CN115674806A - Composite impact-resistant fork and preparation method thereof - Google Patents
Composite impact-resistant fork and preparation method thereof Download PDFInfo
- Publication number
- CN115674806A CN115674806A CN202211399328.6A CN202211399328A CN115674806A CN 115674806 A CN115674806 A CN 115674806A CN 202211399328 A CN202211399328 A CN 202211399328A CN 115674806 A CN115674806 A CN 115674806A
- Authority
- CN
- China
- Prior art keywords
- carbon fiber
- resistant
- layer
- impact
- composite
- 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
Landscapes
- Laminated Bodies (AREA)
Abstract
本发明属于搬运机器人货叉技术领域,公开了一种复合耐冲击货叉及其制备方法,自一侧向另一侧依次设置表面耐冲击层、中间界面层和底部刚性层,其中,所述表面耐冲击层为碳纤维二维编织结构与热塑性树脂基体的复合结构;中间界面层采用芳纶蜂窝结构与热塑性树脂基体的复合结构;底部刚性层包括主体和若干个缓冲片,所述主体为高强度碳纤维三维编织结构与热固性树脂基体的复合结构,若干缓冲片均匀预埋于所述主体的靠近中间界面层的一侧。该结构的货叉具有较好的耐冲击作用、刚性、抗震性能和缓冲性能。
The invention belongs to the technical field of handling robot forks, and discloses a composite impact-resistant fork and a preparation method thereof. A surface impact-resistant layer, an intermediate interface layer, and a bottom rigid layer are sequentially arranged from one side to the other side, wherein the The surface impact-resistant layer is a composite structure of carbon fiber two-dimensional weaving structure and thermoplastic resin matrix; the middle interface layer is a composite structure of aramid honeycomb structure and thermoplastic resin matrix; the bottom rigid layer includes a main body and several buffer sheets, and the main body is high A composite structure of a three-dimensional braided structure of strong carbon fibers and a thermosetting resin matrix, and several buffer sheets are evenly pre-embedded on the side of the main body close to the middle interface layer. The cargo fork of this structure has good impact resistance, rigidity, shock resistance and cushioning performance.
Description
技术领域technical field
本发明属于搬运机器人货叉技术领域,具体涉及一种复合耐冲击货叉及其制备方法。The invention belongs to the technical field of handling robot forks, and in particular relates to a composite impact-resistant fork and a preparation method thereof.
背景技术Background technique
这里的陈述仅提供与本发明相关的背景技术,而不必然地构成现有技术。The statements herein merely provide background information related to the present invention and do not necessarily constitute prior art.
随着科技的不断发展,很多工作渐渐由人工处理转变为由机器人来完成,从而大大节省人力,提高工作效率。搬运机器人具有高速平稳控制技术,通过轨迹优化、提高货叉刚性和关节伺服性能,实现搬运的平稳性。搬运机器人可实现货物的完整自动化搬运转移,它的工作性能直接影响着生产效率,因此对搬运机器人中货叉的改进优化具有积极意义。With the continuous development of science and technology, many tasks are gradually changed from manual processing to robotics, which greatly saves manpower and improves work efficiency. The handling robot has high-speed and stable control technology. Through trajectory optimization, improving the rigidity of the fork and joint servo performance, the stability of handling is realized. The handling robot can realize the complete automatic handling and transfer of goods, and its working performance directly affects the production efficiency, so it has positive significance for the improvement and optimization of the fork in the handling robot.
碳纤维复合材料货叉与普通货叉相比具有质量轻、抗腐蚀性强、抗疲劳强度高等优点,但是货叉在使用过程中一般会受到较大的冲击作用和剪切力,而一般的碳纤维复合材料为层级结构,在这些作用力下,碳纤维复合材料的层级结构之间容易分层,货叉整体容易发生形变,甚至发生弯折,影响货叉的整体使用寿命。Compared with ordinary forks, carbon fiber composite forks have the advantages of light weight, strong corrosion resistance, and high fatigue strength. The composite material has a hierarchical structure. Under these forces, the hierarchical structure of the carbon fiber composite material is easy to delaminate, and the overall fork is prone to deformation or even bending, which affects the overall service life of the fork.
发明内容Contents of the invention
针对现有技术存在的不足,本发明的目的是提供一种复合耐冲击货叉及其制备方法。Aiming at the deficiencies in the prior art, the object of the present invention is to provide a composite impact-resistant fork and a preparation method thereof.
