JPH0324573B2 - - Google Patents

Info

Publication number
JPH0324573B2
JPH0324573B2 JP59170315A JP17031584A JPH0324573B2 JP H0324573 B2 JPH0324573 B2 JP H0324573B2 JP 59170315 A JP59170315 A JP 59170315A JP 17031584 A JP17031584 A JP 17031584A JP H0324573 B2 JPH0324573 B2 JP H0324573B2
Authority
JP
Japan
Prior art keywords
flow path
flap
wall
annular secondary
axis
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
JP59170315A
Other languages
English (en)
Japanese (ja)
Other versions
JPS60184933A (ja
Inventor
Debeneikusu Pieeru
Jozefu Tsuuruneeru Maruseru
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.)
NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC
Original Assignee
NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC
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 NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC filed Critical NASHIONARU DECHUUDO E DO KONSUTORYUKUSHION DE MOTOORU DABIASHION SOC
Publication of JPS60184933A publication Critical patent/JPS60184933A/ja
Publication of JPH0324573B2 publication Critical patent/JPH0324573B2/ja
Granted 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

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)
  • Supercharger (AREA)
JP59170315A 1983-08-18 1984-08-15 複流束ターボジェットエンジンの２次流束調整装置 Granted JPS60184933A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8313418 1983-08-18
FR8313418A FR2550821B1 (fr) 1983-08-18 1983-08-18 Dispositif variateur du flux secondaire d'un turboreacteur multiflux

Publications (2)

Publication Number Publication Date
JPS60184933A JPS60184933A (ja) 1985-09-20
JPH0324573B2 true JPH0324573B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1991-04-03

Family

ID=9291677

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59170315A Granted JPS60184933A (ja) 1983-08-18 1984-08-15 複流束ターボジェットエンジンの２次流束調整装置

Country Status (6)

Country Link
US (1) US4638631A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EP (1) EP0135430B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS60184933A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE3471343D1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2550821B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IL (1) IL72619A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5048286A (en) * 1990-06-29 1991-09-17 General Electric Company Bypass valve door
CA2036821A1 (en) * 1990-06-29 1991-12-30 Larry W. Stransky Bypass valve system
FR2672641B1 (fr) * 1991-02-13 1995-01-13 Snecma Dispositif de post-combustion a volets pivotants.
US5216878A (en) * 1991-06-28 1993-06-08 The Boeing Company Mixed exhaust flow supersonic jet engine and method
BR0306781B1 (pt) * 2002-01-09 2013-01-22 bocal de exaustço de turbofan e mÉtodo para reduzir ruÍdo em um motor turbofan possuindo um bocal de exaustço de turbofan.
US8128057B2 (en) * 2008-02-29 2012-03-06 General Electric Company Methods and apparatus for regulating gas turbine engine fluid flow
US20140216056A1 (en) * 2012-09-28 2014-08-07 United Technologies Corporation Heat exchange module for a turbine engine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3296800A (en) * 1967-01-10 Gas turbine power plant
US3118276A (en) * 1964-01-21 Gas turbine engines
FR1291561A (fr) * 1960-12-02 1962-04-27 Obturateur à papillons pour tri-réacteurs
FR1330633A (fr) * 1961-08-18 1963-06-21 Rolls Royce Turbo-réacteur à by-pass
US3344606A (en) * 1961-09-27 1967-10-03 United Aircraft Corp Recover bleed air turbojet
FR1377199A (fr) * 1963-12-17 1964-10-31 Rolls Royce Moteur à turbine à gaz
US3280561A (en) * 1965-06-07 1966-10-25 Gen Electric Thrust reverser mechanism
FR1496091A (fr) * 1966-04-20 1967-09-29 Snecma Tuyère d'éjection pour propulseurs à plusieurs flux moteurs, notamment à deux flux moteurs
GB1244292A (en) * 1970-01-14 1971-08-25 Rolls Royce Gas turbine engine
US3769797A (en) * 1971-10-28 1973-11-06 Us Air Force By-pass engine having a single, thrust diverter valve mechanism for a v/stol aircraft
US3974646A (en) * 1974-06-11 1976-08-17 United Technologies Corporation Turbofan engine with augmented combustion chamber using vorbix principle
FR2316443A1 (fr) * 1975-07-02 1977-01-28 Snecma Variateur du taux de dilution d'un turboreacteur multiflux
US4086761A (en) * 1976-04-26 1978-05-02 The Boeing Company Stator bypass system for turbofan engine
GB1583952A (en) * 1976-07-13 1981-02-04 Short Brothers & Harland Ltd Gas turbine engines
DE2917303A1 (de) * 1979-04-28 1980-10-30 Dornier Gmbh Antriebsanlage fuer luftfahrzeuge

Also Published As

Publication number Publication date
US4638631A (en) 1987-01-27
FR2550821A1 (fr) 1985-02-22
DE3471343D1 (en) 1988-06-23
JPS60184933A (ja) 1985-09-20
FR2550821B1 (fr) 1985-11-08
EP0135430B1 (fr) 1988-05-18
EP0135430A1 (fr) 1985-03-27
IL72619A (en) 1989-07-31
IL72619A0 (en) 1984-11-30

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Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees