CH326697A - Dispositif de combustion à combustible liquide - Google Patents

Dispositif de combustion à combustible liquide

Info

Publication number
CH326697A
CH326697A CH326697DA CH326697A CH 326697 A CH326697 A CH 326697A CH 326697D A CH326697D A CH 326697DA CH 326697 A CH326697 A CH 326697A
Authority
CH
Switzerland
Prior art keywords
casing
fuel
liquid fuel
oxidant
conduit
Prior art date
Application number
Other languages
English (en)
French (fr)
Inventor
Allen Sidney
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Publication of CH326697A publication Critical patent/CH326697A/fr

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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
CH326697D 1952-12-20 1953-12-11 Dispositif de combustion à combustible liquide CH326697A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB326697X 1952-12-20

Publications (1)

Publication Number Publication Date
CH326697A true CH326697A (fr) 1957-12-31

Family

ID=10342233

Family Applications (1)

Application Number Title Priority Date Filing Date
CH326697D CH326697A (fr) 1952-12-20 1953-12-11 Dispositif de combustion à combustible liquide

Country Status (2)

Country Link
BE (1) BE525083A (ko)
CH (1) CH326697A (ko)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2996288A1 (fr) * 2012-10-01 2014-04-04 Turbomeca Injecteur a double circuit de chambre de combustion de turbomachine.
CN104704294B (zh) * 2012-10-01 2016-11-30 涡轮梅坎公司 涡轮发动机燃烧室的双回路喷射器

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB780493A (en) * 1954-07-20 1957-08-07 Rolls Royce Improvements relating to combustion equipment for gas-turbine engines
US2930195A (en) * 1956-02-14 1960-03-29 United Aircraft Corp Oscillating flow combustion chamber

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2996288A1 (fr) * 2012-10-01 2014-04-04 Turbomeca Injecteur a double circuit de chambre de combustion de turbomachine.
WO2014053730A3 (fr) * 2012-10-01 2014-07-17 Turbomeca Injecteur a double circuit de chambre de combustion de turbomachine
CN104704294A (zh) * 2012-10-01 2015-06-10 涡轮梅坎公司 涡轮发动机燃烧室的双回路喷射器
JP2015531448A (ja) * 2012-10-01 2015-11-02 ターボメカＴｕｒｂｏｍｅｃａ タービンエンジンの燃焼室のための２つの回路の噴射器
CN104704294B (zh) * 2012-10-01 2016-11-30 涡轮梅坎公司 涡轮发动机燃烧室的双回路喷射器
US9927125B2 (en) 2012-10-01 2018-03-27 Turbomeca Two-circuit injector for a turbine engine combustion chamber

Also Published As

Publication number Publication date
BE525083A (ko)

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