为了实现上述目的,本发明是通过如下的技术方案来实现:In order to achieve the above object, the present invention is achieved through the following technical solutions:
第一方面,本发明提供一种复合耐冲击货叉,自一侧向另一侧依次设置表面耐冲击层、中间界面层和底部刚性层,其中,In the first aspect, the present invention provides a composite impact-resistant fork, in which a surface impact-resistant layer, an intermediate interface layer and a bottom rigid layer are sequentially arranged from one side to the other, wherein,
所述表面耐冲击层为碳纤维二维编织结构与热塑性树脂基体的复合结构;The surface impact-resistant layer is a composite structure of carbon fiber two-dimensional weaving structure and thermoplastic resin matrix;
中间界面层采用芳纶蜂窝结构与热塑性树脂基体的复合结构;The middle interface layer adopts the composite structure of aramid fiber honeycomb structure and thermoplastic resin matrix;
底部刚性层包括主体和若干个缓冲片,所述主体为高强度碳纤维三维编织结构与热固性树脂基体的复合结构,若干缓冲片呈矩阵均匀分布且预埋于所述主体的靠近中间界面层的一侧,使缓冲片直接与中间界面层粘结固定;The bottom rigid layer includes a main body and several buffer sheets. The main body is a composite structure of a high-strength carbon fiber three-dimensional braided structure and a thermosetting resin matrix. Side, so that the buffer sheet is directly bonded to the middle interface layer;
缓冲片的厚度大于等于1mm,且底部刚性层的厚度至少为缓冲片厚度的2倍。The thickness of the buffer sheet is greater than or equal to 1 mm, and the thickness of the bottom rigid layer is at least twice the thickness of the buffer sheet.
第二方面,本发明提供所述复合耐冲击货叉的制备方法,包括如下步骤:In a second aspect, the present invention provides a method for preparing the composite impact-resistant fork, comprising the following steps:
铣切成型的芳纶蜂窝,并填充热塑性树脂;Aramid honeycombs milled to shape and filled with thermoplastic resin;
在填充有热塑性树脂的芳纶蜂窝的上下表面分别铺贴热塑性胶膜;Lay thermoplastic films on the upper and lower surfaces of the aramid honeycomb filled with thermoplastic resin;
然后在芳纶蜂窝的上下表面分别铺设碳纤维二维编织结构预浸布和碳纤维三维编织结构预浸布,并在碳纤维三维编织结构预浸布靠近芳纶蜂窝的一侧中均匀预埋缓冲片;Then lay a carbon fiber two-dimensional woven structure prepreg and a carbon fiber three-dimensional woven structure prepreg on the upper and lower surfaces of the aramid honeycomb, and evenly embed a buffer sheet in the side of the carbon fiber three-dimensional woven structure prepreg close to the aramid honeycomb;
铺设完毕后,热压固化成型,即得。After the laying is completed, it is hot-pressed and solidified to form the finished product.
上述本发明的一种或多种实施例取得的有益效果如下:The beneficial effects obtained by one or more embodiments of the present invention are as follows:
表面耐冲击层为碳纤维二维编织结构与热塑性树脂基体的复合结构,碳纤维二维编织结构对树脂基体进行各向同性地加强,不会有薄弱的加强方向,同时加强结构为二维编织结构,碳纤维之间有较强的相互作用力,使其在较强的冲击作用下不会劈裂,具有较强的耐冲击性能。The surface impact-resistant layer is a composite structure of carbon fiber two-dimensional weaving structure and thermoplastic resin matrix. The carbon fiber two-dimensional weaving structure strengthens the resin matrix isotropically, and there will be no weak reinforcement direction. At the same time, the reinforcing structure is a two-dimensional weaving structure. There is a strong interaction force between carbon fibers, so that it will not split under strong impact, and has strong impact resistance.
中间界面层采用芳纶蜂窝和热塑性树脂的复合结构,该种结构具有较强的抗剪切性能,可以有效提高货叉的抗剪切性能,尤其可以提高货叉的抗弯强度。同时,该种结构可以显著减轻货叉的重量,增强货叉的比强度。The middle interface layer adopts a composite structure of aramid fiber honeycomb and thermoplastic resin. This structure has strong shear resistance and can effectively improve the shear resistance of the fork, especially the bending strength of the fork. At the same time, this structure can significantly reduce the weight of the fork and enhance the specific strength of the fork.
底部刚性层的主体为高强度碳纤维三维编织结构与热固性树脂基体的复合结构,该种结构具有较强的刚性,作为底部的最基础的支撑,可以有效减小叉运过程中货叉的形变,为表面耐冲击层和中间界面层提供有力支撑,以有效提高复合材料货叉的使用性能。The main body of the bottom rigid layer is a composite structure of high-strength carbon fiber three-dimensional braided structure and thermosetting resin matrix. This structure has strong rigidity. As the most basic support at the bottom, it can effectively reduce the deformation of the fork during forklifting. Provide strong support for the surface impact-resistant layer and the middle interface layer to effectively improve the performance of the composite fork.
在底部刚性层靠近中间界面层的一侧均匀预埋缓冲片,缓冲片用于吸能,可以对在货叉上施加的冲击力起到较好的缓冲作用,减轻对底部刚性层的瞬时冲击,以改善底部刚性层的受力情况,避免底部刚性层在较大冲击力下断裂。同时,缓冲片还具有减震性能,使叉运过程中更平稳。The buffer sheet is evenly embedded on the side of the bottom rigid layer close to the middle interface layer. The buffer sheet is used for energy absorption, which can better buffer the impact force exerted on the fork and reduce the instantaneous impact on the bottom rigid layer. , to improve the stress of the bottom rigid layer and avoid the bottom rigid layer from breaking under a large impact force. At the same time, the buffer sheet also has shock-absorbing properties, making the forklift more stable.
