AIRCRAFT COCKPIT VISOR DISPLAY

• US 20120140125A1
• Filed: 12/03/2010
• Published: 06/07/2012
• Est. Priority Date: 12/03/2010
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Pepitone, Dave, Sarma, Kalluri R., Wyatt, Sandy
• Application Number:
  US12/959,503
• Publication Number:
  US 20120140125A1
• Time in Patent Office: Days
• US Class Current: 348/794
• CPC Class Codes: G02B 2027/0118 comprising devices for improving the contrast of the display / brillance control visibility
• CPC Class Codes: G02B 2027/0138 comprising image capture systems, e.g. camera
• CPC Class Codes: G02B 2027/0156 with optionally usable elements
• CPC Class Codes: G02B 27/0149 characterised by mechanical features G02B27/0176 takes precedence

Abstract

An overhead visor display system for an aircraft cockpit includes one or more transparent OLED visors. The visor may display text and images, such as aircraft flight or system data, navigational data, conformal images of actual views outside the aircraft, or may function as a sun shade. The visor may be rotated up towards the ceiling of the cockpit out of view. Optionally, the visors may be moved by a pilot on a rail from one side window to the front windscreen, and to the other side window.

Claims

1. A display system contained in an interior of a structure having a first window, the display system comprising:

a rail positioned above the first window;

a first visor display rotatably mounted on the rail so as to be positioned above or in the field of view of the first window; and

a processor configured to provide at least one of text or images to the first visor display.

2. The display system of claim 1 wherein the structure has a second window, the display system further comprising:

the rail being position above the second window; and

the first visor display being slideably mounted on the rail so as to be positioned above or in the field of view of the second window.

3. The display system of claim 2 further comprising:

a second visor display rotatably and slideably attached to the rail so as to be positioned above or in the field of view of the first and second windows.

4. The display system of claim 1 further comprising:

a cable configured to provide power and data to the first visor display, the cable being positioned within an opening defined by the rail.

5. The display system of claim 1 wherein the first visor display comprises:

a transparent active matrix liquid crystal display.

6. The display system of claim 1 further comprising:

an arm coupled between the first visor display and the rail, the arm configured to place the visor display in a first position adjacent the rail, and a second position extended from the rail.

7. The display system of claim 1 further comprising:

a tensioning reel capturing the cable and configured to provide an extended portion of the cable to reach the first visor display.

8. A display system for an aircraft having a first front windscreen and a first side window, the display system comprising:

a rail positioned above the first windscreen;

a visor display rotatably mounted to the rail so as to be positioned in one of above or in the field of view of the first front windscreen; and

a processor configured to provide at least one of text and images to the visor display.

9. The display system of claim 8 wherein the aircraft has a first side window, the rail being positioned above the first side window and the visor display being slideably mounted to the rail so as to be positioned in one of above or in the field of view of the first front windscreen.

10. The display system of claim 8 wherein the aircraft has a second front windscreen, a first side window, and a second side window, the rail being positioned above the second front windscreen, the first side window, and the second side window, and the visor display being slideably mounted to the rail so as to be positioned in one of above or in the field of view of the second front windscreen, the first side window, and the second side window.

11. The display system of claim 10 further comprising:

a second visor display rotatably and slideably mounted on the rail so as to be in one of above or in the field of view of the first and second front windscreens and the first and second side windows.

12. The display system of claim 8 further comprising:

a cable configured to provide power and data to the first visor display, the cable positioned within an opening defined by the rail.

13. The display system of claim 8 further comprising:

circuitry positioned within the first visor display and configured to receive data.

14. The display system of claim 8 wherein the first visor display comprises:

a transparent organic light emitting diode display.

15. The display system of claim 8 wherein the processor is configured to provide at least one of a menu, data, or a conformal view of the field of view of an exterior of the structure.

16. The display system of claim 8 further comprising:

a sensor configured to determine and provide an output of the environment of the exterior of the structure; and

the processor being configured to convert the output to a conformal view for display on the first visor display.

17. The display system of claim 8 wherein the first visor display is further configured to shade the sun.

18. A method of operating a display system of an aircraft, comprising:

rotating a visor display about a rail positioned above a first front windscreen so as to position the visor display in or above the field of view of the front windscreen; and

displaying at least one of text and images on the visor display.

19. The method of claim 18 further comprising:

sliding the visor display along the rail positioned above a first side window so as to position the visor display in or above the field of view of the first side window.

20. The method of claim 18 further comprising:

sliding the visor display along the rail positioned above a second front windscreen so as to position the visor display in or above the field of view of the second front windscreen.