CN100545433C - 将混合物喷射到涡轮机燃烧室的泡腾空气动力系统 - Google Patents

将混合物喷射到涡轮机燃烧室的泡腾空气动力系统 Download PDF

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Publication number
CN100545433C
CN100545433C CNB2005101069062A CN200510106906A CN100545433C CN 100545433 C CN100545433 C CN 100545433C CN B2005101069062 A CNB2005101069062 A CN B2005101069062A CN 200510106906 A CN200510106906 A CN 200510106906A CN 100545433 C CN100545433 C CN 100545433C
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China
Prior art keywords
fuel
air
tubular structure
gas
passage
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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.)
Expired - Lifetime
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CNB2005101069062A
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English (en)
Chinese (zh)
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CN1769654A (zh
Inventor
伊戈尔·曼特什科夫
托马斯·诺埃尔
亚历山大·诺维科夫
弗拉基米尔·奥尔洛夫
瓦莱里·皮卡洛夫
吉勒·罗兰
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Safran Aircraft Engines SAS
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SNECMA SAS
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Publication of CN1769654A publication Critical patent/CN1769654A/zh
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Publication of CN100545433C publication Critical patent/CN100545433C/zh
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Expired - Lifetime legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/16—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour in which an emulsion of water and fuel is sprayed

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Nozzles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CNB2005101069062A 2004-09-23 2005-09-23 将混合物喷射到涡轮机燃烧室的泡腾空气动力系统 Expired - Lifetime CN100545433C (zh)

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 (2)

Publication Number Publication Date
CN1769654A CN1769654A (zh) 2006-05-10
CN100545433C true CN100545433C (zh) 2009-09-30

Family

ID=34949669

Family Applications (1)

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CNB2005101069062A Expired - Lifetime CN100545433C (zh) 2004-09-23 2005-09-23 将混合物喷射到涡轮机燃烧室的泡腾空气动力系统

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)

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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

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GB1421399A (en) * 1972-11-13 1976-01-14 Snecma Fuel injectors
FR2235274B1 (enExample) * 1973-06-28 1976-09-17 Snecma
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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

Also Published As

Publication number Publication date
US7506496B2 (en) 2009-03-24
RU2005129655A (ru) 2007-03-27
EP1640661A3 (fr) 2006-04-19
CN1769654A (zh) 2006-05-10
FR2875585A1 (fr) 2006-03-24
JP2006090327A (ja) 2006-04-06
US20060059914A1 (en) 2006-03-23
DE602005001742T2 (de) 2008-04-30
EP1640661B1 (fr) 2007-07-25
DE602005001742D1 (de) 2007-09-06
RU2309329C2 (ru) 2007-10-27
EP1640661A2 (fr) 2006-03-29
JP4695952B2 (ja) 2011-06-08
FR2875585B1 (fr) 2006-12-08

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Granted publication date: 20090930