ATE380650T1 - Heiss-schmelzimprägnierverfafren eines 3-d, aus fasergewebe bestehenden vorformlings - Google Patents
Heiss-schmelzimprägnierverfafren eines 3-d, aus fasergewebe bestehenden vorformlingsInfo
- Publication number
- ATE380650T1 ATE380650T1 AT02752467T AT02752467T ATE380650T1 AT E380650 T1 ATE380650 T1 AT E380650T1 AT 02752467 T AT02752467 T AT 02752467T AT 02752467 T AT02752467 T AT 02752467T AT E380650 T1 ATE380650 T1 AT E380650T1
- Authority
- AT
- Austria
- Prior art keywords
- resin
- preform
- infuse
- hot
- infusion
- Prior art date
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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
- B29B15/12—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length
- B29B15/122—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length with a matrix in liquid form, e.g. as melt, solution or latex
-
- 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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0067—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other
- B29C37/0075—Using separating agents during or after moulding; Applying separating agents on preforms or articles, e.g. to prevent sticking to each other using release sheets
-
- 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
- B29C70/465—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 and impregnating by melting a solid material, e.g. sheets, powders of fibres
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/18—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/001—Profiled members, e.g. beams, sections
- B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
- Reinforced Plastic Materials (AREA)
- Glass Compositions (AREA)
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Laminated Bodies (AREA)
- Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/942,332 US6676882B2 (en) | 2001-08-28 | 2001-08-28 | Methods of hot-melt resin impregnation of 3-D, woven, textile preforms |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE380650T1 true ATE380650T1 (de) | 2007-12-15 |
Family
ID=25477936
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT02752467T ATE380650T1 (de) | 2001-08-28 | 2002-07-19 | Heiss-schmelzimprägnierverfafren eines 3-d, aus fasergewebe bestehenden vorformlings |
Country Status (6)
Country | Link |
---|---|
US (2) | US6676882B2 (de) |
EP (1) | EP1423257B1 (de) |
AT (1) | ATE380650T1 (de) |
AU (1) | AU2002361466A1 (de) |
DE (1) | DE60224058T2 (de) |
WO (1) | WO2003020495A1 (de) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0229094D0 (en) * | 2002-12-13 | 2003-01-15 | Hexcel Composites Ltd | Improvements in or relating to the preparation of fibre-reinforced composites |
US7244487B2 (en) * | 2003-04-24 | 2007-07-17 | Lockheed Martin Corporation | Apparatus, system, and method of joining structural components with a tapered tension bond joint |
US20050215148A1 (en) * | 2004-03-25 | 2005-09-29 | Pc Composites Ltd. | Pre-impregnated materials |
WO2005091715A2 (en) * | 2004-03-25 | 2005-10-06 | Pc Composites Ltd. | Improved pre-impregnated materials and apparatus and methods for manufacture thereof |
US7276868B2 (en) * | 2004-03-29 | 2007-10-02 | Allred Iii Jimmie B | Carbon-fiber laminate musical instrument sound board |
WO2006026734A2 (en) | 2004-08-31 | 2006-03-09 | Obermeyer Henry K | High strength joining system for fiber reinforced composites |
US7258828B2 (en) * | 2004-09-03 | 2007-08-21 | Lockheed Martin Corporation | Infusion joining of composite structures |
US7153379B2 (en) * | 2004-10-15 | 2006-12-26 | General Electric Company | Methods of producing a ceramic matrix composite |
US7713893B2 (en) * | 2004-12-08 | 2010-05-11 | Albany Engineered Composites, Inc. | Three-dimensional woven integrally stiffened panel |
US7332049B2 (en) * | 2004-12-22 | 2008-02-19 | General Electric Company | Method for fabricating reinforced composite materials |
US7431978B2 (en) * | 2004-12-22 | 2008-10-07 | General Electric Company | Reinforced matrix composite containment duct |
US7931852B2 (en) * | 2005-02-04 | 2011-04-26 | Terry Kieffer | Process and apparatus for reinforced polymer composites |
US8017057B2 (en) | 2006-06-15 | 2011-09-13 | E. I. Du Pont De Nemours And Company | Method for making a pressed part with separations or voids |
US7712488B2 (en) * | 2008-03-31 | 2010-05-11 | Albany Engineered Composites, Inc. | Fiber architecture for Pi-preforms |
US20100055257A1 (en) * | 2008-08-31 | 2010-03-04 | Dana Petersen Hervig | Chocolate candy |
FR2936442B1 (fr) * | 2008-09-30 | 2013-03-08 | Airbus France | Dispositif pour la fabrication d'une piece en materiau composite de forme complexe. |
US8079387B2 (en) * | 2008-10-29 | 2011-12-20 | Albany Engineered Composites, Inc. | Pi-shaped preform |
US8127802B2 (en) * | 2008-10-29 | 2012-03-06 | Albany Engineered Composites, Inc. | Pi-preform with variable width clevis |
US8846553B2 (en) * | 2008-12-30 | 2014-09-30 | Albany Engineered Composites, Inc. | Woven preform with integral off axis stiffeners |
US20100186893A1 (en) | 2009-01-29 | 2010-07-29 | Lockheed Martin Corporation | System, method and apparatus for fabricating composite structures |
