contourseffects 2 Dynamical diffraction theory Dynamical diffraction A beam which is diffracted once will easily be rediffracted many times Understanding diffraction contrast in the TEM image ID: 536105
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Slide1
1
Imaging defects and
contours/effectsSlide2
2
Dynamical diffraction theory
Dynamical diffraction: A beam which is diffracted once will easily be re-diffracted (many times..)
Understanding diffraction contrast in the TEM image
In general, the analysis of the intensity of
diffracted beams
in the TEM is not simple because a beam which
is diffracted
once will easily be
re-diffracted
. We call
this
repeated
diffraction ‘dynamical diffraction.’Slide3
3
Dynamical diffraction:
http://pd.chem.ucl.ac.uk/pdnn/diff2/kinemat1.htm
Assumption:
T
hat
each
individual diffraction/interference
event, from whatever locality within the crystal, acts
independently of the others
M
ultiple
diffraction throughout the crystal; all of these waves can then
interfere
with each other
Ewald
: Diffraction intensity, I, is proportional to just the magnitude of the structure factor, F, is referred to as the dynamical theory of diffraction
We
cannot use
the intensities
of spots in electron DPs (except under
very special
conditions such as CBED) for structure
determination, in
the way that we use intensities in X-ray patterns
.
Ex.
the intensity of the electron beam varies strongly as
the thickness
of the specimen changesSlide4
4
THE AMPLITUDE OF A DIFFRACTED BEAM
The amplitude of the electron beam scattered from a unit cell is:
Structure factor
The
amplitude
in a diffracted
beam:
(
r
n
denotes the position of each unit
cell)
T
he
intensity at some point P, we then
sum over
all the unit cells in the specimen.Slide5
5
If the amplitude
φg changes by a small increment as the beam passes through a thin slice of material which is dz thick we can write down expressions for the changes in
φ
g
and f
0
by using the concept introduced in equation 13.3
but replacing a by the short distance dz
Two beam approximation
Here
χ
O
-χ
D
is the change in wave vector as the
φ
g
beam
scatters into the
φ
0
beam. Similarly
χ
D
-χ
O is the change in wave vector as the φ0 beam scatters into the φg beam.
Now the difference χO-χD is identical to kO
k
D
although
the individual terms are not equal.
Then remember
that kDkO (=K) is g + s for the perfect crystal.Slide6
6
The two equations can be rearranged to give a pair of coupled differential
equations. We say that φ0 and φ
g
are ‘dynamically coupled
.’
The term dynamical diffraction thus means that the amplitudes
(and therefore the intensities) of the direct and diffracted beams are constantly changing, i.e., they are dynamic
Howie-Whelan equations
If we can solve the Howie-Whelan equations, then
we can
predict the intensities in the direct and
diffracted
beamsSlide7
7
I
ntensity
in the
Bragg diffracted beam
T
he
effective excitation error
I
g
, in the diffracted beam
emerging from
the specimen is proportional to
sin
2
(πt
Δ
k
)
T
hus
I
0
is proportional to
cos
2
(
πtΔk)Ig and I0 are both periodic
in both t and seff
Extinction distance , characteristic length for the diffraction vector g
Solving the Howie – Whelan equations , and thenSlide8
8
Intensity related to defects: WHY DO TRANSLATIONS PRODUCE CONTRAST?
A unit cell in a strained crystal will be displaced from its perfect-crystal position so that it is located at
position
r'
0
instead of rn where n is included to remind us that
we are considering scattering from an array of unit cells;
We now modify
these equations intuitively to include
the
effect of adding a displacementSlide9
9
Planar defects are seen when
≠ 0
α
= 2
π
g·R
Simplify by setting:
We see contrast from planar defects because the translation, R, causes a phase
shift
α
=2
π
g·RSlide10
10
Thickness and bending
contoursSlide11
11
Two-beam:
Bend
contours
:
Thickness
–
constant
s
eff
varies
locally
Thickness fringes: seff remains
constant t varies
(Intensity
in the Bragg diffracted
beam)Slide12
12
Thickness fringes
O
scillations
in I
0
or
I
g
are known as thickness
fringes
Y
ou
will only see these fringes when
the thickness of the
specimen varies
locally, otherwise the contrast will be a uniform graySlide13
13Slide14
14
Bending contours
O
ccur
when a
particular set
of diffracting planes is not parallel
everywhere; the planes rock into, and through, the
Bragg
condition
.
