FIELD: machine building.
SUBSTANCE: invention relates to designs of aircraft manual controls. Aircraft control handle (200) contains frame (201), handle (202), installed with possibility to turn relative to frame, and handle with frame connection mechanical devices (203). Mechanical devices (203) contain first connecting element (213, 223), installed with possibility of movement relative to frame (201) around first axis (X), second connecting element (233, 243), installed with possibility of movement relative to frame (201) around second axis (Y), forming with first axis angle other than zero. Third intermediate element (255, 265) is installed with possibility to turn relative to first element (213, 223) around third axis (Y'). Fourth intermediate element (275, 285) is installed with possibility to turn relative to second connecting element (233, 243) around fourth axis (X'), forming with third axis angle other than zero. Connecting elements (213, 223, 233, 243) or intermediate elements (255, 265, 275, 285) are installed with possibility to turn relative to each other around fifth axis (Z').
EFFECT: enabling independence of return forces acting on handle, along two axes of rotation.
19 cl, 15 dwg
