Computer simulation of spherical crystal surfaces: Defects in hexagonal lattices

Computer simulation of spherical crystal surfaces: Defects in hexagonal lattices

SURFACE SCIENCE 14 (1969) 423-430 0 North-Holland Publishing Co., Amsterdam COMPUTER SIMULATION OF SPHERICAL CRYSTAL SURFACES: DEFECTS IN HEXAGONAL...

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SURFACE

SCIENCE 14 (1969) 423-430 0 North-Holland

Publishing Co., Amsterdam

COMPUTER SIMULATION OF SPHERICAL CRYSTAL SURFACES: DEFECTS IN HEXAGONAL LATTICES A. J. PERRY * Battelle Institute, Advanced Studies Center, Geneva, ~wit~er~a~ and D. G. BRANDON Department of Materials Engineering, The Technion, Haifa, lsrael Received 13 August 1968 Previous work on field-ion image simulation of lattice defects in cubic crystal+-5) using the thin shell mode16) has now been extended to the hexagonal case by substituting the atom positions appropriate to a hexagonal metal (ruthenium). By modifying the ideas of Melmed and Ranganathan7-8), the order of prominence of the lattice planes and the multiplicity of dislocation spirals can be accounted for in terms of the relative distances between A and B layers in the lattice. Satisfactory simulations has been achieved for dislocations, dislocation loops and dipoles, and partial dislocations and stacking faults. A program has also been written for twinned crystals. 1. Introduction

In previous workl-5) computer methods have been developed for simulating field-ion images of lattice defects in f.c.c. and b.c.c. metals. The programs so far written have covered unit lattice dislocations, dislocation loops and dipoles and stacking fault ribbons, and the present paper reports a further extension of these same programs and their application to the case of hexagonal metals. As in the authors’ previous calculations, the thin shell models) is used but now with the lattice positions and displacement vectors appropriate to the hexagonal unit cell. 2.

Method of

calcuiation

The previously described programs for the cubic system were adapted to the hexagonal case by writing the displacement vectors and the lattice positions for the hexagonal lattice in terms of orthogonal axes with the following orientation relation: co~~lo~~~~~~l~~ wiom~~~~H. * Present address: Brown Boveri Research Center, 5401 Baden, Switzerland. 423

A.J.PERRY

424

The Miller-Bravais the

3-index

identical W’=(c/a)

form:

vector

indices ti=l[-t,

in the

W, where

the

AND

of a vector V=D-t.

orthogonal unit

D.G.BRANDON

[u u t II.] were first converted

W=H’, system:

of distance

then

transformed

into

U’= - i U+ V. V’= -, in the

system is a. Similarly the normal to any plane whose (/? k il) was expressed in terms of the computer

orthogonal

to the j 17,

coordinate

Miller-Bravais indices are orthogonal cell by: h’=k,

I<’= - (2h + k)/,/3, I’ = (c/a, 1. Once the Miller-Bravais displacement vectors, lattice positions and lattice vectors had been converted into the orthogonal coordinate system, the atom displacement could be determined from the displacement equations given in previous publications. In all cases the value of c/u was taken as 1.582, appropriate to ruthenium. All calculations were programmed in Fortran for a CDC 6600 computer and the results were plotted, without rounding, on-line on a 565 Calcomp plotter. 3. Dislocations Melmed 7, and Ranganathan and Melmed s, have noted some of the peculiarities of the hexagonal lattice which arise from the two-valued interplanar spacing of many of the prominent lattice planes, and have proposed modifying the g -b criterion for predicting the multiplicity of the spiral generated by a dislocation in the hexagonal lattice. If the basal planes are labelled ABAB . . . . according to common practice, then for every lattice plane it is possible to determine the distance between neighbouring A planes, tiAA, in units of a, and to compare this with the shortest distance between an A and a B plane, dAAH.This has been done in table 1, using c/u= 1.582, and compared with the observed order of prominence of the lattice planes seen in published field-ion images of ruthenium7). The case dAjAB/dAA=Ocorresponds to a mixed AB plane, ciJdAAA=+ corresponds to equidistant A and B layers, while other values correspond to the rippled double layers discussed by Melmed’). It is these other values. dAAB/dAAA=+ or +, that correspond to two-valued interplanar spacings. It is not true to say that the simple g -b rule is invalid for the hexagonal lattice, rather the value of g must be correctly chosen so that lg/= I/C/~,. Then g .b will give the correct multiplicity for dAB/dAA=O and one half of the correct multiplicity for u’AB/d AA=+ (compare the order observed in table 1). However, if CjAB/dAA=+ or 4, then the effect is not just to double the multiplicity (as stated by Ranganathan and Melmeds)) but rather to generate sets of “tramlines”. The condition for visibility of the tramlines is determined by the shell thickness, and is simply the condition that succes-

425

sive A and B layers should not overlap in the thin shell. Separation of the tramlines cannot be observed if pOdAB, then the tramlines will be visible near the pole of the prominent planes, but will fade out at an angle 8 from the pole, corresponding to the point

at which p,, = dAB cos 8. TABLE 1

Order of importance (hk.1)

d&a

Oool lOT0 1011 loi

1.582 0.866 0.759 0.583 0.500 0.477 0.450 0.423 0.418 0.363 0.359 0.334 0.321 0.310 0.302

1120 1121 loi

1122 2021 1123 loi

2023 2151 1124 2132

of crystal planes d&d&t

Observed order 1 2 3 5 4 12 7 6 8 14 not observed 9 10 11 13

dnA values from 2/3 2~;

a

= 2/ [h2 + hk + k2 + 3 (a/c) PI,

using c/a = 1.582 ($(a/c)z = 0.300).

