ATE317324T1 - Herstellungsverfahren von co-gehärteten strukturen durch transferspritzen von kunstharz - Google Patents
Herstellungsverfahren von co-gehärteten strukturen durch transferspritzen von kunstharzInfo
- Publication number
- ATE317324T1 ATE317324T1 AT03255455T AT03255455T ATE317324T1 AT E317324 T1 ATE317324 T1 AT E317324T1 AT 03255455 T AT03255455 T AT 03255455T AT 03255455 T AT03255455 T AT 03255455T AT E317324 T1 ATE317324 T1 AT E317324T1
- Authority
- AT
- Austria
- Prior art keywords
- disposing
- skin panel
- preforms
- production
- performs
- Prior art date
Links
- 239000011347 resin Substances 0.000 title abstract 3
- 229920005989 resin Polymers 0.000 title abstract 3
- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 238000000034 method Methods 0.000 title abstract 2
- 238000005507 spraying Methods 0.000 title 1
- 230000035699 permeability Effects 0.000 abstract 2
- 238000001721 transfer moulding Methods 0.000 abstract 1
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
- B29C70/40—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
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
-
- 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)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
- Addition Polymer Or Copolymer, Post-Treatments, Or Chemical Modifications (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/243,796 US7419627B2 (en) | 2002-09-13 | 2002-09-13 | Co-cured vacuum-assisted resin transfer molding manufacturing method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE317324T1 true ATE317324T1 (de) | 2006-02-15 |
Family
ID=31946389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT03255455T ATE317324T1 (de) | 2002-09-13 | 2003-09-02 | Herstellungsverfahren von co-gehärteten strukturen durch transferspritzen von kunstharz |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US7419627B2 (de) |
| EP (1) | EP1400341B1 (de) |
| JP (1) | JP2004106548A (de) |
| AT (1) | ATE317324T1 (de) |
| DE (1) | DE60303484T2 (de) |
| ES (1) | ES2256679T3 (de) |
Families Citing this family (54)
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| US20050236736A1 (en) * | 2004-04-23 | 2005-10-27 | Formella Stephen C | Composite product and forming system |
| US20050255311A1 (en) * | 2004-04-23 | 2005-11-17 | Formella Stephen C | Hybrid composite product and system |
| FR2879498B1 (fr) * | 2004-12-16 | 2009-01-30 | Snecma Propulsion Solide Sa | Densification de structures fibreuses par rtm pour la realisation de pieces en materiau composite |
| US8551381B2 (en) | 2005-02-21 | 2013-10-08 | Airbus Deutschland Gmbh | Fiber composite component and method for the production of a fiber composite component |
| DE102005008252B4 (de) * | 2005-02-21 | 2014-03-20 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbund-Bauelements |
| DE102006002198B4 (de) * | 2006-01-16 | 2011-04-28 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbund-Bauelements |
| US7837147B2 (en) * | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
| FR2890591B1 (fr) * | 2005-09-12 | 2012-10-19 | Eads | Procede de fabrication d'une piece composite rtm et piece composite obtenue selon ce procede |
| US20070090554A1 (en) * | 2005-10-26 | 2007-04-26 | Rick Wykoff | Panel molding method and apparatus |
| DE102006038205B4 (de) * | 2006-08-16 | 2009-07-09 | Küster Automotive Control Systems GmbH | Befestigung eines Betätigungszuges an einem Widerlager eines Kraftfahrzeuges |
| US7749424B2 (en) * | 2006-08-31 | 2010-07-06 | Milgard Manufacturing, Inc. | Vacuum-infused fiberglass-reinforced fenestration framing member and method of manufacture |
| US7897097B2 (en) * | 2006-08-31 | 2011-03-01 | Milgard Manufacturing Incorporated | Vacuum-infused fiberglass-reinforced fenestration framing member and method of manufacture |
