GB673713A - Liquid fuel burner - Google Patents

Liquid fuel burner

Info

Publication number
GB673713A
GB673713A GB32182/49A GB3218249A GB673713A GB 673713 A GB673713 A GB 673713A GB 32182/49 A GB32182/49 A GB 32182/49A GB 3218249 A GB3218249 A GB 3218249A GB 673713 A GB673713 A GB 673713A
Authority
GB
United Kingdom
Prior art keywords
fuel
passageway
liquid
nozzles
pipe
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
GB32182/49A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB673713A publication Critical patent/GB673713A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)

Abstract

673,713. Liquid-fuel burners. MESCHINO, R. G. Dec. 15, 1949 [Dec. 30, 1948], No. '32182/49. Class 75(i) In a liquid fuel burner in which fuel under pressure is passed through ports leading non-radially to an open passageway connecting nozzle orifices at opposite ends thereof, the ports enter the passageway in a like torque-inducing direction so as to produce a swirling, annular body of fuel having an air core extending through the nozzle orifices. Liquid fuel supplied through a conduit 11 to an annular chamber 35 and by a duct 19 therefrom to an annular chamber 35<SP>1</SP> passes through ports 33, 33<SP>1</SP> leading tangentially from the chambers 35, 35<SP>1</SP> into a concentric passageway 36, 36<SP>1</SP> having nozzles 13, 14 at opposite ends to form a swirling body of liquid with an air core 39 extending through the nozzles 13, 14, thus ensuring stability by the absence of any drag at an end wall. The burner shown is a spill-type burner in which the swirl chambers 31, 31<SP>1</SP>, are of greater diameter 'than the passageway 36, 36<SP>1</SP> with the spill returned to the source through a pipe 12.. In a duplex type arrangement, Fig. 6 (not shown), fuel is supplied at constant pressure through one pipe 42 and, at a variable pressure, through a second pipe 43. The fuel issuing from nozzles 13, 14 may be apportioned by a suitable choice of their outlet orifice diameters.
GB32182/49A 1948-12-30 1949-12-15 Liquid fuel burner Expired GB673713A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US673713XA 1948-12-30 1948-12-30

Publications (1)

Publication Number Publication Date
GB673713A true GB673713A (en) 1952-06-11

Family

ID=22075555

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32182/49A Expired GB673713A (en) 1948-12-30 1949-12-15 Liquid fuel burner

Country Status (1)

Country Link
GB (1) GB673713A (en)

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