3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

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3D quantification of trans - and inter - lamellar fatigue crack in Ti alloy L. Babout 1 , L. Jopek 1 , M. Preuss 2 1 Institute of Applied Computer Science, Lodz University of Technology, Poland 2 School of Materials, University of Manchester, UK [email protected], http://lbabout.iis.p.lodz.pl

description

My presentation at 3DMS2014 (Annecy, June 2014) about 3D segmentation of lamellar Ti alloy. This presents CHG filtering for lamellar orientation classification as well as grain boundary and crack segmentation. Unique info to characterise type of cracking occurring in such complex titanium microstructure! Download the presentation to get access to the animations!

Transcript of 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Page 1: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

3D quantification

of trans- and inter-lamellar

fatigue crack in Ti alloy

L. Babout1, L. Jopek1, M. Preuss2

1Institute of Applied Computer Science, Lodz University of

Technology, Poland2School of Materials, University of Manchester, UK

[email protected], http://lbabout.iis.p.lodz.pl

Page 2: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Outline

• Introduction

• Experimental set-up

• Image processing steps

• Results

• Conclusion

Page 3: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Introduction (1/4)

• Myriads of applications of Ti alloy

• Different complex microstructures

• Need to understand short fatigue

crack-microstructure interaction

• X-ray microtomography: technique of

choice for mechanistic studies of

crack propagation

Page 4: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Introduction (2/4)

• Lamellar microstructure of (α+β) Ti alloy

• X-ray CT +EBSD study[1] shown crack

propagation influenced by

– β-gb misorientation

– α-lamellae/colonies favorably oriented for <a>

basal slip and <a> prismatic slip

[1] Birosca et al. Acta Mater., 2009, 57: 5834-5847

Page 5: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Introduction (3/4)

• α plates growth in the β phase Burgers

relationship: (100)β || (0002)α and [1-11]β || [11-20]α

α plates (1-100)

(0002)

TL crack

IL crack

Page 6: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Introduction(4/4)

• What about proportion of trans-/inter-

lamellar cracking?

X-ray μCT / in situ fatigue

Image processing:

crack segmentation

α-lamellar/colony segmentation

(β-gb segmentation)

Local orientation calculation

Page 7: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Experimental set-up• ME1230 (ID19 ESRF, back to 2006!)

– X-ray μCT: 0.7μm, 40 keV, phase contrast

– fatigue: 50 Hz, 0.5σ0.2, R=0.1

• 2 samples of Ti-6246 with notch

notch

β-gb

α-colony

β grain 1

β grain 2

crack1

crack2

27 kcycles

Page 8: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Image processing: α-colony

segmentation

• Existing method: local orientation map

based on image gradient (eigenvector

calculation)[1,2]

• Our method: directional filter bank (DFB)

using special structuring element

sensitive to surface-like objects[3]

[1] D. Jeulin, M. Moreaud, Im. Anal. Stereol., 2008, 27: 183-192.

[2] N. Vanderesse et al., Scripta Mater., 2008,58: 512-515.

[3] L. Babout, L. Jopek, M. Janaszewski, In 13th IAPR International Conference on Machine Vision

Applications. Kyoto. 2013.

Page 9: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

CHG filter(1/2)

• Complementary of HourGlass

– tunable (default: r=5, θ=22.5°)

– Epanechnikov profile

– Default: 13 directions in <100>,<110> and

<111> directions

θ

n

r

[1 0 0]

[0 1 0]

[0 0 1]

[-1 1 1][1 1 1]

[1 -1 1]

[1 1 -1]

[1 0 -1]

[1 0 1]

[1 1 0]

[1 -1 0]

[0 1 1]

[ 0 1 -1]•y

•x

•z

Page 10: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

CHG filter (2/2)

• Lamellar classification (largest

response to DFB)[1 1 1]

[1 1 0]

[1 1 -1]

[1 0 1]

[1 0 0]

[1 0 -1]

[1 -1 1]

[1 -1 0]

[-1 1 1]

[0 1 1]

[0 1 0]

[0 1 -1]

[0 0 1]

x

yz

Page 11: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Image processing: β-gb

segmentation

• Challenging task

– local similarity of

α-layer/α-lamellae

– phase contrast “leaks”

• Multiple step

approach

Page 12: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Step 1: edge preserving smoothing

• Goal: vanish as much as α-lamellae as possible

while keeping sharp β-gb

• Possible methods:

– non linear diffusion

filtering (used in Amira)

– Mean shift smoothing[1]

• Does not fully solve

the problem

[1] Comaniciu et al., IEEE Trans.Pattern Anal.Mach.Intell., 2002, 17: 790-799.

