JP4038094B2 - ２つのオフセットされたヘッドを備えた環状燃焼室 - Google Patents

２つのオフセットされたヘッドを備えた環状燃焼室 Download PDF

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Publication number
JP4038094B2
JP4038094B2 JP2002241496A JP2002241496A JP4038094B2 JP 4038094 B2 JP4038094 B2 JP 4038094B2 JP 2002241496 A JP2002241496 A JP 2002241496A JP 2002241496 A JP2002241496 A JP 2002241496A JP 4038094 B2 JP4038094 B2 JP 4038094B2
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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.)
Expired - Fee Related
Application number
JP2002241496A
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English (en)
Japanese (ja)
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JP2003106529A (ja
JP2003106529A5 (https=
Inventor
クリストフ・ボドワン
パトリス−アンドレ・コマレ
エリツク・ル・レテイ
クリストフ・ビギエ
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Safran Aircraft Engines SAS
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SNECMA SAS
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Publication date
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Publication of JP2003106529A5 publication Critical patent/JP2003106529A5/ja
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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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05004—Special materials for walls or lining
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00004—Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Nozzles (AREA)
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 JP2003106529A5 (https=) 2005-09-15
JP4038094B2 true 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

Also Published As

Publication number Publication date
CN1407279A (zh) 2003-04-02
EP1288579A1 (fr) 2003-03-05
UA79922C2 (uk) 2007-08-10
UA80669C2 (en) 2007-10-25
DE60225095D1 (de) 2008-04-03
US20040011058A1 (en) 2004-01-22
DE60225095T2 (de) 2009-03-05
CA2398669C (fr) 2010-11-30
FR2829228A1 (fr) 2003-03-07
EP1288579B1 (fr) 2008-02-20
CA2398669A1 (fr) 2003-02-28
RU2002123305A (ru) 2004-03-10
ES2300426T3 (es) 2008-06-16
JP2003106529A (ja) 2003-04-09
FR2829228B1 (fr) 2005-07-15
RU2296917C2 (ru) 2007-04-10

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