IP Library › Granted Patent US 10,677,715
Granted Patent B2
US 10,677,715 · App. 15/821,668 · Granted Jun 9, 2020

Thermography inspection for near-surface inconsistencies of composite structures

Inventors: Hong Hue Tat (Redmond, WA); William Joseph Tapia (Kapowsin, WA); Barry Allen Fetzer (Renton, WA); Gary E. Georgeson (Tacoma, WA); Martin L. Freet (Federal Way, WA); Jeffrey G. Thompson (Auburn, WA)
Assignee: The Boeing Company
G01N21/1702G01N25/72G01N29/041G01N2021/1706G01N2021/8472G01N2291/0231G01N2291/101
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Quick Facts
Patent No.
US 10,677,715
App. No.
15/821,668
Granted
Jun 9, 2020
Kind
B2
Abstract

Methods are presented. Signals are sent into a first surface of a structure using an ultrasonic transducer. Ultrasound response signals are received at the ultrasonic transducer. A portion of a second surface of the structure is heated while the ultrasonic transducer is sending signals into the first surface, wherein the second surface is on an opposite side of the structure from the first surface. Infrared images of the portion of the second surface of the structure are taken after heating the second surface.

Claims (38)

1. A method comprising:

sending signals into a first surface of a structure using an ultrasonic transducer;

receiving ultrasound response signals at the ultrasonic transducer;

heating a portion of a second surface of the structure while the ultrasonic transducer is sending signals into the first surface, wherein the second surface is on an opposite side of the structure from the first surface; and

taking infrared images of the portion of the second surface of the structure after heating the second surface.

2. The method of claim 1 further comprising:

identifying a region of localized thermal contrast in the infrared images; and

detecting an inconsistency within ¼ inch of the second surface of the structure using the region of localized thermal contrast.

3. The method of claim 1 , wherein the second surface is trapezoidal, the method further comprising:

detecting an inconsistency in a non-parallel leg of the second surface.

4. The method of claim 1 , wherein heating the portion of the second surface of the structure comprises heating the portion with a line heater.

5. The method of claim 1 , wherein heating the portion of the second surface of the structure comprises heating the portion with a heat lamp or a flash lamp.

6. The method of claim 5 , wherein the heat lamp or flash lamp and an infrared camera are connected to an end effector, the method further comprising:

moving the end effector relative to the structure after taking the infrared images of the portion of the second surface of the structure.

7. The method of claim 1 , wherein the structure is a composite structure.

8. The method of claim 1 , wherein taking infrared images of the portion of the second surface of the structure after heating the second surface comprises taking the infrared images using a number of infrared cameras, each infrared camera positioned at a different orientation relative to each other infrared camera.

9. The method of claim 1 further comprising:

measuring a size of an inconsistency using the ultrasound response signals and the infrared images.

10. The method of claim 9 , wherein the inconsistency is positioned in a co-cured composite interface or a co-bonded composite interface.

11. The method of claim 1 , wherein at least a fraction of the portion of the second surface is not parallel to the first surface.

12. The method of claim 1 , wherein the structure is a composite material, the method further comprising:

identifying an inconsistency non-planar to a majority of plies forming the structure using the infrared images.

13. The method of claim 1 further comprising:

identifying an inconsistency non-planar to the first surface using the infrared images.

14. A method comprising:

positioning a thermography system at a first position relative to a second surface of a structure, wherein the second surface comprises a plurality of sections in which each section of the plurality of sections has a different angle;

heating a portion of the second surface of the structure with a heat source of the thermography system to form a heated portion;

taking infrared images of the heated portion, wherein each section of the second surface within the heated portion has at least one infrared camera of the thermography system positioned within +/−30 degrees from an axis normal to the surface of the section; and

moving the thermography system to a second position relative to the second surface after taking the infrared images of the heated portion.

15. The method of claim 14 , wherein the thermography system comprises a number of infrared cameras, wherein each infrared camera of the thermography system is positioned at a different orientation relative to each other infrared camera of the thermography system.

16. The method of claim 14 further comprising:

detecting an inconsistency within ¼ inch of the second surface using the infrared images of the heated portion.

17. A method comprising:

performing ultrasonic inspection on a first surface of a composite structure;

performing thermographic inspection on a second surface of the composite structure, wherein the second surface is on an opposite side of the composite structure from the first surface, and wherein at least a fraction of the second surface is not parallel to the first surface; and

identifying near-surface inconsistencies for the second surface of the composite structure using the thermographic inspection.

18. The method of claim 17 , wherein the second surface of the composite structure is non-tooled.

19. The method of claim 17 , wherein at least one of the near-surface inconsistencies is non-parallel to the first surface of the composite structure.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 22, 2017
From: TAT, HONG HUE; TAPIA, WILLIAM JOSEPH; FETZER, BARRY ALLEN; GEORGESON, GARY E.; FREET, MARTIN L.; THOMPSON, JEFFREY G.
To: THE BOEING COMPANY
Reel/Frame 044202/0971 →
Continuity (1)
Related Publication 20190154565A1 · May 23, 2019
Cited By (1)
US 12,306,638