Device and method to detect cracks in the countersink of a fastener

Patent metadata

Field	Value
Publication number	US-10234432-B2
Application number	US-201615228940-A
Country	US
Kind code	B2
Filing date	Aug 4, 2016
Priority date	Aug 4, 2016
Publication date	Mar 19, 2019
Grant date	Mar 19, 2019

Abstract

Disclosed are methods and systems to nondestructively detect cracks at or near a countersink of a fastener, such as a rivet, in a thin walled structure using Lamb waves. Generation and detection of Lamb waves at symmetric locations relative to the fastener provides signals used to calculate a symmetry parameter. The symmetry parameter represents a comparison of the relative amplitudes of the detected Lamb wave signals and provides a simple indication of whether a crack exists.

First claim

The invention claimed is:

1. A method for detecting cracks in a structure, the method comprising:
generating a first Lamb wave at a first location, wherein the first Lamb wave propagates towards a fastener in the structure;
detecting, via a detector at a first detector position, a first signal corresponding to the first Lamb wave subsequent to the first Lamb wave's interaction with the fastener;
generating a second Lamb wave at the first location;
detecting, at a second detector position, a second signal corresponding to the second Lamb wave subsequent to the second Lamb wave's interaction with the fastener, wherein the second detector position is symmetric to the first detector position relative to the fastener and the first location; and
calculating a first symmetry parameter from the first signal and the second signal, wherein the first symmetry parameter comprises a value representing a comparison of an amplitude of the first signal and an amplitude of the second signal.

2. The method of claim 1 , further comprising indicating that a crack exists in the structure when the first symmetry parameter exceeds a predetermined threshold.

3. The method of claim 1 , wherein calculating the first symmetry parameter comprises performing one or more of direct subtraction with integration, cross correlation, or integration of the first signal and the second signal.

4. The method of claim 3 , wherein the first and second signals are processed by one or more of signal envelope calculation and continuous wavelet analysis prior to calculating the first symmetry parameter.

5. The method of claim 1 further comprising:
generating a third Lamb wave at a second location, wherein the third Lamb wave propagates towards the fastener;
detecting, at a third detector position, a third signal corresponding to the third Lamb wave subsequent to the third Lamb wave's interaction with the fastener;
generating a fourth Lamb wave at the second location;
detecting, at a fourth detector position, a fourth signal corresponding to the fourth Lamb wave subsequent to the fourth Lamb wave's interaction with the fastener, wherein the fourth detector position is symmetric to the third detector position relative to the fastener and the second location; and
calculating a second symmetry parameter from the third signal and the fourth signal, wherein the second symmetry parameter comprises a value representing a comparison of an amplitude of the third signal and an amplitude of the fourth signal.

6. The method of claim 5 , further comprising indicating that a crack exists in the structure when the second symmetry parameter exceeds a predetermined threshold.

7. The method of claim 1 , wherein generating the first Lamb wave at the first location comprises using one or more of an electromagnetic acoustic transducer (EMAT), a super-conducting EMAT (SEMAT), and a pulsed laser to generate the first Lamb wave.

8. The method of claim 1 , wherein detecting the first signal corresponding to the first Lamb wave comprises using one or more of an interferometer, a SEMAT, a vibrometer, and a capacitive sensor to measure the first signal.

9. The method of claim 1 , wherein detecting the first signal corresponding to the first Lamb wave comprises moving the detector to the first detector position using an automated system, the automated system including a camera and a robotic positioning arm.

10. The method of claim 1 , wherein the structure comprises an aircraft skin and the fastener comprises a rivet countersunk in the aircraft skin.

11. A method for detecting cracks in a structure, the method comprising:
generating a first Lamb wave at a first location, wherein the first Lamb wave propagates towards a fastener in the structure;
detecting, at a first detector position, a first signal corresponding to the first Lamb wave subsequent to the first Lamb wave's interaction with the fastener;
generating a second Lamb wave at a second location, wherein the second location is symmetric to the first location relative to the fastener and the first detector position;
detecting, at the first detector position, a second signal corresponding to the second Lamb wave subsequent to the second Lamb wave's interaction with the fastener; and
calculating a first symmetry parameter from the first signal and the second signal, wherein the first symmetry parameter comprises a value representing a comparison of an amplitude of the first signal and an amplitude of the second signal.

12. The method of claim 11 , further comprising indicating that a crack exists in the structure when the first symmetry parameter exceeds a predetermined threshold.

13. The method of claim 11 , wherein calculating the first symmetry parameter comprises performing one or more of direct subtraction with integration, cross correlation, or integration of the first signal and the second signal.

14. The method of claim 13 , wherein the first and second signals are processed by one or more of signal envelope calculation and continuous wavelet analysis prior to calculating the first symmetry parameter.

15. The method of claim 11 , further comprising:
generating a third Lamb wave at a third location, wherein the third Lamb wave propagates towards the fastener;
detecting, at a second detector position, a third signal corresponding to the third Lamb wave subsequent to the third Lamb wave's interaction with the fastener;
generating a fourth Lamb wave at a fourth location, wherein the fourth location is symmetric to the third location relative to the fastener and the second location;
detecting, at the second detector position, a fourth signal corresponding to the fourth Lamb wave subsequent to the fourth Lamb wave's interaction with the fastener; and
calculating a second symmetry parameter from the third signal and the fourth signal, wherein the second symmetry parameter comprises a value representing a comparison of an amplitude of the third signal and an amplitude of the fourth signal.

16. The method of claim 15 , further comprising indicating that a crack exists in the structure when the second symmetry parameter exceeds a predetermined threshold.

17. A system for detecting cracks in a structure comprising:
a Lamb wave generation device that generates a first Lamb wave that propagates towards a fastener in the structure and that generates a second Lamb wave that propagates towards the fastener;
a Lamb wave detection device that provides a first signal corresponding to the first Lamb wave subsequent to the first Lamb wave's interaction with the fastener and provides a second signal corresponding to the second Lamb wave subsequent to the second Lamb wave's interaction with the fastener;
a positioning system that positions the Lamb wave detection device to measure the first signal at a first position and to measure the second signal at second position, wherein the first position is symmetric to the second position relative to the fastener and the Lamb wave generation device; and
a computing system comprising,
one or more processors, and
a memory system comprising one or more non-transitory computer readable media storing instructions that, when executed by the one or more processors, causes the computing system to calculate a symmetry parameter from the first signal and second signal and compare the symmetry parameter to a predetermined threshold,

wherein the symmetry parameter comprises a value representing a comparison of an amplitude of the first signal and an amplitude of the second signal.

18. The system of claim 17 , wherein the positioni

Assignees

• Boeing Co

Inventors

• Senderos Bruno Zamorano
• Sievers Daniel E

Classifications

• G01N2291/0289

  Internal structure, e.g. defects, grain size, texture · CPC title

• G01N29/50

  using auto-correlation techniques or cross-correlation techniques · CPC title

• G01N2291/0231

  Composite or layered materials · CPC title

• G01N2291/0427

  Flexural waves, plate waves, e.g. Lamb waves, tuning fork, cantilever · CPC title

• G01N29/48 Primary

  by amplitude comparison · CPC title