ONi(wt%) alloys in nominal composition were prepared from 99.99%Cu, 99.99%Al and 99.9Wi by melt- ing in a high frequency induction furnace followed by casting into an iron mold.

The details of the specimen preparation have been reported elsewhere ( 3 ) . The gauge length, width and thickness of the specimens were 5 mm, 2 . 5 mm and 1.5 mm, re- spectively. ( See Fig. I of Ref. (3) .) The tensile tests were carried out a t a strain rate of 3.3~10-41s on an Instron-type tensile machine, Shimadzu Autograph DSS-1OT -S type. The temperature during the tests were controlled by immersing specimens in either methanol cooled by liquid nitrogen or heated oil.

( Orientations of bicrystals and considerations of strain compatibility a t a grain boundary ) I t was suggested in the previous paper that s t r e s s concentration a t grain boundaries played an important role in both the initiation and propagation of cracks in polycrystalline Cu-based shape memory alloys ( 2 ) . The stress concen- tration occurs at a grain boundary in order to make the strain components in each crystals compatible. Two types of strains are important in shape memory alloys, i.e. the elastic strain and the transformation strain. Preliminary considerations of the compatibility of these strains at the grain boundary is given in the following.

Each specimen used in this investigation has a grain boundary in the central portion, vertical to the tensiIe axis. The geometry of the bicrystals is shown in Fig. 1. For type of bicrystal shown in Fig. 1 , the continuity of strain across the

Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphyscol:19824133

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JOURNAL DE PHYSIQUE

XY grain boundary is represented by the follow- ing relationships (4.5) :

A - B A B A B

E ~ ~ - E x x ' E ~ ~ =

Eyy9EXy= & X Y (1) Here the strain components on both sides repre- sent the deformation of the boundary plane of the component crystals A and B respectively.

When both crystals a r e in the elastic range, the degree of incompatibility a t the boundary may be expressed conventionally by differences in the corresponding strain components as shown in the following :

A' c B -

I

= IExx

- x x

Surface

where the strain components E A' A' A '

X X ' ~ Y Y ' E X Y

and ~ i g . 1 Geometry o f b i c r y s t a l s

B ' B' B ' u s e d i n t h e p r e s e n t

cX X ,

5 ,

, c X

,

represent the elastic strains of t e n s i l e t e s t s . the component crystals A and B , when they are

deformed independently of each other a s single crystals. In order to satisfy E q . 1 , the s t r e s s concentration is introduced at the grain boundary according to the value of these strain differences ( A c X X , A cy and A cX ) , which increase with increasing elastic anisotropy of the component crystals. In an isotropic material, the strain differences at a grain boundary are obviously zero, so that stress concentration is absent a t the boundary. In a highly anisotropic material, such as a Cu-Al-Ni alloy, the s t r e s s concentration is present a t the grain boundary and the degree can be varied over a wide range by changing the relative orientations of the two component crystals. Therefore, it will be possible to s'how clearly the effect of the s t r e s s concentration a t a grain boundary on the intergranular fracture, by utilizing bi- crystals with various relative orientations.

When martensites are stress-induced, the transformation strain must also sat- isfy the compatibility condition of E q . 1, if deformation proceeds without fracture.

The transformation strain strongly depends on crystal orientation, and thus large stress concentrations may be induced a t the grain boundary due to large differences in transformation strains in both component crystals (6)%(8).

Two kinds of bicrystal groups were used in this investigation. One type is a symmetric bicrystal, in which both component crystals ( A and B ) are oriented symmetrically with respect to the XY grain boundary plane and the tensile axis in each crystal is inclined a t an angle of 10 or 20 degrees from a <001> direction.

Other types of bicrystals are random bicrystals, in which the component crystals are situated in random orientation to each other. All the tensile axis and the top sur- faces of both component crystals A and B are shown in Table 1.

T a b l e 1 O r i e n t a t i o n s of t e n s i l e a x e s and t o p s u r f a c e s of b o t h component c r y s t a l s A and B.

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Thus stress concentration occurs a t grain boundaries due to elastic anisotropy during elastic deformation. For a highly anisotropic material such as a Cu-Al-Ni alloy ( i.e. A = 2c44/( c - c 1 2 )

-

13 (9) ) , large and complex stress concentra- tion is required to make

21

stram differences simultaneously zero in Eq. 2. If no deformation mode is available a t low stress levels in such a case, the stress con- centration at the grain boundary becomes large enough to reach the fracture s t r e s s during elastic deformation at least macroscopically. Figure 2 shows the stress-strain curves in such a case. The curves (a) and (b) a r e those of random bicrystals ( 2 ) and (3) ( from here called RANDOM 2 and 3 ) , respectively, in which the strain differences defined by Eq. 2 are not zero. The fracture occurred along grain boundaries during elastic deformation in these bicrystals and the fracture stresses were only about 100MPa and about 150MPa. respectively. On the other hand RANDOM I , in which the strain difference in E q . 2 is the largest of all bicrystals used in this investigation, showed intergranular fracture during quenching. The cause of the intergranular fracture in this case is considered to be due to the stress concentration a t the grain boundary introduced by the thermal strain gradient from the specimen surface to the interior during quenching. The results of RANDOM 1

Q, 3 are consistent with the idea that the intergranular fracture is the result of high stress concentration at the grain boundary due to the large elastic anisotropy.

