Display systems and methods for aircraft

Patent metadata

Field	Value
Publication number	US-12422279-B2
Application number	US-202318371842-A
Country	US
Kind code	B2
Filing date	Sep 22, 2023
Priority date	Oct 28, 2019
Publication date	Sep 23, 2025
Grant date	Sep 23, 2025

Abstract

A display system of an aircraft includes a display device defining a display area, a vision system for generating an image of an operating environment of the aircraft on the display area, data processors operatively coupled to the display device and the vision system, and non-transitory machine-readable memory operatively coupled to the one or more data processors and storing instructions executable by the one or more processors and configured to cause the one or more processors to, when a condition of the aircraft is met, cause an alteration of a display of flight information on the display area to declutter a cutout region in the image generated by the vision system, the cutout region devoid of imaging generated by the vision system and displaying an Approach Lighting System (ALS) of a runway of intended landing for the aircraft.

First claim

What is claimed is:

1. A method for altering a display on a display area of an aircraft, the method comprising:
determining whether a condition of the aircraft is met; and
when the condition is met, causing an alteration of a display of flight information on the display area to declutter a cutout region in an image generated by a vision system, the cutout region devoid of imaging generated by the vision system and displaying an Approach Lighting System (ALS) of a runway of intended landing for the aircraft, wherein the alteration of the display of flight information on the display area comprises moving the flight information from a first location overlapping the cutout region on the display area to a second location on the display area to reduce an overlap of the flight information with the cutout region and unobstruct the cutout region.

2. The method of claim 1 , further comprising, when the condition of the aircraft is met, causing an alteration of a display of flight information on the display area to declutter an area of the display area that is proximate the cutout region.

3. The method of claim 1 , wherein the cutout region is devoid of synthetic vision imaging generated by the vision system.

4. The method of claim 1 , wherein the cutout region is devoid of enhanced vision imaging generated by the vision system.

5. The method of claim 1 , wherein the condition comprises a flight phase.

6. The method of claim 1 , wherein the condition comprises an altitude of the aircraft.

7. The method of claim 1 , further comprising displaying enhanced vision in the cutout region of the display area.

8. The method of claim 1 , wherein the alteration of the display of flight information on the display area comprises replacing the flight information.

9. The method of claim 1 , wherein the alteration of the display of flight information on the display area comprises resizing the flight information.

10. The method of claim 1 , wherein the alteration of the display of flight information on the display area comprises increasing transparency of the flight information.

11. The method of claim 1 , wherein the flight information comprises angle of attack information.

12. The method of claim 1 , wherein the flight information comprises attitude information.

13. The method of claim 1 , wherein the flight information comprises lateral deviation information.

14. The method of claim 1 , wherein the flight information comprises at least one of compass rose information, navigation information, course information, range information, altitude information, wind vector information, and information when selected minimums are reached.

15. The method of claim 1 , wherein the display area is defined on a heads up display (HUD) device.

16. The method of claim 1 , wherein the display area is defined on a heads down display (HDD) device.

17. The method of claim 1 , wherein the display area is defined on a primary flight display.

18. The method of claim 1 , wherein the display area includes a display area defined on a heads up display (HUD) device and a display area defined on a heads down display (HDD) device, and the alteration of the display of flight information on the display area includes an alteration of a display of flight information on the display area defined on the HUD device synchronized with an alteration of a display of flight information on the display area defined on the HDD device.

19. The method of claim 1 , further comprising, when a reversion condition is met, reverting the display of the display area to the display of flight information prior to the alteration.

20. The method of claim 19 , wherein the reversion condition comprises actuation of a take-off go-around (TOGA) switch.

21. The method of claim 19 , wherein the reversion condition comprises a partial thrust go-around performed by increasing a throttle level angle by twenty-five degrees.

22. The method of claim 19 , wherein the reversion condition comprises landing of the aircraft.

23. A computer program product for a method for altering a display on a display area of an aircraft, the computer program product comprising a non-transitory computer readable storage medium containing program code, the program code being executable by a computer, processor or logic circuit to perform the method defined in claim 1 .

Assignees

• Bombardier Inc

Inventors

• Martin Christian
• Martin Christopher
• Naipaul Jason
• Bae Nami
• Schlegel Mark
• Colquhoun William Murray
• Barber Anthony J
• Wong Natalie

Classifications

• G08G5/55

  for a single aircraft · CPC title

• G08G5/50

  Navigation or guidance aids · CPC title

• G02B2027/0181

  Adaptation to the pilot/driver · CPC title

• G02B2027/0165

  associated with a head-down display · CPC title

• G02B2027/0141

  characterised by the informative content of the display · CPC title