JP2007183093A5 - - Google Patents
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- Publication number
- JP2007183093A5 JP2007183093A5 JP2007000528A JP2007000528A JP2007183093A5 JP 2007183093 A5 JP2007183093 A5 JP 2007183093A5 JP 2007000528 A JP2007000528 A JP 2007000528A JP 2007000528 A JP2007000528 A JP 2007000528A JP 2007183093 A5 JP2007183093 A5 JP 2007183093A5
- Authority
- JP
- Japan
- Prior art keywords
- wall
- downstream
- upstream
- annular deflector
- annular
- 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
- 238000011144 upstream manufacturing Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0650071 | 2006-01-09 | ||
| FR0650071A FR2896031B1 (fr) | 2006-01-09 | 2006-01-09 | Dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2007183093A JP2007183093A (ja) | 2007-07-19 |
| JP2007183093A5 true JP2007183093A5 (enExample) | 2012-01-05 |
| JP5008400B2 JP5008400B2 (ja) | 2012-08-22 |
Family
ID=36956119
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2007000528A Active JP5008400B2 (ja) | 2006-01-09 | 2007-01-05 | 特にジェットエンジンの燃焼チャンバ用の多モード燃料噴射器 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US8033114B2 (enExample) |
| EP (1) | EP1806535B1 (enExample) |
| JP (1) | JP5008400B2 (enExample) |
| CN (1) | CN101000135B (enExample) |
| CA (1) | CA2572852C (enExample) |
| FR (1) | FR2896031B1 (enExample) |
| RU (1) | RU2429417C2 (enExample) |
Families Citing this family (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2893390B1 (fr) * | 2005-11-15 | 2011-04-01 | Snecma | Fond de chambre de combustion avec ventilation |
| DE102005062079A1 (de) * | 2005-12-22 | 2007-07-12 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner mit einer Zerstäuberlippe |
| FR2903169B1 (fr) * | 2006-06-29 | 2011-11-11 | Snecma | Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif |
| EP1985924A1 (en) * | 2007-04-23 | 2008-10-29 | Siemens Aktiengesellschaft | Swirler |
| FR2919898B1 (fr) | 2007-08-10 | 2014-08-22 | Snecma | Injecteur multipoint pour turbomachine |
| CN101382109B (zh) * | 2007-12-05 | 2011-07-20 | 奇瑞汽车股份有限公司 | 直喷式柴油机喷油器及进气道 |
| US20090249789A1 (en) * | 2008-04-08 | 2009-10-08 | Baifang Zuo | Burner tube premixer and method for mixing air and gas in a gas turbine engine |
| US20090255118A1 (en) * | 2008-04-11 | 2009-10-15 | General Electric Company | Method of manufacturing mixers |
| CN101382292B (zh) * | 2008-10-24 | 2010-09-01 | 孙明路 | 醇基燃烧机及其醇基燃烧喷嘴和气动剪切刀 |
| FR2948749B1 (fr) * | 2009-07-29 | 2011-09-09 | Snecma | Systeme d'injection de carburant pour une chambre de combustion de turbomachine |
| FR2951245B1 (fr) * | 2009-10-13 | 2013-05-17 | Snecma | Dispositif d'injection multi-point pour une chambre de combustion de turbomachine |
| FR2951246B1 (fr) * | 2009-10-13 | 2011-11-11 | Snecma | Injecteur multi-point pour une chambre de combustion de turbomachine |
| FR2956897B1 (fr) * | 2010-02-26 | 2012-07-20 | Snecma | Systeme d'injection pour chambre de combustion de turbomachine, comprenant des moyens d'injection d'air ameliorant le melange air-carburant |
| US8453454B2 (en) * | 2010-04-14 | 2013-06-04 | General Electric Company | Coannular oil injection nozzle |
| IT1399989B1 (it) | 2010-05-05 | 2013-05-09 | Avio Spa | Gruppo di iniezione per un combustore di una turbina a gas |
| CN102538014B (zh) * | 2012-01-11 | 2014-06-11 | 哈尔滨工程大学 | 一种用于化学回热循环的双燃料旋流雾化喷嘴 |
| US9677766B2 (en) * | 2012-11-28 | 2017-06-13 | General Electric Company | Fuel nozzle for use in a turbine engine and method of assembly |
| RU2618801C2 (ru) * | 2013-01-10 | 2017-05-11 | Дженерал Электрик Компани | Топливная форсунка, концевой узел топливной форсунки и газовая турбина |
| BR112016011777A2 (pt) | 2013-11-27 | 2017-08-08 | Gen Electric | Aparelhos de bocal de combustível |
| CA2933539C (en) | 2013-12-23 | 2022-01-18 | General Electric Company | Fuel nozzle with flexible support structures |
| US10451282B2 (en) | 2013-12-23 | 2019-10-22 | General Electric Company | Fuel nozzle structure for air assist injection |
| US9447976B2 (en) | 2014-01-10 | 2016-09-20 | Solar Turbines Incorporated | Fuel injector with a diffusing main gas passage |
| JP6433162B2 (ja) * | 2014-02-12 | 2018-12-05 | 株式会社エンプラス | 燃料噴射装置用ノズルプレート |
| CN104018952A (zh) * | 2014-03-22 | 2014-09-03 | 张鑫宇 | 一种飞机发动机 |
| US10125991B2 (en) * | 2014-08-14 | 2018-11-13 | Siemens Aktiengesellschaft | Multi-functional fuel nozzle with a heat shield |
| GB2548585B (en) * | 2016-03-22 | 2020-05-27 | Rolls Royce Plc | A combustion chamber assembly |
| CN105737200B (zh) * | 2016-03-28 | 2019-04-30 | 中国科学院工程热物理研究所 | 一种雾化喷嘴、喷嘴阵列和燃烧器 |
| US9976522B2 (en) * | 2016-04-15 | 2018-05-22 | Solar Turbines Incorporated | Fuel injector for combustion engine and staged fuel delivery method |
| CN105781835B (zh) * | 2016-04-22 | 2018-08-03 | 天津成立航空技术有限公司 | 一种航空航天发动机用旋风槽等静压分油器组件及其分油方法 |
| CN106091008B (zh) * | 2016-06-13 | 2019-08-02 | 中国科学院工程热物理研究所 | 兼具旋流、雾化与掺混作用的旋流器和喷射装置 |
| FR3084449B1 (fr) * | 2018-07-25 | 2020-07-17 | Safran Aircraft Engines | Dispositif d'injection de carburant multipoint |
| CN109404900B (zh) * | 2018-12-20 | 2024-03-19 | 东莞市鑫龙厨具食品机械有限公司 | 一种旋转汽化燃烧油盘及预蒸发燃烧机 |
| FR3091574B1 (fr) * | 2019-01-08 | 2020-12-11 | Safran Aircraft Engines | Systeme d’injection pour turbomachine, comprenant une vrille et des trous tourbillonnaires de bol melangeur |
| CN112228908A (zh) * | 2020-09-18 | 2021-01-15 | 西北工业大学 | 一种可控制流量式强化雾化的离心式喷嘴 |
| CN112360632B (zh) * | 2020-12-03 | 2024-06-18 | 上海电气燃气轮机有限公司 | 燃气轮机用挡油环 |
| CN112815355B (zh) * | 2021-01-19 | 2023-02-28 | 重庆交通大学绿色航空技术研究院 | 小型涡轮发动机的火焰稳定装置及涡轮发动机 |
| EP4317783A4 (en) * | 2021-03-25 | 2025-04-23 | IHI Corporation | COMBUSTION DEVICE AND GAS TURBINE SYSTEM |
| US12092324B2 (en) | 2022-03-17 | 2024-09-17 | General Electric Company | Flare cone for a mixer assembly of a gas turbine combustor |
| CN117091162A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 具有稀释孔结构的燃烧器 |
| CN117091159A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 燃烧器衬里 |
