CN107011648A - A kind of Kevlar fiber cloths enhancing polyureas based composites and preparation method thereof - Google Patents
A kind of Kevlar fiber cloths enhancing polyureas based composites and preparation method thereof Download PDFInfo
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- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
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- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
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- 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
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- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
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- C08L77/00—Compositions of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Compositions of derivatives of such polymers
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- C08J2375/00—Characterised by the use of polyureas or polyurethanes; Derivatives of such polymers
- C08J2375/02—Polyureas
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- C08J2377/00—Characterised by the use of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Derivatives of such polymers
- C08J2377/10—Polyamides derived from aromatically bound amino and carboxyl groups of amino carboxylic acids or of polyamines and polycarboxylic acids
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- C08J2475/00—Characterised by the use of polyureas or polyurethanes; Derivatives of such polymers
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- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
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- C08J2477/00—Characterised by the use of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Derivatives of such polymers
- C08J2477/10—Polyamides derived from aromatically bound amino and carboxyl groups of amino carboxylic acids or of polyamines and polycarboxylic acids
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/14—Polymer mixtures characterised by other features containing polymeric additives characterised by shape
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Abstract
一种Kevlar纤维布增强聚脲基复合材料及其制备方法,它涉及一种Kevlar纤维布增强聚脲基复合材料及其制备方法。本发明是要解决单一聚脲弹性体材料强度较低以及Kevlar纤维布服役时纤维横向拔出导致的材料失效的问题。Kevlar纤维布增强聚脲基复合材料以Kevlar纤维布作为增强体,以聚脲作为基体进行结合。一、制备聚脲弹性体;二、纤维布料裁剪并浸入聚脲;三、抽真空;四、纤维布铺陈;五、压铸。本发明制备的纤维布增强聚脲基复合材料可用于军用领域,如防弹装甲背板、飞机、导弹结构材料、防护头盔等;民用结构材料领域,如管道、墙板等建筑结构材料。
A Kevlar fiber cloth reinforced polyurea-based composite material and a preparation method thereof relate to a Kevlar fiber cloth reinforced polyurea-based composite material and a preparation method thereof. The invention aims to solve the problems of low strength of a single polyurea elastomer material and material failure caused by lateral pull-out of fibers when the Kevlar fiber cloth is in service. Kevlar fiber cloth-reinforced polyurea-based composite materials use Kevlar fiber cloth as a reinforcement and polyurea as a matrix for bonding. 1. Preparation of polyurea elastomer; 2. Fiber cloth cutting and immersion in polyurea; 3. Vacuuming; 4. Fiber cloth laying; 5. Die-casting. The fiber cloth reinforced polyurea-based composite material prepared by the invention can be used in military fields, such as bulletproof armor backboards, aircraft, missile structural materials, protective helmets, etc.; in the field of civil structural materials, such as building structural materials such as pipes and wall panels.
Description
技术领域technical field
本发明涉及一种Kevlar纤维布增强聚脲基复合材料及其制备方法。The invention relates to a Kevlar fiber cloth reinforced polyurea-based composite material and a preparation method thereof.
背景技术Background technique
聚脲弹性体作为一种高分子材料具有较低的密度和价格,聚脲优异的理化性能包括极高的抗张抗冲击强度、柔韧性、耐磨性、防湿滑、耐老化、防腐蚀等。As a polymer material, polyurea elastomer has low density and price. The excellent physical and chemical properties of polyurea include extremely high tensile impact strength, flexibility, wear resistance, anti-slip, anti-aging, anti-corrosion, etc. .
美空军最先将聚脲涂层应用于建筑物防爆破方面,随后美国海军将聚脲应用于高机动多用途式车辆(HMMWV)装甲板外层,以期减轻弹道碎片和子弹的危害。实验研究表明聚脲层起到了很好的防护效果,能显著增强装甲板对炮火和爆炸碎片的抗穿透能力。聚脲弹性体在高速冲击下会发生玻璃化转变,材料的强度模量会有很大提高,同时耗散了大量能量从而达到防弹的目的,弹性材料往往作为背板形成钢板/陶瓷/弹性材料(德国豹-2、俄罗斯T90坦克)的复合防弹结构。The U.S. Air Force first applied polyurea coatings to building blast protection, and then the U.S. Navy applied polyurea to the outer armor plate of the High Mobility Multipurpose Vehicle (HMMWV) in order to reduce the hazards of ballistic fragments and bullets. Experimental studies have shown that the polyurea layer has a good protective effect and can significantly enhance the penetration resistance of the armor plate against gunfire and explosion fragments. Polyurea elastomer will undergo glass transition under high-speed impact, the strength modulus of the material will be greatly improved, and at the same time dissipate a large amount of energy to achieve the purpose of bulletproof. Elastic materials are often used as back plates to form steel plates/ceramic/elastic materials (German Leopard-2, Russian T90 tank) composite bulletproof structure.
聚脲除了在军事防弹领域有很好的应用前景外,由于其防水、防腐和耐磨的性能在大型基础建设领域也被广泛应用。如管道防腐、隧道防水、桥梁防护等。In addition to having good application prospects in the field of military bulletproof, polyurea is also widely used in the field of large-scale infrastructure construction due to its waterproof, anti-corrosion and wear-resistant properties. Such as pipeline anticorrosion, tunnel waterproofing, bridge protection, etc.
高强度纤维主要包括碳纤维、玻璃纤维、芳纶纤维、超高分子量聚乙烯纤维等。这些纤维由于其超高强度和模量广泛应用于民事、军事领域。纤维增强的聚合物基复合材料也由于其优异的性能而被广泛应用。High-strength fibers mainly include carbon fiber, glass fiber, aramid fiber, ultra-high molecular weight polyethylene fiber, etc. These fibers are widely used in civil and military fields due to their ultra-high strength and modulus. Fiber-reinforced polymer matrix composites are also widely used due to their excellent properties.
纤维增强复合材料有着优于纯纤维和基体的性能。首先,在冲击中基体能够保持纤维对位置和方向不变,并且能够分散纤维之间的应力;其次,基体的存在可以对纤维起到保护作用,避免由环境因素造成纤维性能的降低,如在高湿度条件下纯纤维耐冲击性能的降低和紫外线辐射光降解引起的力学性能的下降;基体破裂导致的分层也是一种能量吸收机制。浸渍的芳纶纤维织物有着更好的动态防侵入性能。在用作轻质防弹或软装甲时,纤维与基质较低的附着力可以使纤维获得更大的变形,从而可以吸收更多的冲击能量。Fiber-reinforced composites have properties superior to pure fibers and matrices. First of all, the matrix can keep the position and direction of the fiber pairs unchanged during the impact, and can disperse the stress between the fibers; secondly, the existence of the matrix can protect the fibers and avoid the degradation of fiber performance caused by environmental factors, such as in The reduction of impact resistance of pure fibers under high humidity conditions and the decrease of mechanical properties caused by ultraviolet radiation photodegradation; delamination caused by matrix rupture is also an energy absorption mechanism. The impregnated aramid fiber fabric has better dynamic anti-intrusion performance. When used as lightweight ballistic or soft armor, the lower fiber-to-matrix adhesion allows the fibers to achieve greater deformation and thus absorb more impact energy.
纤维布增强聚脲基复合材料层合板集合了纤维以及聚脲弹性体共同的优点,通过不同的铺层以及纤维体积分数的设计,可以得到高强、高韧性、低密度、耐腐蚀、防水、以及尤其抗弹体侵切性能的纤维布增强聚脲基复合材料层合板。可以用于大型基础建设领域,如管道防腐、隧道防水、桥梁防护、房屋防爆等;可以用于民用防护领域,如头盔、护膝等护具;还可以用于军事领域,如防弹衣、防弹板、飞机结构等领域。Fiber cloth reinforced polyurea-based composite laminates combine the common advantages of fibers and polyurea elastomers. Through the design of different layers and fiber volume fractions, high strength, high toughness, low density, corrosion resistance, waterproof, and Fiber cloth reinforced polyurea-based composite laminates, especially anti-ballistic cutting performance. It can be used in large-scale infrastructure construction fields, such as pipeline anticorrosion, tunnel waterproofing, bridge protection, house explosion protection, etc.; it can be used in civilian protection fields, such as helmets, knee pads and other protective equipment; it can also be used in military fields, such as bulletproof vests and bulletproof plates , aircraft structures and other fields.
发明内容Contents of the invention
本发明是要解决单一聚脲弹性体材料强度较低以及Kevlar纤维布服役时纤维横向拔出导致的材料失效的问题,而提供一种Kevlar纤维布增强聚脲基复合材料及其制备方法。The invention aims to solve the problems of low strength of a single polyurea elastomer material and material failure caused by lateral pull-out of fibers when Kevlar fiber cloth is in service, and provides a Kevlar fiber cloth reinforced polyurea-based composite material and a preparation method thereof.
一种Kevlar纤维布增强聚脲基复合材料是以Kevlar纤维布作为增强体,以聚脲作为基体进行结合,其中纤维布的体积百分数为50%~90%;所述纤维布的材质为天然纤维或化学纤维;所述聚脲是由二异氰酸酯和二元胺制备而成。A Kevlar fiber cloth-reinforced polyurea-based composite material is combined with Kevlar fiber cloth as a reinforcement and polyurea as a matrix, wherein the volume percentage of the fiber cloth is 50% to 90%; the material of the fiber cloth is natural fiber or chemical fiber; the polyurea is prepared from diisocyanate and diamine.
一种Kevlar纤维布增强聚脲基复合材料的制备方法是按以下步骤完成的:A kind of preparation method of Kevlar fiber cloth reinforced polyurea-based composite material is completed according to the following steps:
一、将二元胺置于反应瓶中,在真空度为100Pa以下磁力搅拌1h~6h至无气泡,得到反应液A;将二异氰酸酯置于反应瓶中,在真空度为100Pa以下磁力搅拌1h~6h至无气泡,得到反应液B;1. Put the diamine in the reaction bottle, stir magnetically for 1h~6h at a vacuum degree below 100Pa until there are no bubbles, and obtain the reaction solution A; put the diisocyanate in the reaction bottle, and magnetically stir for 1h at a vacuum degree below 100Pa ~6h until there is no air bubbles, and the reaction solution B is obtained;
二、将反应液A和反应液B混合,搅拌2~10min,得到聚脲弹性体;所述反应液A中二元胺与反应液B中二异氰酸酯的摩尔比为1:(0.8~1.2);2. Mix the reaction solution A and the reaction solution B, stir for 2-10 minutes to obtain a polyurea elastomer; the molar ratio of the diamine in the reaction solution A to the diisocyanate in the reaction solution B is 1:(0.8-1.2) ;
三、将Kevlar纤维布浸入聚脲弹性体中,抽真空2~10min,得到浸有聚脲的Kevlar纤维布;3. Immerse the Kevlar fiber cloth in the polyurea elastomer, and vacuumize it for 2-10 minutes to obtain the Kevlar fiber cloth soaked in polyurea;
四、将浸有聚脲的Kevlar纤维布逐层铺陈于模具中,在常压或者真空气氛下,使用压力机对最上层的浸有聚脲的Kevlar纤维布施加压力,当压力增加至10~100kN时,在压力为10~100kN下保压0.1~2h,聚脲凝固后脱模得到Kevlar纤维布增强聚脲基复合材料。4. Lay the polyurea-impregnated Kevlar fiber cloth in the mold layer by layer. Under normal pressure or vacuum atmosphere, use a press to apply pressure to the uppermost layer of polyurea-impregnated Kevlar fiber cloth. When the pressure increases to 10~ When the pressure is 100kN, the pressure is maintained at a pressure of 10-100kN for 0.1-2h, and the polyurea is solidified and released from the mold to obtain a Kevlar fiber cloth reinforced polyurea-based composite material.
本发明优点:Advantages of the present invention:
本发明制备工艺简单,无需加热,所得的材料具有高强度,高韧性的特点。其拉伸强度可达100~800MPa,在服役过程中,由于聚脲与纤维结合良好,纤维很难发生横向拔出而失效。The preparation process of the invention is simple, without heating, and the obtained material has the characteristics of high strength and high toughness. Its tensile strength can reach 100-800MPa. During service, due to the good combination of polyurea and fiber, it is difficult for the fiber to be pulled out laterally and fail.