Remembering Bragg’s law, the (2h 2k
2l) planes diffract strongly
when y has increased to 2θ
B. So we’ll see extra contours because of the higher-order diffraction. As θ
increases, the planes rotate through the Bragg condition more quickly (within a small distance Δx) so the bend contours become
much narrower
for
higher order
reflections
.Slide15
15Slide16
16Slide17
17
Moirè
fringesSlide18
18Slide19
19
Imaging
DislocationsSlide20
20
Edge dislocationSlide21
21
Edge dislocationSlide22
22Slide23
23
(u)Slide24
24Slide25
25
FCC
BCC
Slip plane:
S
lip direction:
Burger vector:
Slip plane:
S
lip direction:
Burger vector: Slide26
26
FCC
BCC
Slip plane: {111}
S
lip direction: <110>
Burger vector:
a
o
/2[110]
Slip plane: {110}
S
lip direction: <111>
Burger vector: a
0
/2[111]Slide27
27Slide28
28
Important questions to answer:
Is the dislocation interacting with other dislocations, or with other lattice defects?Is the dislocation jogged, kinked, or straight?
What
is the density of dislocations in that region
of the
specimen (and what was it before we
prepared
the specimen)?Slide29
29
Howie-Whelan equations
Modify the Howie-Whelan equations to include a lattice distortion R. So for the imperfect crystal
Adding lattice displacement
α
= 2
π
g
·
R
Defects are visible when
α
≠
0
Intensity of the scattered beamSlide30
30
Isotropic elasticity theory, the lattice displacement R due to a straight dislocation in the u-direction is:
Contrast from a dislocation:
b is the Burgers vector, b
e
is the
edge component of the Burgers vector, u is a unit vector
along the dislocation line (the line direction), and ν is Poisson’s ratio.
g·R
causes the contrast and for a
dislocation
Slide31
31
g ·
R / g · b analysis
Screw:
Edge:
b
e
= 0
b
|| u b x u = 0
b = b
e
b ˔ u
Invisibility criterion:
Invisibility criterion:Slide32
32
Cindy SmithSlide33
33Slide34
34Slide35
35
g·b = 1
g·b = 2
Screw dislocation
Important to know the value of SSlide36
36
Edge dislocation
Always remember:
g
·
R
causes the contrast and for
a dislocation
, R changes with
z.
We
say that
g·b
= n. If we know g and we determine n, then we know b.
g · b = 0 Gives invisibilityg · b = +1 Gives one intensity dipg · b = +2 Gives two intensity dips close to s=0
Usually set s > 0 for g when imaging a dislocation in
two-beam conditions
. Then the dislocation can appear
dark against
a bright background in a BF imageSlide37
37Slide38
38Slide39
39
Example:
U = [2-1-1]
B=1/2[101]Slide40
40
Imaging dislocations with
Two-beam techniqueSlide41
41Slide42
42Slide43
43
Imaging dislocations with
Weak-beam
techniqueSlide44
44
The contrast of a dislocations are quite wide (~
ξg
eff
/3)
Weak beam
Small effective extinction distance for large S
Two-beam:
Increase s to 0.2 nm
-1
in WF to increase
S
eff
Narrow image of most defects
Characteristic length of the diffraction vectorSlide45
45Slide46
46Slide47
47Slide48
48
Imaging
Stacking faults in FCCSlide49
49Slide50
50Slide51
51Slide52
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Example: Stacking faults in FCCSlide53
53Slide54
54
Intensity of the fringes depends on α
BF: sin α > 0 : FF (First Fringe) – Bright LF (Last
F
ringe
) -- Bright
sin α < 0 : FF – Dark
LF – DarkDF: sin α > 0 : FF
–
Bright
LF -- Dark
sin α < 0 : FF – Dark LF – Bright α ≠
± πα = 2πg·RSlide55
55
(A–D) Four strong-beam images of an SF recorded
using ±g
BF and
±g
DF. The beam was nearly normal to the surfaces;
the SF fringe intensity
is similar at the top surface
but complementary at the bottom surface. The
rules
are summarized
in (E) and (F) where G and W
indicate that the first
fringe is gray or white; (T, B) indicates top/bottom.Slide56
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Then there are some rules for interpreting the contrast:
In the image, the fringe corresponding to the top surface (T) is white in BF if g·R
is > 0 and black if
g·R
<
0.Using the same strong
hkl reflection for BF and DF imaging, the fringe from the bottom (B) of the fault will be complementary whereas the fringe from the top (T) will be the same in both the BF and
DF
images.
The
central fringes fade away as the
thickness increases
. The reason it is important to know the sign of g is that you will use this information to determine
the sign of R.For the geometry shown in Figure 25.3, if the origin of the g vector is placed at the center of the
SF in the DF image, the vector g points away from the bright outer fringe if the fault is extrinsic and toward it if it is intrinsic (200, 222, and 440 reflections); if the reflection is a 400, 111, or 220 the reverse is the case.Slide57
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Images Slide58
58Slide59
59Slide60
60Slide61
61Slide62
62Slide63
63Slide64
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