ATE423060T1 - Elastisch vorgeformte verkleidung für flugzeuge und verfahren zur ihrer herstellung - Google Patents
Elastisch vorgeformte verkleidung für flugzeuge und verfahren zur ihrer herstellungInfo
- Publication number
- ATE423060T1 ATE423060T1 AT06381012T AT06381012T ATE423060T1 AT E423060 T1 ATE423060 T1 AT E423060T1 AT 06381012 T AT06381012 T AT 06381012T AT 06381012 T AT06381012 T AT 06381012T AT E423060 T1 ATE423060 T1 AT E423060T1
- Authority
- AT
- Austria
- Prior art keywords
- fairing
- aircraft
- shells
- producing same
- fuselage
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 239000003381 stabilizer Substances 0.000 abstract 3
- 239000002131 composite material Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 239000007787 solid Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/02—Tailplanes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP06381012A EP1834873B1 (de) | 2006-03-16 | 2006-03-16 | Elastisch vorgeformte Verkleidung für Flugzeuge und Verfahren zur ihrer Herstellung |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE423060T1 true ATE423060T1 (de) | 2009-03-15 |
Family
ID=36741314
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT06381012T ATE423060T1 (de) | 2006-03-16 | 2006-03-16 | Elastisch vorgeformte verkleidung für flugzeuge und verfahren zur ihrer herstellung |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7510144B2 (de) |
| EP (1) | EP1834873B1 (de) |
| AT (1) | ATE423060T1 (de) |
| DE (1) | DE602006005221D1 (de) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7413149B2 (en) * | 2004-07-21 | 2008-08-19 | United Technologies Corporation | Wing enhancement through ion entrainment of media |
| FR2892999B1 (fr) * | 2005-11-08 | 2008-02-01 | Airbus France Sas | Aeronef comportant un carenage central ajusteur de pression voilure par deformations geometriques locales |
| US7998392B2 (en) * | 2007-09-25 | 2011-08-16 | The Boeing Company | Method for manufacturing and attachment of wing fairings |
| ES2373812B1 (es) * | 2008-12-17 | 2012-12-18 | Airbus Operations, S.L. | Superficie estabilizadora horizontal de aeronave. |
| FR2966425B1 (fr) | 2010-10-26 | 2013-08-16 | Eurocopter France | Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique. |
| RU2470833C1 (ru) * | 2011-05-13 | 2012-12-27 | Открытое акционерное общество "Туполев" (ОАО "Туполев") | Приспособление и способ установки передней шторки стабилизатора самолета |
| USD754053S1 (en) * | 2014-02-19 | 2016-04-19 | Aeronautical Testing Service, Inc. | Wing root leading edge extension |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2927749A (en) * | 1956-11-02 | 1960-03-08 | Walter T Brownell | Airfoil wing root fillet |
| US2981504A (en) * | 1959-03-13 | 1961-04-25 | Gen Dynamics Corp | Fuselage blade sealing using conical surfaces |
| US3756529A (en) * | 1972-05-01 | 1973-09-04 | Mc Donnell Douglas Corp | Fuselage seal |
| US3968946A (en) * | 1975-03-31 | 1976-07-13 | The Boeing Company | Extendable aerodynamic fairing |
| US5106037A (en) * | 1990-02-05 | 1992-04-21 | Northrop Corporation | Umbrella seal for aircraft |
| US7216922B2 (en) * | 2005-06-29 | 2007-05-15 | The Boeing Company | Fairing panel retainer apparatus |
-
2006
- 2006-03-16 AT AT06381012T patent/ATE423060T1/de not_active IP Right Cessation
- 2006-03-16 DE DE602006005221T patent/DE602006005221D1/de not_active Expired - Lifetime
- 2006-03-16 EP EP06381012A patent/EP1834873B1/de not_active Expired - Lifetime
- 2006-05-16 US US11/435,364 patent/US7510144B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP1834873A1 (de) | 2007-09-19 |
| US20090057483A1 (en) | 2009-03-05 |
| US7510144B2 (en) | 2009-03-31 |
| DE602006005221D1 (de) | 2009-04-02 |
| EP1834873B1 (de) | 2009-02-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB201101435D0 (en) | Stringer for an aircraft wing and method of forming thereof | |
| WO2009138546A3 (es) | Estructura integrada de aeronave en material compuesto | |
| WO2010118448A3 (de) | Spant und verfahren zur herstellung eines solchen spants | |
| EP2128017A4 (de) | Struktur aus verbundmaterial für flugzeugrümpfe und herstellungsverfahren dafür | |
| DE602006017584D1 (de) | Verfahren zur herstellung eines flugzeugrumps aus verbundmaterial | |
| MX2016002469A (es) | Producto semiacabado y procedimiento para la fabricacion de un componente hibrido con forma tridimensional en el compuesto de metal/material plastico, asi como uso de un producto semiacabado de este tipo. | |
| WO2008149079A3 (en) | Composite flange, duct incorporating a flange and method of making a flange | |
| WO2012127038A3 (de) | Verfahren zur herstellung eines strukturbauteils sowie strukturbauteil | |
| WO2010056705A3 (en) | Method of manufacturing co-molded inserts | |
| WO2010100386A3 (fr) | Procede et dispositif de fabrication automatisee d'au moins une piece allongee a une ou plusieurs couches en materiaux composites | |
| WO2010125001A3 (de) | Verfahren zur herstellung eines faserverbundbauteils für die luft- und raumfahrt | |
| ATE497441T1 (de) | Verfahren und vorrichtung zur herstellung von teilen aus einem verbundwerkstoff, insbesondere abschnitte eines flugzeugrumpfes | |
| WO2009023346A3 (en) | Shaped composite stringers and methods of making | |
| GB201204922D0 (en) | Substrate for additive manufacturing | |
| ATE554913T1 (de) | Verfahren zur herstellung von mehreren faserverbundbauteilen | |
| WO2010070185A3 (es) | Borde de salida de superficie estabilizadora de aeronave | |
| ATE551174T1 (de) | Verfahren zur herstellung eines bauteils | |
| WO2017046217A3 (en) | Automotive body shell | |
| WO2011158172A3 (en) | Mould made of a composite material, as well as master and process for its manufacturing | |
| WO2014195486A3 (en) | Composite part for connecting a bearing to a further component | |
| EP1967353A4 (de) | Verbundprofilträger mit knollenförmigem teil | |
| WO2008113541A3 (de) | Konditionierungsmittel und verfahren zum binden von härtbaren mischungen | |
| ATE490910T1 (de) | Längsspant für einen flugzeugflügel und verfahren zur seiner herstellung | |
| DE602006005221D1 (de) | Elastisch vorgeformte Verkleidung für Flugzeuge und Verfahren zur ihrer Herstellung | |
| EP2602097A3 (de) | Faserverbundstoffkomponentenanordnung mit mindestens zwei plattenförmigen Verbundstoffstrukturen und Verfahren zu deren Herstellung |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |