FR2896030B1 - Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur - Google Patents

Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur

Info

Publication number
FR2896030B1
FR2896030B1 FR0650069A FR0650069A FR2896030B1 FR 2896030 B1 FR2896030 B1 FR 2896030B1 FR 0650069 A FR0650069 A FR 0650069A FR 0650069 A FR0650069 A FR 0650069A FR 2896030 B1 FR2896030 B1 FR 2896030B1
Authority
FR
France
Prior art keywords
turboreactor
cooling
combustion chamber
injection device
multimode injection
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.)
Active
Application number
FR0650069A
Other languages
English (en)
Other versions
FR2896030A1 (fr
Inventor
Didier Hippolyte Hernandez
Thomas Noel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to FR0650069A priority Critical patent/FR2896030B1/fr
Priority to CA2572857A priority patent/CA2572857C/fr
Priority to US11/620,269 priority patent/US7891193B2/en
Priority to JP2007000529A priority patent/JP5008401B2/ja
Priority to EP07100253.9A priority patent/EP1806536B1/fr
Priority to CN2007100000961A priority patent/CN101000136B/zh
Priority to RU2007100426/06A priority patent/RU2431082C2/ru
Publication of FR2896030A1 publication Critical patent/FR2896030A1/fr
Application granted granted Critical
Publication of FR2896030B1 publication Critical patent/FR2896030B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F23D11/36—Details, e.g. burner cooling means, noise reduction 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/34—Feeding into different combustion zones
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00016—Preventing or reducing deposit build-up on burner parts, e.g. from carbon

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
FR0650069A 2006-01-09 2006-01-09 Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur Active FR2896030B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR0650069A FR2896030B1 (fr) 2006-01-09 2006-01-09 Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur
CA2572857A CA2572857C (fr) 2006-01-09 2007-01-04 Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur
JP2007000529A JP5008401B2 (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多モード燃料噴射器の冷却
US11/620,269 US7891193B2 (en) 2006-01-09 2007-01-05 Cooling of a multimode fuel injector for combustion chambers, in particular of a jet engine
EP07100253.9A EP1806536B1 (fr) 2006-01-09 2007-01-08 Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboréacteur
CN2007100000961A CN101000136B (zh) 2006-01-09 2007-01-09 燃烧室—特别是喷气发动机燃烧室—使用的多方式喷油器的冷却
RU2007100426/06A RU2431082C2 (ru) 2006-01-09 2007-01-09 Многорежимное устройство впрыска топлива, камера сгорания и турбореактивный двигатель

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0650069A FR2896030B1 (fr) 2006-01-09 2006-01-09 Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur

Publications (2)

Publication Number Publication Date
FR2896030A1 FR2896030A1 (fr) 2007-07-13
FR2896030B1 true FR2896030B1 (fr) 2008-04-18

Family

ID=36969177

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0650069A Active FR2896030B1 (fr) 2006-01-09 2006-01-09 Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur

Country Status (7)

