Torque balanced rate gyro deriving its spin from a host projecti

Details Torque balanced rate gyro deriving its spin from a host projecti Torque balanced rate gyro deriving its spin from a host projecti

1986-04-11

1988-07-19

Brown, David H.

Aeronautics and astronautics

Missile stabilization or trajectory control

Stabilized by rotation

244 320, 74 5F, F41G 720

Patent

active

047579617

ABSTRACT:
A rate gyro instrument primarily for use in a gun fired spinning projectile eliminates all associated bearings by affixing the rotor to the spinning projectile body to obviate spin rotor bearings and by employing a flexible joint or constriction as a gimbal substitute to eliminate gimbal bearings.

REFERENCES:
patent: 3618403 (1971-11-01), Bilinski
patent: 4431150 (1984-02-01), Epperson, Jr.

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