Aeronautics and astronautics – Aircraft control – Pilot operated
Reexamination Certificate
2011-01-25
2011-01-25
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft control
Pilot operated
C244S220000, C074S512000, C074S560000, C074S562000
Reexamination Certificate
active
07874526
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.
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Boczar Bruce
Stiles Lorren
Witiak Peter T.
Carlson, Caskey & Olds, PC
Dinh Tien
Sanderson Joseph W
Sikorsky Aircraft Corporation
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