Gyroscope cage system for high g environments

Machine element or mechanism – Mechanical movements – Rotary to or from reciprocating or oscillating

Patent

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Details

74 512, 74 522, G01C 1924

Patent

active

043229840

ABSTRACT:
A gyroscope caging system includes a clamping ring encircling a portion of the rotor of the gyro and adapted to engage an annular groove in the rotor simultaneously with engagement of a groove in a base support member, for clamping to and supporting the rotor during very high acceleration launches of a missile or airborne vehicle. The caging system is adapted to preload the gyroscope bearings in order to insure that the maximum load is carried by the cage device.

REFERENCES:
patent: 3992955 (1976-11-01), Evans

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