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FR2951245B1 - Dispositif d'injection multi-point pour une chambre de combustion de turbomachine - Google Patents

Dispositif d'injection multi-point pour une chambre de combustion de turbomachine

Info

Publication number
FR2951245B1
FR2951245B1 FR0904906A FR0904906A FR2951245B1 FR 2951245 B1 FR2951245 B1 FR 2951245B1 FR 0904906 A FR0904906 A FR 0904906A FR 0904906 A FR0904906 A FR 0904906A FR 2951245 B1 FR2951245 B1 FR 2951245B1
Authority
FR
France
Prior art keywords
annular
combustion chamber
injection device
front face
point 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.)
Expired - Fee Related
Application number
FR0904906A
Other languages
English (en)
Other versions
FR2951245A1 (fr
Inventor
Didier Hippolyte Hernandez
Emilie Lachaud
Thomas Olivier Marie 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
Priority to FR0904906A priority Critical patent/FR2951245B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to CA2776848A priority patent/CA2776848C/fr
Priority to US13/501,526 priority patent/US9003802B2/en
Priority to JP2012533670A priority patent/JP5616456B2/ja
Priority to CN201080046194.9A priority patent/CN102575843B/zh
Priority to RU2012119598/06A priority patent/RU2539223C2/ru
Priority to EP10778699.8A priority patent/EP2488791B1/fr
Priority to PCT/FR2010/052101 priority patent/WO2011045503A1/fr
Priority to BR112012008509-3A priority patent/BR112012008509B1/pt
Publication of FR2951245A1 publication Critical patent/FR2951245A1/fr
Application granted granted Critical
Publication of FR2951245B1 publication Critical patent/FR2951245B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36—Details
    • 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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

Dispositif d'injection de carburant pour une chambre annulaire de combustion de turbomachine, comprenant un circuit pilote alimentant un injecteur et un circuit multipoint alimentant des orifices d'injection (80) formés dans une face frontale (72) d'une couronne annulaire (74) montée dans une chambre annulaire (78), et moyens d'isolation thermique de cette face frontale (72), comprenant une cavité annulaire (70) formée autour des orifices d'injection entre la face frontale (72) de la couronne annulaire et une paroi frontale (76) de la chambre annulaire (78) et destinée à être remplie en fonctionnement d'air ou de carburant cokéfié.
FR0904906A 2009-10-13 2009-10-13 Dispositif d'injection multi-point pour une chambre de combustion de turbomachine Expired - Fee Related FR2951245B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0904906A FR2951245B1 (fr) 2009-10-13 2009-10-13 Dispositif d'injection multi-point pour une chambre de combustion de turbomachine
US13/501,526 US9003802B2 (en) 2009-10-13 2010-10-06 Multipoint injection device for a combustion chamber of a turbine engine
JP2012533670A JP5616456B2 (ja) 2009-10-13 2010-10-06 タービンエンジンの燃焼室のための多点式噴射装置
CN201080046194.9A CN102575843B (zh) 2009-10-13 2010-10-06 用于涡轮发动机燃烧室的多点喷油装置
CA2776848A CA2776848C (fr) 2009-10-13 2010-10-06 Dispositif d'injection multi-point pour une chambre de combustion de turbomachine
RU2012119598/06A RU2539223C2 (ru) 2009-10-13 2010-10-06 Устройство многоточечного впрыска для камеры сгорания турбомашины
EP10778699.8A EP2488791B1 (fr) 2009-10-13 2010-10-06 Dispositif d'injection multi-point pour une chambre de combustion de turbomachine
PCT/FR2010/052101 WO2011045503A1 (fr) 2009-10-13 2010-10-06 Dispositif d'injection multi-point pour une chambre de combustion de turbomachine
BR112012008509-3A BR112012008509B1 (pt) 2009-10-13 2010-10-06 Dispositivo de injeção de combustível para uma câmara anular de combustão de turbomáquina, e, câmara anular de combustão de turbomáquina

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0904906A FR2951245B1 (fr) 2009-10-13 2009-10-13 Dispositif d'injection multi-point pour une chambre de combustion de turbomachine

Publications (2)

Publication Number Publication Date
FR2951245A1 FR2951245A1 (fr) 2011-04-15
FR2951245B1 true FR2951245B1 (fr) 2013-05-17

Family

ID=42124636

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0904906A Expired - Fee Related FR2951245B1 (fr) 2009-10-13 2009-10-13 Dispositif d'injection multi-point pour une chambre de combustion de turbomachine

Country Status (9)

