HOMING GYROSEEKER Russian patent published in 2004 - IPC

FIELD: guided missiles, in particular, homing head gyroseekers, used in control systems of artillery guided missiles.

SUBSTANCE: the spring motor in the gyroseeker of the artillery guided missile homing head is joined to the rotor by a double-stage cylindrical bushing installed for rotation on the body of the inner cavity of the spring motor, a catch engageable with the slot on the inner cavity of the spring motor is made on the stage of the smaller diameter. Radially directed dogs entering the bushing slots are positioned on the rear end surface of the rotor. A groove is made on the surface of the gimbal suspension base, and a radial slot that is engageable with the bulge of the L-shaped cylindrical retainer - on the rear end surface of the rotor.

EFFECT: enhanced impact strength of the gyroseeker of the artillery guided missile homing head.

4 dwg