Patent US4060979A successfully refreshed from Google Patents.
US4060979A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Stall warning detector for gas turbine engine
Assignee: RTX Corp
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Filing: 1975-11-19
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Granted: 1977-12-06
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Expires: 1995-11-19
Abstract
Abstract A stall detector for a gas turbine engine is disclosed where detection is obtained by continuously monitoring turbine temperature and either compressor speed or bleed valve position and provide a stall signal solely when turbine temperature exceeds a predetermined value and the compressor speed decreases at a predetermined rate or when turbine temperature exceeds a predetermined value at the time that the compressor bleeds are in the opened position.
Inventors
- 👤 Fred L. Elsaesser
- 👤 Joseph H. Hall
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 15:50
CPC Classifications
F; F02; F02C; F02C7/00
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
127 words
A stall detector system for an axial flow gas turbine engine having a compressor, turbine and burner, bleed valve means for bleeding air from said compressor, means for detecting when stall is imminent including a temperature sensor measuring the temperature of the turbine, comparator means for producing a first signal whenever the measured temperature exceeds a referenced value, signal generator means responsive to the position of said bleed valve means for producing a second signal whenever the bleed valve means is open to bleed said compressor, and gate means responsive to both said first signal and said second signal for producing a stall warning output signal whenever both the temperature of said turbine is abnormally high and said bleed valve means is bleeding air from said compressor.
Claim 2
Dependent Claim
127 words
A stall detector system for an axial flow gas turbine engine having a compressor, turbine and burner, bleed valve means for bleeding air from said compressor, means for detecting when stall is imminent including a temperature sensor measuring the temperature of the turbine, comparator means for producing a first signal whenever the measured temperature exceeds a referenced value, signal generator means responsive to the position of said bleed valve means for producing a second signal whenever the bleed valve means is open to bleed said compressor, and gate means responsive to both said first signal and said second signal for producing a stall warning output signal whenever both the temperature of said turbine is abnormally high and said bleed valve means is bleeding air from said compressor.
Claim 3
Dependent Claim
17 words
A stall indicator as claimed in claim 1 wherein said temperature sensor senses the turbine inlet temperature.
Claim 4
Dependent Claim
17 words
A stall indicator as claimed in claim 1 wherein said temperature sensor senses the turbine exit temperature.
Claim 5
Independent Claim
112 words
The method of detecting stall in flow gas turbine engine that includes a compressor, turbine and burner and compressor bleed valves comprising the steps of: measuring the temperature in proximity to the turbine so as to produce an output signal whenever this temperature is excessive in relation to normal engine operation, measuring the position of the compressor bleed valves so as to produce an output signal whenever the compressor bleed valves are opened, combining the outputs obtained in the steps of measuring so as to produce a signal indicative of stall solely when both output signals are present which signal can then be used as a warning or to initiate corrective action.
Claim 6
Independent Claim
112 words
The method of detecting stall in flow gas turbine engine that includes a compressor, turbine and burner and compressor bleed valves comprising the steps of: measuring the temperature in proximity to the turbine so as to produce an output signal whenever this temperature is excessive in relation to normal engine operation, measuring the position of the compressor bleed valves so as to produce an output signal whenever the compressor bleed valves are opened, combining the outputs obtained in the steps of measuring so as to produce a signal indicative of stall solely when both output signals are present which signal can then be used as a warning or to initiate corrective action.
Claim 7
Dependent Claim
35 words
The method as claimed in claim 4 including the step of holding the output signal obtained in the step of combining for a predetermined time interval so as not to release this output signal prematurely.
Claim 8
Dependent Claim
32 words
A stall indicator as claimed in claim 1 including time delay means responsive to the stall warning output signal to hold and release said stall warning signal a predetermined interval of time.
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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) | 1980-12-05 | 1981-06-06 | 1981-12-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-12-05 | 1985-06-06 | 1985-12-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-12-05 | 1989-06-06 | 1989-12-06 | $7700.00 | Window Closed / Lapsed |