The invention provides an electric mechanism for an
aviation fuel valve, and belongs to the technical field of valve adjustment control. The electric mechanism comprises a motor, a shell, a speed
reducer, magnetic steel, a pointer, a Hall sensor, a
relay and an electric connector; the output end of the motor is connected with the speed
reducer; the pointer is coaxially fixed with the output end of the speed
reducer; the magnetic steel is fixedly connected with the pointer and coaxially rotates; the Hall sensor is arranged along the movement track of the pointer; and the electric connector is connected with a power supply, a superior
system of the host and the
relay. After the electric mechanism for the
aviation fuel valve receives a specified position
signal of a superior
system, the current shaft locking position of an output shaft is judged according to position
signal combinations of Hall sensors at different positions, then the current opening and closing position of a
ball valve assembly is judged, and the rotating direction of a motor is judged after the current opening and closing position is compared with a given position, and the reversing operation of the motor is realized through the
relay. Compared with the prior art, the invention has the advantages of high reliability and strong anti-interference capability, and meets the requirements of reliability and long endurance of
aviation products.