GB653626A - Improvements in or relating to liquid fuel burners - Google Patents

Improvements in or relating to liquid fuel burners

Info

Publication number
GB653626A
GB653626A GB3292147A GB3292147A GB653626A GB 653626 A GB653626 A GB 653626A GB 3292147 A GB3292147 A GB 3292147A GB 3292147 A GB3292147 A GB 3292147A GB 653626 A GB653626 A GB 653626A
Authority
GB
United Kingdom
Prior art keywords
extension
liquid fuel
chamber
open end
axis
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
GB3292147A
Inventor
Arthur Charles Runcim Thompson
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB3292147A priority Critical patent/GB653626A/en
Publication of GB653626A publication Critical patent/GB653626A/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)

Abstract

653,626. Liquid fuel burners. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. Dec. 13, 1947, No. 32921. [Class 75(i)] In a liquid fuel burner of the spill type comprising a swirl chamber 7 Fig. 2, having tangential fuel inlet ports 8, the spill tube 14 has a tubular extension 26 extending towards the discharge orifice 10 for such a length that the liquid fuel swirling around said extension 26 reaches the open end thereof only after it has lost a substantial part of its kinetic energy. The area of the annular section contained between the open end of the extension 26 and the radially adjacent wall of the chamber 7 may be substantially equal to the cross sectional area of the extension 26. As shown in Fig. 3 the tubular extension 29 may be connected to the tube 14 by a ball or other universal joint 31, 32, whereby the extension 29 may align itself automatically with the axis of the fuelvortex and so compensate for any slight offsetting of the orifice 10 relative to the axis of the chamber 7.
GB3292147A 1947-12-13 1947-12-13 Improvements in or relating to liquid fuel burners Expired GB653626A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3292147A GB653626A (en) 1947-12-13 1947-12-13 Improvements in or relating to liquid fuel burners

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3292147A GB653626A (en) 1947-12-13 1947-12-13 Improvements in or relating to liquid fuel burners

Publications (1)

Publication Number Publication Date
GB653626A true GB653626A (en) 1951-05-23

Family

ID=10345980

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3292147A Expired GB653626A (en) 1947-12-13 1947-12-13 Improvements in or relating to liquid fuel burners

Country Status (1)

Country Link
GB (1) GB653626A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1476748B1 (en) * 1965-10-12 1970-12-17 Daimler Benz Ag Filter device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1476748B1 (en) * 1965-10-12 1970-12-17 Daimler Benz Ag Filter device

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