AIRCRAFT WING FLAP AND SLAT CONTROL SWITCHBOARD Russian patent published in 2014 - IPC B64C13/04 G05G1/04 

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering. Switchboard comprises load-carrying case composed of open frame with rectangular outline whereto fitted are two pairs of electromechanical drive toggle switches made up of two aligned two-arm levers. Two double control handles are arranged to act on, either simultaneously or separately, on said pairs of toggle switches. Aforesaid case has axle to support the levers of double handle. Toggle switches are equipped with rods with push heads and mounted at aforesaid frame, below said levers. Every pair of levers is fitted with coaxial slot and hinged two-arm retainer, one arm of the latter being arranged to be forced in coaxial slot of two levers to make a pair for every double handle. Other arm of the retainer is spring-loaded. Lower arm of handle levers is composed of control fork to allow fitting toggle switch rod head therein.

EFFECT: minimised time interval for actuation of standby control.

5 cl, 3 dwg