Pivoting panel for aircraft, and composite support piece

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 9/02 (2006.01) B64C 1/06 (2006.01) B64C 1/26 (2006.01)

Patent

CA 2522949

The invention relates to a pivoting panel for an aircraft and to a composite support piece for this kind panel. The support piece (17) is arranged as a part of the frame structure of the panel (3). The support piece has an extension portion (23) to which an actuator connection fitting (7) of an actuator (4) can be fastened. The extension portion (23) distributes the forces to the structures of the panel (3).

L'invention concerne un panneau pivotant pour un aéronef et une pièce de support composite pour ce type de panneau. La pièce de support (17) est disposée dans la structure de cadre du panneau (3). La pièce de support comporte une partie d'extension (23) à laquelle on peut fixer une armature de raccordement (7) d'un actionneur (4). La partie d'extension (23) distribue les forces sur les structures du panneau (3).

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