Wireless flight control system

Aeronautics and astronautics – Aircraft control

Patent

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Details

244189, B64C 1324

Patent

active

055314023

ABSTRACT:
A primary or backup flight control system for controlling the flight path of an aircraft or spacecraft using wireless transmitters (15 and 16) located near the flight deck (14) and positioned within, or on, the outer skin of the fuselage (10). These transmitters (15 and 16) send pilot-generated, wireless, e.g. infra-red, flight control signals (17 and 18) to receivers (19 and 21) located within, or on, the engines, wings, and tail assembly surfaces. These signals (17 and 18) are then directed to their respective engines or moveable flight control surfaces. These wireless control signals (17 and 18) are transmitted externally of the fuselage structure (10) and the transmission and receipt of these signals takes place on a single aircraft or spacecraft structure. In case of fuselage damage, e.g., due to structural failure, internal explosions, air-to-air collision, or military combat, which damages the primary flight control system (hydraulic, wire or cable), the present system will remain operative.

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Popular Science Magazine, Dec. 1993, pp. 22 and 72 Sun. Nov. 13, 1994, S.F. TV Station Kron, Ch. 4 Program "Next Step" re. Boeing 777.

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