FR66338E - Perfectionnement aux turbo-machines, particulièrement destiné aux propulseurs d'aérodynes - Google Patents

Perfectionnement aux turbo-machines, particulièrement destiné aux propulseurs d'aérodynes

Info

Publication number
FR66338E
FR66338E FR66338DA FR66338E FR 66338 E FR66338 E FR 66338E FR 66338D A FR66338D A FR 66338DA FR 66338 E FR66338 E FR 66338E
Authority
FR
France
Prior art keywords
aerodyne
thrusters
turbo
machines
improvement
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
English (en)
Inventor
Michel-Robert Garnier
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 FR66338E publication Critical patent/FR66338E/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR66338D 1954-05-05 1954-05-05 Perfectionnement aux turbo-machines, particulièrement destiné aux propulseurs d'aérodynes Expired FR66338E (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR66338T 1954-05-05

Publications (1)

Publication Number Publication Date
FR66338E true FR66338E (fr) 1956-06-29

Family

ID=8698679

Family Applications (1)

Application Number Title Priority Date Filing Date
FR66338D Expired FR66338E (fr) 1954-05-05 1954-05-05 Perfectionnement aux turbo-machines, particulièrement destiné aux propulseurs d'aérodynes

Country Status (1)

Country Link
FR (1) FR66338E (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2934894A (en) * 1957-07-23 1960-05-03 Orenda Engines Ltd Fuel supply and flame stabilizing apparatus for afterburners for jet engines
DE1123163B (de) * 1958-05-23 1962-02-01 Gen Electric Rueckstosstriebwerk mit Nachverbrennungseinrichtungen
US3352113A (en) * 1964-08-19 1967-11-14 Rolls Royce Reheat combustion equipment

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2934894A (en) * 1957-07-23 1960-05-03 Orenda Engines Ltd Fuel supply and flame stabilizing apparatus for afterburners for jet engines
DE1123163B (de) * 1958-05-23 1962-02-01 Gen Electric Rueckstosstriebwerk mit Nachverbrennungseinrichtungen
US3352113A (en) * 1964-08-19 1967-11-14 Rolls Royce Reheat combustion equipment

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