US4150561A
Expired / Lapsed
US
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Employing a fluidic oscillator, for determining the constituent gases of a gas mixture
Assignee: Sunoco Inc
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Filing: 1978-05-01
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Granted: 1979-04-24
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Expires: 1998-05-01
Abstract
Abstract In order to determine the constituent gases of a gas mixture, the test gas is employed as the working fluid for an astable fluidic oscillator in a series of runs taken at different temperatures. The pulse repetition frequencies observed are related to similar pulse repetition frequencies observed when air is employed as the working fluid at corresponding temperatures and pressures. By this means, a plurality of equations can be written and solved for the unknown percentages. The characteristics of a given astable multivibrator can readily be predetermined and recorded on a graph in a table to facilitate preparation of equations which can be solved by ordinary simultaneous equation techniques.
Inventors
- 👤 Joseph E. Zupanick
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 23:38
CPC Classifications
G; G01; G01N; G01N29/00; G01N29/02; G01N29/024; Y; Y10; Y10T; Y10T137/00; Y10T137/206; Y10T137/2082; Y10T137/2229; Y10T137/2234
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
277 words
A method of determining the constituent gas proportions of a gas mixture comprising the steps of: (A) measuring the pulse repetition frequency of an astable fluidic oscillator while the gas mixture flows through the oscillator; (B) under the same pressure and temperature conditions employed in step (A), measuring the pulse repetition frequency of the astable fluidic oscillator while a standard example of a constituent gas flows through the oscillator; (C) repeating step (B) for each constituent gas for which the proportion of such gas in the gas mixture is to be determined; (D) repeating steps (A), (B), and (C), at a different temperature; (E) repeating step (D) until the total number of different temperatures at which pulse repetition frequency measurements are taken at least equals the total number of constituent gases for which the proportion of each in the gas mixture is to be determined; (F) solve, for C 1 . . . C n , the following simultaneous equations: 1/(prf)x.sub.T.sbsb.o =C.sub.1 /(prf)1.sub.T.sbsb.o =C.sub.2 /(prf)2.sub.T.sbsb.o =C.sub.3 /(prf)3.sub.T.sbsb.o + . . . +C.sub.n /(prf)n.sub.T.sbsb.o 1/(prf)x.sub.T.sbsb.1 =C.sub.1 /(prf)1.sub.T.sbsb.1 =C.sub.2 /(prf)2.sub.T.sbsb.1 =C.sub.3 /(prf)3.sub.T.sbsb.1 + . . . +C.sub.n /(prf)n.sub.T.sbsb.1 1/(prf)x.sub.T.sbsb.n =C.sub.1 /(prf)1.sub.T.sbsb.n =C.sub.2 /(prf)2.sub.T.sbsb.n =C.sub.3 /(prf)3.sub.T.sbsb.n + . . . +C.sub.n /(prf)n.sub.T.sbsb.n where: (prf)x T .sbsb.o =the pulse repetition frequency at temperature T o using the gas mixture as the working fluid; (prf)1.sub.T.sbsb.o, (prf)2.sub.T.sbsb.o, (prf)3.sub.T.sbsb.o, (prf)n.sub.T.sbsb.o =the pulse repetition frequency at temperature T o successively using each constituent gas as the working fluid; T o , T 1 , T n =signify different temperatures C 1 , c 2 , c 3 , c n =the respective proportions of the individual constituent gases to the whole of the gas mixture.
Claim 2
Independent Claim
277 words
A method of determining the constituent gas proportions of a gas mixture comprising the steps of: (A) measuring the pulse repetition frequency of an astable fluidic oscillator while the gas mixture flows through the oscillator; (B) under the same pressure and temperature conditions employed in step (A), measuring the pulse repetition frequency of the astable fluidic oscillator while a standard example of a constituent gas flows through the oscillator; (C) repeating step (B) for each constituent gas for which the proportion of such gas in the gas mixture is to be determined; (D) repeating steps (A), (B), and (C), at a different temperature; (E) repeating step (D) until the total number of different temperatures at which pulse repetition frequency measurements are taken at least equals the total number of constituent gases for which the proportion of each in the gas mixture is to be determined; (F) solve, for C 1 . . . C n , the following simultaneous equations: 1/(prf)x.sub.T.sbsb.o =C.sub.1 /(prf)1.sub.T.sbsb.o =C.sub.2 /(prf)2.sub.T.sbsb.o =C.sub.3 /(prf)3.sub.T.sbsb.o + . . . +C.sub.n /(prf)n.sub.T.sbsb.o 1/(prf)x.sub.T.sbsb.1 =C.sub.1 /(prf)1.sub.T.sbsb.1 =C.sub.2 /(prf)2.sub.T.sbsb.1 =C.sub.3 /(prf)3.sub.T.sbsb.1 + . . . +C.sub.n /(prf)n.sub.T.sbsb.1 1/(prf)x.sub.T.sbsb.n =C.sub.1 /(prf)1.sub.T.sbsb.n =C.sub.2 /(prf)2.sub.T.sbsb.n =C.sub.3 /(prf)3.sub.T.sbsb.n + . . . +C.sub.n /(prf)n.sub.T.sbsb.n where: (prf)x T .sbsb.o =the pulse repetition frequency at temperature T o using the gas mixture as the working fluid; (prf)1.sub.T.sbsb.o, (prf)2.sub.T.sbsb.o, (prf)3.sub.T.sbsb.o, (prf)n.sub.T.sbsb.o =the pulse repetition frequency at temperature T o successively using each constituent gas as the working fluid; T o , T 1 , T n =signify different temperatures C 1 , c 2 , c 3 , c n =the respective proportions of the individual constituent gases to the whole of the gas mixture.
