CH585373A5 - - Google Patents

Info

Publication number
CH585373A5
CH585373A5 CH1369274A CH1369274A CH585373A5 CH 585373 A5 CH585373 A5 CH 585373A5 CH 1369274 A CH1369274 A CH 1369274A CH 1369274 A CH1369274 A CH 1369274A CH 585373 A5 CH585373 A5 CH 585373A5
Authority
CH
Switzerland
Application number
CH1369274A
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 CH585373A5 publication Critical patent/CH585373A5/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/346Feeding into different combustion zones for staged combustion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Gasification And Melting Of Waste (AREA)
  • Incineration Of Waste (AREA)
  • Regulation And Control Of Combustion (AREA)
  • Control Of Combustion (AREA)
  • Gas Burners (AREA)
CH1369274A 1973-10-15 1974-10-11 CH585373A5 (en)

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 (1)

Publication Number Publication Date
CH585373A5 true CH585373A5 (en) 1977-02-28

Family

ID=23609397

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1369274A CH585373A5 (en) 1973-10-15 1974-10-11

Country Status (11)

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

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 (en) * 1974-09-06 1976-03-13 Mitsubishi Heavy Ind Ltd
US3973395A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Low emission combustion chamber
US3937008A (en) * 1974-12-18 1976-02-10 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
US4058977A (en) * 1974-12-18 1977-11-22 United Technologies Corporation Low emission combustion chamber
US4045956A (en) * 1974-12-18 1977-09-06 United Technologies Corporation Low emission combustion chamber
DE2511171C2 (en) * 1975-03-14 1984-03-15 Daimler-Benz Ag, 7000 Stuttgart Film evaporation combustion chamber
US3993449A (en) * 1975-04-07 1976-11-23 City Of North Olmsted Apparatus for pollution abatement
DE2524319C2 (en) * 1975-06-02 1984-03-08 Société Nationale d'Etude et de Construction de Moteurs d'Aviation, 75015 Paris Combustion chamber with a stepped flame tube
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 (en) * 1975-10-27 1984-10-30 日産自動車株式会社 Gas turbine engine Niokel Nenshiyouki
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 (en) * 1976-07-02 1978-01-05 Volkswagenwerk Ag COMBUSTION CHAMBER FOR GAS TURBINES
JPS5824695B2 (en) * 1977-03-14 1983-05-23 トヨタ自動車株式会社 Gas turbine engine combustor structure
JPS53143815A (en) * 1977-05-23 1978-12-14 Mitsubishi Heavy Ind Ltd Gas turbine combustion
US4145878A (en) * 1977-12-15 1979-03-27 United Technologies Corp. Vorbix augmenter configuration
US4145879A (en) * 1977-12-15 1979-03-27 United Technologies Corp. Modified vorbix burner concept
US4339924A (en) * 1978-08-02 1982-07-20 Solar Turbines Incorporated Combustion systems
US4420929A (en) * 1979-01-12 1983-12-20 General Electric Company Dual stage-dual mode low emission gas turbine combustion system
GB2098720B (en) * 1979-01-12 1983-04-27 Gen Electric Stationary gas turbine combustor arrangements
EP0019022B1 (en) * 1979-05-18 1983-10-12 Robert Storey Babington Liquid fuel burners
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 (en) * 1981-03-18 1982-09-29
JPS59153028A (en) * 1983-02-18 1984-08-31 Hitachi Ltd Combustor of gas turbine
JPS60105576A (en) * 1983-11-15 1985-06-11 Tokyo Electric Co Ltd Printer
US4628694A (en) * 1983-12-19 1986-12-16 General Electric Company Fabricated liner article and method
JPS60109949U (en) * 1983-12-28 1985-07-25 東芝テック株式会社 dot printer
EP0193029B1 (en) * 1985-02-26 1988-11-17 BBC Brown Boveri AG Gas turbine combustor
DE3606625A1 (en) * 1985-03-04 1986-09-04 Kraftwerk Union AG, 4330 Mülheim Pilot burner with low NOx emission for furnace installations, in particular of gas turbine installations, and method of operating it
JPS6238164U (en) * 1985-08-28 1987-03-06
US4784600A (en) * 1986-10-08 1988-11-15 Prutech Ii Low NOx staged combustor with swirl suppression
CH672366A5 (en) * 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 (en) * 1993-05-17 1994-11-24 Abb Management Ag Premix burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or a combustion system
WO1996027766A1 (en) * 1995-03-08 1996-09-12 Bmw Rolls-Royce Gmbh Axially stepped double-ring combustion chamber for a gas turbine
EP0924470B1 (en) * 1997-12-19 2003-06-18 MTU Aero Engines GmbH Premix combustor for a gas turbine
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
EP1660818A2 (en) * 2003-09-05 2006-05-31 Delavan Inc. Pilot combustor for stabilizing combustion in gas turbine engines
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
US8387398B2 (en) * 2007-09-14 2013-03-05 Siemens Energy, Inc. Apparatus and method for controlling the secondary injection of fuel
US7665309B2 (en) 2007-09-14 2010-02-23 Siemens Energy, Inc. Secondary fuel delivery system
US7886539B2 (en) * 2007-09-14 2011-02-15 Siemens Energy, Inc. Multi-stage axial combustion system
EP2107312A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Pilot combustor in a burner
EP2107310A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Burner
US8176739B2 (en) * 2008-07-17 2012-05-15 General Electric Company Coanda injection system for axially staged low emission combustors
WO2010045104A2 (en) * 2008-10-13 2010-04-22 Dow Global Technologies, Inc. Process for the production of chlorinated and/or fluorinated propenes
US20100223930A1 (en) * 2009-03-06 2010-09-09 General Electric Company Injection device for a turbomachine
JP4797079B2 (en) * 2009-03-13 2011-10-19 川崎重工業株式会社 Gas turbine combustor
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
