METHODS AND SYSTEMS FOR DISPLAYING AIRCRAFT INFORMATION

• US 20150120090A1
• Filed: 10/31/2013
• Published: 04/30/2015
• Est. Priority Date: 10/31/2013
• Status: Active Grant

• Current Assignee: Gulfstream Aerospace Corporation (General Dynamics Corporation)
• Original Assignee: Gulfstream Aerospace Corporation (General Dynamics Corporation)
• Inventors: Wischmeyer, Carl Edward
• Granted Patent: US 9,114,887 B2
• Time in Patent Office: Days
• US Class Current: 701/3
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G01C 1/00 Measuring angles
• CPC Class Codes: G09B 19/165 Control of aircraft
• CPC Class Codes: G09B 5/02 with visual presentation of the material to be studied, e.g. using film strip

Abstract

A method and an instrumentation system for an aircraft are provided. The method of presenting aircraft information includes activating a master indicator in response to a trigger event associated with operation of the aircraft, receiving a user input associated with the master indicator, and displaying information associated with the trigger event in response to receiving the user input associated with the master indicator. The instrumentation system performs the operations of the method.

Claims

1. A method of presenting aircraft information, the method comprising:

activating, with a controller, a master indicator in response to a trigger event associated with operation of the aircraft;

receiving, at the controller, a user input associated with the master indicator; and

displaying, on a display, information associated with the trigger event in response to receiving the user input associated with the master indicator.

2. The method of claim 1, wherein displaying information associated with the trigger event includes displaying a checklist associated with the trigger event in a dedicated area of the display.

3. The method of claim 1, wherein displaying information associated with the trigger event includes displaying synoptics or graphics associated with the trigger event.

4. The method of claim 1, wherein activating a master indicator includes activating an aural alarm, and wherein the method further includes de-activating the aural alarm in response to the user input.

5. The method of claim 4, wherein the user input associated with the master indicator includes a first user input and a second user input, and wherein de-activating the aural alarm is in response to receiving the first user input, and wherein displaying the information associated with the trigger event is in response to receiving the second user input.

6. The method of claim 5, wherein the first user input is a single actuation of the master indicator.

7. The method of claim 5, wherein the second user input is a double actuation or a prolonged actuation of the master indicator.

8. The method of claim 5, wherein the second user input is an actuation of a pending checklist icon displayed in a dedicated portion of a display.

9. The method of claim 5, wherein the second user input is a unique gesture on a touchscreen.

10. The method of claim 1, wherein displaying the information includes displaying a checklist and a synoptic or graphic simultaneously.

11. The method of claim 1, further comprising displaying a pending checklist icon in a dedicated area of a display when a checklist associated with the trigger event has not been completed.

12. The method of claim 11, further comprising displaying a no pending checklist icon in the dedicated area of the display when the checklist associated with the trigger event has been completed.

13. The method of claim 1, wherein activating the master indicator includes illuminating an icon of a master warning indicator or a master caution indicator on an electronic display of the aircraft.

14. An instrumentation system for an aircraft, the instrumentation system comprising:

a plurality of aircraft components that are associated with operating the aircraft;

a master indicator for indicating the status of any aircraft component of the plurality of aircraft components;

a controller electronically coupled with the plurality of aircraft components and the master indicator, the controller configured for;

activating the master indicator in response to a trigger event associated with any aircraft component of the plurality of aircraft components;

receiving a user input associated with the master indicator; and

displaying information associated with the trigger event in response to receiving the user input associated with the master indicator.

15. The instrumentation system of claim 14, wherein the controller is further configured for displaying a checklist and synoptics associated with the trigger event.

16. The instrumentation system of claim 14, wherein the user input associated with the master indicator includes a first user input and a second user input, and wherein the controller is configured for de-activating the aural alarm in response to receiving the first user input, and wherein the controller is configured for displaying the checklist based on the trigger event in response to receiving the second user input.

17. The instrumentation system of claim 16, wherein the first user input is a single actuation of the master indicator.

18. The instrumentation system of claim 16, wherein the second user input is a double actuation or a prolonged actuation of the master indicator.

19. The instrumentation system of claim 15, further comprising an electronic display, and wherein the second user input is an actuation of a pending checklist icon on the electronic display.

20. The instrumentation system of claim 14, wherein the master indicator is one of a master warning indicator and a master caution indicator displayed in a dedicated location on an electronic display of an aircraft.