If the cause of the intergranular fracture i s the stress concentration due to elastic anisotropy alone, a bicrystal without stress concentration due to such an effect would not fracture during elastic deformation. This can be tested by utilizing RANDOM 4, in which all three components of the elastic strain differences defined by E q . 2 are simultaneously zero, b u t the transformation strains differ in the two component crystals. The stress-strain curve in this case is shown in Fig. 2 ( c ) , where fracture does not occur in the elastic region, b u t does after transformation at a stress level of about 300MPa. The fracture in this case was an intergranular one. In order to clarify the cause of the intergranular fracture in this case, the same type of bicrystals with different compositions were tested at various tempera- t u r e s , as shown in Fig. 3. Fracture does not occur during elastic deformation at any deformation temperature. The fracture stress is about the same as the critical stress for inducing

martensites in curves (a) and ( b ) . At higher temperature in (c) where martensites can not be induced by an

applied s t r e s s , the

- Fx

specimen deformed a

large amount by slip 200

i

( c ) RANDOM 4

prior to fracture and

- 1

(b) RANDOM 3 Elast. compatible Elart. incompatible

the tensile strength V) Ms = 198K

V) Ms = 236K

was about 6OOMPa. Z ( a ) RANDOM 2 The value of the ten- ;i Elast. incompatible

5

sile strength i s al- M~ = 2 0 3 ~ most the same as that

&oo}/

/

in a single crystal, as shown later. At tem- peratures lower than

Ms , deformation modes Cu-14.6A1-4.ONi

(wt%)

such as twinning are 0.5 %

available at low stress -.

levels. Thus, a large 0 0 0

strain is attained be: Strain (%)

fore fracture a s shown

by the curve ( d l , Fig. 2 The stress-strain curves of random bicrystals since the s t r e s s a t the deformed at room temperature. The mark (X)

indicates the fracture points.

grain boundary is easily relaxed by these

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JOURNAL DE PHYSIQUE

and lor -due to the difference in transformation strains at the grain boundary, a symmet- ric bicrystal would deform like a single crystal. In the sym- metric bicrystal (1) ( from here called SYMMETRIC 1 ) martensites were stress- induced at the shoulder of the specimen and no martensite formed a t the grain boundary at the initial stage of yielding ( 3 ) . This is a clear indication that stress concentration is absent at the grain boundary, as confirmed by a calculation of the strain differences defined by Eq. 2. The stress-strain curves of SYMMETRIC 1 and 2 are shown in Fig. 4.

SYMMETRIC 1, for example, was loaded to more than 600 MPa until fracture occured.

The behavior is essentially the same as that of a single crystal which has the same orientation with one component

deformation modes nearly

Y

I I 1

0 10 20 30

Strain (%I until the variants are re-

arranged to only one pre- ferred variant in each

component crystal of the 600- bicrystal. Fracture

-

finally occurs at the

2

grain boundary due to

the difference of trans-

$

400- formation strains. From

these results, it is clear that the cause of the '4 intergranular fracture F zoo- in RANDOM 4 is the

stress concentration at the boundary due to the incompatibility of trans-

0

Fig. 4 The stress-strain curves of symmetric bicrystals 1 and 2 (in solid line) and that of a single crvstal (in broken line) deformed at room temperature.

The mark ( X ) indicates the fracture point. The Ms and test temperatures of the bicrystals were 197K and 294K, while those of the single crystal were

193K and 296K, respectively.

crystal of the bicrystal, as

indicated by a dotted line in Fig. 4. A clear transgranular fracture was observed in both SYMMETRIC 1 and 2. The fracture stresses of the two bicrystals are quite different. This tendency is essentially the same as that for single crystals, in which the fracture stress has a strong orientation dependence. The above facts are clear evidence to show that intergranular fracture in the Cu-Al-Ni alloy is caused by the brittleness of the boundary itself due to the presence of a secondary phase.

formation strains. Strain 96)

( Case of symmetric Fig. 3 Effect of composition and deformation temper- bicrystals ) As mentioned ature on the stress-strain curves in random in the previous section , bicrystal 4. ( Please note that the measure-

ment of plastic strains is not accurate, if the cause of the intergranular since the strains at the shoulder parts of fracture is the s t r e s s concentra- specimens outside of gauge length also con- tion at a grain boundary due to tribute to the total strain in the present

short tensile specimens. )

the large elastic anisotropv

(C)

R---x

(bl r x

(a)

x

-

3 X

0 0 0

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I N C O M P A T I B L E INCOMPATIBLE INCOMPATIBLE COMPATIBLE ( E L A S T I C S T R A I N ) (ELASTIC S T R A I N ) ( T R A N S F O R M A T I O N S T R A I N ) ( E L A S T I C STRAIN)

( T R A N S F O R M A T I O N STRAIN)

\1/

I

TRANSGRANULAR FRACTURE

Fig. 5 The shematic s t r e s s - s t r a i n curves and fracture modes i n Cu-Al-Ni b i c r y s t a l s .

