US4304093A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Variable clearance control for a gas turbine engine
Assignee: General Electric Co
•
Filing: 1979-08-31
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Granted: 1981-12-08
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Expires: 1999-08-31
Abstract
Abstract Clearance control between an outer air seal of a gas turbine engine and an internal, turbine section of the engine is controlled by selectively modulating a cooling air supply that is directed to selected portions of the air seal supporting structure to control its thermal growth. Impingement of the cooling air causes contraction of the seal structure, thereby lessening the clearance for the purpose of improving engine performance. The flow of cooling air is modulated in response to engine speed and engine altitude to maintain relatively low clearance during critical periods of engine operation.
Inventors
- 👤 Wallace M. Schulze
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 04:08
CPC Classifications
F; F01; F01D; F01D11/00; F01D11/08; F01D11/14; F01D11/20; F01D11/24; F01D25/00; F01D25/08; F01D25/12; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
195 words
In a gas turbine engine having an engine case and a rotating machinery section rotatably supported therein, seal means circumferentially surrounding the rotating machinery section and attached to said engine case, and a clearance control comprising means for directing cooling air on said engine case for cooling thereof, thereby controlling clearance between said rotating machinery and said seal means, an improvement comprising: cooling air control means for varying the amount of cooling air directed on said engine case, said cooling air control means comprising a bypass line in flow communication with a case cooling line for directing a portion of said cooling air from said case cooling line for the purpose of varying the amount of air provided to said clearance control, said bypass line being provided with a bypass line valve that is opened during appropriate engine operations to allow cooling airflow to enter said bypass line, said bypass line valve being controlled by fluid pressure; a pressurized fire extinguishing source incorporated into said engine; and a pressure line connecting said pressurized fire extinguishing source to said bypass line valve for the purpose of closing said bypass line during release of fire extinguishing material.
Claim 2
Dependent Claim
195 words
In a gas turbine engine having an engine case and a rotating machinery section rotatably supported therein, seal means circumferentially surrounding the rotating machinery section and attached to said engine case, and a clearance control comprising means for directing cooling air on said engine case for cooling thereof, thereby controlling clearance between said rotating machinery and said seal means, an improvement comprising: cooling air control means for varying the amount of cooling air directed on said engine case, said cooling air control means comprising a bypass line in flow communication with a case cooling line for directing a portion of said cooling air from said case cooling line for the purpose of varying the amount of air provided to said clearance control, said bypass line being provided with a bypass line valve that is opened during appropriate engine operations to allow cooling airflow to enter said bypass line, said bypass line valve being controlled by fluid pressure; a pressurized fire extinguishing source incorporated into said engine; and a pressure line connecting said pressurized fire extinguishing source to said bypass line valve for the purpose of closing said bypass line during release of fire extinguishing material.
Claim 3
Dependent Claim
38 words
The apparatus recited in claim 1, and further comprising: a case cooling line valve provided in said case cooling line, downstream of said bypass line, for the purpose of directly controlling cooling airflow through said case cooling line.
Claim 4
Dependent Claim
34 words
The apparatus recited in claim 2, wherein said case cooling line valve is responsive to engine speed for the purpose of essentially eliminating cooling airflow to said clearance control below a predetermined engine speed.
Claim 5
Dependent Claim
75 words
The apparatus recited in claim 3 and further comprising: an air line that supplies compressed air to said case cooling line valve for the purpose of controlling the opening of the case cooling line valve; and an engine speed responsive control valve that is controlled by an engine speed responsive apparatus for turning on and off the compressed air in said air line thereby controlling the opening and closing of said case cooling line valve.
Claim 6
Dependent Claim
54 words
The apparatus recited in claim 4 wherein said engine speed responsive control valve is linked to a mechanical variable stator actuation system on a compressor section of the engine and wherein said variable stator actuation system changes condition in response to engine speed, thereby controlling opening and closing of said engine speed responsive valve.
Claim 7
Independent Claim
31 words
The apparatus recited in claims 1, 2, or 5 wherein said bypass line valve is responsive to barometric pressure for the purpose of closing said bypass line valve below a predeter
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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) | 1984-12-07 | 1985-06-08 | 1985-12-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-12-07 | 1989-06-08 | 1989-12-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-12-07 | 1993-06-08 | 1993-12-08 | $7700.00 | Window Closed / Lapsed |