GB658136A - Combustion chamber for liquid fuel - Google Patents

Combustion chamber for liquid fuel

Info

Publication number
GB658136A
GB658136A GB1314549A GB1314549A GB658136A GB 658136 A GB658136 A GB 658136A GB 1314549 A GB1314549 A GB 1314549A GB 1314549 A GB1314549 A GB 1314549A GB 658136 A GB658136 A GB 658136A
Authority
GB
United Kingdom
Prior art keywords
burner
liquid fuel
fuel
combustion chamber
guide vanes
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
GB1314549A
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.)
SVENSKA TURBINFAB AB
Svenska Turbinfabriks Ljungstrom AB
Original Assignee
SVENSKA TURBINFAB AB
Svenska Turbinfabriks Ljungstrom AB
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 SVENSKA TURBINFAB AB, Svenska Turbinfabriks Ljungstrom AB filed Critical SVENSKA TURBINFAB AB
Priority to GB1314549A priority Critical patent/GB658136A/en
Publication of GB658136A publication Critical patent/GB658136A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

658,136. Liquid-fuel burners. F A I R - WEATHER, H. G. C. (Svenska Turbinfabriks Aktiebolaget Ljungstrom). May 17, 1949, No. 13145. [Class 75(i)] [Also in Group XII] A liquid fuel burner has a central fuel inlet nozzle 4 and a surrounding combustion air inlet, an annular set of guiding members being arranged in the air inlet and comprising alternately oppositelyinclined guide vanes 5 so that the air enters the burner in a series of alternately oppositely-rotating helices. The burner may be air-jacketted or have material insulation. The guide vanes 5b are mounted between a central support 13 and a cylindrical wall 5a.
GB1314549A 1949-05-17 1949-05-17 Combustion chamber for liquid fuel Expired GB658136A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1314549A GB658136A (en) 1949-05-17 1949-05-17 Combustion chamber for liquid fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1314549A GB658136A (en) 1949-05-17 1949-05-17 Combustion chamber for liquid fuel

Publications (1)

Publication Number Publication Date
GB658136A true GB658136A (en) 1951-10-03

Family

ID=10017677

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1314549A Expired GB658136A (en) 1949-05-17 1949-05-17 Combustion chamber for liquid fuel

Country Status (1)

Country Link
GB (1) GB658136A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2932378A1 (en) * 1978-08-19 1980-02-21 Rolls Royce COMBUSTION CHAMBER FOR GAS TURBINE ENGINES
US4655044A (en) * 1983-12-21 1987-04-07 United Technologies Corporation Coated high temperature combustor liner
CN116164310A (en) * 2021-11-25 2023-05-26 哈尔滨工业大学 Combustion chamber head part structure of adjustable open-close type gas turbine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2932378A1 (en) * 1978-08-19 1980-02-21 Rolls Royce COMBUSTION CHAMBER FOR GAS TURBINE ENGINES
US4655044A (en) * 1983-12-21 1987-04-07 United Technologies Corporation Coated high temperature combustor liner
CN116164310A (en) * 2021-11-25 2023-05-26 哈尔滨工业大学 Combustion chamber head part structure of adjustable open-close type gas turbine
CN116164310B (en) * 2021-11-25 2024-06-11 哈尔滨工业大学 Combustion chamber head part structure of adjustable open-close type gas turbine

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