AIRCRAFT OPERATIONAL ANOMALY DETECTION

• US 20160318622A1
• Filed: 04/18/2016
• Published: 11/03/2016
• Est. Priority Date: 04/29/2015
• Status: Abandoned Application

• Current Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Haukom, Michael James
• Application Number:
  US15/131,223
• Publication Number:
  US 20160318622A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64D 2045/0065 Black boxes, devices automatically broadcasting distress signals
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: B64D 45/0051 by monitoring passengers or crew on aircraft
• CPC Class Codes: B64D 45/0059 by communicating emergency situations to ground control or between crew members
• CPC Class Codes: G07C 5/008 communicating information to a remotely located station transmission systems for measured values G08C
• CPC Class Codes: G07C 5/0808 Diagnosing performance data testing of vehicles G01M17/00; testing of electrical installation on vehicles G01R31/005
• CPC Class Codes: G07C 5/0841 Registering performance data recording measured values G01D; information storage G11B
• CPC Class Codes: G07C 5/085 using electronic data carriers

Abstract

An example method includes receiving, by an aircraft interface device installed on an aircraft, data corresponding to operational characteristics of the aircraft, and determining, by the aircraft interface device, whether the data corresponding to the operational characteristics of the aircraft indicates that an aircraft anomaly condition is present. The method further includes storing, by the aircraft interface device, selected data corresponding to the operational characteristics of the aircraft at a first storage frequency in response to determining that the aircraft anomaly condition is not present, and storing, by the aircraft interface device, the selected data corresponding to the operational characteristics of the aircraft at a second storage frequency that is greater than the first storage frequency in response to determining that the aircraft anomaly condition is present.

Claims

1. A method comprising:

receiving, by an aircraft interface device installed on an aircraft, data corresponding to operational characteristics of the aircraft;

determining, by the aircraft interface device, whether the data corresponding to the operational characteristics of the aircraft indicates that an aircraft anomaly condition is present;

storing, by the aircraft interface device, selected data corresponding to the operational characteristics of the aircraft at a first storage frequency in response to determining that the aircraft anomaly condition is not present; and

storing, by the aircraft interface device, the selected data corresponding to the operational characteristics of the aircraft at a second storage frequency that is greater than the first storage frequency in response to determining that the aircraft anomaly condition is present.

2. The method of claim 1,

wherein the data corresponding to the operational characteristics of the aircraft comprises aircraft flight performance data;

and

wherein determining whether the data corresponding to the operational characteristics of the aircraft indicates that the aircraft anomaly condition is present comprises;

comparing the aircraft flight performance data to expected aircraft flight performance data;

determining that the data corresponding to the operational characteristics of the aircraft indicates that the aircraft anomaly condition is present in response to determining that the aircraft flight performance data exceeds a threshold deviation from the expected aircraft flight performance data; and

determining that the data corresponding to the operational characteristics of the aircraft indicates that the aircraft anomaly condition is not present in response to determining that the aircraft flight performance data does not exceed the threshold deviation from the expected aircraft flight performance data.

3. The method of claim 2,

wherein the aircraft flight performance data comprises aircraft track information indicating a flight direction of the aircraft at a current geographical location of the aircraft;

and

wherein comparing the aircraft flight performance data to the expected aircraft flight performance data comprises comparing the aircraft track information to a route plan of the aircraft indicating an expected flight direction of the aircraft at the current geographical location of the aircraft.

4. The method of claim 2,

wherein the aircraft flight performance data comprises aircraft vertical speed information;

and

wherein comparing the aircraft flight performance data to the expected aircraft flight performance data comprises comparing the aircraft vertical speed information to a threshold vertical speed.

5. The method of claim 4, wherein the threshold vertical speed corresponds to an expected vertical speed of the aircraft corresponding to a flight plan of the aircraft.

6. The method of claim 2,

wherein the aircraft flight performance data comprises aircraft angle of attack information;

and

wherein comparing the aircraft flight performance data to the expected aircraft flight performance data comprises comparing the aircraft angle of attack information to a threshold angle of attack.

7. The method of claim 6, wherein the threshold angle of attack corresponds to a critical angle of attack associated with a stall angle of the aircraft.

8. The method of claim 2,

wherein the aircraft flight performance data comprises aircraft bank angle information;

and

wherein comparing the aircraft flight performance data to the expected aircraft flight performance data comprises comparing the aircraft bank angle information to a threshold bank angle.

9. The method of claim 1,

wherein the data corresponding to the operational characteristics of the aircraft comprises cabin pressurization data that indicates an air pressure within a cabin of the aircraft;

and

wherein determining whether the data corresponding to the operational characteristics of the aircraft indicates that the aircraft anomaly condition is present comprises comparing the air pressure within the cabin of the aircraft to a threshold cabin air pressure.

10. The method of claim 1, wherein storing the selected data corresponding to the operational characteristics of the aircraft comprises storing the selected data corresponding to the operational characteristics of the aircraft at non-volatile computer-readable memory of the aircraft interface device.

11. The method of claim 1, wherein storing the selected data corresponding to the operational characteristics of the aircraft comprises transmitting the selected data corresponding to the operational characteristics of the aircraft to a flight data recorder device that is installed on the aircraft and is configured to store the selected data.

12. The method of claim 1, wherein the selected data corresponding to the operational characteristics of the aircraft comprises location data indicating a current geographical location of the aircraft.

13. The method of claim 1, further comprising:

transmitting, by the aircraft interface device, the selected data corresponding to the operational characteristics of the aircraft to a remote computing device via a communications network.

14. An aircraft interface device configured to be installed on an aircraft, the aircraft interface device comprising:

at least one processor;

a communications unit operatively coupled to the at least one processor and configured to receive data corresponding to operational characteristics of the aircraft; and

computer-readable memory encoded with instructions that, when executed by the at least one processor, cause the aircraft interface device to;

determine whether the data corresponding to the operational characteristics of the aircraft indicates that an aircraft anomaly condition is present;

store selected data corresponding to the operational characteristics of the aircraft at a first storage frequency in response to determining that the aircraft anomaly condition is not present; and

store the selected data corresponding to the operational characteristics of the aircraft at a second storage frequency that is greater than the first storage frequency in response to determining that the aircraft anomaly condition is present.

15. The aircraft interface device of claim 14,

wherein the data corresponding to the operational characteristics of the aircraft comprises aircraft flight performance data;

and

wherein the instructions to determine whether the data corresponding to the operational characteristics of the aircraft indicates that the aircraft anomaly condition is present comprise instructions that, when executed by the at least one processor, cause the aircraft interface device to;

compare the aircraft flight performance data to expected aircraft flight performance data;

determine that the data corresponding to the operational characteristics of the aircraft indicates that the aircraft anomaly condition is present in response to determining that the aircraft flight performance data exceeds a threshold deviation from the expected aircraft flight performance data; and

determine that the data corresponding to the operational characteristics of the aircraft indicates that the aircraft anomaly condition is not present in response to determining that the aircraft flight performance data does not exceed the threshold deviation from the expected aircraft flight performance data.

16. The aircraft interface device of claim 15,

wherein the aircraft flight performance data comprises aircraft track information indicating a flight direction of the aircraft at a current geographical location of the aircraft;

and

wherein the instructions to compare the aircraft flight performance data to the expected aircraft flight performance data comprise instructions that, when executed by the at least one processor, cause the aircraft interface device to compare the aircraft track information to a route plan of the aircraft indicating an expected flight direction of the aircraft at the current geographical location of the aircraft.

17. The aircraft interface device of claim 15,

wherein the aircraft flight performance data comprises aircraft vertical speed information;

and

wherein the instructions to compare the aircraft flight performance data to the expected aircraft flight performance data comprise instructions that, when executed by the at least one processor, cause the aircraft interface device to compare the aircraft vertical speed to a threshold vertical speed.

18. The aircraft interface device of claim 14, wherein the instructions to store the selected data corresponding to the operational characteristics of the aircraft comprise instructions that, when executed by the at least one processor, cause the aircraft interface device to transmit the selected data to a flight data recorder device that is installed on the aircraft and is configured to store the selected data.

19. The aircraft interface device of claim 14, wherein the selected data corresponding to the operational characteristics of the aircraft comprises location data indicating a current geographical location of the aircraft.

20. The aircraft interface device of claim 14,

wherein the communications unit is further configured to transmit data;

and

wherein the computer-readable memory is further encoded with instructions that, when executed by the at least one processor, cause the aircraft interface device to transmit, via the communications unit, the selected data corresponding to the operational characteristics over a communications network.