AIRCRAFT VIEWING SYSTEM

• US 20100289671A1
• Filed: 11/15/2007
• Published: 11/18/2010
• Est. Priority Date: 11/24/2006
• Status: Abandoned Application

• Current Assignee: Airbus Operations SAS (Airbus SE)
• Original Assignee: Airbus France
• Inventors: HAUTY, Pierre, VIALATTE, Jean-Luc, TRIBUT, Helene, BIGOT, Jean-Louis
• Application Number:
  US11/940,675
• Publication Number:
  US 20100289671A1
• Time in Patent Office: Days
• US Class Current: 340/945
• CPC Class Codes: G01D 7/00 Indicating measured values

Abstract

This invention relates to an aircraft viewing system comprising:

• • a plurality of generation devices (330₁, . . . , 330_k; 730₁, . . . , 730_k; 830₁, . . . , 830_k) adapted to generate video flows from aircraft data;
  • a plurality of display units (310₁, . . . , 310_n; 710₁, . . . , 710_n; 810₁, . . . , 810_n), wherein each display unit is adapted to display an intrinsic display function as well as a video image representing at least one video input;
  • at least one video distribution unit (320₁, . . . , 320_p; 720₁, . . . , 720_p; 820₁, . . . , 820_p) adapted to switch the video flows generated by said generation devices to the video inputs of said display units.

Claims

1. Aircraft viewing system, characterised in that it comprises:

a plurality of generation devices (330₁, . . . , 330_k;

730₁, . . . , 730_k;

830₁, . . . , 830_k) adapted to generate video flows from aircraft data;

a plurality of display units (310₁, . . . , 310_n;

710₁, . . . , 710_n;

810₁, . . . , 810_n), wherein each display unit is adapted to display an intrinsic display function as well as a video image representing at least one video input;

at least one video distribution unit (320₁, . . . , 320_p;

720₁, . . . , 720_p;

820₁, . . . , 820_p) adapted to switch the video flows generated by said generation devices to the video inputs of said display units.

2. Aircraft viewing system according to claim 1, characterised in that at least one generation device (400) comprises an input/output interface (410), a computing module (420) adapted to supply graphic information to a video signal generation module (440) from aircraft data received on the input/output interface, and a video interface (450) adapted to transform said video signal into at least one video flow in a pre-determined format.

3. Aircraft viewing system according to claim 2, characterised in that the input/output interface complies with the ARINC 429 or ARINC 664 standard.

4. Aircraft viewing system according to claim 2 or 3, characterised in that said format complies with the ARINC 818 standard.

5. Aircraft viewing system according to any of claims 2 to 4, characterised in that said generation device (400) further comprises a database (430), wherein the computing module generates said graphic information from said aircraft data and data stored in said database.

6. Aircraft viewing system according to claim 1, characterised in that said video distribution unit (500) comprises a first video interface (510) adapted to receive a plurality of video flows, a synchronisation module (525) adapted to synchronise the flows in a same temporal base downstream or upstream of a processing module (530) of said flows, and a switching module adapted to switch the flows thus processed and synchronised to a plurality of video outputs.

7. Aircraft viewing system according to claim 6, characterised in that said processing module (530) is adapted to merge video flows and/or a composition of images by windowing, wherein each window corresponds to a flow or several merged flows.

8. Aircraft viewing system according to claim 6 or 7, characterised in that the processing module (530) is adapted to rotate and/or resize images.

9. Aircraft viewing system according to claim 6, characterised in that it comprises an auxiliary data management unit (540) adapted to extract and/or insert auxiliary data from or into a video signal, wherein said auxiliary data is transported during the line return and/or frame return of said signal, and a control unit (520) adapted to check the integrity of the video flows from the data extracted by said management unit (540).

10. Aircraft viewing system according to claim 9, characterised in that said control unit (520) is adapted to detect erroneous frames in the video flows, to eliminate and/or replace them on the fly by pre-determined or interpolated frames.

11. Aircraft viewing system according to claim 6, characterised in that the switching module (560) is adapted to duplicate at least one of said processed and synchronised flows to transmit it to at least two of said video outputs.

12. Aircraft viewing system according to claim 1, characterised in that at least one display unit comprises a video display plane to display the video signal and at least one second display plane (P₁), wherein said display unit is adapted to display in a first screen zone (Z₁) said intrinsic display function (F_old) and in the remaining part of the screen said video image (F_new), wherein the video display plane is masked in said first zone by the second display plane.

13. Aircraft viewing system according to any of the previous claims, characterised in that it comprises at least one display computer (715₁, . . . , 715_q) distinct from the display units, wherein said computer is adapted to generate an image representing said intrinsic display function for at least one said display units.

14. Aircraft viewing system according to any of claims 1 to 12, characterised in that it comprises at least one display computer (815₁, . . . , 815_q) distinct from the display units, wherein said computer is adapted to receive at least one first video flow from said video distribution unit, to generate an image representing said intrinsic display function for at least one given display unit, to generate an image representing said intrinsic display function and said first video flow, wherein said image is transmitted in the form of a second video flow to said given display unit.

15. Aircraft characterised in that it comprises an aircraft viewing system according to any of the previous claims.