FR69634E - Improvements to combustion devices - Google Patents

Improvements to combustion devices

Info

Publication number
FR69634E
FR69634E FR69634DA FR69634E FR 69634 E FR69634 E FR 69634E FR 69634D A FR69634D A FR 69634DA FR 69634 E FR69634 E FR 69634E
Authority
FR
France
Prior art keywords
combustion devices
combustion
devices
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
Benjamin Salmon
Jean-Henri Bertin
Hubert-Yves Vigne
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 FR69634E publication Critical patent/FR69634E/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
    • F23R3/24—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type
FR69634D 1956-07-13 1956-07-13 Improvements to combustion devices Expired FR69634E (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR69634T 1956-07-13

Publications (1)

Publication Number Publication Date
FR69634E true FR69634E (en) 1958-11-10

Family

ID=8701453

Family Applications (1)

Application Number Title Priority Date Filing Date
FR69634D Expired FR69634E (en) 1956-07-13 1956-07-13 Improvements to combustion devices

Country Status (1)

Country Link
FR (1) FR69634E (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1127152B (en) * 1959-09-18 1962-04-05 Bristol Siddeley Engines Ltd Air jet engine with an afterburner device in the jet pipe
DE1133185B (en) * 1959-04-21 1962-07-12 Snecma Combustion device on recoil engines, especially for post-combustion
US3600892A (en) * 1968-06-10 1971-08-24 Technology Uk Combustion devices
FR2348372A1 (en) * 1976-04-12 1977-11-10 Messerschmitt Boelkow Blohm Ram jet combustion chamber - has fuel rich gas flowing through venturi section diverging conically through slots into auxiliary combustion chamber

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1133185B (en) * 1959-04-21 1962-07-12 Snecma Combustion device on recoil engines, especially for post-combustion
DE1127152B (en) * 1959-09-18 1962-04-05 Bristol Siddeley Engines Ltd Air jet engine with an afterburner device in the jet pipe
US3600892A (en) * 1968-06-10 1971-08-24 Technology Uk Combustion devices
FR2348372A1 (en) * 1976-04-12 1977-11-10 Messerschmitt Boelkow Blohm Ram jet combustion chamber - has fuel rich gas flowing through venturi section diverging conically through slots into auxiliary combustion chamber

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