缓冲片的厚度大于等于1mm,以保证提供有效的缓冲作用,对底部刚性层的厚度进行限定,使得底部刚性层除去预埋缓冲片的厚度,还有足够的厚度对货叉的表面耐冲击层和中间界面层进行有效支撑。The thickness of the buffer sheet is greater than or equal to 1mm to ensure an effective buffering effect, and the thickness of the bottom rigid layer is limited so that the bottom rigid layer removes the thickness of the embedded buffer sheet, and there is still enough thickness for the impact-resistant layer on the surface of the fork and the intermediate interface layer for effective support.
如果将缓冲片预埋到底部刚性层内部,缓冲片与中间界面层之间通过部分底部刚性层进行粘结时,首先需要该部分底部刚性层通过形变将力传递到缓冲片,使缓冲片起到相应的作用,但是发生形变的底部刚性层会带动其他部位相继发生形变,导致缓冲片的作用被削弱。所以将缓冲片设置为直接与中间界面层粘结固定,当将货物放置于叉体上时,力通过表面耐冲击层和中间界面层直接传递到缓冲片上,使缓冲片起到相应的作用,以减少底部刚性层的形变。If the buffer sheet is pre-embedded inside the bottom rigid layer, when the buffer sheet and the middle interface layer are bonded through a part of the bottom rigid layer, the part of the bottom rigid layer first needs to transmit the force to the buffer sheet through deformation, so that the buffer sheet can However, the deformed bottom rigid layer will drive other parts to deform one after another, resulting in the weakened effect of the buffer sheet. Therefore, the buffer sheet is set to be bonded and fixed directly with the middle interface layer. When the goods are placed on the fork body, the force is directly transmitted to the buffer sheet through the surface impact-resistant layer and the middle interface layer, so that the buffer sheet can play a corresponding role. To reduce the deformation of the bottom rigid layer.
热压过程中,芳纶蜂窝两侧的预浸布中的少量树脂进入芳纶蜂窝中,与芳纶蜂窝复合为一体,使表面耐冲击层、中间界面层和底部刚性层形成一个整体,避免货叉在使用过程中分层,可以进一步提高货叉的刚性和耐冲击性能。同时该种复合材料具有较好的耐腐蚀性能。During the hot pressing process, a small amount of resin in the prepreg cloth on both sides of the aramid honeycomb enters the aramid honeycomb and is combined with the aramid honeycomb to form a whole, so that the surface impact-resistant layer, the middle interface layer and the bottom rigid layer form a whole to avoid The fork is delaminated during use, which can further improve the rigidity and impact resistance of the fork. At the same time, the composite material has good corrosion resistance.
附图说明Description of drawings
构成本发明的一部分的说明书附图用来提供对本发明的进一步理解,本发明的示意性实施例及其说明用于解释本发明,并不构成对本发明的不当限定。The accompanying drawings constituting a part of the present invention are used to provide a further understanding of the present invention, and the schematic embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute improper limitations to the present invention.
图1是本发明实施例的复合耐冲击板材结构的整体结构示意图;Fig. 1 is a schematic diagram of the overall structure of the composite impact-resistant plate structure of the embodiment of the present invention;
图2为本发明实施例的复合耐冲击板材结构的底部刚性层的平面图。Fig. 2 is a plan view of the bottom rigid layer of the composite impact-resistant plate structure of the embodiment of the present invention.
其中,1、表面耐冲击层;2、中间界面层;3、底部刚性层;4、缓冲片。Among them, 1. Surface impact-resistant layer; 2. Intermediate interface layer; 3. Bottom rigid layer; 4. Buffer sheet.
具体实施方式Detailed ways
应该指出,以下详细说明都是例示性的,旨在对本发明提供进一步的说明。除非另有指明,本发明使用的所有技术和科学术语具有与本发明所属技术领域的普通技术人员通常理解的相同含义。It should be noted that the following detailed description is exemplary and intended to provide further explanation of the present invention. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs.
第一方面,本发明提供一种复合耐冲击货叉,自一侧向另一侧依次设置表面耐冲击层、中间界面层和底部刚性层,其中,In the first aspect, the present invention provides a composite impact-resistant fork, in which a surface impact-resistant layer, an intermediate interface layer and a bottom rigid layer are sequentially arranged from one side to the other, wherein,
所述表面耐冲击层为碳纤维二维编织结构与热塑性树脂基体的复合结构;The surface impact-resistant layer is a composite structure of carbon fiber two-dimensional weaving structure and thermoplastic resin matrix;
中间界面层采用芳纶蜂窝结构与热塑性树脂基体的复合结构;The middle interface layer adopts the composite structure of aramid fiber honeycomb structure and thermoplastic resin matrix;
底部刚性层包括主体和若干个缓冲片,所述主体为高强度碳纤维三维编织结构与热固性树脂基体的复合结构,若干缓冲片呈矩阵均匀分布且预埋于所述主体的靠近中间界面层的一侧,使缓冲片直接与中间界面层粘结固定;The bottom rigid layer includes a main body and several buffer sheets. The main body is a composite structure of a high-strength carbon fiber three-dimensional braided structure and a thermosetting resin matrix. Side, so that the buffer sheet is directly bonded to the middle interface layer;
缓冲片的厚度大于等于1mm,且底部刚性层的厚度至少为缓冲片厚度的2倍。The thickness of the buffer sheet is greater than or equal to 1 mm, and the thickness of the bottom rigid layer is at least twice the thickness of the buffer sheet.
碳纤维是一种高强度、高模量特种纤维,具有高强度、高模量等优异的力学性能,而且具有重量轻、化学成分稳定、耐高温性能好等优点。碳纤维复合材料货叉与普通钢货叉相比具有质量轻、高强度质量比、抗腐蚀性强、疲劳强度高等优点。芳纶蜂窝芯层在夹层结构中主要承受剪切应力,使夹层结构具有高抗弯刚度。Carbon fiber is a special fiber with high strength and high modulus. It has excellent mechanical properties such as high strength and high modulus, and has the advantages of light weight, stable chemical composition, and good high temperature resistance. Compared with ordinary steel forks, carbon fiber composite forks have the advantages of light weight, high strength-to-mass ratio, strong corrosion resistance, and high fatigue strength. The aramid honeycomb core mainly bears the shear stress in the sandwich structure, which makes the sandwich structure have high bending stiffness.
该板材采用多层结构,有效提高了货叉的刚性、耐冲击性以及耐摩擦性。The plate adopts a multi-layer structure, which effectively improves the rigidity, impact resistance and friction resistance of the fork.
在一些实施例中,所述缓冲片为短切碳纤维增强硅橡胶复合材料。In some embodiments, the buffer sheet is a chopped carbon fiber reinforced silicone rubber composite material.
刚性层内预埋缓冲片由硅橡胶掺杂短切碳纤维组成,不仅有着良好的高强度和高比刚度,并且还有着优秀的减震防颤缓冲作用。The embedded buffer sheet in the rigid layer is composed of silicone rubber doped with chopped carbon fiber, which not only has good high strength and high specific stiffness, but also has excellent shock absorption and anti-vibration buffering effect.
优选的,缓冲片中硅橡胶的质量百分数为30-50%,短切碳纤维的长度为2-5mm。Preferably, the mass percentage of silicone rubber in the buffer sheet is 30-50%, and the length of the chopped carbon fiber is 2-5mm.
在一些实施例中,表面耐冲击层的二维平面编织结构选自平纹、斜纹或缎纹编织结构,树脂含量为30%-60%。In some embodiments, the two-dimensional planar weave structure of the surface impact-resistant layer is selected from plain weave, twill weave or satin weave structure, and the resin content is 30%-60%.
优选的,表面耐冲击层的碳纤维为高强碳纤维,选自T300、T700、T800或T1000。Preferably, the carbon fibers of the surface impact-resistant layer are high-strength carbon fibers selected from T300, T700, T800 or T1000.
优选的,表面耐冲击层的热塑性树脂选自聚乙烯、聚丙烯、聚氯乙烯或聚苯乙烯。Preferably, the thermoplastic resin of the surface impact-resistant layer is selected from polyethylene, polypropylene, polyvinyl chloride or polystyrene.
优选的,表面耐冲击层的厚度为2-4mm。Preferably, the thickness of the surface impact-resistant layer is 2-4mm.
在一些实施例中,中间界面层的厚度为3-5mm。In some embodiments, the thickness of the intermediate interface layer is 3-5 mm.
优选的,中间界面层的树脂含量为30%-60%。Preferably, the resin content of the intermediate interface layer is 30%-60%.
芳纶蜂窝的制造一般采用拉伸扩展的方法,生产工序主要分为涂胶、叠合、压制、切割、拉伸、定型、浸胶、固化、片切九个工序。热塑性树脂可选用表面耐冲击层所用热塑性树脂当中的任意一种类型,且不限于上述类型。The manufacture of aramid honeycomb generally adopts the method of stretching and expansion. The production process is mainly divided into nine processes: gluing, lamination, pressing, cutting, stretching, shaping, dipping, curing, and sheet cutting. The thermoplastic resin can be selected from any type of thermoplastic resin used in the surface impact-resistant layer, and is not limited to the above-mentioned types.
在一些实施例中,底部刚性层的厚度为3-5mm,缓冲片的厚度为1-2mm。In some embodiments, the bottom rigid layer has a thickness of 3-5 mm, and the buffer sheet has a thickness of 1-2 mm.
优选的,底部刚性层与缓冲片的厚度之差至少为2mm。以保证底部刚性层在未预埋缓冲片一侧的刚性,以提供足够的支撑作用。Preferably, the thickness difference between the bottom rigid layer and the buffer sheet is at least 2 mm. To ensure the rigidity of the bottom rigid layer on the side where the buffer sheet is not embedded, so as to provide sufficient support.
优选的,底部刚性层的树脂含量为30~60%。Preferably, the resin content of the bottom rigid layer is 30-60%.
优选的,底部刚性层的三维编织结构为三维四向、三维五向、三维六向或三维七向的编织结构;Preferably, the three-dimensional braided structure of the bottom rigid layer is a three-dimensional four-way, three-dimensional five-way, three-dimensional six-way or three-dimensional seven-way braided structure;
热固性树脂选自环氧树脂、酚醛树脂、不饱和聚酯树脂或脲醛树脂。The thermosetting resin is selected from epoxy resin, phenolic resin, unsaturated polyester resin or urea-formaldehyde resin.
第二方面,本发明提供所述复合耐冲击货叉的制备方法,包括如下步骤:In a second aspect, the present invention provides a method for preparing the composite impact-resistant fork, comprising the following steps:
铣切成型的芳纶蜂窝,并填充热塑性树脂;Aramid honeycombs milled to shape and filled with thermoplastic resin;
在填充有芳纶蜂窝的上下表面分别铺贴热塑性胶膜;Lay thermoplastic films on the upper and lower surfaces filled with aramid honeycomb;
然后在芳纶蜂窝的上下表面分别铺设碳纤维二维编织结构预浸布和碳纤维三维编织结构预浸布,并在碳纤维三维编织结构预浸布靠近芳纶蜂窝的一侧中均匀预埋缓冲片;Then lay a carbon fiber two-dimensional woven structure prepreg and a carbon fiber three-dimensional woven structure prepreg on the upper and lower surfaces of the aramid honeycomb, and evenly embed a buffer sheet in the side of the carbon fiber three-dimensional woven structure prepreg close to the aramid honeycomb;
铺设完毕后,热压固化成型,即得。After the laying is completed, it is hot-pressed and solidified to form the finished product.
在一些实施例中,所述热塑性胶膜的材质为聚醚酰亚胺(PEI)、聚醚酮(PEK)、聚砜(PSF)或聚醚砜(PES)。In some embodiments, the material of the thermoplastic film is polyetherimide (PEI), polyetherketone (PEK), polysulfone (PSF) or polyethersulfone (PES).
在一些实施例中,碳纤维二维编织结构预浸布的制备方法为:将热塑性胶膜与碳纤维布叠层放置在预热好的压机上,热压,即得;In some embodiments, the preparation method of the carbon fiber two-dimensional woven structure prepreg is as follows: the thermoplastic film and the carbon fiber cloth are stacked on a preheated press, and hot pressed to obtain the product;
热压温度为120~150℃,压强为0.5~2MPa,热压时间为20-60min,热压完成后,再停止加热保持40-60min。The hot-pressing temperature is 120-150°C, the pressure is 0.5-2MPa, and the hot-pressing time is 20-60 minutes. After the hot-pressing is completed, stop heating and keep for 40-60 minutes.
优选的,相邻碳纤维布之间喷涂超细热塑性粘结粉末。Preferably, ultrafine thermoplastic bonding powder is sprayed between adjacent carbon fiber cloths.
进一步优选的,所述超细热塑性粘结粉末选自聚酰胺粉末、聚乙烯粉末或聚氨脂粉末。粉末颗粒度在200~2000目范围内灵活选择。Further preferably, the ultrafine thermoplastic bonding powder is selected from polyamide powder, polyethylene powder or polyurethane powder. The particle size of the powder can be flexibly selected within the range of 200-2000 mesh.
在一些实施例中,热压固化成型的温度为110-130℃,成型压力为0.1-0.5MPa。In some embodiments, the temperature of thermocompression curing molding is 110-130° C., and the molding pressure is 0.1-0.5 MPa.
所述的模压成型是将预浸布压制成的叠层薄板放置在特定金属对模内,经加热、加压固化成型。模压成型工艺流程为首先根据产品尺寸将碳纤维薄板进行削剪,将特定结构模具进行清理,涂脱模剂,放置碳纤维薄板,进行合模处理,上螺丝时螺丝涂上润滑油,确保开模顺利。将完成的碳纤维产品模具放置到预热好的热压机上面,进行3~4次去压,间隔时间10~20s。压机设置温度为130~180℃,压强为2~10MPa,加压时间为30~90min,再停止加热保持30~60min。待模具冷却后进行脱模处理。The compression molding is to place the laminated sheet made of prepreg cloth into a specific metal mold, and then heat and press to solidify and form. The compression molding process is to first cut the carbon fiber sheet according to the size of the product, clean the mold with a specific structure, apply a release agent, place the carbon fiber sheet, and perform mold closing. When screwing the screw, apply lubricating oil to ensure smooth mold opening. . Place the completed carbon fiber product mold on the preheated hot press, and decompress 3 to 4 times with an interval of 10 to 20 seconds. The temperature of the press is set at 130-180°C, the pressure is 2-10 MPa, the pressing time is 30-90 minutes, and then the heating is stopped for 30-60 minutes. After the mold is cooled, demoulding is carried out.
下面结合实施例对本发明作进一步说明。The present invention will be further described below in conjunction with embodiment.
实施例1Example 1
如图1所示,表面耐冲击层1采用T700高强度碳纤维进行二维斜纹编织与聚乙烯树脂进行复合,厚度为3mm,树脂含量为40%。热压成型采用颗粒度为1000目的聚酰胺粉末进行粘结,热塑性胶膜选用聚醚酰亚胺胶膜。热压成型、模压成型皆设置压机温度为150℃,压强为6MPa,加压前进行三次去压,时间间隔为10s,加压时间为40min,再停止加热保持35min。As shown in Figure 1, the surface impact-resistant layer 1 is made of T700 high-strength carbon fiber for two-dimensional twill weaving and composited with polyethylene resin, with a thickness of 3mm and a resin content of 40%. Polyamide powder with a particle size of 1000 mesh is used for hot-press forming, and polyetherimide film is selected as the thermoplastic film. For hot pressing and compression molding, set the temperature of the press to 150°C and the pressure to 6 MPa. Before pressurization, depressurize three times with a time interval of 10s, pressurize for 40min, and then stop heating for 35min.
中间界面层2为蜂窝结构,采用芳纶蜂窝结构与聚丙烯树脂基体复合构成,树脂含量为60%,厚度为5mm。The middle interface layer 2 is a honeycomb structure, which is composed of an aramid honeycomb structure and a polypropylene resin matrix, with a resin content of 60% and a thickness of 5 mm.
底部刚性层3采用T1000高强度碳纤维采用三维七向编织结构配合环氧树脂浸渍复合,缓冲片4由硅橡胶掺杂短切碳纤维构成,硅橡胶含量为30%,短切碳纤维的长度为2mm,缓冲片的厚度为2mm,缓冲片呈矩阵均匀分布在底部刚性层内。底部刚性层的厚度为5mm,树脂含量为40%。The bottom
上述3个叠层部分在热压罐中固化成型的固化温度为120℃,成型压力为0.3Mpa。该结构板材总体树脂基体含量为45%,厚度为13mm。The above three laminated parts are cured and molded in an autoclave at a curing temperature of 120° C. and a molding pressure of 0.3 MPa. The structural board has an overall resin matrix content of 45% and a thickness of 13mm.
实施例2Example 2
表面耐冲击层采用T800高强度碳纤维进行二维平纹编织与聚丙烯树脂进行复合,厚度为2mm,树脂含量为50%。热压成型采用颗粒度为1000目的聚乙烯粉末进行粘结,热塑性胶膜选用聚砜胶膜。热压成型、模压成型皆设置压机温度为180℃,压强为7MPa,加压前进行三次去压,时间间隔为10s,加压时间为80min,再停止加热保持40min。The surface impact-resistant layer is made of T800 high-strength carbon fiber for two-dimensional plain weave and polypropylene resin, with a thickness of 2mm and a resin content of 50%. Polyethylene powder with a particle size of 1000 mesh is used for hot-press forming, and polysulfone film is selected as the thermoplastic film. For hot pressing and compression molding, the temperature of the press is set at 180°C and the pressure is 7 MPa. Before pressurization, depressurization is performed three times with a time interval of 10s. The pressurization time is 80min, and then the heating is stopped for 40min.
中间蜂窝层采用芳纶蜂窝结构与聚乙烯树脂基体复合构成,树脂含量为50%,厚度为4mm。The middle honeycomb layer is composed of aramid honeycomb structure and polyethylene resin matrix, the resin content is 50%, and the thickness is 4mm.
底部刚性层采用T300高强度碳纤维采用三维四向编织结构配合酚醛树脂浸渍复合,缓冲片由硅橡胶掺杂短切碳纤维构成,硅橡胶含量为50%,短切碳纤维的长度为4mm,缓冲片的厚度为2mm,缓冲片呈矩阵均匀分布在底部刚性层内。底部刚性层的厚度为4mm,树脂含量为50%。The rigid layer at the bottom adopts T300 high-strength carbon fiber, adopts three-dimensional four-way weaving structure and phenolic resin impregnation composite, the buffer sheet is composed of silicone rubber doped with chopped carbon fiber, the silicone rubber content is 50%, the length of chopped carbon fiber is 4mm, and the buffer sheet The thickness is 2mm, and the buffer sheets are evenly distributed in the bottom rigid layer in a matrix. The bottom rigid layer has a thickness of 4mm and a resin content of 50%.
上述3个叠层部分在热压罐中固化成型的固化温度为120℃,成型压力为0.3Mpa。该结构板材总体树脂基体含量为50%,厚度为10mm。The above three laminated parts are cured and molded in an autoclave at a curing temperature of 120° C. and a molding pressure of 0.3 MPa. The overall resin matrix content of the structural plate is 50%, and the thickness is 10mm.
