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CN102560808A - Weaving method of high-strength woven hollow-core reinforcer - Google Patents

Weaving method of high-strength woven hollow-core reinforcer Download PDF

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CN102560808A
CN102560808A CN2010105785062A CN201010578506A CN102560808A CN 102560808 A CN102560808 A CN 102560808A CN 2010105785062 A CN2010105785062 A CN 2010105785062A CN 201010578506 A CN201010578506 A CN 201010578506A CN 102560808 A CN102560808 A CN 102560808A
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surface layer
layer
hollow
core
woven
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周頔
吉庆
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Jiangnan University
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Jiangnan University
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Abstract

Disclosed is a forming method of a woven hollow-core reinforcer with the surface layer having multilayer structure. During weaving of the woven hollow-core reinforcer, a core portion is woven into a knotted warp hollow core which connects the upper surface layer and the lower surface layer. Meanwhile, the upper surface layer and the lower surface layer are woven into multiple fabric layers connected with a knotted warp attaching layer. The structure with multiple fabric layers parallel to each other includes that one or more groups of knotted warps of the surface layers run through vertically in the range of the upper surface layer or the lower surface layer in a slow warp feeding speed, and aims to densely connect the multiple fabric layers into the upper layer or the lower layer with a certain thickness and multiple knotted structure. To the core portion between the upper surface layer and the lower surface layer, the inner layers of the upper surface layer and the lower surface layer are connected by another one or more groups of knotted warps of the core portion in a faster warp feeding speed, so that the upper surface layer and the lower surface layer with multiple fabric layers are connected to form an integral spaced hollow-core structure integrally.

Description

一种高强机织空芯增强体的制织方法A Weaving Method of High Strength Woven Hollow Reinforcement

所属技术领域 Technical field

本发明涉及一种机织空芯增强体的形成方法,尤其是一种表面层为多层组织的机织空芯增强体的形成方法。The invention relates to a method for forming a woven hollow reinforcement, in particular to a method for forming a woven hollow reinforcement whose surface layer is multi-layered.

背景技术 Background technique

空芯机织物是一种三维结构的纺织品,通常用途是与树脂复合后形成空芯结构的板型复合材料,常用作轻质承力结构材料。它应用于复合材料领域能够一次完成与树脂基体的复合成型,不但简化了复合材料的后加工工艺,降低了生产成本,而且这种结构材料上下表面层之间是靠接结经和树脂共同联接,具有一定的整体高度,因此可改善复合材料的层间抗剪切能力。由于用作增强体时具有较好的整体机械性能,这种织物已成为研究方向。Hollow-core woven fabric is a three-dimensional structure of textiles. It is usually used to form a hollow-core structure composite material after being compounded with resin. It is often used as a lightweight load-bearing structural material. It is applied in the field of composite materials and can complete the composite molding with the resin matrix at one time, which not only simplifies the post-processing technology of composite materials, but also reduces the production cost, and the upper and lower surface layers of this structural material are jointly connected by joints and resin. , has a certain overall height, so it can improve the interlaminar shear resistance of the composite material. Such fabrics have been the subject of research due to their good overall mechanical properties when used as reinforcements.

目前,公知的机织空芯增强体的形成方法是上下两个系统的经纬纱各自交织形成织物的单层结构形式的上下层,接结经以一定的规律轮流出现在织物上下层,将织物上下层连接成整体空芯结构。At present, the formation method of the known woven hollow reinforcement is that the warp and weft yarns of the upper and lower systems are respectively interwoven to form the upper and lower layers of the single-layer structure of the fabric, and the binding warps appear in the upper and lower layers of the fabric in turn with a certain rule, and the fabric The upper and lower layers are connected to form a whole hollow structure.

例如,在专利CN2863826(一种玻璃纤维整体间隔机织物)中,提出了一种具有较大空芯高度和一定密度的玻璃钢用空芯机织物,其特点是,在织物的中间有连接经纱形成对左层织物和右层织物的“W”型的空芯连接。For example, in the patent CN2863826 (a kind of glass fiber integral spacer woven fabric), a hollow woven fabric for FRP with a relatively large hollow core height and a certain density is proposed, which is characterized in that there are connecting warps in the middle of the fabric to form a pair The "W"-shaped hollow connection of the left fabric and the right fabric.

