GB650608A - Improvements relating to internal combustion engine systems - Google Patents

Improvements relating to internal combustion engine systems

Info

Publication number
GB650608A
GB650608A GB30698/48A GB3069848A GB650608A GB 650608 A GB650608 A GB 650608A GB 30698/48 A GB30698/48 A GB 30698/48A GB 3069848 A GB3069848 A GB 3069848A GB 650608 A GB650608 A GB 650608A
Authority
GB
United Kingdom
Prior art keywords
chamber
vapour
perforated
hot gases
liquid fuel
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
GB30698/48A
Inventor
John Stanley Clarke
Eric Samuel Collinson
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.)
ZF International UK Ltd
Original Assignee
Joseph Lucas 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 Joseph Lucas Ltd filed Critical Joseph Lucas Ltd
Priority to GB30698/48A priority Critical patent/GB650608A/en
Priority to US128188A priority patent/US2622396A/en
Priority to FR1000363D priority patent/FR1000363A/en
Publication of GB650608A publication Critical patent/GB650608A/en
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
    • F23R3/28—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
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Abstract

650,608. Vapour burners. LUCAS, Ltd. J. Nov. 26, 1948, No. 30698. [Class 75(i)] A supplementary liquid fuel vaporizer for re-heating the motive fluid in an internal combustion prime mover comprises the combination of a vaporizing chamber provided with an outlet or outlets for vapour, means for supporting the chamber in a hot gas conduit and for conveying liquid fuel to said chamber, and a baffle or baffles on the chamber for shielding the effluent vapour. A hollow vaporizing chamber c is supported by radial arms b in a conduit a along which hot gases flow, one of the arms b being hollow for conveying liquid fuel from an inlet d to the chamber c, said arm being perforated on its upstream side to allow hot gases to enter and mix with the fuel. The chamber c may be wholly closed at the upstream end or may be perforated to allow entry of the hot gases. The vapour passes from the chamber c through a perforated nose piece e provided with a baffle f for shielding the effluent vapour. In an alternative construction the tubular feed arm b is not perforated, and a plurality of parallel tubes conduct hot gases through the vaporizing chamber to mix with the fuel air mixture at the outlet end. The latter is closed by a perforated plate and the effluent vapour-air mixture is shielded by a pair of baffles.
GB30698/48A 1948-11-26 1948-11-26 Improvements relating to internal combustion engine systems Expired GB650608A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB30698/48A GB650608A (en) 1948-11-26 1948-11-26 Improvements relating to internal combustion engine systems
US128188A US2622396A (en) 1948-11-26 1949-11-18 Fuel vaporizing apparatus for an afterburner
FR1000363D FR1000363A (en) 1948-11-26 1949-11-26 Device for the vaporization of liquid fuel from internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB30698/48A GB650608A (en) 1948-11-26 1948-11-26 Improvements relating to internal combustion engine systems

Publications (1)

Publication Number Publication Date
GB650608A true GB650608A (en) 1951-02-28

Family

ID=10311726

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30698/48A Expired GB650608A (en) 1948-11-26 1948-11-26 Improvements relating to internal combustion engine systems

Country Status (3)

Country Link
US (1) US2622396A (en)
FR (1) FR1000363A (en)
GB (1) GB650608A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4249373A (en) * 1978-01-28 1981-02-10 Rolls-Royce Ltd. Gas turbine engine
US4653278A (en) * 1985-08-23 1987-03-31 General Electric Company Gas turbine engine carburetor
US4730453A (en) * 1985-10-23 1988-03-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Afterburner fuel injection system
US4751815A (en) * 1986-08-29 1988-06-21 United Technologies Corporation Liquid fuel spraybar
US4898001A (en) * 1984-07-10 1990-02-06 Hitachi, Ltd. Gas turbine combustor
US5001898A (en) * 1986-08-29 1991-03-26 United Technologies Corporation Fuel distributor/flameholder for a duct burner

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2664703A (en) * 1949-06-28 1954-01-05 A V Roe Canada Ltd Preheater and vaporizer for gas turbine engines
US2771743A (en) * 1951-08-10 1956-11-27 Rolls Royce Gas-turbine engine with reheat combustion equipment
US2705400A (en) * 1952-01-31 1955-04-05 Armstrong Siddeley Motors Ltd Fuel-burning means for a gaseous fluid propulsion jet
US2799137A (en) * 1952-02-26 1957-07-16 Tenney Method of and apparatus for feeding fuel to a resonant pulse jet engine
US2941361A (en) * 1952-10-15 1960-06-21 Nat Res Dev Combustion apparatus having a flame stabilizing baffle
US2982098A (en) * 1953-04-22 1961-05-02 Power Jets Res & Dev Ltd Liquid fuel vaporizing combustion systems
US2972231A (en) * 1954-09-23 1961-02-21 Ii James W Mullen Rod-igniters for ramjet burners
FR1149404A (en) * 1955-05-25 1957-12-26 Daimler Benz Ag Combustion chamber for combustion turbines, gas generators, hot air jet engines and the like
US2925716A (en) * 1955-09-29 1960-02-23 Joseph F Regan Flame holder
US3046731A (en) * 1955-10-07 1962-07-31 Edward Pohlmann Flame stabilization in jet engines
US2927423A (en) * 1956-02-09 1960-03-08 Henryk U Wisniowski Prevention of screeching combustion in jet engines
US2920445A (en) * 1957-01-15 1960-01-12 Curtiss Wright Corp Flame holder apparatus
GB1184379A (en) * 1967-08-10 1970-03-18 Mini Of Technology London Improvements in or relat ing to Combustion Devices
US4170109A (en) * 1977-11-09 1979-10-09 United Technologies Corporation Thrust augmentor having swirled flows for combustion stabilization
US4170111A (en) * 1977-11-09 1979-10-09 United Technologies Corporation Thrust augmentor

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US617022A (en) * 1899-01-03 irgens
US1319522A (en) * 1919-10-21 Carbureter
FR547536A (en) * 1921-05-24 1922-12-18 Petrol diffuser for internal combustion engine carburettors
FR560099A (en) * 1921-12-27 1923-09-28 Method and device for the use of liquid fuels in internal combustion engines
US1803213A (en) * 1927-04-04 1931-04-28 James W Wilford Fuel-oil vaporizer
US2102800A (en) * 1934-12-12 1937-12-21 Frank A Kane Method of and apparatus for gasifying a liquid fuel
US2385833A (en) * 1943-01-27 1945-10-02 Kevork K Nahigyan Fuel vaporizer for jet propulsion units
NL68431C (en) * 1944-04-15
US2438247A (en) * 1945-08-27 1948-03-23 Knudsen Hans Preheating and vaporization of fuel for internal-combustion reaction motors

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4249373A (en) * 1978-01-28 1981-02-10 Rolls-Royce Ltd. Gas turbine engine
US4898001A (en) * 1984-07-10 1990-02-06 Hitachi, Ltd. Gas turbine combustor
US4653278A (en) * 1985-08-23 1987-03-31 General Electric Company Gas turbine engine carburetor
US4730453A (en) * 1985-10-23 1988-03-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Afterburner fuel injection system
US4751815A (en) * 1986-08-29 1988-06-21 United Technologies Corporation Liquid fuel spraybar
US5001898A (en) * 1986-08-29 1991-03-26 United Technologies Corporation Fuel distributor/flameholder for a duct burner

Also Published As

Publication number Publication date
FR1000363A (en) 1952-02-11
US2622396A (en) 1952-12-23

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