System and method for testing a composite structure using a laser ultrasound testing system

Patent metadata

Field	Value
Publication number	US-9625423-B2
Application number	US-201213663855-A
Country	US
Kind code	B2
Filing date	Oct 30, 2012
Priority date	Oct 30, 2012
Publication date	Apr 18, 2017
Grant date	Apr 18, 2017

Abstract

A method and apparatus for testing a composite structure. A pulsed laser beam having a number of properties is generated. Each of the number of properties is within a selected range. The pulsed laser beam generated by the generation laser system is directed towards a composite structure comprised of a number of composite materials. A number of ultrasonic waves are formed in the composite structure when the pulsed laser beam contacts the composite structure without causing any undesired inconsistencies in the composite structure outside of selected tolerances.

First claim

What is claimed is:

1. A system in a testing environment selected from the group consisting of a factory and an assembly line, the system comprising:
a generation laser system configured to generate from a laser a pulsed laser beam having a number of properties wherein the number of properties includes at least a spot size of the laser less than about 1 millimeter, an optical fluence per pulse of between about 0.1 millijoules per centimeters squared to about 1000 millijoules per centimeters squared, and a pulse repetition rate between about 10,000 hertz and about 500,000 hertz;
a transmission system configured to direct the pulsed laser beam generated by the generation laser system towards a composite structure comprised of a number of composite materials, wherein a number of ultrasonic waves are formed in the composite structure when the pulsed laser beam contacts the composite structure without causing any undesired inconsistencies in the composite structure outside of selected tolerances; and
a movement system configured to control movement of the transmission system and the pulsed laser beam within the testing environment and to move the laser over the composite structure.

2. The system of claim 1 , wherein a selected range for an energy per pulse is between about 1 microjoule and about 10,000 microjoules.

3. The system of claim 1 , wherein the composite material includes a reinforcement material.

4. The system of claim 1 , wherein the transmission system is a fiberoptic transmission system.

5. The system of claim 4 , wherein the fiberoptic transmission system comprises:
a number of optical fibers configured to carry the pulsed laser beam.

6. The system of claim 1 , wherein the movement system is a robotic arm.

7. The system of claim 1 further comprising:
a detection laser system configured to generate a pulsed detection laser beam towards the composite structure, wherein contact between the pulsed detection laser beam and the number of ultrasonic waves causes an alteration in a path of the pulsed detection laser beam; and
a detection system configured to detect the alteration, wherein the detection system comprises a number of detectors.

8. The system of claim 7 , wherein the generation laser system, the detection laser system, and the transmission system are part of a laser system in the system.

9. A method for testing a composite structure in a testing environment selected from the group consisting of a factory and an assembly line, the method comprising:
generating a pulsed laser beam having a number of properties in which each of the number of properties is within a selected range, wherein the number of properties includes a spot size less than about 1 millimeter, an optical fluence per pulse between about 0.1 millijoules per centimeters squared to about 1000 millijoules per centimeters squared, and a pulse repetition rate between about 10,000 hertz and about 500,000 hertz;
moving, using a movement system, the laser over the composite structure within the testing environment;
directing the pulsed laser beam generated by the laser generation system towards the composite structure, wherein a number of ultrasonic waves are formed in the composite structure when the pulsed laser beam contacts the composite structure without causing any undesired inconsistencies in the composite structure outside of selected tolerances; and
determining whether an inconsistency is present in the composite structure using the number of ultrasonic waves.

10. The method of claim 9 , wherein the number of properties additionally comprises:
an energy per pulse between about 1 microjoule and about 10,000 microjoules.

11. The method of claim 9 , wherein the step of directing the pulsed laser beam comprises:
directing the pulsed laser beam towards the composite structure through a number of optical fibers in a fiberoptic transmission system.

12. The method of claim 9 further comprising:
determining whether the inconsistency is an undesirable inconsistency for the composite structure; and
responsive to detecting the undesirable inconsistency, reworking or discarding the composite structure in the testing environment.

13. The method of claim 12 wherein the movement system is a robotic arm.

14. The method of claim 9 , further comprising:
generating a pulsed detection laser beam towards the composite structure;
altering a path of the pulsed detection laser beam when contact between the pulsed detection laser beam and a number of ultrasonic waves is detected; and
detecting the alteration.

15. The method of claim 14 , wherein the alteration is detected using detectors.

Assignees

• Boeing Co

Inventors

• Bossi Richard H
• Georgeson Gary Ernest
• Kollgaard Jeffrey Reyner
• Stewart Alan Frank
• Motzer William P
• Gordon Iii Clarence Lavere
• O'Donnell Matthew
• Xia Jinjun
• Pelivanov Ivan
• Wei Chen-Wei

Classifications

• G01N29/2418

  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 title

• G01N29/225 Primary

  Supports, positioning or alignment in moving situation · CPC title

• G01N29/343

  pulse waves, e.g. particular sequence of pulses, bursts · CPC title

• G01N2291/0231

  Composite or layered materials · CPC title

• G01N2021/1706

  in solids · CPC title