JPS4825688B1 - - Google Patents

Info

Publication number
JPS4825688B1
JPS4825688B1 JP44075937A JP7593769A JPS4825688B1 JP S4825688 B1 JPS4825688 B1 JP S4825688B1 JP 44075937 A JP44075937 A JP 44075937A JP 7593769 A JP7593769 A JP 7593769A JP S4825688 B1 JPS4825688 B1 JP S4825688B1
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.)
Pending
Application number
JP44075937A
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 JPS4825688B1 publication Critical patent/JPS4825688B1/ja
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/068Plants 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 being characterised by a short axial length relative to the diameter
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP44075937A 1968-09-27 1969-09-25 Pending JPS4825688B1 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB46076/68A GB1179204A (en) 1968-09-27 1968-09-27 Gas Turbine Power Plant.

Publications (1)

Publication Number Publication Date
JPS4825688B1 true JPS4825688B1 (ja) 1973-07-31

Family

ID=10439759

Family Applications (1)

Application Number Title Priority Date Filing Date
JP44075937A Pending JPS4825688B1 (ja) 1968-09-27 1969-09-25

Country Status (5)

Country Link
US (1) US3625008A (ja)
JP (1) JPS4825688B1 (ja)
DE (1) DE1948363A1 (ja)
FR (1) FR2018999A1 (ja)
GB (1) GB1179204A (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010089880A1 (ja) * 2009-02-06 2010-08-12 トヨタ自動車株式会社 ターボファンエンジン

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4292803A (en) * 1979-01-19 1981-10-06 Rohr Industries, Inc. Turbo fan engine mixer
GB2117054B (en) * 1982-02-17 1985-01-30 Rolls Royce Aircraft propulsion engine having a rear mounted propfan
US10421553B2 (en) * 2015-01-20 2019-09-24 United Technologies Corporation Pusher fan engine with in wing configuration
US10563516B2 (en) 2016-07-06 2020-02-18 General Electric Company Turbine engine and method of assembling

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010089880A1 (ja) * 2009-02-06 2010-08-12 トヨタ自動車株式会社 ターボファンエンジン
JP5287873B2 (ja) * 2009-02-06 2013-09-11 トヨタ自動車株式会社 ターボファンエンジン

Also Published As

Publication number Publication date
FR2018999A1 (ja) 1970-06-26
US3625008A (en) 1971-12-07
DE1948363A1 (de) 1970-04-23
GB1179204A (en) 1970-01-28

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