JP2003106529A5 - - Google Patents

Download PDF

Info

Publication number
JP2003106529A5
JP2003106529A5 JP2002241496A JP2002241496A JP2003106529A5 JP 2003106529 A5 JP2003106529 A5 JP 2003106529A5 JP 2002241496 A JP2002241496 A JP 2002241496A JP 2002241496 A JP2002241496 A JP 2002241496A JP 2003106529 A5 JP2003106529 A5 JP 2003106529A5
Authority
JP
Japan
Prior art keywords
combustion chamber
head
take
pilot
nozzle
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.)
Granted
Application number
JP2002241496A
Other languages
English (en)
Japanese (ja)
Other versions
JP4038094B2 (ja
JP2003106529A (ja
Filing date
Publication date
Priority claimed from FR0111190A external-priority patent/FR2829228B1/fr
Application filed filed Critical
Publication of JP2003106529A publication Critical patent/JP2003106529A/ja
Publication of JP2003106529A5 publication Critical patent/JP2003106529A5/ja
Application granted granted Critical
Publication of JP4038094B2 publication Critical patent/JP4038094B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

JP2002241496A 2001-08-28 2002-08-22 ２つのオフセットされたヘッドを備えた環状燃焼室 Expired - Fee Related JP4038094B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0111190 2001-08-28
FR0111190A FR2829228B1 (fr) 2001-08-28 2001-08-28 Chambre de combustion annulaire a double tete etagee

Publications (3)

Publication Number Publication Date
JP2003106529A JP2003106529A (ja) 2003-04-09
JP2003106529A5 true JP2003106529A5 (https=) 2005-09-15
JP4038094B2 JP4038094B2 (ja) 2008-01-23

Family

ID=8866786

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002241496A Expired - Fee Related JP4038094B2 (ja) 2001-08-28 2002-08-22 ２つのオフセットされたヘッドを備えた環状燃焼室

Country Status (10)

Country Link
US (1) US20040011058A1 (https=)
EP (1) EP1288579B1 (https=)
JP (1) JP4038094B2 (https=)
CN (1) CN1407279A (https=)
CA (1) CA2398669C (https=)
DE (1) DE60225095T2 (https=)
ES (1) ES2300426T3 (https=)
FR (1) FR2829228B1 (https=)
RU (1) RU2296917C2 (https=)
UA (2) UA80669C2 (https=)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6898938B2 (en) * 2003-04-24 2005-05-31 General Electric Company Differential pressure induced purging fuel injector with asymmetric cyclone
US7013649B2 (en) * 2004-05-25 2006-03-21 General Electric Company Gas turbine engine combustor mixer
FR2920032B1 (fr) * 2007-08-13 2014-08-22 Snecma Diffuseur d'une turbomachine
EP2241808B1 (en) * 2007-11-29 2016-02-17 United Technologies Corporation Method of operation a gas turbine engine
US20100095649A1 (en) * 2008-10-20 2010-04-22 General Electric Company Staged combustion systems and methods
US8745989B2 (en) * 2009-04-09 2014-06-10 Pratt & Whitney Canada Corp. Reverse flow ceramic matrix composite combustor
US9068751B2 (en) * 2010-01-29 2015-06-30 United Technologies Corporation Gas turbine combustor with staged combustion
FR2958014B1 (fr) 2010-03-23 2013-12-13 Snecma Chambre de combustion a injecteurs decales longitudinalement sur une meme couronne
FR2979005B1 (fr) * 2011-08-09 2015-04-03 Snecma Systemes d'injection de carburant pour turbomachine d'aeronef a permeabilites differenciees
FR2982010B1 (fr) * 2011-10-26 2013-11-08 Snecma Chambre de combustion annulaire dans une turbomachine
EP2629008A1 (en) 2012-02-15 2013-08-21 Siemens Aktiengesellschaft Inclined fuel injection of fuel into a swirler slot
RU2493491C1 (ru) * 2012-04-26 2013-09-20 Федеральное государственное бюджетное учреждение науки Институт химической физики им. Н.Н. Семенова Российской академии наук (ИХФ РАН) Способ сжигания топлива в камере сгорания газотурбинной установки и устройство для его реализации
RU2493494C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2493493C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2493492C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд и форсуночный модуль
RU2493495C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2511977C2 (ru) * 2012-06-27 2014-04-10 Николай Борисович Болотин Форсуночный блок камеры сгорания гтд
EP3008391B1 (en) 2013-06-11 2020-05-06 United Technologies Corporation Combustor with axial staging for a gas turbine engine
US9803555B2 (en) * 2014-04-23 2017-10-31 General Electric Company Fuel delivery system with moveably attached fuel tube
GB201701380D0 (en) 2016-12-20 2017-03-15 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal
CN113137630B (zh) * 2021-04-19 2022-05-31 杭州汽轮动力集团有限公司 一种双重抑制热声振荡的燃气轮机燃烧室
CN114992675A (zh) * 2022-05-19 2022-09-02 沈阳航空航天大学 一种航空发动机燃烧室及其组织燃烧的方法
US20240401807A1 (en) * 2023-05-31 2024-12-05 General Electric Company Turbine engine including a combustor
CN118129182A (zh) * 2024-03-29 2024-06-04 中国航发湖南动力机械研究所 一种抗进气畸变火焰筒及燃烧室