附图说明Description of drawings
图1为采用实施例一得到的Kevlar纤维布增强聚脲基复合材料制成的层合板照片;Fig. 1 is the laminated board photo that adopts the Kevlar fiber cloth that embodiment one obtains to strengthen the polyurea-based composite material to make;
图2为实施例一得到的Kevlar纤维布增强聚脲基复合材料的低倍微观形貌图;Fig. 2 is the low-magnification micro-morphological figure of the Kevlar fiber cloth reinforced polyurea-based composite material obtained in Example 1;
图3为实施例一得到的Kevlar纤维布增强聚脲基复合材料的高倍微观形貌图;Fig. 3 is the high-magnification micro-morphological figure of the Kevlar fiber cloth reinforced polyurea-based composite material obtained in Example 1;
图4为所述模具的分解结构示意图;Fig. 4 is the exploded structural schematic diagram of described mould;
图5为所述带孔下底的结构示意图。Fig. 5 is a structural schematic diagram of the lower bottom with holes.
具体实施方式detailed description
具体实施方式一:本实施方式一种Kevlar纤维布增强聚脲基复合材料是以Kevlar纤维布作为增强体,以聚脲作为基体进行结合,其中纤维布的体积百分数为50%~90%;所述纤维布的材质为天然纤维或化学纤维;所述聚脲是由二异氰酸酯和二元胺制备而成。Specific embodiment 1: In this embodiment, a Kevlar fiber cloth reinforced polyurea-based composite material is combined with Kevlar fiber cloth as a reinforcement and polyurea as a matrix, wherein the volume percentage of the fiber cloth is 50% to 90%; The fiber cloth is made of natural fiber or chemical fiber; the polyurea is prepared from diisocyanate and diamine.
本实施方式中纤维与聚脲良好结合,材料中聚脲完全或部分渗入纤维束中的单根纤维中。In this embodiment, the fibers are well combined with the polyurea, and the polyurea in the material completely or partially penetrates into the individual fibers in the fiber bundle.
具体实施方式二:本实施方式与具体实施方式一不同的是:所述Kevlar纤维布的形式为编织布和单向布中的一种或者两种的混合。其他与具体实施方式一相同。Embodiment 2: This embodiment is different from Embodiment 1 in that: the form of the Kevlar fiber cloth is one or a mixture of woven cloth and unidirectional cloth. Others are the same as the first embodiment.
具体实施方式三:本实施方式与具体实施方式一或二不同的是:所述二元胺和二异氰酸酯的摩尔比为1:(0.8~1.2)。其他与具体实施方式一或二相同。Embodiment 3: This embodiment is different from Embodiment 1 or Embodiment 2 in that the molar ratio of the diamine to diisocyanate is 1:(0.8-1.2). Others are the same as those in Embodiment 1 or 2.
具体实施方式四:本实施方式与具体实施方式一至三之一不同的是:所述二元胺和二异氰酸酯的摩尔比为1:1。其他与具体实施方式一至三之一相同。Embodiment 4: This embodiment is different from Embodiment 1 to Embodiment 3 in that the molar ratio of diamine to diisocyanate is 1:1. Others are the same as one of the specific embodiments 1 to 3.
具体实施方式五:本实施方式与具体实施方式一至四之一不同的是:所述二异氰酸酯为甲苯二异氰酸酯、二苯基甲烷-4,4’-二异氰酸酯和改性二苯基甲烷二异氰酸酯中的一种或其中几种的混合物。其他与具体实施方式一至四之一相同。Embodiment 5: The difference between this embodiment and Embodiments 1 to 4 is that the diisocyanate is toluene diisocyanate, diphenylmethane-4,4'-diisocyanate and modified diphenylmethane diisocyanate one or a mixture of several of them. Others are the same as one of the specific embodiments 1 to 4.
具体实施方式六:本实施方式与具体实施方式一至五之一不同的是:所述二元胺为聚-1,4-丁二醇双(4-氨基苯甲酸酯)、端氨基聚氧化丙烯醚和端氨基聚氧化乙烯醚中的一种或其中几种的混合物,当二元胺为混合物时其分子量为230~5000。其他与具体实施方式一至五之一相同。Embodiment 6: The difference between this embodiment and one of Embodiments 1 to 5 is that the diamine is poly-1,4-butanediol bis(4-aminobenzoate), amino-terminated polyoxygen One of propylene ether and amino-terminated polyoxyethylene ether or a mixture of several of them, when the diamine is a mixture, its molecular weight is 230-5000. Others are the same as one of the specific embodiments 1 to 5.