Concluding Remarks. - According to the above investigations, t h e f r a c t u r e of Cu-Al-Ni shape memory alloys may b e classified into t h r e e types ( A, B and C a s shown in Fig. 5, depending upon the compatibility condition of t h e boundary,

Type A : T h e boundary i s elastically incompatible. T h e f r a c t u r e occurs in the elastic region ( a t least macroscopically ) along the grain boundary (RANDOM 2 and 3 ) . If the degree of incompatibility is very l a r g e , t h e f r a c t u r e occurs along the grain boundary during quenching, because of the large s t r e s s concentration a t t h e grain boundary due to large thermal gradient (RANDOM 1 ) .

Type B : The boundary is elastically compatible, b u t plastically incompatible.

The f r a c t u r e occurs along the qrain boundary after martensites a r e stress-induced.

T h u s the fracture occurs in the f i r s t stage of the stress-strain curve (RANDOM 4 ) . Type C : When a bicrystal i s symmetric , the boundary i s compatible both elastically and plastically*. Since no s t r e s s i s concentrated a t the boundary, fracture occurs i n a transgranular manner. In this case t h e deformation and f r a c t u r e behavior a r e essentially the same a s those of one of t h e component c r y s - tals ( SYMMETRIC 1 and 2 ) .

*

When martensites a r e stress-induced inhomogeneously at t h e boundary, other strain components E ~ E Z x , ~ ,E~ must also be continuous through the boundary in Eq. 1. I t is assumed in the present paper t h a t such conditions a r e satisfied by introducing other variants of martensites symmetrically to accomodate the incompatibility, if any.

From the results obtained in this investigation i t may be concluded that the cause of the intergranular fracture in the present alloy and other B phase alloys is s t r e s s concentration a t the grain boundaries due to t h e l a r g e elastic aniso- tropy a n d / o r due to the difference of transformation strains a t t h e grain boundaries, and not due to the brittleness of boundaries themselves due to the presence of a secondary phase. T h u s , from the above conclusionit i s suggested that t h e brit- tleness of Cu-based shape memory alloys may be improved by giving them a certain t e x t u r e to s u p p r e s s the s t r e s s concentration at grain boundaries. I t is also understood b y the above conclusion that one of the causes of ductility in the polycrystalline Ti-Ni alloy i s the small elastic anisotropy of this alloy ( A = 2

(10) QJ( 1 2 ) 1

.

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C4-818 JOURNAL DE PHYSIQUE

A c k n o w l e d g m e n t . - T h e a u t h o r s w o u l d l i k e t o e x p r e s s s i n c e r e a p p r e c i a t i o n t o P r o f e s s o r K . S h i m i z u a n d M r . H . S a k a m o t o a t O s a k a U n i v e r s i t y , a n d t o P r o f e s s o r J . T a k a m u r a a t K y o t o U n i v e r s i t y f o r u s e f u l d i s c u s s i o n s .

R e f e r e n c e s

( 1 ) M E L T 0 N . K . N . a n d M E R C I E R , O . , A c t a M e t . 27 (1979) 137.

( 2 ) MIYAZAKI , S . , O T S U K A , K . , SAKAMOTO , H . a n d S H I M I Z U , K . , T r a n s . J a p a n I n s t . M e t a l s 22 (1981) 244.

( 3 ) M I Y A Z A K I

,x,

KAWAI , T . a n d 0 T S U K A . K . . S c r i p t a M e t .

16

(1982) 431.

( 4 ) L I V I N G S T O N , J . D . a n d C H A L M E R S , B . , A c t a M e t . 5 (1957) 322.

(5) H O O K , R . E . a n d H I R T H , J . P . , A c t a M e t .

15

(19671-535, 1099.

( 6 ) O T S U K A , K . a n d S H I M I Z U . R . , T r a n s . J a p a n I n s t . M e t a l s

15

(1974) 103.

( 7 ) SAKAMOTO , H . , K I Z I M A , Y . a n d S H I M I Z U , K . , A n n u a l M e e t i n g o f t h e J a p a n I n s t . of M e t a l s ( 1 9 8 1 ) .

( 8 ) S A B U R 1 , T a n d N E N N O , S . , t o b e p u b l i s h e d in P r o c e e d i n g o f I n t e r n a t i o n a l C o n f e r e n c e o n S o l i d - s o l i d P h a s e T r a n s f o r m a t i o n s , P i t t s b u r g h , 1981.

( 9 ) SUEZAWA,M. a n d SUMINO , K . , S c r i p t a M e t .

10

(1976) 789.

( 1 0 ) M I Y A Z A K I , S . , O T S U K A , K . a n d S U Z U K I , Y . , S c r i p t a M e t .

15

(1981) 287.

( 1 1 ) MIYAZAKI , S . and O T S U K A , K . , S c i . R e p . R e s . I n s t . T o h o k u U n i v .

A29

S u p p l . 1 (1981) 111.

( 1 2 ) M E R C I E R , O . , M E L T O N , K . N . , GREMAND,G. a n d H A G I , J . , J . A v p l . P h y s . 51 (1980) 1833.

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