FIELD: flying vehicle control systems.
SUBSTANCE: proposed mechanism has base 1 mounted on flying vehicle case, drive for connection of functional unit 4, input bell crank 2 and output bell crank 3 articulated together and provided with hinges for connection of rod 5 of pilot's command lever and rod 6 of functional unit. Both bell cranks are articulated with functional unit cut-in drive and radii of arms from articulation of bell cranks to hinge of attachment to base of input bell crank and to hinge of connection of functional unit rod to output bell crank are equal.
EFFECT: reduced mass of mechanism; enhanced reliability.
2 dwg
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