JP2011064447A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2011064447A5 JP2011064447A5 JP2010151520A JP2010151520A JP2011064447A5 JP 2011064447 A5 JP2011064447 A5 JP 2011064447A5 JP 2010151520 A JP2010151520 A JP 2010151520A JP 2010151520 A JP2010151520 A JP 2010151520A JP 2011064447 A5 JP2011064447 A5 JP 2011064447A5
- Authority
- JP
- Japan
- Prior art keywords
- combustor
- inlet guide
- flow
- fuel nozzles
- disposed
- 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
- 239000000446 fuel Substances 0.000 claims description 7
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 238000011144 upstream manufacturing Methods 0.000 claims 3
- 238000009826 distribution Methods 0.000 description 3
- 238000009827 uniform distribution Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/559,522 | 2009-09-15 | ||
| US12/559,522 US8371101B2 (en) | 2009-09-15 | 2009-09-15 | Radial inlet guide vanes for a combustor |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2011064447A JP2011064447A (ja) | 2011-03-31 |
| JP2011064447A5 true JP2011064447A5 (enExample) | 2013-08-15 |
| JP5572458B2 JP5572458B2 (ja) | 2014-08-13 |
Family
ID=43571181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2010151520A Active JP5572458B2 (ja) | 2009-09-15 | 2010-07-02 | 燃焼器用の半径方向入口案内翼 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8371101B2 (enExample) |
| JP (1) | JP5572458B2 (enExample) |
| CN (1) | CN102022728B (enExample) |
| CH (1) | CH701773B1 (enExample) |
| DE (1) | DE102010017779B4 (enExample) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013043078A1 (en) * | 2011-09-22 | 2013-03-28 | General Electric Company | Combustor cap for damping low frequency dynamics |
| US9353949B2 (en) * | 2012-04-17 | 2016-05-31 | Siemens Energy, Inc. | Device for improved air and fuel distribution to a combustor |
| US20140083111A1 (en) * | 2012-09-25 | 2014-03-27 | United Technologies Corporation | Gas turbine asymmetric fuel nozzle combustor |
| US9297533B2 (en) * | 2012-10-30 | 2016-03-29 | General Electric Company | Combustor and a method for cooling the combustor |
| EP3011231B1 (en) * | 2013-06-18 | 2019-10-30 | Woodward, Inc. | Gas turbine combustor assembly |
| US20150338101A1 (en) * | 2014-05-21 | 2015-11-26 | General Electric Company | Turbomachine combustor including a combustor sleeve baffle |
| US9964308B2 (en) * | 2014-08-19 | 2018-05-08 | General Electric Company | Combustor cap assembly |
| US10788213B2 (en) | 2015-08-27 | 2020-09-29 | Arizona Board Of Regents On Behalf Of Arizona State University | Rayleigh-Taylor assisted combustion with micro-flameholders |
| US10578307B2 (en) | 2015-10-09 | 2020-03-03 | Dresser-Rand Company | System and method for operating a gas turbine assembly including heating a reaction/oxidation chamber |
| DE102015226305A1 (de) * | 2015-12-21 | 2017-06-22 | Siemens Aktiengesellschaft | Gasturbinenanlage und Verfahren zum Betreiben einer Gasturbinenanlage |
| CN108826357A (zh) * | 2018-07-27 | 2018-11-16 | 清华大学 | 发动机的环形燃烧室 |
| CN114576012B (zh) * | 2022-03-29 | 2023-09-26 | 华北电力科学研究院有限责任公司 | 燃气轮机进口导叶调节方法及装置 |
| CN114992672B (zh) * | 2022-06-11 | 2024-04-26 | 江苏中科能源动力研究中心 | 一种微预混式燃气轮机燃烧室 |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2889871A (en) * | 1957-03-13 | 1959-06-09 | Temple S Voorheis | Method and means relating to high capacity forced draft gas burner art |
| DE4110507C2 (de) * | 1991-03-30 | 1994-04-07 | Mtu Muenchen Gmbh | Brenner für Gasturbinentriebwerke mit mindestens einer für die Zufuhr von Verbrennungsluft lastabhängig regulierbaren Dralleinrichtung |
| JPH05203148A (ja) | 1992-01-13 | 1993-08-10 | Hitachi Ltd | ガスタービン燃焼装置及びその制御方法 |
| US5394688A (en) * | 1993-10-27 | 1995-03-07 | Westinghouse Electric Corporation | Gas turbine combustor swirl vane arrangement |
