Headpiece support for rotor of a rotary wing aircraft

Fluid reaction surfaces (i.e. – impellers) – Support mounting – carrier or fairing structure

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Details

416229R, 416241A, B64C 1106

Patent

active

043210139

ABSTRACT:
In a rotor for a rotary wing aircraft, an integral central headpiece supps the rotor blades. The headpiece consists of two plates interconnected by a centrally arranged distance member. Each plate has a similar star-shape with at least four angularly spaced point-like arms. Each plate is formed of a number of superposed layers with each layer containing continuous loops extending in the direction of the point-like arms. At least one loop extends from one point-like arm into another diametrically opposite point-like arm. Others of the loops, located in the other point-like arms, extend radially outwardly from the loop extending through the two point-like arms. The headpiece consisting of the plates and distance member, is a unitary or integral structure.

REFERENCES:
patent: 3279278 (1966-10-01), Eldred
patent: 3384185 (1968-05-01), Fernandez
patent: 4156583 (1979-05-01), Mayerjak
patent: 4257738 (1981-03-01), Schwarz et al.

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