在专利CN1297073(中空层连织物复合材料)中,提出了一种机织物为骨架的复合材料。该复合材料骨架由上层织物的经、纬纱交织形成该织物的上层;下层织物经、纬纱交织形成该织物的下层,然后有一组经纱与所述上、下层织物中的纬纱交织,并将所述的上、下层织物连接为一个整体织物。In the patent CN1297073 (hollow laminated fabric composite material), a composite material with a woven fabric as a skeleton is proposed. The composite material skeleton is formed by interweaving warp and weft yarns of the upper layer fabric to form the upper layer of the fabric; The upper and lower fabrics are connected as a whole fabric.

上述两专利有一共同的不足之处,即所形成的表面层都是单层织物组织,抗弯性能较差。因为在弯曲应力的作用下,应力由材料的上、下表面到中性层逐渐减小,而材料的上表面和下表面承受了较大的应力,这就限制了表面层为单层的织物的力学性能的提高,进而使织物及其复合材料的应用领域的拓展受到影响。The above two patents have a common disadvantage, that is, the formed surface layer is a single-layer fabric structure, and the bending resistance is relatively poor. Because under the action of bending stress, the stress gradually decreases from the upper and lower surfaces of the material to the neutral layer, while the upper and lower surfaces of the material bear greater stress, which limits the fabric with a single layer of surface layer. The improvement of the mechanical properties of the fabric and the expansion of the application fields of the fabric and its composite materials are affected.

如何提高空芯机织物及其复合材料的抗弯强度就成为生产中面临的研究课题。How to improve the flexural strength of hollow-core woven fabrics and their composite materials has become a research topic in production.

作为板材以及各种形态的梁,如工程结构材料中得到大量使用层合板、空芯夹层板,又如矩形、T字型、工字型、∏字型(铁路桥多用)和箱型截面梁等,对各机械强度,如拉伸强度、抗弯强度等都有着较高的要求。As plates and beams of various shapes, such as laminated panels and hollow sandwich panels are widely used in engineering structural materials, such as rectangular, T-shaped, I-shaped, ∏-shaped (multi-purpose for railway bridges) and box-shaped cross-section beams. etc., there are higher requirements for various mechanical strengths, such as tensile strength and bending strength.

由材料力学可知,一般地,材料的抗弯强度与其它的强度成正相关关系。于是,对材料的机械性能的提高的研究及讨论可用抗弯强度为代表,这和许多构件和产品,尤其是板材的使用状态相符,它们在使用中通常也都承受弯曲应力的作用。According to the mechanics of materials, in general, the flexural strength of a material is positively correlated with other strengths. Therefore, the research and discussion on the improvement of the mechanical properties of materials can be represented by the flexural strength, which is consistent with the use status of many components and products, especially plates, which are usually subjected to bending stress during use.

如何不断提高板状材料或型材的机械性能,一直是材料设计、生产和研究的追求,也出现了一些针对于此的技术方案。How to continuously improve the mechanical properties of plate materials or profiles has always been the pursuit of material design, production and research, and some technical solutions for this have also emerged.

例如,在专利CN1038613(高抗弯强度轻体芯板制造方法)中,提出了一种可预先制成大幅面板材的制造方法,这种材料是在芯层的两面分别铺以涂胶的竹筋网等材料,再经热压或冷压工艺,这样来提高抗弯强度的。For example, in the patent CN1038613 (manufacturing method of high bending strength light body core board), a kind of manufacturing method that can be made into a large-scale board in advance is proposed. Materials such as ribs and nets are subjected to hot pressing or cold pressing to improve the bending strength.

在专利CN1289285(层合酚醛树脂泡沫板及其制造方法)中,提供了一种纵向弯曲弹性模量和抗弯强度有所提高且挠曲性得到改进的酚醛树脂泡沫体层合板和它的适宜生产方法,该方法是将通过传送机的条纹状泡沫体在完全固化前沿前进方向被拉伸4-12%来达到的,这种拉伸本身就提高了材料的力学性能。In the patent CN1289285 (laminated phenolic resin foam board and its manufacturing method), a kind of longitudinal bending elastic modulus and bending strength are provided, and the phenolic resin foam laminated board and its suitable flexibility are improved. The production method is achieved by stretching the striped foam passing through the conveyor by 4-12% in the forward direction of the complete curing front, and this stretching itself improves the mechanical properties of the material.

