MX2011013225A - Metodo para producir componentes compuestos avanzados. - Google Patents

Metodo para producir componentes compuestos avanzados.

Info

Publication number
MX2011013225A
MX2011013225A MX2011013225A MX2011013225A MX2011013225A MX 2011013225 A MX2011013225 A MX 2011013225A MX 2011013225 A MX2011013225 A MX 2011013225A MX 2011013225 A MX2011013225 A MX 2011013225A MX 2011013225 A MX2011013225 A MX 2011013225A
Authority
MX
Mexico
Prior art keywords
resin
mould
resin layer
solidifying
opposing
Prior art date
Application number
MX2011013225A
Other languages
English (en)
Spanish (es)
Inventor
Neil Deryck Bray Graham
Original Assignee
Quickstep Technologies Pty Ltd
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
Priority claimed from AU2009902686A external-priority patent/AU2009902686A0/en
Application filed by Quickstep Technologies Pty Ltd filed Critical Quickstep Technologies Pty Ltd
Publication of MX2011013225A publication Critical patent/MX2011013225A/es

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
    • B29C70/24—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 three directions forming a three-dimensional [3D] structure
    • 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
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
    • B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
    • 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
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • 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
    • 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
    • Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
MX2011013225A 2009-06-12 2010-06-10 Metodo para producir componentes compuestos avanzados. MX2011013225A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU2009902686A AU2009902686A0 (en) 2009-06-12 Method of Producing Advanced Composite Components
PCT/AU2010/000709 WO2010141984A1 (en) 2009-06-12 2010-06-10 Method of producing advanced composite components

Publications (1)

Publication Number Publication Date
MX2011013225A true MX2011013225A (es) 2012-04-02

Family

ID=43308309

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2011013225A MX2011013225A (es) 2009-06-12 2010-06-10 Metodo para producir componentes compuestos avanzados.

Country Status (12)

Country Link
US (1) US20120135219A1 (enExample)
EP (1) EP2440391B1 (enExample)
JP (1) JP5901518B2 (enExample)
KR (1) KR20120036969A (enExample)
CN (1) CN102481731B (enExample)
AU (1) AU2010258088B2 (enExample)
BR (1) BR112012000195A2 (enExample)
CA (1) CA2764863A1 (enExample)
IL (1) IL216894A0 (enExample)
MX (1) MX2011013225A (enExample)
RU (1) RU2533132C2 (enExample)
WO (1) WO2010141984A1 (enExample)

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* Cited by examiner, † Cited by third party
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BR0117299B1 (pt) * 2000-03-03 2014-11-25 Quickstep Technologies Pty Ltd Métodos para unir componentes compósitos
ES2445708T3 (es) * 2010-11-04 2014-03-04 Siemens Aktiengesellschaft Método para fabricar una pala
RU2013131287A (ru) * 2010-12-09 2015-01-20 Квикстэп Текнолоджиз Пти Лтд Производство и ремонт армированных волокнами композитных компонентов с улучшенными поверхностными и адгезионными свойствами
CN102729486B (zh) * 2012-06-05 2015-02-25 东华大学 一种热塑性树脂/玉米苞衣复合材料的制备方法
CN103072289A (zh) * 2012-12-24 2013-05-01 中国科学院福建物质结构研究所 一种提高纤维增强树脂基复合材料层间韧性的方法
US10759140B1 (en) 2013-05-17 2020-09-01 United States of America as Represented by the Admin of the National Aeronautics and Space Administration Composite damage tolerance and through thickness conductivity by interleaving carbon fiber veil nanocomposites
RU2611540C2 (ru) * 2014-12-24 2017-02-28 Федеральное государственное бюджетное образовательное учреждение высшего образования "Саратовский национальный исследовательский государственный университет имени Н.Г. Чернышевского" Способ получения композитного материала на подложке
JP7198454B2 (ja) * 2018-02-27 2023-01-04 国立大学法人東海国立大学機構 繊維強化熱可塑性樹脂の成形物の製造方法
CN109228397B (zh) * 2018-08-03 2024-02-23 中国人民解放军92578部队 一种复合材料推进器模压模具及其产品
US11633881B1 (en) 2018-12-20 2023-04-25 General Nano Llc Heated composite tool and method for building and use
JP2023514380A (ja) * 2020-03-06 2023-04-05 ギャラクティック コ.,エルエルシー 車両用成形複合材スキンおよびその高速製造方法
CN111674541B (zh) * 2020-05-25 2023-04-18 哈尔滨工业大学 一种柔性复合蒙皮及其制造方法、工装结构
CN112571828B (zh) * 2020-11-25 2022-10-11 长春长光宇航复合材料有限公司 一种Z-Pin预制结构及使用Z-Pin预制结构Z向增强植入方法
CN112590255A (zh) * 2020-11-25 2021-04-02 廊坊市飞泽复合材料科技有限公司 一种三明治复合材料湿法模压成型方法
FR3124971B1 (fr) 2021-07-06 2023-12-15 Centre Technique Ind De La Plasturgie Et Des Composites Appareil de moulage
CN114161738B (zh) * 2021-11-29 2023-10-13 航天特种材料及工艺技术研究所 一种适用于rtm工艺的低密度纤维增强体增强材料构件净尺寸成型的方法
EP4458567B1 (en) * 2023-05-03 2026-03-04 Fokker Aerostructures B.V. Out-of-autoclave thermoplastic consolidation apparatus and method

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US3048896A (en) * 1959-05-26 1962-08-14 Marlo Arvid Centrifugal rotational molding method
US3809735A (en) * 1968-09-26 1974-05-07 R Cotterell Method of moulding heat-expandable thermoplastic polymeric resinous granules involving enhanced distribution of the hot gaseous medium in the mold cavity
US3755713A (en) * 1972-07-25 1973-08-28 Boeing Co Electrically conductive surface for aircraft
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US4352142A (en) * 1981-04-15 1982-09-28 The Boeing Company Composite aircraft structure having lightning protection
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US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
DE3246803A1 (de) * 1982-12-17 1984-06-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zum herstellen von bauteilen aus lagen von faserverstaerktem kunststoff
US4622091A (en) * 1984-11-29 1986-11-11 The Boeing Company Resin film infusion process and apparatus
FR2592404B1 (fr) * 1985-12-30 1989-06-09 Pradom Ltd Nouveaux materiaux composites fibre-matrice a fibres strictement positionnees et orientees et leur procede de preparation.
US5641366A (en) * 1988-01-20 1997-06-24 Loral Vought Systems Corporation Method for forming fiber-reinforced composite
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Also Published As

Publication number Publication date
CN102481731B (zh) 2014-10-29
EP2440391A4 (en) 2015-04-15
JP5901518B2 (ja) 2016-04-13
KR20120036969A (ko) 2012-04-18
EP2440391B1 (en) 2017-04-26
IL216894A0 (en) 2012-02-29
AU2010258088B2 (en) 2013-11-28
AU2010258088A1 (en) 2012-01-12
US20120135219A1 (en) 2012-05-31
BR112012000195A2 (pt) 2019-09-24
JP2012529385A (ja) 2012-11-22
CA2764863A1 (en) 2010-12-16
RU2533132C2 (ru) 2014-11-20
CN102481731A (zh) 2012-05-30
EP2440391A1 (en) 2012-04-18
WO2010141984A1 (en) 2010-12-16
RU2012100713A (ru) 2013-07-20

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Legal Events

Date Code Title Description
FG Grant or registration