Structural health management architecture using sensor technology

• US 20060004499A1
• Filed: 06/30/2004
• Published: 01/05/2006
• Est. Priority Date: 06/30/2004
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Anderson, David M., Avery, Robert L., Akdeniz, Aydin, Reuter, Richard J., Haugse, Eric D., Trego, Angela, Greenberg, Cori
• Application Number:
  US10/880,659
• Publication Number:
  US 20060004499A1
• Time in Patent Office: Days
• US Class Current: 701/29
• CPC Class Codes: B64D 2045/008 Devices for detecting or indicating hard landing
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: B64F 5/60 Testing or inspecting aircraft components or systems
• CPC Class Codes: G07C 5/085 using electronic data carriers

Abstract

A mobile platform comprising at least one mobile platform system that includes a processor, a structure, and an SHM system. The SHM system also includes a processor as well as a structural sensor. The SHM processor is separate from the mobile platform system processor. In other preferred embodiments, the mobile platform includes a flight control system, a maintenance information system, and an IVHM system. The SHM system may receive parameters from the flight control system and calculate loads therefrom. Alternatively, the sensor may be a structural load sensor, which the SHM processor uses along with the parameters, to calculate other structural loads. In still another preferred embodiment, a method is provided that includes separating SHM functions from a processor of a mobile platform system. The method also includes dedicating an SHM system to perform SHM functions and establishing communications between the SHM system and the mobile platform system.

Claims

1. A mobile platform comprising:

at least one mobile platform system including a processor;

a mobile platform structure; and

a structural health management (SHM) system including;

a SHM processor in communication with the mobile platform system and separate from the mobile platform system processor, and

at least one sensor in communication with the SHM processor and configured to sense a condition of the mobile platform structure.

2. The mobile platform according to claim 1, the at least one mobile platform system further comprising a flight control system configured to sense flight parameters.

3. The mobile platform according to claim 2, wherein the SHM processor is configured to receive the flight parameters from the flight control system and to calculate a load on the mobile platform structure therefrom.

4. The mobile platform according to claim 2, further comprising a load sensor sensing a load on a portion of the structure, the SHM processor further configured to communicate with the load sensor and to calculate a load on another portion of the structure from the load on the portion of the structure and the flight parameters.

5. The mobile platform according to claim 1, wherein the mobile platform is an aircraft.

6. The mobile platform according to claim 1, the mobile platform system further comprising a maintenance information system in communication with the SHM system and to receive information from the SHM system.

7. The mobile platform according to claim 1, further comprising an area exposed to impact and the at least one SHM sensor including an impact sensor positioned near enough to the impact exposed area to sense impacts.

8. The mobile platform according to claim 7, the area further comprising at least one of a cargo bay door, a passenger door, a service door, or a galley.

9. The mobile platform according to claim 1, the at least one mobile platform system further comprising an integrated mobile platform health monitoring system, the SHM system separate from and in communication with the integrated mobile platform health monitoring system.

10. The mobile platform according to claim 1, wherein the at least one mobile platform system has an availability requirement associated therewith which is higher than an availability requirement associated with the SHM system.

11. The mobile platform according to claim 1, wherein the SHM processor further comprises at least one of an algorithm, a neural network, or a look up table.

12. The mobile platform according to claim 1, further comprising a battery to power the SHM system.

13. The mobile platform according to claim 1, further comprising an SHM sensor sampled by a ground portion of the SHM system.

14. The mobile platform according to claim 1, wherein the SHM system is a distributed system.

15. The mobile platform according to claim 1, wherein the sensor is located in a position where access thereto requires removal of at least one of a mobile platform component or mobile platform structural element.

16. The mobile platform according to claim 1, wherein the sensor to be a damage sensor to detect damage to the structure.

17. The mobile platform according to claim 1, wherein the sensor to sense a condition related to corrosion.

18. The mobile platform according to claim 1, further comprising a dedicated SHM sensor the dedicated SHM sensor communicating with the SHM processor via the other mobile platform system.

