CN103998867A - 燃烧室 - Google Patents
燃烧室 Download PDFInfo
- Publication number
- CN103998867A CN103998867A CN201280050137.7A CN201280050137A CN103998867A CN 103998867 A CN103998867 A CN 103998867A CN 201280050137 A CN201280050137 A CN 201280050137A CN 103998867 A CN103998867 A CN 103998867A
- Authority
- CN
- China
- Prior art keywords
- combustion chamber
- air
- fuel
- passage
- compressor
- 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.)
- Pending
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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- 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
- 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
- F23R3/10—Air inlet arrangements for primary air
- F23R3/12—Air inlet arrangements for primary air inducing a vortex
-
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/58—Cyclone or vortex type combustion chambers
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161522412P | 2011-08-11 | 2011-08-11 | |
US61/522,412 | 2011-08-11 | ||
PCT/US2012/050349 WO2013023147A1 (en) | 2011-08-11 | 2012-08-10 | Combustor |
Publications (1)
Publication Number | Publication Date |
---|---|
CN103998867A true CN103998867A (zh) | 2014-08-20 |
Family
ID=47668992
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201280050137.7A Pending CN103998867A (zh) | 2011-08-11 | 2012-08-10 | 燃烧室 |
Country Status (5)
Country | Link |
---|---|
US (1) | US20140190178A1 (de) |
EP (1) | EP2742292A4 (de) |
CN (1) | CN103998867A (de) |
CA (1) | CA2844693A1 (de) |
WO (1) | WO2013023147A1 (de) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104373962A (zh) * | 2014-10-28 | 2015-02-25 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机燃烧室叶片进气旋流喷嘴 |
CN110741205A (zh) * | 2016-11-22 | 2020-01-31 | 贝克特瓦斯公司 | 燃烧器 |
KR20230106246A (ko) * | 2022-01-06 | 2023-07-13 | 두산에너빌리티 주식회사 | 연소기용 노즐, 연소기 및 이를 포함하는 가스 터빈 |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10634354B2 (en) | 2011-08-11 | 2020-04-28 | Beckett Gas, Inc. | Combustor |
US9366187B2 (en) | 2013-03-12 | 2016-06-14 | Pratt & Whitney Canada Corp. | Slinger combustor |
US9228747B2 (en) | 2013-03-12 | 2016-01-05 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
US9541292B2 (en) | 2013-03-12 | 2017-01-10 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
US9958161B2 (en) | 2013-03-12 | 2018-05-01 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
US9127843B2 (en) * | 2013-03-12 | 2015-09-08 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
CN110440290B (zh) * | 2018-05-02 | 2024-03-29 | 中国联合重型燃气轮机技术有限公司 | 用于燃气轮机的微混合喷嘴 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2785878A (en) * | 1953-09-16 | 1957-03-19 | Earl W Conrad | Porous walled conduit for fluid cooling |
US3788065A (en) * | 1970-10-26 | 1974-01-29 | United Aircraft Corp | Annular combustion chamber for dissimilar fluids in swirling flow relationship |
EP0202050A1 (de) * | 1985-04-29 | 1986-11-20 | Avco Corporation | Brennkammerwandstruktur |
US20040148936A1 (en) * | 1999-12-15 | 2004-08-05 | Koji Moriya | Fluid distributor, burner apparatus, gas turbine engine and co-generation system |
US20070028624A1 (en) * | 2005-07-25 | 2007-02-08 | General Electric Company | Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers |
CN101382297A (zh) * | 2007-09-05 | 2009-03-11 | 斯奈克玛 | 一种采用螺线气流的涡轮机燃烧室 |
US20110097189A1 (en) * | 2007-12-31 | 2011-04-28 | Aaron Sandoval | Boundary layer effect turbine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2718757A (en) * | 1951-01-17 | 1955-09-27 | Lummus Co | Aircraft gas turbine and jet |
US4058977A (en) * | 1974-12-18 | 1977-11-22 | United Technologies Corporation | Low emission combustion chamber |
US4996838A (en) * | 1988-10-27 | 1991-03-05 | Sol-3 Resources, Inc. | Annular vortex slinger combustor |
US6314717B1 (en) * | 1996-12-03 | 2001-11-13 | Elliott Energy Systems, Inc. | Electricity generating system having an annular combustor |
JP3600911B2 (ja) * | 2001-01-25 | 2004-12-15 | 川崎重工業株式会社 | 環状燃焼器のライナ支持構造 |
US6623267B1 (en) * | 2002-12-31 | 2003-09-23 | Tibbs M. Golladay, Jr. | Industrial burner |
-
2012
- 2012-08-10 EP EP12822757.6A patent/EP2742292A4/de not_active Withdrawn
- 2012-08-10 CN CN201280050137.7A patent/CN103998867A/zh active Pending
- 2012-08-10 CA CA2844693A patent/CA2844693A1/en not_active Abandoned
- 2012-08-10 WO PCT/US2012/050349 patent/WO2013023147A1/en active Application Filing
- 2012-08-10 US US14/238,067 patent/US20140190178A1/en not_active Abandoned
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2785878A (en) * | 1953-09-16 | 1957-03-19 | Earl W Conrad | Porous walled conduit for fluid cooling |
US3788065A (en) * | 1970-10-26 | 1974-01-29 | United Aircraft Corp | Annular combustion chamber for dissimilar fluids in swirling flow relationship |
EP0202050A1 (de) * | 1985-04-29 | 1986-11-20 | Avco Corporation | Brennkammerwandstruktur |
US20040148936A1 (en) * | 1999-12-15 | 2004-08-05 | Koji Moriya | Fluid distributor, burner apparatus, gas turbine engine and co-generation system |
US20070028624A1 (en) * | 2005-07-25 | 2007-02-08 | General Electric Company | Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers |
CN101382297A (zh) * | 2007-09-05 | 2009-03-11 | 斯奈克玛 | 一种采用螺线气流的涡轮机燃烧室 |
US20110097189A1 (en) * | 2007-12-31 | 2011-04-28 | Aaron Sandoval | Boundary layer effect turbine |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104373962A (zh) * | 2014-10-28 | 2015-02-25 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机燃烧室叶片进气旋流喷嘴 |
CN104373962B (zh) * | 2014-10-28 | 2016-08-24 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机燃烧室叶片进气旋流喷嘴 |
CN110741205A (zh) * | 2016-11-22 | 2020-01-31 | 贝克特瓦斯公司 | 燃烧器 |
CN110741205B (zh) * | 2016-11-22 | 2021-01-26 | 贝克特瓦斯公司 | 燃烧器 |
KR20230106246A (ko) * | 2022-01-06 | 2023-07-13 | 두산에너빌리티 주식회사 | 연소기용 노즐, 연소기 및 이를 포함하는 가스 터빈 |
KR102583222B1 (ko) | 2022-01-06 | 2023-09-25 | 두산에너빌리티 주식회사 | 연소기용 노즐, 연소기 및 이를 포함하는 가스 터빈 |
US11898754B2 (en) | 2022-01-06 | 2024-02-13 | Doosan Enerbility Co., Ltd. | Combustor nozzle, combustor, and gas turbine including the same |
Also Published As
Publication number | Publication date |
---|---|
CA2844693A1 (en) | 2013-02-14 |
WO2013023147A1 (en) | 2013-02-14 |
EP2742292A1 (de) | 2014-06-18 |
EP2742292A4 (de) | 2015-08-12 |
US20140190178A1 (en) | 2014-07-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP6972004B2 (ja) | 軸方向の燃料多段化を備える分割型環状燃焼システム | |
CN103998867A (zh) | 燃烧室 | |
JP6894447B2 (ja) | 分割型環状燃焼システムのための一体型燃焼器ノズル | |
CN205481129U (zh) | 用于燃气涡轮发动机的燃烧器的燃料喷嘴 | |
CN103438480B (zh) | 燃气涡轮发动机的喷嘴、燃烧室及相应的方法 | |
CN104246371B (zh) | 涡轮机燃烧器组装件 | |
US8881531B2 (en) | Gas turbine engine premix injectors | |
CN108779920A (zh) | 用于分段式环形燃烧系统的燃料喷射模块 | |
US9222673B2 (en) | Fuel nozzle and method of assembling the same | |
CN103032900A (zh) | 三元组反向旋转涡漩器和使用方法 | |
US10240795B2 (en) | Pilot burner having burner face with radially offset recess | |
US11708973B2 (en) | Combustor | |
JP2021110532A (ja) | 高圧流体流および低圧流体流を使用する流体混合装置 | |
CN103216851A (zh) | 具有弯曲部段的燃烧器喷嘴/预混器 | |
CN109804201A (zh) | 具有引燃空气供应的引燃器组件 | |
US20230304665A1 (en) | Method of supplying fuel and air to a combustor with an ignition tube | |
ES2870975T3 (es) | Cámara de combustión para una turbina de gas | |
EP3545236B1 (de) | Brennkammer | |
EP4230916A2 (de) | Brennkammer mit einem zündrohr | |
WO2008059045A1 (en) | Improvements in or relating to combustion apparatus | |
CN108431503A (zh) | 用于燃气轮机的燃烧器 | |
CN205717331U (zh) | 燃气涡轮燃烧器中的燃料喷嘴 | |
CN116412414A (zh) | 涡轮发动机燃料预混合器 | |
CN116293796A (zh) | 具有点火器的燃烧器 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140820 |