IP Library Granted Patent US 7,545,288
Granted Patent B2
US 7,545,288 · App. 10/585,003 · Granted Jun 9, 2009

Support system for the monitoring of an air outlet valve in an aircraft

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Quick Facts
Patent No.
US 7,545,288
App. No.
10/585,003
Granted
Jun 9, 2009
Kind
B2
Abstract

The invention proposes that a camera ( 18 ) takes a technical picture of an air outlet valve ( 10 ) of an aircraft, and the picture taken of the outlet valve ( 10 ) is displayed on a picture display unit ( 20 ), for example in the cockpit of the aircraft. By shining light onto the outlet valve from a light source ( 22 ), a clear picture with a high level of contrast is produced. The valve setting of the outlet valve ( 10 ) can thus be monitored visually, in a reliable manner, by the pilot.

Claims (17)

1. A support system for monitoring an air outlet valve in an aircraft, the system comprising:

an air outlet valve disposed between an aircraft cabin and the outside atmosphere, wherein the air outlet valve can be fully opened to equalize the air pressure within the aircraft cabin with the outside atmosphere before aircraft cabin doors are opened;

a camera arranged to capture an image viewed through the air outlet valve; and

a display unit in operable communication with the camera and adapted to display the image taken by the camera;

wherein an observer of the display unit can visually determine whether the air outlet valve is fully opened, partially opened, fully closed, or otherwise obstructed before aircraft cabin doors are opened.

2. The support system of claim 1 , wherein the display unit is positioned within a cockpit of the aircraft.

3. The support system of claim 1 , further comprising:

a valve lighting system designed to direct light onto the air outlet valve.

4. The support system of claim 3 , wherein the camera is disposed on a first side of the air outlet valve and the valve lighting system is disposed on a second side of the air outlet valve.

5. The support system of claim 3 , wherein the valve lighting system directs infrared light onto the air outlet valve.

6. The support system of claim 3 , wherein the valve lighting system directs black light onto the air outlet valve.

7. The support system of claim 3 , wherein the air outlet valve further comprises a coating which reflects at least part of the light from the valve lighting system.

8. The support system of claim 3 , wherein the air outlet valve further comprises a coating which absorbs at least part of the light from the valve lighting system.

9. The support system of claim 1 , wherein the camera further comprises a monochrome camera.

10. The support system of claim 1 , wherein the support system is adapted to allow continuous monitoring of the air outlet valve during operation of the air outlet valve.

11. The support system of claim 1 , wherein the air outlet valve further comprises a valve channel and a butterfly valve flap disposed within the valve channel, the butterfly valve flap configured to rotate between fully closed and fully opened positions.

12. The support system of claim 11 , wherein the camera is positioned along a longitudinal axis of the valve channel so that the position of the butterfly valve flap can be directly observed.

Assignments (2)
CHANGE OF NAME Recorded May 31, 2011
From: AIRBUS DEUTSCHLAND GMBH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 026360/0849 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 27, 2007
From: SCHIEK, THORSTEN; HEUER, THOMAS; CHEN, LEILEI
To: AIRBUS DEUTSCHLAND GMBH
Reel/Frame 019222/0772 →