Claim 3
Independent Claim
277 words
A method of determining the constituent gas portions of a gas mixture comprising the steps of: (A) measuring the pulse repetition frequency of an astable fluidic oscillator while the gas mixture flows through the oscillator; (B) under the same pressure and temperature conditions employed in step (A), measuring the pulse repetition frequency of the astable fluidic oscillator while a standard example of a constituent gas flows through the oscillator; (C) repeating step (B) for each constituent gas for which the proportion of such gas in the gas mixture is to be determined; (D) repeating steps (A), (B), and (C) at a different pressure; (E) repeating step (D) until the total number of different pressures at which pulse repetition frequency measurements are taken at least equals the total number of constituent gases from which the proportion of each in the gas mixture is to be determined; (F) solve, for C 1 . . . C n , the following simultaneous equations: 1/(prf)x.sub.T.sbsb.o =C.sub.1 /(prf)1.sub.T.sbsb.o =C.sub.2 /(prf)2.sub.T.sbsb.o =C.sub.3 /(prf)3.sub.T.sbsb.o + . . . +C.sub.n /(prf)n.sub.T.sbsb.o 1/(prf)x.sub.T.sbsb.1 =C.sub.1 /(prf)1.sub.T.sbsb.1 =C.sub.2 /(prf)2.sub.T.sbsb.1 =C.sub.3 /(prf)3.sub.T.sbsb.1 + . . . +.sub.n /(prf)n.sub.T.sbsb.1 1/(prf)x.sub.T.sbsb.n =C.sub.1 /(prf)1.sub.T.sbsb.n =C.sub.2 /(prf)2.sub.T.sbsb.n =C.sub.3 /(prf)3.sub.T.sbsb.n + . . . +C.sub.n /(prf)n.sub.T.sbsb.n where: (prf)x P .sbsb.o =the pulse repetition frequency at pressure P o using the gas mixture as the working fluid; (prf)1.sub.P.sbsb.o, (prf)2.sub.P.sbsb.o, (prf)3.sub.P.sbsb.o, (prf)n.sub.P.sbsb.o =the pulse repetition frequency at pressure P o successively using each constituent gas as the working fluid; P o , P 1 , P n =signify different pressure C 1 , c 2 , c 3 , c n =the respective proportions of the individual constituent gases to the whole of the gas mixture.
Claim 4
Independent Claim
277 words
A method of determining the constituent gas portions of a gas mixture comprising the steps of: (A) measuring the pulse repetition frequency of an astable fluidic oscillator while the gas mixture flows through the oscillator; (B) under the same pressure and temperature conditions employed in step (A), measuring the pulse repetition frequency of the astable fluidic oscillator while a standard example of a constituent gas flows through the oscillator; (C) repeating step (B) for each constituent gas for which the proportion of such gas in the gas mixture is to be determined; (D) repeating steps (A), (B), and (C) at a different pressure; (E) repeating step (D) until the total number of different pressures at which pulse repetition frequency measurements are taken at least equals the total number of constituent gases from which the proportion of each in the gas mixture is to be determined; (F) solve, for C 1 . . . C n , the following simultaneous equations: 1/(prf)x.sub.T.sbsb.o =C.sub.1 /(prf)1.sub.T.sbsb.o =C.sub.2 /(prf)2.sub.T.sbsb.o =C.sub.3 /(prf)3.sub.T.sbsb.o + . . . +C.sub.n /(prf)n.sub.T.sbsb.o 1/(prf)x.sub.T.sbsb.1 =C.sub.1 /(prf)1.sub.T.sbsb.1 =C.sub.2 /(prf)2.sub.T.sbsb.1 =C.sub.3 /(prf)3.sub.T.sbsb.1 + . . . +.sub.n /(prf)n.sub.T.sbsb.1 1/(prf)x.sub.T.sbsb.n =C.sub.1 /(prf)1.sub.T.sbsb.n =C.sub.2 /(prf)2.sub.T.sbsb.n =C.sub.3 /(prf)3.sub.T.sbsb.n + . . . +C.sub.n /(prf)n.sub.T.sbsb.n where: (prf)x P .sbsb.o =the pulse repetition frequency at pressure P o using the gas mixture as the working fluid; (prf)1.sub.P.sbsb.o, (prf)2.sub.P.sbsb.o, (prf)3.sub.P.sbsb.o, (prf)n.sub.P.sbsb.o =the pulse repetition frequency at pressure P o successively using each constituent gas as the working fluid; P o , P 1 , P n =signify different pressure C 1 , c 2 , c 3 , c n =the respective proportions of the individual constituent gases to the whole of the gas mixture.
