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Dynamically tuned gyroscopes
   
Document Number
US Patent 4357837
Issued Date
November 9, 1982
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Abstract
Gyroscope apparatus includes a tubular rotor that is supported at opposite ends by bearings, such as a gas-lubricated bearing, for rotation about its axis. A gimbal ring encircles the rotor and is resiliently supported with the rotor, for angular displacement about an axis at right angles to the rotor axis, by a pair of flexure pivots located intermediate the ends of the rotor. An inertia ring is mounted concentrically with the gimbal ring by another pair of flexure pivots for angular displacement about an axis at right angles to the rotor axis and the axis of displacement of the gimbal ring. The major part of each flexure pivot is contained within the radial thickness of the gimbal ring. Displacement of the inertia ring is sensed by pick-offs the outputs of which are used to control the restoring torque applied by torquers located outwardly of the pick-offs.
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Dynamically tuned gyroscopes - US Patent 4357837 Drawing
Drawing from US Patent 4357837
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Number of Claims:
12
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Published
November 9, 1982
Application Number
06/200,793
Filed
October 27, 1980
US Classification
74/5F   74/5.46 74/5.6E 74/5.7
Int'l Classification
G01C   19/00   (20060101)   G01C   19/22   (20060101)  
Examiner
Attorney/Law Firm
Priority Data
Nov 16, 1979 [GB] 7939726
USPTO Field of Search
74/5F   74/5.46   74/5.47   74/5.6E   74/5.6D   74/5.7   74/5.4   308/DIG.1   308/2A  
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Claims
Description
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