FR2971039B1 - 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 - Google Patents

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

Info

Publication number
FR2971039B1
FR2971039B1 FR1150807A FR1150807A FR2971039B1 FR 2971039 B1 FR2971039 B1 FR 2971039B1 FR 1150807 A FR1150807 A FR 1150807A FR 1150807 A FR1150807 A FR 1150807A FR 2971039 B1 FR2971039 B1 FR 2971039B1
Authority
FR
France
Prior art keywords
injector
circuit
combustion chamber
starting
gas turbine
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
FR1150807A
Other languages
English (en)
Other versions
FR2971039A1 (fr
Inventor
Bernard Joseph Jean Pierre Carrere
Jean Luc Dabat
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 Helicopter Engines SAS
Original Assignee
Turbomeca SA
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 FR1150807A priority Critical patent/FR2971039B1/fr
Application filed by Turbomeca SA filed Critical Turbomeca SA
Priority to RU2013139354/06A priority patent/RU2584741C2/ru
Priority to US13/982,608 priority patent/US9347667B2/en
Priority to JP2013552244A priority patent/JP5985514B2/ja
Priority to CN201280007105.9A priority patent/CN103354890B/zh
Priority to CA2825864A priority patent/CA2825864C/fr
Priority to ES12706638.9T priority patent/ES2686560T3/es
Priority to PL12706638T priority patent/PL2671028T3/pl
Priority to EP12706638.9A priority patent/EP2671028B1/fr
Priority to KR1020137022157A priority patent/KR101877591B1/ko
Priority to PCT/FR2012/050177 priority patent/WO2012104525A1/fr
Publication of FR2971039A1 publication Critical patent/FR2971039A1/fr
Application granted granted Critical
Publication of FR2971039B1 publication Critical patent/FR2971039B1/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
    • 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
    • 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
    • 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
    • F23D11/101—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 medium and fuel meeting before the burner outlet
    • F23D11/102—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 medium and fuel meeting before the burner outlet in an internal mixing chamber
    • F23D11/103—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 medium and fuel meeting before the burner outlet in an internal mixing chamber with means creating a swirl inside the mixing chamber
    • 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
    • F23D11/106—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 medium and fuel meeting at the burner outlet
    • F23D11/107—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 medium and fuel meeting at the burner outlet at least one of both being subjected to a swirling motion
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23D2900/00014—Pilot burners specially adapted for ignition of main burners in furnaces or gas turbines
    • 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
    • F23D2900/00015—Pilot burners specially adapted for low load or transient conditions, e.g. for increasing stability
    • 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)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR1150807A 2011-02-02 2011-02-02 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 Active FR2971039B1 (fr)

Priority Applications (11)

Application Number Priority Date Filing Date Title
FR1150807A FR2971039B1 (fr) 2011-02-02 2011-02-02 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
EP12706638.9A EP2671028B1 (fr) 2011-02-02 2012-01-27 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
JP2013552244A JP5985514B2 (ja) 2011-02-02 2012-01-27 デュアル燃料回路を有するガスタービンの燃焼室用の噴射装置および少なくとも１つのそのような噴射装置が設けられた燃焼室
CN201280007105.9A CN103354890B (zh) 2011-02-02 2012-01-27 用于燃气涡轮机燃烧室的具有双燃料回路的喷射器及具有至少一个该喷射器的燃烧室
CA2825864A CA2825864C (fr) 2011-02-02 2012-01-27 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
ES12706638.9T ES2686560T3 (es) 2011-02-02 2012-01-27 Inyector de cámara de combustión de turbina de gas con circuito doble de combustible y cámara de combustión equipada con al menos un inyector de este tipo
RU2013139354/06A RU2584741C2 (ru) 2011-02-02 2012-01-27 Инжектор камеры сгорания газовой турбины с двойной топливной системой и камера сгорания, снабженная, по меньшей мере, одним таким инжектором
US13/982,608 US9347667B2 (en) 2011-02-02 2012-01-27 Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector
KR1020137022157A KR101877591B1 (ko) 2011-02-02 2012-01-27 이중 연료 회로를 가진 가스터빈의 연소실을 위한 인젝터 및 적어도 한 개의 상기 이중 회로 인젝터를 가진 연소실
PCT/FR2012/050177 WO2012104525A1 (fr) 2011-02-02 2012-01-27 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
PL12706638T PL2671028T3 (pl) 2011-02-02 2012-01-27 Wtryskiwacz komory spalania turbiny gazowej z podwójnym obwodem paliwa i komora spalania wyposażona w co najmniej jeden taki wtryskiwacz

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1150807A FR2971039B1 (fr) 2011-02-02 2011-02-02 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

Publications (2)

Publication Number Publication Date
FR2971039A1 FR2971039A1 (fr) 2012-08-03
FR2971039B1 true FR2971039B1 (fr) 2013-01-11

Family

ID=45774260

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1150807A Active FR2971039B1 (fr) 2011-02-02 2011-02-02 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

Country Status (11)

Country Link
US (1) US9347667B2 (fr)
EP (1) EP2671028B1 (fr)
JP (1) JP5985514B2 (fr)
KR (1) KR101877591B1 (fr)
CN (1) CN103354890B (fr)
CA (1) CA2825864C (fr)
ES (1) ES2686560T3 (fr)
FR (1) FR2971039B1 (fr)
PL (1) PL2671028T3 (fr)
RU (1) RU2584741C2 (fr)
WO (1) WO2012104525A1 (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2996289B1 (fr) * 2012-10-01 2018-10-12 Turbomeca Chambre de combustion comprenant un tube a flamme fixe au moyen de trois elements de centrage.
FR2996288B1 (fr) * 2012-10-01 2014-09-12 Turbomeca Injecteur a double circuit de chambre de combustion de turbomachine.
FR3001525B1 (fr) * 2013-01-29 2016-12-09 Turbomeca Procede de gestion de la consommation de carburant d un ensemble bimoteur et ensemble associe
FR3001497B1 (fr) * 2013-01-29 2016-05-13 Turbomeca Ensemble de combustion de turbomachine comprenant un circuit d alimentation de carburant ameliore
WO2014171991A2 (fr) * 2013-02-01 2014-10-23 United Technologies Corporation Injecteur de carburant pour démarrage et fonctionnement à haute altitude d'un moteur à turbine à gaz
US9404422B2 (en) * 2013-05-23 2016-08-02 Honeywell International Inc. Gas turbine fuel injector having flow guide for receiving air flow
EP3022492A4 (fr) * 2013-07-15 2017-02-22 Hamilton Sundstrand Corporation Système, appareil et procédé de combustion
US9625156B2 (en) * 2013-10-30 2017-04-18 Honeywell International Inc. Gas turbine engines having fuel injector shrouds with interior ribs
FR3017693B1 (fr) * 2014-02-19 2019-07-26 Safran Helicopter Engines Chambre de combustion de turbomachine
CN104019475A (zh) * 2014-06-23 2014-09-03 叶祖湘 一种装有燃烧机系统的大小灶具
FR3050255B1 (fr) * 2016-04-13 2019-10-25 Safran Helicopter Engines Injecteurs ameliores pour chambre de combustion de turbine a gaz
FR3059047B1 (fr) * 2016-11-21 2020-08-28 Safran Helicopter Engines Injecteur de chambre de combustion pour une turbomachine et son procede de fabrication
FR3067444B1 (fr) * 2017-06-12 2019-12-27 Safran Helicopter Engines Architecture de combustion de carburant de turbomachine comportant des moyens de deflexion
FR3068113B1 (fr) 2017-06-27 2019-08-23 Safran Helicopter Engines Injecteur de carburant a jet plat pour une turbomachine d'aeronef
US10816211B2 (en) 2017-08-25 2020-10-27 Honeywell International Inc. Axially staged rich quench lean combustion system
FR3081211B1 (fr) * 2018-05-16 2021-02-26 Safran Aircraft Engines Ensemble pour une chambre de combustion de turbomachine
CN109185924B (zh) * 2018-08-03 2023-09-12 新奥能源动力科技（上海）有限公司 燃烧室的头部装置、燃烧室及燃气轮机
CN109185923B (zh) * 2018-08-03 2023-09-12 新奥能源动力科技（上海）有限公司 一种燃烧室头部装置、燃烧室及燃气轮机
FR3087250B1 (fr) 2018-10-11 2020-09-25 Safran Helicopter Engines Injecteur de carburant monobloc a jet plat pour une turbomachine d'aeronef et son procede de fabrication
RU187491U1 (ru) * 2018-11-15 2019-03-11 Публичное Акционерное Общество "Одк-Сатурн" Испарительная камера сгорания газотурбинного двигателя
FR3099231B1 (fr) 2019-07-24 2022-08-12 Safran Helicopter Engines Injecteur de carburant a circuit de purge pour une turbomachine d’aeronef
US11988386B2 (en) 2021-12-03 2024-05-21 Honeywell International Inc. Gas turbine engine injector module with thermally coupled fuel lines having respective outlets
US12117174B2 (en) * 2023-02-14 2024-10-15 Collins Engine Nozzles, Inc. Combustor section support structures

