BRPI0922769A2 - componente de construção de casco para aeronaves ou veículos espaciais - Google Patents
componente de construção de casco para aeronaves ou veículos espaciaisInfo
- Publication number
- BRPI0922769A2 BRPI0922769A2 BRPI0922769A BRPI0922769A BRPI0922769A2 BR PI0922769 A2 BRPI0922769 A2 BR PI0922769A2 BR PI0922769 A BRPI0922769 A BR PI0922769A BR PI0922769 A BRPI0922769 A BR PI0922769A BR PI0922769 A2 BRPI0922769 A2 BR PI0922769A2
- Authority
- BR
- Brazil
- Prior art keywords
- spacecraft
- aircraft
- construction component
- hull construction
- hull
- Prior art date
Links
Classifications
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Connection Of Plates (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11874508P | 2008-12-01 | 2008-12-01 | |
| DE102008044229A DE102008044229A1 (de) | 2008-12-01 | 2008-12-01 | Schalenbauteil für ein Luft- oder Raumfahrzeug |
| PCT/EP2009/065823 WO2010063627A2 (de) | 2008-12-01 | 2009-11-25 | Schalenbauteil fuer ein luft- oder raumfahrzeug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0922769A2 true BRPI0922769A2 (pt) | 2016-01-05 |
Family
ID=42145208
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0922769A BRPI0922769A2 (pt) | 2008-12-01 | 2009-11-25 | componente de construção de casco para aeronaves ou veículos espaciais |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US9150299B2 (pt) |
| EP (1) | EP2361195B1 (pt) |
| JP (1) | JP2012510396A (pt) |
| CN (1) | CN102227350B (pt) |
| BR (1) | BRPI0922769A2 (pt) |
| CA (1) | CA2742404C (pt) |
| DE (1) | DE102008044229A1 (pt) |
| RU (1) | RU2011117093A (pt) |
| WO (1) | WO2010063627A2 (pt) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102010042970A1 (de) * | 2010-05-12 | 2011-11-17 | Airbus Operations Gmbh | Strukturbauteil mit verbesserter Leitfähigkeit und mechanischer Festigkeit sowie Verfahren zu dessen Herstellung |
| FR2984274B1 (fr) * | 2011-12-15 | 2014-06-27 | Airbus Operations Sas | Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres |
| EP2799220B1 (en) * | 2013-04-30 | 2020-06-17 | Airbus Operations S.L. | Composite structure for an aircraft and manufacturing method thereof |
| US11260952B2 (en) * | 2019-09-26 | 2022-03-01 | The Boeing Company | Reinforced superplastic formed and diffusion bonded structures |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2489779A1 (fr) | 1980-09-09 | 1982-03-12 | Aerospatiale | Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur |
| FR2766407B1 (fr) * | 1997-07-22 | 1999-10-15 | Aerospatiale | Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs |
| ES2178421T3 (es) * | 1999-03-20 | 2002-12-16 | Dlr Deutsches Zentrum Fur Luft | Material compuesto con una zona de union reforzada. |
| US7134629B2 (en) * | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
| US7410352B2 (en) * | 2005-04-13 | 2008-08-12 | The Boeing Company | Multi-ring system for fuselage barrel formation |
| DE102006051462B4 (de) | 2006-10-31 | 2013-04-18 | Airbus Operations Gmbh | Schalenbauteil für ein Luft- oder Raumfahrzeug und Verfahren zum Herstellen desselben |
| US7635106B2 (en) | 2006-11-30 | 2009-12-22 | The Boeing Company | Composite shear tie |
| EP2128018A4 (en) * | 2007-01-29 | 2013-09-18 | Airbus Operations Sl | AIRCRAFT LOADING FUSELAGE TORQUE MADE FROM COMPOSITE MATERIAL |
| FR2914622B1 (fr) * | 2007-04-04 | 2009-05-15 | Airbus France Sas | Aeronef comprenant une structure assurant les fonctions structurale et electrique |
| DE102007044386A1 (de) * | 2007-09-18 | 2009-04-02 | Airbus Deutschland Gmbh | Strukturbauteil und Verfahren zum Versteifen einer Außenhaut |
| DE102007054053A1 (de) * | 2007-11-13 | 2009-05-20 | Airbus Deutschland Gmbh | Kupplungselement zur Verbindung von zwei Längsversteifungselementen |
-
2008
- 2008-12-01 DE DE102008044229A patent/DE102008044229A1/de not_active Ceased
-
2009
- 2009-11-25 WO PCT/EP2009/065823 patent/WO2010063627A2/de not_active Ceased
- 2009-11-25 RU RU2011117093/11A patent/RU2011117093A/ru unknown
- 2009-11-25 JP JP2011537967A patent/JP2012510396A/ja active Pending
- 2009-11-25 CA CA2742404A patent/CA2742404C/en not_active Expired - Fee Related
- 2009-11-25 US US13/130,257 patent/US9150299B2/en active Active
- 2009-11-25 BR BRPI0922769A patent/BRPI0922769A2/pt not_active Application Discontinuation
- 2009-11-25 EP EP09759946.8A patent/EP2361195B1/de not_active Not-in-force
- 2009-11-25 CN CN200980147814.5A patent/CN102227350B/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| DE102008044229A1 (de) | 2010-06-10 |
| EP2361195B1 (de) | 2017-02-22 |
| EP2361195A2 (de) | 2011-08-31 |
| WO2010063627A3 (de) | 2010-09-30 |
| US20110297788A1 (en) | 2011-12-08 |
| CN102227350B (zh) | 2015-10-14 |
| US9150299B2 (en) | 2015-10-06 |
| RU2011117093A (ru) | 2013-01-10 |
| WO2010063627A4 (de) | 2010-11-18 |
| JP2012510396A (ja) | 2012-05-10 |
| CA2742404C (en) | 2017-02-07 |
| CA2742404A1 (en) | 2010-06-10 |
| WO2010063627A2 (de) | 2010-06-10 |
| CN102227350A (zh) | 2011-10-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B11A | Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing | ||
| B11Y | Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette] |