Vibratory angular rate sensing system

Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect

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310329, 310333, 310370, G01P 904

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active

045384614

ABSTRACT:
A vibratory angular rate sensing system may have one pair of tines forming an angle of about 60 degrees, resulting from the crystalline orientation of the Z-cut quartz wafer of the system. In one configuration each of the tines is provided with a mass offset from the axis of the associated tine, a pivot extends through the plane of symmetry of the tines and may be connected to a dummy reaction mass. The resonant system is suspended from a mounting frame by a pair of suspension bridges. A second embodiment of the invention features two groups of tines, each group including two pairs of tines arranged in the form of a cross. Again, an offset mass is associated with the free end of each tine and each group of tines is secured to its frame by a suspension bridge.

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R. E. Barnaby et al., "General Theory and Operational Characteristics of the Gyrotron Angular Rate Tachometer", Nov. 1953, pp. 31-36, Acoust. Eng. Review.
J. L. Lyman, "A New Space Rate Sensing Instrument", Nov. 1953, pp. 21-30, Acout. Engineering Review.
C. T. Morrow, "Zero Signals in the Sperry Tuning Fork Gyrotron", May 1955, pp. 581-585, Journal of Acoustical Society of America.
G. C. Newton, "Comparison of Vibratory and Rotating Wheel Gyroscopic Rate Indicators", Jul. 1960, pp. 143-150, Part II, Transactions of the American Institute of Electronics Engineers (AIEE).
G. C. Newton, "Theory and Practice in Vibratory Rate Gyros", Jun. 1963, pp. 95-99, Control Engineering.

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