RU2296917C2 - Кольцевая камера сгорания с двумя головками, смещенными по отношению друг к другу - Google Patents

Кольцевая камера сгорания с двумя головками, смещенными по отношению друг к другу Download PDF

Info

Publication number
RU2296917C2
RU2296917C2 RU2002123305/06A RU2002123305A RU2296917C2 RU 2296917 C2 RU2296917 C2 RU 2296917C2 RU 2002123305/06 A RU2002123305/06 A RU 2002123305/06A RU 2002123305 A RU2002123305 A RU 2002123305A RU 2296917 C2 RU2296917 C2 RU 2296917C2
Authority
RU
Russia
Prior art keywords
combustion chamber
head
take
launch
total
Prior art date
Application number
RU2002123305/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2002123305A (ru
Inventor
Кристоф БОДУАН (FR)
Кристоф БОДУАН
Патрис-Андре КОММАРЕ (FR)
Патрис-Андре КОММАРЕ
ЛЕТТИ Эрик ЛЕ (FR)
ЛЕТТИ Эрик ЛЕ
Кристоф ВИГЬЕ (FR)
Кристоф ВИГЬЕ
Original Assignee
Снекма Моторс
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 Снекма Моторс filed Critical Снекма Моторс
Publication of RU2002123305A publication Critical patent/RU2002123305A/ru
Application granted granted Critical
Publication of RU2296917C2 publication Critical patent/RU2296917C2/ru

Links

Images

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)
RU2002123305/06A 2001-08-28 2002-08-27 Кольцевая камера сгорания с двумя головками, смещенными по отношению друг к другу RU2296917C2 (ru)

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 (2)

Publication Number Publication Date
RU2002123305A RU2002123305A (ru) 2004-03-10
RU2296917C2 true RU2296917C2 (ru) 2007-04-10

Family

ID=8866786

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002123305/06A RU2296917C2 (ru) 2001-08-28 2002-08-27 Кольцевая камера сгорания с двумя головками, смещенными по отношению друг к другу

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=)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2493493C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2493494C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
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
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
RU2608513C2 (ru) * 2011-10-26 2017-01-19 Снекма Кольцевая камера сгорания в турбомашине

Families Citing this family (17)

* 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
EP2629008A1 (en) 2012-02-15 2013-08-21 Siemens Aktiengesellschaft Inclined fuel injection of fuel into a swirler slot
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

Citations (3)

* 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
FR2727193A1 (fr) * 1994-11-23 1996-05-24 Snecma Chambre de combustion a deux tetes fonctionnant du ralenti au plein gaz
RU2083926C1 (ru) * 1993-04-13 1997-07-10 Виноградов Евгений Дмитриевич Фронтовое устройство камеры сгорания

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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

Patent Citations (4)

* 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
RU2083926C1 (ru) * 1993-04-13 1997-07-10 Виноградов Евгений Дмитриевич Фронтовое устройство камеры сгорания
FR2727193A1 (fr) * 1994-11-23 1996-05-24 Snecma Chambre de combustion a deux tetes fonctionnant du ralenti au plein gaz
US5642621A (en) * 1994-11-23 1997-07-01 Socoiete Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Dual head combustion chamber

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2608513C2 (ru) * 2011-10-26 2017-01-19 Снекма Кольцевая камера сгорания в турбомашине
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
RU2493493C1 (ru) * 2012-06-25 2013-09-20 Николай Борисович Болотин Камера сгорания гтд
RU2493494C1 (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

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
JP4038094B2 (ja) 2008-01-23
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

Similar Documents

Publication Publication Date Title
RU2296917C2 (ru) Кольцевая камера сгорания с двумя головками, смещенными по отношению друг к другу
US6708498B2 (en) Venturiless swirl cup
US6363726B1 (en) Mixer having multiple swirlers
US6381964B1 (en) Multiple annular combustion chamber swirler having atomizing pilot
RU2444680C2 (ru) Камера сгорания газотурбинного двигателя и газотурбинный двигатель
US6865889B2 (en) Method and apparatus to decrease combustor emissions
US6834505B2 (en) Hybrid swirler
US6367262B1 (en) Multiple annular swirler
US6952927B2 (en) Multiport dome baffle
US6272840B1 (en) Piloted airblast lean direct fuel injector
US9068748B2 (en) Axial stage combustor for gas turbine engines
US6474070B1 (en) Rich double dome combustor
US6609377B2 (en) Multiple injector combustor
CA2034431A1 (en) Lean staged combustion assembly
JPS6367085B2 (https=)
JP2003004232A (ja) ガスタービンエンジンの運転方法、燃焼器及びミキサ組立体
RU2439435C1 (ru) Топливовоздушный модуль фронтового устройства камеры сгорания гтд
JPH06213450A (ja) 燃料噴射ノズル
US5331814A (en) Gas turbine combustion chamber with multiple fuel injector arrays

Legal Events

Date Code Title Description
PD4A Correction of name of patent owner
PD4A Correction of name of patent owner