JPS49135015A - - Google Patents

Info

Publication number
JPS49135015A
JPS49135015A JP48128398A JP12839873A JPS49135015A JP S49135015 A JPS49135015 A JP S49135015A JP 48128398 A JP48128398 A JP 48128398A JP 12839873 A JP12839873 A JP 12839873A JP S49135015 A JPS49135015 A JP S49135015A
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
JP48128398A
Other languages
Japanese (ja)
Other versions
JPS5521179B2 (US06653308-20031125-C00199.png
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 JPS49135015A publication Critical patent/JPS49135015A/ja
Publication of JPS5521179B2 publication Critical patent/JPS5521179B2/ja
Expired 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
    • F02K3/075Plants 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

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)
JP12839873A 1972-11-17 1973-11-16 Expired JPS5521179B2 (US06653308-20031125-C00199.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5316072A GB1415679A (en) 1972-11-17 1972-11-17 Gas turbine engine powerplant

Publications (2)

Publication Number Publication Date
JPS49135015A true JPS49135015A (US06653308-20031125-C00199.png) 1974-12-26
JPS5521179B2 JPS5521179B2 (US06653308-20031125-C00199.png) 1980-06-07

Family

ID=10466838

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12839873A Expired JPS5521179B2 (US06653308-20031125-C00199.png) 1972-11-17 1973-11-16

Country Status (6)

Country Link
US (1) US3913321A (US06653308-20031125-C00199.png)
JP (1) JPS5521179B2 (US06653308-20031125-C00199.png)
DE (1) DE2356699A1 (US06653308-20031125-C00199.png)
FR (1) FR2207244B1 (US06653308-20031125-C00199.png)
GB (1) GB1415679A (US06653308-20031125-C00199.png)
IT (1) IT996472B (US06653308-20031125-C00199.png)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4052845A (en) * 1974-06-20 1977-10-11 United Technologies Corporation Variable ratio bypass gas turbine engine with flow diverter valve
GB2242172B (en) * 1982-03-23 1991-12-11 Rolls Royce Plc Gas turbine engine
US4569199A (en) * 1982-09-29 1986-02-11 The Boeing Company Turboprop engine and method of operating the same
JPS59106958A (ja) * 1982-12-13 1984-06-20 東洋製罐株式会社 アルミニウム層を含む積層体
US5107675A (en) * 1983-03-18 1992-04-28 Rolls-Royce Limited Gas turbine engine
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
DE3467601D1 (en) * 1984-04-02 1987-12-23 Boeing Co Turboprop engine
US4979363A (en) * 1984-11-17 1990-12-25 Rolls-Royce Plc Diverter valve with bypass duct obturator
GB2192940B (en) * 1986-07-25 1990-10-31 Rolls Royce Plc A variable area aircraft air intake
GB2192941B (en) * 1986-07-25 1990-10-03 Rolls Royce Plc A variable area aircraft air intake
US5417055A (en) * 1988-06-28 1995-05-23 Rolls-Royce Plc Valve for diverting fluid flows in turbomachines
GB2301402B (en) * 1988-12-02 1997-09-03 Rolls Royce Plc Valve for diverting fluid flows in gas turbine engines
DE9421496U1 (de) * 1993-05-15 1996-01-18 Ueth & Haug GmbH, 78532 Tuttlingen Vorrichtung zum Austrennen von Endoprothesen
RU2165547C2 (ru) * 1998-03-17 2001-04-20 Владимир Иосифович Белоус Многоступенчатый осевой компрессор авиационного двигателя

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4949013A (US06653308-20031125-C00199.png) * 1972-05-25 1974-05-13

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3316717A (en) * 1965-09-15 1967-05-02 Gen Motors Corp Dual fan engine
US3528246A (en) * 1966-12-29 1970-09-15 Helen M Fischer Fan arrangement for high bypass ratio turbofan engine
US3688504A (en) * 1970-11-27 1972-09-05 Gen Electric Bypass valve control
BE791058A (fr) * 1971-11-08 1973-03-01 Boeing Co Moteurs a taux de derivation accru ou variable
US3792584A (en) * 1972-02-16 1974-02-19 Boeing Co Increased or variable bypass ratio engines
US3841091A (en) * 1973-05-21 1974-10-15 Gen Electric Multi-mission tandem propulsion system

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4949013A (US06653308-20031125-C00199.png) * 1972-05-25 1974-05-13

Also Published As

Publication number Publication date
GB1415679A (en) 1975-11-26
FR2207244A1 (US06653308-20031125-C00199.png) 1974-06-14
FR2207244B1 (US06653308-20031125-C00199.png) 1978-12-01
IT996472B (it) 1975-12-10
DE2356699A1 (de) 1974-05-30
US3913321A (en) 1975-10-21
JPS5521179B2 (US06653308-20031125-C00199.png) 1980-06-07

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