SE7412667L - - Google Patents

Info

Publication number
SE7412667L
SE7412667L SE7412667A SE7412667A SE7412667L SE 7412667 L SE7412667 L SE 7412667L SE 7412667 A SE7412667 A SE 7412667A SE 7412667 A SE7412667 A SE 7412667A SE 7412667 L SE7412667 L SE 7412667L
Authority
SE
Sweden
Prior art keywords
flow
hot
pilot
cooler
directed
Prior art date
Application number
SE7412667A
Other languages
English (en)
Other versions
SE400348B (sv
Inventor
R P Lohmann
S J Markowski
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of SE7412667L publication Critical patent/SE7412667L/xx
Publication of SE400348B publication Critical patent/SE400348B/xx

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
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • 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)
  • Combustion Of Fluid Fuel (AREA)
  • Gas Burners (AREA)
  • Incineration Of Waste (AREA)
  • Gasification And Melting Of Waste (AREA)
  • Regulation And Control Of Combustion (AREA)
  • Control Of Combustion (AREA)
SE7412667A 1973-10-15 1974-10-09 Brennare SE400348B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US406771A US3872664A (en) 1973-10-15 1973-10-15 Swirl combustor with vortex burning and mixing

Publications (2)

Publication Number Publication Date
SE7412667L true SE7412667L (de) 1975-04-16
SE400348B SE400348B (sv) 1978-03-20

Family

ID=23609397

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7412667A SE400348B (sv) 1973-10-15 1974-10-09 Brennare

Country Status (11)

Country Link
US (1) US3872664A (de)
JP (1) JPS5858563B2 (de)
CA (1) CA1004481A (de)
CH (1) CH585373A5 (de)
DE (1) DE2449084C2 (de)
FR (1) FR2247674B1 (de)
GB (1) GB1482145A (de)
IL (1) IL45684A (de)
IT (1) IT1022870B (de)
NO (1) NO145081C (de)
SE (1) SE400348B (de)