Country Link
US (1) US9003802B2 (fr)
EP (1) EP2488791B1 (fr)
JP (1) JP5616456B2 (fr)
CN (1) CN102575843B (fr)
BR (1) BR112012008509B1 (fr)
CA (1) CA2776848C (fr)
FR (1) FR2951245B1 (fr)
RU (1) RU2539223C2 (fr)
WO (1) WO2011045503A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11840994B2 (en) 2018-07-25 2023-12-12 Safran Aircraft Engines Multipoint fuel injection device

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013201232A1 (de) * 2013-01-25 2014-07-31 Siemens Aktiengesellschaft Brenner mit einer zentralen Brennstoffzufuhranordnung
US10859269B2 (en) 2017-03-31 2020-12-08 Delavan Inc. Fuel injectors for multipoint arrays
CN107238106B (zh) * 2017-06-10 2020-01-24 北京航空航天大学 一种用于多点喷射燃烧室的多层环形油轨
WO2019126434A1 (fr) * 2017-12-20 2019-06-27 Wrightspeed, Inc. Évaporation contrôlée de combustibles liquides pour moteurs à turbine
GB201909167D0 (en) 2019-06-26 2019-08-07 Rolls Royce Plc Fuel injector
FR3099546B1 (fr) 2019-07-29 2021-08-06 Safran Aircraft Engines Chambre de combustion comportant des systèmes d'injection secondaires injectant de l'air et du carburant directement dans des zones de recirculation de coin, turbomachine la comprenant, et procédé d'alimentation en carburant de celle-ci
FR3115075B1 (fr) * 2020-10-14 2022-10-21 Safran Aircraft Engines Circuit d’alimentation en carburant pour une chambre de combustion de turbomachine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2596102B1 (fr) 1986-03-20 1988-05-27 Snecma Dispositif d'injection a vrille axialo-centripete
US5253478A (en) * 1991-12-30 1993-10-19 General Electric Company Flame holding diverging centerbody cup construction for a dry low NOx combustor
US6718770B2 (en) * 2002-06-04 2004-04-13 General Electric Company Fuel injector laminated fuel strip
US6898938B2 (en) * 2003-04-24 2005-05-31 General Electric Company Differential pressure induced purging fuel injector with asymmetric cyclone
US7051532B2 (en) * 2003-10-17 2006-05-30 General Electric Company Methods and apparatus for film cooling gas turbine engine combustors
US7788927B2 (en) * 2005-11-30 2010-09-07 General Electric Company Turbine engine fuel nozzles and methods of assembling the same
FR2896031B1 (fr) * 2006-01-09 2008-04-18 Snecma Sa Dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur
FR2896030B1 (fr) * 2006-01-09 2008-04-18 Snecma Sa Refroidissement d'un dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur
US7506510B2 (en) * 2006-01-17 2009-03-24 Delavan Inc System and method for cooling a staged airblast fuel injector
GB2434437B (en) * 2006-01-19 2011-01-26 Siemens Ag Improvements in or relating to combustion apparatus
US20090014561A1 (en) * 2007-07-15 2009-01-15 General Electric Company Components capable of transporting liquids manufactured using injection molding
FR2919898B1 (fr) 2007-08-10 2014-08-22 Snecma Injecteur multipoint pour turbomachine
US8061142B2 (en) * 2008-04-11 2011-11-22 General Electric Company Mixer for a combustor
US8387391B2 (en) * 2010-12-17 2013-03-05 General Electric Company Aerodynamically enhanced fuel nozzle
JP5631223B2 (ja) * 2011-01-14 2014-11-26 三菱重工業株式会社 燃料ノズル、これを備えたガスタービン燃焼器およびこれを備えたガスタービン

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11840994B2 (en) 2018-07-25 2023-12-12 Safran Aircraft Engines Multipoint fuel injection device

Also Published As

Publication number Publication date
BR112012008509B1 (pt) 2020-09-29
CA2776848A1 (fr) 2011-04-21
RU2539223C2 (ru) 2015-01-20
EP2488791B1 (fr) 2014-08-06
FR2951245A1 (fr) 2011-04-15
RU2012119598A (ru) 2013-11-20
US9003802B2 (en) 2015-04-14
US20120198853A1 (en) 2012-08-09
CN102575843A (zh) 2012-07-11
EP2488791A1 (fr) 2012-08-22
JP2013507600A (ja) 2013-03-04
WO2011045503A1 (fr) 2011-04-21
CA2776848C (fr) 2017-07-04
BR112012008509A2 (pt) 2016-04-05
CN102575843B (zh) 2014-12-24
JP5616456B2 (ja) 2014-10-29

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20160630