Nondestructive inspection of a structure including the analysis of cavity electromagnetic field response

• US 7,830,523 B2
• Filed: 10/26/2007
• Issued: 11/09/2010
• Est. Priority Date: 10/26/2007
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Whetham, William John, Bommer, Jason Philip
• Primary Examiner(s): Lyons; Michael A
• Application Number:
  US11/925,622
• Publication Number:
  US 20090108211A1
• Time in Patent Office: 1,110 Days
• Field of Search: 356/450, 736/34
• US Class Current: 356/450
• CPC Class Codes: G01N 22/02 Investigating the presence of flaws

Abstract

Nondestructive inspection (NDI) on a structure having a cavity includes exciting the structure with electromagnetic radiation and analyzing the cavity'"'"'s electromagnetic field response to detect a state change of the structure.

Claims

1. A method comprising performing nondestructive inspection (NDI) on a structure having a cavity, the NDI including exciting the structure with electromagnetic radiation;

analyzing the cavity'"'"'s electromagnetic field response to detect a state change of the structure; and

providing an indication of structural health of the structure based on the analysis of the cavity response.

2. The method of claim 1, wherein the structure is excited to exhibit the characteristics of an electromagnetic waveguide.

3. The method of claim 1, wherein the structure is excited to exhibit the characteristics of a cavity resonator.

4. The method of claim 1, wherein the excitation has a dominant electric field component.

5. The method of claim 1, wherein the excitation has a dominant magnetic field component.

6. The method of claim 1, wherein providing the indication includes correlating the cavity response to a state change of the structure.

7. The method of claim 1, wherein detecting the state change includes measuring the cavity response;

and wherein providing the indication includes comparing the measurements to baseline data for the structure.

8. The method of claim 1, wherein the NDI is performed continuously and the indication is provided automatically.

9. The method of claim 1, wherein the structure is an aircraft structure;

and wherein the NDI is performed in-flight.

10. The method of claim 9, wherein the NDI is performed following a lightning strike.

11. A method of analyzing structural health of an aircraft, the method comprising exciting different aircraft structures exhibiting RF characteristics with electromagnetic radiation and analyzing cavity responses to detect state changes of the structures.

12. The method of claim 11, wherein the excitation and analysis are performed in-flight.

13. The method of claim 11, wherein the excitation and analysis are performed following a lightning strike.

14. The method of claim 11, wherein the excitation and analysis are performed following severe turbulence.

15. The method of claim 11, further comprising identifying those structures whose states changed.

16. The method of claim 11 wherein providing the indication includes identifying the nature and degree of any state changes from signatures and sizes of the responses.

17. The method of claim 11, wherein analyzing the cavity responses includes correlating measurements of the cavity responses to baseline data for the aircraft structures.

18. The method of claim 11, wherein the at least one structure excited with electromagnetic radiation includes at least one of a fuselage, wings and stabilizers.

19. The method of claim 11, wherein the aircraft structures include a fuselage, and wherein the fuselage is excited and analyzed as a single cavity.

20. The method of claim 11, wherein the aircraft structures includes wings, and wherein each wing is excited and analyzed as having multiple cavities.

21. Apparatus comprising an analyzer for performing nondestructive inspection (NDI) on a structure having a cavity, the analyzer analyzing measurements of cavity responses to electromagnetic excitation of the structure, the analysis performed to detect a state change of the structure;

the analyzer also providing an indication of structural health of the structure after the cavity response has been analyzed.

22. The apparatus of claim 21, further comprising at least one element for providing the electromagnetic excitation and measuring the cavity responses.

23. An aircraft comprising a plurality of structures having cavities;

and a system for performing performing nondestructive inspection (NDl) on at least one of the structures, the system including

electromagnetic excitation apparatus for exciting at least one of those structures exhibiting RF characteristics with electromagnetic radiation; and

field response measurement apparatus for measuring field responses to the electromagnetic excitation, the measurements providing information about any state changes of the structures excited with electromagnetic radiation.

24. The aircraft of claim 23, further comprising an analyzer for analyzing the measurements to detect any state changes of the structures.

25. The aircraft of claim 23, wherein the excitation apparatus and the measurement apparatus are operable during flight.

26. The aircraft of claim 23, wherein the state changes include those state changes that relate to structural health of the aircraft.

27. The aircraft of claim 23, further comprising a system for suggesting an appropriate action in response to those state changes that relate to the structural health of the aircraft.

28. The aircraft of claim 23, wherein the electromagnetic excitation apparatus includes a passive antenna that is integrated with an aircraft structure.