Patent US4137710A successfully refreshed from Google Patents.
US4137710A
Expired / Lapsed
US
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Surge detector for gas turbine engines
Assignee: RTX Corp
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Filing: 1977-01-26
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Granted: 1979-02-06
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Expires: 1997-01-26
Abstract
Abstract Sensed engine inlet temperature is utilized to detect compressor surge whenever its computed temperature rate of change or rise signal exceeds a predetermined value. This signal may be coupled to another engine operating parameter, such as rotor speed, compressor discharge pressure and the like and permutations thereof, to guard against false detection. Engine inlet temperature rate of change or rise is an efficacious surge detection parameter particularly when an afterburner is used inasmuch as the hot gases of the afterburner will have a significant influence on the engine inlet temperature sensor in a reverse flow situation making that signal a positive indication of imminent surge.
Inventors
- 👤 Edmond Preti
- 👤 Howard W. Ripy
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 14:43
CPC Classifications
F; F04; F04D; F04D27/00; F04D27/02
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
116 words
In combination, a turbine type power plant having a compressor, an engine inlet leading air into said compressor and an augmentor, means for detecting surge when it is initiated in said compressor when said augmentor is in the operating condition occasioned by the normally rearward flowing of exhaust gases reversing itself and flowing through the engine and heating the engine inlet air, said means including a sensor disposed in said inlet for measuring the temperature of the air therein, and calculating means for producing an output signal as a function of the rate of change of said measured temperature when it exceeds a predetermined value, whereby said output signal is indicative of surge in said compressor.
Claim 2
Dependent Claim
116 words
In combination, a turbine type power plant having a compressor, an engine inlet leading air into said compressor and an augmentor, means for detecting surge when it is initiated in said compressor when said augmentor is in the operating condition occasioned by the normally rearward flowing of exhaust gases reversing itself and flowing through the engine and heating the engine inlet air, said means including a sensor disposed in said inlet for measuring the temperature of the air therein, and calculating means for producing an output signal as a function of the rate of change of said measured temperature when it exceeds a predetermined value, whereby said output signal is indicative of surge in said compressor.
Claim 3
Dependent Claim
65 words
In combination as claimed in claim 1 including additional means for sensing an engine operating variable, computer means for calculating the rate of change of said engine operating variable and means for producing a surge detected signal when both the measured temperature rate of change or rise reaches a predetermined value and the rate of change of said engine operating variable reaches a predetermined value.
Claim 4
Dependent Claim
17 words
In combination as in claim 2 wherein said engine operating variable is rotor speed of said compressor.
Claim 5
Dependent Claim
97 words
A surge detection system for a gas turbine engine having a compressor and an engine inlet for leading air into said compressor, an augmentor normally issuing exhaust gases rearwardly, the surge detection system consisting essentially of means for measuring the temperature rate of change of the air in said inlet and means responsive to said temperature rate of change measuring means for producing a surge detected signal solely when said temperature rate of change exceeds a predetermined value when the direction of flow of the exhaust gases of said augmentor reverse itself and flashback through the engine.
Claim 6
Dependent Claim
97 words
A surge detection system for a gas turbine engine having a compressor and an engine inlet for leading air into said compressor, an augmentor normally issuing exhaust gases rearwardly, the surge detection system consisting essentially of means for measuring the temperature rate of change of the air in said inlet and means responsive to said temperature rate of change measuring means for producing a surge detected signal solely when said temperature rate of change exceeds a predetermined value when the direction of flow of the exhaust gases of said augmentor reverse itself and flashback through the engine.
Claim 7
Dependent Claim
102 words
A surge detection system for a gas turbine engine having an augmentor which has the propensity of forcing air rearwardly with respect to the normal forwardly axial flow of the engines working fluid, said engine including a compressor and an engine inlet for leading said working fluid into said compressor, a temperature sensor disposed in said inlet ahead of said compressor, means responsive to the temperature rate of change produced by said sensor resulting from the working medium flowing in a reverse direction occasioned by said augmentor for producing a surge signal when the temperature rate of change exceeds a predetermined value.
Claim 8
Dependent Claim
102 words
A surge detection system for a gas turbine engine having an augmentor which has the propensity of forcing air rearwardly with respect to the normal forwardly axial flow of the engines working fluid, said engine including a compressor and an engine inlet for leading said working fluid into said compressor, a temperature sensor disposed in said inlet ahead of said compressor, means responsive to the temperature rate of change produced by said sensor resulting from the working medium flowing in a reverse direction occasioned by said augmentor for producing a surge signal when the temperature rate of change exceeds a predetermined value.
Claim 9
Dependent Claim
131 words
A surge detector for a gas turbine engine having a compressor, an inlet for leading air into said compressor, and an augmentor a temperature sensor disposed in said inlet for sensing the temperature of the air in said inlet during augmentor operation, a speed sensor for measuring the rotor speed of said compressor, means responsive to said temperature sensor for producing a first signal upon said temperature rate of change exceeds a predetermined value, means responsive to said speed sensor for producing a second signal when the rate of change of the rotor speed exceeds a predetermined value, and means responsive to both said first signal and said second signal for producing a third signal indicative of surge solely when both said first signal and said second signal exceed predetermined values.
Claim 10
Dependent Claim
131 words
A surge detector for a gas turbine engine having a compressor, an inlet for leading air into said compressor, and an augmentor a temperature sensor disposed in said inlet for sensing the temperature of the air in said inlet during augmentor operation, a speed sensor for measuring the rotor speed of said compressor, means responsive to said temperature sensor for producing a first signal upon said temperature rate of change exceeds a predetermined value, means responsive to said speed sensor for producing a second signal when the rate of change of the rotor speed exceeds a predetermined value, and means responsive to both said first signal and said second signal for producing a third signal indicative of surge solely when both said first signal and said second signal exceed predetermined values.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-02-05 | 1982-08-07 | 1983-02-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-02-05 | 1986-08-07 | 1987-02-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-02-05 | 1990-08-07 | 1991-02-06 | $7700.00 | Window Closed / Lapsed |