Families Citing this family (131)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1454280A (en) * 1972-11-28 1976-11-03 Nissan Motor Combustible mixture supply system
US3974646A (en) * 1974-06-11 1976-08-17 United Technologies Corporation Turbofan engine with augmented combustion chamber using vorbix principle
US3974647A (en) * 1974-08-26 1976-08-17 United Technologies Corporation Combustion instability reduction device having swirling flow
JPS5129726A (de) * 1974-09-06 1976-03-13 Mitsubishi Heavy Ind Ltd
US4045956A (en) * 1974-12-18 1977-09-06 United Technologies Corporation Low emission combustion chamber
US3937008A (en) * 1974-12-18 1976-02-10 United Technologies Corporation Low emission combustion chamber
US4058977A (en) * 1974-12-18 1977-11-22 United Technologies Corporation Low emission combustion chamber
US3973395A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Low emission combustion chamber
US3973390A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones
DE2511171C2 (de) * 1975-03-14 1984-03-15 Daimler-Benz Ag, 7000 Stuttgart Filmverdampfungs-Brennkammer
US3993449A (en) * 1975-04-07 1976-11-23 City Of North Olmsted Apparatus for pollution abatement
DE2524319C2 (de) * 1975-06-02 1984-03-08 Société Nationale d'Etude et de Construction de Moteurs d'Aviation, 75015 Paris Brennkammer mit einem abgestuften Flammmrohr
US4052844A (en) * 1975-06-02 1977-10-11 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Gas turbine combustion chambers
US4012904A (en) * 1975-07-17 1977-03-22 Chrysler Corporation Gas turbine burner
JPS5944491B2 (ja) * 1975-10-27 1984-10-30 日産自動車株式会社 ガスタ−ビンエンジンニオケル ネンシヨウキ
US4204402A (en) * 1976-05-07 1980-05-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reduction of nitric oxide emissions from a combustor
DE2629761A1 (de) * 1976-07-02 1978-01-05 Volkswagenwerk Ag Brennkammer fuer gasturbinen
JPS5824695B2 (ja) * 1977-03-14 1983-05-23 トヨタ自動車株式会社 ガスタ−ビンエンジンの燃焼器構造
JPS53143815A (en) * 1977-05-23 1978-12-14 Mitsubishi Heavy Ind Ltd Gas turbine combustion
US4145879A (en) * 1977-12-15 1979-03-27 United Technologies Corp. Modified vorbix burner concept
US4145878A (en) * 1977-12-15 1979-03-27 United Technologies Corp. Vorbix augmenter configuration
US4339924A (en) * 1978-08-02 1982-07-20 Solar Turbines Incorporated Combustion systems
GB2040031B (en) * 1979-01-12 1983-02-09 Gen Electric Dual stage-dual mode low emission gas turbine combustion system
US4420929A (en) * 1979-01-12 1983-12-20 General Electric Company Dual stage-dual mode low emission gas turbine combustion system
EP0019022B1 (de) * 1979-05-18 1983-10-12 Robert Storey Babington Brenner für flüssige Brennstoffe
US4292801A (en) * 1979-07-11 1981-10-06 General Electric Company Dual stage-dual mode low nox combustor
GB2073400B (en) * 1980-04-02 1984-03-14 United Technologies Corp Fuel injector
US4590769A (en) * 1981-01-12 1986-05-27 United Technologies Corporation High-performance burner construction
JPS57154852U (de) * 1981-03-18 1982-09-29
JPS59153028A (ja) * 1983-02-18 1984-08-31 Hitachi Ltd ガスタ−ビンの燃焼器
JPS60105576A (ja) * 1983-11-15 1985-06-11 Tokyo Electric Co Ltd 印字装置
US4628694A (en) * 1983-12-19 1986-12-16 General Electric Company Fabricated liner article and method
JPS60109949U (ja) * 1983-12-28 1985-07-25 東芝テック株式会社 ドツトプリンタ
EP0193029B1 (de) * 1985-02-26 1988-11-17 BBC Brown Boveri AG Brennkammer für Gasturbinen
DE3606625A1 (de) * 1985-03-04 1986-09-04 Kraftwerk Union AG, 4330 Mülheim Pilotbrenner mit geringer no(pfeil abwaerts)x(pfeil abwaerts)-emission fuer feuerungsanlagen, insbesondere von gasturbinenanlagen, und verfahren zu seinem betrieb
JPS6238164U (de) * 1985-08-28 1987-03-06
US4784600A (en) * 1986-10-08 1988-11-15 Prutech Ii Low NOx staged combustor with swirl suppression
CH672366A5 (de) * 1986-12-09 1989-11-15 Bbc Brown Boveri & Cie
US4891936A (en) * 1987-12-28 1990-01-09 Sundstrand Corporation Turbine combustor with tangential fuel injection and bender jets
US4928481A (en) * 1988-07-13 1990-05-29 Prutech Ii Staged low NOx premix gas turbine combustor
US5284019A (en) * 1990-06-12 1994-02-08 The United States Of America As Represented By The Secretary Of The Air Force Double dome, single anular combustor with daisy mixer
US5197278A (en) * 1990-12-17 1993-03-30 General Electric Company Double dome combustor and method of operation
US5406799A (en) * 1992-06-12 1995-04-18 United Technologies Corporation Combustion chamber
DE4316474A1 (de) * 1993-05-17 1994-11-24 Abb Management Ag Vormischbrenner zum Betrieb einer Brennkraftmaschine, einer Brennkammer einer Gasturbogruppe oder Feuerungsanlage
WO1996027766A1 (de) * 1995-03-08 1996-09-12 Bmw Rolls-Royce Gmbh Axial gestufte doppelring-brennkammer einer gasturbine
DE59808754D1 (de) * 1997-12-19 2003-07-24 Mtu Aero Engines Gmbh Vormischbrennkammer für eine Gasturbine