The slip dislocation commonly found in hexagonal crystals is 3 (1120) (type a) but two other unit lattice dislocations are also observed: (0001) (type c) and +( 1123) (type ~+a). Fig. 1 illustrates the variety of contrast that may be obtained: In fig. la a dislocation of Burgers’ vector +[2iiO] has been allowed to emerge on the (1120) plane to generate a single fold spiral (g - b = 1, dAB/dAA= =O). In fig. lb the same dislocation emerges on the (IOiO) plane (g -b= 1, dAB/dAA=+) and a pair of tramlines is visible over most of the single spiral. -In fig. lc a $[1213] dislocation is seen emerging on the (0001) plane (g-b= 1, dAB/dAA =+) and the doubling of the single spiral as a result of the intermediate B layer is seen. 4. Dislocation loops and dipoles The calculation

for loops

and

dipoles

is straightforward

and

follows

425

A.J.PEKKY

immediately

from the considerations

AND

D.G.

DKANDON

given above

for dislocations

and the

previous calculation for the cubic cases). Fig. 2a shows an example of a dipole centred on the (0001) planes with dislocation axes on the hypothetical (liO9)

poles.

The Burgers

:. . .. I.

vector

:’

**f’

.__

.

.

*

* .

:

I: . ; .. . . . : . .

1

. .

I

.

::

..

“,.

.I

.

-*

** *.

*.. : .

::.

*

.

:

.

.- .*. ** -.. --. **a ...* .. **. * ::* . . . a.. . . .. . ‘.. .

*.

. .; *:, a... ‘+ .. ‘*;* *.. .

:

and this

*

::

.. ..

1, ~/~a/~~~=$)

*--. .*.** _* .*

::

is [OOOl] (g-b=

I

.

. .*

*.*

. . . *: .. . * *

. .

.

-.

:.

.

:* :

:

-

-

-.

Fig. 1. Dislocation of Burger’s vector 4 [ZfiO] emerging on (a) the (I 120) plane (~-6 1, c/~~~]~.~A -- 0) and (b) the (lOi0) plane (S./I -- I, d.ttl/d,t,, -f).(c) A :,[f2i31 dislocation emerging on the (0001) plane (g.15 I, n’,\lr/dlt-\ 4). Tip radius 143~ in all cases.

case obeys the rule given by Ranganathan and Melmeds). In fig. 2b a slightly more complicated case is shown: the Burgers vector is +[1210] and the exit pole (i103) (g*b= I, rt;z,/~AA=&). In this case the tramlines are invisible and the (il03) planes are rippled and not separated into A and B layers (y. >dAa and the layers overlap in the image), In practice it is often more convenient to treat dislocation loops and dipoles as a special case of a multiple dislocation array. The computed

COMPUTER

centre of the simulated of the constituent

SIMULATION

OF SPHERICAL

CRYSTAL

image is then chosen independently

dislocations.

The displacements

421

SURFACES

of the exit poles

due to each dislocation

are then calculated separately and summed to yield the final atom positions in the dislocated crystal. This technique has been used to simulate actual arrays in f.c.c. crystals5).

Fig. 2. Dislocation dipoles: (a) Burgers’ vector [OOOl], emerging on (0001) planes. (g-b = 1, d_&dAA =+, tip radius 804. (b) Burgers’ vector +[T2iO], emerging on (1103) (g-b = 1, dAB/dAA= 4, tip radius 150~1).

5. Stacking faults Stacking faults can form on the basal plane of hexagonal crystals as the result of the dissociation of a glissile dislocation (+[i2iO]+$[OliO]+ ++[ilOO]) or by point defect condensation. Only the former case has been programmed, since the case of point defect condensation is effectively included in the program for loops and dipoles and is obtained by inserting the appropriate partial Burgers vector in the read-in. As in f.c.c. crystals, some care is needed in the identification of stacking fault ribbons because of the sensitivity of the contrast to the exact position and orientation of the line of intersection of the fault with the surface. Fig. 3 illustrates a case in point: a dislocation of Burgers vector 3 [i2iO] has dissociated into the two partials given above, b, =$z[01iO], b,=+a[ilOO] with a separation of 4~. The fault emerges on the (2114) plane, so that g - b, = 0, g ~6, = 1. The contrast from the undissociated dislocation, fig. 3a, is very little different from that from the dissociated ribbon, fig. 3b.

