Gyroscope hinge assembly with adjustable axial compliance

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United States of America Patent

PATENT NO 4464942
SERIAL NO

06284892

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Abstract

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A universal joint hinge assembly for a tuned rotor gyroscope is insensitive to restraint changes due to spin axes accelerations. The hinge assembly is readily trimmable at the gyroscope wheel assembly to permit adjusting of the axial compliance of the gyroscope wheel thereby reducing the rectified torques due to linear acceleration.

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Patent Owner(s)

Patent OwnerAddress
KEARFOTT GUIDANCE AND NAVIGATION CORPORATION1225 MCBRIDGE AVENUE A CORP OF DE LITTLE FALLS NJ 07424

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Krupick, Walter J Succasunna, NJ 8 70

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