GB663485A - Improvements relating to liquid fuel burners - Google Patents

Improvements relating to liquid fuel burners

Info

Publication number
GB663485A
GB663485A GB1564149A GB1564149A GB663485A GB 663485 A GB663485 A GB 663485A GB 1564149 A GB1564149 A GB 1564149A GB 1564149 A GB1564149 A GB 1564149A GB 663485 A GB663485 A GB 663485A
Authority
GB
United Kingdom
Prior art keywords
fitting
liquid fuel
fuel burners
orifice
improvements relating
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
GB1564149A
Inventor
Squire Ronald Jackson
Edmund Cross
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 GB1564149A priority Critical patent/GB663485A/en
Publication of GB663485A publication Critical patent/GB663485A/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 
    • F23C5/00—Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
    • F23C5/02—Structural details of mounting

Abstract

663,485. Liquid-fuel burners. LUCAS, Ltd., J. May 22, 1950 [June 13, 1949], No. 15641/49. Class 75(i) In a mounting for a liquid fuel burner detachment of a hollow first fitting f, closing apertures in inner and outer air jacket walls e, a enables a second fitting m, arranged within fitting f and carrying at o n e end a nozzle d and at the other end extending through a gland u and connected to fuel supply pipes s, t, to bE withdrawn. Orifice k in the wall of the first fitting f and orifice q in the second fitting m enable air to pass from the air jacket to the burner nozzle d. A sleeve 3 and the fuel supply pipe s are held in position by a hollow nut 5 pressing the conical pipe end 6 into a countersink in a lateral hole in the projectend r of the second member.
GB1564149A 1949-06-13 1949-06-13 Improvements relating to liquid fuel burners Expired GB663485A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1564149A GB663485A (en) 1949-06-13 1949-06-13 Improvements relating to liquid fuel burners

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1564149A GB663485A (en) 1949-06-13 1949-06-13 Improvements relating to liquid fuel burners

Publications (1)

Publication Number Publication Date
GB663485A true GB663485A (en) 1951-12-19

Family

ID=10062805

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1564149A Expired GB663485A (en) 1949-06-13 1949-06-13 Improvements relating to liquid fuel burners

Country Status (1)

Country Link
GB (1) GB663485A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3026675A (en) * 1958-08-22 1962-03-27 Snecma Device for the air intake into the primary zone of a combustion chamber in a turbo-machine
US3032990A (en) * 1949-10-22 1962-05-08 Gen Electric Fuel nozzle for gas turbine engine
US3403510A (en) * 1966-11-23 1968-10-01 United Aircraft Corp Removable and replaceable fuel nozzle holder assembly for an annular combustion burner

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3032990A (en) * 1949-10-22 1962-05-08 Gen Electric Fuel nozzle for gas turbine engine
US3026675A (en) * 1958-08-22 1962-03-27 Snecma Device for the air intake into the primary zone of a combustion chamber in a turbo-machine
US3403510A (en) * 1966-11-23 1968-10-01 United Aircraft Corp Removable and replaceable fuel nozzle holder assembly for an annular combustion burner

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