Control apparatus

Aeronautics and astronautics – Aircraft control – Pilot operated

Patent

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Details

244230, B64C 1328

Patent

active

050625969

ABSTRACT:
Control apparatus, such as an aircraft throttle box, includes a manual control member 8 linearly movable on a first shaft 2. The position of the control member is sensed by rotation of the shaft 2 to generate an output control signal. In order to balance the apparatus, especially against high g-forces, a second shaft 3 is provided, parallel to the first carrying a counterweight 13 that moves together with the control member 8, but in the opposite direction.

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patent: 4494061 (1985-01-01), Kaye
patent: 4513235 (1985-04-01), Acklam et al.
patent: 4516063 (1985-05-01), Kaye et al.
patent: 4569453 (1986-02-01), Oustad
patent: 4947070 (1990-08-01), Hill
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