Aeronautics and astronautics – Aircraft control – Pilot operated
Reexamination Certificate
2009-12-01
2010-10-05
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft control
Pilot operated
C244S220000, C244S235000
Reexamination Certificate
active
07806372
ABSTRACT:
A pedal system particularly tailored to a Fly-By-Wire (FBW) flight control system includes a double gradient linkage assembly. The double gradient linkage assembly includes a damper system and a spring system that improves yaw axis (azimuth) control of the aircraft. Control is only required when a change in the yaw axis state is demanded. Since only minimal displacement inputs to such a FBW flight control system is required, the travel of the pedals are exceeding compact, such that pilot workload is significantly reduced through the reduction in the frequency and magnitude of aircraft control inputs.
REFERENCES:
patent: 3733039 (1973-05-01), O'Conner et al.
patent: 3747876 (1973-07-01), Fortna et al.
patent: 4206891 (1980-06-01), Perez et al.
patent: 4345195 (1982-08-01), Griffith et al.
patent: 4529155 (1985-07-01), Bramwell et al.
patent: 4531692 (1985-07-01), Mateus
patent: 5131604 (1992-07-01), Yoerkie, Jr. et al.
patent: 5149023 (1992-09-01), Sakurai et al.
patent: 5601257 (1997-02-01), McKann
patent: 5607122 (1997-03-01), Hicks et al.
patent: 5738310 (1998-04-01), Rollet et al.
patent: 5746398 (1998-05-01), Rollet et al.
patent: 5868359 (1999-02-01), Cartmell et al.
patent: 5878981 (1999-03-01), Dewey
patent: 6053452 (2000-04-01), Yamakawa et al.
patent: 6128554 (2000-10-01), Damotte
patent: 6142413 (2000-11-01), Dequin et al.
patent: 6254037 (2001-07-01), Fenny et al.
patent: 6338454 (2002-01-01), Rollet et al.
patent: 6416015 (2002-07-01), Carson
patent: 6526338 (2003-02-01), Kubica et al.
patent: 6644600 (2003-11-01), Olson et al.
patent: 6755374 (2004-06-01), Carson
patent: 7644893 (2010-01-01), Boczar et al.
patent: 2004/0259687 (2004-12-01), Ritter et al.
patent: 2005/0204855 (2005-09-01), Fujiwara et al.
patent: 2005/0235820 (2005-10-01), Fujiwara et al.
patent: 2007/0112473 (2007-05-01), Ueno et al.
patent: 2010/0072322 (2010-03-01), Boczar et al.
Boczar Bruce
Stiles Lorren
Witiak Peter T.
Carlson & Gaskey & Olds PC
Dinh Tien
Sanderson Joseph W
Sikorsky Aircraft Corporation
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