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.