Apparatus and method of providing power control based on environmental conditions

• US 5,889,466 A
• Filed: 01/14/1997
• Issued: 03/30/1999
• Est. Priority Date: 01/14/1997
• Status: Expired due to Term

• Current Assignee: Rockwell Collins, Inc. (Rtx Corporation)
• Original Assignee: Sony Transcom Incorporated (Rockwell International Corporation), Sony Corporation (Sony Group Corp.)
• Inventors: Ferguson, Bruce R.
• Primary Examiner(s): Hofsass, Jeffrey A.
• Assistant Examiner(s): LIEU, JULIE BICHNGOC
• Application Number:
  US08/783,604
• Time in Patent Office: 805 Days
• Field of Search: 340/602, 340/584, 307/29, 307/116, 307/112, 307/115, 307/117, 307/118
• US Class Current: 340/602
• CPC Class Codes: B64D 11/0015 Arrangements for entertainment or communications, e.g. radio, television
• CPC Class Codes: B64D 11/00155 Individual entertainment or communication system remote controls therefor, located in or connected to seat components, e.g. to seat back or arm rest
• CPC Class Codes: B64D 47/00 Equipment not otherwise provided for

Abstract

The present invention is a method and apparatus for controlling power supply to aircraft electronic systems based on ambient environmental conditions. The apparatus comprises a monitor for detecting an environmental condition, a power supply for providing power, a circuit which receives power from the power supply, and a switch coupled to the monitor. Upon detection of the environmental condition, the switch connects the power supply to the circuit, otherwise the switch disconnects the circuit from the power supply.

Claims

1. A power control apparatus for an in-flight entertainment system, comprising:

power supply means for providing power;

monitor means for detecting an on-board environmental condition, said monitor means receiving power independently of the environmental condition deteted by said monitor;

a power circuit for receiving power from the power supply and for coupling power to an electronic system; and

switch means coupled to the monitor means, said switch means for connecting the power supply means to the power circuit for providing power to the in-flight entertainment system upon detection of the environmental condition and otherwise completely disconnecting the power circuit from the power supply means without interrupting power to the monitor.

2. The apparatus as recited in claim 1, wherein the monitor means comprises a temperature sensor and the environmental condition is a predetermined temperature range.

3. The apparatus as recited in claim 1, wherein the monitor means comprises a humidity sensor and the environmental condition is a predetermined humidity range.

4. The apparatus as recited in claim 1, wherein the monitor means comprises a temperature sensor, a humidity sensor and an AND gate that is coupled to the temperature sensor and the humidity sensor and wherein the environmental condition is the presence of a predetermined temperature range and a predetermined humidity range.

5. The apparatus as recited in claim 1, wherein the environmental condition is within a predetermined range.

6. The apparatus as recited in claim 1, wherein the environmental condition is outside a predetermined range.

7. A power control apparatus for an in-flight entertainment system, comprising:

a first power supply;

a second power supply;

a monitor coupled to the second power supply for detecting an on-board environmental condition, said monitor receiving power from the second power supply independently of the environmental condition detected by said monitor;

a circuit configured to receive power from the first power supply; and

a switch coupled to the monitor, said switch for connecting the first power supply to the circuit upon detection of the environmental condition and for otherwise completely disconnecting the circuit from the first power supply without interrupting power to the monitor, wherein the in-flight entertainment system or components thereof is selectively energized or deenergized in response to the on-board environmental condition.

8. The apparatus as recited in claim 7, wherein the monitor comprises a temperature sensor and the environmental condition is a predetermined temperature range.

9. The apparatus as recited in claim 7, wherein the monitor comprises a humidity sensor and the environmental condition is a predetermined humidity range.

10. The apparatus as recited in claim 7, wherein the environmental condition is within a predetermined range.

11. The apparatus as recited in claim 7, wherein the environmental condition is outside a predetermined range.

12. The apparatus as recited in claim 7, wherein the monitor comprises a temperature sensor, a humidity sensor and an AND gate that is coupled to the temperature sensor and the humidity sensor and wherein the environmental condition is the presence of a predetermined temperature range and a predetermined humidity range.

13. A power control apparatus for an in-flight entertainment system, comprising:

a power supply for providing power;

a monitor for detecting an on-board environmental condition, the monitor receiving power independently of the environmental condition detected by said monitor;

a power circuit which receives power from the power supply and couples it to the in-flight entertainment system to provide power thereto; and

a switch coupled to the monitor, said switch for connecting the power supply to the power circuit upon detection of the environmental condition and otherwise completely disconnecting the power circuit from the power supply without interrupting power to the monitor.

14. The apparatus as recited in claim 13, wherein the monitor comprises a temperature sensor and the environmental condition is a predetermined temperature range.

15. The apparatus as recited in claim 13, wherein the monitor comprises a humidity sensor and the environmental condition is a predetermined humidity range.

16. The apparatus as recited in claim 13, wherein the environmental condition is within a predetermined range.

17. The apparatus as recited in claim 13, wherein the environmental condition is outside a predetermined range.

18. The apparatus as recited in claim 13, wherein the monitor comprises a temperature sensor, a humidity sensor and an AND gate that is coupled to the temperature sensor and the humidity sensor and wherein the environmental condition is the presence of a predetermined temperature range and a predetermined humidity range.

25. The method as recited in claim 17, wherein in the detecting, the monitor comprises a humidity sensor and the environmental condition is a predetermined humidity range.

19. A method of controlling power supply in an aircraft in-flight entertainment system, comprising:

detecting an on-board environmental condition;

determining if the environmental condition is within a predetermined range independently of the detected environmental condition; and

connecting a power supply to the aircraft in-flight entertainment system upon determination of the environmental condition being within said predetermined range, otherwise completely disconnecting the in-flight entertainment system from the power supply without interrupting said detecting.

20. The method as recited in claim 19, wherein in the determining, the predetermined range is a predetermined temperature range.

21. The method as recited in claim 19, wherein in the determining the predetermined range is a predetermined humidity range.

22. The method as recited in claim 19, wherein in the determining, the predetermined range is a predetermined temperature range and a predetermined humidity range.

23. A method of controlling power supply in an in-flight entertainment system, comprising:

providing a first power supply and a second power supply;

detecting an on-board environmental condition using a monitor that receives power from the second power supply independently of the environmental condition detected by said monitor; and

connecting the first power supply to a circuit in an in-flight entertainment system upon detection of the environmental condition and completely disconnecting the circuit from the first power supply without interrupting power to the monitor when the environmental condition is no longer detected.

24. The method as recited in claim 23, wherein in the detecting, the monitor comprises a temperature sensor and the environmental condition is a predetermined temperature range.

26. The method as recited in claim 23, wherein in the detecting, the monitor comprises a temperature sensor, a humidity sensor and an AND gate that is coupled to the temperature sensor and the humidity sensor and wherein the environmental condition is the presence of a predetermined temperature range and a predetermined humidity range.

27. The method as recited in claim 23, wherein in the detecting, the environmental condition is within a predetermined range.

28. The method as recited in claim 23, wherein in the detecting, the environmental condition is outside a predetermined range.