FIELD: machine building.
SUBSTANCE: invention relates to a control system unit, in particular to a control system unit comprising a three-axis control handle. Module of aircraft control handle includes assembly containing first and second shaft connected to each other, and gimbal mechanism. At that joint is jointed with universal joint and joint rotation source coincides with cardan mechanism rotation source. Cardan mechanism provides a rotation axis for the first shaft, and the connection provides a rotational axis for the first shaft. Rotational axes provided by the cardan mechanism and axes of rotation provided by the connection intersect at coincidence of rotation sources. Cardan mechanism contains the first universal joint located inside the second cardan joint and connected with possibility of rotation with this second cardan joint. Besides, the second cardan joint is located inside the frame and is connected to this frame with possibility of rotation. At that, said assembly comprises sensors for measurement and control of rotation of the first cardan joint, the second cardan joint and the second shaft.
EFFECT: higher convenience in aircraft control.
9 cl, 8 dwg
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Authors
Dates
2020-06-16—Published
2016-04-22—Filed