AIRCRAFT WING FLAP STANDBY CONTROL BOARD Russian patent published in 2014 - IPC B64C13/04 G05G1/04 

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering. Proposed switchboard comprises two electromechanical toggle switches of drive selectors for split interlocking and dual control handle composed of two aligned two-arm levers and arranged in switchboard case to actuate, simultaneously or independently, said toggle switches. Said levers have coaxial grooves and pivoted two-arm retainer, one arm thereof can be fitted in said groove. Other arm of the retainer is spring-loaded. Said case is composed of the frame with axle for dual handle levers to be fitted thereon. Toggle switches are equipped with rods with push heads and mounted at aforesaid frame, below said levers. Top arm of every lever has through exposed coaxial slot for it to be fitted in said slot and articulated with heat part of one of said levers. Lower arm of handle levers is composed of control fork to allow fitting toggle switch rod head therein.

EFFECT: fast actuation of standby control.

4 cl, 2 dwg