Device for displaying critical and non-critical information, and aircraft including such a device

• US 8,694,179 B2
• Filed: 11/25/2010
• Issued: 04/08/2014
• Est. Priority Date: 12/01/2009
• Status: Active Grant

• Current Assignee: Safran Electronics & Defense
• Original Assignee: Sagem Defense Securite (Safran SA)
• Inventors: Guillot, Franois, Coppee, Pascal, Vandenbaviere, Yann, Pierson, Jerme
• Primary Examiner(s): Black, Thomas
• Assistant Examiner(s): PAYNE, ROBERT T
• Application Number:
  US13/513,496
• Publication Number:
  US 20120245759A1
• Time in Patent Office: 1,230 Days
• Field of Search: 701/1, 701/120, 701/301, 701/521, 701/28, 701/532, 701/16, 701/540, 701/52, 701/17, 345/502, 345/522, 345/545
• US Class Current: 701/2
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G06F 3/147 using display panels
• CPC Class Codes: G09G 2340/125 wherein one of the images is motion video
• CPC Class Codes: G09G 2360/06 Use of more than one graphics processor to process data before displaying to one or more screens
• CPC Class Codes: G09G 2380/12 Avionics applications

Abstract

An information display device has a first processor unit and a second processor unit that are connected to at least one information source. The first processor unit is also connected to a display and to the second processor unit. The first processor unit and the second processor unit each include a computer and a memory. The computer of the second unit is arranged to construct an image for displaying on the display and to transmit it to the computer of the first processor unit, which is arranged to modify the image by incorporating therein information from the information source, and to transmit the modified image to the display. An aircraft fitted with such a device is also provided.

Claims

1. An information display device arranged to display information in an aircraft cockpit, the device comprising a first processor unit arranged to be connected to a unit supplying flight data such as the speed and the altitude of the aircraft, and a second processor unit arranged to be connected to an altitude database containing the coordinates of a mesh of a territory together with the associated altitudes, and to a photographic database containing the coordinates of the same mesh of the same territory together with associated photographs, the first processor unit also being connected to a display and to the second processor unit, the first processor unit and the second processor unit each comprising a computer and a memory, the computer of the second unit being arranged to construct a terrain rendering image on the basis of information from the altitude database and from the photographic database, and to transmit the image to the computer of the first processor unit, which is arranged to modify the image by incorporating therein information from the information source and to transmit the modified image to the display.

2. The device according to claim 1, wherein the memory of the first unit is organized to store an image for modification, an image being modified, and a modified image being displayed.

3. The device according to claim 1, wherein the computer of the first unit is synchronized with the computer of the second unit to modify the images while they are being transmitted from the computer of the second processor unit to the computer of the first processor unit.

4. The device according to claim 1, wherein the computer of the first processor unit is arranged to verify consistency between the image transmitted by the second processor unit and information from the information source.

5. The device according to claim 1, wherein the first processor unit is also connected to the altitude database to verify consistency between the image supplied by the second processor unit and the information from the altitude database.

6. The device according to claim 5, wherein the computer of the first processor unit is arranged to create a simplified image of the relief on the basis of information from the altitude database and to compare the simplified image with the image transmitted by the second processor unit in order to verify consistency between the two images.

7. The device according to claim 6, wherein the computer of the first processor unit is arranged, in the event of inconsistency, to cause the flight data to be displayed on its own, or else to display the flight data incorporated in the simplified image.

8. The device according to claim 1, wherein the computer of the first processor unit is arranged to write the information as an overlay on the image and/or to create an information display window in the image.

9. An aircraft fitted with a device according to claim 1.