Claim 5
Independent Claim
286 words
A method of determining the constituent gas proportions of a gas mixture comprising the steps of: (A) measuring the pulse repetition frequency of an astable fluidic oscillator while the gas mixture flows through the oscillator; (B) under the same pressure and temperature conditions employed in step (A), measuring the pulse repetition frequency of the astable fluidic oscillator while a standard example of a constituent gas flows through the oscillator; (C) repeating step (B) for each constituent gas for which the proportion of such gas in the gas mixture is to be determined; (D) repeating steps (A), (B), and (C) employing a different length feedback loop for the fluidic oscillator; (E) repeating step (D) until the total number of different feedback lengths employed at least equals the total number constituent gases from which the proportion of each in the gas mixture is to be determined; (F) solve, for C 1 . . . C n , the following simultaneous equations: 1/(prf)x.sub.l.sbsb.o =C.sub.1 /(prf)1.sub.l.sbsb.o =C.sub.2 /(prf)2.sub.l.sbsb.o =C.sub.3 /(prf)3.sub.l.sbsb.o + . . . +C.sub.n /(prf)n.sub.l.sbsb.o 1/(prf)x.sub.l.sbsb.1 =C.sub.1 /(prf)1.sub.l.sbsb.1 =C.sub.2 /(prf)2.sub.l.sbsb.1 =C.sub.3 /(prf)3.sub.l.sbsb.1 + . . . +C.sub.n /(prf)n.sub.l.sbsb.1 1/(prf)x.sub.l.sbsb.n =C.sub.1 /(prf)1.sub.l.sbsb.n =C.sub.2 /(prf)2.sub.l.sbsb.n =C.sub.3 /(prf)3.sub.l.sbsb.n + . . . +C.sub.n /(prf)n.sub.l.sbsb.n where: (prf)x l .sbsb.o =the pulse repetition frequency using the gas mixture as the working fluid; and employing feedback loop length l o ; (prf)1.sub.l.sbsb.o, (prf)2.sub.l.sbsb.o, (prf)3.sub.l.sbsb.o, (prf)n.sub.l.sbsb.o =the pulse repetition frequency successively using each constituent gas as the working fluid and employing feedback loop length l o ; l o , l 1 , l n =signify different feedback loop lengths; C 1 , c 2 , c 3 , c n =the respective proportions of the individual constituent gases to the whole of the gas mixture.
Claim 6
Independent Claim
286 words
A method of determining the constituent gas proportions of a gas mixture comprising the steps of: (A) measuring the pulse repetition frequency of an astable fluidic oscillator while the gas mixture flows through the oscillator; (B) under the same pressure and temperature conditions employed in step (A), measuring the pulse repetition frequency of the astable fluidic oscillator while a standard example of a constituent gas flows through the oscillator; (C) repeating step (B) for each constituent gas for which the proportion of such gas in the gas mixture is to be determined; (D) repeating steps (A), (B), and (C) employing a different length feedback loop for the fluidic oscillator; (E) repeating step (D) until the total number of different feedback lengths employed at least equals the total number constituent gases from which the proportion of each in the gas mixture is to be determined; (F) solve, for C 1 . . . C n , the following simultaneous equations: 1/(prf)x.sub.l.sbsb.o =C.sub.1 /(prf)1.sub.l.sbsb.o =C.sub.2 /(prf)2.sub.l.sbsb.o =C.sub.3 /(prf)3.sub.l.sbsb.o + . . . +C.sub.n /(prf)n.sub.l.sbsb.o 1/(prf)x.sub.l.sbsb.1 =C.sub.1 /(prf)1.sub.l.sbsb.1 =C.sub.2 /(prf)2.sub.l.sbsb.1 =C.sub.3 /(prf)3.sub.l.sbsb.1 + . . . +C.sub.n /(prf)n.sub.l.sbsb.1 1/(prf)x.sub.l.sbsb.n =C.sub.1 /(prf)1.sub.l.sbsb.n =C.sub.2 /(prf)2.sub.l.sbsb.n =C.sub.3 /(prf)3.sub.l.sbsb.n + . . . +C.sub.n /(prf)n.sub.l.sbsb.n where: (prf)x l .sbsb.o =the pulse repetition frequency using the gas mixture as the working fluid; and employing feedback loop length l o ; (prf)1.sub.l.sbsb.o, (prf)2.sub.l.sbsb.o, (prf)3.sub.l.sbsb.o, (prf)n.sub.l.sbsb.o =the pulse repetition frequency successively using each constituent gas as the working fluid and employing feedback loop length l o ; l o , l 1 , l n =signify different feedback loop lengths; C 1 , c 2 , c 3 , c n =the respective proportions of the individual constituent gases to the whole of the gas mixture.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-04-23 | 1982-10-23 | 1983-04-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-04-23 | 1986-10-23 | 1987-04-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-04-23 | 1990-10-23 | 1991-04-24 | $7700.00 | Window Closed / Lapsed |