Country Link
US (1) US7891193B2 (fr)
EP (1) EP1806536B1 (fr)
JP (1) JP5008401B2 (fr)
CN (1) CN101000136B (fr)
CA (1) CA2572857C (fr)
FR (1) FR2896030B1 (fr)
RU (1) RU2431082C2 (fr)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7513116B2 (en) * 2004-11-09 2009-04-07 Woodward Fst, Inc. Gas turbine engine fuel injector having a fuel swirler
GB2439097B (en) * 2006-06-15 2008-10-29 Rolls Royce Plc Fuel injector
FR2911667B1 (fr) * 2007-01-23 2009-10-02 Snecma Sa Systeme d'injection de carburant a double injecteur.
FR2919898B1 (fr) * 2007-08-10 2014-08-22 Snecma Injecteur multipoint pour turbomachine
GB2455729B (en) * 2007-12-19 2012-06-13 Rolls Royce Plc A fuel distribution apparatus
US8549859B2 (en) * 2008-07-28 2013-10-08 Siemens Energy, Inc. Combustor apparatus in a gas turbine engine
US8528340B2 (en) * 2008-07-28 2013-09-10 Siemens Energy, Inc. Turbine engine flow sleeve
US20100071377A1 (en) * 2008-09-19 2010-03-25 Fox Timothy A Combustor Apparatus for Use in a Gas Turbine Engine
JP4733195B2 (ja) 2009-04-27 2011-07-27 川崎重工業株式会社 ガスタービンエンジンの燃料噴霧装置
FR2951246B1 (fr) 2009-10-13 2011-11-11 Snecma Injecteur multi-point 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
US9151227B2 (en) * 2010-11-10 2015-10-06 Solar Turbines Incorporated End-fed liquid fuel gallery for a gas turbine fuel injector
FR2971039B1 (fr) 2011-02-02 2013-01-11 Turbomeca Injecteur de chambre de combustion de turbine a gaz a double circuit de carburant et chambre de combustion equipee d'au moins un tel injecteur
US9188063B2 (en) 2011-11-03 2015-11-17 Delavan Inc. Injectors for multipoint injection
US11015808B2 (en) * 2011-12-13 2021-05-25 General Electric Company Aerodynamically enhanced premixer with purge slots for reduced emissions
FR2996286B1 (fr) * 2012-09-28 2014-09-12 Snecma Dispositif d'injection pour une chambre de combustion de turbomachine
GB2516445A (en) * 2013-07-22 2015-01-28 Rolls Royce Plc A fuel spray nozzle
FR3013421B1 (fr) * 2013-11-20 2018-12-07 Safran Aircraft Engines Dispositif d'injection multipoint pour moteur d'aeronef
US10288293B2 (en) 2013-11-27 2019-05-14 General Electric Company Fuel nozzle with fluid lock and purge apparatus
CN104713128B (zh) * 2013-12-12 2018-09-11 中国航发商用航空发动机有限责任公司 喷嘴杆部、燃油喷嘴及航空发动机燃气轮机
US9995220B2 (en) 2013-12-20 2018-06-12 Pratt & Whitney Canada Corp. Fluid manifold for gas turbine engine and method for delivering fuel to a combustor using same
WO2015147934A1 (fr) 2013-12-23 2015-10-01 General Electric Company Structure d'injecteur de carburant pour injection à assistance pneumatique
CN105829802B (zh) * 2013-12-23 2018-02-23 通用电气公司 具有柔性支承结构的燃料喷嘴
JP6535442B2 (ja) * 2014-08-18 2019-06-26 川崎重工業株式会社 燃料噴射装置
US9897321B2 (en) * 2015-03-31 2018-02-20 Delavan Inc. Fuel nozzles
US10385809B2 (en) 2015-03-31 2019-08-20 Delavan Inc. Fuel nozzles
US10364751B2 (en) * 2015-08-03 2019-07-30 Delavan Inc Fuel staging
US9889418B2 (en) * 2015-09-29 2018-02-13 Dow Global Technologies Llc Fluidized fuel gas combustor system for a catalytic dehydrogenation process
US10876477B2 (en) 2016-09-16 2020-12-29 Delavan Inc Nozzles with internal manifolding
US11181269B2 (en) * 2018-11-15 2021-11-23 General Electric Company Involute trapped vortex combustor assembly
CN111981512B (zh) * 2020-07-31 2022-09-02 中国航发贵阳发动机设计研究所 一种燃油空气雾化装置
KR102498060B1 (ko) * 2021-04-12 2023-02-10 동우에이치에스티 주식회사 가스 공급유닛
CN114810424B (zh) * 2022-04-29 2024-02-02 西北工业大学 一种基于喷雾冷却的发动机主动冷却凹腔结构

