FR2411758A1 - Gouverne laterale a geometrie d'aile variable a haute efficacite - Google Patents

Gouverne laterale a geometrie d'aile variable a haute efficacite

Info

Publication number
FR2411758A1
FR2411758A1 FR7834243A FR7834243A FR2411758A1 FR 2411758 A1 FR2411758 A1 FR 2411758A1 FR 7834243 A FR7834243 A FR 7834243A FR 7834243 A FR7834243 A FR 7834243A FR 2411758 A1 FR2411758 A1 FR 2411758A1
Authority
FR
France
Prior art keywords
governor
high efficiency
wing
lateral
variable wing
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
FR7834243A
Other languages
English (en)
Other versions
FR2411758B3 (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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2411758A1 publication Critical patent/FR2411758A1/fr
Application granted granted Critical
Publication of FR2411758B3 publication Critical patent/FR2411758B3/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/08—Stabilising surfaces mounted on, or supported by, wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Tires In General (AREA)

Abstract

L'INVENTION A POUR OBJET UNE GOUVERNE LATERALE A HAUTE EFFICACITE, A GEOMETRIE D'AILE VARIABLE POUR GRANDS ANGLES D'ATTAQUE. LA GOUVERNE LATERALE PEUT PIVOTER AUTOUR D'UN AXE PARALLELE A L'AXE LONGITUDINAL DU FUSELAGE DANS LE PLAN DE L'AILE, LES PARTIES D'AILE EXTERIEURES 2 ETANT RELIEES SOUS UN ANGLE T A UNE GOUVERNE LATERALE 1 DIRIGEE VERTICALEMENT VERS LE BAS EN POSITION DE BASE, LES ENSEMBLES 3 CONSTITUES PAR LESDITES PARTIES 1, 2 ET LA GOUVERNE LATERALE 1 POUVANT PIVOTER VERS LE HAUT AUTOUR DES AXES 4. LA GOUVERNE LATERALE PEUT NOTAMMENT ETRE UTILISEE AVEC DES AVIONS DU TYPE AILE VOLANTE, NOTAMMENT DES AVIONS A AILE DELTA.
FR7834243A 1977-12-16 1978-12-05 Gouverne laterale a geometrie d'aile variable a haute efficacite Granted FR2411758A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2756107A DE2756107C2 (de) 1977-12-16 1977-12-16 Hochwirksames Seitenleitwerk mit variabler Flügelgeometrie

Publications (2)

Publication Number Publication Date
FR2411758A1 true FR2411758A1 (fr) 1979-07-13
FR2411758B3 FR2411758B3 (fr) 1981-01-02

Family

ID=6026294

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7834243A Granted FR2411758A1 (fr) 1977-12-16 1978-12-05 Gouverne laterale a geometrie d'aile variable a haute efficacite

Country Status (6)

Country Link
US (1) US4247062A (fr)
JP (1) JPS54113196A (fr)
DE (1) DE2756107C2 (fr)
FR (1) FR2411758A1 (fr)
GB (1) GB2010195B (fr)
IT (1) IT1100627B (fr)