US6405523B1 (en) * 2000-09-29 2002-06-18 General Electric Company Method and apparatus for decreasing combustor emissions
GB2398375A (en) * 2003-02-14 2004-08-18 Alstom A mixer for two fluids having a venturi shape
RU2406936C2 (ru) * 2003-09-05 2010-12-20 Делэвэн Инк Горелка для камеры сгорания газовой турбины (варианты)
US7093441B2 (en) * 2003-10-09 2006-08-22 United Technologies Corporation Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
US20070119183A1 (en) * 2005-11-28 2007-05-31 General Electric Company Gas turbine engine combustor
US7886539B2 (en) * 2007-09-14 2011-02-15 Siemens Energy, Inc. Multi-stage axial combustion system
US7665309B2 (en) 2007-09-14 2010-02-23 Siemens Energy, Inc. Secondary fuel delivery system
US8387398B2 (en) * 2007-09-14 2013-03-05 Siemens Energy, Inc. Apparatus and method for controlling the secondary injection of fuel
EP2107310A1 (de) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Brenner
EP2107312A1 (de) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Pilotverbrennkammer in einem Brenner
US8176739B2 (en) * 2008-07-17 2012-05-15 General Electric Company Coanda injection system for axially staged low emission combustors
BRPI0914033A2 (pt) * 2008-10-13 2015-11-03 Dow Global Technologies Inc processo de uma etapa para a produção de de propenos clorados e fluorados e processo para preparar 2,3,3,3- tetrafluorprop-1 eno( 1,3,3,3- tetrafluorprop-1 eno (hfo-123ze)
US20100223930A1 (en) * 2009-03-06 2010-09-09 General Electric Company Injection device for a turbomachine
JP4797079B2 (ja) * 2009-03-13 2011-10-19 川崎重工業株式会社 ガスタービン燃焼器
US8689559B2 (en) * 2009-03-30 2014-04-08 General Electric Company Secondary combustion system for reducing the level of emissions generated by a turbomachine
US8667800B2 (en) * 2009-05-13 2014-03-11 Delavan Inc. Flameless combustion systems for gas turbine engines
EP2485832B1 (de) * 2009-10-09 2016-11-23 Blue Cube IP LLC Verfahren zur herstellung eines chlorierten und/oder fluorierten propens in einem isothermischen multiröhrenreaktoren
JP5767231B2 (ja) 2009-10-09 2015-08-19 ダウ グローバル テクノロジーズ エルエルシー 塩素化及び／又はフッ素化されたプロペン及びより高級なアルケンを製造するプロセス
US20110087056A1 (en) * 2009-10-09 2011-04-14 Dow Global Technologies Adiabatic plug flow reactors and processes incorporating the same
US8581011B2 (en) * 2009-10-09 2013-11-12 Dow Global Technologies, Llc Process for the production of chlorinated and/or fluorinated propenes
RU2506499C2 (ru) * 2009-11-09 2014-02-10 Дженерал Электрик Компани Топливные форсунки газовой турбины с противоположными направлениями завихрения
RU2534189C2 (ru) * 2010-02-16 2014-11-27 Дженерал Электрик Компани Камера сгорания для газовой турбины(варианты) и способ эксплуатации газовой турбины
US8752386B2 (en) 2010-05-25 2014-06-17 Siemens Energy, Inc. Air/fuel supply system for use in a gas turbine engine
US9068748B2 (en) * 2011-01-24 2015-06-30 United Technologies Corporation Axial stage combustor for gas turbine engines
EP2714631B1 (de) 2011-05-31 2020-05-13 Blue Cube IP LLC Verfahren zur herstellung von chlorierten propenen
US8907149B2 (en) 2011-05-31 2014-12-09 Dow Global Technologies Llc Process for the production of chlorinated propenes
US8601820B2 (en) 2011-06-06 2013-12-10 General Electric Company Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
CN103596908A (zh) 2011-06-08 2014-02-19 陶氏益农公司 生产氯化和/或氟化丙烯的方法
US9222674B2 (en) * 2011-07-21 2015-12-29 United Technologies Corporation Multi-stage amplification vortex mixture for gas turbine engine combustor
US9297534B2 (en) 2011-07-29 2016-03-29 General Electric Company Combustor portion for a turbomachine and method of operating a turbomachine
US8919137B2 (en) 2011-08-05 2014-12-30 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US9010120B2 (en) 2011-08-05 2015-04-21 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US9233896B2 (en) 2011-08-07 2016-01-12 Blue Cube Ip Llc Process for the production of chlorinated propenes
US8907148B2 (en) 2011-08-07 2014-12-09 Dow Global Technologies Llc Process for the production of chlorinated propenes
EP2780636A1 (de) * 2011-11-17 2014-09-24 General Electric Company Brennkammer einer turbomaschine sowie verfahren zum betrieb einer turbomaschine
WO2013078035A1 (en) 2011-11-21 2013-05-30 Dow Global Technologies, Llc Process for the production of chlorinated alkanes
CN104024186B (zh) 2011-12-02 2016-10-12 蓝立方知识产权有限责任公司 生产氯化烷烃的方法
CN104024187B (zh) 2011-12-02 2017-04-12 蓝立方知识产权有限责任公司 生产氯化烷烃的方法
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9194586B2 (en) 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9243802B2 (en) 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
JP6170068B2 (ja) 2011-12-13 2017-07-26 ブルー キューブ アイピー エルエルシー 塩素化プロパン及びプロペンの製造方法
EP2794528B1 (de) 2011-12-22 2020-02-26 Blue Cube IP LLC Verfahren zur herstellung von tetrachlormethan
BR112014015123A2 (pt) 2011-12-23 2017-06-13 Dow Global Technologies Llc processo para a produção de um ou mais alcenos ou compostos aromáticos
US9140455B2 (en) 2012-01-04 2015-09-22 General Electric Company Flowsleeve of a turbomachine component
US20130213046A1 (en) * 2012-02-16 2013-08-22 General Electric Company Late lean injection system
CN104755448A (zh) 2012-09-20 2015-07-01 陶氏环球技术有限公司 用于制造氯化丙烯的方法
WO2014046970A1 (en) 2012-09-20 2014-03-27 Dow Global Technologies, Llc Process for the production of chlorinated propenes
EP2900364B1 (de) 2012-09-30 2018-06-13 Blue Cube IP LLC Wehrlöschung und verfahren damit
IN2015DN03949A (de) 2012-10-26 2015-10-02 Dow Global Technologies Llc
US9512053B2 (en) 2012-12-18 2016-12-06 Blue Cube Ip Llc Process for the production of chlorinated propenes
WO2014100039A1 (en) 2012-12-19 2014-06-26 Dow Global Technologies, Llc Process for the production of chlorinated propenes
JP2016507590A (ja) 2013-02-27 2016-03-10 ブルー キューブ アイピー エルエルシー 塩素化プロペンを生成するための方法
WO2014164368A1 (en) 2013-03-09 2014-10-09 Dow Global Technologies Llc Process for the production of chlorinated alkanes
US9228747B2 (en) * 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9316155B2 (en) 2013-03-18 2016-04-19 General Electric Company System for providing fuel to a combustor
US9631812B2 (en) 2013-03-18 2017-04-25 General Electric Company Support frame and method for assembly of a combustion module of a gas turbine
US9360217B2 (en) 2013-03-18 2016-06-07 General Electric Company Flow sleeve for a combustion module of a gas turbine
US9322556B2 (en) 2013-03-18 2016-04-26 General Electric Company Flow sleeve assembly for a combustion module of a gas turbine combustor
US10436445B2 (en) 2013-03-18 2019-10-08 General Electric Company Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine
US9383104B2 (en) 2013-03-18 2016-07-05 General Electric Company Continuous combustion liner for a combustor of a gas turbine
US9316396B2 (en) * 2013-03-18 2016-04-19 General Electric Company Hot gas path duct for a combustor of a gas turbine
US9400114B2 (en) 2013-03-18 2016-07-26 General Electric Company Combustor support assembly for mounting a combustion module of a gas turbine
US11143407B2 (en) 2013-06-11 2021-10-12 Raytheon Technologies Corporation Combustor with axial staging for a gas turbine engine
US9303871B2 (en) 2013-06-26 2016-04-05 Siemens Aktiengesellschaft Combustor assembly including a transition inlet cone in a gas turbine engine
US20150052905A1 (en) * 2013-08-20 2015-02-26 General Electric Company Pulse Width Modulation for Control of Late Lean Liquid Injection Velocity
EP3060851B1 (de) * 2013-10-24 2019-11-27 United Technologies Corporation Umfänglich und axial gestufte brennkammer für gasturbinenmotor
WO2015108583A2 (en) * 2013-10-24 2015-07-23 United Technologies Corporation Circumferentially and axially staged annular combustor for gas turbine engine combustor
US20150159877A1 (en) * 2013-12-06 2015-06-11 General Electric Company Late lean injection manifold mixing system
US9976743B2 (en) * 2014-07-03 2018-05-22 United Technologies Corporation Dilution hole assembly
US10359194B2 (en) 2014-08-26 2019-07-23 Siemens Energy, Inc. Film cooling hole arrangement for acoustic resonators in gas turbine engines
US10060629B2 (en) * 2015-02-20 2018-08-28 United Technologies Corporation Angled radial fuel/air delivery system for combustor
US20170284675A1 (en) * 2016-03-30 2017-10-05 Siemens Energy, Inc. Injector assembly and ducting arrangement including such injector assemblies in a combustion system for a gas turbine engine
JP6822868B2 (ja) * 2017-02-21 2021-01-27 三菱重工業株式会社 燃焼器及びガスタービン
US11255543B2 (en) * 2018-08-07 2022-02-22 General Electric Company Dilution structure for gas turbine engine combustor
US11287134B2 (en) * 2019-12-31 2022-03-29 General Electric Company Combustor with dual pressure premixing nozzles
US11828467B2 (en) 2019-12-31 2023-11-28 General Electric Company Fluid mixing apparatus using high- and low-pressure fluid streams
US11371709B2 (en) 2020-06-30 2022-06-28 General Electric Company Combustor air flow path
US11333360B2 (en) * 2020-09-25 2022-05-17 General Electric Company Fuel injector for a turbomachine
US20220364729A1 (en) * 2021-05-14 2022-11-17 General Electric Company Combustor dilution with vortex generating turbulators
US11566790B1 (en) * 2021-10-28 2023-01-31 General Electric Company Methods of operating a turbomachine combustor on hydrogen
CN114353121B (zh) * 2022-01-18 2022-12-20 上海交通大学 一种用于燃气轮机的多喷嘴燃料注入方法
US11578871B1 (en) * 2022-01-28 2023-02-14 General Electric Company Gas turbine engine combustor with primary and secondary fuel injectors
CN116658932A (zh) * 2022-02-18 2023-08-29 通用电气公司 具有带旋流轮叶的稀释开口的燃烧器衬套
US20230408098A1 (en) * 2022-05-25 2023-12-21 General Electric Company Combustor with secondary fuel nozzle in dilution fence

