Patent US4722180A successfully refreshed from Google Patents.
US4722180A
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Method and means for enhancing recovery of a surge condition in a gas turbine engine
Assignee: RTX Corp
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Filing: 1986-11-20
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Granted: 1988-02-02
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Expires: 2006-11-20
Abstract
Abstract A system (38) and method for directing control actions to recover from the occurrence of a surge condition within a turbocompressor includes a high/low engine power output discriminator (40). Control action is taken by the system (38) in response to both the detection of a surge condition and the current engine power output level. The system (38) selects among a plurality of corrective control actions (56, 62, 68) to best achieve a return to normal engine operation.
Inventors
- 👤 Anita S. Lindler
- 👤 James B. Kelly
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 23:55
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/48; F02C9/26; F02C9/28; F05; F05D; F05D2270/00; F05D2270/01; F05D2270/10; F05D2270/101
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
115 words
A method for recovering from an occurrence of a surge condition in a gas turbine engine operating within a power output range and including a plurality of variable position compressor vanes, comprising the steps of (a) detecting the occurrence of the surge condition; (b) determining a current power output level within the power output range, including the steps of monitoring the current position of the compressor vanes, and determining the current engine power output level from the current position of the compressor vanes; (c) correctively controlling the gas turbine engine, responsive to both the detected surge condition and the current engine power output level, for restoring the gas turbine engine to a normal operating condition.
Claim 2
Independent Claim
115 words
A method for recovering from an occurrence of a surge condition in a gas turbine engine operating within a power output range and including a plurality of variable position compressor vanes, comprising the steps of (a) detecting the occurrence of the surge condition; (b) determining a current power output level within the power output range, including the steps of monitoring the current position of the compressor vanes, and determining the current engine power output level from the current position of the compressor vanes; (c) correctively controlling the gas turbine engine, responsive to both the detected surge condition and the current engine power output level, for restoring the gas turbine engine to a normal operating condition.
Claim 3
Independent Claim
107 words
A method for recovering from an occurrence of a surge condition within a gas turbine engine operating within a power output range and including a thrust augmentor having a controllable flow of augmentor flow and a variable area exhaust nozzle, comprising the steps of: (a) detecting the occurrence of the surge condition; (b) determining a current engine power output level within the power output range, including the step of monitoring the augmentor fuel flow; and (c) correctively controlling the gas turbine engine, responsive to both the detected surge condition and the current engine power output level, for restoring the gas turbine engine to a normal operating condition.
Claim 4
Independent Claim
107 words
A method for recovering from an occurrence of a surge condition within a gas turbine engine operating within a power output range and including a thrust augmentor having a controllable flow of augmentor flow and a variable area exhaust nozzle, comprising the steps of: (a) detecting the occurrence of the surge condition; (b) determining a current engine power output level within the power output range, including the step of monitoring the augmentor fuel flow; and (c) correctively controlling the gas turbine engine, responsive to both the detected surge condition and the current engine power output level, for restoring the gas turbine engine to a normal operating condition.
Claim 5
Dependent Claim
33 words
The method for recovering from a surge condition as recited in claim 1, wherein the engine power output level is determined to be either a low power level or a high power level.
Claim 6
Dependent Claim
59 words
The method for recovering from a surge condition as recited in claim 3, wherein the gas turbine engine receives a controllable flow of fuel, and wherein step (c) further includes the step of reducing the rate of flow of engine fuel responsive to both the detected surge condition and the determined engine power level being a low power level.
Claim 7
Dependent Claim
90 words
The method for recovering from a surge condition as recited in claim 1, wherein step (c) further comprises the steps of delaying correctively controlling the gas turbine engine for a preset period of time in response to the detected surge condition and a monitored augmentor fuel flow other than zero; subsequent to the expiration of the preset period of time, determining if the surge condition is still occurring within the gas turbine engine, and shutting off the flow of augmentor fuel following a determination of a continued surge condition occurrence.
Claim 8
Dependent Claim
46 words
The method for recovery from a surge condition as recited in claim 4, wherein the gas turbine engine includes a thrust augmentor having a controllable flow of augmentor fuel and a variable area exhaust nozzle, and wherein step (b) further includes monitoring the augmentor fuel flow.
Claim 9
Dependent Claim
90 words
The method for recovering from a surge condition as recited in claim 6, wherein step (c) further comprises the steps of delaying correctively controlling the gas turbine engine for a preset period of time in response to the detected surge condition and a monitored augmentor fuel flow other than 0; subsequent to the expiration of the preset period of time, determining if the surge condition is still occurring within the gas turbine engine, and shutting off the flow of augmentor fuel following a determination of a continued surge condition occurrence.
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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) | 1991-02-01 | 1991-08-03 | 1992-02-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-02-01 | 1995-08-03 | 1996-02-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-02-01 | 1999-08-03 | 2000-02-02 | $7700.00 | Window Closed / Lapsed |