GB1541408A - Combustion chambers operating on a supersonic stream chiefly for jet engines - Google Patents

Combustion chambers operating on a supersonic stream chiefly for jet engines

Info

Publication number
GB1541408A
GB1541408A GB3854868A GB3854868A GB1541408A GB 1541408 A GB1541408 A GB 1541408A GB 3854868 A GB3854868 A GB 3854868A GB 3854868 A GB3854868 A GB 3854868A GB 1541408 A GB1541408 A GB 1541408A
Authority
GB
United Kingdom
Prior art keywords
combustion chambers
jet engines
chambers operating
supersonic stream
chiefly
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
GB3854868A
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to GB3854868A priority Critical patent/GB1541408A/en
Publication of GB1541408A publication Critical patent/GB1541408A/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
    • F23R3/16—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
GB3854868A 1968-08-12 1968-08-12 Combustion chambers operating on a supersonic stream chiefly for jet engines Expired GB1541408A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3854868A GB1541408A (en) 1968-08-12 1968-08-12 Combustion chambers operating on a supersonic stream chiefly for jet engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3854868A GB1541408A (en) 1968-08-12 1968-08-12 Combustion chambers operating on a supersonic stream chiefly for jet engines

Publications (1)

Publication Number Publication Date
GB1541408A true GB1541408A (en) 1979-02-28

Family

ID=10404188

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3854868A Expired GB1541408A (en) 1968-08-12 1968-08-12 Combustion chambers operating on a supersonic stream chiefly for jet engines

Country Status (1)

Country Link
GB (1) GB1541408A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0602404A1 (en) * 1992-12-17 1994-06-22 Asea Brown Boveri Ag Gas turbine combustor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0602404A1 (en) * 1992-12-17 1994-06-22 Asea Brown Boveri Ag Gas turbine combustor

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Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed