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HAL Id: jpa-00208882

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Submitted on 1 Jan 1979

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A new way of using positron-lifetime measurements to study lattice defects

Ch. Janot, B. George, M. Boidron

To cite this version:

Ch. Janot, B. George, M. Boidron. A new way of using positron-lifetime measurements to study lattice defects. Journal de Physique, 1979, 40 (1), pp.39-45. �10.1051/jphys:0197900400103900�. �jpa- 00208882�

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A

new way

of using positron-lifetime measurements

to

study lattice defects

Ch. Janot, B.

George

Laboratoire de Physique du Solide, Faculté des Sciences, C.O. 140, 54037 Nancy Cedex, France

and M. Boidron

Centre d’Etudes Nucléaires, B.P. 6, 92260 Fontenay aux Roses, France (Reçu le 26 juin 1978, accepté le 21 septembre 1978)

Résumé. 2014 Dans le but d’étendre les mesures de temps de vie des positons vers les hautes températures et d’éviter

les complications dues aux annihilations dans la source et à la surface de l’échantillon, des experiences ont été

réalisées à partir de sources intégrées où les isotopes émetteurs de positons sont à l’état d’impureté isolée dans le materiau étudié. Par ailleurs, on montre qu’il est possible, à partir des mesures de temps de vie, d’obtenir l’énergie

de formation des lacunes

EF1V,

sans être tributaire des imperfections du modèle du piégeage. On explique aussi

les correlations observées précédemment entre

EF1V

et la température Ti du point d’inflexion dans la courbe

03C4(1/T).

Abstract. 2014 With the aim of extending positron-lifetime measurements to high temperature and avoiding surface

and source contributions, experiments have been performed with positron emitting isotopes in a state of diluted

solid solution in the material investigated. Further, it has been shown that the positron-lifetime data can be used

in a new way to obtain the vacancy formation energy

EF1V

without the many uncertainties of the trapping model.

The previously observed linear correlation between

EF1V

and the inflection temperature Ti in the 03C4(1/T) curve

has also been explained.

Classification Phvsics Abstracts

61.70 - 78.70B

1. Introduction. - Since the

pioneering

work of

MacKenzie et al. [1] positron annihilation has become

a widely used tool for investigating the

properties

of

vacancies in metals in thermal

equilibrium.

The many

experimental

results that have been obtained and the many ways of

analysing

them have been extensively

presented

in a number of review papers [2]-[7].

1. 1. - Positron sources for lifetime measurements

were often

prepared by depositing

the source

isotope

(commonly 22Na in the form of sodium chloride)

either directly on a surface, or between thin

organic

(or metallic) foils sandwiched between two plates of

the material to be

investigated.

Measuring tempe-

ratures are then limited either by the

melting

point

or by the

evaporation

of the source material. The method has the extra disadvantage of a

relatively

large fraction of

positrons

annihilating either in the

source-supporting

material or at the

specimen

surface,

giving

rise to serious background

problems [8],

[9], [ 10]

and drastic limitations in the total activity that can be really used.

Integrated source-specimen

systems for

high temperature positron annihilation

experiments

have been recently

designed

[11]-[13]. In this so-called sealed-source

technique,

the source material ( N 10

uCi

of carrier-free

22NaCl)

is

hermetically

sealed between two discs of the material to be

investigated

which are

electron-beam welded under

high

vacuum.

Obviously,

this method has

proved

to be

quite

effective at

high

temperature and has brought some

improvements regarding

the parasitic

intensity

of the long-lived

source component. Limitations are, the still present surface component and a

possible

break of the weld under the vapour pressure of the source material [11], [14].

A technique

using

metal

specimens containing positron

source

isotopes

as bulk

impurities

is

presented

in this paper.

1.2. - Data on positron annihilation near ther-

mally generated vacancies in metals are conven-

tionally

analysed by a trapping model which is

generally recognized

to contain

questionable approxi-

mations and too many

adjustable

parameters [ 15], [16] ;

Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphys:0197900400103900

(3)

40

factors such as thermal expansion, temperature

depen-

dence of the

trapping

rate,

detrapping

mechanisms,

self-trapping

or

phonon-assisted trapping

[17], pre-

sence of other defects

(impurities,

dislocations...)

have influences that cannot be taken into account as

they should be. This usually

produces

values of the

monovacancy formation energy

E ;,

which are some-

what low when

compared

with results from established

techniques, or are not intemally consistent [18], [19], [3]. There is additional concern arising from the fact that for instance, data on Al can be

analysed

equally

well [20] in terms of a

temperature-independent

or a strongly

temperature-dependent Eiv

of the type

suggested

by Popovic et al. [21] ; moreover, when

the model is used with metals

of higher

melting

points,

such as the noble metals [22], [13] the agreement with

other methods is far from

satisfactory. Consequently,

it has often been

suggested

[23], [6],

[24], [12]

that,

until the many uncertainties of the

trapping

model

have been clarified, it may be

preferable

to analyse

positron

data through a more

phenomenological approach,

using the

empirical

linear correlations between

Eiv

and some characteristic temperatures :

1.1.1. -

T;

which is the temperature of the inflec- tion

point

in the plot of i (mean lifetime of

positrons)

against 1/T :

E’

(eV) = 1.13 x 10-3 Ti (K) [6].

1.1. 2. - The threshold temperatures

Tt

at which thermally

generated

vacancies

produce

measurable

positron trapping.

This has the additional

advantage

of

giving

a

precise

determination of

Eiv

without

approaching

the melting

point

- a

major

one in

dealing

with refractories [12], with metals

having high

vapour pressure in the solid state [24], [13], or with alloys [6].

It will be the main purposes of this paper to show that :

a)

positron

annihilation data can be fruitfully analysed without the need of the

trapping

model formalism,

b) the linear correlation between

E F

and Ti is not

fortuitious but derived from the trapping model and

must be used carefully because of a

possible

crystallo- graphic structure

dependence

of the

proportionality

factor,

c) computer simulated

r(I/T)

curves as derived

from the

trapping

model are strongly affected by

changes

in

trapping

rates,

detrapping

process, etc.

except for the value

of E1v

that can be calculated from the characteristics of the inflection

point

Both the new source technique and the new method

of analysis will be tested on aluminium metal.

2.

Expérimental

procédure and results. - The electronic apparatus used to measure the

positron-

annihilation lifetimes is basically a high-resolution timing device with fast and slow coincidence circuits, plastic scintillators, a

time-to-amplitude

conversion capacitor and an energy discriminator. The data are

accumulated in a multichannel analyser in the form

of a

histogram

of the number of events as a function

of time. In a metal this is the sum of exponential components folded with the resolution of the instru- ment and a constant

background

due to random

coincidence. The mean lifetime as a function of temperature is obtained by a computer fit

analysis

as described elsewhere [25], [14]. A

good

estimate of the resolution may be obtained

by

substituting a 6°Co

source in

place

of the

sample.

Since 6°Co emits two

y-rays within - 5 ps of each other, the measured time spectrum will be essentially the resolution of the instrument. Such a prompt coincidence curve has been found to have a half width of 300 ps. In the lifetime

region studied here ( 150 i

300 ps) the uncertainty

will be of about 2 ps.

A new type of

positron-lifetime

source has been tested,

using

5 sCo

positrons emitting isotope

in a

state of diluted solid solution in the material to be

investigated.

In the case of interest, the specimen was

a

cylinder

of 99.999

%

purity aluminium, 3 mm thick and 10 mm in diameter in which about 50

yci

of S8Co

were diffused by

annealing

near the

melting

tempe- rature, after

electrodeposition

of 58CO from chloride ;

undiffused cobalt and

possible

corrosion

products

were carefully removed from the

sample

surface by

polishing. Although

the two y-photons emitted at

birth and annihilation of

positrons

are less easily

discriminated here than with a 22Na source (0.511,

1.28 MeV for 22Na and 0.511, 0.81 MeV for

58Co),

the

improvement regarding

the

intensity

of the

long-

lived source and surface components is obvious

(Fig.

1). In addition such a

diffused

source is very suitable for

high

temperature work and lifetime measurements after thermal or mechanical treatments.

Aluminium has been chosen as a test material because of the abundance of good data available

regarding

the vacancy formation energy

(see

for

instance [6] table

II).

To obtain

reproducible

data in

the low temperature part of the 7(T) curve, the spe- cimen has to be

carefully

annealed near the

melting

temperature in order to stabilize the dislocations in the material.

Table 1

gives

some

typical

values of the mean

lifetime i of the

positrons

as a function

of temperature.

Table I.

(4)

Fig. 1. - Positron-lifetime spectra in aluminium : (a) with 22Na conventional source; (b) with 58CO diffused source.

Fig. 2. - Temperature dependence of the mean lifetime in alumi-

nium : (a) i( T) full line : best fit from a trapping model (upper scale) ; (b) 77(l / T)

(lower

scale).

(c)- dr-/d(I/T)1

This is

pictured

in figure 2

(curve (a))

along with two

other curves : the variation of ? with the

reciprocal

temperature

(curve (b))

and the derivative curve

d’f/d(I/T) (curve (c))

whose maximum

gives

the

coordinates of the inflection

point

in 7(1/T), that is :

Let us remark that

using T;

= 653.6 K in the

empirical

formula

proposed

by Doyama [6]

(Efv

= 1.13 x 10 - 3

rj

results in

E F

= 0.73 eV

which is in

good

agreement with the other available data [26].

3. An

original

method to calculate

Eiv

from 1(T)

data. - In this section the

trapping

model will be

fully criticized. In particular, it will be shown that a

direct

fitting procedure

of the 7(T) curve on the

trapping

model formula cannot lead to the proper value of the vacancy formation energy

Efv.

The

drastic influence of factors such as the

positron

trapping rate, the

detrapping

occurrence, the thermal

expansion

of the lattice, the presence of other defects,

a proper choice for the asymptotic lifetime in the

lattice iL

and in the vacancy trap i 1 v will be systema- tically analysed. Incidentally, the empirical formula

E’(Ti)

will be shown to be contained in the

trapping

model.

Eventually, we will demonstrate that the many uncertainties of the

trapping

model can be easily

bypassed

if

E’

is calculated from the coordinates of the inflection

point

in the i(1/T) curve.

3.1 THE TRAPPING MODEL

(see

for instance Ref. [6], [19],

[27]).

- Let the number of free positrons in the

lattice and those

trapped

by vacancies

be nL

and n 1 v

respectively.

Then the rate equations are given by :

where :

. Jll v’ the

specific

positron trapping rate is usually

written

concentration at température T [26],

is the

detrapp-

ing rate expressed in terms ’of a

vacancy-positron

binding

energy eB, the positron mass m and the radius a

of the

trapping

volume.

0

TL( T) and r, 1v(T)

are usually

naively

supposed

to vary only through the lattice thermal expansion,

that is :

and

iL

and

To

are merely deduced from the extrapolated

values of the 7(T) experimental curve at low and high temperature (a = 8.4 x 10- 5 K-1 in Al).

Solution of eq. (1) in steady state conditions gives

the mean lifetime of positrons i(T) :

(5)

42

Table II.

When there are many kinds of trapping centres, M1v

Ci v

must be

replaced

in eq. (1) by a

sum 03A3

mi

Ci

i over all the different

trapping

centres. In metals for instance, there is always a contribution from the so-

called Frank lattice dislocations which is

equivalent

to

a concentration of

Cd

vacancies whatever the tempe-

rature.

By

using

a standard least-square

procedure,

eq. (2)

has been fitted as usual to the present

experimental

data on the assumption that no

detrapping

of

positrons

occurs. The values for best fit are given in table II

and have been used to draw the full line in figure 2a.

In addition to a too low value of

E’V,

the results are

unrealistic in

particular

because of an overestimate of the

trapping

rate. Indeed, from eq. (1) the

expected

order of magnitude for

lilv is

about 200

ps-1,

10’

smaller than the fitted value. We will see later that the

discrepancy

comes mainly from the opposite influences

of

detrapping

and thermal expansion which are

difficult to take into account with their true values in the

trapping

model.

3.2 THE ORIGINAL « INFLECTION POINT » METHOD.

-

If detrapping

might be neglected, eq. (2) could be

rewritten :

where t(T),

yl,(T)

and

C1v(T)

are supposed to be temperature

dependent

as described in 3.1. In the

following,

7(T) as given by eq. (3) will be referred to

as the

simple

trapping model. A

straightforward

calcu- lation,

stating

that

d2t/d(I/T)2

= 0 for the particular temperature Ti, shows that at the inflection point of the curve t(I/T), the fraction of

positrons annihilating

in a

perfect region

of the lattice is equal to the fraction

annihilating

at vacancies, and consequently :

or

which is

just

an expression of

Efv

equivalent to the

so-called empirical formula of Doyama [6].

The reason

why

Ln

[.LI v 1:L ex p slv k ]

i s a cons-

tant, is not very clear and might vary from a f.c.c.

structure, to b.c.c. or h.c.p.... because of the influence of the

crystallographic

order on

sBfv

and of the

influence of the packing fraction on

iL(T). In

any

case, eq. (4) cannot be used directly to calculate

Efv

since

J1v(Ti}

and

SF1v

are not given by

positron

annihilation experiments.

However,

calculating 1

dI at the inflection point

dT

temperature

Ti,

and using eq. (4) with

results in a new

expression

for

El,

that is :

It is easy to show by numerical estimates that the two first terms in the right hand side

of eq.

(5) account

for about 10-’ in

Eiy

of vacancies in metals; this contribution will be neglected in the

following

because

of its irrelevance to experimental accuracy in

E ;,

measurements. The x term contribution is

relatively

small as well (about 4 x

10- 2)

but will be kept so far.

Then,

Eiy

can be

expressed

from eq. (5) :

Tl, î5(T;)

and

dT/d(I/T)i

are directly obtained from the derivative curve

of i(1/T)

(Fig. 2c) ;

iL(T;)

has to

be calculated by a thermal

expansion

formula from the 7(T) curve

extrapolated

at low temperature

(iL

= 165 ps at 20 °C). There is no need to know

,rlv(Ti)

and this is very fortunate as it will be shown in a

moment.

Although

the true value of x does not really

matter for the

E F

calculation, it is sometimes of interest to determine the temperature

dependence

of

the

trapping

rate. It will be seen further that x = 0.5,

as found by the

trapping

model fitting

procedure

(Table II), is the more reasonable.

Thus, using eqs. (6) and (4) along with the data of

the present work (see section 2) and the entropy coefficient

SF Ik

= 1.8 in aluminium obtained else- where [26], gives :

E F

= 0.70 + 0.03 eV

,Mu°v

= 164

ps -1

which are indeed reasonable values.

(6)

3.3 ADVANTAGES OF THE « INFLECTION POINT » METHOD COMPARED TO THE FITTING PROCEDURE. -

As eq. (6) giving

Eiv

in the inflection point method is

deduced from a trapping model formula, it could be

thought

that the same uncertainties could still influence the result. To show that it is not the case, i(1/T)

behaviours have been simulated by computer calcu- lations and the influence of the various factors has been

analysed.

The main conclusion is that the

inflection

point keeps on

giving

the same

Efv

value

(within

experimental

accuracy) even when drastic

changes are observed in the

i( 1 / T)

curve.

3.3.1 Specific trapping rate influence. - Using

eqs. (3) and (4), sets

of 7(T)

values can be calculated with arbitrary though reasonable parameters

(Efv

= 0.70

eV, TO

= 170 ps,

T1v

= 260

ps)

and

different temperature

dependence

of the

specific trapping

rate [x = - 0.5, 0, 0.5 and 1 in a

J1.1v(T) = MIVO T x law .

Then,

T-,,(I/T)

curves are

Mlv(T ) iv T 0 vo/

law

J

Then

(I/T)

curvcs are

drawn and

compared

to each other (see

Fig.

3).

Fig. 3. - Computer simulation for different specific trapping rate

functions Jl1V = u’v(TITO)’ : : (a) x = - 0.5 ; (b) x = 0 ; (c) x=0.5;(d) x= 1.

The main features are the

following :

e all the calculated curves are

quite

similar except in the

high

temperature

region

e the recalculated value

E F (X)

obtained from the

inflection

points

of all the

ix( 1 / T)

curves and with

eq. (6) are all the same within reasonable accuracy range, as evidenced in table III

Table III.

e in addition x = 0.5 seems to be the best value to fit the experimental data at

high

temperature ;

Tx> 0.5(I/T) slopes

are

slightly

too low

and Tx 0.5(I/T)

slopes are

slightly

too large at

high

temperature.

3.3.2 Influence

of

other

defects.

- The simulation

will be limited here to the influence of dislocations, that will be considered as equivalent to an extra

concentration

Cd

of vacancies, kept constant with

changing

temperature. The

TD(1/T)

curves have to be

calculated from eq. (3) with

C,v(T)

substituted by

Clv(T)

+

Cd. Again,

all calculated curves are very similar within realistic values of

Cd ( 104

to 106 cm - 2

in well annealed aluminium) and recalculated

E’(Cd)

values by the inflection point method are all the same (Table IV). Incidentally, the rather

unexpected

large

values of

7,,.P(I/T)

below 280 OC appear as not due to

dislocations (within reasonable concentrations) and

cannot so far be interpreted

by

a coherent

trapping

model (Fig. 2a).

Table IV. - (same units as in table III).

3.3.3 Influence of the thermal expansion. - In

eq. (3),

Ta(T)

can be calculated with the parameter

set as given in section 3.3.1, with rlv and iL either

kept

constant or being temperature

dependent

The

-=taCT),

for a ranging from 0 to the thermal expan- sion coefficient in aluminium (a = 8.4 x 10- 5

K-1),

are quite similar at low temperature, but

diverge drastically

at

high

temperature. But

again,

the recal-

culated values of

Eiv(rx)

given by the inflection

point

method (eq. 6) are not really

changed.

Table V presents the main features of the

rL(T) and rlv(T)

influences.

Table V.

3.3.4 Influence of the

detrapping

occurrence. -

Going

back now to the full eq. (2) we will now simu-

late the influence of

positron detrapping

before

annihilation. In this calculation,

rL and

’t 1 v will be

kept

constant in a first stage. The data presented in

table VI show that, opposite to the influence of thermal

(7)

44

expansion,

detrapping

results in

lowering

the high temperature values of

t"b(T).

Again, the recalculated values of

Eiv(h)

are not really af’ected by

changes

in

the binding energy of the vacancy-positron pair.

Just for the sake of it, an attempt has been made to compensate the thermal expansion influence by allow- ing detrapping to occur so that

1/2(ia(T)

+

:t"b(T»)

would be equal to the

experimental

data

Texp(T)’

This resulted in a surprisingly low value of

f.b=0.67

eV, compared with the theoretical estimate of Hodges [28].

This is

pictured

in

figure

4.

Fig. 4. - Influence of thermal expansion and detrapping occurrence (a) computer simulation of the thermal expansion influence ; (b) computer simulation of the detrapping influence ; (c) : experimental data, full line : computer simulation of a compensation

between thermal expansion and detrapping.

Table VI.

4. Discussion and conclusion. - This paper has

reported

new

experimental

and theoretical approaches

to positron-lifetime

experiments

for the measurement

of the vacancy formation energy in metals.

It has been shown that

diffused

sources, with the

positron active material as impurities in the investi-

gated metal, are very suitable for high temperature work, and that they reduce quite

obviously

the long

lived source and surface components in lifetime spectra and permit direct thermal or mechanical treatment of the specimen.

A direct analysis of the lifetime data by a trapping

model formula has been shown to be quite hazardous

without a perfect

knowledge of many physical

factors :

e temperature

dependence

of the specific trapping

rate,

e

binding

energy of the

vacancy-positron

pair which might be less tied to each other than previously

expected,

. presence of other defects,

. and last but not least, the true temperature

dependence

of the

positron-lifetime

in the perfect

lattice and at vacancy trap. The lattice thermal

expansion approximation

that has been commonly

used until now

might

be a very crude one,

especially

because of a

possible phonon-assisted trapping

of

positrons

[17] before the occurrence of a vacancy.

This

point

is

supported

by the observation of a syste- matic difference in the lifetime obtained in the tran-

sition region ( T 300 OC) when measurements carried out at

equilibrium

temperature are

compared

to data

obtained in

cooled-samples

containing quenched-in

vacancies [29].

Although derived from the

trapping

model, the inflection point method which allows one to calculate

Efy

from the coordinates of the inflection

point

in the T( 1 /T) curve, does not suffer the same uncertainties and

gives

always the same value

(expected

to be

accurate !) of the vacancy formation energy. In fact,

this is not very

surprising.

First of all, this method does not need to know

’t"ly(T)

which, on the contrary, interfers in the

trapping

model formula and is

impos-

sible to determine from

experimental

data because of the influence of both thermal expansion and

detrapping

processes.

Secondly,

the inflection point

of the :r(I/T) curve is equally far from the

high

and

low temperature

regions

and, as a consequence, is

expected

to be insensitive to high temperature detrapp- ing and low temperature

phonon-assisted trapping.

Finally,

this

inflection

point method has one

impor-

tant advantage

because T;

occurs at

approximately

0.7

T. ( Tm

=

melting temperature).

In the case of

refractories or metals with

high

vapour pressure in the solid state, it will be

possible

to evaluate

E F

without measurements near the melting

point.

References

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[2] GOLAND, A. N., B.N.L. Report (1970), 16517.

[3] SEEGER, A., J. Phys. F : Metal Phys. 3 (1973) 248.

[4] WEST, R. N., Adv. Phys. 22 (1973) 263.

[5] JANOT, Ch., J. Phys. 11 (1976) 89.

[6] DOYAMA, M., In Progress in the study of point defects.

Doyama M. and Yoshida S. Eds. (University of Tokyo Press) 1977, p. 3.

[7] HALL, T. M., Phys. Rev. B 10 (1974) 3062.

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