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High Resolution and Large Dynamic Range Resonant Pressure Sensor Based on Q-Factor MeasurementA pressure sensor has a high degree of accuracy over a wide range of pressures. Using a pressure sensor relying upon resonant oscillations to determine pressure, a driving circuit drives such a pressure sensor at resonance and tracks resonant frequency and amplitude shifts with changes in pressure. Pressure changes affect the Q-factor of the resonating portion of the pressure sensor. Such Q-factor changes are detected by the driving/sensing circuit which in turn tracks the changes in resonant frequency to maintain the pressure sensor at resonance. Changes in the Q-factor are reflected in changes of amplitude of the resonating pressure sensor. In response, upon sensing the changes in the amplitude, the driving circuit changes the force or strength of the electrostatic driving signal to maintain the resonator at constant amplitude. The amplitude of the driving signals become a direct measure of the changes in pressure as the operating characteristics of the resonator give rise to a linear response curve for the amplitude of the driving signal. Pressure change resolution is on the order of 10(exp -6) torr over a range spanning from 7,600 torr to 10(exp -6) torr. No temperature compensation for the pressure sensor of the present invention is foreseen. Power requirements for the pressure sensor are generally minimal due to the low-loss mechanical design of the resonating pressure sensor and the simple control electronics.
Document ID
20010010296
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Gutierrez, Roman C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Stell, Christopher B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Tang, Tony K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Vorperian, Vatche
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Wilcox, Jaroslava
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Shcheglov, Kirill
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Kaiser, William J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 7, 2013
Publication Date
July 11, 2000
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-158163
Patent Number: NASA-Case-NPO-20051-1-CU
Patent Number: US-Patent-6,085,594
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-NPO-20051-1-CU|US-Patent-6,085,594
Patent Application
US-Patent-Appl-SN-158163
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