CONTROL UNIT OF UNMANNED CONTROLLED AIRCRAFT Russian patent published in 2020 - IPC F42B10/14 F42B15/00 

FIELD: aviation.

SUBSTANCE: invention relates to control of aircraft and can be used in guided missiles intended for planning of unmanned aerial vehicles. Proposed device comprises casing with radial partitions arranged in cross-like manner, rudder opening mechanism, electric motor and electronic control system. Between the walls of each radial partitions there is a steering machine with a steering wheel. Electric motor is located along the central axis of the steering unit. Each rudder is rigidly connected with the output shaft of the corresponding steering machine containing a cylindrical reduction gear with a motor. Each steering machine is arranged on its transverse axis with the possibility of rotation on this axis together with the rudder by the angle required for the rudder output into the working position under the action of the moment transmitted to the steering machine housing through the worm sector fixed on the body, which is engaged with the corresponding steering machine worm gear shaft. Each worm shaft is provided with possibility to receive torque through cylindrical gear transmission from electric motor. It is possible to issue control commands to steering machines by electronic control system.

EFFECT: ensuring synchronization of opening of rudders, reduction of overall dimensions and increase in reliability.

1 cl, 5 dwg