ATE446991T1 - Epoxidharzzusammensetzungen für die herstellung von blasenfreien laminaten - Google Patents
Epoxidharzzusammensetzungen für die herstellung von blasenfreien laminatenInfo
- Publication number
- ATE446991T1 ATE446991T1 AT03078545T AT03078545T ATE446991T1 AT E446991 T1 ATE446991 T1 AT E446991T1 AT 03078545 T AT03078545 T AT 03078545T AT 03078545 T AT03078545 T AT 03078545T AT E446991 T1 ATE446991 T1 AT E446991T1
- Authority
- AT
- Austria
- Prior art keywords
- epoxy resin
- resin compositions
- producing bubble
- free laminates
- chem
- Prior art date
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- 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
-
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/546—Measures for feeding or distributing the matrix material in the reinforcing structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
- C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
- C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
- C08G59/20—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
- C08G59/32—Epoxy compounds containing three or more epoxy groups
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
- C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
- C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
- C08G59/20—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
- C08G59/32—Epoxy compounds containing three or more epoxy groups
- C08G59/3218—Carbocyclic compounds
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
- C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
- C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
- C08G59/20—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
- C08G59/32—Epoxy compounds containing three or more epoxy groups
- C08G59/38—Epoxy compounds containing three or more epoxy groups together with di-epoxy compounds
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
- C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
- C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L63/00—Compositions of epoxy resins; Compositions of derivatives of epoxy resins
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/249928—Fiber embedded in a ceramic, glass, or carbon matrix
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/249933—Fiber embedded in or on the surface of a natural or synthetic rubber matrix
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/249942—Fibers are aligned substantially parallel
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/249942—Fibers are aligned substantially parallel
- Y10T428/249944—Fiber is precoated
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/249942—Fibers are aligned substantially parallel
- Y10T428/249945—Carbon or carbonaceous fiber
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
- Y10T428/24994—Fiber embedded in or on the surface of a polymeric matrix
- Y10T428/249942—Fibers are aligned substantially parallel
- Y10T428/249947—Polymeric fiber
Landscapes
- Chemical & Material Sciences (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Inorganic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Reinforced Plastic Materials (AREA)
- Epoxy Resins (AREA)
- Laminated Bodies (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US8614298P | 1998-05-20 | 1998-05-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE446991T1 true ATE446991T1 (de) | 2009-11-15 |
Family
ID=22196547
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT03078545T ATE446991T1 (de) | 1998-05-20 | 1999-05-20 | Epoxidharzzusammensetzungen für die herstellung von blasenfreien laminaten |
AT99949525T ATE256550T1 (de) | 1998-05-20 | 1999-05-20 | Herstellung von blasenfreien laminaten und deren anwendung |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT99949525T ATE256550T1 (de) | 1998-05-20 | 1999-05-20 | Herstellung von blasenfreien laminaten und deren anwendung |
Country Status (13)
Country | Link |
---|---|
US (1) | US6391436B1 (de) |
EP (2) | EP1408084B1 (de) |
JP (1) | JP4477271B2 (de) |
KR (1) | KR100576767B1 (de) |
AT (2) | ATE446991T1 (de) |
AU (1) | AU764214C (de) |
BR (1) | BR9911042B1 (de) |
CA (5) | CA2511571C (de) |
DE (2) | DE69941609D1 (de) |
ES (2) | ES2213390T5 (de) |
MX (1) | MXPA00011445A (de) |
NO (1) | NO325325B1 (de) |
WO (1) | WO2001000405A2 (de) |
Families Citing this family (88)
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DE10013409C1 (de) * | 2000-03-17 | 2000-11-23 | Daimler Chrysler Ag | Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens |
GB0110316D0 (en) * | 2001-04-27 | 2001-06-20 | Advanced Composites Group Ltd | Improvements in or relating to moulding materials |
US6676882B2 (en) * | 2001-08-28 | 2004-01-13 | Lockheed Martin Corporation | Methods of hot-melt resin impregnation of 3-D, woven, textile preforms |
GB0205498D0 (en) | 2002-03-08 | 2002-04-24 | Structural Polymer Systems Ltd | Moulding material |
US7100656B2 (en) * | 2002-04-15 | 2006-09-05 | Northrop Grumman Corporation | System and method for curing composite material |
CN100431815C (zh) * | 2002-07-18 | 2008-11-12 | 三菱丽阳株式会社 | 半固化片、frp成型用中间材料及其制造方法和纤维增强复合材料的制造方法 |
