Russian Aviation two-phase engine DID-1TA. 

1W, 18000 rpm  , Lot of 1 pcs.

 The DID-1TA two-phase induction engine is designed to work in reversible low-inertia drives of aviation automation.

    Designed to operate in conditions of high rigidity, typical for products of aviation equipment. Heat resistant. Hollow non-magnetic rotor. 

    Technical characteristics of devices engines DID-1TA two-phase induction: 

    Control and excitation winding voltage 30 V

    Maximum power on the shaft - 1W;

    Electromechanical time constant of the device engine DID-1TA two-phase induction - 38ms;

    Rotation speed at a temperature of 20ºС ± 5ºС - 18000 rpm;

    Power supply - 36 V;

    The frequency of the device engine DID-1TA two-phase induction  50 - 400 Hz;

    Net engine power - 0,014W;

    Nominal torque - 0,068Н ∙ m;

    D=33mm, L=55mm.

1,3 - Excitation winding.

2,4 - Control winding.

5,6 - Jumper.