GB643559A - Improvements relating to liquid fuel burners - Google Patents

Improvements relating to liquid fuel burners

Info

Publication number
GB643559A
GB643559A GB1878248A GB1878248A GB643559A GB 643559 A GB643559 A GB 643559A GB 1878248 A GB1878248 A GB 1878248A GB 1878248 A GB1878248 A GB 1878248A GB 643559 A GB643559 A GB 643559A
Authority
GB
United Kingdom
Prior art keywords
air
apertures
combustion chamber
liquid
tube
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
GB1878248A
Inventor
Albert Edward Clarke
Allan Kingdon North
Kenneth Hedley Holliday
John Stanley Clarke
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 GB1878248A priority Critical patent/GB643559A/en
Publication of GB643559A publication Critical patent/GB643559A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00—Subject-matter not provided for in other groups of this subclass
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
    • F23C2700/02—Combustion apparatus using liquid fuel
    • F23C2700/026—Combustion apparatus using liquid fuel with pre-vaporising means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)

Abstract

643,559. Liquid-fuel burners. LUCAS, Ltd., J. July 13, 1948, No. 18782. [Class 75(i)] [Also in Group XII] A liquid-fuel burner, for use particularly with a gas turbine or a jet-propulsion engine, comprises the combination of a liquid fuel vaporizer j, a mixing tube a which is closed at one end and has at the closed end a vapour injection nipple band adjacent air admission apertures c, a primary air tube d surrounding the mixing tube a and supplied with air at the end remote from the apertures c, and an air jacketed combustion chamber e in which the tubes a and d are coaxially mounted with the discharge end of the mixing tube a in the principal combustion zone. The vapourizer j shown is in the form of a coil surrounding the tubes a, d; and the apertures c are surrounded by a shield n having an end plate o, excess air being passed into the combustion chamber e through apertures p. Additional primary air from the surrounding duct h enters the combustion chamber e through an inlet f past a baffle g and through apertures q; and secondary air is admitted through apertures m. Tertiary air may be admitted at a position further along the chamber e. Air is supplied to the primary air tube d through one or more connections i.
GB1878248A 1948-07-13 1948-07-13 Improvements relating to liquid fuel burners Expired GB643559A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1878248A GB643559A (en) 1948-07-13 1948-07-13 Improvements relating to liquid fuel burners

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1878248A GB643559A (en) 1948-07-13 1948-07-13 Improvements relating to liquid fuel burners

Publications (1)

Publication Number Publication Date
GB643559A true GB643559A (en) 1950-09-20

Family

ID=10118329

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1878248A Expired GB643559A (en) 1948-07-13 1948-07-13 Improvements relating to liquid fuel burners

Country Status (1)

Country Link
GB (1) GB643559A (en)

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