non-contact emerging nondestructive techniques for ... · – non destructive inspection of...
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NDT Innovation Day, SIRRIS, Leuven, Nov 17, 2016 1
Dr. Marc GEORGES Laboratoire Laser et Contrôles Non Destructifs Centre Spatial de Liège – Université de Liège
4031 Angleur (Liège) - BELGIUM
Non-contact emerging nondestructive techniques for aerospace composite inspection
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NDT Innovation Day, SIRRIS, Leuven, Nov 17, 2016 2
Simulated space environment testing Large chambers with optical benches
Development of optical Space instrumentation
Development of Advanced Technologies
• Vacuum-Cryogeny • Quality insurance • Thermal Design • Signal Processing • Spaceborne Electronics • Smart sensors • Surface processing • Optical Design • Optical Metrology • Non Destructive Testing
« Center of Excellence » in Optics for the European Space Agency
Centre Spatial de Liège
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The Laser & NDT Lab
Dimensional measurement • Fringe projection • Digital Image Correlation
Research in laser and optical metrology and NDT for aerospace
Deformation measurement • Holography • Speckle interferometry • Shearography
Thermography • Pulsed + Lock-in • Vibrothermography (ULg)
Laser Ultrasonics
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NDT Innovation Day, SIRRIS, Leuven, Nov 17, 2016
NDT of composites • Applications
– Non destructive inspection of composites (foreign materials, damages,…) – Non destructive testing of composite structures (CTE measurement,….)
• Main role of CSL in recent/current projects: – Compare non-contact NDI techniques based on optics/lasers – Develop new techniques/sensors – Projects led by industries – Projects funded by EU, Wallonia
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NDT/NDI
Holography/Shearography
IR Active Thermography
Laser Ultrasonics
e.g. TECCOMA (2015-2019)
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NDT Innovation Day, SIRRIS, Leuven, Nov 17, 2016
• Shearography with heating
Shearography
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• Various techniques
Infrared Thermography
Flash lamp Fourier processing
Modulated lamp
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• Principle
Laser Ultrasonics
No couplant – No water Signal independent of geometry Economically interesting for curved parts (see. Airbus-Lockheed Martin publications)
Generation of ultrasound by laser Thermoelastic effect
Detection of ultrasound by laser Interferometric probe (with laser) and Two-Wave Mixing
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• First tests with LUIS - Laser ultrasound system of CTA (Montreal) • Detection Two-Wave Mixing (TWM) + long pulse laser (PDL) • Generation by CO2 laser (10.6 µm)
Laser illumination brought by a complex articulated arm with mirror (flexibility problems)
- Generation : pulsed CO2 laser (10.6 µm) - Detection : pulsed YAG laser (1064 nm) - Probe TWM - repetition rate : 100 Hz - Laser Spot : 2 mm - Scanning step : 0,5 mm - manufacturer TECNAR
Laser Ultrasonics
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Samples
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• Compared studies on various structures with defects Monolithic CFRPs
Sandwich CFRP/GFRP
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Compared results Laser Ultrasound
Vibrothermography
Shearo
Optical pulse thermography
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Laser Ultrasound Results
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Comparison Thermography Shearography Laser UT
Depth 1,5 mm > 1,5 mm >>> 1,5 mm
Dimensions 3-4 mm 3-4 mm 2 mm
Interpretation + - ++
Measurement Qualitative Qualitative Quantitative
Depth assessment
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Set-up + + - (scanning)
Cost $$ $ $$$$
Calibrated Defects are made of teflon to represent delaminations for UT technique No fast conclusion !
NDT techniques must be envisaged in complementarity
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NDT Innovation Day, SIRRIS, Leuven, Nov 17, 2016
Post-processing techniques
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Our recent/current developments
• Improvement of holography-shearography
• Robotized fully fiber-coupled laser ultrasound system
• Combination of holography/IR thermography
IR holography
• Data Fusion between various NDT techniques
• Combined experimental-simulated NDT
• Terahertz Holography NDT
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IR Holography: motivation • IR Thermography and Holography/Shearography
– Imaging full-field, non-contact (except for some excitation) – Require excitation
• IR Thermography – Easier interpretation of images than holo/shearography – A lot of post-processing methods exist
• Allow defect depth assessment – Better introduced than holo/shearography in many fields
• Why using holographic techniques in NDT ?
• Holography provides mechanical information – Behavior of structure and damage during life-cycle – Propagation of damage depending on thermo-mechanical load
• In many experiments : – Temperature variations AND deformations need to be captured – Both in space and time
Combine holography and thermography
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IR Holography
Laser OFF
Thermal background
Laser ON
Hologram
,.)(xI ,.)(xI
• Principle
Single sensor Simultaneous measurement of • Temperature variation • Deformation
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IR Holography • Decoupling temperature and deformation
Wrapped phase Unwrapped phase
Temperature variation Helicopter panel
3D plot of deformation
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IR Holography • Thermo-mechanical assessment of composite coupons
FANTOM thermogramFANTOM deformationCoupons on heating baseplate(d) (e) (f)
ThermogramFringe projection deformationFringe projection +Thermographic camera
(a) (b) (c)
Coupons
Fringe projection Thermalcamera
Coupons
Baseplate
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NDT Innovation Day, SIRRIS, Leuven, Nov 17, 2016
IR Holography • Airbus on-site testing
Airbus D41 « Tear Down »
« All Composite Aircraft » A350 Fuselage FANTOM industrial prototype
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IR Holography • Industrial tests : delamination on composite
∆T
∆φ
timeLamp start
After 2 seconds After 30 seconds After 6 minutes
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Development of Laser Ultrasonics • Detection by Two-Wave Mixing
– fiber-coupled system by Tecnar
• Generation by YAG laser (green) – fiber-coupling by CSL
• Robot arm (6 axes)
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Development of Laser Ultrasonics • Development of optical head
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Development of Laser Ultrasonics
C-s
can
Am
plitu
de
LUIS (10 µm) CSL system (532 nm)
C-s
can
Tim
e of
Flig
ht
CFRP sample Flat bottom holes 2 sizes – 3 depths
A-s
can
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Development of Laser Ultrasonics
Defects seen at different angles C-Scan Amplitude
C-Scan Time of Flight
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Thanks for your attention !
[email protected] www.csl.ulg.ac.be
Publications on ORBI (University repository)
mailto:[email protected]
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