Device for retracting aircraft landing gear

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/14 (2006.01) B64C 25/20 (2006.01)

Patent

CA 2744503

The present invention relates to aircraft landing gear, comprising a box-type structure (1) to be mounted in a hinged manner onto a structure of the aircraft, and a lower portion (2) carrying the wheels and which is movable relative to the box-type structure, the landing gear also comprising a device for retracting the landing gear between a deployed position and a raised position, said device comprising a first and a second member (11, 12) which are hitched to each other, the first member (11) being hitched to the lower portion (2) of the landing gear or to an element (5) that is movable with said lower portion during a movement of said lower portion relative to the box-type structure, while the second member (12) is hinged to the aircraft structure such that, while the landing gear is raised, the second member engages before the landing gear reaches the raised position.

Atterrisseur d'aéronef, comportant un caisson (1) destiné à être monté articulé sur une structure de 1'aéronef, et une partie inférieure (2) portant les roues et mobile relativement au caisson, l'atterrisseur comportant en outre un dispositif de raccourcissement de l' atterrisseur entre une position déployée et une position relevée, ledit dispositif comportant un premier et un deuxième membres (11, 12) attelés l'un à l'autre, le premier membre (11) étant attelé à la partie inférieure (2) de l'atterrisseur ou à un élément mobile (5) avec cette partie inférieure lors d'un mouvement de cette partie inférieure relativement au caisson, tandis que le deuxième membre (12) est articulé à la structure de l'aéronef de façon qu'au cours du relevage de l'atterrisseur, le deuxième membre vienne en butée avant que l'atterrisseur ne parvienne en position relevée.

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