AR011159A1 - Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aire - Google Patents
Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aireInfo
- Publication number
- AR011159A1 AR011159A1 ARP980100779A ARP980100779A AR011159A1 AR 011159 A1 AR011159 A1 AR 011159A1 AR P980100779 A ARP980100779 A AR P980100779A AR P980100779 A ARP980100779 A AR P980100779A AR 011159 A1 AR011159 A1 AR 011159A1
- Authority
- AR
- Argentina
- Prior art keywords
- transition
- cooled transition
- air
- steam
- cooled
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/005—Combined with pressure or heat exchangers
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Un método de convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas que tiene una compresoren comunicacion de fluido con un mechero, una seccion de turbina en comunicacion de fluido con el mechero, la transicion dispuesta en una vaina demechero y que tiene un circuito de refrigeracion que conecta una salida de vapor y una entrada de vapor y en donde fluye gas caliente desde el mechero através de la transicion y haciala seccion de turbina, incluye formar una salida de aire en la transicion en comunicacion de fluido con el circuito derefrigeracion y proveer una entrada de aire en la transicion en comunicacion de fluido con el circuito refrigerante. Incluye una turbina para llevar a cabodicho método y una transicion refrigerada por vapor convertible a una transicion refrigerada por aire.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/803,614 US5906093A (en) | 1997-02-21 | 1997-02-21 | Gas turbine combustor transition |
Publications (1)
Publication Number | Publication Date |
---|---|
AR011159A1 true AR011159A1 (es) | 2000-08-02 |
Family
ID=25187008
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ARP980100779A AR011159A1 (es) | 1997-02-21 | 1998-02-20 | Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aire |
Country Status (7)
Country | Link |
---|---|
US (1) | US5906093A (es) |
EP (1) | EP1009915B1 (es) |
JP (1) | JP2002511121A (es) |
KR (1) | KR20000070976A (es) |
AR (1) | AR011159A1 (es) |
DE (1) | DE69810940T2 (es) |
WO (1) | WO1998037311A1 (es) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3202636B2 (ja) * | 1997-02-12 | 2001-08-27 | 東北電力株式会社 | 蒸気冷却燃焼器の冷却壁構造 |
JP3110338B2 (ja) * | 1997-02-12 | 2000-11-20 | 東北電力株式会社 | 燃焼器の蒸気による冷却構造 |
JP3310900B2 (ja) * | 1997-04-15 | 2002-08-05 | 三菱重工業株式会社 | 燃焼器尾筒の冷却構造 |
DE60137099D1 (de) * | 2000-04-13 | 2009-02-05 | Mitsubishi Heavy Ind Ltd | Kühlstruktur für das Endstück einer Gasturbinenbrennkammer |
JP2002243154A (ja) * | 2001-02-16 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器 |
JP2002309903A (ja) * | 2001-04-10 | 2002-10-23 | Mitsubishi Heavy Ind Ltd | ガスタービンの蒸気配管構造 |
JP4008212B2 (ja) * | 2001-06-29 | 2007-11-14 | 三菱重工業株式会社 | フランジ付中空構造物 |
JP2005163812A (ja) * | 2003-11-28 | 2005-06-23 | Nissan Motor Co Ltd | 支持構造 |
US7096668B2 (en) * | 2003-12-22 | 2006-08-29 | Martling Vincent C | Cooling and sealing design for a gas turbine combustion system |
US7178341B2 (en) * | 2004-06-17 | 2007-02-20 | Siemens Power Generation, Inc. | Multi-zone tubing assembly for a transition piece of a gas turbine |
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 |
US7870739B2 (en) * | 2006-02-02 | 2011-01-18 | Siemens Energy, Inc. | Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions |
US7827801B2 (en) * | 2006-02-09 | 2010-11-09 | Siemens Energy, Inc. | Gas turbine engine transitions comprising closed cooled transition cooling channels |
US20100236244A1 (en) * | 2006-06-28 | 2010-09-23 | Longardner Robert L | Heat absorbing and reflecting shield for air breathing heat engine |
US8245515B2 (en) * | 2008-08-06 | 2012-08-21 | General Electric Company | Transition duct aft end frame cooling and related method |
US8549861B2 (en) * | 2009-01-07 | 2013-10-08 | General Electric Company | Method and apparatus to enhance transition duct cooling in a gas turbine engine |
US8281601B2 (en) * | 2009-03-20 | 2012-10-09 | General Electric Company | Systems and methods for reintroducing gas turbine combustion bypass flow |
US8955330B2 (en) * | 2011-03-29 | 2015-02-17 | Siemens Energy, Inc. | Turbine combustion system liner |
EP2691609A1 (en) * | 2011-03-31 | 2014-02-05 | General Electric Company | Power augmentation system with dynamics damping |
US8966910B2 (en) * | 2011-06-21 | 2015-03-03 | General Electric Company | Methods and systems for cooling a transition nozzle |
US9188009B2 (en) * | 2012-10-30 | 2015-11-17 | United Technologies Corporation | Bore cavity thermal conditioning system |
US9574498B2 (en) * | 2013-09-25 | 2017-02-21 | General Electric Company | Internally cooled transition duct aft frame with serpentine cooling passage and conduit |
KR101829572B1 (ko) * | 2014-07-25 | 2018-02-14 | 미츠비시 히타치 파워 시스템즈 가부시키가이샤 | 연소기용 통체, 연소기 및 가스 터빈 |
KR102403512B1 (ko) | 2015-04-30 | 2022-05-31 | 삼성전자주식회사 | 공기 조화기의 실외기, 이에 적용되는 컨트롤 장치 |
DE102015212573A1 (de) * | 2015-07-06 | 2017-01-12 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammer mit integriertem Turbinenvorleitrad sowie Verfahren zu deren Herstellung |
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 |
US10605459B2 (en) | 2016-03-25 | 2020-03-31 | General Electric Company | Integrated combustor nozzle for a segmented annular combustion system |
US10641491B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Cooling of integrated combustor nozzle of 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 |
US10641175B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Panel fuel injector |
US10584880B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Mounting of integrated combustor nozzles in a segmented annular combustion system |
US11428413B2 (en) | 2016-03-25 | 2022-08-30 | General Electric Company | Fuel injection module for 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 |
US10830142B2 (en) * | 2016-10-10 | 2020-11-10 | General Electric Company | Combustor aft frame cooling |
US11156362B2 (en) | 2016-11-28 | 2021-10-26 | General Electric Company | Combustor with axially staged fuel injection |
US10690350B2 (en) | 2016-11-28 | 2020-06-23 | General Electric Company | Combustor with axially staged fuel injection |
US11371702B2 (en) | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
US11614233B2 (en) | 2020-08-31 | 2023-03-28 | General Electric Company | Impingement panel support structure and method of manufacture |
US11994292B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus for turbomachine |
US11994293B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus 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 (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4719748A (en) * | 1985-05-14 | 1988-01-19 | General Electric Company | Impingement cooled transition duct |
DE3615226A1 (de) * | 1986-05-06 | 1987-11-12 | Mtu Muenchen Gmbh | Heissgasueberhitzungsschutzeinrichtung fuer gasturbinentriebwerke |
