IT7948169A0 - Tubo di scarico a getto per la propulsione ed il comando di aerei - Google Patents

Tubo di scarico a getto per la propulsione ed il comando di aerei

Info

Publication number
IT7948169A0
IT7948169A0 IT7948169A IT4816979A IT7948169A0 IT 7948169 A0 IT7948169 A0 IT 7948169A0 IT 7948169 A IT7948169 A IT 7948169A IT 4816979 A IT4816979 A IT 4816979A IT 7948169 A0 IT7948169 A0 IT 7948169A0
Authority
IT
Italy
Prior art keywords
propulsion
aircraft
control
exhaust pipe
jet exhaust
Prior art date
Application number
IT7948169A
Other languages
English (en)
Other versions
IT1115113B (it
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 IT7948169A0 publication Critical patent/IT7948169A0/it
Application granted granted Critical
Publication of IT1115113B publication Critical patent/IT1115113B/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
    • 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)
IT48169/79A 1978-03-03 1979-03-01 Tubo di scarico a getto per la propulsione ed il comando di aerei IT1115113B (it)

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
IT7948169A0 true IT7948169A0 (it) 1979-03-01
IT1115113B IT1115113B (it) 1986-02-03

Family

ID=6033458

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48169/79A IT1115113B (it) 1978-03-03 1979-03-01 Tubo di scarico a getto per la propulsione ed il comando di aerei

Country Status (5)

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

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

Family Cites Families (12)

* 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
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
US3776467A (en) * 1971-02-26 1973-12-04 Mtu Muenchen Gmbh Means for actuating a multiple tube jet defector device
GB1579434A (en) * 1976-04-30 1980-11-19 Sperry Ltd Combined actuation and suspension systems for exhaust nozzles of jet propelled vehicles
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
IT1115113B (it) 1986-02-03
GB2015950A (en) 1979-09-19
FR2418873A1 (fr) 1979-09-28
DE2809169A1 (de) 1979-09-13
FR2418873B1 (it) 1984-09-21
DE2809169B2 (de) 1980-03-27
DE2809169C3 (de) 1980-11-27
US4281795A (en) 1981-08-04
GB2015950B (en) 1982-06-09

Similar Documents

Publication Publication Date Title
GB2047820B (en) Exhaust pipe of turbine
DK171579A (da) Styresystem til jetmotor
IT1114372B (it) Apparecchio per montare un motore a getto in particolare sull'ala di un aeromobile
GB2009683A (en) Thrust reverser for an asymmetric aircraft exhaust nozzle
JPS5539895A (en) Actuator device of aircraft steering wing surface
DE69211557D1 (de) Verkleidungform eines unbemannten luftfahrzeuges
IT1141160B (it) Cappottatura di motore a turbina a gas
DE3175723D1 (en) Extending rocket engine exhaust nozzle assembly
IT1162567B (it) Sistema di controllo dello scappamento di una stampatrice
GB2001392A (en) Jet propulsion engine assembly for aircraft
GB2012370B (en) Air intake for supersonic air breathing jet propulsion engines
IT7949979A0 (it) Dispositivo per impianti di lancio di veicoli con propulsione a scarico di gas
IT7948169A0 (it) Tubo di scarico a getto per la propulsione ed il comando di aerei
GB2017448B (en) Method of flight guidance
IT1158286B (it) Apparecchiatura per il controllo di motori di propulsione
DE3561344D1 (de) Thrust reverser for a jet engine
IT8567530A0 (it) Elicottero con gruppo propulsore a turbina provvisto di dispositivo mascheratore di scarico
DE3363144D1 (en) Device to be deployed for the extension of the exhaust nozzle of a rocket engine
AU516321B2 (en) Tail pipe orientation of exhaust system
IT8241561A1 (it) Apparecchiatura per il controllo di motori di propulsione di veicoli
IT1167303B (it) Dispositivo di direzione per aeromobili razzi e simili con propulsione a getto
IT1132495B (it) Dispositivo di partenza per aeromobili e razzi con propulsione a getto
IT1219996B (it) Apparecchiatura per il controllo di motori a propulsione
JPS543303A (en) Method of air jet construction
IT7847587A0 (it) Apparecchiatura per comando o regolazione di getto-propulsori a turbina a gas per aerei

Legal Events

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

Effective date: 19970228