FR2124141B1 - - Google Patents

Info

Publication number
FR2124141B1
FR2124141B1 FR7104265A FR7104265A FR2124141B1 FR 2124141 B1 FR2124141 B1 FR 2124141B1 FR 7104265 A FR7104265 A FR 7104265A FR 7104265 A FR7104265 A FR 7104265A FR 2124141 B1 FR2124141 B1 FR 2124141B1
Authority
FR
France
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
FR7104265A
Other languages
French (fr)
Other versions
FR2124141A1 (en
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR7104265A priority Critical patent/FR2124141B1/fr
Publication of FR2124141A1 publication Critical patent/FR2124141A1/fr
Application granted granted Critical
Publication of FR2124141B1 publication Critical patent/FR2124141B1/fr
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
FR7104265A 1971-02-09 1971-02-09 Expired FR2124141B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7104265A FR2124141B1 (en) 1971-02-09 1971-02-09

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7104265A FR2124141B1 (en) 1971-02-09 1971-02-09

Publications (2)

Publication Number Publication Date
FR2124141A1 FR2124141A1 (en) 1972-09-22
FR2124141B1 true FR2124141B1 (en) 1975-02-21

Family

ID=9071593

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7104265A Expired FR2124141B1 (en) 1971-02-09 1971-02-09

Country Status (1)

Country Link
FR (1) FR2124141B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3931707A (en) * 1975-01-08 1976-01-13 General Electric Company Augmentor flameholding apparatus

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1134847A (en) * 1954-07-20 1957-04-18 Rolls Royce Improvements to combustion equipment for gas turbine engines
FR1150640A (en) * 1956-05-18 1958-01-16 Improvements to combustion chambers, in particular for aircraft
FR1330443A (en) * 1961-08-03 1963-06-21 Rolls Royce Combustion chamber for gas turbo-engine
FR1525092A (en) * 1967-01-23 1968-05-17 Snecma Hot gas flow and cold air flow turbo-reactor

Also Published As

Publication number Publication date
FR2124141A1 (en) 1972-09-22

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Legal Events

Date Code Title Description
ST Notification of lapse