FR2418873A1 - Tube de reacteur pour la propulsion et la commande des avions - Google Patents

Tube de reacteur pour la propulsion et la commande des avions

Info

Publication number
FR2418873A1
FR2418873A1 FR7904261A FR7904261A FR2418873A1 FR 2418873 A1 FR2418873 A1 FR 2418873A1 FR 7904261 A FR7904261 A FR 7904261A FR 7904261 A FR7904261 A FR 7904261A FR 2418873 A1 FR2418873 A1 FR 2418873A1
Authority
FR
France
Prior art keywords
reactor tube
tubular element
control
around
airplane propulsion
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
FR7904261A
Other languages
English (en)
Other versions
FR2418873B1 (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 GmbH
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 FR2418873A1 publication Critical patent/FR2418873A1/fr
Application granted granted Critical
Publication of FR2418873B1 publication Critical patent/FR2418873B1/fr
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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Joints Allowing Movement (AREA)
  • Catching Or Destruction (AREA)

Abstract

Ce tube de réacteur est du type comportant un premier élément tubulaire fixe sur lequel un second élément tubulaire muni d'une tuyère de poussée est disposé pour pivoter. Suivant l'invention, il est caractérisé en ce que des éléments de manoeuvre sont disposés sur le premier élément tubulaire 1 et sont accouplés à l'articulation par des leviers coudés 8, 9 avec le second élément tubulaire 2 de manière que celui-ci puisse pivoter soit autour d'un axe de rotation vertical, soit autour d'un axe de rotation horizontal, soit simultanément autour de ces deux axes.
FR7904261A 1978-03-03 1979-02-20 Tube de reacteur pour la propulsion et la commande des avions Granted FR2418873A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2809169A DE2809169C3 (de) 1978-03-03 1978-03-03 Strahlrohr zum Antrieb und zur Steuerung von Flugzeugen

Publications (2)

Publication Number Publication Date
FR2418873A1 true FR2418873A1 (fr) 1979-09-28
FR2418873B1 FR2418873B1 (fr) 1984-09-21

Family

ID=6033458

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7904261A Granted FR2418873A1 (fr) 1978-03-03 1979-02-20 Tube de reacteur pour la propulsion et la commande des avions

Country Status (5)

Country Link
US (1) US4281795A (fr)
DE (1) DE2809169C3 (fr)
FR (1) FR2418873A1 (fr)
GB (1) GB2015950B (fr)
IT (1) IT1115113B (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2196587B (en) * 1980-10-31 1988-08-24 Rolls Royce Jet pipe for jet propulsion in aircraft
US4732106A (en) * 1986-07-22 1988-03-22 Milad Anis I Steering control for submarines and the like
US4892253A (en) * 1988-08-15 1990-01-09 Versatron Corporation Yoke nozzle actuation system
US5505408A (en) * 1993-10-19 1996-04-09 Versatron Corporation Differential yoke-aerofin thrust vector control system
GB2342079B (en) * 1998-07-27 2002-10-23 S & C Thermofluids Ltd Rotating coanda surfaces for thrust vector
DE69918531T2 (de) * 1999-05-13 2005-08-18 Industria De Turbo Propulsores S.A., Zamudio Verstelleinrichtung für den Auslassquerschnitt einer konvergent-divergenten Schubdüse
CN114562381B (zh) * 2022-01-13 2024-01-30 中国航发沈阳发动机研究所 一种可旋转式作动筒短距可调引气喷管

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
US2765993A (en) * 1955-03-16 1956-10-09 Willard R Custer Jet propelled aircraft with channel control means
US2921435A (en) * 1957-10-07 1960-01-19 Ryan Aeronautical Company Directional control for aircraft
DE2109205A1 (de) * 1971-02-26 1972-09-07 Motoren- und Turbinen-Union München GmbH, 8000 München Vorrichtung zur Betätigung einer aus Rohrabschnitten gebildeten Strahlablenkvorrichtung
DE2639474A1 (de) * 1976-09-02 1978-03-09 Messerschmitt Boelkow Blohm Schwenkanordnung fuer schubduesen

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3155342A (en) * 1961-05-25 1964-11-03 Bolkow Entwicklungen Kg Vtol aircraft construction
US3249306A (en) * 1962-09-14 1966-05-03 Aerojet General Co Automatically adjustable rocket nozzle
US3358932A (en) * 1965-06-16 1967-12-19 Thiokol Chemical Corp Directional control for rockets
US3361362A (en) * 1965-09-02 1968-01-02 Arde Portland Inc Mounting comprised of interconnected piston and cylinder assemblies
US3727843A (en) * 1969-07-16 1973-04-17 A Parilla Duct-forming assemblies and vector control
GB1579434A (en) * 1976-04-30 1980-11-19 Sperry Ltd Combined actuation and suspension systems for exhaust nozzles of jet propelled vehicles

Patent Citations (7)

* 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
US2765993A (en) * 1955-03-16 1956-10-09 Willard R Custer Jet propelled aircraft with channel control means
US2921435A (en) * 1957-10-07 1960-01-19 Ryan Aeronautical Company Directional control for aircraft
DE2109205A1 (de) * 1971-02-26 1972-09-07 Motoren- und Turbinen-Union München GmbH, 8000 München Vorrichtung zur Betätigung einer aus Rohrabschnitten gebildeten Strahlablenkvorrichtung
US3776467A (en) * 1971-02-26 1973-12-04 Mtu Muenchen Gmbh Means for actuating a multiple tube jet defector device
DE2639474A1 (de) * 1976-09-02 1978-03-09 Messerschmitt Boelkow Blohm Schwenkanordnung fuer schubduesen

Also Published As

Publication number Publication date
DE2809169A1 (de) 1979-09-13
FR2418873B1 (fr) 1984-09-21
GB2015950B (en) 1982-06-09
DE2809169B2 (de) 1980-03-27
DE2809169C3 (de) 1980-11-27
IT1115113B (it) 1986-02-03
US4281795A (en) 1981-08-04
IT7948169A0 (it) 1979-03-01
GB2015950A (en) 1979-09-19

Similar Documents

Publication Publication Date Title
FR2397534A1 (fr) Tuyere d'ejection a section variable perfectionnee
GB881513A (en) Improvements relating to turbo-jet propulsion units in aircraft
CA2141164A1 (fr) Pelle electrique a calage variable
FR2418873A1 (fr) Tube de reacteur pour la propulsion et la commande des avions
CA2204823A1 (fr) Inverseur de poussee de turboreacteur a double flux, a obstacles lies au capot primaire
FR2433722A1 (fr) Dispositif de chargement pour fours a cuve
JPS5312030A (en) Power converter
CA2152883A1 (fr) Inverseur de poussee de turboreacteur a double flux, a obstacles lies au capot primaire
FR2376012A1 (fr) Dispositif de levage a fixer a l'arriere d'un vehicule pour en faciliter le chargement
JPS56102646A (en) Sun following mechanism
FR2396177A1 (fr) Machine pour transformer l'energie d'un courant de milieu fluide ou semi-fluide en un mouvement mecanique
SE9003836L (sv) Ryggstoedsanordning foer anvaendning i saengar
DE3169038D1 (en) Directional vibrator
JPS52139892A (en) Fuel assembly
GB1533165A (en) Scaffold for performing operations in enclosed spaces
JPS5576763A (en) Power steering device
JPS568754A (en) Tilt-away steering arrangement
FR1547154A (fr) Dispositif de commande à servo-moteur pour un robinet à soupape, utilisant la poussée de la tige de manoeuvre pour commander l'arrêt du moteur lorsque cette tige se trouve en fin de course
FR2443586A1 (fr) Statoreacteur avec commande du vecteur de poussee
GB2113797A (en) Rack-and-pinion device
JPS57207231A (en) Collapsible mount device for camera
JPS5475746A (en) Device for moving crane operating room
EP0185644A3 (fr) Mécanisme de commande pour écran de protection
JPS5545956A (en) Working car
SU546719A1 (ru) Устройство дл изменени направлени насадка

Legal Events

Date Code Title Description
DL Decision of the director general to leave to make available licences of right
ST Notification of lapse