Elastomeric universal rotor hub

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

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Details

416148, 464 91, B64C 2752

Patent

active

044772254

ABSTRACT:
This invention is directed to helicopter rotor hubs which includes an elastomeric material between an inner and outer hub. The inclusion of elastomeric material transmits torque, thrust and in-plane loads and is flexible in the tilt direction.

REFERENCES:
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patent: 2932179 (1960-04-01), Grant
patent: 3518025 (1970-06-01), Schmidt et al.
patent: 3804552 (1974-04-01), Covington
patent: 4297078 (1981-10-01), Martin
patent: 4323332 (1982-04-01), Fradenburgh
patent: 4333728 (1982-06-01), Drees

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