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2172383A (en) * 1936-03-23 1939-09-12 Honn Harlan Verne Fuel injection device
GB1114728A (en) * 1967-03-20 1968-05-22 Rolls Royce Burner e.g. for a gas turbine engine combustion chamber
US3684186A (en) * 1970-06-26 1972-08-15 Ex Cell O Corp Aerating fuel nozzle
US4139157A (en) * 1976-09-02 1979-02-13 Parker-Hannifin Corporation Dual air-blast fuel nozzle
US4111369A (en) * 1977-07-05 1978-09-05 General Motors Corporation Fuel nozzle
US4798330A (en) * 1986-02-14 1989-01-17 Fuel Systems Textron Inc. Reduced coking of fuel nozzles
US4865542A (en) * 1988-02-17 1989-09-12 Shell Oil Company Partial combustion burner with spiral-flow cooled face
US5423178A (en) * 1992-09-28 1995-06-13 Parker-Hannifin Corporation Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle
FR2721694B1 (fr) * 1994-06-22 1996-07-19 Snecma Refroidissement de l'injecteur de décollage d'une chambre de combustion à deux têtes.
US6161387A (en) * 1998-10-30 2000-12-19 United Technologies Corporation Multishear fuel injector
US6321541B1 (en) * 1999-04-01 2001-11-27 Parker-Hannifin Corporation Multi-circuit multi-injection point atomizer
US6755024B1 (en) * 2001-08-23 2004-06-29 Delavan Inc. Multiplex injector
US6802178B2 (en) * 2002-09-12 2004-10-12 The Boeing Company Fluid injection and injection method
US6898926B2 (en) * 2003-01-31 2005-05-31 General Electric Company Cooled purging fuel injectors
JP2007162998A (ja) * 2005-12-13 2007-06-28 Kawasaki Heavy Ind Ltd ガスタービンエンジンの燃料噴霧装置

Also Published As

Publication number Publication date
CA2572857C (fr) 2014-10-21
JP2007183094A (ja) 2007-07-19
FR2896030A1 (fr) 2007-07-13
RU2431082C2 (ru) 2011-10-10
CN101000136A (zh) 2007-07-18
EP1806536B1 (fr) 2017-08-16
CA2572857A1 (fr) 2007-07-09
US7891193B2 (en) 2011-02-22
CN101000136B (zh) 2010-12-08
JP5008401B2 (ja) 2012-08-22
RU2007100426A (ru) 2008-07-20
US20070157616A1 (en) 2007-07-12
EP1806536A1 (fr) 2007-07-11

Similar Documents

Publication Publication Date Title
FR2896030B1 (fr) Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur
FR2896031B1 (fr) Dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur
FR2886714B1 (fr) Systeme d'injection anti-rotatif pour turbo-reacteur
FR2896303B1 (fr) Systeme et procede pour refroidir un injecteur de carburant etage a jet d'air.
EP1876332A4 (fr) Moteur diesel a injection directe
DE502005007594D1 (de) Brennstoffeinspritzvorrichtung
DE602007012704D1 (de) Dieselmotor mit direkteinspritzung
DE502005006014D1 (de) Kraftstoffeinspritzsystem
FR2865505B1 (fr) Dispositif d'injection de carburant empechant l'abrasion
FR2902063B1 (fr) Dispositif d'arrosage pour essuie-glace
DE602004016066D1 (de) Kraftstoffeinspritzsystem
DE502004007496D1 (de) Brennstoffeinspritzventil
EP1835143A4 (fr) Moteur diesel a injection directe
FR2933454B1 (fr) Module d'injection pour soupape d'injection
DE502005006051D1 (de) Kraftstoffeinspritzeinrichtung
DE502004005519D1 (de) Brennstoffeinspritzventil
FR2902840B1 (fr) Dispositif de demarrage pour moteur thermique
FR2918121B1 (fr) Injecteur de carburant a commutation rapide pour des pressions d'injection elevees
DE602004026189D1 (de) Kraftstoffeinspritzsteuervorrichtung für kraftstoffeinspritzpumpe
FR2897752B3 (fr) Dispositif de defeuillage, notamment pour ceps de vigne
FR2932096B1 (fr) Dispositif de securite pour un dispositif d'injection
DE502004010790D1 (de) Brennstoffeinspritzsystem
DE502004007150D1 (de) Brennstoffeinspritzventil
FR2906576B1 (fr) Agencement de refroidissement d'un injecteur comportant un empilement de rondelles.
FI20061113A0 (fi) Suihkutuslaite polttomoottoreille

Legal Events

Date Code Title Description
CL Concession to grant licences
PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16

PLFP Fee payment

Year of fee payment: 17

PLFP Fee payment

Year of fee payment: 18

PLFP Fee payment

Year of fee payment: 19