Weak bond detection

Patent metadata

Field	Value
Publication number	US-9488620-B2
Application number	US-201214004594-A
Country	US
Kind code	B2
Filing date	Mar 15, 2012
Priority date	Mar 15, 2011
Publication date	Nov 8, 2016
Grant date	Nov 8, 2016

Abstract

Apparatuses and methods are disclosed for determining whether a structure of bonded layers includes locations where the layers are weakly bonded. Embodiments include evaluating the frequency response of the structure in response to vibrational inputs. Alternate embodiments include evaluating the non-linear response of the structure using a modal analysis. Further embodiments include obtaining the vibrational information with an accelerometer contacting the structure, while additional embodiments include exciting the structure with an impact force, which may be applied at multiple locations on the structure's surface. Still further embodiments include performing a MAC, COMAC, and/or FRF analysis. Still other embodiments include varying the amplitude of the input vibration. Additional embodiments locate the areas of weakened bonding. Still other embodiments include methods and apparatuses for simulating a laminated structure with defective bonding, such as kiss bonding.

First claim

What is claimed is:

1. A method, comprising the acts of:
vibrating a structure of bonded layers at a first amplitude by impacting the surface of the structure;
vibrating the structure at a second amplitude different from the first amplitude by impacting the surface of the structure;
evaluating a modal response of the structure to said vibrating at a first amplitude;
evaluating a modal response of the structure to said vibrating at a second amplitude;
correlating the modal responses; and
determining the existence of weak bonding between layers of the structure by identifying a weak correlation between the modal responses.

2. The method of claim 1 , wherein said vibrating at first and second amplitudes includes impacting the structure with a modal hammer.

3. The method of claim 1 , wherein said vibrating at first and second amplitudes includes vibrating the structure at multiple locations.

4. The method of claim 3 , wherein the vibration amplitude at each of the multiple locations is within ten percent (10%) of a target vibration amplitude.

5. The method of claim 3 , wherein the multiple locations form a repeating spatial pattern.

6. The method of claim 3 , wherein the multiple locations do not form a repeating spatial pattern.

7. The method of claim 3 , wherein each of the multiple locations is vibrated at the first and second amplitudes.

8. The method of claim 1 , comprising:
evaluating the frequency response for the first and second amplitudes.

9. The method of claim 8 , wherein the frequency response of each of the first and second amplitudes includes a modal vector and a phase associated with the modal vector, the method comprising:
evaluating the phase of the modal vectors of the frequency response for the first and second amplitudes.

10. The method of claim 9 , comprising:
comparing the modal parameters of the frequency response for the first and second amplitudes.

11. The method of claim 9 , wherein said evaluating includes evaluating a Coordinate Modal Assurance Criterion (COMAC) of the frequency response for the first and second amplitudes.

12. The method of claim 1 , wherein said evaluating includes comparing the modal responses at frequencies less than 1,000 Hz.

13. The method of claim 1 , wherein said evaluating includes comparing the modal responses at frequencies equal to at least 150 Hz and at most 650 Hz.

14. The method of claim 1 , wherein said evaluating includes performing a Complex Mode Indicator Function (CMIF) analysis of the modal response.

15. The method of claim 1 , wherein said evaluating includes performing a Complex Mode Indicator Function (CMIF) analysis of the frequency response.

16. The method of claim 1 , wherein said evaluating includes comparing the modal response to the modal response of a structure with no known weak bonding.

17. The method of claim 1 , wherein said evaluating includes creating a baseline modal response for a structure with no known weak bonding; and combining the baseline modal response with the modal response of the structure being evaluated.

18. The method of claim 1 , wherein said evaluating includes determining the locations where the modal response of the structure being evaluated differs from the modal response of a structure with no known weak bonding.

19. The method of claim 1 , wherein said evaluating includes evaluating the Coordinate Modal Assurance Criterion (COMAC) of the frequency response.

20. The method of claim 19 , wherein said evaluating the COMAC is performed for at least two separate modal points located between 150 Hz and 650 Hz inclusive.

21. The method of claim 1 , wherein said determining includes determining the location of the weak bonding by identifying a location of weak correlation between the modal responses.

22. The method of claim 21 , wherein said determining includes determining the location of the weak bonding within one centimeter (1 cm).

23. The method of claim 1 , further comprising:
sensing the response of the structure to said vibrating.

24. The method of claim 23 , wherein said sensing is accomplished by at least one accelerometer.

25. The method of claim 24 , wherein the at least one accelerometer is a single axis accelerometer.

26. The method of claim 24 , wherein the at least one accelerometer is a multiple axis accelerometer.

27. The method of claim 23 , wherein said sensing is accomplished by at least three accelerometers.

Assignees

• Adams Douglas E
• Sharp Nathan D
• Sterkenburg Ronald
• Purdue Research Foundation

Inventors

• Adams Douglas E
• Sharp Nathan D
• Sterkenburg Ronald

Classifications

• G01N29/045

  by imparting shocks to the workpiece and detecting the vibrations or the acoustic waves caused by the shocks (measuring resonant frequency G01H13/00; measuring strength properties by application of mechanical stress G01N3/00) · CPC title

• G01N3/32

  by applying repeated or pulsating forces · CPC title

• G01N29/46

  by spectral analysis, e.g. Fourier analysis {or wavelet analysis (spectral signal processing per se G06F17/14)} · CPC title

• G01N2291/02491

  Materials with nonlinear acoustic properties · CPC title

• G01M7/025 Primary

  Measuring arrangements · CPC title