FR916262A - Perfectionnements apportés aux brûleurs et vaporiseurs pour combustibles liquides ainsi qu'aux moteurs et systèmes à combustion comprenant de tels brûleurs et vaporiseurs - Google Patents

Perfectionnements apportés aux brûleurs et vaporiseurs pour combustibles liquides ainsi qu'aux moteurs et systèmes à combustion comprenant de tels brûleurs et vaporiseurs

Info

Publication number
FR916262A
FR916262A FR916262DA FR916262A FR 916262 A FR916262 A FR 916262A FR 916262D A FR916262D A FR 916262DA FR 916262 A FR916262 A FR 916262A
Authority
FR
France
Prior art keywords
vaporizers
burners
systems
well
combustion engines
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
English (en)
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR916262A publication Critical patent/FR916262A/fr
Expired legal-status Critical Current

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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
    • 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
    • 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
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
    • 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
FR916262D 1939-12-09 1945-09-15 Perfectionnements apportés aux brûleurs et vaporiseurs pour combustibles liquides ainsi qu'aux moteurs et systèmes à combustion comprenant de tels brûleurs et vaporiseurs Expired FR916262A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB258412X 1939-12-09

Publications (1)

Publication Number Publication Date
FR916262A true FR916262A (fr) 1946-12-02

Family

ID=10234212

Family Applications (1)

Application Number Title Priority Date Filing Date
FR916262D Expired FR916262A (fr) 1939-12-09 1945-09-15 Perfectionnements apportés aux brûleurs et vaporiseurs pour combustibles liquides ainsi qu'aux moteurs et systèmes à combustion comprenant de tels brûleurs et vaporiseurs

Country Status (7)

Country Link
US (1) US2404335A (xx)
BE (1) BE460697A (xx)
CH (1) CH258412A (xx)
DE (1) DE951062C (xx)
FR (1) FR916262A (xx)
GB (1) GB577972A (xx)
NL (2) NL70682C (xx)

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US2632296A (en) * 1947-12-06 1953-03-24 Eugene J Houdry Process of generating power involving catalytic oxidation
US2685168A (en) * 1948-01-02 1954-08-03 Phillips Petroleum Co Combustion chamber
US2560207A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Annular combustion chamber with circumferentially spaced double air-swirl burners
US2560223A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Double air-swirl baffle construction for fuel burners
US2632994A (en) * 1948-04-05 1953-03-31 Mcdonnell Aircraft Corp Ram jet engine and flame holder therefor
US2625011A (en) * 1948-07-31 1953-01-13 Armstrong Siddeley Motors Ltd Igniter for liquid fuel combustion chambers
US2654996A (en) * 1948-10-26 1953-10-13 Oerlikon Maschf Gas turbine combustion chamber
US2541900A (en) * 1948-12-24 1951-02-13 A V Roe Canada Ltd Multiple fuel jet burner and torch igniter unit with fuel vaporizing tubes
US2648951A (en) * 1949-03-31 1953-08-18 Gen Motors Corp Combustor igniter cup which becomes incandescent from combustion therein
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US2664703A (en) * 1949-06-28 1954-01-05 A V Roe Canada Ltd Preheater and vaporizer for gas turbine engines
US2648950A (en) * 1949-08-24 1953-08-18 Westinghouse Electric Corp Gas turbine engine apparatus designed to burn wet pulverized fuel
US2635421A (en) * 1949-10-24 1953-04-21 Felix A Blum Pulse jet convertible to ram jetpropulsion means
US3035413A (en) * 1950-01-17 1962-05-22 Linderoth Erik Torvald Thermodynamic combustion device using pulsating gas pressure
US2827759A (en) * 1950-01-18 1958-03-25 Bruno W Bruckmann Gas turbine aricraft power plant having a contraflow air-fuel combustion system
US2773350A (en) * 1950-01-31 1956-12-11 Hillard E Barrett Combustion chamber assembly for ram jet fuel burner
US2697910A (en) * 1950-07-29 1954-12-28 Thermal Res And Engineering Co Fluid fuel burner with self-contained fuel vaporizing unit
US2720754A (en) * 1950-09-29 1955-10-18 Mcdonnell Aircraft Corp Flameholder for ram jet engine
US2798360A (en) * 1950-10-06 1957-07-09 Gen Motors Corp Ducted fan type jet propulsion engine
US2672729A (en) * 1950-10-28 1954-03-23 Boeing Co Spark plug
US2648197A (en) * 1951-01-06 1953-08-11 A V Roe Canada Ltd Vaporizer tube system
US2768497A (en) * 1951-02-03 1956-10-30 Gen Motors Corp Combustion chamber with swirler
US2694444A (en) * 1951-03-17 1954-11-16 American Mach & Foundry Jet-type burner for tobacco curers
US2984979A (en) * 1951-03-27 1961-05-23 Eldon R Babcock Vortex pilot flame source for ramjet engines
US2780062A (en) * 1951-04-03 1957-02-05 Curtiss Wright Corp Jet engine burner construction
US2722803A (en) * 1951-05-23 1955-11-08 Gen Electric Cooling means for combustion chamber cross ignition tubes
US2672727A (en) * 1951-05-31 1954-03-23 Westinghouse Electric Corp Fuel vaporizer system for combustion chambers
US2727358A (en) * 1952-03-27 1955-12-20 A V Roe Canada Ltd Reverse-flow vaporizer with single inlet and plural outlets
US2839048A (en) * 1952-09-08 1958-06-17 Jr Harold M Jacklin Fluid heater
US2775238A (en) * 1953-01-29 1956-12-25 Surface Combustion Corp Fuel burning and air heating apparatus
GB757332A (en) * 1953-06-11 1956-09-19 Lucas Industries Ltd Liquid fuel combustion chambers for jet-propulsion, engines, gas turbines, or other purposes
BE535180A (xx) * 1954-01-27
BE535905A (xx) * 1954-02-23
US2906094A (en) * 1954-04-14 1959-09-29 Glenn H Damon Fuel and rapid ignition apparatus for ignition of fuel in ram jets and rockets
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DE955465C (de) * 1954-09-01 1957-01-03 Daimler Benz Ag Brennstoffverdampfer fuer Brennkammern, insbesondere von Gasturbinen
US2941364A (en) * 1955-04-05 1960-06-21 Armstrong Siddeley Motors Ltd Igniter chamber for a gas turbine engine
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
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US2930194A (en) * 1956-11-19 1960-03-29 Bendix Aviat Corp Combustor having high turbulent mixing for turbine-type starter
DE1167594B (de) * 1960-04-25 1964-04-09 Rolls Royce Kreisringfoermige Brennkammer fuer Gasturbinenstrahltriebwerke
DE1214940B (de) * 1963-03-12 1966-04-21 Licentia Gmbh Rohrartige Gasturbinenbrennkammer
NL7801395A (nl) * 1977-02-23 1978-08-25 Foerenade Fabriksverken Werkwijze en inrichting voor het verbranden van vloeibare, gasvormige of poedervormige brandstoffen.
JPS57129325A (en) * 1981-02-03 1982-08-11 Nissan Motor Co Ltd Structure of air piping for air injection valve of gas turbine engine
US4838029A (en) * 1986-09-10 1989-06-13 The United States Of America As Represented By The Secretary Of The Air Force Externally vaporizing system for turbine combustor
JPH0684817B2 (ja) * 1988-08-08 1994-10-26 株式会社日立製作所 ガスタービン燃焼器及びその運転方法
US5657631A (en) * 1995-03-13 1997-08-19 B.B.A. Research & Development, Inc. Injector for turbine engines
US7313916B2 (en) * 2002-03-22 2008-01-01 Philip Morris Usa Inc. Method and apparatus for generating power by combustion of vaporized fuel
US8502064B2 (en) * 2003-12-11 2013-08-06 Philip Morris Usa Inc. Hybrid system for generating power
US20070180814A1 (en) * 2006-02-03 2007-08-09 General Electric Company Direct liquid fuel injection and ignition for a pulse detonation combustor
JP6327826B2 (ja) * 2013-10-11 2018-05-23 川崎重工業株式会社 ガスタービンの燃料噴射装置
US9534788B2 (en) * 2014-04-03 2017-01-03 General Electric Company Air fuel premixer for low emissions gas turbine combustor
US9765972B2 (en) * 2015-01-30 2017-09-19 Delavan Inc. Fuel injectors for gas turbine engines

Also Published As

Publication number Publication date
BE460697A (xx)
US2404335A (en) 1946-07-16
GB577972A (en) 1941-07-26
NL82403C (xx)
CH258412A (de) 1948-11-30
NL70682C (xx)
DE951062C (de) 1956-10-18

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