Stiff-in-plane gimbaled tiltrotor hub

Details Stiff-in-plane gimbaled tiltrotor hub Stiff-in-plane gimbaled tiltrotor hub

B - Operations, Transporting

64

C

B64C 27/32 (2006.01)

Patent

CA 2635672

A rotor-hub for a rotary-wing aircraft is disclosed. The rotor-hub comprises a yoke comprising a plurality of yoke arms and a plurality of yoke straps, wherein the yoke arms are joined together by the yoke straps, and wherein a plurality of inner walls of the yoke define a central void space. A pitch horn is movably connected to the yoke and a portion of the pitch horn is located within the central void space. A connecting shell is fixedly attached to the yoke.

L'invention concerne un moyeu de rotor pour aéronef à voilure tournante. Ledit moyeu de rotor comprend une noix de cardan pourvue de plusieurs bras et de plusieurs sangles, lesdits bras étant reliés par les sangles, et plusieurs parois intérieures de la noix de cardan définissant un espace central vide. Un bras de commande de pas est connecté de manière amovible à la noix de cardan, une partie du bras de commande de pas étant placée dans l'espace central vide. Une coque de connexion est attachée de manière fixe à la noix de cardan.

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