US9551094B2 (en) * | 2011-12-14 | 2017-01-24 | Snecma | Fiber preform of π-shaped section, in particular for a fan platform made of composite material |
DE102012010271B4 (de) * | 2012-05-25 | 2017-10-12 | Premium Aerotec Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils mittels eines Vakuumaufbaues |
US9889613B2 (en) | 2012-11-01 | 2018-02-13 | Israel Aerospace Industries Ltd. | Manufacture of integrated structures formed of composite materials |
US20140166191A1 (en) * | 2012-12-14 | 2014-06-19 | Aurora Flight Sciences Corporation | Methods for combining components of varying stages of cure |
US10807320B1 (en) | 2013-04-29 | 2020-10-20 | Terry Kieffer | Fabrication apparatuses and methods |
US11969931B1 (en) | 2013-04-29 | 2024-04-30 | Plastics Unlimited, Inc. | Fabrication apparatuses and methods |
US11052619B1 (en) | 2013-04-29 | 2021-07-06 | Plastics Unlimited, Inc. | Fabrication apparatuses and methods |
US10818274B2 (en) | 2016-05-23 | 2020-10-27 | Andrew Glasser | Apparatus and methods for carbon composite stringed instruments |
DK3475068T3 (da) * | 2016-06-28 | 2021-06-21 | Vestas Wind Sys As | Fremstilling af en vindmøllevinge |
US11332228B2 (en) | 2018-04-06 | 2022-05-17 | Aurora Flight Sciences Corporation | Aircraft fuselage with composite pre-form |
CN112454948B (zh) * | 2020-10-22 | 2022-10-18 | 中国航空制造技术研究院 | 一种rfi工艺树脂膜预置方式的确定方法 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2497839A1 (fr) * | 1981-01-12 | 1982-07-16 | Brochier Fils J | Tissu tridimensionnel pour le renforcement de materiaux stratifies et elements en forme obtenus a partir d'un tel tissu |
US4622091A (en) | 1984-11-29 | 1986-11-11 | The Boeing Company | Resin film infusion process and apparatus |
US4966802A (en) * | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
US4671470A (en) | 1985-07-15 | 1987-06-09 | Beech Aircraft Corporation | Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors |
JPH0778303B2 (ja) | 1987-02-03 | 1995-08-23 | 三菱重工業株式会社 | 複合材強化用の繊維構造体の製造方法 |
US5139405A (en) * | 1988-05-31 | 1992-08-18 | Phillips Petroleum Company | Composite with integrally molded rib and manufacture thereof |
FR2699449B1 (fr) | 1992-12-17 | 1995-03-24 | Eurocopter France | Procédé de fabrication de liaisons en matériau composite de structures en forme de treillis ou d'éléments de treillis, et treillis obtenus par ce procédé. |
US6242090B1 (en) * | 1993-07-26 | 2001-06-05 | Hexcel Corporation | Fibre reinforced resin composite products |
ES2112744B1 (es) * | 1994-12-02 | 1998-12-01 | Porta Miguel Alives | Procedimiento y disposicion para modelado de una forma tridimensional en una tela. |
US5874133A (en) | 1995-06-07 | 1999-02-23 | Randemo, Inc. | Process for making a polyurethane composite |
US5681513A (en) | 1995-08-04 | 1997-10-28 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method for fabricating composite structures using continuous press forming |
US6139942A (en) * | 1997-02-06 | 2000-10-31 | Cytec Technology, Inc. | Resin composition, a fiber reinforced material having a partially impregnated resin and composites made therefrom |
US5902535A (en) * | 1997-07-30 | 1999-05-11 | Mcdonnell Douglas Corporation | Resin film infusion mold tooling and molding method |
DE19803062C1 (de) | 1998-01-28 | 1999-10-28 | Rainer Lebmeier | Verfahren zur Herstellung von Faserverbund-Formteilen, insbesondere Hohlprofilteilen |
DE69913737T3 (de) * | 1998-05-20 | 2009-05-14 | Cytec Technology Corp., Wilmington | Herstellung von blasenfreien Laminaten und Verwendung derselben |
US6128998A (en) | 1998-06-12 | 2000-10-10 | Foster Miller, Inc. | Continuous intersecting braided composite structure and method of making same |
US6520706B1 (en) | 2000-08-25 | 2003-02-18 | Lockheed Martin Corporation | Composite material support structures with sinusoidal webs and method of fabricating same |
US6374570B1 (en) * | 2000-08-25 | 2002-04-23 | Lockheed Martin Corporation | Apparatus and method for joining dissimilar materials to form a structural support member |
-
2001
- 2001-08-28 US US09/942,332 patent/US6676882B2/en not_active Expired - Lifetime
-
2002
- 2002-07-19 AT AT02752467T patent/ATE380650T1/de not_active IP Right Cessation
- 2002-07-19 WO PCT/US2002/022987 patent/WO2003020495A1/en active IP Right Grant
- 2002-07-19 EP EP02752467A patent/EP1423257B1/de not_active Expired - Lifetime
- 2002-07-19 AU AU2002361466A patent/AU2002361466A1/en not_active Abandoned
- 2002-07-19 DE DE60224058T patent/DE60224058T2/de not_active Expired - Lifetime
-
2003
- 2003-11-12 US US10/706,511 patent/US6911175B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US20040104516A1 (en) | 2004-06-03 |
DE60224058D1 (de) | 2008-01-24 |
EP1423257A1 (de) | 2004-06-02 |
AU2002361466A1 (en) | 2003-03-18 |
WO2003020495A8 (en) | 2003-04-10 |
US6911175B2 (en) | 2005-06-28 |
US6676882B2 (en) | 2004-01-13 |
EP1423257B1 (de) | 2007-12-12 |
DE60224058T2 (de) | 2008-12-04 |
WO2003020495A1 (en) | 2003-03-13 |
US20030042659A1 (en) | 2003-03-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |