JPS5192917A - ****** *************e*****no******** - Google Patents

****** *************e*****no********

Info

Publication number
JPS5192917A
JPS5192917A JP51000027A JP2776A JPS5192917A JP S5192917 A JPS5192917 A JP S5192917A JP 51000027 A JP51000027 A JP 51000027A JP 2776 A JP2776 A JP 2776A JP S5192917 A JPS5192917 A JP S5192917A
Authority
JP
Japan
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.)
Granted
Application number
JP51000027A
Other languages
Japanese (ja)
Other versions
JPS5924260B2 (en
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 filed Critical
Publication of JPS5192917A publication Critical patent/JPS5192917A/en
Publication of JPS5924260B2 publication Critical patent/JPS5924260B2/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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/077—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
JP2776A 1975-01-02 1976-01-05 Variable cycle gas turbo fan engine Expired JPS5924260B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US53816775A 1975-01-02 1975-01-02

Publications (2)

Publication Number Publication Date
JPS5192917A true JPS5192917A (en) 1976-08-14
JPS5924260B2 JPS5924260B2 (en) 1984-06-08

Family

ID=24145795

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2776A Expired JPS5924260B2 (en) 1975-01-02 1976-01-05 Variable cycle gas turbo fan engine

Country Status (5)

Country Link
JP (1) JPS5924260B2 (en)
DE (1) DE2557735A1 (en)
FR (1) FR2296769A1 (en)
GB (1) GB1535765A (en)
IT (1) IT1052016B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005133713A (en) * 2003-10-31 2005-05-26 General Electric Co <Ge> Method and apparatus for flade engine nozzle
JP2008151135A (en) * 2006-12-18 2008-07-03 General Electric Co <Ge> Turbine engine with flow control fan, and its operation method

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4791783A (en) * 1981-11-27 1988-12-20 General Electric Company Convertible aircraft engine
GB2305976B (en) * 1981-12-21 1998-01-07 British Aerospace Jet propulsion powerplants
GB2165892B (en) * 1984-10-22 1988-10-26 Gen Electric Variable cycle engine
FR2685385B1 (en) * 1991-12-24 1995-03-31 Snecma VARIABLE CYCLE PROPULSION ENGINE FOR SUPERSONIC AIRCRAFT.
CA2091473A1 (en) * 1992-04-20 1993-10-21 Mark J. Wagner Bypass injector valve for variable cycle aircraft engines
CN108087149B (en) * 2016-11-22 2020-05-19 江西洪都航空工业集团有限责任公司 Turbojet engine with high thrust-weight ratio and low oil consumption
FR3097016B1 (en) 2019-06-06 2021-07-23 Safran Aircraft Engines CONFLUENCE STRUCTURE OF A PRIMARY VEIN AND A SECONDARY VEIN IN A DOUBLE-FLOW TURBOMACHINE
CN111594316A (en) * 2020-05-11 2020-08-28 中国航发沈阳发动机研究所 Intermediary cartridge receiver assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB978658A (en) * 1962-05-31 1964-12-23 Rolls Royce Gas turbine by-pass engines
GB980306A (en) * 1963-05-10 1965-01-13 Rolls Royce Gas turbine engine
GB1069033A (en) * 1965-01-30 1967-05-17 Rolls Royce Improvements in or relating to gas turbine jet propulsion engines
GB1313841A (en) * 1967-01-18 1973-04-18 Secr Defence Gas turbine jet propulsion engine
US3449914A (en) * 1967-12-21 1969-06-17 United Aircraft Corp Variable flow turbofan engine
DE2149619A1 (en) * 1971-10-05 1973-04-19 Motoren Turbinen Union TURBINE JET FOR VERTICAL OR SHORT-STARTING OR LANDING AIRPLANES
DE2153929A1 (en) * 1971-10-29 1973-05-10 Motoren Turbinen Union DEVICE FOR AIR EXTRACTION FOR AIRCRAFT WITH JETS

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005133713A (en) * 2003-10-31 2005-05-26 General Electric Co <Ge> Method and apparatus for flade engine nozzle
JP4658542B2 (en) * 2003-10-31 2011-03-23 ゼネラル・エレクトリック・カンパニイ Method and apparatus for a flade engine nozzle
JP2008151135A (en) * 2006-12-18 2008-07-03 General Electric Co <Ge> Turbine engine with flow control fan, and its operation method

Also Published As

Publication number Publication date
DE2557735A1 (en) 1976-07-08
GB1535765A (en) 1978-12-13
IT1052016B (en) 1981-06-20
JPS5924260B2 (en) 1984-06-08
FR2296769A1 (en) 1976-07-30
FR2296769B1 (en) 1982-11-19

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