GR20060100385A - Διαταξη ελεγχου της στροφης περι κατακορυφου αξονα για ενα ακροφυσιο που εχει ορθογωνικη διατομη εξοδου - Google Patents

Διαταξη ελεγχου της στροφης περι κατακορυφου αξονα για ενα ακροφυσιο που εχει ορθογωνικη διατομη εξοδου

Info

Publication number
GR20060100385A
GR20060100385A GR20060100385A GR20060100385A GR20060100385A GR 20060100385 A GR20060100385 A GR 20060100385A GR 20060100385 A GR20060100385 A GR 20060100385A GR 20060100385 A GR20060100385 A GR 20060100385A GR 20060100385 A GR20060100385 A GR 20060100385A
Authority
GR
Greece
Prior art keywords
nozzle
control device
aircraft
yaw
supersonic
Prior art date
Application number
GR20060100385A
Other languages
English (en)
Inventor
Francois Buffenoir
Andre Lafond
Original Assignee
Snecma Propulsion Solide
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 Snecma Propulsion Solide filed Critical Snecma Propulsion Solide
Publication of GR20060100385A publication Critical patent/GR20060100385A/el

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F05D2220/00—Application
    • F05D2220/80—Application in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/12—Two-dimensional rectangular
    • 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
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent
    • 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
    • F05D2250/50—Inlet or outlet
    • F05D2250/52—Outlet
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Toys (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Η εφεύρεση αναφέρεται σε μία διάταξη ελέγχου της στροφής περί κατακόρυφο άξονα για ένα αεροσκάφος (100) εφοδιασμένο με ένα υπερηχητικό ακροφύσιο (110) που έχει ορθογωνική ή επίπεδη διατομή το οποίο περιλαμβάνει έναν υπερηχητικό λαιμό (111) εκτεινόμενο δι' ενός αποκλίνοντος τμήματος (112) στο οποίο λαμβάνει χώρα υπερηχητική ροή (Esup). Προκειμένου να επιτραπεί ο έλεγχος της στροφής περί κατακόρυφοάξονα του αεροσκάφους εν απουσία κατακόρυφου πτερυγίου, η διάταξη της εφευρέσεως χρησιμοποίει επιφάνειες ελέγχου πίδακα καυσαερίων (120) υπό την μορφήαεροδυναμικών σωμάτων που τοποθετούνται στο αποκλίνον τμήμα (112) του ακροφυσίου. Οι επιφάνειες ελέγχου μπορούν να κινούνται περί αντίστοιχους άξονεςπεριστροφής (121) προκειμένου να παραχθεί μία πλευρική δύναμη όταν είναι σε εκτραπείσα θέση, έτσι ώστε να επιτραπεί στο αεροσκάφος (100) να στραφεί περι τον κατακόρυφό του άξονα (102) ("yaw axis").
GR20060100385A 2005-07-06 2006-06-29 Διαταξη ελεγχου της στροφης περι κατακορυφου αξονα για ενα ακροφυσιο που εχει ορθογωνικη διατομη εξοδου GR20060100385A (el)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0507190A FR2888211B1 (fr) 2005-07-06 2005-07-06 Dispositif et procede de pilotage en lacets pour tuyere a section de sortie rectangulaire

Publications (1)

Publication Number Publication Date
GR20060100385A true GR20060100385A (el) 2007-02-15

Family

ID=36095920

Family Applications (1)

Application Number Title Priority Date Filing Date
GR20060100385A GR20060100385A (el) 2005-07-06 2006-06-29 Διαταξη ελεγχου της στροφης περι κατακορυφου αξονα για ενα ακροφυσιο που εχει ορθογωνικη διατομη εξοδου

Country Status (9)

Country Link
US (1) US7628356B2 (el)
DE (1) DE102006031625A1 (el)
ES (1) ES2286957B1 (el)
FR (1) FR2888211B1 (el)
GB (1) GB2428029B (el)
GR (1) GR20060100385A (el)
IL (1) IL176632A (el)
IT (1) ITTO20060493A1 (el)
SE (1) SE532283C2 (el)

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SE527787C2 (sv) * 2004-11-05 2006-06-07 Volvo Aero Corp Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning
US20100281874A1 (en) * 2007-01-09 2010-11-11 Rolls-Royce Corporation Airflow vectoring member
US8020367B2 (en) * 2007-03-16 2011-09-20 General Electric Company Nozzle with yaw vectoring vane
US8240125B2 (en) * 2007-07-26 2012-08-14 The Boeing Company Thrust vectoring system and method
FR2919268B1 (fr) * 2007-07-26 2009-10-02 Airbus France Sa Avion a decollage court
DE102008022289B4 (de) 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper
DE102010023938A1 (de) * 2010-06-16 2011-12-22 Eads Deutschland Gmbh Angetriebenes Fluggerät, insbesondere als Nurflügler und/oder mit geringer Radarsignatur ausgebildetes Fluggerät
US8469308B2 (en) * 2010-11-12 2013-06-25 Textron Innovations Inc. Aircraft wing extension and nozzle system
US8359128B1 (en) * 2011-07-13 2013-01-22 The Boeing Company Solar energy collection flight path management system for aircraft
GB201112045D0 (en) * 2011-07-14 2011-08-31 Rolls Royce Plc A gas turbine engine exhaust nozzle
FR2995941B1 (fr) * 2012-09-21 2018-08-31 Roxel France Divergent a deviateurs de jet pour propulseurs a charge solide
US9719465B2 (en) * 2013-03-14 2017-08-01 United Technologies Corporation Reverse core engine with thrust reverser
EP2813696B1 (de) * 2013-06-12 2015-12-02 MTU Aero Engines GmbH Schubumlenkvorrichtung sowie Flugtriebwerk
JP6361404B2 (ja) * 2014-09-17 2018-07-25 三菱重工業株式会社 推力偏向装置、および、推力偏向装置を備える飛しょう体
CN104554739B (zh) * 2014-12-16 2016-08-24 空气动力学国家重点实验室 一种可以增强和调整无尾布局飞机航向稳定性的进气道唇口
WO2018222388A1 (en) * 2017-05-31 2018-12-06 The Regents Of The University Of California Tilt-frame uav for agricultural air sampling with a propeller-thrust-governing system that facilitates vtol capability
DE102018206421B4 (de) * 2018-04-25 2020-10-01 Deutsches Zentrum für Luft- und Raumfahrt e.V. Antrieb für einen Flugkörper, insbesondere für ein Flugzeug
US11879415B2 (en) * 2020-07-13 2024-01-23 Rafael Mártinez-Vilanova Piñó Jet engine for aircraft

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US2969017A (en) * 1948-03-19 1961-01-24 Richard B Kershner Stabilizers for jet-propelled vehicles
GB764180A (en) * 1952-09-24 1956-12-19 Rolls Royce Improvements in or relating to jet arrangements
US3224190A (en) * 1959-02-11 1965-12-21 Daimler Benz Ag Jet power plant particularly for aircraft
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US3443757A (en) * 1966-10-14 1969-05-13 Aviat Uk Supersonic fluid flow exhaust nozzles
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Also Published As

Publication number Publication date
FR2888211B1 (fr) 2008-11-14
US20070095972A1 (en) 2007-05-03
IL176632A0 (en) 2006-10-31
DE102006031625A1 (de) 2007-03-01
GB0612521D0 (en) 2006-08-02
SE0601426L (sv) 2007-01-07
GB2428029A (en) 2007-01-17
IL176632A (en) 2011-03-31
GB2428029B (en) 2010-08-18
US7628356B2 (en) 2009-12-08
SE532283C2 (sv) 2009-12-01
FR2888211A1 (fr) 2007-01-12
ES2286957B1 (es) 2008-11-01
ITTO20060493A1 (it) 2007-01-07
ES2286957A1 (es) 2007-12-01

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