具体实施方式七:本实施方式一种Kevlar纤维布增强聚脲基复合材料的制备方法是按以下步骤完成的:Embodiment 7: In this embodiment, a method for preparing a Kevlar fiber cloth reinforced polyurea-based composite material is completed in the following steps:
一、将二元胺置于反应瓶中,在真空度为100Pa以下磁力搅拌1h~6h至无气泡,得到反应液A;将二异氰酸酯置于反应瓶中,在真空度为100Pa以下磁力搅拌1h~6h至无气泡,得到反应液B;1. Put the diamine in the reaction bottle, stir magnetically for 1h~6h at a vacuum degree below 100Pa until there are no bubbles, and obtain the reaction solution A; put the diisocyanate in the reaction bottle, and magnetically stir for 1h at a vacuum degree below 100Pa ~6h until there is no air bubbles, and the reaction solution B is obtained;
二、将反应液A和反应液B混合,搅拌2~10min,得到聚脲弹性体;所述反应液A中二元胺与反应液B中二异氰酸酯的摩尔比为1:(0.8~1.2);2. Mix the reaction solution A and the reaction solution B, stir for 2-10 minutes to obtain a polyurea elastomer; the molar ratio of the diamine in the reaction solution A to the diisocyanate in the reaction solution B is 1:(0.8-1.2) ;
三、将Kevlar纤维布浸入聚脲弹性体中,抽真空2~10min,得到浸有聚脲的Kevlar纤维布;3. Immerse the Kevlar fiber cloth in the polyurea elastomer, and vacuumize it for 2-10 minutes to obtain the Kevlar fiber cloth soaked in polyurea;
四、将浸有聚脲的Kevlar纤维布逐层铺陈于模具中,在常压或者真空气氛下,使用压力机对最上层的浸有聚脲的Kevlar纤维布施加压力,当压力增加至10~100kN时,在压力为10~100kN下保压0.1~2h,聚脲凝固后脱模得到Kevlar纤维布增强聚脲基复合材料。4. Lay the polyurea-impregnated Kevlar fiber cloth in the mold layer by layer. Under normal pressure or vacuum atmosphere, use a press to apply pressure to the uppermost layer of polyurea-impregnated Kevlar fiber cloth. When the pressure increases to 10~ When the pressure is 100kN, the pressure is maintained at a pressure of 10-100kN for 0.1-2h, and the polyurea is solidified and released from the mold to obtain a Kevlar fiber cloth reinforced polyurea-based composite material.
本实施方式步骤三中所述抽真空的真空度为1000Pa以下。The degree of vacuum described in step 3 of this embodiment is below 1000 Pa.
具体实施方式八:本实施方式与具体实施方式七不同的是:步骤一中所述二异氰酸酯为甲苯二异氰酸酯、二苯基甲烷-4,4’-二异氰酸酯和改性二苯基甲烷二异氰酸酯中的一种或其中几种的混合物。其他与具体实施方式七相同。Embodiment 8: The difference between this embodiment and Embodiment 7 is that the diisocyanate described in step 1 is toluene diisocyanate, diphenylmethane-4,4'-diisocyanate and modified diphenylmethane diisocyanate one or a mixture of several of them. Others are the same as the seventh embodiment.
具体实施方式九:本实施方式与具体实施方式七或八不同的是:所述二元胺为聚-1,4-丁二醇双(4-氨基苯甲酸酯)、端氨基聚氧化丙烯醚和端氨基聚氧化乙烯醚中的一种或其中几种的混合物,当二元胺为混合物时其分子量为230~5000。其他与具体实施方式七或八相同。Specific embodiment nine: the difference between this embodiment and specific embodiment seven or eight is that the diamine is poly-1,4-butanediol bis(4-aminobenzoate), amino-terminated polyoxypropylene One of ether and amino-terminated polyoxyethylene ether or a mixture of several of them, when the diamine is a mixture, its molecular weight is 230-5000. Others are the same as the seventh or eighth specific embodiment.
