METHODS AND SYSTEM FOR BACKUP POWER SUPPLY

• US 20100103628A1
• Filed: 10/29/2008
• Published: 04/29/2010
• Est. Priority Date: 10/29/2008
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Steffler, Joseph B.
• Granted Patent: US 7,952,329 B2
• Time in Patent Office: Days
• US Class Current: 361/730
• CPC Class Codes: G07C 5/085 using electronic data carriers
• CPC Class Codes: H05K 5/021 specially adapted for data recorders, e.g. for flight recorders

Abstract

A system and methods for an avionics system are provided. The avionics system includes an enclosure, a recording device positioned within the enclosure, and an energy storage device positioned within the enclosure wherein the energy storage device electrically coupled to the recording device to supply electrical power to the recording device for a time period of greater than thirty seconds

Claims

1. An avionics system comprising:

an enclosure;

a recording device positioned within said enclosure; and

an energy storage device positioned within said enclosure, said energy storage device electrically coupled to said recording device to supply electrical power to said recording device for a time period of greater than thirty seconds.

2. An avionics system in accordance with claim 1 further comprising an electrical connector extending through said enclosure, said electrical connector configured to electrically couple at least one of said recording device and said energy storage device to a source of electrical power external to said enclosure.

3. An avionics system in accordance with claim 1 wherein said recording device comprises a cockpit voice recorder.

4. An avionics system in accordance with claim 1 wherein said energy storage device is capable of supplying all electrical power requirements of said recording device for a time period of greater than ten minutes.

5. An avionics system in accordance with claim 1 wherein said energy storage device is capable of supplying all electrical power requirements of said recording device for a time period of approximately twenty minutes.

6. An avionics system in accordance with claim 1 wherein said energy storage device comprises an electrochemical storage device.

7. An avionics system in accordance with claim 1 wherein said energy storage device comprises a supercapacitor.

8. An avionics system in accordance with claim 1 wherein said energy storage device comprises a ceramic material.

9. An avionics system in accordance with claim 1 wherein said energy storage device comprises barium titanate.

10. An avionics system in accordance with claim 1 further comprising a maintenance module electrically coupled to the energy storage device, said maintenance module configured to maintain a predetermined energy storage capability within the energy storage device.

11. A method of providing an integrated back up power supply for an avionics unit, said method comprising:

providing an enclosure;

positioning a voice recorder within the enclosure;

positioning an energy storage device within the enclosure, the energy storage device electrically coupled to said voice recorder, said energy storage device capable of providing all the electrical power requirements for the operation of the voice recorder for a time period greater than ten minutes.

12. A method in accordance with claim 11 wherein said providing an enclosure comprises providing a retrofit enclosure having substantially similar dimensions as an avionics unit being replaced by the avionics unit including the integrated back up power supply.

13. A method in accordance with claim 11 wherein said providing an enclosure comprises providing a retrofit enclosure that is plug compatible with an avionics unit being replaced by the avionics unit including the integrated back up power supply.

14. A method in accordance with claim 11 further comprising electrically coupling at least one of the voice recorder and the energy storage device to a power supply bus of an aircraft.

15. A method in accordance with claim 11 further comprising electrically coupling a maintenance module to the energy storage device, said maintenance module configured to maintain a predetermined energy storage capability within the energy storage device.

16. A method of providing a back up power supply for an avionics equipment integrated into a single enclosure of an avionics unit, said method comprising:

disconnecting a first avionics unit from an electrical connector that includes power supply wires to the first avionics unit;

removing the first avionics unit from a mounting location;

installing a second avionics unit into the mounting location; and

electrically coupling the second avionics unit to the electrical connector, the second avionics unit comprising a back up energy storage device within an interior of the second avionics unit, the back up energy storage device capable of providing all the electrical power requirements for the operation of the second avionics unit for a time period greater than ten minutes.

17. A method in accordance with claim 16 wherein electrically coupling the second avionics unit to the electrical connector comprises electrically coupling a sound recorder to a primary power supply that supplies power to the voice recorder during normal operation.

18. A method in accordance with claim 17 further comprising supplying back up power to the sound recorder from a back up power supply when the primary power supply is not available.

19. A method in accordance with claim 17 further comprising supplying back up power to the sound recorder from at least one of a supercapacitor and an electrochemical energy storage device.

20. A method in accordance with claim 17 further comprising electrically coupling a maintenance module to the back up energy storage device, said maintenance module configured to maintain a predetermined energy storage capability within the energy storage device.