Cover for an aircraft access opening

Details Cover for an aircraft access opening Cover for an aircraft access opening

B - Operations, Transporting

64

C

B64C 1/14 (2006.01) B64C 3/34 (2006.01)

Patent

CA 2692291

The invention relates to a cover for the access opening in a composite material aircraft structure, characterized in that it comprises the following elements: an outer cover (18) arranged on the outer part of the aircraft skin (28), the carbon fiber layers (14) forming the skin (28) being deformed towards the inner part of the aircraft structure, leaving enough space between the aircraft structure and the outer part of the skin (28) for the seating of the outer cover (18); a composite material plate (15) arranged in the outer part of the skin (28) and surrounding the area for installing the outer cover (18); an inner cover (27) arranged on the inner part of the aircraft skin (28).

L'invention concerne un couvercle pour une ouverture d'accès formée dans une structure d'aéronef en matériau composite. Ce couvercle se caractérise en ce qu'il comprend les éléments suivants : un couvercle externe (18) disposé sur la partie externe du revêtement de l'aéronef (28), les couches de fibres de carbone (14) constituant le revêtement (28) étant déformées en direction de la partie interne de la structure d'aéronef, laissant ainsi suffisamment d'espace entre la structure d'aéronef et la partie externe du revêtement (28) pour le placement du couvercle externe (18) ; une plaque en matériau composite (15) disposée dans la partie externe du revêtement (28) et entourant la zone de montage du couvercle externe (18) ; et un couvercle interne (27) disposé sur la partie interne du revêtement d'aéronef (28).

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