Oleo strut with positive retention in a retracted and crash...

Details Oleo strut with positive retention in a retracted and crash... Oleo strut with positive retention in a retracted and crash...

B - Operations, Transporting

64

C

B64C 25/60 (2006.01)

Patent

CA 2627224

The invention relates to a telescopic shock strut for aircraft landing gear, comprising a strut assembly (1) in which a rod (2) is mounted for sliding, the shock strut comprises controlled means (41 43) for retracting the rod into the strut assembly up to a reacted position. The strut assembly comprises means (27, 29) for positively retaining the rod in the strut assembly and are designed for holding the rod in a retracted position when the rod is brought therein by the retracting means, the positive retaining means being designed for, at least during a hard landing of the aircraft, enabling the rod to push into the strut assembly beyond the retracted position.

L~invention concerne un amortisseur télescopique pour atterrisseur d'aéronef, comportant un caisson (1) dans lequel une tige (2) est montée pour coulisser, l'amortisseur comportant des moyens commandés de rétraction (41~43) de la tige dans le caisson jusqu'à une position rétractée. L'amortisseur comporte des moyens de retenue positive (27, 29) de la tige dans le caisson adaptés à retenir la tige en position rétractée lorsque la tige y est amenée par les moyens de rétraction, les moyens de retenue positive étant agencés pour, au moins lors d'un atterrissage sévère de l'aéronef, autoriser l'enfoncement de la tige dans le caisson au delà de la position rétractée.

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