| CN117091157A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 用于耐用燃烧室衬里的板吊架结构 |
| CN117091161A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 燃烧器衬里的中空板设计和结构 |
| CN117091158A (zh) | 2022-05-13 | 2023-11-21 | 通用电气公司 | 燃烧器室网状结构 |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2719338B1 (fr) * | 1994-04-27 | 1996-06-28 | Aerospatiale | Tubulure d'échappement pour dispositif d'échappement à catalyse, et tube composite destiné à équiper ladite tubulure. |
| EP0956475B1 (de) * | 1996-12-20 | 2001-09-26 | Siemens Aktiengesellschaft | Brenner für fluidische brennstoffe |
| GB2337102A (en) * | 1998-05-09 | 1999-11-10 | Europ Gas Turbines Ltd | Gas-turbine engine combustor |
| US6082113A (en) * | 1998-05-22 | 2000-07-04 | Pratt & Whitney Canada Corp. | Gas turbine fuel injector |
| US6539724B2 (en) * | 2001-03-30 | 2003-04-01 | Delavan Inc | Airblast fuel atomization system |
| US20020162333A1 (en) * | 2001-05-02 | 2002-11-07 | Honeywell International, Inc., Law Dept. Ab2 | Partial premix dual circuit fuel injector |
| US6418726B1 (en) * | 2001-05-31 | 2002-07-16 | General Electric Company | Method and apparatus for controlling combustor emissions |
| EP1499800B1 (en) * | 2002-04-26 | 2011-06-29 | Rolls-Royce Corporation | Fuel premixing module for gas turbine engine combustor |
| US6718770B2 (en) * | 2002-06-04 | 2004-04-13 | General Electric Company | Fuel injector laminated fuel strip |
| US7143583B2 (en) * | 2002-08-22 | 2006-12-05 | Hitachi, Ltd. | Gas turbine combustor, combustion method of the gas turbine combustor, and method of remodeling a gas turbine combustor |
| JP3959632B2 (ja) * | 2002-09-04 | 2007-08-15 | 石川島播磨重工業株式会社 | 拡散燃焼方式低NOx燃焼器 |
| US6834505B2 (en) * | 2002-10-07 | 2004-12-28 | General Electric Company | Hybrid swirler |
| US7104066B2 (en) * | 2003-08-19 | 2006-09-12 | General Electric Company | Combuster swirler assembly |
| RU2264584C2 (ru) * | 2003-09-24 | 2005-11-20 | Открытое акционерное общество "Авиадвигатель" | Топливовоздушная горелка камеры сгорания газотурбинного двигателя |
| EP1568942A1 (de) * | 2004-02-24 | 2005-08-31 | Siemens Aktiengesellschaft | Vormischbrenner sowie Verfahren zur Verbrennung eines niederkalorischen Brenngases |
| US7065972B2 (en) * | 2004-05-21 | 2006-06-27 | Honeywell International, Inc. | Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions |
| US7581396B2 (en) * | 2005-07-25 | 2009-09-01 | General Electric Company | Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers |
-
2006
- 2006-01-09 FR FR0650071A patent/FR2896031B1/fr active Active
-
2007
- 2007-01-04 CA CA2572852A patent/CA2572852C/fr active Active
- 2007-01-05 JP JP2007000528A patent/JP5008400B2/ja active Active
- 2007-01-05 US US11/620,314 patent/US8033114B2/en active Active
- 2007-01-08 EP EP07100246.3A patent/EP1806535B1/fr active Active
- 2007-01-09 CN CN2007100000957A patent/CN101000135B/zh active Active
- 2007-01-09 RU RU2007100424/06A patent/RU2429417C2/ru active
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