Elastomeric helicopter rotor load reaction system

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

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Details

416140, 416141, B64C 1106, B64C 2738

Patent

active

042355702

ABSTRACT:
A helicopter rotor having one or more blades mounted for rotation with the rotor hub and each supported therefrom by an elastomeric bearing, and having a lead-lag damper connected to the blade and the hub and extending substantially parallel to the blade axis, and including the improvement of apparatus for preventing tension loading of the elastomeric bearing as the blade moves radially inwardly as a result of rotor braking.

REFERENCES:
patent: 3282350 (1966-11-01), Kisovec
patent: 3591310 (1971-07-01), Mouille
patent: 3862812 (1975-01-01), Gorndt et al.
patent: 4028001 (1977-06-01), Watson
patent: 4141664 (1979-02-01), Moran et al.

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