ATE512048T1 - Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profil - Google Patents
Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profilInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/48—Varying 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)
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) |
Families Citing this family (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
-
2004
- 2004-09-21 DE DE102004045651A patent/DE102004045651B4/de not_active Expired - Fee Related
-
2005
- 2005-09-21 US US11/231,917 patent/US7530533B2/en not_active Expired - Fee Related
- 2005-09-21 AT AT05020578T patent/ATE512048T1/de active
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 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ATE512048T1 (de) | Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profil | |
| ATE408555T1 (de) | Flügel, insbesondere tragflügel eines flugzeugs, mit veränderbarem profil | |
| DE60335895D1 (de) | Schlitzflügel für flugzeug | |
| WO2009032384A3 (en) | Airfoil system for cruising flight | |
| WO2011087475A3 (en) | Laminar flow wing optimized for supersonic and high subsonic cruise aircraft | |
| ATE512049T1 (de) | Flugzeug mit ringförmigem heck | |
| DE602007006292D1 (de) | Luftfahrzeug mit einer vorrichtung zur erzeugung einer aerodynamischen auftriebskraft | |
| DK201370046A (en) | Wind turbine rotor blade assembly with root extension panel and method of assembly | |
| ATE506255T1 (de) | Hochauftriebssystem am tragflügel eines flugzeugs | |
| DE60325141D1 (de) | Flugzeug mit aktiver Verwindungskontrolle seiner Tragflächen | |
| WO2015198296A3 (en) | Air intake structure and airflow control system | |
| DK2153059T3 (da) | En vindmøllevinge | |
| JP2011504149A5 (ja) | 航空機翼の後縁フラップを移動させるための装置及び同装置を備えた航空機 | |
| ES2387001T5 (es) | Aparato y método para controlar el flujo de plasma en el borde de salida de un perfil aerodinámico | |
| WO2008082437A3 (en) | Composite wing slat for aircraft | |
| WO2010124914A3 (en) | Wind turbine rotor blade | |
| WO2009029796A3 (en) | Oblique blended wing body aircraft | |
| FR2924681B1 (fr) | Element aerodynamique allonge deformable en torsion | |
| WO2008094207A3 (en) | High performance low noise helicopter blade aerodynamic design | |
| WO2011002530A3 (en) | Reinforced inflatable wings for fitment-constrained air vehicles | |
| GB2470524A (en) | Leading edge element of aircraft, method for manufacturing one, wing and stabilizer | |
| US10252822B2 (en) | Process for assembling aircraft control surfaces | |
| WO2009000227A3 (de) | Rotorblatt für ein drehflügelflugzeug | |
| DE502006005803D1 (de) | Fortschrittliche flügelhinterkante am flügel eines flugzeugs | |
| ATE531618T1 (de) | Rumpfstruktur |