FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly, to designs of aircraft control devices. Aircraft control handle (1) contains frame (2), handle (3), handle with frame connection mechanical devices (4), providing possibility of handle (3) rotation relative to frame (2) around first axis (X) of rotation. Mechanical devices (4) comprise first hinged joint (9), wherein first hinged joint (9) comprises first part, second part, installed with possibility of movement relative to first part, and at least two flexible plates. Each of flexible plates has end, attached to first part, and other end attached to second part, and can be resilient deformed to enable possibility of second part rotation relative to first part around first turning axis (X) creating return torque counteracting second part turning relative to first part.
EFFECT: enabling possibility to create return forces with high accuracy and stability.
14 cl, 23 dwg
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Authors
Dates
2017-01-19—Published
2013-06-07—Filed