CN101675228A - 燃气轮机燃烧器 - Google Patents
燃气轮机燃烧器 Download PDFInfo
- Publication number
- CN101675228A CN101675228A CN200880014221A CN200880014221A CN101675228A CN 101675228 A CN101675228 A CN 101675228A CN 200880014221 A CN200880014221 A CN 200880014221A CN 200880014221 A CN200880014221 A CN 200880014221A CN 101675228 A CN101675228 A CN 101675228A
- Authority
- CN
- China
- Prior art keywords
- combustion
- air flue
- area
- flow direction
- main flow
- 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.)
- Granted
Links
Images
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
- 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
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
-
- 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
- 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
- F02C7/24—Heat or noise insulation
-
- 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
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00018—Manufacturing combustion chamber liners or subparts
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03042—Film cooled combustion chamber walls or domes
-
- 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
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Combustion Of Fluid Fuel (AREA)
Abstract
Description
Claims (13)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP247226/2007 | 2007-09-25 | ||
JP2007247226A JP4823186B2 (ja) | 2007-09-25 | 2007-09-25 | ガスタービン燃焼器 |
PCT/JP2008/067189 WO2009041436A1 (ja) | 2007-09-25 | 2008-09-24 | ガスタービン燃焼器 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101675228A true CN101675228A (zh) | 2010-03-17 |
CN101675228B CN101675228B (zh) | 2013-07-17 |
Family
ID=40511319
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2008800142217A Active CN101675228B (zh) | 2007-09-25 | 2008-09-24 | 燃气轮机燃烧器 |
Country Status (6)
Country | Link |
---|---|
US (1) | US20100170260A1 (zh) |
EP (1) | EP2187021B1 (zh) |
JP (1) | JP4823186B2 (zh) |
KR (1) | KR101133487B1 (zh) |
CN (1) | CN101675228B (zh) |
WO (1) | WO2009041436A1 (zh) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103321693A (zh) * | 2012-03-22 | 2013-09-25 | 通用电气公司 | 用于冷却涡轮机排气框架的压缩器抽气流的主动控制 |
CN105531543A (zh) * | 2013-09-09 | 2016-04-27 | 西门子公司 | 具有火焰管端部区域的管式燃烧室和燃气轮机 |
CN108603443A (zh) * | 2016-03-10 | 2018-09-28 | 三菱日立电力系统株式会社 | 燃烧器用面板、燃烧器、燃烧装置、燃气轮机、以及燃烧器用面板的冷却方法 |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5653705B2 (ja) * | 2010-09-30 | 2015-01-14 | 三菱重工業株式会社 | 回収式空気冷却ガスタービン燃焼器冷却構造 |
US8733496B2 (en) * | 2011-03-22 | 2014-05-27 | Mitsubishi Heavy Industries, Ltd. | Acoustic damper, combustor, and gas turbine |
KR20130116948A (ko) * | 2011-05-24 | 2013-10-24 | 미츠비시 쥬고교 가부시키가이샤 | 중공 만곡판 및 그 제조 방법 및 가스 터빈의 연소기 |
US9239165B2 (en) * | 2012-06-07 | 2016-01-19 | United Technologies Corporation | Combustor liner with convergent cooling channel |
AU2013219140B2 (en) * | 2012-08-24 | 2015-10-08 | Ansaldo Energia Switzerland AG | Method for mixing a dilution air in a sequential combustion system of a gas turbine |
US9939154B2 (en) * | 2013-02-14 | 2018-04-10 | United Technologies Corporation | Combustor liners with U-shaped cooling channels |
EP2863018B1 (en) * | 2013-10-17 | 2018-03-21 | Ansaldo Energia Switzerland AG | Combustor of a gas turbine with a transition piece having a cooling structure |
