Pressure bulkhead and method for subdivision of an aircraft...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/10 (2006.01)

Patent

CA 2698422

The present invention provides a pressure bulkhead for subdivision of an aircraft or spacecraft into an internal and an external pressure region. The pressure bulkhead comprises a pressure plate having an edge shaped so as to correspond to an inner contour of the aircraft or spacecraft, a supporting means which tiltably supports the edge on the inner contour, and a seal which seals the edge with the inner contour. A further aspect of the invention provides a method for subdivision of an aircraft or spacecraft into an internal and an external pressure region. Firstly, a pressure plate is provided that has an edge shaped so as to correspond to an inner contour of the aircraft or spacecraft. In further steps, the edge is tiltably supported on the inner contour and sealed with the inner contour.

L'invention concerne une cloison de pressurisation (100) pour diviser un aéronef ou un véhicule spatial en une zone à pression intérieure (102) et une zone à pression extérieure (104). La cloison de pressurisation comprend : un panneau de pressurisation (106) qui présente un bord façonné conformément à un contour intérieur (108) de l'aéronef ou du véhicule spatial ; un dispositif de soutien (112) qui soutient le bord à pivotement contre le contour intérieur ; et un joint d'étanchéité (114) qui réalise l'étanchéité entre le bord et le contour intérieur. Selon un autre point de vue, l'invention concerne un procédé pour diviser un aéronef ou un véhicule spatial en une zone à pression intérieure et une zone à pression extérieure. On fournit d'abord un panneau de pressurisation qui présente un bord façonné conformément à un contour intérieur de l'aéronef ou du véhicule spatial. Au cours d'étapes suivantes, on soutient le bord à pivotement contre le contour intérieur, et on réalise l'étanchéité entre le bord et le contour intérieur.

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