DE602005009231D1 - Versteifungselement und Verfahren zu dessen Herstellung - Google Patents
Versteifungselement und Verfahren zu dessen HerstellungInfo
- Publication number
- DE602005009231D1 DE602005009231D1 DE602005009231T DE602005009231T DE602005009231D1 DE 602005009231 D1 DE602005009231 D1 DE 602005009231D1 DE 602005009231 T DE602005009231 T DE 602005009231T DE 602005009231 T DE602005009231 T DE 602005009231T DE 602005009231 D1 DE602005009231 D1 DE 602005009231D1
- Authority
- DE
- Germany
- Prior art keywords
- stiffening element
- composite material
- folding line
- production
- edge
- 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
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/345—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/462—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Manufacturing Of Tubular Articles Or Embedded Moulded Articles (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP05112455A EP1800841B1 (de) | 2005-12-20 | 2005-12-20 | Versteifungselement und Verfahren zu dessen Herstellung |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005009231D1 true DE602005009231D1 (de) | 2008-10-02 |
Family
ID=35954060
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005009231T Expired - Fee Related DE602005009231D1 (de) | 2005-12-20 | 2005-12-20 | Versteifungselement und Verfahren zu dessen Herstellung |
Country Status (5)
Country | Link |
---|---|
US (1) | US20070138695A1 (de) |
EP (1) | EP1800841B1 (de) |
AT (1) | ATE405413T1 (de) |
DE (1) | DE602005009231D1 (de) |
ES (1) | ES2311937T3 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8632653B2 (en) * | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
CA2685481A1 (en) * | 2007-04-30 | 2008-11-06 | Airbus Operations S.L. | Complex geometries made of composite material and forming process for same |
US9278484B2 (en) | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
DE102010044584A1 (de) * | 2010-09-07 | 2012-03-08 | Kautex Textron Gmbh & Co. Kg | Kraftstoffbehälter aus thermoplastischem Kunststoff |
FR2978372B1 (fr) * | 2011-07-27 | 2013-09-13 | Airbus Operations Sas | Panneau raidi pour aeronef, comprenant des raidisseurs a ames entaillees |
GB201120219D0 (en) * | 2011-11-23 | 2012-01-04 | Airbus Operations Ltd | Wrinkle control method and tool therefor |
FR2993856B1 (fr) * | 2012-07-30 | 2015-09-18 | Airbus Operations Sas | Element de structure de fuselage d'aeronef a section evolutive |
EP2888095B1 (de) * | 2012-08-21 | 2020-09-30 | Saab Ab | Verstärkte struktur und verfahren zur herstellung einer verstärkten struktur |
US10105940B2 (en) * | 2016-04-18 | 2018-10-23 | The Boeing Company | Formation of composite laminates having one or more divergent flanges |
DE102016109284B3 (de) * | 2016-05-20 | 2017-03-23 | Cotesa Gmbh | Bogenförmige Faserverbundkunststoff-Preform und Verfahren zur Herstellung gekrümmter Profile |
GB2624449A (en) * | 2022-11-18 | 2024-05-22 | Airbus Operations Ltd | Aircraft structural component and a method of fabricating an aircraft structural component |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4425424B2 (ja) * | 2000-05-01 | 2010-03-03 | 本田技研工業株式会社 | 繊維強化複合材からなるジョグル付き半硬化物品の製造方法、及びそれを用いた予備成形構造体の製造方法 |
EP1547756A1 (de) | 2003-12-24 | 2005-06-29 | Airbus UK Limited | Verfahren zur Herstellung von Flugzeugsteilen |
-
2005
- 2005-12-20 EP EP05112455A patent/EP1800841B1/de not_active Not-in-force
- 2005-12-20 AT AT05112455T patent/ATE405413T1/de not_active IP Right Cessation
- 2005-12-20 DE DE602005009231T patent/DE602005009231D1/de not_active Expired - Fee Related
- 2005-12-20 ES ES05112455T patent/ES2311937T3/es active Active
-
2006
- 2006-11-30 US US11/564,851 patent/US20070138695A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP1800841A1 (de) | 2007-06-27 |
EP1800841B1 (de) | 2008-08-20 |
ATE405413T1 (de) | 2008-09-15 |
ES2311937T3 (es) | 2009-02-16 |
US20070138695A1 (en) | 2007-06-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |