FIELD: aircraft engineering.
SUBSTANCE: proposed device is composed by lever-spring or linear-spring mechanism in unstable equilibrium and comprises the lever attached to controlled element and/or control member and/or mid kinematic link and articulated with compression or tension spring end. Spring force is directed to controlled element pivot pin. Spring or push rod should be attached to the lever and to aircraft by two hinges.
EFFECT: reduced manual control force.
12 cl, 3 dwg
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