FR1094871A - Improvements to injected fuel combustion devices - Google Patents

Improvements to injected fuel combustion devices

Info

Publication number
FR1094871A
FR1094871A FR1094871DA FR1094871A FR 1094871 A FR1094871 A FR 1094871A FR 1094871D A FR1094871D A FR 1094871DA FR 1094871 A FR1094871 A FR 1094871A
Authority
FR
France
Prior art keywords
fuel combustion
injected fuel
combustion devices
devices
injected
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
Application number
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Compagnie Francaise Thomson Houston SA
Original Assignee
Compagnie Francaise Thomson Houston SA
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 Compagnie Francaise Thomson Houston SA filed Critical Compagnie Francaise Thomson Houston SA
Application granted granted Critical
Publication of FR1094871A publication Critical patent/FR1094871A/en
Expired legal-status Critical Current

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
    • F23R3/02Continuous 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)
FR1094871D 1959-01-22 1953-09-15 Improvements to injected fuel combustion devices Expired FR1094871A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US788399A US3030773A (en) 1959-01-22 1959-01-22 Vortex type combustion with means for supplying secondary air

Publications (1)

Publication Number Publication Date
FR1094871A true FR1094871A (en) 1955-05-25

Family

ID=25144376

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1094871D Expired FR1094871A (en) 1959-01-22 1953-09-15 Improvements to injected fuel combustion devices

Country Status (2)

Country Link
US (1) US3030773A (en)
FR (1) FR1094871A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2086476A1 (en) * 1970-04-30 1971-12-31 Gen Electric
DE2641605A1 (en) * 1975-12-24 1977-07-07 Gen Electric FUEL EQUIPMENT WITH CENTRAL INJECTION
DE2737773A1 (en) * 1976-08-27 1978-03-09 Hitachi Ltd Burner and combustion chamber for gas turbines - has divergent inner tube ensuring combustion with reduced nitrogen oxide(s)
FR2452598A1 (en) * 1979-03-27 1980-10-24 Gen Electric COMBUSTION APPARATUS COMPRISING A CYCLONE PRE-COMBUSTION CHAMBER, AND COMBUSTION METHOD FOR LIQUID FUEL GAS TURBINES
FR2484020A1 (en) * 1980-06-06 1981-12-11 Snecma FUEL INJECTION ASSEMBLY FOR TURBOREACTOR CHAMBER

Families Citing this family (60)

* Cited by examiner, † Cited by third party
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US3244219A (en) * 1961-04-11 1966-04-05 Midland Ross Corp Self-stabilizing apparatus
US3187799A (en) * 1961-04-11 1965-06-08 Midland Ross Corp Self-stabilizing combustion apparatus and method
US3273622A (en) * 1965-06-07 1966-09-20 Midland Ross Corp Self-stabilizing combustion apparatus
US3273623A (en) * 1965-11-03 1966-09-20 Midland Ross Corp Self-stabilizing combustion apparatus
FR1500110A (en) * 1966-07-08 1967-11-03 Snecma Improvements to turbo-reactors
US3545947A (en) * 1967-08-25 1970-12-08 Texas Instruments Inc Liquid fuel-air partial oxidation system
US3577729A (en) * 1969-03-11 1971-05-04 Glenn B Warren Reciprocating internal combustion engine with constant pressure combustion
US3603711A (en) * 1969-09-17 1971-09-07 Edgar S Downs Combination pressure atomizer and surface-type burner for liquid fuel
US3630024A (en) * 1970-02-02 1971-12-28 Gen Electric Air swirler for gas turbine combustor
US3864073A (en) * 1970-03-24 1975-02-04 Collin Consult Method for combustion fuels which are ejected from an orifice in a manner to form a substantially conically shaped curtain of fuel and a device for putting the method into effect
SE410218B (en) * 1970-03-24 1979-10-01 Collin Ab Rolf BURNER
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
US3859786A (en) * 1972-05-25 1975-01-14 Ford Motor Co Combustor
FR2290634A1 (en) * 1974-11-06 1976-06-04 Lorraine Houilleres COMPLETE COMBUSTION PROCESS OF HOT GASES WITH LOW CALORIFIC CAPACITY
GB1524194A (en) * 1974-12-06 1978-09-06 Secr Defence Combustion apparatus
US4007001A (en) * 1975-04-14 1977-02-08 Phillips Petroleum Company Combustors and methods of operating same
US4056091A (en) * 1975-04-23 1977-11-01 Moncrieff Yeates Alexander Joh Vortical flow aerothermodynamic fireplace unit
US4197869A (en) * 1975-04-23 1980-04-15 Moncrieff Yeates Alexander J Method and apparatus for generating a stable vortex fluid flow pattern
US4132180A (en) * 1975-07-31 1979-01-02 Fredrick William L Apparatus and method for enhancing combustibility of solid fuels
US4160640A (en) * 1977-08-30 1979-07-10 Maev Vladimir A Method of fuel burning in combustion chambers and annular combustion chamber for carrying same into effect
US4203720A (en) * 1978-03-31 1980-05-20 Gilmore & Tatge Mfg. Co. Oil burner
DE2836534C2 (en) * 1978-08-21 1982-09-02 Oertli AG Dübendorf, Dübendorf Process for burning liquid fuel and burners for carrying out the process
US4373325A (en) * 1980-03-07 1983-02-15 International Harvester Company Combustors
US4470262A (en) * 1980-03-07 1984-09-11 Solar Turbines, Incorporated Combustors
DE3690574C2 (en) * 1985-11-15 1995-09-28 Nippon Oxygen Co Ltd Oxygen heating device
US4765136A (en) * 1985-11-25 1988-08-23 United Technologies Corporation Gas turbine engine augmentor
US5009174A (en) * 1985-12-02 1991-04-23 Exxon Research And Engineering Company Acid gas burner
US5163287A (en) * 1989-12-22 1992-11-17 Sundstrand Corporation Stored energy combustor with fuel injector containing igniter means for accommodating thermal expansion
US5197290A (en) * 1990-03-26 1993-03-30 Fuel Systems Textron Inc. Variable area combustor air swirler
CA2093316C (en) * 1990-10-05 2002-12-03 Janos M. Beer Combustion system for reduction of nitrogen oxides
US5165241A (en) * 1991-02-22 1992-11-24 General Electric Company Air fuel mixer for gas turbine combustor
US5462430A (en) * 1991-05-23 1995-10-31 Institute Of Gas Technology Process and apparatus for cyclonic combustion
US5209187A (en) * 1991-08-01 1993-05-11 Institute Of Gas Technology Low pollutant - emission, high efficiency cyclonic burner for firetube boilers and heaters
US5251447A (en) * 1992-10-01 1993-10-12 General Electric Company Air fuel mixer for gas turbine combustor
US5823759A (en) * 1993-03-20 1998-10-20 Cabot Corporation Apparatus and method for burning combustible gases
US5636510A (en) * 1994-05-25 1997-06-10 Westinghouse Electric Corporation Gas turbine topping combustor
US5584178A (en) * 1994-06-14 1996-12-17 Southwest Research Institute Exhaust gas combustor
DE4441641A1 (en) * 1994-11-23 1996-05-30 Abb Management Ag Combustion chamber with premix burners
US6550251B1 (en) * 1997-12-18 2003-04-22 General Electric Company Venturiless swirl cup
US6270337B1 (en) * 1998-06-12 2001-08-07 Precision Combustion, Inc. Dry, low NOx pilot
US20060241075A1 (en) * 2001-05-18 2006-10-26 Sirna Therapeutics, Inc. RNA interference mediated inhibition of desmoglein gene expression using short interfering nucleic acid (siNA)
JP4426841B2 (en) * 2001-08-06 2010-03-03 サウスウェスト リサーチ インスティテュート Method and apparatus for testing the durability of a catalytic converter
US7175422B2 (en) * 2001-08-06 2007-02-13 Southwest Research Institute Method for accelerated aging of catalytic converters incorporating injection of volatilized lubricant
US7741127B2 (en) * 2001-08-06 2010-06-22 Southwest Research Institute Method for producing diesel exhaust with particulate material for testing diesel engine aftertreatment devices
US20040007056A1 (en) * 2001-08-06 2004-01-15 Webb Cynthia C. Method for testing catalytic converter durability
US6983645B2 (en) * 2002-08-06 2006-01-10 Southwest Research Institute Method for accelerated aging of catalytic converters incorporating engine cold start simulation
US7212926B2 (en) * 2002-08-06 2007-05-01 Southwest Research Institute Testing using a non-engine based test system and exhaust product comprising alternative fuel exhaust
US7299137B2 (en) 2002-08-06 2007-11-20 Southwest Research Institute Method for drive cycle simulation using non-engine based test system
US7412335B2 (en) * 2002-08-06 2008-08-12 Southwest Research Institute Component evaluations using non-engine based test system
JP2004207025A (en) * 2002-12-25 2004-07-22 Nissan Motor Co Ltd Catalytic combustor and fuel cell system
US7044163B1 (en) * 2004-02-10 2006-05-16 The Ohio State University Drag reduction in pipe flow using microbubbles and acoustic energy
WO2006101991A2 (en) 2005-03-17 2006-09-28 Southwest Research Institute Mass air flow compensation for burner-based exhaust gas generation system
WO2006101987A2 (en) * 2005-03-17 2006-09-28 Southwest Research Institute Use of recirculated exhaust gas in a burner-based exhaust generation system for reduced fuel consumption and for cooling
US20070039381A1 (en) * 2005-08-05 2007-02-22 Timmons Suzanne A Secondary Air Injector For Use With Exhaust Gas Simulation System
US7628606B1 (en) * 2008-05-19 2009-12-08 Browning James A Method and apparatus for combusting fuel employing vortex stabilization
US8622737B2 (en) 2008-07-16 2014-01-07 Robert S. Babington Perforated flame tube for a liquid fuel burner
US20120052451A1 (en) * 2010-08-31 2012-03-01 General Electric Company Fuel nozzle and method for swirl control
US8455056B1 (en) * 2012-07-30 2013-06-04 James A. Browning Rapidly-mixing high velocity flame torch and method
CN103032891B (en) * 2013-01-04 2015-07-29 中国科学院工程热物理研究所 A kind of many eddy combustion methods
US11713878B2 (en) * 2020-01-08 2023-08-01 F. Michael Lewis Method and mobile apparatus for improving in-situ combustion of a combustible material lying on nominally planar surface

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2607193A (en) * 1947-10-25 1952-08-19 Curtiss Wright Corp Annular combustion chamber with multiple notched fuel nozzles
US2654996A (en) * 1948-10-26 1953-10-13 Oerlikon Maschf Gas turbine combustion chamber
US2592110A (en) * 1949-05-21 1952-04-08 Curtiss Wright Corp Orifice type flame holder construction
US2698050A (en) * 1949-06-10 1954-12-28 Lummus Co Combustion for liquid fuels
US2674846A (en) * 1950-12-18 1954-04-13 Lummus Co Combustion chamber with baffle means to control secondary air
US2745250A (en) * 1952-09-26 1956-05-15 Gen Electric Reverse vortex combustion chamber

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2086476A1 (en) * 1970-04-30 1971-12-31 Gen Electric
DE2641605A1 (en) * 1975-12-24 1977-07-07 Gen Electric FUEL EQUIPMENT WITH CENTRAL INJECTION
DE2737773A1 (en) * 1976-08-27 1978-03-09 Hitachi Ltd Burner and combustion chamber for gas turbines - has divergent inner tube ensuring combustion with reduced nitrogen oxide(s)
FR2452598A1 (en) * 1979-03-27 1980-10-24 Gen Electric COMBUSTION APPARATUS COMPRISING A CYCLONE PRE-COMBUSTION CHAMBER, AND COMBUSTION METHOD FOR LIQUID FUEL GAS TURBINES
FR2484020A1 (en) * 1980-06-06 1981-12-11 Snecma FUEL INJECTION ASSEMBLY FOR TURBOREACTOR CHAMBER
EP0041878A2 (en) * 1980-06-06 1981-12-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Fuel injection device for a gas turbine
EP0041878A3 (en) * 1980-06-06 1982-09-22 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Fuel injection device for a gas turbine

Also Published As

Publication number Publication date
US3030773A (en) 1962-04-24

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