Multi-bladed rotor system for rotorcraft

Details Multi-bladed rotor system for rotorcraft Multi-bladed rotor system for rotorcraft

B - Operations, Transporting

64

C

B64C 27/72 (2006.01) B64C 27/48 (2006.01)

Patent

CA 2707599

A rotor system for a rotorcraft includes a rotor having a plurality of pitch control links and a pair of rotor blades mechanically coupled with each of the plurality of pitch control links. A rotorcraft includes a power train, a mast extending from the power train, a rotor having a plurality of pitch control links, the rotor mechanically coupled with the mast, and a pair of rotor blades mechanically coupled with each of the plurality of pitch control links.

La présente invention se rapporte à un système de rotor pour giravion comprenant un rotor comportant une pluralité de liaisons de commande de tangage et une paire de pales de rotor couplées mécaniquement à chaque liaison de la pluralité de liaisons de commande de tangage. Un giravion comprend une transmission, un pylône s'étendant depuis la transmission, un rotor comportant une pluralité de liaisons de commande de tangage, le rotor couplé mécaniquement au pylône, et une paire de pales de rotor mécaniquement couplées à chaque liaison de la pluralité de liaisons de commande de tangage.

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