System and method for reporting emergencies from an aircraft

• US 6,963,292 B1
• Filed: 05/15/2002
• Issued: 11/08/2005
• Est. Priority Date: 05/15/2002
• Status: Expired due to Fees

• Current Assignee: Sprint Spectrum LP (Deutsche Telekom AG)
• Original Assignee: Sprint Spectrum LP (Deutsche Telekom AG)
• Inventors: White, Brian H.
• Primary Examiner(s): GOINS, DAVETTA WOODS
• Application Number:
  US10/146,155
• Time in Patent Office: 1,273 Days
• Field of Search: 340/963, 340/937, 340/988, 340/945, 340/541, 340/990, 340/426.12, 340/825.72, 701/3, 701/2, 701/36, 244/118.5, 713/200
• US Class Current: 340/963
• CPC Class Codes: B64D 45/0059 by communicating emergency situations to ground control or between crew members
• CPC Class Codes: G08B 25/12 Manually actuated calamity alarm transmitting arrangements emergency non-personal manually actuated alarm, activators, e.g. details of alarm push buttons mounted on an infrastructure
• CPC Class Codes: G08B 31/00 Predictive alarm systems characterised by extrapolation or other computation using updated historic data
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

A system and method is provided for passenger reporting of emergencies aboard an aircraft. An exemplary aircraft security system may have a panic device accessible to and activated by a passenger who may be seated. The panic device may be within a passenger compartment of an aircraft, and a wireless interface associated with the aircraft may respond to activation of the panic device by transmitting an emergency signal outside of the aircraft. The emergency signal may be indicative of panic data and/or aircraft data determined within the aircraft. The panic data may indicate the presence of an emergency within the aircraft, and the aircraft data may include the status of aircraft systems, telemetry data, and media transmission of the passenger compartment. The panic data and/or aircraft data may be extracted from the emergency signal and sent to authorities.

Claims

1. An aircraft security system comprising:

a panic device fixed to an aircraft and accessible to and activated by a seated passenger, wherein the panic device is within a passenger compartment of the aircraft;

a wireless interface associated with the aircraft that responds to activation of the panic device by transmitting an emergency signal outside of the aircraft; and

a control device in communication with the panic device and the wireless interface, wherein the panic device sends panic data to the control device, and wherein the panic device receives via the control device information for presentation to the seated passenger in response to the emergency signal transmitted outside of the aircraft.

2. The system of claim 1, wherein the emergency signal transmitted by the wireless interface is indicative of the panic data.

3. The system of claim 1 further comprising an aircraft data interface in communication with the control device, wherein the aircraft data interface sends aircraft data to the control device.

4. The system of claim 3, wherein the emergency signal transmitted by the wireless interface is indicative of the panic data and the aircraft data.

5. The system of claim 3 wherein the aircraft data comprises telemetry data for the aircraft.

6. The system of claim 5, wherein the telemetry data comprises an indication selected from the group consisting of an indication of a location coordinate of the aircraft, an indication of a orientation and routing of the aircraft, an indication of a horizontal and a vertical velocity of the aircraft, an indication of an origination and destination of the aircraft, and an indication of an altitude of the aircraft.

7. The system of claim 3, wherein the aircraft data comprises an indication selected from the group consisting of an indication of fuel status, an indication of engine status, an indication of computer status, an indication of navigation status, an indication of communications status, an indication of Global Positioning System status, an indication of radar status, an indication of transponder status, an indication of radio status, an indication of power generation and distribution status, an indication of flight control surfaces status, an indication of wing control status, an indication of rudder control status, an indication of landing gear status, an indication of flight management status, an indication of decompression status, an indication of automatic pilot status, an indication of hydraulics status, an indication of avionics status, an indication of sudden loss of altitude, and an indication of an explosion.

8. The system of claim 3 wherein at least a portion of the aircraft data is generated by Built In Test Equipment.

9. The system of claim 3, wherein the aircraft data comprises a media recording of the passenger compartment.

10. The system of claim 1 further comprising a base station that receives the emergency signal from the wireless interface.

11. The system of claim 10, wherein the wireless interface comprises a Personal Communications Services mobile station and the base station comprises a Personal Communications Services base station having a transceiver for communicating with the wireless interface.

12. The system of claim 10, wherein the base station extracts data from the emergency signal, and the data is sent to an emergency dispatcher.

13. The system of claim 12, wherein the data comprises at least one of panic data and aircraft data.

14. The system of claim 1, wherein the aircraft comprises a commercial airliner.

15. The system of claim 1, wherein the panic device is connected to a network of panic devices within the passenger compartment, and the network of panic devices is connected to the control device.

16. The system of claim 1, wherein the emergency signal is transmitted over a code division multiple access air interface.

17. The system of claim 1, wherein the aircraft further comprises a panic indicator that indicates the activation of the panic device.

18. The system of claim 17, wherein the panic indicator is prevented from indicating the activation of the panic device if a hijacking is occurring aboard the aircraft.

19. A method for reporting an emergency on an aircraft comprising:

activating a panic device fixed to the aircraft by a seated passenger within a passenger compartment of the aircraft;

sending panic data by the panic device to a control device;

transmitting an emergency signal outside of the aircraft in response to the seated passenger activating the panic device, wherein the emergency signal is indicative of the panic data sent from the panic device; and

sending to the panic device via the control device information for presentation to the seated passenger in response to the emergency signal transmitted outside of the aircraft.

20. The method of claim 19, wherein the emergency signal is further indicative of aircraft data determined within an aircraft data interface.

21. The method of claim 20 further comprising receiving the panic data and the aircraft data at the control device.

22. The method of claim 19 further comprising extracting data from the emergency signal and sending the data to an emergency dispatcher.

23. The method of claim 22, wherein the information for presentation to the seated passenger includes instructions from the emergency dispatcher for the seated passenger on how to respond to the emergency.

24. The method of claim 22 further comprising determining a type of the emergency from the data extracted from the emergency signal.

25. The method of claim 22 further comprising using the data to obtain identification information from an airline database.

26. The method of claim 25 further comprising using the identification information to obtain classification information from a records database.

27. A panic device for use in an aircraft, wherein the panic device is fixed to the aircraft, comprising:

a selection mechanism activated by a seated passenger during an emergency, wherein the selection mechanism has a plurality of possible selection states; and

a transceiver that receives panic data indicating the emergency from the selection mechanism and sends the panic data to a control device, and wherein the transceiver further receives information from the control device for presentation to the seated passenger in response to an emergency signal transmitted outside of the aircraft, the emergency signal being indicative of the panic data.

28. The panic device of claim 27, wherein the selection mechanism comprises at least one of a knob, a switch, a dial, and a button.

29. The panic device of claim 27, wherein the selection mechanism comprises an input interface for allowing the seated passenger to input the panic data.

30. The panic device of claim 29, wherein the input interface comprises at least one of a keypad, handwriting recognition area, and touch-screen display.

31. The panic device of claim 27 further comprising a display for presenting the information to the seated passenger, wherein the information includes at least one message regarding the emergency.

32. The panic device of claim 27, wherein the panic device has a location selected from the group consisting of a cushion on a seat, an armrest on a seat, a pop-up armrest panel on a seat, a ceiling above a seat, a floor below a seat and a wall adjacent to a seat.

33. The panic device of claim 27, wherein the panic data is selected from the group consisting of an indication of a bomb threat, an indication of a hijacking event, an indication of a pilot disabled, an indication of a passenger injury, an indication of a crew injury, an indication of a death, an indication of a request for medical attention, and an indication of a weapon threat.

34. The panic device of claim 27 further comprising an inadvertent activation prevention mechanism.