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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416107, B64C 2738

Patent

active

046522115

ABSTRACT:
Helicopter rotor on which each blade is connected in articulated manner to a center hub by means of a fork

REFERENCES:
patent: 4342540 (1982-08-01), Lovera et al.
patent: 4361415 (1982-11-01), Aubry
patent: 4369019 (1983-01-01), Lovera et al.
patent: 4504193 (1985-03-01), Mouille
patent: 4512717 (1985-04-01), Pancotti et al.
patent: 4516909 (1985-05-01), Caramaschi et al.
patent: 4540340 (1985-09-01), Pariani
patent: 4549851 (1985-10-01), Pariani
patent: 4549852 (1985-10-01), Hibyan
patent: 4551067 (1985-11-01), Caramaschi et al.

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