Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect
Patent
1988-03-09
1989-06-06
Chapman, John
Measuring and testing
Speed, velocity, or acceleration
Angular rate using gyroscopic or coriolis effect
310351, G01P 904
Patent
active
048360236
ABSTRACT:
To increase the quality factor Q of the vibrational angular rate sensor and therefore the sensitivity of the sensor, stabilize the sensor performance, facilitate wiring work, and minimize the sensor, a square pillar shaped vibrator, four vibrator node support pins and an external vibrator support base are all formed integral with each other from a single constant elasticity material block. Further, at least three and preferably four piezoelectric elements are connected to an external circuit via at least three and preferably four separate thin film conductive layers each extending from each piezoelectric element, on and along each vibrator node support pin, to an external vibrator support base.
REFERENCES:
patent: 4511821 (1985-04-01), Nakamura et al.
"Vibrating Angular Rate Sensor May Threaten the Gyroscope," William D. Gates, Electronics, Jun. 10, 1968, pp. 130-134.
"Solid State Angular Rate Sensor (VYRO)," L. D. Sunderland and E. F. Arthur, AIAA Control Conf., 1980, pp. 183-187.
Chapman John
Yazaki -Corporation
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