Split pivot fitting for helicopter landing gear

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/06 (2006.01) B64C 27/00 (2006.01)

Patent

CA 2712671

A multi-piece pivot fitting for use on aircraft with skid type landing gear has a forward fitting, and aft fitting, and at least a lower strap. This configuration allows cross tube loads to be transferred to the keel beams of the aircraft, thereby allowing selected longitudinal rocking of the aircraft and preventing the aircraft from going into a resonance state.

La présente invention concerne un raccord pivotant en plusieurs parties destiné à être utilisé sur un aéronef doté d'un train d'atterrissage de type à patins, le raccord présentant un raccord avant, et un raccord arrière, et au moins une sangle inférieure. Cette configuration permet de transférer les charges de traverse sur les poutres principales de l'aéronef, permettant de ce fait une embardée longitudinale sélectionnée de l'aéronef et empêchant l'aéronef de passer en état de résonance.

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