CN104411871B - 拆散碳纤维丝束及模塑包含该类纤维的组合物的方法 - Google Patents

拆散碳纤维丝束及模塑包含该类纤维的组合物的方法 Download PDF

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CN104411871B
CN104411871B CN201380035292.6A CN201380035292A CN104411871B CN 104411871 B CN104411871 B CN 104411871B CN 201380035292 A CN201380035292 A CN 201380035292A CN 104411871 B CN104411871 B CN 104411871B
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roller bearing
carbon fibre
carbon fiber
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CN104411871A (zh
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普罗比尔·库马尔·古哈
迈克尔·J·西瓦耶克
迈克尔·约瑟夫·希尔图宁
沙恩·什科普
克里斯托弗·希尔图宁
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Kang Tingnan Opens Up Structural Plastic Co Ltd
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    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02JFINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
    • D02J1/00Modifying the structure or properties resulting from a particular structure; Modifying, retaining, or restoring the physical form or cross-sectional shape, e.g. by use of dies or squeeze rollers
    • D02J1/18Separating or spreading
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B15/00Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
    • B29B15/08Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B17/00Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B17/00Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/06Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
    • B32B17/067Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of fibres or filaments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/22Layered 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
    • B32B5/24Layered 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
    • B32B5/26Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/04Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B9/047Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H51/00Forwarding filamentary material
    • B65H51/005Separating a bundle of forwarding filamentary materials into a plurality of groups
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04Reinforcing macromolecular compounds with loose or coherent fibrous material
    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01GPRELIMINARY TREATMENT OF FIBRES, e.g. FOR SPINNING
    • D01G1/00Severing continuous filaments or long fibres, e.g. stapling
    • D01G1/02Severing continuous filaments or long fibres, e.g. stapling to form staple fibres not delivered in strand form
    • D01G1/04Severing continuous filaments or long fibres, e.g. stapling to form staple fibres not delivered in strand form by cutting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00Use of elements other than metals as reinforcement
    • B29K2307/04Carbon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/022 layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/101Glass fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/106Carbon fibres, e.g. graphite fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00Handled material; Storage means
    • B65H2701/30Handled filamentary material
    • B65H2701/31Textiles threads or artificial strands of filaments
    • B65H2701/314Carbon fibres
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2300/00Characterised by the use of unspecified polymers
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49801Shaping fiber or fibered material
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • Y10T428/2495Thickness [relative or absolute]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
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    • Y10T83/04Processes
    • Y10T83/0405With preparatory or simultaneous ancillary treatment of work
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    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/04Processes
    • Y10T83/0405With preparatory or simultaneous ancillary treatment of work
    • Y10T83/041By heating or cooling
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
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Abstract

提供一种用于将碳纤维丝束拆散为适合在模塑组合物的配方中使用的分散的短切碳纤维的方法。碳纤维丝束被送入具有流体流动开口的模具,通过它一种流体撞击丝束的一侧来扩大丝束横截面区域。被扩大横截面区域的丝束从模具延伸到一个常规的纤维切断装置的路径来形成短切碳纤维,或者通过机械拆散器的接触式尖齿(contacting tines)。通过流体流动开口相对于纤维丝束通过的模具孔洞的相对位置的调整,在此结合撞击丝束的流体的性质、孔洞的形状,获得一种改进的短切碳纤维分散。然后,获得的短切碳纤维可以用来在配方固化之前根据模塑组合物的配方分散。

Description

拆散碳纤维丝束及模塑包含该类纤维的组合物的方法
与之相关的专利申请
该申请主张2012年5月1日递交的序列号为61/641,136的美国临时申请的优先权,据此,其内容通过引用的方式并入。
技术领域
本发明通常涉及一种用于拆散碳纤维丝束的方法,以及特别地涉及一种用于产生服从于内含物模塑组合物的(amenable to inclusion molding compositions)短切的及分散的碳纤维的方法。
背景技术
使用纤维内含物来增强基质是公知的现有技术。用于增强的完善机制包括通过基质减缓和延伸裂纹扩展的路径,和与从周围的基质材料中牵拉出一纤维有关的能量分布。在片状模塑组合物(SMC)配方和团状模塑组合物(BMC)配方,以下被统称为“模塑组合物”的情况下,传统地,纤维增强已经涉及短切玻璃纤维的使用。在模塑组合物领域中用碳纤维替换模塑组合物中的部分或全部的玻璃纤维的认知日益增加。但是,由于玻璃和碳纤维之间的区别,该效果仅获得有限的成功。特别地,这些区别包括纤维直径,用于模塑组合物的玻璃纤维通常具有16和30微米之间的直径,然而碳纤维通常具有2和10微米之间的直径。另外,玻璃粗纱纤维织物,或丝束通常具有数十到数百个单独的纤维,然而碳纤维丝束通常来自数千丝束和甚至数万独立纤维。更进一步的区别存在于纤维-纤维的相互作用(fiber-fiber interactions),其中玻璃纤维倾向于散射和基于切断的拆散,范德华力(Van derwaals bonding)和其他的纤维间(interfiber)表面相互作用力倾向于使碳纤维丝束无法在被切成作为一模塑组合物中的加固的所需长度后拆散。尽管碳纤维束的拆散是根据实验室规模模塑通过手工操作解决的,碳纤维丝束拆散为单独的短切碳纤维的生产规模存在问题。
因此,存在一种通过连续方式将碳纤维丝束拆散为单独的短切碳纤维的方法的需求。进一步地,存在一种促进碳纤维和模塑组合物组分之间的相互作用,以提高所得到的SMC或BMC的强度的需求。
发明内容
提供一种用于将共同形成一丝束的大量碳纤维拆散为适合在模塑组合物的配方中使用的分散的短切碳纤维的改进设备和方法。根据本发明的一个实施方式,碳纤维丝束被送入具有流体流动开口的模具,通过它一种流体撞击丝束的一侧来扩大丝束横截面区域。被扩大横截面区域的丝束从模具延伸到常规的纤维切断装置的路径来形成短切碳纤维。通过流体流动开口相对于纤维丝束通过的模具孔洞的相对位置的调整,在此结合撞击丝束的流体的性质、孔洞的形状,获得一种相比现有方法改进的短切碳纤维分散。然后,在某些具体实施中,根据本发明获得的短切碳纤维可以用来在配方固化之前根据模塑组合物的配方分散。通过模塑组合物的单体极性的控制,还得到短切碳纤维的进一步分散和有向性。
一个机械拆散器(mechanical debundler)容纳丝束状材料,例如碳纤维丝束,输入进一介于两个具有尖齿的对立滚轴之间的顶层输送区域,其中,第一滚轴顺时针旋转并且第二滚轴逆时针旋转,以便于将内部的丝束牵拉向一旋转快于所述的上两个滚轴的下尖齿滚轴,随着丝束通过,它被牵拉开并且扭折(pulled open and kinked),来将丝束在高度上扩大至大约5倍。在实施方式中,机械拆散器(mechanical debundler)也可以与高温、吹气或等离子体同时使用。在使用等离子的实施方式中,对尖齿进行充电以在丝束被拉开的区域中生成等离子体。
在本发明的另一个实施方式中,一个常规的短切纤维丝束根据一个含有模塑组合物的极性单体分散。
附图说明
在本说明书的结论声明中特别指出和明确声明的主题被认为是本发明的主题。本发明的前述和其它目标、特征及优势在下列结合附图的详细描述中是显而易见的,其中:
图1A为一个根据本发明有效拆散碳纤维丝束的模具的横截面示意图;
图1B为一个在图1A中所示的模具的纵向截面示意图;和
图2为一个在本发明中有效用于拆散碳纤维丝束的模具的第二种实施方式。
图3说明了一个根据本发明的一个实施方式的机械拆散器(mechanicaldebundler)。
具体实施方式
本发明具有将共同形成一丝束的大量碳纤维拆散为适合在模塑组合物的配方中使用的分散的短切碳纤维的实用性。根据本发明,碳纤维丝束被送入具有流体流动开口的模具,通过它一种流体撞击丝束的一侧来扩大丝束横截面区域。被扩大横截面区域的丝束从模具延伸到常规的纤维切断装置的路径来形成短切碳纤维。通过流体流动开口相对于纤维丝束通过的模具孔洞的相对位置的调整,在此结合在丝束上撞击的流体的性质、孔洞的形状,获得一种相比现有方法改进的短切碳纤维分散。然后,在某些具体实施方式中,根据本发明获得的短切碳纤维可以用来在配方固化之前根据模塑组合物的配方分散。通过模塑组合物的单体极性的控制,得到短切碳纤维的进一步分散和有向性。
在本发明的另一个实施方式中,一个常规的短切纤维丝束根据一个含有模塑组合物的极性单体分散。
现在参阅图1A和1B,一个本发明的模具通常按10所示。该模具10具有一个孔洞12,其尺寸上大于通过于此的碳纤维丝束T的横截面区域。至少两个流体流动开口14,16和18如图1A和1B所示,用于允许流体流入孔洞12并且在碳纤维丝束T的一侧上。孔洞12被示出具有一个三角形的横截面。理应领会,本发明的模具的孔洞具有其他横截面形状,例如圆形、椭圆形、沙漏形和其他多边形横截面形状。流体开口14,16和18允许流体注入孔洞12中,以便于撞击碳纤维丝束T的一侧并诱导拆散,以便于增加丝束T的横截面区域。根据本发明,提供至少两个流体开口。理应领会流体流入仅需要通过流体开口存在,因为流体能够从靠近一个纤维切断装置A的端子模具表面20离开模具10。通过控制丝束T的输送速度和切碎机A的运行速度,获得一长度可控的拆散的短切纤维C。
作为流体冲击,流体开口14,16和18每个分别以一角度与孔洞12相交,阿尔法(α),贝它(β)和伽马(γ)。每一个角度都是独立变量。在具体实施方式中,角度阿尔法,贝它和伽马每个独立地为30和150度之间,虽然理应领会在此其他角度是可行的。
不打算与一个特定的理论绑定,据信流体进入孔洞12在如流体渗透到丝束T的情况下在由此产生的被扩大的丝束横截面区域中产生一个较大的空隙容积。流体进入孔洞12作为一膨胀流体倾向于沿着阻力最小的路径,较佳地建立有利于流体渗透通过丝束T的条件,从而在流体通过一个与流体单独进入的开口相比较低压力的流体流动开口流出前增加丝束T的横截面,或者结合通过端子模具表面20的离开。最佳如图1B所示,理应领会流体流动开口不需要都存在于一个单平面,其中,流体流动出口18在开口12和16的下游,相对于丝束T的运动。
本发明的模具的另一个实施方式通常按图2中的30显示,具有圆形孔洞12’和流体开口14’和16’;
如本文所用,术语“流体”意在包括气体、液体和气溶胶雾化液体。在本文中可操作的用于拆散碳纤维丝束的流体示例性地包括空气、氮气、惰性气体、二氧化碳、一氧化碳和蒸汽。理应领会有机分子和硅烷,上述各自分别的沸腾温度在本文中也是可操作的,作为气态流体用于拆散碳纤维丝。适用于拆散碳纤维丝束的液态流体示例性地包括具有大于0.5的相对极性的高极性液体。除了简单的流体,根据本发明,流体还带有一个添加剂,例如,微粒,基团,偶联剂,及其组合物。适用于在一撞击碳纤维束的流体夹带的微粒示例性地包括炭黑,碳酸钙,胶态二氧化硅,二氧化钛,及其组合物。本文中可操作的偶联剂示例性地包括环氧树脂,有机钛酸盐,有机锆酸盐,羟基甲基间苯二酚,及其组合物。基团可作为添加剂;尤其气态流体,示例性地包括臭氧,单态氧,和等离子体。理应领会因素控制很容易实现,例如孔洞的横截面积区域,孔洞的形状,流体的进气压力,以及流体出口的相对位置影响碳纤维丝束拆散的程度,通过切断装置A切断丝束之后用以生产分散的碳纤维丝束。
如图2所示,其中相似的数字对应于归结于另外相关的图1A和1B的含义,提供另一个模具作为本发明的方法的一部分。不打算与一个特定的理论绑定,在本发明的实施方式中,为了成功拆散,在限制碳纤维丝束扭曲的情况下,如图2所示同时从两个流体流动开口撞击碳纤维丝束是合适的。
图3说明一个本发明的机械拆散器(mechanical debundler)40,容纳丝束状材料,例如碳纤维丝束,作为输入进入一介于两个具有齿尖48的对立滚轴之间的顶层输送区域,其中,第一滚轴42顺时针旋转并且第二滚轴44逆时针旋转,以便于将内部的丝束牵拉向一旋转快于上两个滚轴(42,44)的下尖齿滚轴46,随着丝束通过,它被牵拉开并且扭折(pulled open and kinked),来将丝束在高度上扩大至大约5倍。在实施方式中,机械拆散器(mechanical debundler)也可以与高温、吹气或等离子体同时使用来分开丝束。在某些具体实施方式中,施加高温足以去除在碳纤维的表面上的任何涂料或其它常规表面涂层。在其它实施方式中,在隔绝或者还原性气氛下施加高温,从核心碳纤维促进涂料热解。在接合第二滚轴44之前,期间或之后,等离子体很容易通过常规的等离子发生器源生成来处理纤维丝束。在使用等离子体的实施方式中,对尖齿充电以在丝束正被开放拉毛的区域中生成等离子体。理应领会丝束与机械拆散器(mechanical debundler)连接,配合空气拆散或作为一个独立的方法。
本发明的方法,碳纤维丝束通过模具,伴随丝束一侧受到流体的冲击以及贯穿碳纤维丝束,以便于增加横截面区域,或者通过机械拆散器(mechanical debundler)被输送后,丝束然后切成碳纤维束的预选长度。然后,由此产生的丝束按SMC,BMC或RTM配方分散,用于后续成型和固化。人们已经发现,当模塑组合物具有较强极性,该种短切纤维丝束趋向于分散并实现纤维拆散和有向性两者的更大程度。在本发明的具体实施方式中,这样产生的短切碳纤维根据甲基丙烯酸甲酯单体分散。用于模塑组合物配方生产的其它合适的单体示例性地包括不饱和聚酯树脂、环氧树脂及其组合物。基于环氧树脂的模塑组合物配方示例性地包括基于双酚A和酚醛的封端环氧树脂(bis-phenol-A and Novolac based epoxyterminated resins)。合适用于如基于环氧树脂的模塑组合物配方的固化剂示例性地包括酸酐类,例如偏苯三酸酐,甲基四氢邻苯二甲酸酐(MTHPA),纳迪克甲基酸酐(NMA),二-和三-官能胺(di-and tri-functional amines),及其组合物。
本发明的另一个实施方式中,包括根据模塑组合物单体或者包含相对极性大于0.26并在某些具体实施方式中大于0.5,但是在其他具体实施方式中介于0.5和0.8之间的单体的溶液分散常规的短切和捆绑的碳丝束。相对极性的定义按照克里斯·蒂赖卡特,溶剂以及在有机化学中的溶剂反应,威利-VCH,第3版,2003(Christian Recihardt,Solventsand Solvent Effects in Organic Chemistry,Wiley-VCH,3rd edition,2003)。
根据本发明的方法生产的短切碳纤维丝束很容易先于固化在模塑组合物配方中分散,用于代替或者结合玻璃纤维。作为根据一个本发明的方法拆散碳纤维丝束的结果,形成一个加强的SMC,BMC或者树脂传递模塑(RTM)固化制品,具有较低的密度整体,和按重量较低百分比负荷的纤维。此外,通过使用偶联剂得到优异的拉伸性能。另外,值得注意的是,本发明的方法作为用于制造短切碳纤维的连续方法适合于结合生产规模制造使用。
由此产生的短切和拆散的碳纤维找到特殊的效用,在一个具备内部的SMC中,其内部包括按重量从10至40%的碳纤维,和基于市售的包含玻璃纤维的TCA(大陆结构塑料公司,Continental Structural Plastics)的SMC表皮,TCA部分包含按重量介于10和60%之间的玻璃纤维,正如在美国专利7,655,297中的实施例。内部和表皮的厚度比例范围为1:1~10:1。将此产生的SMC内部和表皮层单独地固化并结合,或者彼此接触固化。该具有包含碳纤维的内部的SMC双层被指出具有一个比完全来自TCA形成的可比较的制品低10,20,30甚至40%的密度。以这种方式形成轻质制品,保留了与TCA相关的甲类表面的高表面玻璃。
本说明书中提及的专利文献和出版物表明本领域技术人员的层次,即本发明所属的层次。这些文献和出版物都通过引用的方式并入本文,其程度如同每个单独的文献或出版物被具体和单独地通过引用的方式并入本文。
上述描述是本发明的特定的具体实施例的说明,但是此处并不意味着在实施中的限制。以下的权利要求,包括其中的所有等同物,意在限定本发明的范围。

Claims (36)

1.一种用于将碳纤维丝束拆散为短切碳纤维的方法,包括:
将由一束横截面区域和一丝束表面限定的碳纤维丝束输送进一个具有一孔洞的模具,所述的模具具有至少两个流体流动开口,所述的孔洞大小大于所述的束横截面区域;
通过所述的至少两个流体流动开口中的一个第一开口用一流速的流体撞击所述的碳纤维丝束,来将碳纤维丝束扩大至一个比在所述的孔洞内的所述的束横截面区域更大的被扩大的横截面区域;
在离开所述的模具时切断所述的被扩大横截面区域的碳纤维丝束,来形成短切碳纤维。
2.根据权利要求1所述的方法,其特征在于,所述的碳纤维丝束中具有至少1000根单独的碳纤维。
3.根据权利要求1所述的方法,其特征在于,所述的碳纤维丝束中具有至少10000根单独的碳纤维。
4.根据权利要求1所述的方法,其特征在于,切断发生于靠近所述的模具的一端面。
5.根据权利要求1所述的方法,其特征在于,所述的孔洞为一三角形,圆形,椭圆形,沙漏形,或其他多边形的横截面形状。
6.根据权利要求1所述的方法,其特征在于,沿孔洞的长度在侧向开设至少两个流体流动开口。
7.根据权利要求1所述的方法,其特征在于,所述的流体流动开口中至少一个限定一个流体排放口。
8.根据权利要求1所述的方法,其特征在于,所述的流体为空气。
9.根据权利要求1所述的方法,其特征在于,所述的流体是气态的,并进一步包括微粒状物质。
10.根据权利要求9所述的方法,其特征在于,所述的微粒状物质为炭黑、碳酸钙、二氧化硅或二氧化钛中的至少一种。
11.根据权利要求1所述的方法,其特征在于,所述的流体是气态的,并进一步包括自由基。
12.根据权利要求11所述的方法,其特征在于,所述的自由基包括单线态氧或等离子体。
13.根据权利要求1所述的方法,其特征在于,所述的流体是气态的,并进一步包括一偶联剂。
14.根据权利要求13所述的方法,其特征在于,所述的偶联剂为环氧树脂、钛酸或锆酸盐中的至少一种。
15.根据权利要求1所述的方法,进一步包括根据模塑组合物预聚物配方分散短切碳纤维。
16.根据权利要求15所述的方法,其特征在于,所述的模塑组合物预聚物包括极性单体。
17.根据权利要求16所述的方法,其特征在于,所述的极性单体包括除去纤维和填料的所述的模塑组合物重量的绝大部分。
18.根据权利要求16所述的方法,其特征在于,所述的极性单体为甲基丙烯酸甲酯。
19.一种用于将碳纤维丝束拆散为短切碳纤维的方法,包括:
将所述的碳纤维丝束切成短切丝束,并将所述的短切丝束根据一个单体、或者根据一个包含一具有大于0.25的相对极性的上述单体的模塑组合物分散。
20.根据权利要求19所述的方法,其特征在于,所述的相对极性大于0.5。
21.根据权利要求19所述的方法,其特征在于,所述的相对极性介于0.5和0.8之间。
22.根据权利要求1至21中任一项所述的方法,进一步包括连接所述的丝束与多个旋转尖齿。
23.根据权利要求1所述的方法,进一步包括连接所述的丝束与多个旋转尖齿,同时将所述的丝束暴露于高温或等离子体中的至少一个。
24.根据权利要求23所述的方法,其特征在于,在隔绝或者还原气氛下施加高温。
25.一制品,其特征在于,包括:
一第一片状模塑组合物的一固化内部,通过短切碳纤维进行显著地强化;和
一第二片状模塑组合物的一固化表皮,通过玻璃纤维进行显著地强化。
26.根据权利要求25所述的制品,其特征在于,所述的固化内部实质上缺少玻璃纤维。
27.根据权利要求25所述的制品,或其特征在于,所述的表皮具有汽车表面质量油剂。
28.根据权利要求27所述的制品,其特征在于,所述的表皮实质上缺少短切碳纤维。
29.根据权利要求27所述的制品,其特征在于,所述的表皮具有甲类油剂。
30.根据权利要求25所述的制品,其特征在于,所述的内部具有一内层厚度并且所述的表皮具有一表皮厚度,并且所述的内层厚度与表皮厚度的比例介于1:1~10:1之间。
31.一种用于将碳纤维丝束拆散为短切碳纤维的方法,其特征在于,包括:
将由一束横截面区域和一丝束表面限定的碳纤维丝束输送进一机械拆散器(mechanical debundler),包括:一输送区域,容纳所述的丝束,介于两个具有尖齿的对立滚轴之间,其中,所述的两个对立滚轴中的一个第一滚轴顺时针旋转,并且所述的两个对立滚轴中的一个第二滚轴逆时针旋转,以便于将所述的输送区域内部的丝束牵拉向一旋转快于所述的两个对立滚轴的下尖齿滚轴;
将所述的丝束在放样室内(loft)扩大至大约5倍。
32.根据权利要求31所述的方法,进一步包括在离开具有模具的所述的机械拆散器时切断所述的被扩大横截面区域的碳纤维丝束,来形成短切碳纤维。
33.根据权利要求31所述的方法,进一步包括在介于所述的下尖齿滚轴和所述的上两个滚轴之间的一区域中对所述的丝束施加吹气、高温或等离子体中的至少一种。
34.一机械拆散器包括:
一顶部输送区域,容纳丝束材料,介于两个具有尖齿的对立滚轴之间,其中,所述的两个对立滚轴中的一个第一滚轴顺时针旋转,并且所述的两个对立滚轴中的一个第二滚轴逆时针旋转,以便于将所述的顶部输送区域内部的丝束牵拉向一旋转快于所述的两个对立滚轴的下尖齿滚轴;和
一等离子体发生器,形成一靠近所述的两个对立滚轴中的一个或者所述的下尖齿滚轴的等离子体。
35.根据权利要求34所述的拆散器,其中,对所述的尖齿充电生成所述的等离子体。
36.根据权利要求34所述的拆散器,其中,所述的丝束材料为碳纤维丝束。
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Publication number Priority date Publication date Assignee Title
WO2015084956A1 (en) 2013-12-03 2015-06-11 Continental Structural Plastics, Inc. In-line plasma source for introducing pieces of spread carbon fiber tow into molding compositions on a compounding production line
US9815224B2 (en) * 2015-03-30 2017-11-14 Ut-Battelle, Llc Carbon fiber reinforcements for sheet molding composites
EP3408434A4 (en) 2016-01-26 2019-11-13 Continental Structural Plastics, Inc. METHOD AND SYSTEM FOR DISMANTLING FIBER CUTTER FOR USE IN PREFORM MATS, AND MOLDING COMPOSITIONS CONTAINING SUCH FIBERS
US11072093B2 (en) 2016-06-03 2021-07-27 Magna Exteriors Inc. Method to uniformly debundle and evenly distribute high fiber count carbon tow
CN108368646A (zh) * 2016-08-25 2018-08-03 仓敷纺绩株式会社 碳纤维开纤片材的制造方法
US10570536B1 (en) 2016-11-14 2020-02-25 CFA Mills, Inc. Filament count reduction for carbon fiber tow
JP7164523B2 (ja) 2016-11-30 2022-11-01 テイジン オートモーティブ テクノロジーズ, インコーポレイテッド 構造適用のためのブレンドされた繊維マット形成
WO2018102529A1 (en) * 2016-11-30 2018-06-07 Continental Structural Plastics, Inc. Fiber mat formation for structural applications
WO2018102347A1 (en) * 2016-11-30 2018-06-07 Continental Structural Plastics, Inc. Dispersed fiber mat formation
US10864686B2 (en) * 2017-09-25 2020-12-15 Apple Inc. Continuous carbon fiber winding for thin structural ribs

Family Cites Families (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3795944A (en) * 1971-12-08 1974-03-12 Philco Ford Corp Pneumatic spreading of filaments
GB1454394A (en) * 1973-02-22 1976-11-03 Nat Res Dev Heating panels
JPS5648256A (en) 1979-09-28 1981-05-01 Toho Beslon Co Method of changing carbon fiber into ultrashort fiber
US4476807A (en) * 1983-02-18 1984-10-16 R. J. Reynolds Tobacco Company Apparatus for application of additives to cigarette filter tow
JPS61157335A (ja) * 1984-12-28 1986-07-17 Irie Hekizai:Kk カ−ボン短繊維を単繊維状に分散混合した乾状態の微粉体原材料製造装置
JPS62117820A (ja) 1985-11-19 1987-05-29 Nitto Boseki Co Ltd 炭素繊維チヨツプドストランドの製造方法
US5241731A (en) * 1987-03-03 1993-09-07 Concordia Mfg. Co., Inc. Apparatus for commingling continuous multifilament yarns
JP2783561B2 (ja) 1987-10-29 1998-08-06 大阪瓦斯株式会社 複合材料用炭素繊維
US5001172A (en) 1987-12-19 1991-03-19 Kabushiki Kaisha Toyota Chuo Kenkyusho Fiber reinforced plastics
US5101542A (en) * 1989-04-05 1992-04-07 Ube Industries, Ltd. Fiber separator for producing fiber reinforced metallic or resin body
US5079812A (en) * 1989-10-12 1992-01-14 Chisso Corporation Tow feeding apparatus
JP2657135B2 (ja) 1991-07-26 1997-09-24 日東紡績株式会社 炭素繊維チョップトストランドおよび同製造用紡糸塗布液
CA2099675C (en) 1991-11-01 1998-12-15 Edward Philip Thicthener Polymeric mouldings reinforced with tows of fibres
EP0609711A1 (en) 1993-02-05 1994-08-10 Hercules Incorporated Method for producing chopped fiber strands
JP3011055B2 (ja) 1995-05-18 2000-02-21 東レ株式会社 ヘルメット
JPH08323924A (ja) 1995-05-30 1996-12-10 Mitsubishi Plastics Ind Ltd 繊維強化樹脂製単位板
EP0957189A2 (de) * 1995-08-23 1999-11-17 Maschinenfabrik Rieter Ag Verfahren und Vorrichtung zum Stauchkräuseln synthetischer Filamentfäden
US6066395A (en) 1997-05-23 2000-05-23 Toray Industries, Inc. Chopped carbon fibers and a production process there of
DE19811014A1 (de) * 1998-03-13 1999-09-16 Hauni Maschinenbau Ag Verfahren und Vorrichtung zum Herstellen von Filterstäben für stabförmige Artikel der tabakverarbeitenden Industrie
KR100302243B1 (ko) * 1998-12-30 2002-06-20 조민호 프리프레그 및 그 제조방법
US6253431B1 (en) 1999-10-25 2001-07-03 Celanese Acetate Llc Air opening jet apparatus
US6315004B1 (en) * 2000-06-26 2001-11-13 Ats Products, Inc. Electrostatic charge neutralizing fume duct
US6453106B1 (en) * 2000-06-30 2002-09-17 Ge-Act Communications, Inc. Method and apparatus for a cable location and protection system
JP3077410U (ja) * 2000-10-31 2001-05-18 林 京子 炭素繊維混抄シート発熱体
GB0026763D0 (en) * 2000-11-02 2000-12-20 Univ Manchester Water/air jet texturing
US20030124314A1 (en) * 2001-12-31 2003-07-03 Michael Rajendran S. Structurally enhanced sound and heat energy absorbing liner and related method
JP2003268674A (ja) 2002-03-08 2003-09-25 Toray Ind Inc サイズされた炭素繊維束の製造方法およびチョップド炭素繊維
US6854166B2 (en) * 2002-05-08 2005-02-15 Atlantic Integrated Technologies Insulative non-woven fabric and method for forming same
US6855283B2 (en) * 2002-07-25 2005-02-15 Patent Holdings Company Method for forming a sheet, fiber and resin composite
JP2004084133A (ja) 2002-08-28 2004-03-18 Toray Ind Inc 炭素繊維チョップドストランドおよびその製造方法
KR200302243Y1 (ko) * 2002-10-26 2003-02-05 표상준 샌드위치 패널 절단장치
US6868662B2 (en) * 2002-11-14 2005-03-22 Invista North America S.A.R.L. Entangled bicomponent yarn and process to make the same
JP4278969B2 (ja) 2002-12-13 2009-06-17 三菱レイヨン株式会社 高導電性を発現する繊維強化樹脂用の炭素繊維束及びチョップド炭素繊維束並びに炭素繊維強化樹脂組成物
US6729676B1 (en) 2003-01-22 2004-05-04 Daimlerchrysler Corporation Hybrid composite reinforced door inner panel
US20050095415A1 (en) * 2003-10-30 2005-05-05 Raghavendran Venkat K. Glass mat thermoplastic composite
JP2005155971A (ja) 2003-11-21 2005-06-16 Nippon Oil Corp 煙突用繊維強化プラスチック製ライニングパネル
JP4788599B2 (ja) 2004-08-19 2011-10-05 東レ株式会社 水系プロセス用炭素繊維及び水系プロセス用チョップド炭素繊維
US20060141260A1 (en) 2004-12-29 2006-06-29 Enamul Haque Sandwich composite material using an air-laid process and wet glass
CN2838950Y (zh) * 2005-08-26 2006-11-22 上海汽车集团股份有限公司 汽车用碳纤复合材料
US7968024B2 (en) 2005-09-12 2011-06-28 Ford Global Technologies, Llc Method for forming molding compounds and articles therefrom
US20070132126A1 (en) * 2005-12-14 2007-06-14 Shao Richard L Method for debundling and dispersing carbon fiber filaments uniformly throughout carbon composite compacts before densification
US7943073B2 (en) 2006-06-23 2011-05-17 Battelle Memorial Institute Composite materials and method of making
US7655297B2 (en) 2006-10-19 2010-02-02 Continental Structural Plastics Electrically conductive polyester molding composition having a high quality surface finish
US7691223B2 (en) 2007-01-25 2010-04-06 Ford Global Technologies, Llc Apparatus and method for making fiber reinforced sheet molding compound
DE102007012607B4 (de) * 2007-03-13 2009-02-26 Eads Deutschland Gmbh Spreizvorrichtung zum Aufspreizen von Faserfilamentbündeln sowie damit versehene Preform-Herstellvorrichtung
JP2008254191A (ja) 2007-03-30 2008-10-23 Honda Motor Co Ltd 炭素繊維複合材料製造装置、これを用いた炭素繊維複合材料製造方法および炭素繊維複合材料
US8196631B2 (en) 2008-11-25 2012-06-12 Ford Global Technologies, Llc Fiber transfer apparatus for laminating fiber-reinforced sheet molding compound
US20100143692A1 (en) 2008-12-10 2010-06-10 Ryan James P Carbon and Glass Fiber Reinforced Composition
JP5700496B2 (ja) 2010-03-08 2015-04-15 東邦テナックス株式会社 炭素繊維チョップドストランド及びその製造法
CN102504492B (zh) * 2011-11-16 2014-03-05 金柏青 碳纤维与玻璃纤维混杂增强的片状模塑料及其生产工艺
US9371468B2 (en) 2013-01-16 2016-06-21 Composites Intellectual Holdings, Inc. Co-cured gel coats, elastomeric coatings, structural layers, and in-mold processes for their use

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