Helicopter rotor

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Including movement limit stop or damping means

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416106, B64C 2738

Patent

active

045510679

ABSTRACT:
A rotor for helicopters, in which a central hub supports a plurality of radial blades connected thereto, each of which blade is provided with a surface rigidly connected to it and able to cooperate with respective abutment elements supported by the hub and movable with respect to this latter in a substantially horizontal plane to limit the oscillations of the respective blade in a horizontal plane between limits which are variable as a direct function of the angular velocity of the rotor itself.

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patent: 4235570 (1980-11-01), Ferris et al.
patent: 4297079 (1981-10-01), Marshall
patent: 4368006 (1983-01-01), Ferris et al.
patent: 4369019 (1983-01-01), Lovera et al.

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