NC>2950

Page 13: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Step 2: hole closing correction

Manual

segmentation

• Undersegmentation of β-gb leaves holes

• Can be filled using

Hole Closing Algorithm[1,2]

• Successfully used for

IGSCC in stainless steel[3]

[1] Z. Aktouf et al., Pattern Recogn. Lett., 2002, 23: 523-531.

[2] M. Janaszewski, et al., Pattern Recogn. Lett., 2011, 32: 2231-2238.

[3] L. Babout et al., Scripta Mater., 2011, 65: 131-134.

20 μm

crack

bridge

Page 14: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Step 3: CHG filtering +topological

criterion• Numerous surface-like defects can be distinguished from

β-gb using CHG-DFB

• Size criterion and topological

criterion helps at removing

them

– based on topological numbers

– usually defects have more border

pts than 2D junction pts

i

s

t

h

m

u

s

Defect

After CHG-DFB

Page 15: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Image processing: crack

segmentation and image registration

• Crack segmented

from tomo. image at

t1 …

• … Superimposed

with microstructural

features from tomo.

image at t0

x

y

z

[1 1 1]

[1 1 0]

[1 1 -1]

[1 0 1]

[1 0 0]

[1 0 -1]

[1 -1 1]

[1 -1 0]

[-1 1 1]

[0 1 1]

[0 1 0]

[0 1 -1]

[0 0 1]

crack

notch

β-gb

Page 16: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Results (1/4)• 2 samples – 2 scenarios (notch position)

• Crack orientation w.r.t. fatigue loading (z-axis)

– CHG classification + MV=max{λi}i=1,2,3V

Sample A

30°-40°

20°-30°

10°-20°

0°-10°

80°-90°

70°-80°

60°-70°

50°-60°

40°-50°

x

y

z

crack #2

crack #1

Sample B

30°-40°

20°-30°

10°-20°

0°-10°

80°-90°

70°-80°

60°-70°

50°-60°

40°-50°

z

x

y

β-gb1

β-gb2

β-gb3

Page 17: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Results (2/4)

• Cracks crossing colonies of ≠ orientations

– sA: crack1 not deflected by numerous colonies

– sB: strong deflection in same colony ([001]) near notch

x

y

z

[1 1 1]

[1 1 0]

[1 1 -1]

[1 0 1]

[1 0 0]

[1 0 -1]

[1 -1 1]

[1 -1 0]

[-1 1 1]

[0 1 1]

[0 1 0]

[0 1 -1]

[0 0 1]

[0 1 -1]

[-1 1 1] [1 1 1]

[1 1 -1]

[1 -1 1]

x

y

z

[0 1 1]

[0 0 1]

[0 1 1]β-gb1

β-gb2

β-gb3

Page 18: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Results (3/4)• Angle between crack and lamellar orientation

– lamellar orientation: 3D gradient map + MV=max{λi}i=1,2,3V

– inter- lamellar: angle < 30°

x

y

z

80°-90°

70°-80°

60°-70°

50°-60°

40°-50°

30°-40°

0°-30°

x

y

z

β-gb1

β-gb2

β-gb3

Page 19: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Results (4/4)• Trans-lamellar cracking predominant

– ~60% larger than 70°

– colonies favorably oriented for basal <a> slip

• Non negligible

inter-lamellar

– 10-20%

– prismatic <a> slip

• Samples show

similar trends

• Comfort Birosca

et al. EBSD observations

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Conclusions

First 3D quantitative analysis of cracking type in

lamellar Ti Alloy using well-suited image

processing strategy

Short fatigue crack propagation strongly driven

by the crystallographic nature of the colonies

when favorably oriented (i.e. basal/prismatic slip)

Possible future work

Test method on Birosca et al. tomography data

DCT (above β transus) + IP + known variants 3D

crystallographic orientation of α phase

Microstructure Faithful Modeling

Page 21: 3D quantification of trans- and inter-lamellar fatigue crack in Ti alloy

Acknowledgements

• Polish National Research Centre (grant no:

6522/B/T02/2011/40)

• ME1230 team

– J.Y Buffiere (Quezac support )

– M. Karadge

– F. Garcia-Pastor