WIRELESS AIRCRAFT MAINTENANCE LOG

• US 20110140866A1
• Filed: 02/22/2011
• Published: 06/16/2011
• Est. Priority Date: 03/26/2008
• Status: Abandoned Application

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Geib, Andrew F., Donahue, Kevin, Ouzounov, Alexey Sergeev, Beacham, William H. JR., Masslon, Dale R., Weakley, Thomas Craig, Scheid, Paul Raymond
• Application Number:
  US13/032,235
• Publication Number:
  US 20110140866A1
• Time in Patent Office: Days
• US Class Current: 340/10.51
• CPC Class Codes: G06Q 10/06 Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
• CPC Class Codes: G06Q 50/40 Business processes related to the transportation industry shipping G06Q10/083
• CPC Class Codes: G07C 5/008 communicating information to a remotely located station transmission systems for measured values G08C

Abstract

A method of aircraft maintenance involves storing part information relating to an aircraft part on the aircraft part. The part information is wirelessly transmitting from the aircraft part to a receiver. A note of a change relating to the aircraft part is made. The part information with the note of the change relating to the aircraft part is electronically stored at a location remote from the aircraft part.

Claims

1. An aircraft part assembly comprising:

an aircraft part;

a metal data plate mounted on said aircraft part; and

a radio frequency identification tag (RFID tag) coupled to said metal data plate such that said metal data plate is an RFID tag resonator.

2. The aircraft part assembly of claim 1, wherein said RFID tag is between said metal data plate and said aircraft part.

3. The aircraft part assembly of claim 1, wherein said RFID tag comprises:

a writeable memory unit for storing part information;

a processor for processing part information;

a wireless transmitter in communication with the writeable memory unit; and

a wireless receiver in communication with the writable memory unit.

4. The aircraft part assembly of claim 3, wherein said part information comprises at least one of a revision history, a service history, a part configuration, a part number, and a serial number.

5. The aircraft part assembly of claim 1, wherein said RFID tag is capacitively coupled to said metal data plate.

6. The aircraft part assembly of claim 1, wherein said RFID tag is inductively coupled to said metal data plate.

7. The aircraft part assembly of claim 1, wherein said metal data plate is mounted to said aircraft part via a U-shaped bracket.

8. The aircraft part assembly of claim 7, wherein said RFID tag is mounted to a dielectric substrate within a gap defined by said U-shaped bracket.

9. The aircraft part assembly of claim 1, wherein said RFID tag is mounted to said metal data plate via a dielectric layer.

10. An aircraft part assembly comprising:

an aircraft part;

a metal data plate mounted on said aircraft part; and

a radio frequency identification (RFID) tag mounted between said aircraft part and said metal data plate.

11. The aircraft part assembly of claim 10, wherein said RFID tag comprises:

a writeable memory unit for storing part information;

a processor for processing part information;

a wireless transmitter in communication with the writeable memory unit; and

a wireless receiver in communication with the writable memory unit.

12. The aircraft part assembly of claim 11, wherein said part information comprises at least one of a revision history, a service history, a part configuration, a part number, and a serial number.

13. The aircraft part assembly of claim 10, wherein said data plate is coupled to said RFID tag such that said metal data plate is an RFID tag resonator.

14. The aircraft part assembly of claim 10, wherein said RFID tag is capacitively coupled to said metal data plate.

15. The aircraft part assembly of claim 10, wherein said RFID tag is inductively coupled to said metal data plate.

16. The aircraft part assembly of claim 10, wherein said metal data plate is mounted to said aircraft part via a U-shaped bracket.

17. A method of conducting aircraft maintenance, comprising the steps of:

receiving stored part information relating to an aircraft part from a radio frequency identification (RFID) tag coupled to a part data plate, such that said part data plate is an RFID tag resonator, on said part using a portable device;

receiving stored replacement part information relating to a replacement part from an RFID tag coupled to a replacement part data plate, such that said replacement part data plate is an RFID tag resonator, on said replacement part using said portable device;

formatting said part information and said replacement part information into an electronic document; and

wirelessly transmitting the electronic document to a server.

18. The method of claim 17, wherein each of said part information and said replacement part information comprises at least one of a revision history, a service history, a part configuration, a part number, and a serial number.

19. The method of claim 17, further comprising the step of transmitting new replacement part information from said portable device to said replacement part RFID tag, thereby causing said replacement part information to be overwritten with said new replacement part information.

20. The method of claim 17, wherein said server is on an aircraft containing said aircraft part.

21. The method of claim 20, further comprising the step of relaying the electronic document from said server to a remote server, wherein said remote server is away from said aircraft.