US4655608A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Non-perturbing beam deflection system and method for high repetition rate temperature measurement of combustion flames
Assignee: United States Department of the Air Force
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Filing: 1985-10-24
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Granted: 1987-04-07
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Expires: 2005-10-24
Abstract
Abstract A novel laser beam deflection system and method for temperature measurement of combustion flames of known composition is described which comprises a thin wire for placement at a predetermined location within the flame; a pulsed laser source for directing a pulsed beam onto the wire for heating the wire and immediately surrounding gases of the flame to produce an acoustic pulse in the flame; a pair of probe laser sources for directing parallel probe beams through the flame in predetermined spaced relationship to each other and to the wire, and a pair of detectors and associated electronics for detecting the respective deflections of the probe beams resulting from interactions with the pulse and measuring the time difference between respective deflections of the probe beams to determine the speed of the acoustic pulse through the flame and the temperature of the flame from the speed determination.
Inventors
- 👤 Larry P. Goss
- 👤 Dennis F. Grosjean
- 👤 Benjamin Sarka, Jr.
- 👤 Sigmund W. Kizirnis
- 👤 Biswa N. Ganguly
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 06:09
CPC Classifications
G; G01; G01K; G01K11/00; G01K11/22; G01K11/24
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
180 words
A method for determining the temperature of a combustion flame of known composition comprising: a. supporting a thin wire at a preselected position within said flame, said wire selected to rapidly couple energy to the immediately surrounding gases of said flame when said wire is heated; b. directing a first pulsed laser beam onto said wire to produce localized heating of said wire and the immediately surrounding gases of said flame whereby a pressure increase in the form of an acoustic pulse is generated within said flame; c. directing parallel second and third laser beams through said flame in predetermined spaced relationship to each other and to said wire; d. detecting the respective deflections of said second and third laser beams resulting from interactions thereof with said acoustic pulse; e. measuring the time difference between respective said deflections of said second and third laser beams to determine the speed of said acoustic pulse through said flame; and f. determining the temperature of said flame from said speed determination and said predetermined spaced relationship between said second and third laser beams.
Claim 2
Independent Claim
180 words
A method for determining the temperature of a combustion flame of known composition comprising: a. supporting a thin wire at a preselected position within said flame, said wire selected to rapidly couple energy to the immediately surrounding gases of said flame when said wire is heated; b. directing a first pulsed laser beam onto said wire to produce localized heating of said wire and the immediately surrounding gases of said flame whereby a pressure increase in the form of an acoustic pulse is generated within said flame; c. directing parallel second and third laser beams through said flame in predetermined spaced relationship to each other and to said wire; d. detecting the respective deflections of said second and third laser beams resulting from interactions thereof with said acoustic pulse; e. measuring the time difference between respective said deflections of said second and third laser beams to determine the speed of said acoustic pulse through said flame; and f. determining the temperature of said flame from said speed determination and said predetermined spaced relationship between said second and third laser beams.
Claim 3
Dependent Claim
21 words
The method as recited in claim 1 wherein said first laser beam is produced by a low power pulsed Nd:YAG laser.
Claim 4
Dependent Claim
19 words
The method as recited in claim 1 wherein said second and third laser beams are produced by HeNe lasers.
Claim 5
Dependent Claim
31 words
The method as recited in claim 1 wherein said wire comprises a material selected from the group consisting of tungsten, titanium, aluminum titanium alloy, nickel, stainless steel, copper, brass, and aluminum.
Claim 6
Independent Claim
185 words
A system for determining the temperature of a combustion flame of known composition comprising: a. a thin wire for placement at a predetermined location within said flame, said wire selected to rapidly couple energy to the immediately surrounding gases of said flame when said wire is heated; b. a first pulsed laser source for directing a first pulsed laser beam onto said wire for heating said wire and the immediately surrounding gases of said flame to produce an acoustic pulse within said flame; c. second and third laser sources for directing parallel second and third laser beams through said flame in predetermined spaced relationship to each other and to said wire; d. means for detecting the respective deflections of said second and third laser beams resulting from interactions thereof with said acoustic pulse; and e. means for measuring the time difference between respective said deflections of said second and third laser beams to determine the speed of said acoustic pulse through said flame and the temperature of said flame from said speed determination and said predetermined spaced relationship between said second and third laser beams.
Claim 7
Independent Claim
185 words
A system for determining the temperature of a combustion flame of known composition comprising: a. a thin wire for placement at a predetermined location within said flame, said wire selected to rapidly couple energy to the immediately surrounding gases of said flame when said wire is heated; b. a first pulsed laser source for directing a first pulsed laser beam onto said wire for heating said wire and the immediately surrounding gases of said flame to produce an acoustic pulse within said flame; c. second and third laser sources for directing parallel second and third laser beams through said flame in predetermined spaced relationship to each other and to said wire; d. means for detecting the respective deflections of said second and third laser beams resulting from interactions thereof with said acoustic pulse; and e. means for measuring the time difference between respective said deflections of said second and third laser beams to determine the speed of said acoustic pulse through said flame and the temperature of said flame from said speed determination and said predetermined spaced relationship between said second and third laser beams.
Claim 8
Dependent Claim
19 words
The system as recited in claim 5 wherein said first laser source comprises a low power pulsed Nd:YAG laser.
Claim 9
Dependent Claim
17 words
The system as recited in claim 5 wherein said second and third laser sources comprise HeNe lasers.
Claim 10
Dependent Claim
31 words
The system as recited in claim 5 wherein said wire comprises a material selected from the group consisting of tungsten, titanium, aluminum titanium alloy, nickel, stainless steel, copper, brass, and aluminum.
Claim 11
Dependent Claim
16 words
The system as recited in claim 5 wherein said first laser source has predetermined pulse rate.
Claim 12
Independent Claim
219 words
A method for determining the temperature of a combustion flame of known composition comprising: a. supporting a thin wire at a preselected position within said flame, said wire selected to rapidly couple energy to the immediately surrounding gases of said flame when said wire is heated; b. directing a first pulsed laser beam onto said wire to produce localized heating of said wire and the immediately surrounding gases of said flame whereby a pressure increase in the form of an acoustic pulse is generated within said flame; c. directing parallel second and third laser beams through said flame in predetermined spaced relationship to each other and to said wire; d. detecting the respective deflections of said second and third laser beams resulting from interactions thereof with said acoustic pulse; e. measuring the time difference between respective said deflections of said second and third laser beams to determine the speed of said acoustic pulse between said second and third laser beams; f. performing the foregoing steps a through e in air at ambient conditions with said flame removed; g. comparing the measurements taken in the presence of said flame with the measurements taken in ambient air; and h. determining the temperature of said flame from said speed determinations and said predetermined spaced relationship between said second and third laser beams.
Claim 13
Independent Claim
219 words
A method for determining the temperature of a combustion flame of known composition comprising: a. supporting a thin wire at a preselected position within said flame, said wire selected to rapidly couple energy to the immediately surrounding gases of said flame when said wire is heated; b. directing a first pulsed laser beam onto said wire to produce localized heating of said wire and the immediately surrounding gases of said flame whereby a pressure increase in the form of an acoustic pulse is generated within said flame; c. directing parallel second and third laser beams through said flame in predetermined spaced relationship to each other and to said wire; d. detecting the respective deflections of said second and third laser beams resulting from interactions thereof with said acoustic pulse; e. measuring the time difference between respective said deflections of said second and third laser beams to determine the speed of said acoustic pulse between said second and third laser beams; f. performing the foregoing steps a through e in air at ambient conditions with said flame removed; g. comparing the measurements taken in the presence of said flame with the measurements taken in ambient air; and h. determining the temperature of said flame from said speed determinations and said predetermined spaced relationship between said second and third laser beams.
Claim 14
Dependent Claim
21 words
The method as recited in claim 10 wherein said first laser beam is produced by a low power pulsed Nd:YAG laser.
Claim 15
Dependent Claim
19 words
The method as recited in claim 10 wherein said second and third laser beams are produced by HeNe lasers.
Claim 16
Dependent Claim
31 words
The method as recited in claim 10 wherein said wire comprises a material selected from the group consisting of tungsten, titanium, aluminum titanium alloy, nickel, stainless steel, copper, brass, and aluminum.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
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| 3.5 Years (Year 4) | 1990-04-06 | 1990-10-06 | 1991-04-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-04-06 | 1994-10-06 | 1995-04-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-04-06 | 1998-10-06 | 1999-04-07 | $7700.00 | Window Closed / Lapsed |