Skid-type landing gear for helicopter

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/52 (2006.01)

Patent

CA 2207787

Landing gear for helicopter, including two skids P each having a longitudinal ground contact section 1 and being connected to a forward crossmember and an aft crossmember 2, which are in turn attached to the airframe by brackets 4, 6, the aft crossmember 2 being attached at the tips of its lower ends 2a to the after part of the said longitudinal contact sections 1. Each of the said skids P has at its forward end an inclined transition zone T having two curves C1, C2 and being aligned perpendicular to the said longitudinal ground contact sections, above the plane of these sections, the two transition zones constituting together, in this manner, an integrated forward crossmember, offset in relation to the forward limit of the plane of contact with the ground of the said longitudinal contact sections of the skids. Application to light helicopters.

Train d'atterrissage pour hélicoptère, comprenant deux patins P présentant chacun une plage longitudinale d'appui au sol 1 et reliés à une traverse avant et à une traverse arrière 2 elles-mêmes assujetties à la structure de l'appareil par des organes de liaison 4, 6, la traverse arrière 2 étant fixée par les extrémités de ses branches descendantes 2a à la partie arrière desdites plages longitudinales d'appui 1. Chacun desdits patins P présente à l'avant une zone de transition inclinée T à double courbure C1, C2 s'orientant transversalement auxdites plages longitudinales d'appui au sol, au-dessus du plan de ces dernières, les deux zones de transition constituant ensemble, de la sorte, une traverse avant intégrée, décalée par rapport à la délimitation avant du plan de contact desdites plages longitudinales d'appui des patins sur le sol. Application aux hélicoptères légers.

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