6. Twinning Twinning

is a major

deformation

mode

in hexagonal

crystals

and the

A. J. PERRY

428

identification

of twinned

materials. A program been written. In principle

structures

AND D. G. BRANDON

is therefore

for the simulation

it is possible

to simulate

of some importance

of twinned any boundary

crystals

in these

has therefore

by selecting

the centre

Fig. 3. Dissociation into a stacking fault ribbon: (a) Perfect dislocation of Burgers’ - 0). (b) The same disvector f-[1210] emerging on the (21 14) plane (g.h = 1, dl~~~/d.za location after dissociation into two partials on the basal plane. 3 [i2iO]~ ’ .\ [Ol TO] ‘m -I~+[ilOO] (g.bl0, g-62 I). Tip radius 150~1.

of the image for one grain, transforming to this axis in the second grain, and then running both cases and using a pair of scissors on the results. In actual fact twinning in the hexagonal lattice cannot readily be handled in this way. The basic problem is that the twin cannot be formed by simple shear - the atoms have to rearrange (“shuffle”). It follows that a twinning dislocation with a Burgers vector as defined by the twinned structure will not in fact translate the atoms into the final twinned positions. A secondary problem, not usually considered, is that a lattice twin and a crystallographic twin are not necessarily the same thing. A crystallographic twin is formed when crystal planes and directions in the two grains are twin-related, but a lattice twin requires that each atom in the matrix lattice should find a corresponding atom position in the twinned lattice. In hexagonal crystals this is almost certainly not the case, the minimum twin boundary energy corresponding instead to a matrix lattice, ABAB . . . . being “twinned” into the lattice positions, BCBC . . . or CACA . . I. In other words the twinned lattice may be displaced bodily by the lattice vector +( IiOO). There are three possible ways of simulating the twinned structure: a) shear and shuffle; b) a rotation based on the coincidence or O-lattice transformationg);

COllPPUTER

SI~LATION

OF SPHERlCAL

CRYSTAL

SURFACES

429

c) a mirror reflection in the composition plane, plus a lattice displacement if necessary. The last is the easiest to program, but has the disadvantage that effects associated with the growth of the twin cannot be simulated. That is, the twin boundary is constrained to be coherent and twinning dislocations are not present. A particular composition plane defined by the direction cosines lmn in the computer orthogonal axes, is constrained to pass through the pole on the surface with direction cosines pqr in a crystal of radius R. An atom at t is then reflected to the twinned lattice position ,F, given by F==t+2[R(Ep+mq+nr

-t*n]n,

where n is the normalized vector [pqr]. The thin shell test is then performed on each reflected atom and the results centred on any convenient pole. The extension to a displaced lattice only requires substituting F’= F-4- 6, where b is the lattice displacement vector. For c/a< I .633, (lOi2) and (11%) are possible composition planes. Fig. 4a

Fig. 4. Coherent twin boundaries passing through the (i01.5) plane. (a) (1012) composition plane, twinning direction [Toll]; (b) (1122) composition plane, twinning direction [TT23].

shows (lOi2) twin boundary emerging on the (iOl5) plane while fig. 4b shows a (I 122) twin boundary emerging on the same plane. In fig. 4a the twinning direction is tangential to the exit plane. 7. Discussion There appears to be no limit to the possibilities of computer simulation for field-ion images of lattice defects although the application of these

430

A. J. PERRY

techniques

to actual

AND

experimental

D. G. BRANDON

results

is not so simple.

The extension

of previous work on cubic metals to the case of the hexagonal lattice has revealed some interesting features but is in the main straightforward. Most of the peculiarities

of the hexagonal

lattice are connected

with the spacing

of alternate A and B layers, with dAB/d,4A=0, $, $: or -f depending on g. For dAB/dA,#O the multiplicity of dislocation spirals may be doubled or tramlines may appear. The condition for invisibility of the tramlines is just dA,
8. Conclusions I) Dislocations, dislocation loops and dipoles, stacking fault ribbons and coherent twin boundaries have been successfuhy simulated in the hexagonal close packed lattice. 2) The effect of the hexagonal close packing on the g 6 criterion for dislocation spirals has been reconsidered and the conclusions of Ranganathan and Melmeds) modified accordingly. 3) The conditions for visibility of the above defects have been discussed within the framework of the thin shell model for defect lattices. l

References 1) 2) 3) 4) 5) 6) 7) 8) 9)

D. G. Brandon and A. J. Perry, Phil. Mag. 16 (1967) 131. A. J. Perry and D. G. Brandon, Phil. Mag. 17 (1968) 255. A. J. Perry and D. G. Brandon, Phil. Mag. (1968) to be published. R. C. Sanwald, S. Ranganathan and J. J. Hren, Appl. Phys. Letters 9 (1966) 393. R. C. Sanwald and J. J. Hren, Surface Sci. 9 (1968) 257. A. J. W. Moore, J. Phys. Chem. Solids 23 (1962) 907. A. J. Melmed, Surface Sci. 5 (1966) 359. S. Ranganathan and A. J. Melmed, Phil. Mag. 15 (1966) 1309. W. Bollman, Phil. Mag. 16 (1967) 363, 383.