Family Cites Families (11)

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Publication number Priority date Publication date Assignee Title
US4817389A (en) * 1987-09-24 1989-04-04 United Technologies Corporation Fuel injection system
SU1560923A1 (ru) * 1988-06-29 1990-04-30 Войсковая часть 27177 Камера сгорани газотурбинного двигател
US7513116B2 (en) * 2004-11-09 2009-04-07 Woodward Fst, Inc. Gas turbine engine fuel injector having a fuel swirler
JP3958767B2 (ja) * 2005-03-18 2007-08-15 川崎重工業株式会社 ガスタービン燃焼器およびその着火方法
US7624576B2 (en) * 2005-07-18 2009-12-01 Pratt & Whitney Canada Corporation Low smoke and emissions fuel nozzle
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
US20070193272A1 (en) * 2006-02-21 2007-08-23 Woodward Fst, Inc. Gas turbine engine fuel injector
FR2906868B1 (fr) * 2006-10-06 2011-11-18 Snecma Injecteur de carburant pour chambre de combustion de moteur a turbine a gaz
US7908864B2 (en) * 2006-10-06 2011-03-22 General Electric Company Combustor nozzle for a fuel-flexible combustion system
FR2911667B1 (fr) * 2007-01-23 2009-10-02 Snecma Sa Systeme d'injection de carburant a double injecteur.
US9513009B2 (en) * 2009-02-18 2016-12-06 Rolls-Royce Plc Fuel nozzle having aerodynamically shaped helical turning vanes

Also Published As

Publication number Publication date
JP5985514B2 (ja) 2016-09-06
KR20140008350A (ko) 2014-01-21
FR2971039A1 (fr) 2012-08-03
EP2671028A1 (fr) 2013-12-11
CN103354890B (zh) 2016-06-29
CA2825864C (fr) 2019-05-21
JP2014504696A (ja) 2014-02-24
CN103354890A (zh) 2013-10-16
ES2686560T3 (es) 2018-10-18
EP2671028B1 (fr) 2018-07-25
CA2825864A1 (fr) 2012-09-09
WO2012104525A1 (fr) 2012-08-09
RU2013139354A (ru) 2015-03-10
KR101877591B1 (ko) 2018-07-12
US20130305726A1 (en) 2013-11-21
RU2584741C2 (ru) 2016-05-20
PL2671028T3 (pl) 2018-11-30
US9347667B2 (en) 2016-05-24

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