[go: up one dir, main page]

RU2014131075A - Углеродноволокнистая основа, препрег и композитный материал, армированный углеродным волокном - Google Patents

Углеродноволокнистая основа, препрег и композитный материал, армированный углеродным волокном Download PDF

Info

Publication number
RU2014131075A
RU2014131075A RU2014131075A RU2014131075A RU2014131075A RU 2014131075 A RU2014131075 A RU 2014131075A RU 2014131075 A RU2014131075 A RU 2014131075A RU 2014131075 A RU2014131075 A RU 2014131075A RU 2014131075 A RU2014131075 A RU 2014131075A
Authority
RU
Russia
Prior art keywords
carbon fiber
carbon fibers
fiber base
canvas
prepreg
Prior art date
Application number
RU2014131075A
Other languages
English (en)
Inventor
Каори НАРИМАЦУ
Нориюки ХИРАНО
Масато ХОНМА
Ацуки ЦУТИЯ
Акихико КИТАНО
Original Assignee
Торэй Индастриз, Инк.
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
Application filed by Торэй Индастриз, Инк. filed Critical Торэй Индастриз, Инк.
Publication of RU2014131075A publication Critical patent/RU2014131075A/ru

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
    • 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
    • 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
    • B32B5/02—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 structural features of a fibrous or filamentary layer
    • B32B5/022—Non-woven fabric
    • 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
    • B32B5/02—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 structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • 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
    • B32B5/02—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 structural features of a fibrous or filamentary layer
    • B32B5/028—Net structure, e.g. spaced apart filaments bonded at the crossing points
    • 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
    • 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
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
    • C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
    • 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
    • C08J5/247—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using fibres of at least two types
    • 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
    • B32B2250/00—Layers arrangement
    • B32B2250/20—All layers being fibrous or filamentary
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/202—Conductive
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558—Impact strength, toughness
    • 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
    • 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
    • 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
    • C08J2363/02—Polyglycidyl ethers of bis-phenols
    • 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
    • C08J2463/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
    • C08J2463/10—Epoxy resins modified by unsaturated compounds
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • 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
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3065—Including strand which is of specific structural definition

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Textile Engineering (AREA)
  • Medicinal Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Health & Medical Sciences (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Inorganic Chemistry (AREA)
  • Reinforced Plastic Materials (AREA)
  • Laminated Bodies (AREA)

Abstract

1. Углеродноволокнистая основа, содержащая слой непрерывных углеродных волокон, формованный из непрерывных углеродных волокон, и холст из коротких углеродных волокон, в котором короткие углеродные волокна, имеющие среднюю длину волокна 2-12 мм, диспергированы в форме монофиламентов, причем холст из коротких углеродных волокон предусмотрен на одной или обеих поверхностях слоя непрерывных углеродных волокон.2. Углеродноволокнистая основа по п. 1, в которой холст из коротких углеродных волокон имеет свойство пружинить обратно.3. Углеродноволокнистая основа по п. 1, в которой холст из коротких углеродных волокон имеет массу на единицу площади 1-10 г/м.4. Углеродноволокнистая основа по п. 1, в которой короткие углеродные волокна в холсте из коротких углеродных волокон имеют средний диаметр волокна 1-20 мкм.5. Препрег, формованный пропиткой части или всей углеродноволокнистой основы по любому из пп. 1-4 матричной смолой.6. Препрег по п. 5, в котором холст из коротких углеродных волокон в формованном продукте, полученном формованием препрега под давлением с нагреванием, имеет толщину 60 мкм или менее.7. Препрег по п. 5, в котором матричной смолой является эпоксидная смола.8. Ламинат углеродноволокнистых основ, формованный ламинированием углеродноволокнистой основы по любому из пп. 1-4 в два или более слоев в направлении толщины.9. Ламинат препрегов, формованный ламинированием препрега по п. 5 в два или более слоев в направлении толщины.10. Композитный материал, армированный углеродным волокном, формованный объединением в одно целое углеродноволокнистой основы по любому из пп. 1-4 с матричной смолой.11. Композитный материал, армированный углеродным волокном, формованный объедине

Claims (11)

1. Углеродноволокнистая основа, содержащая слой непрерывных углеродных волокон, формованный из непрерывных углеродных волокон, и холст из коротких углеродных волокон, в котором короткие углеродные волокна, имеющие среднюю длину волокна 2-12 мм, диспергированы в форме монофиламентов, причем холст из коротких углеродных волокон предусмотрен на одной или обеих поверхностях слоя непрерывных углеродных волокон.
2. Углеродноволокнистая основа по п. 1, в которой холст из коротких углеродных волокон имеет свойство пружинить обратно.
3. Углеродноволокнистая основа по п. 1, в которой холст из коротких углеродных волокон имеет массу на единицу площади 1-10 г/м2.
4. Углеродноволокнистая основа по п. 1, в которой короткие углеродные волокна в холсте из коротких углеродных волокон имеют средний диаметр волокна 1-20 мкм.
5. Препрег, формованный пропиткой части или всей углеродноволокнистой основы по любому из пп. 1-4 матричной смолой.
6. Препрег по п. 5, в котором холст из коротких углеродных волокон в формованном продукте, полученном формованием препрега под давлением с нагреванием, имеет толщину 60 мкм или менее.
7. Препрег по п. 5, в котором матричной смолой является эпоксидная смола.
8. Ламинат углеродноволокнистых основ, формованный ламинированием углеродноволокнистой основы по любому из пп. 1-4 в два или более слоев в направлении толщины.
9. Ламинат препрегов, формованный ламинированием препрега по п. 5 в два или более слоев в направлении толщины.
10. Композитный материал, армированный углеродным волокном, формованный объединением в одно целое углеродноволокнистой основы по любому из пп. 1-4 с матричной смолой.
11. Композитный материал, армированный углеродным волокном, формованный объединением в одно целое ламината углеродноволокнистых основ по п. 8 с матричной смолой.
RU2014131075A 2011-12-26 2012-12-20 Углеродноволокнистая основа, препрег и композитный материал, армированный углеродным волокном RU2014131075A (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2011283400 2011-12-26
JP2011-283400 2011-12-26
PCT/JP2012/082997 WO2013099741A1 (ja) 2011-12-26 2012-12-20 炭素繊維基材、プリプレグおよび炭素繊維強化複合材料

Publications (1)

Publication Number Publication Date
RU2014131075A true RU2014131075A (ru) 2016-02-20

Family

ID=48697230

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014131075A RU2014131075A (ru) 2011-12-26 2012-12-20 Углеродноволокнистая основа, препрег и композитный материал, армированный углеродным волокном

Country Status (11)

Country Link
US (1) US20140322504A1 (ru)
EP (1) EP2799470B1 (ru)
JP (1) JP5967084B2 (ru)
KR (1) KR101959771B1 (ru)
CN (1) CN103987764B (ru)
BR (1) BR112014012796A8 (ru)
CA (1) CA2859007A1 (ru)
ES (1) ES2704634T3 (ru)
RU (1) RU2014131075A (ru)
TW (1) TW201333084A (ru)
WO (1) WO2013099741A1 (ru)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10124605B2 (en) * 2012-10-05 2018-11-13 Livingston Systems, LLC Printer platen material holding apparatus
WO2015122366A1 (ja) 2014-02-14 2015-08-20 帝人株式会社 炭素繊維強化成形材料及び成形体
JP6012653B2 (ja) * 2014-03-10 2016-10-25 三菱電機株式会社 繊維強化プラスチック成形体の製造方法
US10632718B2 (en) * 2014-09-30 2020-04-28 The Boeing Company Filament network for a composite structure
KR20170125879A (ko) * 2015-02-27 2017-11-15 도레이 카부시키가이샤 수지 공급 재료, 프리폼 및 섬유 강화 수지의 제조 방법
CN106595269A (zh) * 2015-10-19 2017-04-26 上海绿特丹保温工程有限公司 一种带式往复双程烘干机
JP6519492B2 (ja) * 2016-01-29 2019-05-29 東レ株式会社 プリプレグおよび繊維強化複合材料
CA3109972C (en) 2016-03-04 2023-12-12 Bauer Hockey Ltd. 3d weaving material and method of 3d weaving for sporting implements
US11471736B2 (en) 2016-03-04 2022-10-18 Bauer Hockey, Llc 3D braiding materials and 3D braiding methods for sporting implements
KR102294301B1 (ko) * 2016-09-28 2021-08-25 코오롱인더스트리 주식회사 오토클레이브를 이용한 골프채 샤프트의 제조방법
KR101942258B1 (ko) 2016-09-29 2019-01-25 (주)엘지하우시스 열가소성 복합재, 열가소성 복합재의 제조방법 및 패널
US10807277B2 (en) * 2016-11-07 2020-10-20 The Boeing Company Resin-infused short fiber composite materials
US20180222145A1 (en) * 2017-02-07 2018-08-09 Kabushiki Kaisha Toshiba Fiber-oriented material and method for manufacturing the same
CN106827711A (zh) * 2017-03-01 2017-06-13 联想(北京)有限公司 电子产品外壳及其制造方法
JP2018171724A (ja) * 2017-03-31 2018-11-08 住友ベークライト株式会社 複合体の製造方法
WO2018199154A1 (ja) * 2017-04-25 2018-11-01 三菱ケミカル株式会社 繊維強化樹脂成形材料及びその製造方法、並びに繊維強化樹脂成形品
WO2018176067A2 (en) * 2017-08-07 2018-09-27 Zoltek Corporation Polyvinyl alcohol-sized fillers for reinforcing plastics
WO2019111416A1 (ja) * 2017-12-08 2019-06-13 日立化成株式会社 プリプレグ、積層板、及びそれらの製造方法、並びにプリント配線板及び半導体パッケージ
CN108189386A (zh) * 2017-12-15 2018-06-22 北京机科国创轻量化科学研究院有限公司 一种纤维增强树脂基复合材料三维打印成形方法
BR112020015869A2 (pt) 2018-03-06 2020-12-08 Toray Industries, Inc. Material de fita seco para colocação de fibra, método de fabricação do mesmo, e corpo laminado de fibra de reforço e de plástico reforçado com fibra produzido com o mesmo
TWI666120B (zh) * 2018-04-03 2019-07-21 厚生股份有限公司 橡膠複合結構及其製造方法
JP6790023B2 (ja) * 2018-05-18 2020-11-25 三菱重工業株式会社 複合材の製造方法および複合材
KR102167055B1 (ko) * 2018-12-19 2020-10-16 재단법인 포항산업과학연구원 탄소 섬유 강화 플라스틱의 제조방법
WO2020137442A1 (ja) * 2018-12-28 2020-07-02 倉敷紡績株式会社 樹脂一体化強化繊維シート及びその製造方法
JP6929424B2 (ja) * 2019-01-17 2021-09-01 株式会社東芝 繊維配向材の製造方法
JP7489335B2 (ja) 2019-02-14 2024-05-23 倉敷紡績株式会社 繊維強化樹脂成形体及びこれに用いる炭素繊維シートの製造方法
US20220289922A1 (en) * 2019-06-20 2022-09-15 Fukuvi Chemical Industry Co., Ltd. Fiber-reinforced epoxy resin composite sheet, fiber-reinforced composite plate and fiber-reinforced molded article, and method for producing same
CN111997781B (zh) * 2020-07-17 2022-02-08 上海复合材料科技有限公司 基于rtm工艺半固化表面的复合材料扩散段成型方法
KR102276413B1 (ko) * 2020-12-22 2021-07-12 주식회사 에디스플레이 탄소섬유 복합수지를 포함하는 모바일 표시장치 브라켓용 수지 조성물 및 이를 이용한 모바일용 표시장치
CN114379167A (zh) * 2022-03-10 2022-04-22 国家纳米科学中心 一种层间改性碳纤维复合材料及其制备方法和应用
CN114643754A (zh) * 2022-03-28 2022-06-21 贵州至当科技有限公司 一种织物增强的cf-smc片材及制备方法
CN114874605B (zh) * 2022-05-09 2024-05-14 上海大学 一种连续碳纤维增强热固性树脂预浸丝及其制备方法和应用
CN115581815B (zh) * 2022-10-12 2023-07-28 江苏君华特种工程塑料制品有限公司 连续碳纤维cf/paek热塑性复合材料股骨接骨板及其制备方法
CN117362061A (zh) * 2023-04-08 2024-01-09 山东晶盾新材料科技有限公司 一种碳化硅晶须横向分布的陶瓷插板的制备方法
CN116462525B (zh) * 2023-06-19 2023-09-05 中国人民解放军国防科技大学 一种连续碳纤维增强超高温陶瓷基复合材料及其制备方法
CN117586040B (zh) * 2023-11-21 2025-02-07 烟台美丰机械集团有限公司 短纤维模压碳/碳刹车盘用预浸料的制备工艺
CN119636120A (zh) * 2024-12-27 2025-03-18 中北大学 基于预制层间增韧结构的抗高速冲击碳纤维/树脂复合材料一体成型精简制备工艺

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53139872A (en) * 1977-05-10 1978-12-06 Toray Industries Porous body comprising metal coated carbon fiber
JPS6044334A (ja) * 1983-08-22 1985-03-09 三菱レイヨン株式会社 補強プリプレグ
JPS61176633A (ja) * 1985-01-31 1986-08-08 Mitsubishi Rayon Co Ltd 複合プリプレグ
JPH07103244B2 (ja) * 1987-09-24 1995-11-08 株式会社クラレ スタンピング成形材料
JPH01250456A (ja) * 1988-03-31 1989-10-05 Agency Of Ind Science & Technol 繊維強化複合材料等のための三次元的多層構造基材
DE69322427T2 (de) * 1992-03-30 1999-10-07 Toray Industries, Inc. Prepreg und Verbundwerkstoffe
JPH05318472A (ja) * 1992-05-22 1993-12-03 Sekisui Chem Co Ltd 繊維強化熱可塑性樹脂シート
JP3387100B2 (ja) 1993-01-14 2003-03-17 東レ株式会社 プリプレグ，その製造方法および積層複合体
JP3179247B2 (ja) 1993-06-07 2001-06-25 三菱レイヨン株式会社 スポーツ関連部材の製造方法
JPH0834864A (ja) 1994-07-22 1996-02-06 Nippon Steel Chem Co Ltd 耐衝撃性プリプレグ
JP3440615B2 (ja) 1995-03-22 2003-08-25 東レ株式会社 プリプレグおよび繊維強化複合材料
JPH10138375A (ja) 1996-11-08 1998-05-26 Toray Ind Inc 繊維強化プラスチック板およびその製造方法
JPH10251973A (ja) * 1997-03-12 1998-09-22 Sanko Techno Kk 構造体補強用のシートモールディングコンパウンドの製造方法
US6265333B1 (en) * 1998-06-02 2001-07-24 Board Of Regents, University Of Nebraska-Lincoln Delamination resistant composites prepared by small diameter fiber reinforcement at ply interfaces
US6995099B1 (en) * 1999-03-23 2006-02-07 Toray Industries, Inc. Composite reinforcing fiber base material, preform and production method for fiber reinforced plastic
EP1314548A1 (en) 2000-08-28 2003-05-28 Sakase Adtech Co., Ltd. Composite material, formed product, and prepreg
JP5011613B2 (ja) 2001-07-06 2012-08-29 東レ株式会社 プリフォームおよび成形方法
JP5153052B2 (ja) * 2004-05-12 2013-02-27 本田技研工業株式会社 繊維強化プラスチックおよび、その製造方法
JP4635674B2 (ja) 2005-03-24 2011-02-23 東レ株式会社 導電性織物およびその製造方法
JP2007268735A (ja) 2006-03-30 2007-10-18 Toho Tenax Co Ltd 炭素繊維シート及びその製造方法
WO2009142291A1 (ja) * 2008-05-22 2009-11-26 東洋紡績株式会社 繊維強化熱可塑性樹脂成形体

Also Published As

Publication number Publication date
KR101959771B1 (ko) 2019-03-19
EP2799470A1 (en) 2014-11-05
KR20140113636A (ko) 2014-09-24
JP5967084B2 (ja) 2016-08-10
CN103987764A (zh) 2014-08-13
WO2013099741A1 (ja) 2013-07-04
EP2799470A4 (en) 2015-08-26
ES2704634T3 (es) 2019-03-19
CN103987764B (zh) 2017-09-15
BR112014012796A2 (pt) 2017-06-13
BR112014012796A8 (pt) 2017-06-20
EP2799470B1 (en) 2018-11-28
CA2859007A1 (en) 2013-07-04
US20140322504A1 (en) 2014-10-30
JPWO2013099741A1 (ja) 2015-05-07
TW201333084A (zh) 2013-08-16

Similar Documents

Publication Publication Date Title
RU2014131075A (ru) Углеродноволокнистая основа, препрег и композитный материал, армированный углеродным волокном
MX2014001657A (es) Refuerzo interlaminar de termoplasticos.
RU2013102590A (ru) Термопластичный препрег, содержащий непрерывные и длинные волокна
GB201008884D0 (en) Improvements in composite materials
RU2012144030A (ru) Способ изготовления ламинатных материалов
JP2013542834A5 (ru)
JP2010538866A5 (ru)
RU2013101800A (ru) Панель, содержащая полимерный композиционный слой и армирующий слой
MX2012014176A (es) Miembro estructural formado a partir de un perfil lineal solido.
RU2018121308A (ru) Гибридная вуаль в качестве промежуточного слоя в композиционных материалах
MX377547B (es) Materiales compuestos de gel segmentados y paneles rigidos manufacturados a partir de los mismos.
DE602008003824D1 (de) Verfahren zur herstellung eines gekrümmten elements aus einem verbundstoff
RU2014138919A (ru) Способ получения изделий из углеродного волокна и изделие, полученное указанным способом
JP2010532720A5 (ru)
RU2012135472A (ru) Панели типа сэндвича
JP2016531026A5 (ru)
WO2009008312A1 (ja) 複合材料
RU2014147687A (ru) Применение операции пробивания при изготовлении композиционного изделия для улучшения поперечной электропроводности композитного изделия
RU2014119786A (ru) Ламинированные ленты с высокими эксплуатационными характеристиками и связанные с ними изделия для применения в области создания бронезащиты
RU2010140221A (ru) Улучшенный полуфабрикат и преформа из композитного материала для изготовления его части
RU2013146846A (ru) Способы улучшения технологических характеристик однонаправленных композитов
MX2015010497A (es) Articulo balistico duro y proceso para fabricar dicho articulo.
WO2015060917A3 (en) Process of producing a thermoplastic-fiber composite and fan blades formed therefrom
RU2014110898A (ru) Прочная мягкая индивидуальная бронезащита
RU2014138061A (ru) Композитный материал для изготовления пуленепробиваемого изделия

Legal Events

Date Code Title Description
FA93 Acknowledgement of application withdrawn (no request for examination)

Effective date: 20151221