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FR1380744A - Perfectionnement aux rampes d'injection des turbo-machines - Google Patents

Perfectionnement aux rampes d'injection des turbo-machines

Info

Publication number
FR1380744A
FR1380744A FR951782A FR951782A FR1380744A FR 1380744 A FR1380744 A FR 1380744A FR 951782 A FR951782 A FR 951782A FR 951782 A FR951782 A FR 951782A FR 1380744 A FR1380744 A FR 1380744A
Authority
FR
France
Prior art keywords
turbo
improvement
machine injection
injection rails
rails
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
FR951782A
Other languages
English (en)
Inventor
Henry Leon Guilbert
Louis Jules Bauger
Marcel Jean Baraut
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 FR951782A priority Critical patent/FR1380744A/fr
Application granted granted Critical
Publication of FR1380744A publication Critical patent/FR1380744A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR951782A 1963-10-25 1963-10-25 Perfectionnement aux rampes d'injection des turbo-machines Expired FR1380744A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR951782A FR1380744A (fr) 1963-10-25 1963-10-25 Perfectionnement aux rampes d'injection des turbo-machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR951782A FR1380744A (fr) 1963-10-25 1963-10-25 Perfectionnement aux rampes d'injection des turbo-machines

Publications (1)

Publication Number Publication Date
FR1380744A true FR1380744A (fr) 1964-12-04

Family

ID=8815159

Family Applications (1)

Application Number Title Priority Date Filing Date
FR951782A Expired FR1380744A (fr) 1963-10-25 1963-10-25 Perfectionnement aux rampes d'injection des turbo-machines

Country Status (1)

Country Link
FR (1) FR1380744A (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2471480A1 (fr) * 1979-12-13 1981-06-19 Snecma Dispositif d'injection pour chambre a combustion de moteur a turbine
FR2504195A1 (fr) * 1981-04-17 1982-10-22 Gen Electric Systeme d'alimentation en combustible des turbines a gaz
CH666340A5 (en) * 1985-05-29 1988-07-15 Bbc Brown Boveri & Cie Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
EP0495587A1 (fr) * 1991-01-18 1992-07-22 General Electric Company Rampe de distribution de carburant pour turbine à gaz
US5231833A (en) * 1991-01-18 1993-08-03 General Electric Company Gas turbine engine fuel manifold
WO1994008179A1 (fr) * 1992-09-28 1994-04-14 Parker-Hannifin Corporation Circuit de refroidissement a plusieurs passages pour buse d'injection de carburant de turbine a gaz
WO1996000345A1 (fr) * 1994-06-24 1996-01-04 United Technologies Corporation Support d'injecteur de carburant d'un recipient sous pression, destine a un moteur industriel a turbine a gaz
EP2326816A4 (fr) * 2008-08-20 2015-10-14 Woodward Inc Tige/support d injecteur de carburant

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2471480A1 (fr) * 1979-12-13 1981-06-19 Snecma Dispositif d'injection pour chambre a combustion de moteur a turbine
EP0030880B1 (fr) * 1979-12-13 1983-08-31 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif d'injection pour chambre à combustion de moteur à turbine
FR2504195A1 (fr) * 1981-04-17 1982-10-22 Gen Electric Systeme d'alimentation en combustible des turbines a gaz
CH666340A5 (en) * 1985-05-29 1988-07-15 Bbc Brown Boveri & Cie Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
EP0495587A1 (fr) * 1991-01-18 1992-07-22 General Electric Company Rampe de distribution de carburant pour turbine à gaz
US5231833A (en) * 1991-01-18 1993-08-03 General Electric Company Gas turbine engine fuel manifold
WO1994008179A1 (fr) * 1992-09-28 1994-04-14 Parker-Hannifin Corporation Circuit de refroidissement a plusieurs passages pour buse d'injection de carburant de turbine a gaz
US5423178A (en) * 1992-09-28 1995-06-13 Parker-Hannifin Corporation Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle
US5570580A (en) * 1992-09-28 1996-11-05 Parker-Hannifin Corporation Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle
WO1996000345A1 (fr) * 1994-06-24 1996-01-04 United Technologies Corporation Support d'injecteur de carburant d'un recipient sous pression, destine a un moteur industriel a turbine a gaz
EP2326816A4 (fr) * 2008-08-20 2015-10-14 Woodward Inc Tige/support d injecteur de carburant

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