Helicopter rotor hub

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Nonmetallic resilient mounting

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416244R, 416141, B64C 1106

Patent

active

045211574

ABSTRACT:
A helicopter rotor hub having a lobed shape defining a plurality of bridge structures each allowing the attachment of a respective blade; each bridge structure is formed of superimposed sections of three annular bands, of synthetic material, the intermediate one of which forms an outer frame extending around the whole of the periphery of the hub, while the other two define one of the said lobes and connect the said outer frame to an inner metal structure.

REFERENCES:
patent: 3384185 (1968-05-01), Fernandez
patent: 3824037 (1974-07-01), Mautz
patent: 4156583 (1979-05-01), Mayerjak
patent: 4195967 (1980-04-01), Weiland
patent: 4257738 (1981-03-01), Schwarz et al.
patent: 4321013 (1982-03-01), Schwarz et al.
patent: 4352632 (1982-10-01), Schwarz et al.
patent: 4425082 (1984-01-01), Mussi et al.

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