Soft inplane bearingless helicopter rotor

B - Operations – Transporting – 64 – C

Patent

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244/15

B64C 27/32 (2006.01) B64C 27/33 (2006.01) B64C 27/51 (2006.01)

Patent

CA 1209558

Abstract: The present invention relates to a soft inplane bearingless rotor which is to be rigidly mounted on a helicopter mast. The rotor is comprised of a unitary yoke which has a flat hub section adapted to be anchored to the end of the mast and has diametrically opposed blade-supporting arms which extend from the hub section. Each arm has a thin flapping section adjacent the hub section and a feathering section which extends from the flapping section. Blade attachments are located at the end of each of the arms. The arms include a plurality of fiber reinforced composite parallel ribs which extend span-wise with a predetermined inplane spacing. A blade is secured to each attachment with a cuff which extends inboard to the flapping section. A bearing structure interconnects the inboard end of the cuff and the flapping section and includes an inplane resilient structure for soft inplane restraint of the blade.

431061

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