Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Nonmetallic resilient mounting
Patent
1982-01-29
1984-10-16
Powell, Jr., Everette A.
Fluid reaction surfaces (i.e., impellers)
Articulated, resiliently mounted or self-shifting impeller...
Nonmetallic resilient mounting
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:
patent: 2259460 (1941-10-01), Dexter
patent: 2312822 (1943-03-01), Julien et al.
patent: 2333166 (1943-11-01), Fraser
patent: 2369538 (1945-02-01), D'Aubarede
patent: 2640553 (1953-06-01), Hafner
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
Powell Jr. Everette A.
The Boeing Company
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