实施例3Example 3
表面耐冲击层采用T700高强度碳纤维进行二维缎纹编织与聚氯乙烯树脂进行复合,厚度为3mm,树脂含量为60%。热压成型采用颗粒度为800目的聚酰胺粉末进行粘结,热塑性胶膜选用聚醚酰亚胺胶膜。热压成型、模压成型皆设置压机温度为150℃,压强为6MPa,加压前进行三次去压,时间间隔为10s,加压时间为90min,再停止加热保持35min。The surface impact-resistant layer is made of T700 high-strength carbon fiber for two-dimensional satin weaving and polyvinyl chloride resin, with a thickness of 3mm and a resin content of 60%. Polyamide powder with a particle size of 800 mesh is used for hot-press forming, and polyetherimide film is selected as the thermoplastic film. For hot pressing and compression molding, set the temperature of the press to 150°C and the pressure to 6 MPa. Before pressurization, depressurize three times with a time interval of 10s, pressurize for 90min, and then stop heating for 35min.
中间界面层为蜂窝结构,采用芳纶蜂窝结构与聚氯乙烯树脂基体复合构成,树脂含量为60%,厚度为5mm。The middle interface layer is a honeycomb structure, which is composed of an aramid honeycomb structure and a polyvinyl chloride resin matrix, with a resin content of 60% and a thickness of 5mm.
底部刚性层采用T1000高强度碳纤维采用三维五向编织结构配合脲醛树脂浸渍复合,缓冲片由硅橡胶掺杂短切碳纤维构成,硅橡胶含量为40%,短切碳纤维的长度为5mm,缓冲片的厚度为1mm,缓冲片呈矩阵均匀分布在底部刚性层内。底部刚性层的厚度为4mm,树脂含量为55%。The bottom rigid layer adopts T1000 high-strength carbon fiber, adopts three-dimensional five-way weaving structure and is impregnated with urea-formaldehyde resin. The buffer sheet is composed of silicone rubber doped with chopped carbon fiber. The silicone rubber content is 40%. The thickness is 1mm, and the buffer sheets are evenly distributed in the bottom rigid layer in a matrix. The bottom rigid layer has a thickness of 4mm and a resin content of 55%.
上述3个叠层部分在热压罐中固化成型的固化温度为120℃,成型压力为0.3Mpa。该结构板材总体树脂基体含量为58%,厚度为12mm。The above three laminated parts are cured and molded in an autoclave at a curing temperature of 120° C. and a molding pressure of 0.3 MPa. The structural board has an overall resin matrix content of 58% and a thickness of 12 mm.
实施例4Example 4
表面耐冲击层采用T300高强度碳纤维进行二维斜纹编织与聚乙烯树脂进行复合,厚度为3mm,树脂含量为50%。热压成型采用颗粒度为500目的聚酰胺粉末进行粘结,热塑性胶膜选用聚醚酰亚胺胶膜。热压成型、模压成型皆设置压机温度为130℃,压强为5MPa,加压前进行三次去压,时间间隔为10s,加压时间为50min,再停止加热保持60min。The surface impact-resistant layer is made of T300 high-strength carbon fiber for two-dimensional twill weaving and polyethylene resin, with a thickness of 3mm and a resin content of 50%. Polyamide powder with a particle size of 500 mesh is used for hot-press forming, and polyetherimide film is selected as the thermoplastic film. For hot pressing and compression molding, the temperature of the press is set at 130°C and the pressure is 5 MPa. Before pressurization, depressurization is performed three times with a time interval of 10s, and the pressurization time is 50 minutes, and then the heating is stopped for 60 minutes.
中间界面层为蜂窝结构,采用芳纶蜂窝结构与聚丙烯树脂基体复合构成,树脂含量为30%,厚度为4mm。底部刚性层采用T1000高强度碳纤维采用三维六向编织结构配合环氧树脂浸渍复合,缓冲片由硅橡胶掺杂短切碳纤维构成,硅橡胶含量为30%,短切碳纤维的长度为2mm,缓冲片的厚度为2mm,缓冲片呈矩阵均匀分布在底部刚性层内。底部刚性层的厚度为4mm,树脂含量为40%。The middle interface layer is a honeycomb structure, which is composed of an aramid honeycomb structure and a polypropylene resin matrix, with a resin content of 30% and a thickness of 4mm. The bottom rigid layer adopts T1000 high-strength carbon fiber, adopts three-dimensional six-way weaving structure and epoxy resin impregnation composite, the buffer sheet is composed of silicone rubber doped with chopped carbon fiber, the silicone rubber content is 30%, the length of chopped carbon fiber is 2mm, the buffer sheet The thickness is 2mm, and the buffer sheets are evenly distributed in the bottom rigid layer in a matrix. The bottom rigid layer has a thickness of 4mm and a resin content of 40%.
上述3个叠层部分在热压罐中固化成型的固化温度为120℃,成型压力为0.3Mpa。该结构板材总体树脂基体含量为40%,厚度为11mm。The above three laminated parts are cured and molded in an autoclave at a curing temperature of 120° C. and a molding pressure of 0.3 MPa. The structural board has an overall resin matrix content of 40% and a thickness of 11 mm.
以上所述仅为本发明的优选实施例而已,并不用于限制本发明,对于本领域的技术人员来说,本发明可以有各种更改和变化。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and changes. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included within the protection scope of the present invention.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211399328.6A CN115674806A (en) | 2022-11-09 | 2022-11-09 | Composite impact-resistant fork and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211399328.6A CN115674806A (en) | 2022-11-09 | 2022-11-09 | Composite impact-resistant fork and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN115674806A true CN115674806A (en) | 2023-02-03 |
Family
ID=85050014
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202211399328.6A Pending CN115674806A (en) | 2022-11-09 | 2022-11-09 | Composite impact-resistant fork and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN115674806A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116039121A (en) * | 2023-02-15 | 2023-05-02 | 歌尔股份有限公司 | Carbon fiber-based composite part, preparation method thereof, spectacle frame and spectacles |
CN118124236A (en) * | 2024-05-07 | 2024-06-04 | 山东华特天维新材料有限公司 | Impact-resistant composite material sliding plate and preparation method thereof |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108248124A (en) * | 2018-01-30 | 2018-07-06 | 深圳市郎搏万先进材料有限公司 | A kind of pp cellular sandwich compound plates and preparation method thereof |
CN109849479A (en) * | 2019-01-29 | 2019-06-07 | 连云港市工业投资集团有限公司 | A kind of honeycomb type carbon fibre composite trim panel and preparation method thereof |
KR20210056813A (en) * | 2019-11-11 | 2021-05-20 | 디엘이앤씨 주식회사 | Impact load concentrated floor absorbing system |
CN216860863U (en) * | 2021-09-27 | 2022-07-01 | 上海骏珲新材料科技有限公司 | Solidified honeycomb multilayer material |
-
2022
- 2022-11-09 CN CN202211399328.6A patent/CN115674806A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108248124A (en) * | 2018-01-30 | 2018-07-06 | 深圳市郎搏万先进材料有限公司 | A kind of pp cellular sandwich compound plates and preparation method thereof |
CN109849479A (en) * | 2019-01-29 | 2019-06-07 | 连云港市工业投资集团有限公司 | A kind of honeycomb type carbon fibre composite trim panel and preparation method thereof |
KR20210056813A (en) * | 2019-11-11 | 2021-05-20 | 디엘이앤씨 주식회사 | Impact load concentrated floor absorbing system |
CN216860863U (en) * | 2021-09-27 | 2022-07-01 | 上海骏珲新材料科技有限公司 | Solidified honeycomb multilayer material |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116039121A (en) * | 2023-02-15 | 2023-05-02 | 歌尔股份有限公司 | Carbon fiber-based composite part, preparation method thereof, spectacle frame and spectacles |
CN118124236A (en) * | 2024-05-07 | 2024-06-04 | 山东华特天维新材料有限公司 | Impact-resistant composite material sliding plate and preparation method thereof |
CN118124236B (en) * | 2024-05-07 | 2024-10-11 | 山东华特天维新材料有限公司 | Impact-resistant composite material sliding plate and preparation method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN115674806A (en) | Composite impact-resistant fork and preparation method thereof | |
US5279892A (en) | Composite airfoil with woven insert | |
US9534322B2 (en) | Fabric for carbon fiber reinforced composite material and method of manufacturing the same | |
US12179438B2 (en) | Semi-finished product and method for producing a structural component | |
CN108955385B (en) | Local reinforced composite material bulletproof helmet | |
CN107234818A (en) | A kind of High Performance Thermoplastic Composites pyramid and X-type dot-matrix sandwich panel and preparation method thereof | |
WO2022041358A1 (en) | Novel composite panel and production method therefor | |
CN105965989B (en) | A kind of preparation method of Carbon fibe reinforced resin composite material | |
CN105128357A (en) | Plate spring of interlayer reinforced two-dimensional/three-dimensional braided composite material and preparation method thereof | |
KR20040047837A (en) | Three-dimensional knit spacer fabric sandwich composite | |
CN108506393B (en) | A kind of bionic composite disc spring part and preparation method thereof | |
CN111890706A (en) | Laminated hybrid thermoplastic composite sheet prepreg structure, sheet and preparation method thereof | |
CN111844947A (en) | Novel equipment cabin plate and preparation method thereof | |
JP5036381B2 (en) | Fiber reinforced composite material | |
CN113696509B (en) | Integrated forming method of super-hybrid panel/three-dimensional woven hollow interlayer composite material | |
CN102514117B (en) | Carbon fiber enhanced polyphenylene sulfide composite material for automobile anticollision beam and method for manufacturing automobile anticollision beam | |
CN115716358A (en) | Bionic fiber composite material sandwich composite board and preparation method thereof | |
US5081861A (en) | Resin die for sheet metal pressing and method for producing same | |
JP5424549B2 (en) | Manufacturing method of fiber reinforced resin structure | |
CN206765397U (en) | A kind of fiber-reinforced composite deck board | |
CN212422241U (en) | Laminated hybrid thermoplastic composite plate pre-impregnation structure | |
CN101048276A (en) | Thin ply laminates | |
CN212979447U (en) | Novel composite board | |
CN217947586U (en) | Laminated hollow hybrid structure composite material fork | |
CN219171835U (en) | Combined type carbon fiber composite mechanical arm |
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 |