Anvil-strap rotor

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Sectional – staged or nonrigid working member

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416134A, 416230, B64C 2738

Patent

active

044627556

ABSTRACT:
An aerodynamic rotor having a flexible blade comprising a plurality of planar layers and an anvil having configured bearing areas engagable with the flexed blade is presented. The plurality of layers are slidably movable in a shearing motion with respect to other layers. The blade is secured by the anvil with the configured bearing areas being engagable with an adjacent portion of the blade when the blade is flexed by forces created by the driven rotory motion of the anvil about an axis of rotation. Such a rotor with a laminated blade exhibits reduced head moment forces and reduced stress/strain forces within the blade thereby permitting improved reliability and maintenance.

REFERENCES:
patent: 1851098 (1932-03-01), Hermanson
patent: 2917274 (1959-12-01), Davidson
patent: 3706511 (1972-12-01), Abbott
patent: 4037990 (1977-07-01), Harris
patent: 4047839 (1977-09-01), Ferris et al.
patent: 4051289 (1977-09-01), Adamson
patent: 4137007 (1979-01-01), Schonball
patent: 4255478 (1981-03-01), Crane
patent: 4323332 (1982-04-01), Fradenburgh
patent: 4349317 (1982-09-01), Desjardins
patent: 4369018 (1983-01-01), Brunsch et al.
Report No. SER 13429 of Sikorsky Aircraft Division of the United Technolos Corporation dated Aug. 28, 1980, and in particular pp. 83, 84, 86, 112 and Figures 51 and 52 of said report.

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