JPS5557648A - End part of reversed engine - Google Patents

End part of reversed engine

Info

Publication number
JPS5557648A
JPS5557648A JP13411979A JP13411979A JPS5557648A JP S5557648 A JPS5557648 A JP S5557648A JP 13411979 A JP13411979 A JP 13411979A JP 13411979 A JP13411979 A JP 13411979A JP S5557648 A JPS5557648 A JP S5557648A
Authority
JP
Japan
Prior art keywords
end part
reversed engine
reversed
engine
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.)
Granted
Application number
JP13411979A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6120704B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html
Inventor
Shibuikeru Rudouitsuhi
Guroine Kurisuchiyan
Rotsutesu Pauru
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of JPS5557648A publication Critical patent/JPS5557648A/ja
Publication of JPS6120704B2 publication Critical patent/JPS6120704B2/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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/008—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector in any rearward direction
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient 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)
  • Joints Allowing Movement (AREA)
  • Exhaust Silencers (AREA)
  • Supports For Pipes And Cables (AREA)
  • Control Of Turbines (AREA)
  • Excavating Of Shafts Or Tunnels (AREA)
JP13411979A 1978-10-17 1979-10-16 End part of reversed engine Granted JPS5557648A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2845149A DE2845149C2 (de) 1978-10-17 1978-10-17 Strahltriebwerk, insbesondere zum Antrieb eines Flugzeugs

Publications (2)

Publication Number Publication Date
JPS5557648A true JPS5557648A (en) 1980-04-28
JPS6120704B2 JPS6120704B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1986-05-23

Family

ID=6052391

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13411979A Granted JPS5557648A (en) 1978-10-17 1979-10-16 End part of reversed engine

Country Status (7)

Country Link
US (1) US4266725A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS5557648A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2845149C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2439304B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB2032862B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT1164837B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
SE (1) SE443549B (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
FR2501786A1 (fr) * 1981-03-13 1982-09-17 Snecma Dispositif de roulement et de guidage d'une tuyere orientable de propulseur a reaction
DE3860847D1 (de) * 1987-02-26 1990-11-29 Rolls Royce Plc Schwenkbare schubduese mit variablem, verstellbarem querschnitt.
JPS6443647A (en) * 1987-08-10 1989-02-15 Nichiee Yoshida Kk Method and apparatus for preventing cracking of opening part of reinforced concrete wall
DE3909347A1 (de) * 1989-03-22 1990-09-27 Mtu Muenchen Gmbh Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete
US5261604A (en) * 1992-05-11 1993-11-16 General Electric Company Yaw vectoring blade
ES2153300B1 (es) * 1998-09-04 2001-07-16 Turbo Propulsores Ind Mecanismo de guiado para toberas orientables de geometria variable aplicables a turbinas de gas.
JP2001123829A (ja) * 1999-10-25 2001-05-08 Honda Motor Co Ltd カバー部材取付構造

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB600397A (en) * 1946-08-27 1948-04-07 Fairey Aviat Co Ltd Improvements in or relating to controlling means for high speed aircraft
FR1025827A (fr) * 1950-10-11 1953-04-20 Perfectionnement apporté aux engins aériens à réaction
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
US2921435A (en) * 1957-10-07 1960-01-19 Ryan Aeronautical Company Directional control for aircraft
FR1215236A (fr) * 1958-11-12 1960-04-15 Snecma Tuyère réglable et propulseur à réaction équipé d'une telle tuyère
US3438581A (en) * 1967-02-06 1969-04-15 Continental Aviat & Eng Corp Internally gimbaled vectoring nozzle
US3599875A (en) * 1969-02-10 1971-08-17 United Aircraft Corp Translating air scoop ejector nozzle
GB1306588A (en) * 1969-12-23 1973-02-14 Messerschmitt Boelkow Blohm Nozzle assembly for jet propulsion engines
GB1386480A (en) * 1972-07-08 1975-03-05 British Aircraft Corp Ltd Guided missiles
US3972475A (en) * 1975-07-31 1976-08-03 United Technologies Corporation Nozzle construction providing for thermal growth
DE2639474C2 (de) * 1976-09-02 1982-06-16 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkanordnung für eine Schubdüse

Also Published As

Publication number Publication date
IT1164837B (it) 1987-04-15
DE2845149A1 (de) 1980-04-24
GB2032862B (en) 1982-09-15
FR2439304B1 (fr) 1985-07-19
SE7907967L (sv) 1980-04-18
DE2845149C2 (de) 1982-03-04
JPS6120704B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1986-05-23
FR2439304A1 (fr) 1980-05-16
US4266725A (en) 1981-05-12
SE443549B (sv) 1986-03-03
GB2032862A (en) 1980-05-14
IT7950559A0 (it) 1979-10-15

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