在专利CN1344602(竹(木)板材的抗弯结构)中,提供了一种竹(木)板材抗弯结构,该方法是将通过在竹(木)板材抗弯结构设置有加强筋结构来达到的。In the patent CN1344602 (bending structure of bamboo (wood) plate), a kind of bending structure of bamboo (wood) plate is provided, and the method is to achieve of.

从上述的专利和生产实际中,可以看出抗弯强度的提高不但与材料本身的性能有关,而且与截面或材料空间分布有关。From the above patents and production practice, it can be seen that the improvement of the flexural strength is not only related to the performance of the material itself, but also related to the cross-section or the spatial distribution of the material.

在生产实际中,为提高空芯机织物的抗弯等机械强度,常用的改善方式为,在表面层都是单层织物组织的空芯机织物的上、下表面,在将织物与树脂复合成型的加工过程中,再叠合一层或更多层的普通结构的织物,以加厚表层组织。但这种方式的不足之处是层合成的制品在后续加工或使用中容易产生撕裂分层现象,这就影响了最终材料的整体性能和使用寿命。In actual production, in order to improve the mechanical strength of the hollow woven fabric such as bending resistance, the commonly used improvement method is to combine the fabric with resin on the upper and lower surfaces of the hollow woven fabric with a single-layer fabric structure. During the forming process, one or more layers of fabric of ordinary structure are laminated to thicken the surface tissue. However, the disadvantage of this method is that the laminated product is prone to tearing and delamination during subsequent processing or use, which affects the overall performance and service life of the final material.

发明内容 Contents of the invention

为了克服现有的空芯机织物中上下表面层为单层组织,从而影响该类织物增强的复合材料的抗弯性能的不足,或者,为了克服现有的空芯机织材料中上下表面层为层合结构,容易产生撕裂分层破坏的不足,本发明提供一种表面层为多层组织的机织空芯整体结构的形成方法。该方法所形成的织物上下表面层的厚度得到增加,从而提高了织物的力学性能,尤其是最终复合材料的力学性能。In order to overcome the deficiency that the upper and lower surface layers of the existing hollow-core woven fabrics are single-layer structures, which affect the bending resistance of this type of fabric-reinforced composite material, or, in order to overcome the upper and lower surface layers of the existing hollow-core woven materials As a laminated structure, it is easy to cause tearing and delamination damage. The invention provides a method for forming a woven hollow core integral structure with a surface layer of multi-layer structure. The thickness of the upper and lower surface layers of the fabric formed by the method is increased, thereby improving the mechanical properties of the fabric, especially the mechanical properties of the final composite material.

本发明解决其技术问题所采用的技术方案是:在机织空芯增强体的织造过程中就增加织物上、下表层的组成层数。即,无论是对上表层或下表层而言,均是由两个或两个以上系统的经纬纱交织形成数层互相平行的织物结构,并且,在整个组织循环中,这种数层互相平行的织物结构由一组或多组表层接结经以较慢的送经速度在上表层或下表层范围进行上下贯穿运动,目的将这数层织物紧密地连接成一个结构上为接结多层组织的具有一定整体厚度的上表层或下表层;同时,对于位处上表层和下表层之间的芯部而言,由另一组或多组芯部接结经以较快的送经速度对上下两表面层的内层进行连接,将上下两个已成多层结构的表面层连接成一个整体的间隔状态的空芯结构。The technical scheme adopted by the present invention to solve the technical problem is: in the weaving process of the woven hollow reinforcement, the number of layers of the upper and lower surface layers of the fabric is increased. That is to say, whether it is the upper surface layer or the lower surface layer, the warp and weft yarns of two or more systems are interwoven to form a fabric structure with several layers parallel to each other, and, in the entire weaving cycle, these layers are parallel to each other. The fabric structure consists of one or more sets of surface binding warps that move up and down on the upper or lower surface at a slower let-off speed, in order to tightly connect these layers of fabrics into a structurally multi-layered joint. The upper or lower surface of the tissue with a certain overall thickness; at the same time, for the core between the upper surface and the lower surface, another group or more groups of cores are bound by a faster let-off speed The inner layer of the upper and lower surface layers is connected, and the upper and lower two surface layers that have formed a multi-layer structure are connected to form a whole hollow core structure in a spaced state.

