Control apparatus

Aeronautics and astronautics – Aircraft control – Pilot operated

Patent

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Details

244236, B64C 1304

Patent

active

051433303

ABSTRACT:
Control apparatus comprises a throttle stick suitable for STOVL aircraft which incorporates vectorable nozzle control means with thrust demand, thus obviating the need for a separate control lever for controlling vectorable nozzles. A handle (10) rotates to pre-determined angular positions in response to operator-exerted pressure, said pressure being sensed by force transducers (7a, 7b) hence providing the operator with tactile feedback proportional to thrust demand. A control lever (2) attached to the handle (10) is pivotable about a hinge pin (8). Rotation of the lever (2) about the pin (8) is sensed by a potentiometer (9) whose output is used to control vectorable nozzles.

REFERENCES:
patent: 2481776 (1949-09-01), Osborn
patent: 3061241 (1962-10-01), Holland, Jr.
patent: 3098628 (1963-07-01), Chaplin
patent: 3166273 (1965-01-01), Balluff
patent: 3409252 (1968-11-01), Miller
patent: 4574651 (1986-03-01), Nordstrom
patent: 4667909 (1987-05-01), Curci
patent: 4901948 (1990-02-01), Panos
patent: 4901952 (1990-02-01), Curtis
patent: 4982918 (1991-01-01), Kaye

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