WO2011044522A2 (en) * 2009-10-09 2011-04-14 Dow Global Technologies, Inc Adiabatic plug flow reactors and processes incorporating the same
WO2011044514A2 (en) 2009-10-09 2011-04-14 Dow Global Technologies, Inc Isothermal multitube reactors and processes incorporating the same
JP5706432B2 (en) * 2009-10-09 2015-04-22 ダウ グローバル テクノロジーズ エルエルシー Method for producing chlorinated and / or fluorinated propene
EP2485997B1 (en) * 2009-10-09 2015-09-09 Dow Global Technologies LLC Process for the production of chlorinated and/or fluorinated propenes and higher alkenes
RU2506499C2 (en) * 2009-11-09 2014-02-10 Дженерал Электрик Компани Fuel atomisers of gas turbine with opposite swirling directions
RU2534189C2 (en) * 2010-02-16 2014-11-27 Дженерал Электрик Компани Gas turbine combustion chamber (versions) and method of its operation
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
WO2012166394A1 (en) 2011-05-31 2012-12-06 Dow Global Technologies, Llc Process for the production of chlorinated propenes
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
WO2012170239A1 (en) 2011-06-08 2012-12-13 Dow Agrosciences, Llc Process for the production of chlorinated and/or fluorinated propenes
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
CN108929192A (en) 2011-08-07 2018-12-04 蓝立方知识产权有限责任公司 The method for producing the propylene of chlorination
US9233896B2 (en) 2011-08-07 2016-01-12 Blue Cube Ip Llc Process for the production of chlorinated propenes
CN103917826B (en) * 2011-11-17 2016-08-24 通用电气公司 Turbomachine combustor assembly and the method for operation turbine
EP2782889B1 (en) 2011-11-21 2016-12-21 Blue Cube IP LLC Process for the production of chlorinated alkanes
EP2785670B1 (en) 2011-12-02 2017-10-25 Blue Cube IP LLC Process for the production of chlorinated alkanes
CN104024187B (en) 2011-12-02 2017-04-12 蓝立方知识产权有限责任公司 Process for the production of chlorinated alkanes
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
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9334205B2 (en) 2011-12-13 2016-05-10 Blue Cube Ip Llc Process for the production of chlorinated propanes and propenes
CN110128239A (en) 2011-12-22 2019-08-16 蓝立方知识产权有限责任公司 The method for producing tetrachloromethane
CN104159874B (en) 2011-12-23 2016-08-24 陶氏环球技术有限责任公司 Produce alkene and/or the method for aromatic compounds
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
CA2884435A1 (en) 2012-09-20 2014-03-27 Dow Global Technologies Llc Process for the production of chlorinated propenes
US9321707B2 (en) 2012-09-20 2016-04-26 Blue Cube Ip Llc Process for the production of chlorinated propenes
WO2014052945A2 (en) 2012-09-30 2014-04-03 Dow Global Technologies, Llc Weir quench and processes incorporating the same
CN104902989B (en) 2012-10-26 2017-09-08 蓝立方知识产权有限责任公司 Blender and reactor and and there is the method for the blender and reactor
WO2014100066A1 (en) 2012-12-18 2014-06-26 Dow Global Technologies, 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
CN104981449B (en) 2013-02-27 2016-12-28 蓝立方知识产权有限责任公司 For the method producing propylene dichloride
US9403741B2 (en) 2013-03-09 2016-08-02 Blue Cube Ip 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
US9400114B2 (en) 2013-03-18 2016-07-26 General Electric Company Combustor support assembly for mounting a combustion module of a gas turbine
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
US9322556B2 (en) 2013-03-18 2016-04-26 General Electric Company Flow sleeve assembly for a combustion module of a gas turbine combustor
US9316155B2 (en) 2013-03-18 2016-04-19 General Electric Company System for providing fuel to a combustor
US9316396B2 (en) * 2013-03-18 2016-04-19 General Electric Company Hot gas path duct for a combustor of a gas turbine
US9383104B2 (en) 2013-03-18 2016-07-05 General Electric Company Continuous combustion liner for a combustor of a gas turbine
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
US9360217B2 (en) 2013-03-18 2016-06-07 General Electric Company Flow sleeve for a combustion module of a gas turbine
EP3008391B1 (en) * 2013-06-11 2020-05-06 United 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
WO2015108583A2 (en) * 2013-10-24 2015-07-23 United Technologies Corporation Circumferentially and axially staged annular combustor for gas turbine engine combustor
US10330321B2 (en) * 2013-10-24 2019-06-25 United Technologies Corporation Circumferentially and axially staged can combustor for gas turbine engine
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
WO2016032434A1 (en) 2014-08-26 2016-03-03 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 (en) * 2017-02-21 2021-01-27 三菱重工業株式会社 Combustor and gas turbine
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 (en) * 2022-01-18 2022-12-20 上海交通大学 Multi-nozzle fuel injection method for gas turbine
US11578871B1 (en) * 2022-01-28 2023-02-14 General Electric Company Gas turbine engine combustor with primary and secondary fuel injectors
CN116658932A (en) * 2022-02-18 2023-08-29 通用电气公司 Combustor liner with dilution openings having swirl vanes
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 (en) * 1951-01-28 1970-08-27 Lucas Industries Ltd Burners for gas turbines
DE1074920B (en) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Method and device for regulating gas turbine combustion chambers with subdivided combustion and several pressure levels
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 (en) * 1970-12-22 1972-08-02
US3703259A (en) * 1971-05-03 1972-11-21 Gen Electric Air blast fuel atomizer
JPS5326481Y2 (en) * 1973-06-05 1978-07-06

Also Published As

Publication number Publication date
IL45684A (en) 1976-11-30
SE400348B (en) 1978-03-20
CA1004481A (en) 1977-02-01
FR2247674B1 (en) 1980-05-23
SE7412667L (en) 1975-04-16
AU7329574A (en) 1976-03-18
NO145081C (en) 1982-01-06
JPS5858563B2 (en) 1983-12-26
NO145081B (en) 1981-09-28
NO743677L (en) 1975-06-02
GB1482145A (en) 1977-08-03
US3872664A (en) 1975-03-25
DE2449084A1 (en) 1975-04-17
IT1022870B (en) 1978-04-20
FR2247674A1 (en) 1975-05-09
IL45684A0 (en) 1974-12-31
JPS5065708A (en) 1975-06-03
DE2449084C2 (en) 1984-09-06

Similar Documents

Publication Publication Date Title
FR2247674B1 (en)
AU476761B2 (en)
AU465372B2 (en)
AU474593B2 (en)
AU474511B2 (en)
AU474838B2 (en)
AU465453B2 (en)
AU471343B2 (en)
AU465434B2 (en)
AU450229B2 (en)
AU476714B2 (en)
AU472848B2 (en)
AU476696B2 (en)
AU466283B2 (en)
AU477823B2 (en)
AU471461B2 (en)
AU461342B2 (en)
AU476873B1 (en)
AU477824B2 (en)
AR196123Q (en)
CH1514473A4 (en)
CH565107A5 (en)
CH561829A5 (en)
AU470923A (en)
CH567484A5 (en)

Legal Events

Date Code Title Description
PL Patent ceased