Control yoke apparatus for computerized aircraft simulation

Education and demonstration – Vehicle operator instruction or testing – Flight vehicle

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G09B 908

Patent

active

046593136

ABSTRACT:
An aircraft control yoke apparatus includes an inexpensive mechanism for manipulating a two axis variable transducer and is especially adaptable for use with microcomputers. The apparatus includes a control wheel attached at one end to a shaft which is in turn supported by a linear bearing. The linear bearing permits the shaft to rotate and simultaneously move back and forth. A crank mechanism is attached to the other end of the shaft and serves to amplify the rotational movement of the steering wheel. A resilient, elastic material like natural isoprene rubber connects the crank to a two axis variable transducer. The elastic material causes the two axis transducer to follow the motion of the rotational and back and forth movement of the steering wheel. A return-to-center mechanism causes the wheel to return to a neutral position when no force is applied to it. A very life-like simulation of airplane flight is achieved with a minimum of expense and a high degree of realism.

REFERENCES:
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patent: 2937458 (1960-05-01), Leuthold
patent: 3024539 (1962-03-01), Rider
patent: 3031775 (1962-05-01), Cohen
patent: 3918021 (1975-11-01), Nishioka et al.
patent: 4386914 (1983-06-01), Dustman
patent: 4478407 (1984-10-01), Manabe
patent: 4599070 (1986-07-01), Hladky et al.

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