Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1976-04-27
1977-05-24
Pinkham, Richard C.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244 83D, G09B 908
Patent
active
040246515
ABSTRACT:
A variable feel side stick controller for producing and regulating feedback orces on a side stick for optimum pilot response. The controller consists of the floating table assembly which transfers the three-dimensional motion of the side stick into a two-dimensional motion. A series of hydraulic cylinders mounted on the floating table which are connected to a series of hydraulic circuits regulate the feedback forces produced on the side stick. The instantaneous position of the side stick can be determined from a series of linear potentiometers coupled to the hydraulic cylinders or from a series of force transducers connected to the hydraulic circuits. The two-dimensional floating table assembly allows use of a cam and cam follower arrangement which allows the force field to be varied with the shape of the cam.
REFERENCES:
patent: 2522434 (1950-09-01), Dehmel
patent: 2627675 (1953-02-01), Kittredge
patent: 3023516 (1962-03-01), Eisenberg
patent: 3031775 (1962-05-01), Cohen
patent: 3228478 (1966-01-01), Edenborough
patent: 3508346 (1970-04-01), Norman et al.
patent: 3805413 (1974-04-01), Burny et al.
Cochran II William W.
Hum Vance Y.
Pinkham Richard C.
Sciascia Richard S.
St.Amand Joseph M.
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