19. The mobile platform according to claim 1, wherein the at least one sensor is located at approximately at least one location selected from the group consisting of a lavatory, a galley, a floor beam, a door, a pressure bulkhead, a fuselage, a wing hard landing inspection area, a vertical stabilizer attachment, a pylon to wing attachment, a strut, a fuselage crown structure, a fuselage structure under wing to body fairing, a wing rib, a cockpit window sill, a wing center section, a fuselage structure above the wing center section, a main landing gear bay, and a fuselage structure in the bilge area.

20. A method of monitoring the health of a mobile platform including a structure and at least one mobile platform system including a processor, the method comprising:

separating system health management (SHM) functions from the processor of the at least one mobile platform system;

dedicating an SHM system that includes an SHM processor to perform the SHM functions, whereby the separate SHM processor enables an open architecture for the SHM processor; and

establishing communications between the SHM system and the at least one mobile platform system.

21. The method according to claim 20, further comprising accepting a flight parameter from the at least one mobile platform system.

22. The method according to claim 21, further comprising calculating a load on the mobile platform structure with the SHM processor using the flight parameters.

23. The method according to claim 20, further comprising sensing a load on a portion of the mobile platform structure, accepting the flight parameter, and calculating a load on another portion of the mobile platform structure using the flight parameter and the sensed load.

24. The method according to claim 20, wherein the mobile platform is an aircraft.

25. The method according to claim 20, further comprising communicating data from the SHM system to a maintenance information system of the at least one mobile platform system.

26. The method according to claim 20, further comprising sensing an impact to an impact exposed area of the mobile platform.

27. The method according to claim 20, further comprising the sensing occurring near at least one of a cargo bay door, a passenger door, a service door, or a galley of the mobile platform.

28. The method according to claim 20, further comprising communicating between the SHM system and an integrated vehicle health management system of the at least one mobile platform systems.

29. The method according to claim 20, further comprising meeting an availability requirement associated with the at least one mobile platform system, meeting an availability requirement associated with the SHM system, the SHM system availability requirement being less stringent than the at least one mobile platform system availability requirement.

30. The method according to claim 20, further comprising using at least one of an algorithm, a neural network, or a look up table to perform an SHM function.

31. The method according to claim 20, further comprising powering the SHM system with a battery.

32. The method according to claim 20, further comprising sensing a condition related to corrosion.

33. The method according to claim 20, further comprising sensing an SHM related condition with a sensor and communicating the sensed condition to the SHM system via the at least one mobile platform system.

34. The mobile platform according to claim 20, further comprising placing an SHM sensor at approximately at least one location selected from the group consisting of a lavatory, a galley, a floor beam, a door, a pressure bulkhead, a fuselage, a wing hard landing inspection area, a vertical stabilizer attachment, a pylon to wing attachment, a strut, a fuselage crown structure, a fuselage structure under wing to body fairing, a wing rib, a cockpit window sill, a wing center section, a fuselage structure above the wing center section, a main landing gear bay, and a fuselage structure in the bilge area.

35. An aircraft comprising:

at least one aircraft system including a processor, the at least one system including an integrated vehicle health management system and a flight control system sensing a flight parameter;

a structure;

a structural health management (SHM) system including;

a SHM processor separate from the at least one aircraft system processor, in communication with the flight control system to calculate a load from the flight parameter, including a neural network, and located on the ground;

at least one sensor, the at least one sensor in communication with the SHM processor and configured to sense a condition of the aircraft structure, the at least one sensor including an impact sensor positioned near an impact exposed area of the aircraft structure to sense impacts, the SHM processor to locate the impact; and

a battery to power the SHM system.

36. A system for a fleet of mobile platforms, comprising:

at least one mobile platform including

at least one mobile platform system including a processor,

a mobile platform structure, and

a mobile platform based structural health management (SHM) system including;

a SHM processor in communication with the mobile platform system and separate from the mobile platform system processor, and

at least one sensor in communication with the SHM processor and configured to sense a condition of the mobile platform structure; and

a ground based SHM system in communication with the mobile platform SHM system.