Automatic Emergency Reporting

• US 20110125348A1
• Filed: 11/23/2009
• Published: 05/26/2011
• Est. Priority Date: 11/23/2009
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Cornell, Bradley David, Sandell, Gordon Robert Andrew, Lee, Stephen Y.
• Application Number:
  US12/623,909
• Publication Number:
  US 20110125348A1
• Time in Patent Office: Days
• US Class Current: 701/14
• CPC Class Codes: G07C 5/006 Indicating maintenance
• CPC Class Codes: G07C 5/008 communicating information to a remotely located station transmission systems for measured values G08C
• CPC Class Codes: G07C 5/0841 Registering performance data recording measured values G01D; information storage G11B

Abstract

Technologies are described herein for providing automatic emergency reporting. The technologies are adapted to receive values of aircraft state parameters collected from one or more sensors arranged within an aircraft. The technologies then determine whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft. Responsive to the determination of whether the aircraft state parameters indicate normal or anomalous operation of the aircraft, the technologies initiate an emergency reporting function. The emergency reporting function may transmit a report containing the collected values of the aircraft state parameters to a ground system via a data-link.

Claims

1. A computer-implemented method for providing automatic emergency reporting, the method comprising computer-implemented operations for:

receiving values of aircraft state parameters collected from one or more sensors arranged within an aircraft;

determining whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft; and

responsive to the determination of whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft, initiating an emergency reporting function, the emergency reporting function transmitting a report containing the collected values of the aircraft state parameters to a ground system via a data-link.

2. The computer-implemented method of claim 1, wherein determining whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft comprises comparing the collected values of the aircraft state parameters to normal values of the aircraft state parameters;

and wherein the normal values of the aircraft state parameters comprise numeric values or parameter statuses of one or more parameters.

3. The computer-implemented method of claim 1, the method comprising further computer-implemented operations for:

upon initiating the emergency reporting function, causing instrumentation on the aircraft to display an indication that the emergency reporting function has been initiated.

4. The computer-implemented method of claim 1, the method comprising further computer-implemented operations for:

receiving an instruction through instrumentation on the aircraft to initiate the emergency reporting function;

in response to receiving the instruction through the instrumentation to initiate the emergency reporting function, initiating the emergency reporting function; and

upon initiating the emergency reporting function, causing the instrumentation on the aircraft to display an indication that the emergency reporting function has been manually initiated.

5. The computer-implemented method of claim 1, the method comprising further computer-implemented operations for:

receiving an instruction through instrumentation on the aircraft to terminate the emergency reporting function;

in response to receiving the instruction through the instrumentation to terminate the emergency reporting function, terminating the emergency reporting function; and

upon terminating the emergency reporting function, causing the instrumentation on the aircraft to display an indication that the emergency reporting function has been manually terminated.

6. The computer-implemented method of claim 1, the method comprising further computer-implemented operations for:

receiving an instruction from the ground system to terminate the emergency reporting function;

in response to receiving the instruction from the ground system to terminate the emergency reporting function, terminating the emergency reporting function; and

upon terminating the emergency reporting function, causing instrumentation on the aircraft to display an indication that the emergency reporting function has been terminated by the ground system.

7. The computer-implemented method of claim 1, wherein the report embodiments the collected values of the aircraft state parameters in a single Aircraft Communications Addressing and Reporting System (“

ACARS”

) block transmitted via the data-link.

8. The computer-implemented method of claim 1, the method comprising further computer-implemented operations for:

upon initiating an emergency reporting function, initiating additional communications to the ground system through at least one of Automatic Dependent Surveillance-Contract (“

ADS-C”

) and Controller Pilot Data Link Communications (“

CPDLC”

).

9. A system for providing automatic emergency reporting, the system comprising:

a processor;

a memory coupled to the processor; and

a program module (i) which executes in the processor from the memory and (ii) which, when executed by the processor, causes the system to provide automatic emergency reporting by

receiving values of aircraft state parameters collected from one or more sensors arranged within an aircraft, the sensors collecting data regarding condition or operation of the aircraft,

determining whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft by comparing the collected values of the aircraft state parameters to normal values of the aircraft state parameters, the normal values of the aircraft state parameters comprising numeric values and/or statuses of one or more parameters, and

responsive to the determination of whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft, initiating an emergency reporting function, the emergency reporting function transmitting a report containing the collected values of the aircraft state parameters to a ground system via a data-link.

10. The system of claim 9, wherein aircraft comprises instrumentation, the instrumentation comprising a visual display and a response mechanism.

11. The system of claim 10, wherein the instrumentation comprises at least one of a dedicated data link display and an Engine Indicating and Crew Alerting System (“

EICAS”

) display.

12. The system of claim 10, wherein the program module, when executed by the processor, further causes the system to provide automatic emergency reporting by

upon initiating the emergency reporting function, causing the visual display to display an indication that the emergency reporting function has been initiated.

13. The system of claim 10, wherein the program module, when executed by the processor, further causes the system to provide automatic emergency reporting by

receiving an instruction through the response mechanism to initiate the emergency reporting function,

in response to receiving the instruction through the response mechanism to initiate the emergency reporting function, initiating the emergency reporting function, and

upon initiating the emergency reporting function, causing the visual display to display an indication that the emergency reporting function has been manually initiated.

14. The system of claim 10, wherein the program module, when executed by the processor, further causes the system to provide automatic emergency reporting by

receiving an instruction through the response mechanism to terminate the emergency reporting function;

in response to receiving the instruction through the response mechanism to terminate the emergency reporting function, terminating the emergency reporting function; and

upon terminating the emergency reporting function, causing the visual display to display an indication that the emergency reporting function has been manually terminated.

15. The system of claim 10, wherein the program module, when executed by the processor, further causes the system to provide automatic emergency reporting by

receiving an instruction from the ground system to terminate the emergency reporting function;

in response to receiving the instruction from the ground system to terminate the emergency reporting function, terminating the emergency reporting function; and

upon terminating the emergency reporting function, causing the visual display to display an indication that the emergency reporting function has been terminated by the ground system.

16. The system of claim 10, wherein the program module, when executed by the processor, further causes the system to provide automatic emergency reporting by

upon initiating the emergency reporting function, causing the visual display to display which of the aircraft state parameters indicate anomalous operation of the aircraft.

17. The system of claim 9, wherein the report embodiments the collected values of the aircraft state parameters in a single ACARS block transmitted via the data-link.

18. The system of claim 9, wherein the program module, when executed by the processor, further causes the system to provide automatic emergency reporting by

upon initiating an emergency reporting function, initiating additional communications to the ground system through at least one of ADS-C and CPDLC.

19. A computer-readable storage medium having computer-executable instructions stored thereon which, when executed by a computer, cause the computer to:

receive values of aircraft state parameters collected from one or more sensors arranged within an aircraft, the sensors collecting data regarding condition or operation of the aircraft;

determine whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft by comparing the collected values of the aircraft state parameters to normal values of the aircraft state parameters, the normal values the aircraft state parameters comprising numeric values and/or statuses of one or more parameters;

responsive to the determination of whether the collected values of the aircraft state parameters indicate normal or anomalous operation of the aircraft, initiate an emergency reporting function, the emergency reporting function transmitting a report containing the collected values of the aircraft state parameters to a ground system via a data-link; and

upon initiating the emergency reporting function, cause a visual display in instrumentation on the aircraft to display an indication that the emergency reporting function has been initiated.

20. The computer-readable storage medium of claim 19, wherein the emergency reporting function terminates after a given period of time.