具体实施方式十:本实施方式与具体实施方式七至九之一不同的是:步骤四中所述逐层铺陈的方式为[0°/22.5°]n铺设、[0°/45°]n铺设、[0°/67.5°]n铺设、[0°/90°]n铺设、[0°/30°]n铺设、[0°/60°]n铺设、[-30°/30°]n铺设、[-60°/60°]n铺设、[0°/22.5°/45°/67.5°/90°]n铺设和[0°/45°/90°/135°]n铺设中的一种或其中几种的组合。其他与具体实施方式七至九之一相同。Specific Embodiment 10: The difference between this embodiment and one of specific embodiments 7 to 9 is that the way of layer-by-layer laying described in step 4 is [0°/22.5°] n laying, [0°/45°] n Lay, [0°/67.5°] nlay , [0°/90°] nlay , [0°/30°] nlay , [0°/60°] nlay , [-30°/30°] n laying, [-60°/60°] n laying, [0°/22.5°/45°/67.5°/90°] n laying, and [0°/45°/90°/135°] n laying one or a combination of several of them. Others are the same as one of the seventh to ninth specific embodiments.
具体实施方式十一:本实施方式与具体实施方式七至十之一不同的是:步骤四中所述模具由上压头1、模具主体2和带孔下底3组成;所述模具主体2中间开有通孔,所述带孔下底3设置在通孔的一侧,所述上压头1从另一侧压入,所述带孔下底3与所述模具主体2过盈连接,过盈尺寸为0.01mm~1mm。其他与具体实施方式七至十之一相同。Embodiment 11: This embodiment differs from Embodiment 7 to Embodiment 11 in that: the mold described in step 4 is composed of an upper indenter 1, a mold body 2 and a lower bottom 3 with holes; the mold body 2 There is a through hole in the middle, the lower bottom 3 with holes is arranged on one side of the through hole, the upper indenter 1 is pressed in from the other side, and the lower bottom 3 with holes is in interference connection with the mold main body 2 , The interference size is 0.01mm ~ 1mm. Others are the same as one of the seventh to tenth specific embodiments.
具体实施方式十二:本实施方式与具体实施方式七至十一之一不同的是:步骤二中所述反应液A中二元胺与反应液B中二异氰酸酯的摩尔比为1:1。其他与具体实施方式七至十一之一相同。Embodiment 12: This embodiment differs from Embodiment 7 to Embodiment 11 in that the molar ratio of the diamine in the reaction solution A to the diisocyanate in the reaction solution B in step 2 is 1:1. Others are the same as one of the seventh to eleventh specific embodiments.
采用以下实施例验证本发明的有益效果:Adopt the following examples to verify the beneficial effects of the present invention:
实施例一:一种Kevlar纤维布增强聚脲基复合材料的制备方法是按以下步骤完成的:Embodiment one: a kind of preparation method of Kevlar fiber cloth reinforced polyurea-based composite material is completed according to the following steps:
一、将二元胺置于反应瓶中,在真空度为10Pa以下磁力搅拌3h至无气泡,得到反应液A;将二异氰酸酯置于反应瓶中,在真空度为10Pa以下磁力搅拌3h至无气泡,得到反应液B;所述二元胺与二异氰酸酯的摩尔比为1;1. Put the diamine in the reaction bottle, stir magnetically for 3 hours at a vacuum degree below 10Pa until there is no bubble, and obtain the reaction solution A; put the diisocyanate in the reaction bottle, and stir magnetically for 3 hours at a vacuum degree below 10Pa until there is no air bubbles. bubbles to obtain reaction solution B; the molar ratio of the diamine to diisocyanate is 1;
二、将反应液A和反应液B混合,搅拌3min,得到聚脲弹性体;2. Mix the reaction solution A and the reaction solution B, and stir for 3 minutes to obtain a polyurea elastomer;
三、将Kevlar编织纤维布浸入聚脲弹性体中,抽真空3min,得到浸有聚脲的Kevlar纤维布;3. Immerse the Kevlar woven fiber cloth in the polyurea elastomer, and vacuumize it for 3 minutes to obtain the Kevlar fiber cloth soaked in polyurea;
四、将浸有聚脲的Kevlar纤维布以[0°]n铺层方式铺陈于模具中,在常压气氛下,使用压力机对最上层的浸有聚脲的Kevlar纤维布施加压力,当压力增加至50kN时,在压力为50kN下保压1h,聚脲凝固后脱模得到Kevlar纤维布增强聚脲基复合材料。4. Lay the polyurea-impregnated Kevlar fiber cloth in [0°]n layers in the mold. Under normal pressure atmosphere, use a press to apply pressure to the uppermost polyurea-impregnated Kevlar fiber cloth. When When the pressure was increased to 50kN, the pressure was kept at 50kN for 1h, and the polyurea was solidified and released from the mold to obtain a Kevlar fiber cloth reinforced polyurea-based composite material.
图1为采用实施例一得到的Kevlar纤维布增强聚脲基复合材料制成的层合板照片;图2为实施例一得到的Kevlar纤维布增强聚脲基复合材料的低倍微观形貌图;图3为实施例一得到的Kevlar纤维布增强聚脲基复合材料的高倍微观形貌图。从图2和图3可以看出层压复合材料致密,纤维单丝与聚脲结合良好。Fig. 1 is the laminated board photo that adopts the Kevlar fiber cloth reinforced polyurea-based composite material that embodiment one obtains to make; Fig. 2 is the low-magnification microscopic topography figure of the Kevlar fiber cloth reinforced polyurea-based composite material that embodiment one obtains; Fig. 3 is a high-magnification microscopic morphology diagram of the Kevlar fiber cloth reinforced polyurea-based composite material obtained in Example 1. It can be seen from Figure 2 and Figure 3 that the laminated composite material is dense, and the fiber monofilament is well combined with polyurea.
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110822998A (en) * | 2018-08-14 | 2020-02-21 | 郭骏 | Method for protecting equipment or equipment parts |
CN111256536A (en) * | 2020-02-28 | 2020-06-09 | 南京航空航天大学 | Penetrating cutting wire laying reinforced flat integral breaking type fragile cover and preparation method thereof |
CN113480840A (en) * | 2021-07-09 | 2021-10-08 | 成都上泰科技有限公司 | Method for manufacturing high-performance polyurea composite material containing reinforced fiber cloth |
CN113831822A (en) * | 2021-07-09 | 2021-12-24 | 成都上泰科技有限公司 | Method for manufacturing high-performance polyurea composite material |
CN115406307A (en) * | 2022-07-11 | 2022-11-29 | 东华大学 | Bulletproof flashboard based on oxide filament reinforced ceramic composite material and preparation method |
CN118794304A (en) * | 2024-08-26 | 2024-10-18 | 哈尔滨工程大学 | Aramid fiber reinforced polyurea/epoxy matrix hybrid laminate and preparation method and application thereof |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1326476A (en) * | 1998-11-16 | 2001-12-12 | 亨茨曼国际有限公司 | Polyisocyanurate compositions and composites |
CN1394219A (en) * | 2000-01-13 | 2003-01-29 | 陶氏环球技术公司 | Process for in-line forming of pultruded composites |
US20080020194A1 (en) * | 2005-11-02 | 2008-01-24 | Younes Usama E | Composite articles and a process for their production |
DE102007025870A1 (en) * | 2007-06-01 | 2008-12-04 | Henkel Ag & Co. Kgaa | Thermosetting, thermally expandable molded body with long fibers or fibrous structures |
CN101462382A (en) * | 2009-01-16 | 2009-06-24 | 武汉理工大学 | Sandwich structure composite material with elastic core material and preparation method thereof |
CN102692686A (en) * | 2012-05-23 | 2012-09-26 | 四川航天拓鑫玄武岩实业有限公司 | Fiber reinforced plastic rod for optical cables and manufacturing method thereof |
CN103225369A (en) * | 2013-03-15 | 2013-07-31 | 哈尔滨工业大学 | Fiber composite bar with surface having helicitic texture, and making method thereof |
CN103507278A (en) * | 2012-06-27 | 2014-01-15 | 上海杰事杰新材料(集团)股份有限公司 | Method for preparing glass fiber cloth reinforced thermoplastic polyurethane composite material by solution dipping method |
CN103524695A (en) * | 2012-07-02 | 2014-01-22 | 上海杰事杰新材料(集团)股份有限公司 | Glass fiber reinforced thermoplastic polyurethane composite material and preparation method thereof |
CN103804888A (en) * | 2012-11-07 | 2014-05-21 | 合肥杰事杰新材料股份有限公司 | Continuous glass fiber-reinforced thermoplastic polyurethane composite material and preparation method thereof |
CN104650322A (en) * | 2015-02-18 | 2015-05-27 | 中国科学院长春应用化学研究所 | Preparation method of carbon-dioxide-base polyurea high polymer material |
-
2017
- 2017-06-01 CN CN201710404555.6A patent/CN107011648B/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1326476A (en) * | 1998-11-16 | 2001-12-12 | 亨茨曼国际有限公司 | Polyisocyanurate compositions and composites |
CN1394219A (en) * | 2000-01-13 | 2003-01-29 | 陶氏环球技术公司 | Process for in-line forming of pultruded composites |
US20080020194A1 (en) * | 2005-11-02 | 2008-01-24 | Younes Usama E | Composite articles and a process for their production |
DE102007025870A1 (en) * | 2007-06-01 | 2008-12-04 | Henkel Ag & Co. Kgaa | Thermosetting, thermally expandable molded body with long fibers or fibrous structures |
CN101462382A (en) * | 2009-01-16 | 2009-06-24 | 武汉理工大学 | Sandwich structure composite material with elastic core material and preparation method thereof |
CN102692686A (en) * | 2012-05-23 | 2012-09-26 | 四川航天拓鑫玄武岩实业有限公司 | Fiber reinforced plastic rod for optical cables and manufacturing method thereof |
CN103507278A (en) * | 2012-06-27 | 2014-01-15 | 上海杰事杰新材料(集团)股份有限公司 | Method for preparing glass fiber cloth reinforced thermoplastic polyurethane composite material by solution dipping method |
CN103524695A (en) * | 2012-07-02 | 2014-01-22 | 上海杰事杰新材料(集团)股份有限公司 | Glass fiber reinforced thermoplastic polyurethane composite material and preparation method thereof |
CN103804888A (en) * | 2012-11-07 | 2014-05-21 | 合肥杰事杰新材料股份有限公司 | Continuous glass fiber-reinforced thermoplastic polyurethane composite material and preparation method thereof |
CN103225369A (en) * | 2013-03-15 | 2013-07-31 | 哈尔滨工业大学 | Fiber composite bar with surface having helicitic texture, and making method thereof |
CN104650322A (en) * | 2015-02-18 | 2015-05-27 | 中国科学院长春应用化学研究所 | Preparation method of carbon-dioxide-base polyurea high polymer material |
Non-Patent Citations (2)
Title |
---|
中国大百科全书出版社编辑部: "《中国大百科全书 化学1》", 28 February 1989, 中国大百科全书出版社 * |
赵雨花: ""短Kevlar纤维增强的热塑性聚氨酯弹性体"", 《中国聚氨酯工业协会第八次年会论文集》 * |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110822998A (en) * | 2018-08-14 | 2020-02-21 | 郭骏 | Method for protecting equipment or equipment parts |
CN111256536A (en) * | 2020-02-28 | 2020-06-09 | 南京航空航天大学 | Penetrating cutting wire laying reinforced flat integral breaking type fragile cover and preparation method thereof |
CN111256536B (en) * | 2020-02-28 | 2021-06-22 | 南京航空航天大学 | Penetrating cutting wire laying reinforced flat integral breaking type fragile cover and preparation method thereof |
CN113480840A (en) * | 2021-07-09 | 2021-10-08 | 成都上泰科技有限公司 | Method for manufacturing high-performance polyurea composite material containing reinforced fiber cloth |
CN113831822A (en) * | 2021-07-09 | 2021-12-24 | 成都上泰科技有限公司 | Method for manufacturing high-performance polyurea composite material |
CN115406307A (en) * | 2022-07-11 | 2022-11-29 | 东华大学 | Bulletproof flashboard based on oxide filament reinforced ceramic composite material and preparation method |
CN115406307B (en) * | 2022-07-11 | 2024-01-26 | 东华大学 | A bulletproof insert plate based on oxide filament-reinforced ceramic composite material and its preparation method |
CN118794304A (en) * | 2024-08-26 | 2024-10-18 | 哈尔滨工程大学 | Aramid fiber reinforced polyurea/epoxy matrix hybrid laminate and preparation method and application thereof |
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