EP1563974B1 (de) * | 2002-10-23 | 2009-07-01 | Mitsubishi Rayon Co., Ltd. | Herstellungsverfahren für ein prepreg |
US20040079474A1 (en) * | 2002-10-24 | 2004-04-29 | Nitto Denko Corporation | Production method of anisotropic conductive connector |
JP2004330474A (ja) * | 2003-05-01 | 2004-11-25 | Kawasaki Heavy Ind Ltd | 複合材製品の製造方法 |
US7213629B2 (en) * | 2003-05-14 | 2007-05-08 | The Boeing Company | Vacuum assisted ply placement shoe and method |
ATE353042T1 (de) * | 2003-10-14 | 2007-02-15 | Saab Ab | Verfahren zur herstellung einer verbundstruktur |
US20050126699A1 (en) * | 2003-12-15 | 2005-06-16 | Anna Yen | Process for the manufacture of composite structures |
US20050255311A1 (en) * | 2004-04-23 | 2005-11-17 | Formella Stephen C | Hybrid composite product and system |
US20050236736A1 (en) * | 2004-04-23 | 2005-10-27 | Formella Stephen C | Composite product and forming system |
US7153379B2 (en) * | 2004-10-15 | 2006-12-26 | General Electric Company | Methods of producing a ceramic matrix composite |
US7332049B2 (en) | 2004-12-22 | 2008-02-19 | General Electric Company | Method for fabricating reinforced composite materials |
DE102005008231A1 (de) * | 2005-02-23 | 2006-08-24 | Hübner GmbH | Elastische Seitenwand zur Abdeckung eines Balges eines Übergangs zwischen zwei gelenkig miteinander verbundenen Fahrzeugen oder Fahrzeugteilen |
US7766063B2 (en) * | 2005-04-28 | 2010-08-03 | The Boeing Company | Machine assisted laminator and method |
JP5144010B2 (ja) * | 2005-10-06 | 2013-02-13 | 三菱レイヨン株式会社 | 繊維強化プラスチックパネルの製造方法 |
JP2007098819A (ja) * | 2005-10-06 | 2007-04-19 | Mitsubishi Rayon Co Ltd | サンドイッチパネルの製造方法 |
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US20080044659A1 (en) * | 2005-12-15 | 2008-02-21 | Polystrand, Inc. | Composite laminate and method of manufacture |
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US20090280324A1 (en) * | 2006-05-22 | 2009-11-12 | Florida State University Research Foundation | Prepreg Nanoscale Fiber Films and Methods |
DE102006038666B4 (de) * | 2006-08-17 | 2009-09-24 | Airbus Deutschland Gmbh | Herstellungsverfahren für ein Werkstück aus einem Faserverbundwerkstoff und Vorrichtung zum Herstellen eines Werkstücks aus einem Faserverbundwerkstoff |
US8920698B2 (en) | 2006-08-17 | 2014-12-30 | Airbus Operations Gmbh | Production method for a workpiece composed of a fibre-composite material |
JP2009523083A (ja) | 2006-09-06 | 2009-06-18 | ポリストランド インコーポレイティッド | 複合積層板とその製法 |
US7849729B2 (en) * | 2006-12-22 | 2010-12-14 | The Boeing Company | Leak detection in vacuum bags |
US20080274343A1 (en) * | 2007-05-01 | 2008-11-06 | The Diller Corporation | Thick solid surface laminate product and method of making same |
US8568551B2 (en) * | 2007-05-22 | 2013-10-29 | The Boeing Company | Pre-patterned layup kit and method of manufacture |
US9770871B2 (en) | 2007-05-22 | 2017-09-26 | The Boeing Company | Method and apparatus for layup placement |
EP2148907B1 (de) | 2007-05-23 | 2012-04-11 | Hexcel Composites, Ltd. | Haftvermittlerschicht für verbundanordnungen |
US9042338B2 (en) | 2007-07-09 | 2015-05-26 | Intel Mobile Communications GmbH | Communication device and method for transmitting data |
US8029642B2 (en) | 2007-07-27 | 2011-10-04 | The Boeing Company | Tape removal apparatus and process |
US8936695B2 (en) | 2007-07-28 | 2015-01-20 | The Boeing Company | Method for forming and applying composite layups having complex geometries |
US8333864B2 (en) * | 2008-09-30 | 2012-12-18 | The Boeing Company | Compaction of prepreg plies on composite laminate structures |
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US8345269B2 (en) | 2007-09-22 | 2013-01-01 | The Boeing Company | Method and apparatus for measuring the width of composite tape |
US9302436B2 (en) | 2007-11-26 | 2016-04-05 | Textron Innovations Inc | In-situ, multi-stage debulk, compaction, and single stage curing of thick composite repair laminates |
CA2705777C (en) | 2007-11-26 | 2014-01-07 | Bell Helicopter Textron Inc. | Multi-stage debulk and compaction of thick composite repair laminates |
EP2212100B1 (de) * | 2007-11-26 | 2016-02-17 | Bell Helicopter Textron Inc. | In-situ mehrstufiges verkleinern, verdichten und einstufiges aushärten von dicken verbundreparaturlaminaten |
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US9096734B2 (en) | 2009-01-23 | 2015-08-04 | Hexcel Corporation | Prepreg with integrated multi-dimensional gas venting network |
US8308101B2 (en) | 2009-03-09 | 2012-11-13 | The Boeing Company | Simplified fiber tensioning for automated fiber placement machines |
US8454788B2 (en) | 2009-03-13 | 2013-06-04 | The Boeing Company | Method and apparatus for placing short courses of composite tape |
WO2011037239A1 (ja) | 2009-09-28 | 2011-03-31 | 三菱レイヨン株式会社 | 繊維強化複合材料 |
JP5473585B2 (ja) * | 2009-12-24 | 2014-04-16 | 三菱レイヨン株式会社 | エポキシ樹脂組成物 |
GB201009851D0 (en) * | 2010-06-14 | 2010-07-21 | Hexcel Composites Ltd | Improvements in composite materials |
CN103201102B (zh) | 2010-11-08 | 2015-07-01 | 东丽株式会社 | 用于纤维强化复合材料的环氧树脂组合物、预浸料坯和纤维强化复合材料 |
US8551380B2 (en) | 2010-11-12 | 2013-10-08 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
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