| JP2950720B2 (ja) | 1994-02-24 | 1999-09-20 | 株式会社東芝 | ガスタービン燃焼装置およびその燃焼制御方法 |
| IT1273369B (it) * | 1994-03-04 | 1997-07-08 | Nuovo Pignone Spa | Sistema perfezionato combustione a basse emissioni inquinanti per turbine a gas |
| US5983642A (en) * | 1997-10-13 | 1999-11-16 | Siemens Westinghouse Power Corporation | Combustor with two stage primary fuel tube with concentric members and flow regulating |
| US20020162333A1 (en) * | 2001-05-02 | 2002-11-07 | Honeywell International, Inc., Law Dept. Ab2 | Partial premix dual circuit fuel injector |
| DE10219354A1 (de) * | 2002-04-30 | 2003-11-13 | Rolls Royce Deutschland | Gasturbinenbrennkammer mit gezielter Kraftstoffeinbringung zur Verbesserung der Homogenität des Kraftstoff-Luft-Gemisches |
| US6761033B2 (en) | 2002-07-18 | 2004-07-13 | Hitachi, Ltd. | Gas turbine combustor with fuel-air pre-mixer and pre-mixing method for low NOx combustion |
| WO2006021543A1 (de) * | 2004-08-27 | 2006-03-02 | Alstom Technology Ltd | Mischeranordnung |
| US20070028618A1 (en) * | 2005-07-25 | 2007-02-08 | General Electric Company | Mixer assembly for combustor of a gas turbine engine having a main mixer with improved fuel penetration |
| US7685824B2 (en) * | 2005-09-09 | 2010-03-30 | The Regents Of The University Of Michigan | Rotary ramjet turbo-generator |
| JP2008082590A (ja) * | 2006-09-27 | 2008-04-10 | Hitachi Ltd | ガスタービン燃焼器 |
| US8117845B2 (en) * | 2007-04-27 | 2012-02-21 | General Electric Company | Systems to facilitate reducing flashback/flame holding in combustion systems |
| CN101398186A (zh) * | 2008-10-24 | 2009-04-01 | 北京大学 | 自吸式旋流气动雾化喷嘴装置 |
-
2009
- 2009-09-15 US US12/559,522 patent/US8371101B2/en active Active
-
2010
- 2010-07-02 JP JP2010151520A patent/JP5572458B2/ja active Active
- 2010-07-06 DE DE102010017779.2A patent/DE102010017779B4/de active Active
- 2010-07-07 CH CH01111/10A patent/CH701773B1/de not_active IP Right Cessation
- 2010-07-15 CN CN201010236511.5A patent/CN102022728B/zh active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP2011064447A5 (enExample) | ||
| CN102052681B (zh) | 用于调节穿过喷嘴的空气流的设备 | |
| RU2570989C2 (ru) | Осевой завихритель для камеры сгорания газовой турбины | |
| EP3250856B1 (en) | Fuel injector including a lobed mixer and vanes for injecting alternate fuels in a gas turbine | |
| US9151223B2 (en) | Gas turbine combustion chamber arrangement of axial type of construction | |
| JP5572458B2 (ja) | 燃焼器用の半径方向入口案内翼 | |
| CN103123121B (zh) | 具有可调式限流器的燃气涡轮机燃烧室端盖以及相关方法 | |
| CN108204250A (zh) | 用于涡轮发动机的流体喷嘴组件 | |
| CN101900340A (zh) | 增强燃气涡轮发动机中火焰稳定性的方法和系统 | |
| US9127554B2 (en) | Gas turbine engine with radial diffuser and shortened mid section | |
| US20120198810A1 (en) | Strut airfoil design for low solidity exhaust gas diffuser | |
| JP2012149869A5 (enExample) | ||
| CA2660211A1 (en) | Gas turbine engine exhaust duct ventilation | |
| US9297390B2 (en) | Exhaust gas diffuser for a gas turbine and a method for operating a gas turbine that comprises such an exhaust gas diffuser | |
| JP2009047411A (ja) | ターボ機械ディフューザ | |
| US9810432B2 (en) | Method for premixing air with a gaseous fuel and burner arrangement for conducting said method | |
| JP2014077627A5 (enExample) | ||
| US20120111013A1 (en) | System for directing air flow in a fuel nozzle assembly | |
| JP2012102995A5 (enExample) | ||
| JP2014181898A (ja) | ガス・タービンの下流燃料及び空気噴射に関わるシステム及び装置 | |
| US11815269B2 (en) | Fuel-air mixing assembly in a turbine engine | |
| CN104110698A (zh) | 一种用于燃气轮机燃烧室的预混合喷嘴 | |
| US20180187563A1 (en) | Gas turbine transition duct with late lean injection having reduced combustion residence time | |
| JP2016166728A (ja) | 燃焼器の燃料噴射装置用のエアシールド | |
| US10330047B2 (en) | Asymmetric fan nozzle in high-BPR separate-flow nacelle |