STANDBY FLIGHT DISPLAY SYSTEM

• US 20150015422A1
• Filed: 07/12/2013
• Published: 01/15/2015
• Est. Priority Date: 07/12/2013
• Status: Abandoned Application

• Current Assignee: Gulfstream Aerospace Corporation (General Dynamics Corporation)
• Original Assignee: Gulfstream Aerospace Corporation (General Dynamics Corporation)
• Inventors: Michaels, Charles
• Application Number:
  US13/941,055
• Publication Number:
  US 20150015422A1
• Time in Patent Office: Days
• US Class Current: 340/973
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C

Abstract

A standby flight display system for use on an aircraft is disclosed herein. The aircraft has a primary flight display system that is configured to display a first image on a primary flight display screen. The standby flight display system includes a subsystem configured to determine a dynamic state of the aircraft. The standby flight display system further includes an image generator. The standby flight display system still further includes a processing unit. The subsystem, the image generator, and the processing unit are each independent of the primary flight display system. The processing unit is communicatively coupled with the subsystem and with the image generator and is configured to receive information from the subsystem relating to the dynamic state of the aircraft and to control the image generator to generate a second image overlaying the first image on the primary flight display screen.

Claims

1. A standby flight display system for use on an aircraft, the aircraft having a primary flight display system configured to display a first image on a primary flight display screen, the standby flight display system comprising:

a subsystem configured to determine a dynamic state of the aircraft, the subsystem being independent of the primary flight display system;

an image generator independent of the primary flight display system; and

a processing unit independent of the primary flight display system, the processing unit communicatively coupled with the subsystem and with the image generator, the processing unit configured to receive information from the subsystem relating to the dynamic state of the aircraft and to control the image generator to generate a second image on the primary flight display screen relating to the dynamic state of the aircraft, the second image overlaying the first image.

2. The standby flight display system of claim 1, wherein the second image is substantially identical to the first image.

3. The standby flight display system of claim 2, wherein the second image is substantially aligned with the first image.

4. The standby flight display system of claim 3, wherein the processing unit is configured to substantially align the second image with the first image.

5. The standby flight display system of claim 3, wherein the image generator is configured for adjustment to permit alignment of the second image with the first image.

6. The standby flight display system of claim 1, wherein the image generator comprises a projector.

7. The standby flight display system of claim 6, wherein the projector comprises a digital light projector.

8. The standby flight display system of claim 6, wherein the projector is arranged to project the second image on a rear portion of the primary flight display screen.

9. The standby flight display system of claim 1, further comprising a plurality of the subsystems.

10. The standby flight display system of claim 1, wherein the subsystem comprises one of an air data system, an altitude heading reference system, and a navigation radio system.

11. A standby flight display system for use on an aircraft, the aircraft having a primary flight display system configured to display a first image on a primary flight display screen, the standby flight display system comprising:

a subsystem configured to determine a dynamic state of the aircraft, the subsystem being independent of the primary flight display system;

an image generator independent of the primary flight display system; and

a processing unit independent of the primary flight display system, the processing unit including a data processor and a graphics processor, the data processor and the graphics processor communicatively coupled with one another, the data processor further communicatively coupled with the subsystem and configured to receive information from the subsystem relating to the dynamic state of the aircraft, to generate a signal based on the information received from the subsystem, and to provide the signal to the graphics processor, the graphics processor configured to utilize the signal to control the image generator to generate a second image on the primary flight display screen relating to the dynamic state of the aircraft, the second image overlaying the first image.

12. The standby flight display system of claim 11, wherein the second image is substantially identical to the first image.

13. The standby flight display system of claim 12, wherein the second image is substantially aligned with the first image.

14. The standby flight display system of claim 13, wherein the processing unit is configured to substantially align the second image with the first image.

15. The standby flight display system of claim 13, wherein the image generator is configured for adjustment to permit alignment of the second image with the first image.

16. The standby flight display system of claim 11, wherein the image generator comprises a projector.

17. The standby flight display system of claim 16, wherein the projector comprises a digital light projector.

18. The standby flight display system of claim 16, wherein the projector is arranged to project the second image on a rear portion of the primary flight display screen.

19. A standby flight display system for use on an aircraft, the aircraft having a primary flight display system configured to display a first image on a primary flight display screen, the standby flight display system comprising:

a subsystem configured to determine a dynamic state of the aircraft, the subsystem being independent of the primary flight display system;

an image generator independent of the primary flight display system; and

a processing unit communicatively coupled with the subsystem, with the image generator, and with the primary flight display system, the processing unit configured to receive information from the subsystem relating to the dynamic state of the aircraft and to control the image generator to generate a second image on the primary flight display screen relating to the dynamic state of the aircraft, the second image overlaying the first image, and the processing unit further configured to receive information from the primary flight display system relating to the first image and to utilize the information to align the second image with the first image.

20. The standby flight display system of claim 19, wherein the processing unit is configured to substantially align the second image with the first image by aligning a plurality of pixels of the second image with a corresponding plurality of pixels of the first image.