JPS63309733A (ja) * | 1987-06-12 | 1988-12-16 | Hitachi Ltd | ガスタ−ビン燃焼器 |
FR2656657A1 (fr) * | 1989-12-28 | 1991-07-05 | Snecma | Turbomachine refroidie par air et procede de refroidissement de cette turbomachine. |
DE59010740D1 (de) * | 1990-12-05 | 1997-09-04 | Asea Brown Boveri | Gasturbinen-Brennkammer |
KR930013441A (ko) * | 1991-12-18 | 1993-07-21 | 아더 엠.킹 | 다수의 연소기들을 포함한 가스터어빈 연소장치 |
DE4210544A1 (de) * | 1992-03-31 | 1993-10-07 | Asea Brown Boveri | Gasturbinenanlage |
US5237813A (en) * | 1992-08-21 | 1993-08-24 | Allied-Signal Inc. | Annular combustor with outer transition liner cooling |
US5685158A (en) * | 1995-03-31 | 1997-11-11 | General Electric Company | Compressor rotor cooling system for a gas turbine |
WO1997014875A1 (en) * | 1995-10-17 | 1997-04-24 | Westinghouse Electric Corporation | Gas turbine regenerative cooled combustor |
-
1997
- 1997-02-21 US US08/803,614 patent/US5906093A/en not_active Expired - Lifetime
-
1998
- 1998-02-10 JP JP53667098A patent/JP2002511121A/ja not_active Ceased
- 1998-02-10 KR KR1019997007242A patent/KR20000070976A/ko not_active Application Discontinuation
- 1998-02-10 WO PCT/US1998/002218 patent/WO1998037311A1/en not_active Application Discontinuation
- 1998-02-10 DE DE69810940T patent/DE69810940T2/de not_active Expired - Lifetime
- 1998-02-10 EP EP98908472A patent/EP1009915B1/en not_active Expired - Lifetime
- 1998-02-20 AR ARP980100779A patent/AR011159A1/es unknown
Also Published As
Publication number | Publication date |
---|---|
EP1009915A1 (en) | 2000-06-21 |
US5906093A (en) | 1999-05-25 |
JP2002511121A (ja) | 2002-04-09 |
EP1009915B1 (en) | 2003-01-22 |
DE69810940T2 (de) | 2003-08-28 |
DE69810940D1 (de) | 2003-02-27 |
WO1998037311A1 (en) | 1998-08-27 |
KR20000070976A (ko) | 2000-11-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AR011159A1 (es) | Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aire | |
KR100598447B1 (ko) | 연소 터빈 전이부의 냉각에 사용하기 위한 압축공기 스팀발생기 | |
US7600382B2 (en) | Turbine engine with interstage heat transfer | |
CN110185501B (zh) | 带具有冷却入口的导叶的燃气涡轮发动机 | |
EP1363078A3 (en) | Bulkhead panel for use in a combustion chamber of a gas turbine engine | |
EP1239121A3 (en) | An air-cooled gas turbine exhaust casing | |
SE8904209D0 (sv) | Turbine engine with air and steam cooling | |
US7052015B2 (en) | Cooling arrangement for brush seal | |
EP1600615A3 (en) | Intercooler system for gas turbine engines | |
ATE549577T1 (de) | Wärmekraftanlage mit sequentieller verbrennung und reduziertem co2-ausstoss sowie verfahren zum betreiben einer derartigen anlage | |
KR930019989A (ko) | 가스 터어빈 그룹을 작동하는 방법 | |
KR930021925A (ko) | 개스 터빈 그룹의 작동방법 | |
EP1167722A3 (en) | Methods and apparatus for delivering cooling air within gas turbines | |
ES2126881T3 (es) | Camara de combustion para una turbina de gas. | |
AR011336A1 (es) | Turbina de gas | |
US20150167554A1 (en) | Gas turbine device using supercritical fluid as cooling fluid | |
WO2006069948A3 (de) | Kraftwerksanlage | |
EP1433924A3 (en) | Gas turbine combustor | |
JP2011085135A (ja) | 蒸気タービンロータを冷却するためのシステム及び方法 | |
EP0900919A3 (en) | Steam-cooled gas turbine | |
US10830146B2 (en) | Compressor bleed cooling system for mid-frame torque discs downstream from a compressor assembly in a gas turbine engine | |
ATE421632T1 (de) | Dampf- und gasturbinenanlage | |
CN106103900A (zh) | 具有使用高低压冷却流体的冷却***的涡轮机翼型件 | |
JP2009103127A (ja) | ターボ機械用の冷却ブレード | |
SE0401496D0 (sv) | Gas turbine compression system and compressor structure |