Method of assessing bond integrity in bonded structures

• US 8,004,689 B2
• Filed: 05/09/2007
• Issued: 08/23/2011
• Est. Priority Date: 05/10/2006
• Status: Active Grant

• Current Assignee: National Research Council Canada
• Original Assignee: National Research Council Canada
• Inventors: Monchalin, Jean-Pierre, Campagne, Benjamin, Blouin, Alain
• Primary Examiner(s): Connolly; Patrick J
• Application Number:
  US12/227,115
• Publication Number:
  US 20090168074A1
• Time in Patent Office: 1,567 Days
• Field of Search: 356/502, 736/55, 736/57
• US Class Current: 356/502
• CPC Class Codes: G01N 21/1702 with opto-acoustic detection, e.g. for gases or analysing solids
• CPC Class Codes: G01N 2291/0231 Composite or layered materials
• CPC Class Codes: G01N 2291/0423 Surface waves, e.g. Rayleigh waves, Love waves
• CPC Class Codes: G01N 29/2418 using optoacoustic interaction with the material, e.g. laser radiation, photoacoustics photoacoustic cells G01N21/1702; measuring characteristics of vibrations by using radiation-sensitive means G01H9/00; acousto-optical conversion techniques for short-range imaging G01S15/8965; sound-producing devices using laser bundle G10K15/046
• CPC Class Codes: G01N 29/265 by moving the sensor relative to a stationary material

Abstract

A technique for acoustic detection of a disbond within a bonded structure involves thermal excitation of the surface of the bonded structure to induce a lifting and membrane vibration and is applicable to laminates and coated structures, as well as foam core structures or a honeycomb structures. The technique does not require access to both sides of the bonded structure. A large etendue interferometer is used to provide surface displacement measurement. The surface displacement measurement can be analyzed both by frequency or amplitude to determine existence of a disbond by membrane vibration, and further a thickness of the disbond can be determined using traditional pulse-echo time analysis. The technique may allow detection of stick bonds.

Claims

1. A method for assessing bond integrity at a region of a surface of a bonded material, the method comprising:

a. producing transient heating in the region so that if the region overlies a disbond in the bonded material, membrane vibration having a vibration period is induced over the disbond; and

b. detecting any surface displacement at or adjacent the region with a large etendue interferometer having a response time sufficiently short to adapt to ambient vibrations and speckle changes, but substantially longer than the vibration period;

whereby the surface displacement can be used to determine whether a disbond is present.

2. The method of claim 1 wherein producing transient heating comprises applying a generation laser pulse having an intensity and wavelength to the surface sufficient to cause lifting of the disbonded material and to induce membrane vibration.

3. The method of claim 2 wherein the large etendue interferometer is based on one of:

the photorefractive effect;

the photoelectromotive force; and

the polarization self-modulation effect.

4. The method of claim 2 wherein the large etendue interferometer is based on an array of interferometers followed by electronic processing, so as to use effectively a plurality of speckles.

5. The method of claim 2 wherein detecting any surface displacement comprises directing an interrogation laser beam of coherent light and a pump beam, both from a detection laser, onto a photorefractive material to produce a transient hologram within the photorefractive material.

6. The method of claim 5 wherein detecting any surface displacement comprises optically detecting interference of a reference beam produced by diffraction of the pump beam through the transient hologram, with respect to the interrogation beam.

7. The method of claim 5 wherein detecting any surface displacement comprises electrically detecting the transient hologram within the photorefractive material.

8. The method of claim 5 wherein directing the detection laser beam and directing the generation laser pulse onto the surface is performed by controlling a common set of optical components, such as by operating an intermittent or continuous beam moving device operable to scan across the surface of the bonded structure.

9. The method of claim 8 wherein controlling the common set of optical components involves operating a continuous beam moving device, and where detecting any surface displacement comprises applying a Doppler shift compensation using a velocity sensing arrangement and an acousto-optic shifter for frequency adjustment of one or both of the interrogation and pump beams.

10. The method of claim 2 wherein producing transient heating comprises applying a generation laser pulse having a pulse duration that is shorter than a time taken by an acoustic wave to pass through the membrane, reflect off a bottom thereof, and return to the surface, and the method further comprises analyzing a high frequency component of the detected surface displacement to obtain from a pulse echo interval, a thickness of the membrane.

11. The method of claim 10 wherein applying a generation laser pulse comprises applying the generation laser pulse for a duration less than 1 microsecond.

12. The method of claim 2 wherein detecting any surface displacement further comprises receiving a signal representing the surface displacement, and analyzing the signal to identify one of:

a highest amplitude pulse in the time domain and a highest amplitude frequency in the frequency domain.

13. The method of claim 12 wherein the bonded structure has an exposed first layer overlying a second material, and the method further comprises:

replicating the signal representing the surface displacement;

high pass filtering the replica; and

identifying one of a highest amplitude pulse within a time domain and a highest amplitude frequency within the frequency domain.

14. The method of claim 13 wherein the bonded structure is a honeycomb structured material having a honeycomb core sandwiched between two skins, the method further comprising:

applying a spectral analysis of the signal to identify spectral components in one of a plurality of frequency bands for the region, and

comparing the components within the region with those of other regions on the surface to identify a stiffened membrane vibration caused by a disbond between the honeycomb core and a distal one of the two skins.

15. The method of claim 13 wherein the bonded structure has a skin bonded to a core having a substantial proportion of material voids, and the method further comprises comparing a peak amplitude of the high pass filtered signal with that of the representative signal to determine whether the disbond is within the skin or between the skin and core.

16. The method as in claim 2 wherein producing transient heating in the region comprises applying sufficient energy to detach a stick bond.

17. An apparatus for assessing bond integrity at a region of a surface of a bonded material, the apparatus comprising:

a. a generation laser beam for producing transient heating in the region so that if the region overlies a disbond in the bonded material, membrane vibration having a vibration period will be induced over the disbond;

b. a large etendue interferometer for producing an interference in dependence on any surface displacement at the region, the large entendue interferometer having a response time sufficiently short to adapt to ambient vibrations and speckle changes, but substantially longer than the vibration period; and

c. a detector for detecting the interference.

18. The apparatus of claim 17 wherein the large etendue interferometer operates on one of a photoelectromotive force effect;

and a polarization self-modulation effect.

19. The apparatus of claim 17 wherein the large etendue interferometer consists of an array of single speckle interferometers the ouputs of which are compounded by electronic processing so as to effectively use a plurality of speckles.

20. The apparatus of claim 17 wherein large etendue interferometer comprises a beam splitter for separating a detection laser beam of coherent light into a pump beam, and an interrogation beam scattered off of the surface, and optical components for focusing the interrogation beam and pump beam onto a photorefractive material to produce a transient hologram within the photorefractive material.

21. The apparatus of claim 20 wherein the detector comprises an optical detector for detecting interference of a reference beam produced by diffraction of the pump beam through the transient hologram, with respect to the interrogation beam.

22. The apparatus of claim 20 wherein the detector comprises electrodes coupled to the photorefractive material for detecting a signal representative of the surface vibration.

23. The apparatus of claim 20 further comprising a beam moving device operable to scan the generation beam and interrogation beam across the surface of the bonded structure.

24. The apparatus of claim 23 further comprising a mechanism for moving the beam moving device to continuously scan the generation and interrogation beams across the surface, and the interferometer further comprises a Doppler frequency shift detection arrangement, as well as an acousto-optic shifter driven by the Doppler frequency shift detection arrangement for applying a frequency adjustment to one or both of the interrogation and pump beams to compensate for a Doppler shift.

25. The apparatus of claim 17 further comprising an analysis program for receiving a signal representing the detected surface displacement, and computing a highest amplitude frequency component.

26. The apparatus of claim 25 wherein the analysis program analyzing a high frequency component of the detected surface displacement to obtain from a pulse echo interval, the depth of the disbond.

27. The apparatus of claim 25 wherein the analysis program replicates a signal representing the surface displacement, high pass filters the replica, and identifies a highest amplitude pulse.

28. The apparatus of claim 25 wherein the bonded structure is a honeycomb structured material having a honeycomb core sandwiched between two skins, and the analysis program comprising spectral analysis program instructions for identifying spectral components in one of a plurality of frequency bands for the region, and comparing the components within the region with those of other regions on the surface to identify a stiffened membrane vibration caused by a disbond between the honeycomb core and a distal one of the two skins.

29. The apparatus of claim 27 wherein the bonded structure has a skin bonded to a substantially porous core, and the analysis program is further adapted to compare an amplitude and frequency of the high pass filtered signal with the representative signal to determine whether the disbond is within the skin or between the skin and core.