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1601607A1 (de) * 1951-01-28 1970-08-27 Lucas Industries Ltd Brenner fuer Gasturbinen
DE1074920B (de) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Verfahren und \ orrichtung zur Regelung von Gas turbmenbrennkammern mit unterteilter Verbrennung und mehreren Druckstufen
GB854135A (en) * 1958-03-05 1960-11-16 Rolls Royce Improvements in or relating to combustion equipment
US3134229A (en) * 1961-10-02 1964-05-26 Gen Electric Combustion chamber
US3338051A (en) * 1965-05-28 1967-08-29 United Aircraft Corp High velocity ram induction burner
US3643430A (en) * 1970-03-04 1972-02-22 United Aircraft Corp Smoke reduction combustion chamber
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
JPS4724483Y1 (de) * 1970-12-22 1972-08-02
US3703259A (en) * 1971-05-03 1972-11-21 Gen Electric Air blast fuel atomizer
JPS5326481Y2 (de) * 1973-06-05 1978-07-06

Also Published As

Publication number Publication date
NO145081B (no) 1981-09-28
CH585373A5 (de) 1977-02-28
JPS5065708A (de) 1975-06-03
GB1482145A (en) 1977-08-03
NO145081C (no) 1982-01-06
SE400348B (sv) 1978-03-20
FR2247674A1 (de) 1975-05-09
NO743677L (de) 1975-06-02
IL45684A0 (en) 1974-12-31
US3872664A (en) 1975-03-25
AU7329574A (en) 1976-03-18
IL45684A (en) 1976-11-30
CA1004481A (en) 1977-02-01
JPS5858563B2 (ja) 1983-12-26
IT1022870B (it) 1978-04-20
DE2449084C2 (de) 1984-09-06
DE2449084A1 (de) 1975-04-17
FR2247674B1 (de) 1980-05-23

Similar Documents

Publication Publication Date Title
SE7412667L (de)
GB1449150A (en) Combustion
GB1136543A (en) Liquid fuel combustion apparatus for gas turbine engines
SE7500960L (de)
GB1256951A (de)
GB1530831A (en) Low nox burner
GB1459258A (en) Combustion chamber for a gas turbine engine
GB1489110A (en) Hot-gas generator
GB1529808A (en) Fuel-water vapour premix for low nox burning
ES216010U (es) Quemador de combustibles liquidos pulverizados.
GB1516868A (en) Combustion chamber for gas turbine engines
ES413765A1 (es) Perfeccionamientos en quemadores de combustible gaseoso.
ATE124528T1 (de) Brennkammer einer gasturbine.
GB1391199A (en) Gas burners especially for domestic appliances
CH608587A5 (en) Swirl device for burner using liquid fuel atomised at high pressure
GB1120326A (en) Method and burner for producing flame jet
GB1535131A (en) Burners
JPS57157935A (en) Gas turbine combustor
SE8104982L (sv) Forbrenningsutrustning
GB1524217A (en) Combustion chamber for a gas turbine engine
GB1017900A (en) Combustion chambers
GB704468A (en) Improvements in or relating to combustion chambers for liquid, gaseous or pulverisedsolid fuels
GB1059199A (en) Flame tube
GB1366144A (en) Combustion chambers for gas turbine engines
JPS57131822A (en) Swirl-chamber type diesel engine

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 7412667-3

Effective date: 19930510

Format of ref document f/p: F