Onboard Maintenance System Network Optimization

• US 20120203401A1
• Filed: 02/08/2011
• Published: 08/09/2012
• Est. Priority Date: 02/08/2011
• Status: Abandoned Application

• Current Assignee: GE Aviation Systems LLC (GE Aerospace)
• Original Assignee: GE Aviation Systems LLC (GE Aerospace)
• Inventors: Dunsdon, Jonathan Mark, Thomson, Mark
• Application Number:
  US13/022,806
• Publication Number:
  US 20120203401A1
• Time in Patent Office: Days
• US Class Current: 701/3
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

An aircraft communication system includes an aircraft component, an Integrated Modular Avionics (IMA) unit, an Onboard Maintenance System (OMS), and a switch. The switch routes data provided by the aircraft component via a first communications protocol to the IMA unit, and mirrors the routed data to the OMS via a second communications protocol. The OMS processes and stores the received data, part of the received data, or the results of said processing.

Claims

1. An aircraft communication system comprising:

an aircraft component configured to provide data;

an Integrated Modular Avionics unit configured to receive the provided data;

an Onboard Maintenance System configured to receive the provided data; and

a switch configured to;

receive the data provided by the aircraft component,

route the provided data to the Integrated Modular Avionics unit, and

mirror the provided data to the Onboard Maintenance System.

2. The aircraft communication system of claim 1 wherein the switch is configured to route the data from the aircraft component to the Integrated Modular Avionics unit via a first communications protocol and mirrors the data to the Onboard Maintenance System in a second communications protocol.

3. The aircraft communication system of claim 1 wherein the first communications protocol is ARINC 664 part 7 or Avionics Full Duplex Switched Ethernet at 100 megabits per second.

4. The aircraft communication system of claim 1 wherein the second communications protocol is Institute of Electrical and Electronics Engineers (IEEE) 802 at 1 gigabit per second.

5. The aircraft communication system of claim 1 wherein the Integrated Modular Avionics unit is further configured to provide commands to the aircraft component via the switch.

6. The aircraft communication system of claim 1 wherein the Onboard Maintenance System is configured to store the data mirrored to the Onboard Maintenance System by the switch for up to 100 flights of an aircraft comprising the aircraft communication system.

7. An aircraft communications switch comprising:

a switching fabric configured to route data via a first communications protocol from an origin to a first destination; and

a port configured to provide routed data to a second destination via a second communications protocol.

8. The aircraft communications switch of claim 7 wherein the first communications protocol is ARINC 664 part 7 or Avionics Full Duplex Switched Ethernet at 100 megabits per second.

9. The aircraft communications switch of claim 7 wherein the second communications protocol is Institute of Electrical and Electronics Engineers (IEEE) 802 at 1 gigabit per second.

10. The aircraft communications switch of claim 7 wherein the origin is an aircraft component.

11. The aircraft communications switch of claim 7 wherein the destination is an Integrated Modular Avionics unit

12. The aircraft communications switch of claim 7 wherein the first destination is an Integrated Modular Avionics unit configured to provide commands to the origin via the switching fabric.

13. The aircraft communications switch of claim 7 wherein the second destination is an Onboard Maintenance System configured to store data mirrored to the Onboard Maintenance System via the port for up to 100 flights of an aircraft comprising the aircraft communications switch.

14. A method of communicating data on board an aircraft, said method comprising:

providing data from an aircraft component to a switch;

routing the provided data from the switch to an Integrated Modular Avionics unit of the aircraft; and

mirroring the provided data from the switch to an Onboard Maintenance System of the aircraft.

15. The method of claim 14 wherein the switch is configured to route the data from the aircraft component to the Integrated Modular Avionics unit via a first communications protocol and mirror the data to the Onboard Maintenance System in a second communications protocol.

16. The method of claim 14 wherein the first communications protocol is ARINC 664 part 7 or Avionics Full Duplex Switched Ethernet at 100 megabits per second.

17. The method of claim 14 wherein the second communications protocol is Institute of Electrical and Electronics Engineers (IEEE) 802 at 1 gigabit per second.

18. The method of claim 14 wherein the origin is an aircraft component.

19. The method of claim 14 wherein the destination is an Integrated Modular Avionics unit

20. The method of claim 14 wherein the Integrated Modular Avionics unit is configured to provide commands to the aircraft component via the switch, and the Onboard Maintenance System is configured to store data mirrored to the Onboard Maintenance System by the switch for up to 100 flights of an aircraft comprising the aircraft communication system.