GYROSCOPIC INSTRUMENT Russian patent published in 2004 - IPC

Abstract RU 2239788 C1

FIELD: control system of guided artillery projectiles; anti-tank and anti-aircraft missiles.

SUBSTANCE: proposed gyroscopic instrument has outer gimbal frame ring with brush of angle sensor mounted on base; plate with rounded-off edges mounted in parallel with rotor axis is engageable with two flat springs mounted on base of gimbal suspension symmetrically relative to outer frame ring whose planes are perpendicular to axis of rotation of outer frame ring. Deceleration unit mounted of base of gimbal suspension is used for application of friction moment to outer frame ring during its turn through angle exceeding dead zone relative to base.

EFFECT: increase of angle of turn of projectile.

3 dwg

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RU 2 239 788 C1

Authors

Filimonov V.Ja.

Dates

2004-11-10—Published

2003-06-18—Filed