FR1124190A - Improvements to stato-reactors - Google Patents

Improvements to stato-reactors

Info

Publication number
FR1124190A
FR1124190A FR1124190DA FR1124190A FR 1124190 A FR1124190 A FR 1124190A FR 1124190D A FR1124190D A FR 1124190DA FR 1124190 A FR1124190 A FR 1124190A
Authority
FR
France
Prior art keywords
stato
reactors
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
Other languages
French (fr)
Inventor
Gerhard Eggers
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
Application granted granted Critical
Publication of FR1124190A publication Critical patent/FR1124190A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/24Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
FR1124190D 1955-03-29 1955-03-29 Improvements to stato-reactors Expired FR1124190A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1124190T 1955-03-29

Publications (1)

Publication Number Publication Date
FR1124190A true FR1124190A (en) 1956-10-05

Family

ID=9633685

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1124190D Expired FR1124190A (en) 1955-03-29 1955-03-29 Improvements to stato-reactors

Country Status (1)

Country Link
FR (1) FR1124190A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1192876B (en) * 1960-02-02 1965-05-13 Gen Electric Burner arrangement for a jet engine, the combustion chamber of which is surrounded by a heat exchanger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1192876B (en) * 1960-02-02 1965-05-13 Gen Electric Burner arrangement for a jet engine, the combustion chamber of which is surrounded by a heat exchanger

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