Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Reexamination Certificate
2006-04-11
2009-11-03
Eldred, J. Woodrow (Department: 3641)
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
C244S012200, C244S012300, C244S02300R, C073S458000, C073S468000
Reexamination Certificate
active
07611091
ABSTRACT:
A high-speed vertical take-off and land aircraft includes a body with an engine supported by the body. A fan assembly is also carried by the body. The fan assembly includes a hub and a plurality of blades to provide vertical lift for the aircraft. A plurality of frictionless air bearings vertically support the fan assembly while a plurality of idler wheels horizontally center the fan assembly. In addition the aircraft includes an active system for sensing vibration and balancing the fan assembly.
REFERENCES:
patent: 2667226 (1954-01-01), Doblhoff
patent: 2863261 (1958-12-01), Davis
patent: 2988152 (1961-06-01), Katzenberger et al.
patent: 3182929 (1965-05-01), Lemberger
patent: 3327969 (1967-06-01), Head
patent: 3514053 (1970-05-01), McGuinness
patent: 4452410 (1984-06-01), Everett
patent: 4773618 (1988-09-01), Ow
patent: 5039031 (1991-08-01), Valverde
patent: 5099430 (1992-03-01), Hirsch
patent: 5197010 (1993-03-01), Andersson
patent: 5507453 (1996-04-01), Shapery
patent: 5738302 (1998-04-01), Freeland
patent: 6382560 (2002-05-01), Ow
Ow Gordon Y. W.
Trent Donald J.
Eldred J. Woodrow
Go Aircraft Ltd.
King & Schickli PLLC
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