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FIFTH CANADIAN CONFERENCE ON NONDESTRUCTIVE ... - IAEA

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- 430 -<br />

PULSED PILATOMETRIC INSPECTI<strong>ON</strong> OF UNB<strong>ON</strong>DED LAYERS<br />

Thermographie techniques are particularly convenient for the inspection of<br />

high emissivity surfaces such as graphite-epoxy laminates or anodized<br />

coatings. However, the thermographie signal is normally lower by an order of<br />

magnitude when inspecting metallic surfaces such as Al-epoxy honeycomb panels<br />

such as the one shown in fig. 7. This is a consequence of the low emissivity<br />

of bare aluminium surfaces, which is typically of the order of 0.1. On the<br />

other hand, thermography measures an indirect property of the material i.e.<br />

thermal resistance of the layer-to-layer interface, rather than the property<br />

which is of real interest i.e. the adhesive bond at the interface. A lack of<br />

adhesion between the aluminium skin and the honeycomb core in a laminate such<br />

as the one shown in fig. 7 would be quite difficult to detect thermographically,<br />

because the thermal conductivity of the air-filled honeycomb core<br />

is lower by several orders of magnitude than the thermal conductivity of the<br />

aluminium skin.<br />

i 2 u<br />

The holographic interferometry approach • » , on the other hand, provides<br />

a direct bond evaluation by mechanically lifting the bonded layer between the<br />

two hologram exposures. Although either vibration, pressure or heat can be<br />

applied to lift the unbonded layer, thermal stressing is the most convenient<br />

technique for a fast and non-contact inspection of laminates ~ . With this<br />

technique, the structure is holographically inspected before and after surface<br />

heating by a lamp or a hot-air gun. unbonded areas are revealed by the<br />

appearance of localized fringe patterns if the therraoelastic bending forces<br />

produce a- normal displacement of the unbonded layer of more than half a<br />

wavelength.<br />

In order to take advantage of the mechanical inspection capability of<br />

holography while avoiding its sensitivity to ambient vibration and stray<br />

light, a thermoelastic interferometric technique has been developed at our<br />

Institute 21 .<br />

The basic principle is shown in fig. 8. The layer to be inspected is heated<br />

by a pulsed and focused laser beam. The pulse duration, typically 1 ms or<br />

less, is comparable to the thermal propagation time across the layer<br />

thickness. Consequently, a transient therraoelastic moment causes the layer to<br />

lift, if unbonded, while its position is monitored by a sensitive focused<br />

interferometer. Because of the short duration of each pulse, large surfaces<br />

can be scanned rapidly. Apart from eliminating fringe-counting and heat<br />

uniformity problems, this approach has the following advantages with respect<br />

to holography:<br />

1. Every point being inspected during a very short period of time,<br />

low-frequency ambient vibration noise can be avoided. Operation on the<br />

industrial floor Is thus possible with our approach. High-power pulsed<br />

lasers have been used in the past to avoid hologram blurring during the<br />

exposure time, but ambient vibrations during the heating period between<br />

the two exposures cannot be avoided with such a method. Moreover, the<br />

colllmated interferometer beam can be spatially filtered to avoid stray<br />

light, so that our system can operate under conditions of normal ambient<br />

illumination.

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