| DE102006050579B3 (de) * | 2006-10-26 | 2008-03-06 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zur Herstellung von Faserverbundbauteilen |
| GB0622691D0 (en) * | 2006-11-14 | 2006-12-27 | Airbus Uk Ltd | Method and apparatus for controlling the geometry of a composite component |
| US9511571B2 (en) | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
| DE102007004313B4 (de) * | 2007-01-29 | 2015-01-15 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Bauteils für ein Luft- oder Raumfahrzeug |
| DE102007004312B4 (de) | 2007-01-29 | 2014-08-21 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für ein Luft- oder Raumfahrzeug |
| GB2447964B (en) | 2007-03-29 | 2012-07-18 | Gurit Uk Ltd | Moulding material |
| US7861969B2 (en) * | 2007-05-24 | 2011-01-04 | The Boeing Company | Shaped composite stringers and methods of making |
| US7879276B2 (en) * | 2007-11-08 | 2011-02-01 | The Boeing Company | Foam stiffened hollow composite stringer |
| DE102008008386A1 (de) * | 2008-02-09 | 2009-08-13 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines FVW-Bauteils |
| US8668857B1 (en) * | 2008-04-25 | 2014-03-11 | Abe Karem | High quality out-of-autoclave composites |
| US8540921B2 (en) | 2008-11-25 | 2013-09-24 | The Boeing Company | Method of forming a reinforced foam-filled composite stringer |
| US8230713B2 (en) | 2008-12-30 | 2012-07-31 | Usamp | Elevated temperature forming die apparatus |
| US8459084B2 (en) | 2009-02-05 | 2013-06-11 | Usamp | Elevated temperature forming method and preheater apparatus |
| US8425710B2 (en) | 2009-03-13 | 2013-04-23 | The Boeing Company | Automated placement of vibration damping materials |
| US20100249277A1 (en) * | 2009-03-31 | 2010-09-30 | General Electric Company | Cured composite composition |
| US8500066B2 (en) | 2009-06-12 | 2013-08-06 | The Boeing Company | Method and apparatus for wireless aircraft communications and power system using fuselage stringers |
| US8570152B2 (en) | 2009-07-23 | 2013-10-29 | The Boeing Company | Method and apparatus for wireless sensing with power harvesting of a wireless signal |
| US8617687B2 (en) | 2009-08-03 | 2013-12-31 | The Boeing Company | Multi-functional aircraft structures |
| US8628717B2 (en) | 2010-06-25 | 2014-01-14 | The Boeing Company | Composite structures having integrated stiffeners and method of making the same |
| US9682514B2 (en) | 2010-06-25 | 2017-06-20 | The Boeing Company | Method of manufacturing resin infused composite parts using a perforated caul sheet |
| US8940213B2 (en) | 2010-06-25 | 2015-01-27 | The Boeing Company | Resin infusion of composite parts using a perforated caul sheet |
| US8636252B2 (en) | 2010-06-25 | 2014-01-28 | The Boeing Company | Composite structures having integrated stiffeners with smooth runouts and method of making the same |
| CA2803414C (en) | 2010-07-02 | 2018-09-04 | Hexcel Holding Gmbh | Fibre reinforced composite moulding |
| DE102011010384B4 (de) * | 2011-02-05 | 2015-06-11 | Premium Aerotec Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils |
| WO2012149939A2 (en) * | 2011-05-04 | 2012-11-08 | Vestas Wind Systems A/S | Method of preparing a composite laminate |
| WO2012154544A2 (en) * | 2011-05-06 | 2012-11-15 | Purdue Research Foundation | Method and system of vacuum assisted resin transfer molding for repair of composite materials and structure |
| DE102011079943A1 (de) * | 2011-07-27 | 2013-01-31 | Airbus Operations Gmbh | Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren |
| GB201120707D0 (en) * | 2011-12-01 | 2012-01-11 | Airbus Operations Ltd | Leading edge structure |
| CA2864881A1 (en) * | 2012-02-17 | 2013-08-22 | Saab Ab | Method and mould system for net moulding of a co-cured, integrated structure |
| ES2427038B1 (es) | 2012-04-26 | 2014-09-02 | Airbus Operations, S.L. | Método de prevención de porosidad en piezas de material compuesto. |
| WO2014175795A1 (en) * | 2013-04-25 | 2014-10-30 | Saab Ab | A method and a production line for the manufacture of a torsion-box type skin composite structure |
| WO2014175799A1 (en) * | 2013-04-25 | 2014-10-30 | Saab Ab | A method and a production line for the manufacture of a torsion-box type skin composite structure |
| ITMI20131364A1 (it) * | 2013-08-08 | 2015-02-09 | Sparco S P A | Metodo per produzione di un prodotto composito che prevede una matrice polimerica presentante fibre di rinforzo, e prodotto ottenuto con tale metodo |
| ES2674659T3 (es) | 2013-09-23 | 2018-07-03 | Airbus Operations S.L. | Método para fabricar una caja de torsión aeronáutica, caja de torsión y herramienta para fabricar una caja de torsión aeronáutica |
| US20170274577A1 (en) * | 2016-03-24 | 2017-09-28 | The Boeing Company | Composite structures with stiffeners and method of making the same |
| DE102018105765A1 (de) * | 2018-03-13 | 2019-09-19 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zum Herstellen eines Faserverbund-Hohlbauteils und Faserverbund-Hohlbauteil |
| US10899084B2 (en) * | 2018-07-16 | 2021-01-26 | Textron Innovations, Inc. | Methods for forming composite structures |
| US12195201B2 (en) * | 2020-11-18 | 2025-01-14 | The Boeing Company | Composite preform assembly method and apparatus |
| CN114103171B (zh) * | 2021-11-24 | 2024-04-12 | 长三角先进材料研究院 | 一种适用于多腔结构的预浸料增强树脂传递成型方法 |
| US12203333B2 (en) | 2022-06-06 | 2025-01-21 | Halliburton Energy Services, Inc. | Composite wellbore sealing device |
| US12122501B1 (en) | 2023-09-06 | 2024-10-22 | Jetzero, Inc. | Aircraft with carbon fiber material and a method of manufacture |
| CN119305223B (zh) * | 2024-11-19 | 2025-12-19 | 江苏新扬新材料股份有限公司 | 一种复合材料电磁防护罩制作方法 |
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| US4758395A (en) * | 1986-11-04 | 1988-07-19 | Owens-Corning Fiberglas Corporation | Method of molding thick parts of fibrous-ply-reinforced resin |
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| US5968445A (en) * | 1998-01-05 | 1999-10-19 | The Boeing Company | Method and apparatus for curing large composite panels |
| JP2000238154A (ja) * | 1999-02-19 | 2000-09-05 | Toray Ind Inc | ハニカムサンドイッチパネル |
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| WO2001041993A2 (en) | 1999-12-07 | 2001-06-14 | The Boeing Company | Double bag vacuum infusion process and system for low cost, advanced composite fabrication |
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| JP4609745B2 (ja) * | 2000-12-06 | 2011-01-12 | 東レ株式会社 | Frpの真空成形方法 |
| US6638466B1 (en) * | 2000-12-28 | 2003-10-28 | Raytheon Aircraft Company | Methods of manufacturing separable structures |
| US20030051434A1 (en) * | 2001-09-20 | 2003-03-20 | Lockheed Martin Corporation | Composite structure and method for constructing same |
| DE10156123B4 (de) | 2001-11-16 | 2006-07-27 | Eads Deutschland Gmbh | Verfahren und Vorrichtung zur Herstellung von faserverstärkten Kunststoffbauteilen |
-
2002
- 2002-09-13 US US10/243,796 patent/US7419627B2/en not_active Expired - Lifetime
-
2003
- 2003-09-02 DE DE60303484T patent/DE60303484T2/de not_active Expired - Lifetime
- 2003-09-02 AT AT03255455T patent/ATE317324T1/de not_active IP Right Cessation
- 2003-09-02 ES ES03255455T patent/ES2256679T3/es not_active Expired - Lifetime
- 2003-09-02 EP EP03255455A patent/EP1400341B1/de not_active Expired - Lifetime
- 2003-09-05 JP JP2003314299A patent/JP2004106548A/ja not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| US20040051214A1 (en) | 2004-03-18 |
| US7419627B2 (en) | 2008-09-02 |
| JP2004106548A (ja) | 2004-04-08 |
| EP1400341A1 (de) | 2004-03-24 |
| DE60303484T2 (de) | 2006-10-19 |
| EP1400341B1 (de) | 2006-02-08 |
| ES2256679T3 (es) | 2006-07-16 |
| DE60303484D1 (de) | 2006-04-20 |
| HK1064989A1 (en) | 2005-02-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |