DE69107988D1 - Gasturbine mit modulierter Kühlluft. - Google Patents
Gasturbine mit modulierter Kühlluft.Info
- Publication number
- DE69107988D1 DE69107988D1 DE69107988T DE69107988T DE69107988D1 DE 69107988 D1 DE69107988 D1 DE 69107988D1 DE 69107988 T DE69107988 T DE 69107988T DE 69107988 T DE69107988 T DE 69107988T DE 69107988 D1 DE69107988 D1 DE 69107988D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- cooling air
- modulated cooling
- modulated
- turbine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/02—Arrangement of sensing elements
- F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
- F01D17/085—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure to temperature
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/634,905 US5157914A (en) | 1990-12-27 | 1990-12-27 | Modulated gas turbine cooling air |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69107988D1 true DE69107988D1 (de) | 1995-04-13 |
DE69107988T2 DE69107988T2 (de) | 1995-11-02 |
Family
ID=24545631
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69107988T Expired - Fee Related DE69107988T2 (de) | 1990-12-27 | 1991-12-24 | Gasturbine mit modulierter Kühlluft. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5157914A (de) |
EP (1) | EP0493111B1 (de) |
JP (1) | JP3100723B2 (de) |
DE (1) | DE69107988T2 (de) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5232339A (en) * | 1992-01-28 | 1993-08-03 | General Electric Company | Finned structural disk spacer arm |
US5217348A (en) * | 1992-09-24 | 1993-06-08 | United Technologies Corporation | Turbine vane assembly with integrally cast cooling fluid nozzle |
DE69606392T2 (de) * | 1995-03-15 | 2000-09-07 | United Technologies Corp., Hartford | Abriebfeste lagerung eines dichtringes in einer gasturbine |
US6032457A (en) * | 1996-06-27 | 2000-03-07 | United Technologies Corporation | Fuel nozzle guide |
GB2319307B (en) * | 1996-11-12 | 2000-11-08 | Rolls Royce Plc | Gas turbine engine cooling air flow control |
DE19931765A1 (de) * | 1999-07-08 | 2001-01-11 | Rolls Royce Deutschland | Zweistufige oder mehrstufige Axialturbine einer Gasturbine |
US6431824B2 (en) * | 1999-10-01 | 2002-08-13 | General Electric Company | Turbine nozzle stage having thermocouple guide tube |
US6546735B1 (en) * | 2001-03-07 | 2003-04-15 | General Electric Company | Methods and apparatus for operating turbine engines using rotor temperature sensors |
US6832891B2 (en) | 2001-10-29 | 2004-12-21 | Man Turbomaschinen Ag | Device for sealing turbomachines |
EP1696102B1 (de) * | 2005-02-28 | 2015-07-29 | Siemens Aktiengesellschaft | Verfahren zur Betriebsüberwachung einer Gasturbine und Gasturbine |
US7230205B2 (en) * | 2005-03-29 | 2007-06-12 | Siemens Power Generation, Inc. | Compressor airfoil surface wetting and icing detection system |
US7914254B2 (en) * | 2007-02-13 | 2011-03-29 | General Electric Company | Integrated support/thermocouple housing for impingement cooling manifolds and cooling method |
US8474268B2 (en) * | 2007-08-16 | 2013-07-02 | General Electric Company | Method of mitigating undesired gas turbine transient response using event based actions |
DE102008014743A1 (de) * | 2008-03-18 | 2009-09-24 | Rolls-Royce Deutschland Ltd & Co Kg | Verdichterstator mit Teildeckband |
US8221057B2 (en) * | 2008-06-25 | 2012-07-17 | General Electric Company | Method, system and controller for establishing a wheel space temperature alarm in a turbomachine |
JP5185859B2 (ja) * | 2009-02-26 | 2013-04-17 | 三菱重工業株式会社 | 温度検出装置、タービン静翼、および、ガスタービン |
IT1399156B1 (it) * | 2009-12-19 | 2013-04-11 | Nuovo Pignone Spa | Metodo e sistema di raffreddamento per specifici componenti di una turbina a gas e relativa turbina. |
JP5818717B2 (ja) | 2012-02-27 | 2015-11-18 | 三菱日立パワーシステムズ株式会社 | ガスタービン |
US9540940B2 (en) * | 2012-03-12 | 2017-01-10 | General Electric Company | Turbine interstage seal system |
US9028205B2 (en) * | 2012-06-13 | 2015-05-12 | United Technologies Corporation | Variable blade outer air seal |
US10094389B2 (en) * | 2012-12-29 | 2018-10-09 | United Technologies Corporation | Flow diverter to redirect secondary flow |
JP6392310B2 (ja) | 2013-03-15 | 2018-09-19 | ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation | 計器移送用支柱 |
JP6320063B2 (ja) | 2014-02-03 | 2018-05-09 | 三菱日立パワーシステムズ株式会社 | ガスタービン、ガスタービンの制御装置、ガスタービンの冷却方法 |
RU2712560C2 (ru) * | 2014-10-15 | 2020-01-29 | Сафран Серамикс | Ротационный узел для турбинного двигателя, содержащего самоподдерживающийся кожух ротора |
US10337345B2 (en) | 2015-02-20 | 2019-07-02 | General Electric Company | Bucket mounted multi-stage turbine interstage seal and method of assembly |
DE102015226732A1 (de) * | 2015-12-24 | 2017-06-29 | Rolls-Royce Deutschland Ltd & Co Kg | Sensoranordnung und Messverfahren für eine Turbomaschine |
ITUB20160240A1 (it) * | 2016-01-20 | 2017-07-20 | Turboden Srl | Metodo e dispositivo per ridurre le perdite di trafilamento in una turbina |
DE102017205573A1 (de) | 2017-03-31 | 2018-10-04 | Rolls-Royce Deutschland Ltd & Co Kg | Messvorrichtung und Messverfahren für eine Strömung |
JP6252819B1 (ja) * | 2017-09-26 | 2017-12-27 | 三菱日立パワーシステムズ株式会社 | 制御装置、ガスタービン、制御方法及びプログラム |
JP7129810B2 (ja) * | 2018-04-13 | 2022-09-02 | 三菱重工業株式会社 | 冷却空気調整弁の弁開度決定装置、ディスクキャビティ目標温度決定装置、およびディスクキャビティ温度制御装置 |
US11255267B2 (en) * | 2018-10-31 | 2022-02-22 | Raytheon Technologies Corporation | Method of cooling a gas turbine and apparatus |
US10961857B2 (en) * | 2018-12-21 | 2021-03-30 | Rolls-Royce Plc | Turbine section of a gas turbine engine with ceramic matrix composite vanes |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2896906A (en) * | 1956-03-26 | 1959-07-28 | William J Durkin | Turbine cooling air metering system |
US2971997A (en) * | 1958-03-06 | 1961-02-14 | Gen Motors Corp | Sampling thermocouple |
GB1348127A (en) * | 1971-04-19 | 1974-03-13 | Secr Defence | Gas turbine engine |
US4213738A (en) * | 1978-02-21 | 1980-07-22 | General Motors Corporation | Cooling air control valve |
US4217755A (en) * | 1978-12-04 | 1980-08-19 | General Motors Corporation | Cooling air control valve |
US4332133A (en) * | 1979-11-14 | 1982-06-01 | United Technologies Corporation | Compressor bleed system for cooling and clearance control |
US4487016A (en) * | 1980-10-01 | 1984-12-11 | United Technologies Corporation | Modulated clearance control for an axial flow rotary machine |
US4416111A (en) * | 1981-02-25 | 1983-11-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Air modulation apparatus |
GB2170865A (en) * | 1985-02-08 | 1986-08-13 | Rolls Royce | Gas turbine engine with cooling device |
US4815928A (en) * | 1985-05-06 | 1989-03-28 | General Electric Company | Blade cooling |
US4815272A (en) * | 1987-05-05 | 1989-03-28 | United Technologies Corporation | Turbine cooling and thermal control |
US4893983A (en) * | 1988-04-07 | 1990-01-16 | General Electric Company | Clearance control system |
US4869640A (en) * | 1988-09-16 | 1989-09-26 | United Technologies Corporation | Controlled temperature rotating seal |
US5022817A (en) * | 1989-09-12 | 1991-06-11 | Allied-Signal Inc. | Thermostatic control of turbine cooling air |
-
1990
- 1990-12-27 US US07/634,905 patent/US5157914A/en not_active Expired - Lifetime
-
1991
- 1991-12-24 DE DE69107988T patent/DE69107988T2/de not_active Expired - Fee Related
- 1991-12-24 EP EP91312012A patent/EP0493111B1/de not_active Expired - Lifetime
- 1991-12-27 JP JP03360068A patent/JP3100723B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP3100723B2 (ja) | 2000-10-23 |
DE69107988T2 (de) | 1995-11-02 |
US5157914A (en) | 1992-10-27 |
EP0493111A1 (de) | 1992-07-01 |
JPH04292530A (ja) | 1992-10-16 |
EP0493111B1 (de) | 1995-03-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |