CN114670466A - 具有高冲击后压缩强度的层压板及其制备方法 - Google Patents
具有高冲击后压缩强度的层压板及其制备方法 Download PDFInfo
- Publication number
- CN114670466A CN114670466A CN202210412273.1A CN202210412273A CN114670466A CN 114670466 A CN114670466 A CN 114670466A CN 202210412273 A CN202210412273 A CN 202210412273A CN 114670466 A CN114670466 A CN 114670466A
- Authority
- CN
- China
- Prior art keywords
- carbon fiber
- epoxy resin
- fiber prepreg
- curing
- prepreg
- Prior art date
- Legal status (The legal status 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 status listed.)
- Pending
Links
Images
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
- B29C70/28—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
- B29C70/342—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 using isostatic pressure
-
- 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
-
- 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
- B29C70/545—Perforating, cutting or machining during or after moulding
-
- 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
-
- 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
-
- 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
-
- 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
- C08J2423/00—Characterised by the use of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Derivatives of such polymers
- C08J2423/26—Characterised by the use of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Derivatives of such polymers modified by chemical after-treatment
- C08J2423/36—Characterised by the use of homopolymers or copolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond; Derivatives of such polymers modified by chemical after-treatment by reaction with nitrogen-containing compounds, e.g. by nitration
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
- C08K3/18—Oxygen-containing compounds, e.g. metal carbonyls
- C08K3/24—Acids; Salts thereof
- C08K3/26—Carbonates; Bicarbonates
- C08K2003/265—Calcium, strontium or barium carbonate
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K7/00—Use of ingredients characterised by shape
- C08K7/02—Fibres or whiskers
- C08K7/04—Fibres or whiskers inorganic
- C08K7/06—Elements
Abstract
本发明公开了一种具有高冲击后压缩强度的层压板及其制备方法。所述方法将碳纤维增强树脂基复合材料预浸料单向带以[45/0/‑45‑90]ns、n=3或4的铺层顺序铺层,将预浸料坯件和辅助材料进行组合装袋,然后将组合坯件送入热压罐,按树脂体系的固化工艺制备层压板。本发明采用特定的铺层顺序,结合热压罐成型工艺,在不添加其他增强成分的前提下明显提高了CFRP层压板的冲击后压缩性能,为其性能的进一步优化提供了基础。
Description
技术领域
本发明属于先进复合材料技术领域,涉及一种具有高冲击后压缩强度的层压板及其制备方法。
背景技术
碳纤维预浸料是一种制备高性能碳纤维增强复合材料(CFRP)的极为重要的新型中间基材,随着CFRP在航空航天等高新技术领域的应用逐渐广泛,对碳纤维预浸料层压板制备工艺的要求逐渐提高。其中,热压罐成型工艺由于其能在很大范围内适应各种材料对加工工艺条件的要求,受到广泛关注。
CFRP层压板的力学性能直接影响碳纤维预浸料的研制与应用,其中,落锤冲击后层压板的损伤特性以及其压缩性能是复合材料结构损伤容限设计必须考虑的严重情况之一,甚至可以用来对CFRP韧性进行表征。因此CFRP层压板冲击损伤及其冲击后压缩强度(CAI)的试验研究一直是许多研究者关注的中心。文献1对环氧树脂进行改性处理,采用真空辅助树脂传递模塑成型(VARTM)工艺分别制备了[±45/0/90]S、[908]T、[08]T三种铺层角度下的CFRP层合板。与其他铺层角度相比,[±45/0/90]S铺层CFRP有效抑制了冲击裂纹的扩展,其冲击后压缩强度达到124.8MPa(王森,赖佳美,阮金琦等.不同粒子改性环氧树脂基碳纤维复合材料低速冲击及冲击后压缩强度.材料导报,2021,35(2).)。文献2利用浸渍提拉法制备PEK-C膜,通过热压成型制备了层间增韧CFRP层合板,其冲击后压缩强度最佳可达186.67MPa(姚佳伟,刘梦瑶,牛一凡.PEK-C膜层间增韧碳纤维/环氧树脂复合材料的力学性能.复合材料学报,2019,36(5).)。综上所述,现有的CFRP层压板的冲击后压缩强度仍有待进一步提高。
发明内容
本发明的目的是提供一种具有高冲击后压缩强度的层压板及其制备方法。
实现本发明目的的技术方案如下:
具有高冲击后压缩强度的层压板,由碳纤维预浸料单向层组成,铺层顺序为[45/0/-45-90]ns,n=3或4。
本发明中,所述的碳纤维预浸料为本领域常规使用的碳纤维预浸料,例如T800级碳纤维预浸料、T700级碳纤维预浸料等。
本发明所述的具有高冲击后压缩强度的层压板的制备方法,包括以下步骤:
(1)模具准备:用软质材料清理模具,后在模具上涂抹脱模剂;
(2)裁切与铺层:使用预浸料裁切机裁切适当数量的碳纤维预浸料单向带,再以[45/0/-45-90]ns、n=3或4的铺层顺序将预浸料单向带铺层;
(3)组合与装袋:将制件预浸料坯件和辅助材料进行组合并装入真空袋,确保真空袋与周边密封胶条不漏气;
(4)固化与出罐脱模:待复合材料坯件组合装袋完成后,采用热压罐成型工艺,以树脂体系的固化制度进行升温加压固化,固化结束后,保压降温,卸压出罐并脱模,制得具有高冲击后压缩强度的层压板。
本发明的碳纤维预浸料中的树脂体系为常规使用的树脂体系,例如环氧树脂、聚酯、乙烯基酯等。
在本发明具体实施方式中,采用的树脂体系为中温固化环氧树脂体系,按重量份数计由以下成分组成:环氧树脂预聚体混合物45份,热塑性塑料氨基改性乙烯-辛烯共聚物20份,增韧粒子纳米级碳酸钙15份,固化剂二乙氨基丙胺20份和HDG-A/B环氧树脂固化促进剂0.5份,所述的环氧树脂预聚体混合物由双酚A型环氧树脂、双酚F型环氧树脂和海因环氧树脂组成。其热压罐成型工艺为室温抽真空,真空袋内真空为-0.090~-0.098MPa;室温起始加压,以0.02MPa/min速率加压到0.6MPa;再以1.5℃/min,升温至180℃保温保压180min;最后以1.5℃/min,保压降温至60℃以下,卸压出罐。
与现有技术相比,本发明具有以下优点:
本发明采用特定的铺层顺序,结合热压罐成型工艺,制备具有优异的冲击后压缩性能的CFRP层压板。其中,T800级碳纤维预浸料单向带铺层顺序为[45/0/-45/90]3s时,制备的层压板在23℃/50%RH下的冲击后压缩强度可以达到290MPa,在不添加其他增强成分的前提下明显提高了CFRP层压板的冲击后压缩性能,为其性能的进一步优化提供了基础。
附图说明
图1为本发明制备CFRP层压板[45/0/-45-90]3s的铺层顺序示意图。
具体实施方式
为了更清楚地说明本发明的技术方案,下面结合附图和实施例作简单介绍,显而易见地,下面描述的附图和实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以获得其他的技术方案。但任何与本发明等同或相类似的技术方案都属于本发明保护的范围。
下述实施例中,碳纤维预浸料的制备方法如下:
(1)中温固化环氧树脂体系的制备:按重量份数,将环氧树脂预聚体混合物45份,热塑性塑料氨基改性乙烯-辛烯共聚物20份,增韧粒子纳米级碳酸钙15份,固化剂二乙氨基丙胺20份和HDG-A/B环氧树脂促进剂0.5份混合均匀,形成环氧树脂体系;
(2)将制得的中温固化环氧树脂体系涂覆成胶膜,再利用热熔法,与连续碳纤维制成预浸料。
实施例1
用软质材料清理模具,后在模具上涂抹脱模剂。使用预浸料裁切机裁切适当数量的T800级碳纤维预浸料单向带,再以[45/0/-45-90]3s的铺层顺序将预浸料单向带铺层。将制件预浸料坯件和各种辅助材料进行组合并装入真空袋,确保真空袋与周边密封胶条不漏气。待复合材料坯件组合装袋完成后,接好真空管路,锁紧热压罐门,以树脂体系的固化制度进行升温加压固化:室温抽真空,真空袋内真空为-0.090~-0.098MPa;室温起始加压,以0.02MPa/min速率加压到0.6MPa;再以1.5℃/min,升温至180℃保温保压180min。固化结束后,以1.5℃/min,保压降温至60℃以下,卸压出罐并脱模,取出CFRP层压板。将层压板制备成CAI测试用试样,待状态调节后,按ASTM D7136/D7137的标准进行落锤冲击及冲击后压缩性能测试。在23℃/50%RH下的冲击后压缩强度(CAI)为290MPa。CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
实施例2
方法如实施例1,将铺层顺序改为[45/0/-45-90]4s。测试CFRP层压板在23℃/50%RH下的CAI为278MPa。CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
实施例3
方法如实施例1,将T800级碳纤维预浸料改为T700级碳纤维预浸料。测试CFRP层压板在23℃/50%RH下的CAI为187MPa。CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
实施例4
方法如实施例1,将T800级碳纤维预浸料改为T700级碳纤维预浸料,将铺层顺序改为[45/0/-45-90]4s。测试CFRP层压板在23℃/50%RH下的CAI为174MPa。CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
对比例1
方法如实施例1,将铺层顺序改为[45/0/-45-90]2s。测试CFRP层压板在23℃/50%RH下的CAI为226MPa。CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
对比例2
方法如实施例1,将铺层顺序改为[45/0/-45-90]5s。测试CFRP层压板在23℃/50%RH下的CAI为263MPa。将CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
对比例3
方法如实施例1,将T800级碳纤维预浸料改为T700级碳纤维预浸料,将铺层顺序改为[45/0/-45-90]2s。测试CFRP层压板在23℃/50%RH下的CAI为156MPa。CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
对比例4
方法如实施例1,将T800级碳纤维预浸料改为T700级碳纤维预浸料,将铺层顺序改为[45/0/-45-90]5s。测试CFRP层压板在23℃/50%RH下的CAI为168MPa。CFRP层压板的铺层顺序,样板厚度及CAI列于表1中。
表1各实施例和对比例的CFRP层压板的铺层顺序,样板厚度及CAI
铺层顺序 | 样板厚度/mm | CAI/MPa | |
实施例1 | [45/0/-45-90]<sub>3s</sub> | 4.488 | 290 |
实施例2 | [45/0/-45-90]<sub>4s</sub> | 5.984 | 278 |
实施例3 | [45/0/-45-90]<sub>3s</sub> | 4.473 | 187 |
实施例4 | [45/0/-45-90]<sub>4s</sub> | 5.969 | 174 |
对比例1 | [45/0/-45-90]<sub>2s</sub> | 2.992 | 226 |
对比例2 | [45/0/-45-90]<sub>5s</sub> | 7.480 | 263 |
对比例3 | [45/0/-45-90]<sub>2s</sub> | 2.977 | 156 |
对比例4 | [45/0/-45-90]<sub>5s</sub> | 7.465 | 168 |
从表1可以看出,对于同一碳纤维预浸料,采用[45/0/-45-90]3s和[45/0/-45-90]4s的铺层顺序制备的CFRP层压板相较于[45/0/-45-90]2s和[45/0/-45-90]5s的铺层顺序制备的CFRP层压板,具有更高的CAI。其中T800级碳纤维预浸料以[45/0/-45-90]2s铺层顺序制备的CFRP层压板具有最高的CAI,可达290MPa。比较分别以T800级碳纤维预浸料和T700级碳纤维预浸料为原料的实施例和对比例可知,T700级碳纤维预浸料层压板的CAI均低于同等制备工艺下制得的T800级碳纤维预浸料层压板。
Claims (6)
1.具有高冲击后压缩强度的层压板,其特征在于,由碳纤维预浸料单向层组成,铺层顺序为[45/0/-45-90]ns,n=3或4。
2.根据权利要求1所述的层压板,其特征在于,所述的碳纤维预浸料为本T800级碳纤维预浸料或T700级碳纤维预浸料。
3.根据权利要求1或2所述的层压板的制备方法,其特征在于,包括以下步骤:
(1)模具准备:用软质材料清理模具,后在模具上涂抹脱模剂;
(2)裁切与铺层:使用预浸料裁切机裁切适当数量的碳纤维预浸料单向带,再以[45/0/-45-90]ns、n=3或4的铺层顺序将预浸料单向带铺层;
(3)组合与装袋:将制件预浸料坯件和辅助材料进行组合并装入真空袋,确保真空袋与周边密封胶条不漏气;
(4)固化与出罐脱模:待复合材料坯件组合装袋完成后,采用热压罐成型工艺,以树脂体系的固化制度进行升温加压固化,固化结束后,保压降温,卸压出罐并脱模,制得具有高冲击后压缩强度的层压板。
4.根据权利要求3所述的制备方法,其特征在于,碳纤维预浸料中的树脂体系环氧树脂体系、聚酯体系或乙烯基酯体系。
5.根据权利要求3所述的制备方法,其特征在于,碳纤维预浸料中的树脂体系为中温固化环氧树脂体系,按重量份数计由以下成分组成:环氧树脂预聚体混合物45份,热塑性塑料氨基改性乙烯-辛烯共聚物20份,增韧粒子纳米级碳酸钙15份,固化剂二乙氨基丙胺20份和HDG-A/B环氧树脂固化促进剂0.5份,所述的环氧树脂预聚体混合物由双酚A型环氧树脂、双酚F型环氧树脂和海因环氧树脂组成。
6.根据权利要求5所述的制备方法,其特征在于,热压罐成型工艺具体为:室温抽真空,真空袋内真空为-0.090~-0.098MPa;室温起始加压,以0.02MPa/min速率加压到0.6MPa;再以1.5℃/min,升温至180℃保温保压180min;最后以1.5℃/min,保压降温至60℃以下,卸压出罐。
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210412273.1A CN114670466A (zh) | 2022-04-19 | 2022-04-19 | 具有高冲击后压缩强度的层压板及其制备方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210412273.1A CN114670466A (zh) | 2022-04-19 | 2022-04-19 | 具有高冲击后压缩强度的层压板及其制备方法 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN114670466A true CN114670466A (zh) | 2022-06-28 |
Family
ID=82078805
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210412273.1A Pending CN114670466A (zh) | 2022-04-19 | 2022-04-19 | 具有高冲击后压缩强度的层压板及其制备方法 |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114670466A (zh) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116001309A (zh) * | 2022-12-16 | 2023-04-25 | 江苏君华特种工程塑料制品有限公司 | 单向连续纤维增强热塑性树脂基复合材料制品的成型方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101503014A (zh) * | 2009-03-27 | 2009-08-12 | 中国航空工业第一集团公司北京航空材料研究院 | 一种表面显示内部损伤的复合材料层压板 |
CN106553355A (zh) * | 2015-09-25 | 2017-04-05 | 北京百慕航材高科技股份有限公司 | 一种碳纤维复合材料假脚成型工艺 |
US20190283279A1 (en) * | 2018-02-09 | 2019-09-19 | Ai-Carbon Co., Ltd. | Methods for manufacturing carbon fiber and for manufacturing carbon fiber reinforced resin composition |
CN112679908A (zh) * | 2019-10-17 | 2021-04-20 | 中国石油化工股份有限公司 | 一种预浸料增韧材料、高韧性预浸料及其制备方法 |
CN113059828A (zh) * | 2021-04-21 | 2021-07-02 | 南京聚隆科技股份有限公司 | 一种耐高温碳纤维复合材料筒体承力层及其制备工艺 |
-
2022
- 2022-04-19 CN CN202210412273.1A patent/CN114670466A/zh active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101503014A (zh) * | 2009-03-27 | 2009-08-12 | 中国航空工业第一集团公司北京航空材料研究院 | 一种表面显示内部损伤的复合材料层压板 |
CN106553355A (zh) * | 2015-09-25 | 2017-04-05 | 北京百慕航材高科技股份有限公司 | 一种碳纤维复合材料假脚成型工艺 |
US20190283279A1 (en) * | 2018-02-09 | 2019-09-19 | Ai-Carbon Co., Ltd. | Methods for manufacturing carbon fiber and for manufacturing carbon fiber reinforced resin composition |
CN112679908A (zh) * | 2019-10-17 | 2021-04-20 | 中国石油化工股份有限公司 | 一种预浸料增韧材料、高韧性预浸料及其制备方法 |
CN113059828A (zh) * | 2021-04-21 | 2021-07-02 | 南京聚隆科技股份有限公司 | 一种耐高温碳纤维复合材料筒体承力层及其制备工艺 |
Non-Patent Citations (2)
Title |
---|
孔德拴: "《非热压罐预浸料T700SC/#2510层板的低速冲击损伤特性》", 《玻璃钢/复合材料》 * |
杨旭: "《低速冲击下复合材料层板压缩许用值》", 《复合材料学报》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116001309A (zh) * | 2022-12-16 | 2023-04-25 | 江苏君华特种工程塑料制品有限公司 | 单向连续纤维增强热塑性树脂基复合材料制品的成型方法 |
CN116001309B (zh) * | 2022-12-16 | 2023-09-08 | 江苏君华特种工程塑料制品有限公司 | 单向连续纤维增强热塑性树脂基复合材料制品的成型方法 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN107215039B (zh) | 一种夹芯复合材料及其制备方法 | |
AU761069B2 (en) | Moulding materials | |
CN111187438A (zh) | 一种真空袋成型工艺用碳纤维/增韧环氧树脂预浸料的制备方法 | |
US7887916B2 (en) | Process for producing sandwich structure and adhesive film used therefor | |
CN103963319A (zh) | 一种复合材料加筋壁板的预浸料/树脂膜熔渗共固化成型方法 | |
CN105082569A (zh) | 一种提高复合材料层压板压缩性能的工艺 | |
CN111648027A (zh) | 一种基于超薄纤维预浸料的高性能碳纤维层合板及其制备方法 | |
CN112265347A (zh) | 一种结构承载-烧蚀防热一体化复合材料及其制备方法 | |
EP2091709A2 (en) | Foamed tools | |
CN114670466A (zh) | 具有高冲击后压缩强度的层压板及其制备方法 | |
CN114030268B (zh) | 具备高强胶接性能的蜂窝夹层结构复合材料的制备方法 | |
CN106218146A (zh) | 一种箱包用柔性材料增韧的复合材料及其制备和应用 | |
CN106785415A (zh) | 含立体辐射体树脂基复合材料天线罩及其成型方法 | |
CN207128360U (zh) | 一种夹芯复合材料 | |
CN108384188B (zh) | 一种基于工程塑料非织造布的预浸料及其应用 | |
CN111087757A (zh) | 耐高温高韧性预浸料及其制备方法和应用 | |
CN114163670B (zh) | 一种节能环保环氧乙烯基酯树脂预浸料及其制备方法和固化方法 | |
CN111349311A (zh) | 一种粉末状环氧树脂组合物、预浸料及其复合材料板 | |
CN115011071A (zh) | Smc复合材料及其制备方法 | |
CN112677602B (zh) | 一种用于预浸料的增韧材料、高韧性复合材料及其制备方法 | |
CN112409618A (zh) | 一种单向热固性芳纶纤维复合材料及制备方法 | |
CN209600012U (zh) | 一种易于热成型的轻质高抗冲高模量多层复合板材 | |
CN114932693B (zh) | 高开孔拉伸强度的碳纤维复合材料层压板的制备方法 | |
CN114044922B (zh) | 纳米合金热塑粒子、纳米合金膜及其制备方法和应用 | |
CN109263089A (zh) | 一种通过纤维增强树脂拉挤工艺制备夹芯型材的方法及所得型材 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |