Patent ID: 8956117
Filing Date: 2015-02-17
Classification: B64C

Abstract:
1. A rotor assembly for a rotary-wing aircraft, the rotor comprising: a central hub assembly having a flexure-type, twist-shank yoke with multiple arms, each arm being adapted for a rotor blade to be mounted thereto, the arms providing for pitch changes of blades attached to the yoke through twisting of portions of the arms about a corresponding pitch axis; an arm aperture formed in an inboard portion of each arm; an inboard pitch bearing associated with each arm, the inboard pitch bearing being attached to the hub assembly and allowing for rotation of the attached blade about the pitch axis, the inboard pitch bearing also allowing for out-of-plane motion of the arm relative to the hub assembly about a flapping axis; an inboard beam connected to each inboard pitch bearing and adapted to be attached to an associated blade, the beam extending through the associated arm aperture; and an outboard pitch bearing associated with each arm, the outboard pitch bearing being attached to the associated arm a selected distance from the inboard pitch bearing and allowing for rotation of the attached blade about the pitch axis.