CONTROL CHANNEL FOR VEHICLE SYSTEMS USING THE VEHICLE'S POWER DISTRIBUTION SYSTEM

• US 20080300750A1
• Filed: 05/30/2007
• Published: 12/04/2008
• Est. Priority Date: 05/30/2007
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Davis, Terry L., VonDoenhoff, Roger C., Shetty, Sudhakar
• Application Number:
  US11/755,386
• Publication Number:
  US 20080300750A1
• Time in Patent Office: Days
• US Class Current: 701/36
• CPC Class Codes: B64D 2221/00 Electric power distribution systems onboard aircraft
• CPC Class Codes: H04B 2203/5458 Monitor sensor; Alarm systems
• CPC Class Codes: H04B 3/546 Combination of signalling, telemetering, protection circuits for remote indication of supply or distribution network condition H02J13/00
• CPC Class Codes: H04L 12/462 LAN interconnection over a bridge based backbone
• CPC Class Codes: H04L 2012/4028 the transportation system being an aircraft

Abstract

A control channel for controlling a system of a vehicle may include an electrical power distribution system for supplying electrical power to a plurality of different systems onboard the vehicle. The control channel may also include a first interface to convert a signal for controlling or communicating with a selected vehicle system of the plurality of different systems on board the vehicle into a format for insertion and transmission over a power line that also supplies electrical power to the selected vehicle system, wherein the power line forms a part of the electrical power distribution system of the vehicle. The control channel may also include a second interface to convert a signal received over the power line into a format for use by the selected vehicle system.

Claims

1. A control channel for controlling a system of a vehicle, comprising:

an electrical power distribution system for supplying electrical power to a plurality of different systems onboard the vehicle;

a first interface to convert a signal for controlling or communicating with a selected vehicle system of the plurality of different systems on board the vehicle into a format for insertion and transmission over a power line that also supplies electrical power to the selected vehicle system, wherein the power line forms a part of the electrical power distribution system of the vehicle; and

a second interface to convert a signal received over the power line into a format for use by the selected vehicle system.

2. The control channel of claim 1, wherein the first interface is associated with a first component of the selected vehicle system and the second interface is associated with a second component of the selected vehicle system to permit communications between the first and second components of the selected vehicle system over the electrical power distribution system of the vehicle that also supplies electrical power to each of the components.

3. The control channel of claim 1, wherein the first interface and the second interface form a single bidirectional interface and wherein the control channel further comprises a bidirectional interface associated with each component of the selected vehicle system, wherein the bidirectional interface is adapted to both convert signals to a format for insertion and transmission over the electrical power distribution system of the vehicle and to convert signals received over the electrical power distribution system of the vehicle for use by the component of the selected vehicle system.

4. The control channel of claim 1, wherein the electrical power distribution system simultaneously supplies electrical power and control or communications signaling to the selected vehicle system.

5. The control channel of claim 1, wherein the electrical power distribution system simultaneously supplies electrical power and control or communications signaling between components of the selected vehicle system.

6. The control channel of claim 1, further comprising a bridging link associated with each interface to physically connect each interface to the electrical power distribution system.

7. The control channel of claim 1, wherein each of the first and second interfaces are adapted for out-of-band secure signaling over the electrical power distribution system.

8. The control channel of claim 1, further comprising a controller to control transmission of data over the electrical power distribution system.

9. The control channel of claim 1, wherein the first interface converts Ethernet data signals into one of BPL, X10, PLC and symmetrical hi-broadband BPL type signals for insertion into the electrical power distribution system, and wherein the second interface converts the BPL, X10, PLC or symmetrical hi-broadband BPL types signals from the vehicle'"'"'s electrical power distribution system into Ethernet data signals for use by the selected vehicle system.

10. The control channel of claim 1, wherein the first and second interfaces are each respectively adapted to convert Ethernet data signaling into one of BPL type signaling, X10 type signaling, automotive-style PLC and symmetrical hi-broadband BPL type signaling for insertion into the electrical power distribution system, and to convert the BPL, X10, automotive-style PLC or symmetrical hi-broadband BPL type signaling from the power distribution system into Ethernet data signaling for use by an associated component of the selected vehicle system.

11. A system for transmitting electrical power and communications over an aerospace vehicle'"'"'s electrical power system, comprising:

a first interface to convert a signal for controlling or communicating with a selected aerospace vehicle system of a plurality of different systems on board the aerospace vehicle into a format for insertion and transmission over a power line that also supplies electrical power to the selected aerospace vehicle system, wherein the power line forms a part of the electrical power distribution system of the aerospace vehicle; and

a second interface to convert a signal received over the power line into a format for use by the selected aerospace vehicle system.

12. The system of claim 11, wherein the first interface and the second interface are combined in a single bidirectional interface and wherein the system further comprises a bidirectional interface associated with each component of the selected aerospace vehicle system, wherein the bidirectional interface is adapted to both convert signals to a format for insertion and transmission over the electrical power distribution system of the aerospace vehicle and to convert signals received over the electrical power distribution system of the aerospace vehicle for use by the component of the selected aerospace vehicle system.

13. The system of claim 11, wherein the aerospace vehicle is a passenger aircraft and wherein the power distribution system supplies electrical power and out-of-band secure communications to each passenger seat.

14. The system of claim 11, wherein the each of the first and second interfaces are adapted for out-of-band secure signaling over the electrical power distribution system.

15. The system of claim 11, wherein the aerospace vehicle is a passenger aircraft and further comprising a first and second interface associated with each passenger seat for at least one of data and voice communications over the electrical power distribution system of the passenger aircraft.

16. The system of claim 11, further comprising a bridging link associated with each interface to physically connect each interface to the electrical power distribution system.

17. The system of claim 11, further comprising a controller to control transmission of communications or data over the electrical power distribution system.

18. The system of claim 17, wherein the controller comprises a fault annunciation circuit, a signal transmission control circuit, a signal monitoring circuit, and an output device to present system'"'"'s control data.

19. An aerospace vehicle, comprising:

a plurality of vehicle systems for operation of the aerospace vehicle;

an electrical power distribution system for supplying electrical power to each of the plurality of vehicle systems; and

a control channel associated with each vehicle system for controlling operation of each of the vehicle systems by sending control data signals to each of the vehicle systems over the electrical power distribution system that also supplies electrical power to each of the systems.

20. The aerospace vehicle of claim 19, wherein the control channel is adapted for out-of-band secure communications over the electrical power distribution system of the aerospace vehicle.

21. The aerospace vehicle of claim 19, wherein each control channel comprises an interface to convert a signal for controlling or communicating with the associated aerospace vehicle system of the plurality of systems on board the aerospace vehicle into a format for insertion and transmission over a power line that also supplies electrical power to the associated aerospace vehicle system, wherein the power line forms a part of the electrical power distribution system of the aerospace vehicle.

22. The aerospace vehicle of claim 21, wherein each control channel further comprises a second interface to convert a signal received over the power line into a format for use by the selected aerospace vehicle system.

23. The aerospace vehicle of claim 21, further comprising a bridging link associated with each interface to physically connect each interface to the electrical power distribution system of the aerospace vehicle.

24. The aerospace vehicle of claim 19, wherein each control channel comprises an interface to at one of convert Ethernet data signaling into one of BPL type signaling, X10 type signaling, automotive-style PLC type signaling and symmetrical hi-broadband BPL type signaling for insertion into the electrical power distribution system, and convert the BPL, X10, PLC or symmetrical hi-broadband BPL type signaling from the electrical power distribution system into Ethernet data signaling for use by the associated vehicle system.

25. A method for transmitting electrical power and communications over an aerospace vehicle'"'"'s power system, comprising:

generating a signal for transmission to a selected aerospace vehicle system;

converting the signal to a converted signal in a format for transmission over the aerospace vehicle'"'"'s electrical power system;

inserting the converted signal on a power line of the electrical power system; and

receiving the converted signal at the selected aerospace vehicle system via the power line.

26. The method of claim 25, further comprising:

extracting the received signal from the power line at the selected aerospace vehicle system; and

converting the received signal to another format for use by the aerospace vehicle system.

27. The method of claim 25, further comprising supplying communications and electrical power to each passenger seat in the aerospace vehicle over the aerospace vehicle'"'"'s electrical power system.

28. The method of claim 25, wherein converting the signal to a converted signal in a format for transmission over the aerospace vehicle'"'"'s electrical power system comprises converting the signal for out-of band secure communications.

29. The method of claim 25, wherein converting the signal to a converted signal in a format for transmission over the aerospace vehicle'"'"'s electrical power system comprises converting the signal to one of a BPL type signal, an X10 type signal, an automotive-style PLC type signal and a hi-broadband BPL type signal.