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ATE353042T1 - Verfahren zur herstellung einer verbundstruktur - Google Patents

Verfahren zur herstellung einer verbundstruktur

Info

Publication number
ATE353042T1
ATE353042T1 AT03078237T AT03078237T ATE353042T1 AT E353042 T1 ATE353042 T1 AT E353042T1 AT 03078237 T AT03078237 T AT 03078237T AT 03078237 T AT03078237 T AT 03078237T AT E353042 T1 ATE353042 T1 AT E353042T1
Authority
AT
Austria
Prior art keywords
prepreg sheets
stack
vacuum
vacuum bag
mold
Prior art date
Application number
AT03078237T
Other languages
English (en)
Inventor
Max Krogager
Jan Vaara
Original Assignee
Saab Ab
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=34354522&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ATE353042(T1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Saab Ab filed Critical Saab Ab
Application granted granted Critical
Publication of ATE353042T1 publication Critical patent/ATE353042T1/de

Links

Classifications

    • 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
    • B29C70/544—Details of vacuum bags, e.g. materials or shape
    • 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
    • B29C70/547—Measures for feeding or distributing the matrix material in the reinforcing structure using channels or porous distribution layers incorporated in or associated with the product
    • 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
    • B32B5/28—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 impregnated with or embedded in a plastic substance
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B32B2260/023—Two or more layers
    • 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
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Glass Compositions (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
AT03078237T 2003-10-14 2003-10-14 Verfahren zur herstellung einer verbundstruktur ATE353042T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03078237A EP1524106B1 (de) 2003-10-14 2003-10-14 Verfahren zur Herstellung einer Verbundstruktur

Publications (1)

Publication Number Publication Date
ATE353042T1 true ATE353042T1 (de) 2007-02-15

Family

ID=34354522

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03078237T ATE353042T1 (de) 2003-10-14 2003-10-14 Verfahren zur herstellung einer verbundstruktur

Country Status (5)

Country Link
US (1) US20050194724A1 (de)
EP (1) EP1524106B1 (de)
AT (1) ATE353042T1 (de)
DE (1) DE60311580T2 (de)
ES (1) ES2279930T3 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050236736A1 (en) * 2004-04-23 2005-10-27 Formella Stephen C Composite product and forming system
US8287681B2 (en) * 2005-08-04 2012-10-16 Israel Aerospace Industries Ltd. Method for making composite articles with artificial defects
US20070222122A1 (en) * 2006-03-23 2007-09-27 Ching-Long Ong Brightened composite sheel and method for making the same
FR2905891B1 (fr) * 2006-09-15 2008-12-05 Airbus France Sa Procede de fabrication d'un panneau en materiau composite thermoplastique
ATE555636T1 (de) 2007-01-25 2012-05-15 Gen Hospital Corp Verfahren zur herstellung von oxidationsbeständigem vernetztem polymermaterial
US20080277531A1 (en) * 2007-05-11 2008-11-13 The Boeing Company Hybrid Composite Panel Systems and Methods
DE102008008198A1 (de) * 2008-01-31 2009-08-06 Deutsches Zentrum für Luft- und Raumfahrt e.V. Mehrlagiges faserverstärktes Thermoplast-Flachmaterial sowie Verfahren zu seiner Herstellung
CA2741171A1 (en) * 2008-10-29 2010-05-06 Saab Ab Hot drape forming by means of a stiffness controlled vacuum bag
DE102008056307A1 (de) 2008-11-07 2010-05-12 Benteler Sgl Gmbh & Co. Kg Vorrichtung und Verfahren zur Herstellung von Formbauteilen durch Formgebung von Prepregs
US9073270B2 (en) * 2009-01-21 2015-07-07 Vestas Wind Systems A/S Method of manufacturing a wind turbine blade by embedding a layer of pre-cured fibre reinforced resin
DE102010054055A1 (de) * 2010-12-10 2012-06-14 Giesecke & Devrient Gmbh Herstellung eines kartenförmigen Datenträgers
WO2014013137A1 (en) * 2012-07-20 2014-01-23 Ahlstrom Corporation A unidirectional reinforcement and a method of producing a unidirectional reinforcement
CN102926577B (zh) * 2012-11-19 2015-01-21 北京玻钢院复合材料有限公司 一种可调节松紧的复合材料联接构件及制作方法与组装
BR112015020629A2 (pt) * 2013-02-26 2017-07-18 Hexcel Holding Gmbh fabricação de uma peça moldada
CN105269830A (zh) * 2014-07-08 2016-01-27 哈尔滨飞机工业集团有限责任公司 一种用于高厚度低密度蜂窝预成型方法
CN104772913B (zh) * 2015-04-22 2017-02-01 哈尔滨工业大学 一种多稳态可变形开关结构的设计方法
CN105014988A (zh) * 2015-06-18 2015-11-04 上海耀华大中新材料有限公司 一种碳纤维汽车电池盒的制造方法及碳纤维汽车电池盒
CN104999673A (zh) * 2015-06-19 2015-10-28 湖南大学 一种替代金属的无纺纤维复合材料成型方法
US10556691B2 (en) 2015-11-25 2020-02-11 The Boeing Company Seat tracks with composite frames
KR102362050B1 (ko) 2016-10-26 2022-02-11 도레이 카부시키가이샤 프리프레그 적층체, 섬유 강화 복합 재료 및 섬유 강화 복합 재료의 제조 방법
EP3535490B1 (de) 2016-12-21 2022-10-19 Siemens Gamesa Renewable Energy A/S Verfahren zum aufbringen einer schutzschicht auf einer windturbinenrotorschaufel
CN107599451A (zh) * 2017-10-17 2018-01-19 浙江石金玄武岩纤维股份有限公司 一种制作双面光滑的复合材料制品的真空袋成型工艺

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2482981A (en) * 1948-01-28 1949-09-27 Kamrass Ellis Deep-drawn recessed decorated pleated doily
US2913036A (en) * 1956-08-10 1959-11-17 Anthony Bros Fibre Glass Pool Process and apparatus for molding large plastic structures
GB2124130B (en) * 1982-07-24 1985-11-27 Rolls Royce Vacuum moulding fibre reinforced resin
US5589016A (en) * 1994-04-29 1996-12-31 The Boeing Company Prescored foam for panel fabrication
JPH08118381A (ja) * 1994-10-19 1996-05-14 Mitsubishi Rayon Co Ltd Ｃｆｒｐ成形物の製造方法
US6017484A (en) * 1997-01-21 2000-01-25 Harold P. Hale Method for manufacture of minimum porosity, wrinkle free composite parts
DE69913737T3 (de) * 1998-05-20 2009-05-14 Cytec Technology Corp., Wilmington Herstellung von blasenfreien Laminaten und Verwendung derselben

Also Published As

Publication number Publication date
ES2279930T3 (es) 2007-09-01
EP1524106A1 (de) 2005-04-20
DE60311580D1 (de) 2007-03-22
EP1524106B1 (de) 2007-01-31
US20050194724A1 (en) 2005-09-08
DE60311580T2 (de) 2007-10-31

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Legal Events

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