ATE512048T1 - Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profil - Google Patents

Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profil

Info

Publication number
ATE512048T1
ATE512048T1 AT05020578T AT05020578T ATE512048T1 AT E512048 T1 ATE512048 T1 AT E512048T1 AT 05020578 T AT05020578 T AT 05020578T AT 05020578 T AT05020578 T AT 05020578T AT E512048 T1 ATE512048 T1 AT E512048T1
Authority
AT
Austria
Prior art keywords
wings
aircraft
changable
profile
linked
Prior art date
Application number
AT05020578T
Other languages
English (en)
Inventor
Juan-Mauricio Perez-Sanchez
Original Assignee
Airbus Operations 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 Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Application granted granted Critical
Publication of ATE512048T1 publication Critical patent/ATE512048T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/48Varying camber by relatively-movable parts of wing structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Prostheses (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AT05020578T 2004-09-21 2005-09-21 Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profil ATE512048T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004045651A DE102004045651B4 (de) 2004-09-21 2004-09-21 Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderbarem Profil
US63134104P 2004-11-29 2004-11-29

Publications (1)

Publication Number Publication Date
ATE512048T1 true ATE512048T1 (de) 2011-06-15

Family

ID=36011533

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05020578T ATE512048T1 (de) 2004-09-21 2005-09-21 Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profil

Country Status (3)

Country Link
US (1) US7530533B2 (de)
AT (1) ATE512048T1 (de)
DE (1) DE102004045651B4 (de)

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* Cited by examiner, † Cited by third party
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US20060118675A1 (en) * 2004-12-07 2006-06-08 Tidwell John Z Transformable fluid foil with pivoting spars and ribs
DE102004062998B4 (de) * 2004-12-22 2010-09-09 Airbus Deutschland Gmbh Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderlicher Profilform
BRPI0710353B1 (pt) * 2006-04-27 2020-03-17 Flexsys, Inc. Arranjo de alteração morfológica de borda para um aerofólio que tem superfícies de controle superior e inferior
DE102006032003B4 (de) * 2006-07-11 2015-10-22 Airbus Operations Gmbh Trimmbares Höhenleitwerk
DE102007023394A1 (de) * 2007-05-18 2008-11-20 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Fehlerdetektierung im Lastpfad eines Spindelaktuators
ITTO20080566A1 (it) * 2008-07-23 2010-01-24 Alenia Aeronautica Spa Dispositivo attuatore basato su lega a memoria di forma e gruppo di flap alare dotato di un tale dispositivo attuatore
US8500060B2 (en) * 2009-02-10 2013-08-06 The Boeing Company Aircraft with a pressurized vessel
US8056865B2 (en) * 2009-03-05 2011-11-15 The Boeing Company Mechanism for changing the shape of a control surface
US8590842B2 (en) * 2009-03-18 2013-11-26 The Boeing Company Tailorable stiffness shape morphing flow-path
US9944356B1 (en) 2009-03-25 2018-04-17 Alexander T. Wigley Shape shifting foils
DE102009026457A1 (de) 2009-05-25 2010-12-09 Eads Deutschland Gmbh Aerodynamisches Bauteil mit verformbarer Außenhaut
US8534610B1 (en) 2009-07-17 2013-09-17 The Boeing Company Method and apparatus for a leading edge slat on a wing of an aircraft
US8534611B1 (en) * 2009-07-17 2013-09-17 The Boeing Company Moveable leading edge device for a wing
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
US20120104181A1 (en) * 2010-11-02 2012-05-03 Matthew Boyd Rix Cross-Sectionally Morphing Airfoil
US8650811B2 (en) 2011-02-04 2014-02-18 The Boeing Company Solar collector frame
US8714476B2 (en) * 2011-10-21 2014-05-06 Raytheon Company Aircraft wing with flexible skins
DE102012002812A1 (de) 2012-02-15 2013-08-22 Technische Universität Braunschweig Carolo-Wilhelmina Flügel
US9555871B2 (en) * 2012-03-05 2017-01-31 The Boeing Company Two-surface sandwich structure for accommodating in-plane expansion of one of the surfaces relative to the opposing surface
EP2864195B1 (de) 2012-06-21 2017-11-01 Bombardier Inc. Adaptiver flügel für flugzeug
US9180961B2 (en) * 2013-01-28 2015-11-10 The Boeing Company Control surface for creating variable camber along a wing
US20150023797A1 (en) * 2013-07-16 2015-01-22 Nitin Kitchley Egbert Aerodynamic Variable Cross-Section Airfoil and Constant Lateral Surface Area Truss
DE102013011915A1 (de) * 2013-07-17 2015-01-22 Airbus Defence and Space GmbH Veränderbares Flügelprofil
DE102013011917A1 (de) * 2013-07-17 2015-01-22 Airbus Defence and Space GmbH Veränderbares Flügeprofil
ES2728917T3 (es) * 2014-06-12 2019-10-29 Airbus Operations Gmbh Dispositivo de borde de salida de variación progresiva de un perfil aerodinámico
US10272984B2 (en) 2015-06-25 2019-04-30 The Boeing Company Apparatuses and methods for flexurally controlling elongated structures
CA3016039C (en) * 2016-02-29 2023-09-26 Flexsys, Inc. Edge morphing arrangement for an airfoil
US11203409B2 (en) * 2018-02-19 2021-12-21 Charles J. Fenske Geometric morphing wing with adaptive corrugated structure
CA3048431A1 (en) 2019-07-03 2021-01-03 Jaye Mangione Deforming foil structure for bridging curved fluid-dynamic surface
CN110834714B (zh) * 2019-10-16 2024-08-06 中国航天空气动力技术研究院 一种轻质柔性可变后缘弯度机翼
CN110697023A (zh) * 2019-11-19 2020-01-17 中国飞机强度研究所 一种机翼后缘变弯度结构
WO2021257271A1 (en) * 2020-06-17 2021-12-23 Coflow Jet, LLC Fluid systems having a variable configuration
GB2603528A (en) 2021-02-08 2022-08-10 Airbus Operations Ltd An aircraft wing section assembly
FR3129372A1 (fr) 2021-11-24 2023-05-26 Airbus Operations Pilier flexible pour une ossature flexible d’une gouverne à géométrie variable.
US12286222B2 (en) * 2023-02-18 2025-04-29 The Boeing Company Expandable strut assembly for a wing of an aircraft and method of using the same
US12202601B2 (en) * 2023-02-18 2025-01-21 The Boeing Company Extendable compression chain system and method of using the same
CN116461691A (zh) * 2023-04-19 2023-07-21 西北工业大学 一种基于滑杆-柔性桁架-蒙皮的翼面连续变形机构

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US2152029A (en) * 1936-05-28 1939-03-28 Robert W Cone Airplane wing construction
GB1536331A (en) * 1976-04-01 1978-12-20 Secr Defence Aerofoils
US4247066A (en) * 1978-02-21 1981-01-27 General Dynamics Corporation Airfoil variable cambering device and method
US4296900A (en) * 1979-04-23 1981-10-27 Vought Corporation Airfoil construction
US4312486A (en) * 1979-09-20 1982-01-26 The Boeing Company Variable camber trailing edge for airfoil
IT1129034B (it) * 1979-10-19 1986-06-04 British Aerospace Perfezionamento nelle ali a curvatura variabile per aeromobili
SE9601956D0 (sv) 1996-05-22 1996-05-22 Saab Ab Segmenterad klaff med variabel krökning för flygplansvinge
DE19936721B4 (de) 1999-08-06 2005-09-15 Deutsches Zentrum für Luft- und Raumfahrt e.V. Tragflügelprofil mit adaptiver Verwölbung
US6375127B1 (en) * 2000-07-07 2002-04-23 Kari Appa Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression
DE10055961B4 (de) 2000-11-11 2004-09-09 Eads Deutschland Gmbh Variabler Flügelbereich mit einstellbarer, sich in Spannweiten-Richtung erstreckender Profilform
DE10325950A1 (de) * 2003-06-07 2005-01-05 Airbus Deutschland Gmbh Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderbarem Profil

Also Published As

Publication number Publication date
US7530533B2 (en) 2009-05-12
US20070152106A9 (en) 2007-07-05
DE102004045651A1 (de) 2006-03-30
DE102004045651B4 (de) 2010-09-16
US20060237596A1 (en) 2006-10-26

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