IT1164837B - Elemento terminale di un motore a reazione in particolare previsto per un aereo - Google Patents

Elemento terminale di un motore a reazione in particolare previsto per un aereo

Info

Publication number
IT1164837B
IT1164837B IT50559/79A IT5055979A IT1164837B IT 1164837 B IT1164837 B IT 1164837B IT 50559/79 A IT50559/79 A IT 50559/79A IT 5055979 A IT5055979 A IT 5055979A IT 1164837 B IT1164837 B IT 1164837B
Authority
IT
Italy
Prior art keywords
plane
terminal element
particular intended
reaction engine
engine
Prior art date
Application number
IT50559/79A
Other languages
English (en)
Italian (it)
Other versions
IT7950559A0 (it
Inventor
Ludwig Schweikl
Christian Greune
Paul Lottes
Peter Maderitsch
Original Assignee
Mtu 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 Muenchen Gmbh filed Critical Mtu Muenchen Gmbh
Publication of IT7950559A0 publication Critical patent/IT7950559A0/it
Application granted granted Critical
Publication of IT1164837B publication Critical patent/IT1164837B/it

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)
IT50559/79A 1978-10-17 1979-10-15 Elemento terminale di un motore a reazione in particolare previsto per un aereo IT1164837B (it)

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
IT7950559A0 IT7950559A0 (it) 1979-10-15
IT1164837B true IT1164837B (it) 1987-04-15

Family

ID=6052391

Family Applications (1)

Application Number Title Priority Date Filing Date
IT50559/79A IT1164837B (it) 1978-10-17 1979-10-15 Elemento terminale di un motore a reazione in particolare previsto per un aereo

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
DE2845149A1 (de) 1980-04-24
GB2032862B (en) 1982-09-15
FR2439304B1 (fr) 1985-07-19
JPS5557648A (en) 1980-04-28
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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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19940930