Bearingless rotor for single and tandem helicopters

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

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416141, B64C 2740

Patent

active

043493173

ABSTRACT:
A bearingless rotor system has a flexible strap member to which the root of a rotor blade is attached, and a pitch rod aligned with the pitch axis and mounted to the rotor blade root and to a pitch arm, which arm transmits control system variations by way of a pitch link to the pitch rod. Tapered shoes are disposed adjacent the surfaces of the strap and are capable of applying a restoring force to the strap in opposition to flexural displacements of the strap member.

REFERENCES:
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patent: 3762834 (1973-10-01), Bourquardez et al.
patent: 3765267 (1973-10-01), Bourquardez et al.
patent: 3874815 (1975-04-01), Baskin
patent: 3880551 (1975-04-01), Kisovec
patent: 3999887 (1976-12-01), McGuire
patent: 4008980 (1977-02-01), Noehren et al.
patent: 4047839 (1977-09-01), Ferris et al.
patent: 4104003 (1978-08-01), Mouille
patent: 4111605 (1978-09-01), Roman et al.
patent: 4293277 (1981-10-01), Aubry

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