JP2006090327A5 - - Google Patents
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- Publication number
- JP2006090327A5 JP2006090327A5 JP2005275038A JP2005275038A JP2006090327A5 JP 2006090327 A5 JP2006090327 A5 JP 2006090327A5 JP 2005275038 A JP2005275038 A JP 2005275038A JP 2005275038 A JP2005275038 A JP 2005275038A JP 2006090327 A5 JP2006090327 A5 JP 2006090327A5
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- JP
- Japan
- 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
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Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0410052 | 2004-09-23 | ||
| FR0410052A FR2875585B1 (fr) | 2004-09-23 | 2004-09-23 | Systeme aerodynamique a effervescence d'injection air/carburant dans une chambre de combustion de turbomachine |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2006090327A JP2006090327A (ja) | 2006-04-06 |
| JP2006090327A5 true JP2006090327A5 (enExample) | 2010-11-04 |
| JP4695952B2 JP4695952B2 (ja) | 2011-06-08 |
Family
ID=34949669
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2005275038A Expired - Lifetime JP4695952B2 (ja) | 2004-09-23 | 2005-09-22 | ターボ機械燃焼室に空気／燃料混合物を噴射する発泡性空気力式システム |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US7506496B2 (enExample) |
| EP (1) | EP1640661B1 (enExample) |
| JP (1) | JP4695952B2 (enExample) |
| CN (1) | CN100545433C (enExample) |
| DE (1) | DE602005001742T2 (enExample) |
| FR (1) | FR2875585B1 (enExample) |
| RU (1) | RU2309329C2 (enExample) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8266911B2 (en) * | 2005-11-14 | 2012-09-18 | General Electric Company | Premixing device for low emission combustion process |
| KR20100022491A (ko) * | 2007-05-25 | 2010-03-02 | 코닝 인코포레이티드 | 유리 시트를 취급하기 위한 장치 |
| US7874157B2 (en) * | 2008-06-05 | 2011-01-25 | General Electric Company | Coanda pilot nozzle for low emission combustors |
| US8240150B2 (en) * | 2008-08-08 | 2012-08-14 | General Electric Company | Lean direct injection diffusion tip and related method |
| US8359870B2 (en) * | 2009-05-12 | 2013-01-29 | General Electric Company | Automatic fuel nozzle flame-holding quench |
| US9777637B2 (en) * | 2012-03-08 | 2017-10-03 | General Electric Company | Gas turbine fuel flow measurement using inert gas |
| RU2511992C2 (ru) * | 2012-06-27 | 2014-04-10 | Николай Борисович Болотин | Форсуночный блок камеры сгорания гтд |
| US11326775B2 (en) | 2013-02-28 | 2022-05-10 | Raytheon Technologies Corporation | Variable swirl fuel nozzle |
| FR3003013B1 (fr) * | 2013-03-05 | 2016-07-29 | Snecma | Dispositif de dosage compact pour injecteur a deux circuits de carburant, de preference pour turbomachine d'aeronef |
| EP3401529A1 (en) | 2013-03-14 | 2018-11-14 | United Technologies Corporation | Hollow-wall heat shield for fuel injector component |
| EP2789915A1 (en) * | 2013-04-10 | 2014-10-15 | Alstom Technology Ltd | Method for operating a combustion chamber and combustion chamber |
| FR3031798B1 (fr) | 2015-01-20 | 2018-08-10 | Safran Aircraft Engines | Systeme d'injection de carburant pour turbomachine d'aeronef, comprenant un canal de traversee d'air a section variable |
| US9927126B2 (en) | 2015-06-10 | 2018-03-27 | General Electric Company | Prefilming air blast (PAB) pilot for low emissions combustors |
| US10184665B2 (en) | 2015-06-10 | 2019-01-22 | General Electric Company | Prefilming air blast (PAB) pilot having annular splitter surrounding a pilot fuel injector |
| FR3043173B1 (fr) * | 2015-10-29 | 2017-12-22 | Snecma | Systeme d'injection aerodynamique pour turbomachine d'aeronef, a melange air/carburant ameliore |
| ES2645299B1 (es) * | 2016-06-03 | 2018-09-12 | Bsh Electrodomésticos España, S.A. | Quemador de gas y aparato de cocción doméstico |
| US10520195B2 (en) * | 2017-06-09 | 2019-12-31 | General Electric Company | Effervescent atomizing structure and method of operation for rotating detonation propulsion system |
| FR3105985B1 (fr) * | 2020-01-03 | 2023-11-24 | Safran Aircraft Engines | Circuit multipoint d’injecteur amélioré |
| FR3139378A1 (fr) * | 2022-09-05 | 2024-03-08 | Safran | Dispositif et procede d’injection de melange hydrogene-air pour bruleur de turbomachine |
| CN116878026B (zh) * | 2023-07-25 | 2025-07-22 | 新奥能源动力科技（上海）有限公司 | 一种燃烧器组件及燃烧装置 |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1421399A (en) * | 1972-11-13 | 1976-01-14 | Snecma | Fuel injectors |
| FR2235274B1 (enExample) * | 1973-06-28 | 1976-09-17 | Snecma | |
| GB1537671A (en) * | 1975-04-25 | 1979-01-04 | Rolls Royce | Fuel injectors for gas turbine engines |
| SU846929A1 (ru) * | 1977-11-16 | 1981-07-15 | Казанское Высшее Военное Инженерноеучилище | Смеситель двух потоков |
| US4189914A (en) * | 1978-06-19 | 1980-02-26 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Supercritical fuel injection system |
| US4443180A (en) * | 1981-05-11 | 1984-04-17 | Honeywell Inc. | Variable firing rate oil burner using aeration throttling |
| ZA841679B (en) * | 1983-03-10 | 1984-10-31 | Fuel Tech Inc | Catalyst system for delivering catalytic material to a selected portion of a combustion chamber |
| GB2169695B (en) * | 1984-12-20 | 1989-06-28 | Gen Electric | Gas turbine engine |
| FR2662377B1 (fr) * | 1990-05-23 | 1994-06-03 | Total France | Procede et dispositif de pulverisation de liquide, ainsi que leurs applications. |
| US5170727A (en) * | 1991-03-29 | 1992-12-15 | Union Carbide Chemicals & Plastics Technology Corporation | Supercritical fluids as diluents in combustion of liquid fuels and waste materials |
| DE19653059A1 (de) * | 1996-12-19 | 1998-06-25 | Asea Brown Boveri | Verfahren zum Betrieb eines Brenners |
| JP2002508242A (ja) * | 1997-12-17 | 2002-03-19 | ユニバーシィダッド デ セビリヤ | 燃料噴射ノズルおよびその使用方法 |
| RU2161719C2 (ru) * | 1999-02-23 | 2001-01-10 | Федеральное государственное унитарное предприятие Конструкторское бюро химавтоматики | Соосно-струйная форсунка |
| FR2826102B1 (fr) * | 2001-06-19 | 2004-01-02 | Snecma Moteurs | Perfectionnements apportes aux chambres de combustion de turbine a gaz |
| FR2832493B1 (fr) * | 2001-11-21 | 2004-07-09 | Snecma Moteurs | Systeme d'injection multi-etages d'un melange air/carburant dans une chambre de combustion de turbomachine |
| EP1319896A3 (en) * | 2001-12-14 | 2004-05-12 | R. Jan Mowill | Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities |
| RU2215242C2 (ru) * | 2001-12-17 | 2003-10-27 | Открытое акционерное общество "Авиадвигатель" | Камера сгорания турбомашины |
| JP3584289B2 (ja) * | 2002-01-21 | 2004-11-04 | 独立行政法人 宇宙航空研究開発機構 | 液体微粒化ノズル |
-
2004
- 2004-09-23 FR FR0410052A patent/FR2875585B1/fr not_active Expired - Fee Related
-
2005
- 2005-09-09 DE DE602005001742T patent/DE602005001742T2/de not_active Expired - Lifetime
- 2005-09-09 EP EP05291869A patent/EP1640661B1/fr not_active Expired - Lifetime
- 2005-09-21 US US11/230,640 patent/US7506496B2/en active Active
- 2005-09-22 JP JP2005275038A patent/JP4695952B2/ja not_active Expired - Lifetime
- 2005-09-22 RU RU2005129655/06A patent/RU2309329C2/ru active
- 2005-09-23 CN CNB2005101069062A patent/CN100545433C/zh not_active Expired - Lifetime