FR1230868A - Thrust Boost System for Jet Engines - Google Patents

Thrust Boost System for Jet Engines

Info

Publication number
FR1230868A
FR1230868A FR800647A FR800647A FR1230868A FR 1230868 A FR1230868 A FR 1230868A FR 800647 A FR800647 A FR 800647A FR 800647 A FR800647 A FR 800647A FR 1230868 A FR1230868 A FR 1230868A
Authority
FR
France
Prior art keywords
jet engines
boost system
thrust boost
thrust
engines
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
FR800647A
Other languages
French (fr)
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to FR800647A priority Critical patent/FR1230868A/en
Priority claimed from CH7862059A external-priority patent/CH375176A/en
Application granted granted Critical
Publication of FR1230868A publication Critical patent/FR1230868A/en
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
    • F02C7/228—Dividing fuel between various burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR800647A 1959-07-21 1959-07-21 Thrust Boost System for Jet Engines Expired FR1230868A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR800647A FR1230868A (en) 1959-07-21 1959-07-21 Thrust Boost System for Jet Engines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR800647A FR1230868A (en) 1959-07-21 1959-07-21 Thrust Boost System for Jet Engines
CH7862059A CH375176A (en) 1959-09-24 1959-09-24 Thrust booster on jet engine

Publications (1)

Publication Number Publication Date
FR1230868A true FR1230868A (en) 1960-09-20

Family

ID=25738397

Family Applications (1)

Application Number Title Priority Date Filing Date
FR800647A Expired FR1230868A (en) 1959-07-21 1959-07-21 Thrust Boost System for Jet Engines

Country Status (1)

Country Link
FR (1) FR1230868A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1272637B (en) * 1963-05-24 1968-07-11 Dowty Fuel Syst Ltd Control device for gas turbine jet engines
FR2588920A1 (en) * 1985-10-23 1987-04-24 Snecma POSTCOMBUSTION TURBOREACTOR WITH INDIVIDUAL RADIAL POSTCOMBUSTION INJECTORS
FR2629136A1 (en) * 1985-09-17 1989-09-29 Aerospatiale STATOREACTOR PROVIDED WITH A PLURALITY OF CARBIDE AND MISSILE AIR SUPPLY SLEEVES PROVIDED WITH SUCH A STATOREACTOR

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1272637B (en) * 1963-05-24 1968-07-11 Dowty Fuel Syst Ltd Control device for gas turbine jet engines
FR2629136A1 (en) * 1985-09-17 1989-09-29 Aerospatiale STATOREACTOR PROVIDED WITH A PLURALITY OF CARBIDE AND MISSILE AIR SUPPLY SLEEVES PROVIDED WITH SUCH A STATOREACTOR
FR2588920A1 (en) * 1985-10-23 1987-04-24 Snecma POSTCOMBUSTION TURBOREACTOR WITH INDIVIDUAL RADIAL POSTCOMBUSTION INJECTORS
EP0222654A1 (en) * 1985-10-23 1987-05-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Gas turbine engine with an afterburner having radially disposed individual atomizers
US4730453A (en) * 1985-10-23 1988-03-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Afterburner fuel injection system

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