FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft manual control systems. Besides, control component can be jointed with controlled element via one or two springs arranged nearby control or controlled component, or nearby linkage elements. Said springs at control component neutral position stay at half the working stroke and are locked by spring end tooth.
EFFECT: higher precision of control.
3 cl, 2 dwg
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|
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| CONTROL FORCE COMPENSATOR | 2012 |
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|
RU2466445C2 |
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|
RU2531706C2 |
