DE3668438D1 - Federbeladene vorderkantenklappe. - Google Patents
Federbeladene vorderkantenklappe.Info
- Publication number
- DE3668438D1 DE3668438D1 DE8686201364T DE3668438T DE3668438D1 DE 3668438 D1 DE3668438 D1 DE 3668438D1 DE 8686201364 T DE8686201364 T DE 8686201364T DE 3668438 T DE3668438 T DE 3668438T DE 3668438 D1 DE3668438 D1 DE 3668438D1
- Authority
- DE
- Germany
- Prior art keywords
- spring
- front edge
- edge flap
- loaded front
- loaded
- 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.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
- B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
-
- 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
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Blinds (AREA)
- Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/814,604 US4753402A (en) | 1985-12-30 | 1985-12-30 | Biased leading edge slat apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3668438D1 true DE3668438D1 (de) | 1990-03-01 |
Family
ID=25215536
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8686201364T Expired - Fee Related DE3668438D1 (de) | 1985-12-30 | 1986-08-01 | Federbeladene vorderkantenklappe. |
DE19863643157 Withdrawn DE3643157A1 (de) | 1985-12-30 | 1986-12-17 | Vorgespannte vorderkantenvorfluegeleinrichtung |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19863643157 Withdrawn DE3643157A1 (de) | 1985-12-30 | 1986-12-17 | Vorgespannte vorderkantenvorfluegeleinrichtung |
Country Status (4)
Country | Link |
---|---|
US (1) | US4753402A (de) |
EP (1) | EP0230681B2 (de) |
JP (1) | JPS62157895A (de) |
DE (2) | DE3668438D1 (de) |
Families Citing this family (57)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2204538B (en) * | 1987-05-06 | 1990-12-12 | British Aerospace | Wing leading edge arrangements for aircraft |
GB8711252D0 (en) * | 1987-05-13 | 1987-07-15 | British Aerospace | High lift device |
US5544847A (en) * | 1993-11-10 | 1996-08-13 | The Boeing Company | Leading edge slat/wing combination |
GB2304656B (en) * | 1995-08-26 | 1999-10-13 | British Aerospace | Deployment mechanisms for aircraft auxiliary aerofoils |
US5927656A (en) * | 1996-06-26 | 1999-07-27 | The Boeing Company | Wing leading edge flap and method therefor |
US6644168B1 (en) * | 2002-08-12 | 2003-11-11 | General Dynamics Armament And Technical Products, Inc. | System and method for active control of recoil mechanism |
GB0410375D0 (en) * | 2004-05-10 | 2004-06-16 | Airbus Uk Ltd | High lift device for an aircraft |
US7101297B2 (en) * | 2004-06-10 | 2006-09-05 | Moog Inc. | Compact actuator |
EP1757519B1 (de) * | 2005-08-25 | 2010-03-31 | GKN Aerospace Services Limited | Vorflügel für eine Flugzeugtragfläche |
US20070102587A1 (en) * | 2005-11-07 | 2007-05-10 | The Boeing Company | Wing leading edge slat system |
DE102006030315A1 (de) * | 2006-06-30 | 2008-01-17 | Airbus Deutschland Gmbh | Hochauftriebssystem am Tragflügel eines Flugzeugs |
US7912548B2 (en) * | 2006-07-21 | 2011-03-22 | Cardiac Pacemakers, Inc. | Resonant structures for implantable devices |
GB0708641D0 (en) * | 2007-05-04 | 2007-06-13 | Goodrich Actuation Systems Ltd | Actuator |
JP4699487B2 (ja) * | 2007-05-25 | 2011-06-08 | 三菱重工業株式会社 | 高揚力発生装置、翼および高揚力発生装置の騒音低減構造 |
US7913949B2 (en) | 2007-06-11 | 2011-03-29 | The Boeing Company | Symmetric leading edge device and method to delay flow separation |
GB0721284D0 (en) * | 2007-10-31 | 2007-12-12 | Airbus Uk Ltd | Actuation system for leading edge high-lift device |
GB0722425D0 (en) * | 2007-11-15 | 2007-12-27 | Airbus Uk Ltd | Slat support funk plate |
US10023302B2 (en) * | 2007-12-06 | 2018-07-17 | Roller Bearing Company Of America, Inc. | Actuation system for a lift assisting device and lined track rollers used therein |
US20140131512A1 (en) * | 2007-12-06 | 2014-05-15 | Roller Bearing Company Of America, Inc. | Seal and electrical conductor for lined track rollers used on actuation system for aircraft lift assisting devices |
US20140339358A1 (en) * | 2007-12-06 | 2014-11-20 | Roller Bearing Company Of America, Inc. | Electrical conductor for lined track rollers used on actuation system for aircraft lift assisting devices |
US20110220762A1 (en) * | 2007-12-06 | 2011-09-15 | Roller Bearing Company Of America, Inc. | Actuation system for a lift assisting device and roller bearings used therein |
US10400818B2 (en) * | 2007-12-06 | 2019-09-03 | Roller Bearing Company Of America, Inc. | Track roller bearings with rolling elements or liners |
US8025257B2 (en) * | 2007-12-06 | 2011-09-27 | Roller Bearing Company Of America, Inc. | Actuation system for a lift assisting device and roller bearings used therein |
GB0805599D0 (en) * | 2008-03-28 | 2008-04-30 | Airbus Uk Ltd | Slat deployment mechanism |
GB0810460D0 (en) * | 2008-06-09 | 2008-07-09 | Airbus Uk Ltd | Support assembly |
GB0810724D0 (en) | 2008-06-12 | 2008-07-16 | Airbus Uk Ltd | Slat assembly |
GB0816022D0 (en) * | 2008-09-03 | 2008-10-08 | Airbus Uk Ltd | Slat support assembly |
DE102008050544A1 (de) | 2008-10-06 | 2010-04-29 | Airbus Deutschland Gmbh | An der Tragfläche eines Flugzeugs angeordneter Vorflügel |
GB0906074D0 (en) | 2009-04-08 | 2009-05-20 | Airbus Uk Ltd | Track container |
US9261132B2 (en) | 2009-04-24 | 2016-02-16 | Roller Bearing Company Of America, Inc. | Low friction bearing assembly and link apparatus |
ES2427390T3 (es) * | 2009-10-29 | 2013-10-30 | Asco Industries | Carril de guiado para dispositivo hipersustentador |
GB201008773D0 (en) * | 2010-05-26 | 2010-07-14 | Airbus Uk Ltd | Aircraft slat assembly |
DE102011018906A1 (de) * | 2011-04-28 | 2012-10-31 | Airbus Operations Gmbh | Hochauftriebssystem für ein Flugzeug und Verfahren zum Beeinflussen der Hochauftriebseigenschaften eines Flugzeugs |
US8876065B2 (en) * | 2011-10-21 | 2014-11-04 | Gulfstream Aerospace Corporation | Flap roller arrangement, flap assembly, and method for removing a roller assembly from a flap fitting |
GB201121435D0 (en) * | 2011-12-14 | 2012-01-25 | Airbus Operations Ltd | Aircraft wing assembly |
WO2014021958A1 (en) | 2012-04-30 | 2014-02-06 | Roller Bearing Company Of America, Inc. | Hybrid bearing assembly with rolling elements and plain bearing |
GB201209686D0 (en) * | 2012-05-31 | 2012-07-18 | Airbus Operations Ltd | A slat support assembly |
GB2530326A (en) * | 2014-09-22 | 2016-03-23 | Airbus Operations Ltd | A link for coupling an aircraft lift device to a track |
GB2533311A (en) * | 2014-12-15 | 2016-06-22 | Airbus Operations Ltd | A track container |
GB201522327D0 (en) * | 2015-12-17 | 2016-02-03 | Airbus Operations Ltd | Wing structure |
AT518606A1 (de) | 2016-04-29 | 2017-11-15 | Facc Ag | Aerodynamischer Profilkörper für ein Flugzeug |
GB2562019A (en) * | 2016-11-14 | 2018-11-07 | Airbus Operations Ltd | Roller components |
EP3326909B1 (de) * | 2016-11-23 | 2019-10-02 | Airbus Operations GmbH | Vorflügelanordnung |
EP3339165B1 (de) * | 2016-12-22 | 2020-09-09 | Goodrich Actuation Systems Limited | Flügelvorflügelaktuatortrennungserkennung |
EP3395678B1 (de) | 2017-04-26 | 2021-05-26 | Asco Industries NV | Führungsanordnung für eine hochauftriebsvorrichtungsträgerbahn einer tragflächenvorderkante |
RU2746479C1 (ru) * | 2017-04-28 | 2021-04-14 | Эйрбас Оперейшнз Гмбх | Консоль крыла для летательного аппарата |
CN110573422B (zh) | 2017-04-28 | 2023-05-23 | 空中客车运作有限责任公司 | 飞行器的机翼 |
US10364019B2 (en) * | 2017-12-13 | 2019-07-30 | Thomas Hsueh | Aircraft flap mechanism |
EP3501977B1 (de) | 2017-12-19 | 2021-08-11 | Asco Industries NV | Freisetzungssystem für eine hochauftriebsvorrichtung einer tragflächenvorderkante |
WO2019154698A1 (en) * | 2018-02-06 | 2019-08-15 | Airbus Operations Gmbh | Wing for an aircraft |
GB2579221A (en) * | 2018-11-26 | 2020-06-17 | Airbus Operations Ltd | Aircraft control mechanism |
US11840336B2 (en) | 2019-05-28 | 2023-12-12 | Airbus Operations Gmbh | Antivibration kit-of-parts and parts therefor, airfoil structure and aircraft provided therewith |
US11420727B2 (en) * | 2019-07-25 | 2022-08-23 | Airbus Operations Gmbh | Airfoil arrangement for an aircraft |
GB2588899A (en) * | 2019-11-12 | 2021-05-19 | Airbus Operations Ltd | Aircraft wings having moveable structures |
EP3878734B1 (de) * | 2020-03-11 | 2023-07-19 | Airbus Operations GmbH | Führungselement für eine hochauftriebsprofilanordnung eines flugzeugs, hochauftriebsprofilanordnung und herstellungsverfahren |
EP4032801B1 (de) * | 2021-01-22 | 2024-08-28 | Airbus Operations GmbH | Flügel für ein flugzeug |
EP4140878A1 (de) * | 2021-08-31 | 2023-03-01 | Airbus Operations GmbH | Flügel für ein flugzeug |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1780838A (en) * | 1927-07-09 | 1930-11-04 | Handley Page Ltd | Means for controlling aeroplanes |
US1830019A (en) * | 1931-05-06 | 1931-11-03 | Edward H Davis | Airplane |
US2361574A (en) * | 1940-02-28 | 1944-10-31 | Tampier Rene | Aircraft |
US2406475A (en) * | 1944-02-19 | 1946-08-27 | Samuel H Pearis | Slotted airplane wing |
US2938680A (en) * | 1957-07-02 | 1960-05-31 | North American Aviation Inc | Multiple position airfoil slat |
EP0227643A3 (de) * | 1980-08-13 | 1988-07-20 | The Boeing Company | Führungseinbau für einen ausziehbaren Tragflügel |
US4422606A (en) * | 1981-06-25 | 1983-12-27 | Munroe Ronald G | Automatic leading edge slat for aircraft |
FR2547270B1 (fr) * | 1983-06-10 | 1985-09-06 | Boeing Co | Mecanisme d'extension et de retraction pour un volet de bord d'attaque d'une aile d'avion |
-
1985
- 1985-12-30 US US06/814,604 patent/US4753402A/en not_active Expired - Fee Related
-
1986
- 1986-08-01 EP EP86201364A patent/EP0230681B2/de not_active Expired - Lifetime
- 1986-08-01 DE DE8686201364T patent/DE3668438D1/de not_active Expired - Fee Related
- 1986-12-17 DE DE19863643157 patent/DE3643157A1/de not_active Withdrawn
- 1986-12-25 JP JP61315947A patent/JPS62157895A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
EP0230681B2 (de) | 1993-04-14 |
EP0230681A3 (en) | 1988-01-07 |
JPS62157895A (ja) | 1987-07-13 |
DE3643157A1 (de) | 1987-07-02 |
EP0230681B1 (de) | 1990-01-24 |
EP0230681A2 (de) | 1987-08-05 |
US4753402A (en) | 1988-06-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8366 | Restricted maintained after opposition proceedings | ||
8339 | Ceased/non-payment of the annual fee |