Automatic downlink messaging during emergency flight situations

• US 8,428,793 B2
• Filed: 07/31/2007
• Issued: 04/23/2013
• Est. Priority Date: 07/31/2007
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Mettes, W. Jerry
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): PIPALA, EDWARD J
• Application Number:
  US11/831,317
• Publication Number:
  US 20090037037A1
• Time in Patent Office: 2,093 Days
• Field of Search: 701/1, 701/3, 701/4, 701 7- 9, 701/11, 701/14, 701/29, 701/36, 701/207, 701/213, 701/300, 701/29.1, 701/29.2, 701/29.6, 701/31.4, 701/31.5, 701/32.3, 701/32.4, 701/32.7, 701/33.2, 701/33.3, 701/33.4, 340/945, 340/961, 340/963, 340488-490, 340/971, 340/993, 340/994, 244/75.1, 244/76.R, 244/175, 244/194, 731/78.R
• US Class Current: 701/11
• CPC Class Codes: G08G 5/00 Traffic control systems for aircraft , e.g. air-traffic control [ATC]
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

According to an example embodiment, a method includes receiving an emergency status signal indicating that an aircraft is in an emergency condition, formatting a downlink message in response to receiving the emergency status signal, the downlink message describing the emergency condition and an autopilot response to the emergency condition, and transmitting the downlink message to a controller of the aircraft.

Claims

1. A method comprising:

receiving an emergency status signal indicating that an aircraft is in an emergency condition;

formatting a downlink message by a processor in response to receiving the emergency status signal, the downlink message describing the emergency condition and an autopilot response to the emergency condition; and

transmitting the downlink message to a controller of the aircraft.

2. The method of claim 1, wherein the emergency condition is an Emergency Descent Mode (EDM).

3. The method of claim 1, further comprising monitoring for a safe signal, the safe signal indicative that an aircraft crewmember has manually responded to the emergency condition.

4. The method of claim 3, wherein transmitting the downlink message comprises transmitting the downlink message after a time interval measured from receiving the emergency status signal has elapsed and in response to determining that the safe signal was not received during the time interval.

5. The method of claim 1, wherein the downlink message comprises a Controller Pilot Data Link Communication (CPDLC) emergency report.

6. The method of claim 5, wherein the CPDLC emergency report comprises a MAYDAY message element.

7. The method of claim 6, wherein the CPDLC emergency report further comprises an Air Traffic Control (ATC) Position Report.

8. An aircraft communication system comprising:

an emergency status indicator;

a processor coupled to the emergency status indicator, the processor configured to prepare an emergency Controller Pilot Data Link Communication (CPDLC) message in response to receiving an emergency status signal from the emergency status indicator, the emergency CPDLC message comprising data that describes an autopilot command generated in response to the emergency; and

a transceiver coupled to the processor, the transceiver configured to receive the emergency CPDLC message from the processor and transmit the emergency CPDLC message to an aircraft controller station.

9. The aircraft communication system of claim 8, further comprising an autopilot coupled to the processor, the processor configured to receive an autopilot signal from the autopilot.

10. The aircraft communication system of claim 9, the emergency CPDLC message comprising data that describes an emergency that prompted the emergency status signal.

11. The aircraft communication system of claim 8, the emergency comprising a loss of cabin pressure.

12. The aircraft communication system of claim 9, further comprising an input interface coupled to the processor, the input interface configured to allow an operator of the aircraft to input data to the processor.

13. The aircraft communication system of claim 12, further comprising a display device coupled to the processor, the display device configured to visually prompt and notify the operator of relevant data.

14. A processor-readable non-transient storage medium, that when read, causes a processor in an aircraft to perform functions comprising:

preparing a Controller Pilot Data Link Communication (CPDLC) message in response to receiving an emergency status signal including text that indicates an Emergency Descent Mode has been activated; and

transmitting the CPDLC message.

15. The processor-readable medium of claim 14, wherein transmitting the CPDLC message comprises waiting a predetermined amount of time prior to transmitting the CPDLC message.

16. The processor-readable medium of claim 14, wherein preparing the CPDLC message comprises inserting text that indicates an Emergency Descent Mode has been activated.

17. The processor-readable medium of claim 16, wherein preparing the CPDLC message further comprises inserting text that indicates a number of Souls On Board (SOB) the aircraft.

18. The processor-readable medium of claim 17, wherein preparing the CPDLC message further comprises inserting text that indicates an altitude that the aircraft was commanded to descend to by an autopilot.

19. The processor-readable medium of claim 18, wherein preparing the CPDLC message further comprises inserting text that indicates a new heading that the aircraft was commanded to follow by the autopilot.