Bladed aircraft rotor with flexible blade mountings

Details Bladed aircraft rotor with flexible blade mountings Bladed aircraft rotor with flexible blade mountings

B - Operations, Transporting

64

C

244/15

B64C 27/32 (2006.01) B64C 27/35 (2006.01) B64C 27/41 (2006.01)

Patent

CA 1303002

ABSTRACT OF THE DISCLOSURE A bladed aircraft rotor is disclosed having blades mounted by means of flexible devices providing freedom for blade motions, at least in the flapping sense and in the pitch-change sense, without employment of flapping or pitch bearings or pivots, the rotor also being provided with a central bearingless joint for transmitting thrust forces while providing freedom for angular movement of the rotor as a whole about a center point on the axis of rotation. A constant velocity torque-transmitting system is also provided.

525960

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