FR2439304A1 - Piece d'extremite d'un reacteur prevu notamment sur un avion - Google Patents

Piece d'extremite d'un reacteur prevu notamment sur un avion

Info

Publication number
FR2439304A1
FR2439304A1 FR7925838A FR7925838A FR2439304A1 FR 2439304 A1 FR2439304 A1 FR 2439304A1 FR 7925838 A FR7925838 A FR 7925838A FR 7925838 A FR7925838 A FR 7925838A FR 2439304 A1 FR2439304 A1 FR 2439304A1
Authority
FR
France
Prior art keywords
end part
aircraft
reactor provided
pipes
reactor
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
FR7925838A
Other languages
English (en)
Other versions
FR2439304B1 (fr
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 FR2439304A1 publication Critical patent/FR2439304A1/fr
Application granted granted Critical
Publication of FR2439304B1 publication Critical patent/FR2439304B1/fr
Expired 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)
  • Supports For Pipes And Cables (AREA)
  • Excavating Of Shafts Or Tunnels (AREA)
  • Exhaust Silencers (AREA)
  • Control Of Turbines (AREA)

Abstract

A.PARTIE D'EXTREMITE D'UN REACTEUR DANS LAQUELLE LE TUYAU A BUSE DE POUSSEE EST MONTE SUR UN TUYAU FIXE DE FACON A POUVOIR PIVOTER EN TOUS SENS. B.L'INVENTION EST CARACTERISEE EN CE QUE CES DEUX TUYAUX SONT REGLES EN POSITION MUTUELLE, RADIALEMENT AU MOYEN D'ORGANES DE REGLAGE ARTICULES SUR LES DEUX TUYAUX ET DEPLACABLES LONGITUDINALEMENT. C.L'INVENTION S'APPLIQUE PRINCIPALEMENT A LA CONSTITUTION DES PARTIES D'EXTREMITES DE REACTEURS PREVUS NOTAMMENT SUR DES AVIONS.
FR7925838A 1978-10-17 1979-10-17 Piece d'extremite d'un reacteur prevu notamment sur un avion Expired FR2439304B1 (fr)

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
FR2439304A1 true FR2439304A1 (fr) 1980-05-16
FR2439304B1 FR2439304B1 (fr) 1985-07-19

Family

ID=6052391

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7925838A Expired FR2439304B1 (fr) 1978-10-17 1979-10-17 Piece d'extremite d'un reacteur prevu notamment sur un avion

Country Status (7)

Country Link
US (1) US4266725A (fr)
JP (1) JPS5557648A (fr)
DE (1) DE2845149C2 (fr)
FR (1) FR2439304B1 (fr)
GB (1) GB2032862B (fr)
IT (1) IT1164837B (fr)
SE (1) SE443549B (fr)

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
EP0281264B1 (fr) * 1987-02-26 1990-10-24 ROLLS-ROYCE plc Tuyère propulsive orientable à section variable
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

Citations (6)

* 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
US2921435A (en) * 1957-10-07 1960-01-19 Ryan Aeronautical Company Directional control for aircraft
US3438581A (en) * 1967-02-06 1969-04-15 Continental Aviat & Eng Corp Internally gimbaled vectoring nozzle
FR2072009A7 (fr) * 1969-12-23 1971-09-24 Messerschmitt Boelkow Blohm
DE2639474A1 (de) * 1976-09-02 1978-03-09 Messerschmitt Boelkow Blohm Schwenkanordnung fuer schubduesen

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
FR1215236A (fr) * 1958-11-12 1960-04-15 Snecma Tuyère réglable et propulseur à réaction équipé d'une telle tuyère
US3599875A (en) * 1969-02-10 1971-08-17 United Aircraft Corp Translating air scoop ejector nozzle
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

Patent Citations (6)

* 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
US2921435A (en) * 1957-10-07 1960-01-19 Ryan Aeronautical Company Directional control for aircraft
US3438581A (en) * 1967-02-06 1969-04-15 Continental Aviat & Eng Corp Internally gimbaled vectoring nozzle
FR2072009A7 (fr) * 1969-12-23 1971-09-24 Messerschmitt Boelkow Blohm
DE2639474A1 (de) * 1976-09-02 1978-03-09 Messerschmitt Boelkow Blohm Schwenkanordnung fuer schubduesen

Also Published As

Publication number Publication date
JPS6120704B2 (fr) 1986-05-23
IT1164837B (it) 1987-04-15
US4266725A (en) 1981-05-12
FR2439304B1 (fr) 1985-07-19
IT7950559A0 (it) 1979-10-15
DE2845149A1 (de) 1980-04-24
GB2032862B (en) 1982-09-15
SE7907967L (sv) 1980-04-18
JPS5557648A (en) 1980-04-28
DE2845149C2 (de) 1982-03-04
SE443549B (sv) 1986-03-03
GB2032862A (en) 1980-05-14

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse
ST Notification of lapse