ES2529601A1 - Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde - Google Patents
Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde Download PDFInfo
- Publication number
- ES2529601A1 ES2529601A1 ES201331115A ES201331115A ES2529601A1 ES 2529601 A1 ES2529601 A1 ES 2529601A1 ES 201331115 A ES201331115 A ES 201331115A ES 201331115 A ES201331115 A ES 201331115A ES 2529601 A1 ES2529601 A1 ES 2529601A1
- Authority
- ES
- Spain
- Prior art keywords
- stringers
- mould
- producing fibre
- fibre
- producing
- 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.)
- Granted
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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/02—Bending or folding
- B29C53/04—Bending or folding of plates or sheets
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde, comprendiendo un útil hembra (1) y un útil macho (2), mediante los cuales se conforma un laminado de fibra (13) que se corta por la zona media, para formar dos perfiles en "L" con los que se compone un perfil en "T"; estando formado el útil hembra (1) por dos conjuntos laterales (3) enfrentados provistos de unas membranas (6) inflables; mientras que el útil macho (2) está compuesto por un bloque central (7) y dos bloques laterales (8), entre los cuales se hallan intercalados unos bloques intermedios (9) que están provistos a su vez con unas membranas (10) inflables; para doblar y unir las dos mitades del laminado de fibra (13), mediante un juego combinado de ambos útiles (1 y 2) e inflado de las membranas (6 y 10).
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201331115A ES2529601B1 (es) | 2013-07-23 | 2013-07-23 | Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde |
PCT/ES2014/070512 WO2015011316A1 (es) | 2013-07-23 | 2014-06-23 | Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201331115A ES2529601B1 (es) | 2013-07-23 | 2013-07-23 | Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2529601A1 true ES2529601A1 (es) | 2015-02-23 |
ES2529601B1 ES2529601B1 (es) | 2015-10-09 |
Family
ID=52392773
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201331115A Withdrawn - After Issue ES2529601B1 (es) | 2013-07-23 | 2013-07-23 | Molde para fabricar larguerillos de fibra para estructuras aeroespaciales y proceso para fabricar larguerillos de fibra con dicho molde |
Country Status (2)
Country | Link |
---|---|
ES (1) | ES2529601B1 (es) |
WO (1) | WO2015011316A1 (es) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016125959A1 (de) * | 2016-12-30 | 2018-07-05 | Airbus Operations Gmbh | Membranwerkzeug zum Umformen von Verstärkungsfaserlagen zu vorumgeformten T-förmigen Profilen |
US10864688B2 (en) | 2018-04-26 | 2020-12-15 | The Boeing Company | Method and apparatus of modular punch forming plates for alignment of a stringer for a vehicle |
US10780971B2 (en) | 2018-04-26 | 2020-09-22 | The Boeing Company | Methods of manufacturing a panel having a composite stringer for a vehicle |
US11135789B2 (en) * | 2018-04-26 | 2021-10-05 | The Boeing Company | Methods and devices of forming a tensioned stringer for a vehicle |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007032819B4 (de) * | 2007-07-13 | 2014-08-28 | Airbus Operations Gmbh | Verfahren und Werkzeug zur Herstellung eines T-Stringers |
DE102008041832B4 (de) * | 2008-09-05 | 2013-03-21 | Airbus Operations Gmbh | Vorrichtung und Verfahren |
ES2413189B1 (es) * | 2012-01-10 | 2015-02-11 | Manuel Torres Martínez | Instalacion para fabricar larguerillos de fibra para estructuras aeroespaciales |
-
2013
- 2013-07-23 ES ES201331115A patent/ES2529601B1/es not_active Withdrawn - After Issue
-
2014
- 2014-06-23 WO PCT/ES2014/070512 patent/WO2015011316A1/es active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2015011316A1 (es) | 2015-01-29 |
ES2529601B1 (es) | 2015-10-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 2529601 Country of ref document: ES Kind code of ref document: B1 Effective date: 20151009 |
|
FA2A | Application withdrawn |
Effective date: 20160309 |