Rotor hub and controls for multi-bladed rotor system

Details Rotor hub and controls for multi-bladed rotor system Rotor hub and controls for multi-bladed rotor system

B - Operations, Transporting

64

C

B64C 27/54 (2006.01)

Patent

CA 2762219

A rotor system for a rotorcraft includes a rotor hub having a plurality of rotor blade pairs mechanically coupled to a rotor mast. A pitch link assembly is mechanically coupled to each rotor blade pair for controlling the pitch angle of each rotor blade pair in tandem. Each rotor blade pair has an upper rotor blade and a lower rotor blade. The plurality of rotor blade pairs rotor in a single direction and about a single axis of rotation.

L'invention concerne un système de rotor pour un giravion comprenant un moyeu de rotor comprenant une pluralité de paires de pales de rotor couplées mécaniquement à un mât de rotor. Un ensemble de commande de pas est mécaniquement couplé à chaque paire de pales de rotor pour contrôler l'angle de pas de chaque paire de pales de rotor en tandem. Chaque paire de pales de rotor comprend une pale de rotor supérieure et une pale de rotor inférieure. La pluralité de paires de pales de rotor tourne dans un sens unique et autour d'un axe de rotation unique.

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