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DE3103095C2 (de) * 1981-01-30 1985-05-09 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flugzeug mit Tragflächen negativer Pfeilung und einem Heckleitwerk
US4538779A (en) * 1982-09-30 1985-09-03 The Boeing Company Caster type empennage assembly for aircraft
DE3242584A1 (de) * 1982-11-18 1984-05-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung von zusatzflaechen an den spitzen eines tragfluegels
US4545552A (en) * 1983-06-20 1985-10-08 Welles Stanley W Airframe design
US4542866A (en) * 1983-09-30 1985-09-24 The Boeing Company Aircraft with directional controlling canards
US4682746A (en) * 1984-12-05 1987-07-28 Lockheed Corporation Control force generator
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JPH0412842Y2 (fr) * 1986-07-14 1992-03-26
DE3638347A1 (de) * 1986-11-10 1988-05-19 Andreas Heinrich Rudersystem zur steuerung von flugzeugen
EP0416268A3 (en) * 1989-09-04 1991-04-03 British Aerospace Public Limited Company Tail unit
US5072894A (en) * 1989-10-02 1991-12-17 Rockwell International Corporation Apparatus and method for increasing the angle of attack operating range of an aircraft
US5078338A (en) * 1990-01-19 1992-01-07 Neill Terrence O Means for maintaining a desired relationship between roll and yaw stability in a swept-wing aircraft by varying dihedral as a function of lift coefficient
US5156358A (en) * 1991-04-11 1992-10-20 Northrop Corporation Aircraft outboard control
US5398888A (en) * 1993-05-12 1995-03-21 Northrop Grumman Corporation Skewed hinge control surface
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FR2841532B1 (fr) * 2002-06-27 2004-12-17 Airbus France Avion a controle actif du vrillage de ses ailes
GB0326228D0 (en) * 2003-11-10 2003-12-17 Airbus Uk Ltd Wing tip device
US7475848B2 (en) * 2003-11-11 2009-01-13 Morgenstern John M Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
GB0518755D0 (en) 2005-09-14 2005-10-19 Airbus Uk Ltd Wing tip device
CN102149599B (zh) 2008-06-20 2014-11-19 航空伙伴股份有限公司 弯曲的机翼末梢
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
US20110127383A1 (en) * 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet
US9162755B2 (en) 2009-12-01 2015-10-20 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
FR2954275B1 (fr) * 2009-12-22 2012-01-13 Astrium Sas Vehicule aerien ultra-rapide et procede de locomotion aerienne associe
GB201011843D0 (en) 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
DE102010048139A1 (de) * 2010-10-11 2012-04-12 Eads Deutschland Gmbh Fluggerät mit variabler Geometrie
GB201018185D0 (en) * 2010-10-28 2010-12-08 Airbus Operations Ltd Wing tip device attachment apparatus and method
DK3372493T3 (da) * 2011-06-09 2019-12-09 Aviation Partners Inc Den delt-formet blandede winglet
US10538307B2 (en) * 2011-10-01 2020-01-21 The Boeing Company Hinged raked wing tip
US9481446B2 (en) 2012-10-30 2016-11-01 The Boeing Company System for latching and locking a foldable airfoil
GB201301680D0 (en) * 2013-01-31 2013-03-13 Airbus Uk Ltd Downwardly extending wing tip device
US9567066B2 (en) * 2013-02-05 2017-02-14 Tamarack Aerospace Group, Inc. Controllable airflow modification device periodic load control
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
CN105015795A (zh) * 2014-04-28 2015-11-04 张焰 飞机设计方法与方案
US10011350B2 (en) * 2014-05-20 2018-07-03 Sikorsky Aircraft Corporation Vertical take-off and landing drag rudder
FR3037560B1 (fr) * 2015-06-16 2018-06-01 Airbus Operations Aile d'aeronef comprenant un embout d'aile pilotable en incidence
CN105035304A (zh) * 2015-08-13 2015-11-11 中国航空工业集团公司西安飞机设计研究所 一种带分裂式翼尖的无尾飞翼布局飞机
RU2616458C1 (ru) * 2016-04-01 2017-04-17 Борис Владимирович Мищенко Сверхзвуковой летательный аппарат
EP3269635A1 (fr) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Aile d'avion
GB2565768B (en) * 2017-08-15 2022-05-18 Bae Systems Plc A vehicle
EP3668787B1 (fr) 2017-08-15 2023-06-07 BAE Systems PLC Un véhicule
EP3486162B1 (fr) * 2017-11-17 2020-07-01 Airbus Operations GmbH Procédé pour faire fonctionner une aile d'aéronef comprenant une partie d'extrémité d'aile pliable
EP3511243B1 (fr) * 2018-01-15 2021-12-29 The Aircraft Performance Company GmbH Aile d'avion
US11440638B2 (en) * 2018-05-03 2022-09-13 Airbus Operations Gmbh Wing for an aircraft
US20190351994A1 (en) * 2018-05-16 2019-11-21 Richard Michael Truhill Retractable aircraft control surface
US11370526B2 (en) * 2018-05-31 2022-06-28 Airbus Operations Gmbh Latching device for a wing arrangement for an aircraft
US11319054B2 (en) * 2018-05-31 2022-05-03 Airbus Operations Gmbh Wing arrangement for an aircraft
US11214353B2 (en) * 2018-06-01 2022-01-04 Airbus Operations Gmbh Wing arrangement for an aircraft and aircraft
EP3587252A1 (fr) * 2018-06-28 2020-01-01 Airbus Operations GmbH Système d'arrêt pour arrêter un premier composant d'aéronef par rapport à un second composant d'aéronef
US11254412B2 (en) 2019-03-29 2022-02-22 The Boeing Company Foldable raked wing tips having aerodynamic devices
GB2615311A (en) * 2022-01-31 2023-08-09 Airbus Operations Ltd Aircraft wing with movable wing tip device
GB2616252A (en) * 2022-01-31 2023-09-06 Airbus Operations Ltd Aircraft with movable wing tip device

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3104079A (en) * 1960-10-07 1963-09-17 William H Phillips Variable-geometry winged reentry vehicle
GB934286A (en) * 1961-06-16 1963-08-14 English Electric Co Ltd Improvements in and relating to wing tip folding mechanisms

Also Published As

Publication number Publication date
IT1100627B (it) 1985-09-28
JPS54113196A (en) 1979-09-04
FR2411758B3 (fr) 1981-01-02
DE2756107B1 (de) 1979-06-28
DE2756107C2 (de) 1980-02-28
GB2010195A (en) 1979-06-27
IT7830825A0 (it) 1978-12-14
GB2010195B (en) 1982-03-03
US4247062A (en) 1981-01-27

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Referenoes LIST OF APBEXJXCES
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Legal Events

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