Helicopter rotor hub, and rotor featuring such a hub

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Distally supported on radial arm

Reexamination Certificate

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Details

C416S13400R

Reexamination Certificate

active

06910865

ABSTRACT:
There is described a hub for a helicopter rotor, having a main body, and a number of connecting members projecting from the main body and for the connection of respective blades; the main body and the connecting members being defined by separate components connectable to one another by releasable fastening means.

REFERENCES:
patent: 3606575 (1971-09-01), Lermusiaux
patent: 3941503 (1976-03-01), Bruel
patent: 4342540 (1982-08-01), Lovera et al.
patent: 4568245 (1986-02-01), Hibyan et al.
patent: 4808075 (1989-02-01), Pariani et al.
patent: 4868962 (1989-09-01), McArdle et al.
patent: 4915585 (1990-04-01), Guimbal
patent: 5409183 (1995-04-01), Gunsallus
patent: 6032899 (2000-03-01), Mondet et al.
patent: 6200097 (2001-03-01), Mouille
patent: 1966039 (1971-09-01), None
patent: 0 362 117 (1990-04-01), None

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