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4498288A (en) * 1978-10-13 1985-02-12 General Electric Company Fuel injection staged sectoral combustor for burning low-BTU fuel gas
US4292801A (en) * 1979-07-11 1981-10-06 General Electric Company Dual stage-dual mode low nox combustor
US5749219A (en) * 1989-11-30 1998-05-12 United Technologies Corporation Combustor with first and second zones
US5197289A (en) * 1990-11-26 1993-03-30 General Electric Company Double dome combustor
CA2089302C (en) * 1992-03-30 2004-07-06 Joseph Frank Savelli Double annular combustor
RU2083926C1 (ru) * 1993-04-13 1997-07-10 Виноградов Евгений Дмитриевич Фронтовое устройство камеры сгорания
FR2727193B1 (fr) * 1994-11-23 1996-12-20 Snecma Chambre de combustion a deux tetes fonctionnant du ralenti au plein gaz
DE19720402A1 (de) * 1997-05-15 1998-11-19 Bmw Rolls Royce Gmbh Axial gestufte Ringbrennkammer einer Gasturbine
DE19745683A1 (de) * 1997-10-16 1999-04-22 Bmw Rolls Royce Gmbh Aufhängung einer ringförmigen Gasturbinen-Brennkammer
FR2770283B1 (fr) * 1997-10-29 1999-11-19 Snecma Chambre de combustion pour turbomachine
GB9917957D0 (en) * 1999-07-31 1999-09-29 Rolls Royce Plc A combustor arrangement
FR2826102B1 (fr) * 2001-06-19 2004-01-02 Snecma Moteurs Perfectionnements apportes aux chambres de combustion de turbine a gaz

Similar Documents

Publication Publication Date Title
JP2003106529A5 (https=)
US4222243A (en) Fuel burners for gas turbine engines
JP4038094B2 (ja) ２つのオフセットされたヘッドを備えた環状燃焼室
EP1413830B1 (en) Piloted airblast fuel injector with modified air splitter
EP3126741B1 (en) Pre-film liquid fuel cartridge
CN101526227B (zh) 具有冠状混合孔的燃烧帽
US9951955B2 (en) Annular combustion chamber for a turbine engine
US6474569B1 (en) Fuel injector
JP5930731B2 (ja) ガスタービンエンジン用の燃焼器、およびガスタービンエンジンの燃焼器の運転方法
US3886736A (en) Combustion apparatus for gas turbine
US2404335A (en) Liquid fuel burner, vaporizer, and combustion engine
EP0800041B1 (en) Gas turbine engine combustion equipment
US4107918A (en) Combustion assembly
US4170108A (en) Fuel injectors for gas turbine engines
EP2589877A2 (en) Multipoint fuel injection arrangements
JP2001324144A (ja) ガスタービン燃焼器
CN108351104B (zh) 用于飞行器涡轮发动机的具有改进的空气/燃料混合的空气动力学喷射系统
EP2772690B1 (en) Fuel nozzle with discrete jet inner air swirler
US3530667A (en) Fuel injector for gas turbine engines
US10161634B2 (en) Airblast fuel injector
US3483699A (en) Fuel injector for a gas turbine engine
JP2017524891A (ja) デュアルオリフィス噴霧器を備える多機能燃料ノズル
US5479774A (en) Combustion chamber assembly in a gas turbine engine
US4187674A (en) Combustion equipment for gas turbine engines
GB2106632A (en) Fuel and gas mixing