Skin of an airplane door

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/14 (2006.01)

Patent

CA 2353288

The invention relates to a skin of an airplane door, which conforms to the surrounding surface contour of the fuselage, and which during the flight is exposed to a pressure load direction. It is an object of the invention to provide the skin of an airplane door with a clearly smaller dimension for the purpose of a light construction, thus permitting a weight reduction of the door. The object is achieved in that the skin is performed against the pressure load direction and connected with supports of a door frame. During flight at cruising altitude, the internal fuselage pressures deform the skin away from a predetermined shape so as to conform the exterior of the skin with adjacent exterior surfaces of the fuselage, thereby minimizing flow resistance.

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