GB681800A - Apparatus for burning liquid fuel - Google Patents

Apparatus for burning liquid fuel

Info

Publication number
GB681800A
GB681800A GB1831051A GB1831051A GB681800A GB 681800 A GB681800 A GB 681800A GB 1831051 A GB1831051 A GB 1831051A GB 1831051 A GB1831051 A GB 1831051A GB 681800 A GB681800 A GB 681800A
Authority
GB
United Kingdom
Prior art keywords
valve
duct
fuel
spill
orifice
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
GB1831051A
Inventor
Alan William Wilson
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.)
Shell Refining and Marketing Co Ltd
Original Assignee
Shell Refining and Marketing Co 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 Shell Refining and Marketing Co Ltd filed Critical Shell Refining and Marketing Co Ltd
Priority to GB1831051A priority Critical patent/GB681800A/en
Publication of GB681800A publication Critical patent/GB681800A/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
    • F23D11/26Burners 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 with provision for varying the rate at which the fuel is sprayed
    • F23D11/28Burners 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 with provision for varying the rate at which the fuel is sprayed with flow-back of fuel at the burner, e.g. using by-pass

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

681,800. Liquid-fuel burners. SHELL REFINING & MARKETING CO., Ltd. Aug. 2, 1951, No. 18310/51. Class 75(i) A spill type burner having a tip valve 6 to close a final outlet orifice 11 the valve 6 being connected to a piston 38 of which one face is exposed to a fuel supply duct 9 and the other to a spill duct 18 is provided with control valve means whereby the discharge line 30 of a fuel pump can be connected at will to either the fuel supply duct 9 or the spill duct 18. When the burner is in operation fuel is supplied under pressure from the line 30 through recesses 26, 25 and connecting duct 28 in a four-way valve 21 to an annular passage 8 to move the piston 38 and the tip valve 6 away from the orifice 11; the fuel spill returns through an orifice 16, holes 17, a passage 15, the spill duct 18, a recess 23 in the valve 21 and a line 29 to the fuel reservoir. When a burner is to be put out of operation but to continue to receive a fuel flow to keep the burner cool a lever 31 for the valve 21 is moved to the chain dotted position to connect the pump discharge line 30 through recesses 26, 25 and connecting duct 28 with the spill duct 18 to move the piston 38 and the tip valve 6 to close the orifice 11, the supply duct 9 meanwhile being connected through recesses 24, 23 and connecting duct 27 with the line 29 to the reservoir. A weak spring 39 normally holds the tip valve 6 in the closed position. The valve 21 may be used to control one or more burners.
GB1831051A 1951-08-02 1951-08-02 Apparatus for burning liquid fuel Expired GB681800A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1831051A GB681800A (en) 1951-08-02 1951-08-02 Apparatus for burning liquid fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1831051A GB681800A (en) 1951-08-02 1951-08-02 Apparatus for burning liquid fuel

Publications (1)

Publication Number Publication Date
GB681800A true GB681800A (en) 1952-10-29

Family

ID=10110293

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1831051A Expired GB681800A (en) 1951-08-02 1951-08-02 Apparatus for burning liquid fuel

Country Status (1)

Country Link
GB (1) GB681800A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1040980B (en) * 1956-09-21 1958-10-09 Koppers Gmbh Heinrich Drive device for hydraulic or pneumatic operation by means of a double piston motor
DE1268771B (en) * 1958-12-11 1968-05-22 Dowty Fuel Syst Ltd Device to prevent the dripping and coking of liquid fuel on atomizing nozzles operated with heavy oil
WO1982003906A1 (en) * 1981-04-30 1982-11-11 Mccormack Wallace Liquid fuel burner
EP1965054A3 (en) * 2007-02-28 2012-10-10 Mitsubishi Heavy Industries, Ltd. Gas turbine fuel nozzle apparatus and method of controlling fuel nozzle apparatus

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1040980B (en) * 1956-09-21 1958-10-09 Koppers Gmbh Heinrich Drive device for hydraulic or pneumatic operation by means of a double piston motor
DE1268771B (en) * 1958-12-11 1968-05-22 Dowty Fuel Syst Ltd Device to prevent the dripping and coking of liquid fuel on atomizing nozzles operated with heavy oil
WO1982003906A1 (en) * 1981-04-30 1982-11-11 Mccormack Wallace Liquid fuel burner
US4546921A (en) * 1981-04-30 1985-10-15 Credfeld Camtorc Limited Liquid fuel burner
EP1965054A3 (en) * 2007-02-28 2012-10-10 Mitsubishi Heavy Industries, Ltd. Gas turbine fuel nozzle apparatus and method of controlling fuel nozzle apparatus

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