JP6239938B2 (ja) * | 2013-11-05 | 2017-11-29 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器 |
KR101772837B1 (ko) * | 2014-04-25 | 2017-08-29 | 미츠비시 히타치 파워 시스템즈 가부시키가이샤 | 가스터빈 연소기 및 해당 연소기를 구비한 가스터빈 |
WO2016013585A1 (ja) * | 2014-07-25 | 2016-01-28 | 三菱日立パワーシステムズ株式会社 | 燃焼器用筒体、燃焼器及びガスタービン |
JP6623485B2 (ja) * | 2014-09-25 | 2019-12-25 | 三菱日立パワーシステムズ株式会社 | 燃焼器、及びこれを備えるガスタービン |
JP6476516B2 (ja) * | 2015-01-30 | 2019-03-06 | 三菱日立パワーシステムズ株式会社 | トランジションピース、これを備える燃焼器、及び燃焼器を備えるガスタービン |
GB201501971D0 (en) * | 2015-02-06 | 2015-03-25 | Rolls Royce Plc | A combustion chamber |
JP6484546B2 (ja) * | 2015-11-13 | 2019-03-13 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器 |
US20170138595A1 (en) * | 2015-11-18 | 2017-05-18 | General Electric Company | Combustor Wall Channel Cooling System |
US10584638B2 (en) * | 2016-03-25 | 2020-03-10 | General Electric Company | Turbine nozzle cooling with panel fuel injector |
JP7008722B2 (ja) * | 2017-03-30 | 2022-01-25 | シーメンス アクティエンゲゼルシャフト | ガスタービンエンジンの燃焼器セクションにおける冷却流体の二重利用のための導管配置を備えたシステム |
RU2644668C1 (ru) * | 2017-05-24 | 2018-02-13 | Владислав Юрьевич Климов | Парогазогенератор |
US11371702B2 (en) * | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
US11994293B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus support structure and method of manufacture |
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 |
US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
KR102468746B1 (ko) * | 2020-11-18 | 2022-11-18 | 한국항공우주연구원 | 열교환 구조를 포함하는 연소기 및 이를 포함하는 로켓 |
JP7370364B2 (ja) * | 2021-09-30 | 2023-10-27 | 三菱重工業株式会社 | トランジションピース、燃焼器及びガスタービンエンジン |
US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4195474A (en) * | 1977-10-17 | 1980-04-01 | General Electric Company | Liquid-cooled transition member to turbine inlet |
US4302941A (en) * | 1980-04-02 | 1981-12-01 | United Technologies Corporation | Combuster liner construction for gas turbine engine |
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 |
JPH1015743A (ja) * | 1996-07-05 | 1998-01-20 | Mitsubishi Heavy Ind Ltd | 冷却板の製造方法 |
JP3626861B2 (ja) * | 1998-11-12 | 2005-03-09 | 三菱重工業株式会社 | ガスタービン燃焼器の冷却構造 |
CA2288557C (en) * | 1998-11-12 | 2007-02-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor cooling structure |
JP3930252B2 (ja) * | 2000-01-07 | 2007-06-13 | 三菱重工業株式会社 | ガスタービン燃焼器 |
JP2001289062A (ja) * | 2000-04-07 | 2001-10-19 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器の壁面冷却構造 |
JP2002155757A (ja) * | 2000-11-17 | 2002-05-31 | Mitsubishi Heavy Ind Ltd | 燃焼器およびその燃焼器を備えたガスタービン |
DE60135436D1 (de) * | 2001-01-09 | 2008-10-02 | Mitsubishi Heavy Ind Ltd | 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 |
JP3962554B2 (ja) * | 2001-04-19 | 2007-08-22 | 三菱重工業株式会社 | ガスタービン燃焼器及びガスタービン |
JP3831638B2 (ja) * | 2001-08-09 | 2006-10-11 | 三菱重工業株式会社 | 板状体接合方法、接合体、ガスタービン燃焼器用の尾筒、及び、ガスタービン燃焼器 |
US6840048B2 (en) * | 2002-09-26 | 2005-01-11 | General Electric Company | Dynamically uncoupled can combustor |
US6890148B2 (en) * | 2003-08-28 | 2005-05-10 | Siemens Westinghouse Power Corporation | Transition duct cooling system |
JP4545158B2 (ja) * | 2007-01-31 | 2010-09-15 | 三菱重工業株式会社 | 燃焼器尾筒の冷却構造 |
-
2007
- 2007-09-25 JP JP2007247226A patent/JP4823186B2/ja active Active
-
2008
- 2008-09-24 US US12/598,106 patent/US20100170260A1/en not_active Abandoned
- 2008-09-24 KR KR1020097021998A patent/KR101133487B1/ko active IP Right Grant
- 2008-09-24 WO PCT/JP2008/067189 patent/WO2009041436A1/ja active Application Filing
- 2008-09-24 CN CN2008800142217A patent/CN101675228B/zh active Active
- 2008-09-24 EP EP08834165.6A patent/EP2187021B1/en active Active
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103321693A (zh) * | 2012-03-22 | 2013-09-25 | 通用电气公司 | 用于冷却涡轮机排气框架的压缩器抽气流的主动控制 |
CN105531543A (zh) * | 2013-09-09 | 2016-04-27 | 西门子公司 | 具有火焰管端部区域的管式燃烧室和燃气轮机 |
CN105531543B (zh) * | 2013-09-09 | 2017-03-22 | 西门子公司 | 具有火焰管端部区域的管式燃烧室和燃气轮机 |
CN108603443A (zh) * | 2016-03-10 | 2018-09-28 | 三菱日立电力系统株式会社 | 燃烧器用面板、燃烧器、燃烧装置、燃气轮机、以及燃烧器用面板的冷却方法 |
Also Published As
Publication number | Publication date |
---|---|
EP2187021A4 (en) | 2015-03-11 |
JP4823186B2 (ja) | 2011-11-24 |
KR20090128508A (ko) | 2009-12-15 |
JP2009079484A (ja) | 2009-04-16 |
CN101675228B (zh) | 2013-07-17 |
EP2187021A1 (en) | 2010-05-19 |
WO2009041436A1 (ja) | 2009-04-02 |
US20100170260A1 (en) | 2010-07-08 |
EP2187021B1 (en) | 2016-09-21 |
KR101133487B1 (ko) | 2012-04-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101675228B (zh) | 燃气轮机燃烧器 | |
CA2587060C (en) | Combustor with improved swirl | |
US9759426B2 (en) | Combustor nozzles in gas turbine engines | |
CN100443806C (zh) | 切向驻涡燃烧室 | |
CN102985758B (zh) | 用于燃气涡轮发动机的具有无叶片涡轮的切向燃烧室 | |
EP2211104B1 (en) | Venturi cooling system | |
CN101063422B (zh) | 用于降低燃气涡轮发动机内的压力损失的方法和系统 | |
US7624577B2 (en) | Gas turbine engine combustor with improved cooling | |
US9151500B2 (en) | System for supplying a fuel and a working fluid through a liner to a combustion chamber | |
US8904796B2 (en) | Flashback resistant tubes for late lean injector and method for forming the tubes | |
JP6138584B2 (ja) | タービンエンジンに使用するための燃料注入組立体及びそれを組み立てる方法 | |
CN101892908A (zh) | 用于冷却燃气涡轮机燃烧器的壁的系统和方法 | |
JP2008286199A (ja) | タービンエンジンを冷却する方法及び装置 | |
CN102844622B (zh) | 一种多燃料燃烧系统 | |
KR20100074108A (ko) | 연소기 접속 구조체, 연소기 미통, 연소기 미통의 설계 방법, 및 가스 터빈 | |
CN101713549A (zh) | 用于在燃气涡轮机中混合空气-燃料的系统及方法 | |
CN104053883B (zh) | 混合用于在燃气涡轮发动机内燃烧的燃烧反应物的方法 | |
US20200248905A1 (en) | Rotating detonation combustor with discrete detonation annuli | |
JP4961415B2 (ja) | ガスタービン燃焼器 | |
JP2017116250A (ja) | ガスタービンにおける燃料噴射器および段階的燃料噴射システム | |
US9181812B1 (en) | Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines | |
US20130074506A1 (en) | Turbine burner | |
JP2009079483A (ja) | ガスタービン燃焼器 | |
US8640974B2 (en) | System and method for cooling a nozzle | |
JP5934795B2 (ja) | ガス・タービン・エンジンで使用するための接線方向で火炎のない環状燃焼器 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
ASS | Succession or assignment of patent right |
Owner name: MITSUBISHI HITACHI POWER SYSTEM LTD. Free format text: FORMER OWNER: MITSUBISHI JUKOGIO KK Effective date: 20150409 |
|
C41 | Transfer of patent application or patent right or utility model | ||
TR01 | Transfer of patent right |
Effective date of registration: 20150409 Address after: yokohama Patentee after: Mitsubishi Hitachi Power System Ltd. Address before: Tokyo, Japan Patentee before: Mit-subishi Heavy Industries Ltd. |
|
CP01 | Change in the name or title of a patent holder | ||
CP01 | Change in the name or title of a patent holder |
Address after: yokohama Patentee after: Mitsubishi Power Co., Ltd Address before: yokohama Patentee before: MITSUBISHI HITACHI POWER SYSTEMS, Ltd. |