DE60119753D1 - Druckluftdampferzeuger zur kühlung eines gasturbinenüberströmkanals - Google Patents
Druckluftdampferzeuger zur kühlung eines gasturbinenüberströmkanalsInfo
- Publication number
- DE60119753D1 DE60119753D1 DE60119753T DE60119753T DE60119753D1 DE 60119753 D1 DE60119753 D1 DE 60119753D1 DE 60119753 T DE60119753 T DE 60119753T DE 60119753 T DE60119753 T DE 60119753T DE 60119753 D1 DE60119753 D1 DE 60119753D1
- Authority
- DE
- Germany
- Prior art keywords
- cooling
- gas turbine
- steam generator
- transfer channel
- air steam
- 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 - Lifetime
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000004326 stimulated echo acquisition mode for imaging Methods 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
- F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US677043 | 2000-09-29 | ||
US09/677,043 US6298656B1 (en) | 2000-09-29 | 2000-09-29 | Compressed air steam generator for cooling combustion turbine transition section |
PCT/US2001/042331 WO2002027167A2 (en) | 2000-09-29 | 2001-09-27 | Compressed air steam generator for use in cooling a combustion turbine transition section |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60119753D1 true DE60119753D1 (de) | 2006-06-22 |
DE60119753T2 DE60119753T2 (de) | 2006-11-30 |
Family
ID=24717070
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60119753T Expired - Lifetime DE60119753T2 (de) | 2000-09-29 | 2001-09-27 | Druckluftdampferzeuger zur kühlung eines gasturbinenüberströmkanals |
Country Status (6)
Country | Link |
---|---|
US (1) | US6298656B1 (de) |
EP (1) | EP1320664B1 (de) |
JP (1) | JP3974519B2 (de) |
KR (1) | KR100598447B1 (de) |
DE (1) | DE60119753T2 (de) |
WO (1) | WO2002027167A2 (de) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6412285B1 (en) * | 2001-06-20 | 2002-07-02 | General Electric Company | Cooling air system and method for combined cycle power plants |
US6412270B1 (en) * | 2001-09-12 | 2002-07-02 | General Electric Company | Apparatus and methods for flowing a cooling or purge medium in a turbine downstream of a turbine seal |
JP2005516125A (ja) * | 2002-01-29 | 2005-06-02 | ザウラー ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | 溶融紡糸されたフィラメントを冷却する方法および溶融紡糸するための装置 |
US7093446B2 (en) * | 2004-09-15 | 2006-08-22 | General Electric Company | Gas turbine engine having improved core system |
US7096674B2 (en) * | 2004-09-15 | 2006-08-29 | General Electric Company | High thrust gas turbine engine with improved core system |
US7310938B2 (en) * | 2004-12-16 | 2007-12-25 | Siemens Power Generation, Inc. | Cooled gas turbine transition duct |
US8015818B2 (en) * | 2005-02-22 | 2011-09-13 | Siemens Energy, Inc. | Cooled transition duct for a gas turbine engine |
US8524734B2 (en) | 2005-05-18 | 2013-09-03 | Mpex Pharmaceuticals, Inc. | Aerosolized fluoroquinolones and uses thereof |
US7581401B2 (en) * | 2005-09-15 | 2009-09-01 | General Electric Company | Methods and apparatus for cooling gas turbine engine components |
ES2809177T3 (es) | 2008-10-07 | 2021-03-03 | Horizon Orphan Llc | Inhalación de levofloxacino para reducir la inflamación pulmonar |
JP2012505223A (ja) | 2008-10-07 | 2012-03-01 | エムペックス・ファーマシューティカルズ・インコーポレーテッド | 薬物動態の改善のためのエアゾールフルオロキノロン配合物 |
US8549861B2 (en) * | 2009-01-07 | 2013-10-08 | General Electric Company | Method and apparatus to enhance transition duct cooling in a gas turbine engine |
CA2773033C (en) | 2009-09-04 | 2016-10-11 | Mpex Pharmaceuticals, Inc. | Use of aerosolized levofloxacin for treating cystic fibrosis |
GB2484254A (en) * | 2010-08-04 | 2012-04-11 | Combined Cycle Enhancements Ltd | Gas turbine apparatus with energy recovery heat exchange system |
US8943838B2 (en) * | 2011-08-24 | 2015-02-03 | General Electric Company | Integrated turbomachine plant |
US9086019B2 (en) | 2012-07-02 | 2015-07-21 | United Technologies Corporation | Turbomachine thermal energy exchange |
EP2957746B1 (de) * | 2014-06-17 | 2021-04-28 | Raytheon Technologies Corporation | Hochdruckturbinenkühlung |
US10520193B2 (en) | 2015-10-28 | 2019-12-31 | General Electric Company | Cooling patch for hot gas path components |
US10830442B2 (en) | 2016-03-25 | 2020-11-10 | General Electric Company | Segmented annular combustion system with dual fuel capability |
US10563869B2 (en) | 2016-03-25 | 2020-02-18 | General Electric Company | Operation and turndown of a segmented annular combustion system |
US10584880B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Mounting of integrated combustor nozzles in a segmented annular combustion system |
US10641176B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Combustion system with panel fuel injector |
US10641491B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Cooling of integrated combustor nozzle of segmented annular combustion system |
US10605459B2 (en) | 2016-03-25 | 2020-03-31 | General Electric Company | Integrated combustor nozzle for a segmented annular combustion system |
US11428413B2 (en) | 2016-03-25 | 2022-08-30 | General Electric Company | Fuel injection module for segmented annular combustion system |
US10584876B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system |
US10520194B2 (en) | 2016-03-25 | 2019-12-31 | General Electric Company | Radially stacked fuel injection module for a segmented annular combustion system |
US10690350B2 (en) | 2016-11-28 | 2020-06-23 | General Electric Company | Combustor with axially staged fuel injection |
US11156362B2 (en) | 2016-11-28 | 2021-10-26 | General Electric Company | Combustor with axially staged fuel injection |
US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
US11994293B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus support structure and method of manufacture |
US11371702B2 (en) | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
US11994292B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus for turbomachine |
US11614233B2 (en) | 2020-08-31 | 2023-03-28 | General Electric Company | Impingement panel support structure and method of manufacture |
US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3795816A (en) * | 1972-05-09 | 1974-03-05 | Sulzer Ag | Apparatus to prevent overspeeding of a combination including a supercharged steam generator, a gas turbine and a compressor |
US4680927A (en) | 1979-07-23 | 1987-07-21 | International Power Technology, Inc. | Control system for Cheng dual-fluid cycle engine system |
JPS575520A (en) | 1980-06-11 | 1982-01-12 | Mitsubishi Gas Chem Co Inc | Method for recovering heat |
US4509324A (en) * | 1983-05-09 | 1985-04-09 | Urbach Herman B | Direct open loop Rankine engine system and method of operating same |
JPH0643811B2 (ja) | 1985-07-29 | 1994-06-08 | 株式会社日立製作所 | ガスタービンのホットパーツ冷却方法 |
US4765142A (en) * | 1987-05-12 | 1988-08-23 | Gibbs & Hill, Inc. | Compressed air energy storage turbomachinery cycle with compression heat recovery, storage, steam generation and utilization during power generation |
EP0474893B1 (de) | 1990-09-10 | 1994-11-23 | Asea Brown Boveri Ag | Gasturbinenanordnung |
US5357741A (en) | 1992-05-01 | 1994-10-25 | Dresser-Rand Company | NOx and CO control for gas turbine |
US5617719A (en) | 1992-10-27 | 1997-04-08 | Ginter; J. Lyell | Vapor-air steam engine |
US5329758A (en) | 1993-05-21 | 1994-07-19 | The United States Of America As Represented By The Secretary Of The Navy | Steam-augmented gas turbine |
US5564269A (en) | 1994-04-08 | 1996-10-15 | Westinghouse Electric Corporation | Steam injected gas turbine system with topping steam turbine |
US5640840A (en) | 1994-12-12 | 1997-06-24 | Westinghouse Electric Corporation | Recuperative steam cooled gas turbine method and apparatus |
DE19508018A1 (de) | 1995-03-07 | 1996-09-12 | Abb Management Ag | Verfahren zum Betrieb einer Kraftwerksanlage |
US5697208A (en) | 1995-06-02 | 1997-12-16 | Solar Turbines Incorporated | Turbine cooling cycle |
US5724806A (en) | 1995-09-11 | 1998-03-10 | General Electric Company | Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine |
US5826430A (en) * | 1996-04-23 | 1998-10-27 | Westinghouse Electric Corporation | Fuel heating system used in conjunction with steam cooled combustors and transitions |
JP3276289B2 (ja) * | 1996-05-13 | 2002-04-22 | 三菱重工業株式会社 | ガスタービン燃焼器 |
JP3500020B2 (ja) * | 1996-11-29 | 2004-02-23 | 三菱重工業株式会社 | 蒸気冷却ガスタービンシステム |
DE19654472A1 (de) * | 1996-12-27 | 1998-07-02 | Asea Brown Boveri | Verfahren zur Kühlung von thermisch hochbelasteten Aggregaten einer Gasturbogruppe |
-
2000
- 2000-09-29 US US09/677,043 patent/US6298656B1/en not_active Expired - Lifetime
-
2001
- 2001-09-27 EP EP01977827A patent/EP1320664B1/de not_active Expired - Lifetime
- 2001-09-27 WO PCT/US2001/042331 patent/WO2002027167A2/en active IP Right Grant
- 2001-09-27 JP JP2002530512A patent/JP3974519B2/ja not_active Expired - Fee Related
- 2001-09-27 KR KR1020037004424A patent/KR100598447B1/ko active IP Right Grant
- 2001-09-27 DE DE60119753T patent/DE60119753T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US6298656B1 (en) | 2001-10-09 |
WO2002027167A2 (en) | 2002-04-04 |
WO2002027167A3 (en) | 2002-09-26 |
JP3974519B2 (ja) | 2007-09-12 |
KR20030045088A (ko) | 2003-06-09 |
KR100598447B1 (ko) | 2006-07-10 |
DE60119753T2 (de) | 2006-11-30 |
JP2004510096A (ja) | 2004-04-02 |
EP1320664A2 (de) | 2003-06-25 |
EP1320664B1 (de) | 2006-05-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |