1Xxxxxx Titre xxxx © NDT expert © NDT expert - The ultimate control INFRARED THERMOGRAPHY ON...

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1 Xxxxxx Titre xxxx © NDT expert © NDT expert - The ultimate control INFRARED THERMOGRAPHY INFRARED THERMOGRAPHY ON AIRCRAFT ON AIRCRAFT

Transcript of 1Xxxxxx Titre xxxx © NDT expert © NDT expert - The ultimate control INFRARED THERMOGRAPHY ON...

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INFRARED INFRARED THERMOGRAPHYTHERMOGRAPHY

ON AIRCRAFTON AIRCRAFT

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Basic kit for the IRT control

Measurement chain

COMPAQ

V70 V70

(4)

(1)

(3)

(2)

Calibration pieceheating 1- IR camera

2 – control panel of the camera

3 – Direct view on the screen

4 – Signal processing of the acquisition

INSTRUMENTATION

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Instrumentation used in IRT

Choice of the camera :

• Multiple use of the detector : IR night vision, thermal control of active sources, military application, ….

• Thermal sensitivity : (0,1° till 0,01°C)

• Acquisition frequency (25 till 300 image/s)

• Line acquisition mode or Focal Plane Array (FPA)

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Instrumentation used in IRT

Heating choices :

• Different techniques : hot air blower, tubes, flash lamps, hot water, pulsed heating, laser, sun for space shuttle, heating blanckets

• Surface heating or linear heating

• Homogeneity, reproductibility, calibration, characterization

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IRT CONTROL ON COMPOSITE

transmission technique :

14 mm

carbon

rubber

Applied Heat

Transmitted Heat

Without defect With defect

T

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IRT CONTROL ON COMPOSITE

Reflexion technique :

Emitted Heat

Reflected Heat

Absorbed Heat

T

With defectWithout defect

14 mm

carbon

rubber

THERMOGRAM

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Temperature variation in a point

Reflexion technique :

Transmission technique :

heating

time

heating

time

Without defect

With defect (isolation)

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Thermographic Inspection

Advantages of the method :• Global examination of part

• Only ONE SIDE access is required for the examination

• Real Time inspection

• Apply for all composite structure and materials even porous

• not very sensitive to part geometry, well suited for large surfaces

Disavantages :• Sensitive to heating mode (type,duration,position)

• Response time must be studied

• Exact composition of the pieces and the thicknesses must be known

• Less definition than Ultrasonic C-Scan and Radiography

• Inhomogeneous heating on complex part

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DEFECTS ENCOUNTERED

• Lack of adhesion of cohesion, bubbles

• Delamination

• Defects on surface coatings

• Inclusions of foreign materials

• Liquid ingress

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Pulse heating method

Detection of defects inside a honeycomb composite part

Reflexion method

Heating pulse : 0.1 sec

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Pulse method – reflexion inspection on part M88

• 7 defects visible

• Contrast is decreasing after optimum image

Picture of part First image Heated part at T0

Optimum image 5 Sec after 10 sec after

1 2

3 4 5

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• 7 defects are detected

Transmission face 1

Defects seen as dark spots

Reflexion face 1

Reflexion face 2

Transmission Vs Reflexion method

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Modulated thermography

440 mm

370 mm

carbon

14 mm

Test sample, composite bonding Carbon/Elastomer

rubber

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Phase Image Amplitude image

Method : reflexion heating, rubber sideFrequency : 0.006 HzModulation : 1000 images

Modulated thermography

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Method : transmission heating, rubber sideFrequency : 0.003 HzModulation : 1000 images

Phase imageAmplitude image

Modulated thermography

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Disbonded area

A A

Cross section AA

rubber

aluminium

kevlar

bonding

Modulated thermography

Test sample, composite bonding Metal/Elastomer/Kevlar

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Phase imageAmplitude Image

Modulated thermography

Method : transmission heating, kevlar sideFrequency : 0.006 HzModulation : 3000 images

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Conclusions

• Global method, quick, well suited for detection on composite and complex shaped surface, and for large areas

• Easy to set up on site (maintenance, expertise, production control)

• Quick evolution of the technology, lower price of detectors, new powerfull software for analysis tools will increase :

• maximum inspected thickness

• spatial and thermal resolution

• velocity of inspection