US4869097A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Sonic gas pressure gauge
Assignee: Boeing North American Inc
•
Filing: 1988-03-23
•
Granted: 1989-09-26
•
Expires: 2008-03-23
Abstract
Abstract A method and an apparatus are provided for measuring the pressure of a gas within a sealed vessel. A sonic transducer is used to apply an oscillating force to the surface of the vessel. The frequency of the ultrasonic wave is swept through a range which causes resonant vibration of the gas in the vessel. A receiving transducer measures the amplitude of the resultant vibration at the vessel surface and reveals the resonant frequency of the gas as peaks in the amplitude of the sweep. The resonant frequency obtained depends upon the composition of the gas, its pressure and temperature, and the shape of the confining vessel. These relationships can be predetermined empirically so that the pressure inside the vessel can be calculated when the composition of the gas, its temperature, and shape of the confining vessel are known. The output of the receiver is fed into a computer which is programmed to calculate the pressure based upon these predetermined relationships which are stored in the computer.
Inventors
- 👤 Bernhard R. Tittmann
- 👤 John M. Richardson
- 👤 James R. Bulau
- 👤 Lawrence R. Bivins
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 19:49
CPC Classifications
G; G01; G01L; G01L11/00; G01L11/04
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
102 words
A method of measuring the gas pressure inside a closed vessel having stiff walls, comprising the steps of: applying an oscillating force to the external surface of the vessel at a particular frequency which is low enough to distinguish a gas resonance frequency peak from vessel wall resonance; detecting the amplitude of the resulting vibration of the vessel at the particular frequency; repeating the steps of applying and detecting for a range of frequencies; determining from the detected amplitudes the gas resonance frequency peak for acoustic energy within the vessel; and relating the resonance peak to the gas pressure within the vessel.
Claim 2
Independent Claim
102 words
A method of measuring the gas pressure inside a closed vessel having stiff walls, comprising the steps of: applying an oscillating force to the external surface of the vessel at a particular frequency which is low enough to distinguish a gas resonance frequency peak from vessel wall resonance; detecting the amplitude of the resulting vibration of the vessel at the particular frequency; repeating the steps of applying and detecting for a range of frequencies; determining from the detected amplitudes the gas resonance frequency peak for acoustic energy within the vessel; and relating the resonance peak to the gas pressure within the vessel.
Claim 3
Dependent Claim
38 words
The method as claimed in claim 1 wherein the step of determining a resonance peak comprises obtaining a relationship between frequency and amplitude within a predetermined frequency range and selecting the frequency at which a maximum amplitude occurs.
Claim 4
Dependent Claim
55 words
The method as claimed in claim 1 wherein the step of relating the resonance peak to the gas pressure comprises obtaining an empirical relationship between pressure and frequency of the resonance peak, and selecting the gas pressure inside the vessel which corresponds to the resonance peak obtained during the step of determining a resonance peak.
Claim 5
Dependent Claim
56 words
The method as claimed in claim 1 including the step of compensating the measured gas pressure for the effect of temperature by obtaining a relationship between resonant frequency of a gas and pressure at selected temperatures, measuring the temperature of the vessel, and selecting the gas pressure corresponding to the measured temperature and the determined frequency.
Claim 6
Independent Claim
132 words
An apparatus for measuring the gas pressure inside a closed vessel having stiff walls, comprising: a transmitting transducer for applying an oscillating force to the external surface of the vessel over a predetermined frequency range; a frequency generator connected to the transmitting transducer for causing the transducer to produce an oscillating force which sweeps with time over a predetermined frequency range at a low enough frequency to distinguish a gas resonance frequency peak from vessel wall resonance; a receiving transducer for detecting the amplitude of vibration at the surface of the vessel as a function of the sweep frequency; means coupled to the output of the receiving transducer for obtaining the gas resonance frequency peak within the vessel and for relating this frequency to the pressure of the gas in the vessel.
Claim 7
Independent Claim
132 words
An apparatus for measuring the gas pressure inside a closed vessel having stiff walls, comprising: a transmitting transducer for applying an oscillating force to the external surface of the vessel over a predetermined frequency range; a frequency generator connected to the transmitting transducer for causing the transducer to produce an oscillating force which sweeps with time over a predetermined frequency range at a low enough frequency to distinguish a gas resonance frequency peak from vessel wall resonance; a receiving transducer for detecting the amplitude of vibration at the surface of the vessel as a function of the sweep frequency; means coupled to the output of the receiving transducer for obtaining the gas resonance frequency peak within the vessel and for relating this frequency to the pressure of the gas in the vessel.
Claim 8
Dependent Claim
19 words
The apparatus as claimed in claim 5, wherein the transmitting transducer and the receiving transducer comprise a single transducer.
Claim 9
Dependent Claim
25 words
The apparatus as claimed in claim 5 wherein the transmitting transducer is a first piezoelectric transducer and the receiving transducer is a second piezoelectric transducer.
Claim 10
Dependent Claim
76 words
The apparatus as claimed in claim 5 wherein the means for obtaining the frequency of gas resonance and for relating this frequency to pressure comprise a computer which is coupled to the frequency generator and to the output from the receiving transducer, the computer being programmed to identify the frequency of gas resonance and to calculate the pressure from an empirically determined relationship between gas resonance frequency and gas pressure which is stored in its memory.
References Cited (Backward Citations)
US3252325A
Cited
US3802252A
Cited
US3942381A
Cited
US4187718A
Cited
SU759860A1
Cited
US4406157A
Cited
DE3029838A1
Cited
US4474061A
Cited
US4520654A
Cited
US4604898A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-09-25 | 1993-03-27 | 1993-09-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-09-25 | 1997-03-27 | 1997-09-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-09-25 | 2001-03-27 | 2001-09-26 | $7700.00 | Window Closed / Lapsed |