本发明解决其技术问题所采用的技术方案在材料力学理论上的根据是(以抗弯强度为性能指标的代表来讨论):合理设计及优化材料的截面形状来增大抗弯截面模量是提高弯曲强度的重要措施。因为结构材料的截面上的最大正应力

Figure BSA00000377680000021
其中,Mmax为最大弯矩,W称为截面图形的抗弯截面模量,W只与截面图形的几何性质有关。对于高为h,宽为b的矩形截面,抗弯截面模量
Figure BSA00000377680000022
因此可知,当材料所受最大弯矩Mmax不变时,材料的高度h越大,抗弯截面模量就W越大,截面上所受最大正应力σmax越小,也就提高了结构材料的抗弯强度。由此也可以看出,在外边缘达到许用应力时,中性轴附近的应力很小,为尽可能地避免材料的使用造成浪费,材料在结构设计时应尽可能往“上、下”分布,以增大高h。例如,对具有一定高度的矩形截面的板或梁来说,理想的情况是,将面积之半分布于距中性轴为h/2处,在结构上对中性轴距离越小处,耗用材料应越少。整体空芯板正是符合该设计原则。而本发明的解决其技术问题所采用的增加织物上下表层的层数的技术方案也正是该设计原则的进一步的运用。The technical solution adopted by the present invention to solve its technical problems is based on the theory of material mechanics (discussing as a representative of the performance index with the flexural strength): rationally designing and optimizing the cross-sectional shape of the material to increase the flexural section modulus is An important measure to improve the bending strength. Because the maximum normal stress on the cross-section of the structural material
Figure BSA00000377680000021
Among them, M max is the maximum bending moment, W is called the flexural section modulus of the cross-sectional figure, and W is only related to the geometric properties of the cross-sectional figure. For a rectangular section with height h and width b, the flexural section modulus
Figure BSA00000377680000022
Therefore, it can be seen that when the maximum bending moment M max of the material is constant, the greater the height h of the material, the greater the flexural section modulus W, and the smaller the maximum normal stress σ max on the section, which improves the structure. The flexural strength of the material. It can also be seen from this that when the outer edge reaches the allowable stress, the stress near the neutral axis is very small. In order to avoid material waste as much as possible, the material should be distributed as "up and down" as possible in the structural design , to increase the height h. For example, for a plate or beam with a rectangular section with a certain height, the ideal situation is to distribute half of the area at a distance of h/2 from the neutral axis, and the smaller the distance to the neutral axis in the structure, the less energy consumption Use less material. The overall hollow core board is in line with this design principle. And the technical scheme of increasing the number of layers of the upper and lower surface layers of the fabric adopted to solve the technical problems of the present invention is also the further application of this design principle.

本发明解决其技术问题所采用的技术方案在纺织技术上的实现性是:由上述的本发明的技术方案可知,要制成表面层为多层组织的机织空芯结构的织物,织机必须具备两个基本条件,一是具有多综框的分层织造技术,另一是具有多轴或多速送经技术,而现在的机织布机在机械结构及功能上,存在着能够完全满足所需的这两个基本条件的成熟技术。The realization of the technical solution adopted by the present invention to solve its technical problems in textile technology is: by the above-mentioned technical solution of the present invention, it can be known that the surface layer is to be made into a fabric with a woven hollow core structure of a multi-layer structure, and the loom Two basic conditions must be met, one is the layered weaving technology with multi-heald frames, and the other is multi-axis or multi-speed warp let-off technology. However, in terms of mechanical structure and function, the current woven looms have the ability to completely A proven technology that meets these two basic conditions required.

本发明的有益效果是,提供了一种表面层为多层组织的机织空芯结构的形成方法,增加了织物表面层的厚度,改善了织物及其与其它材料复合后的最终制品的抗弯、抗冲击等物理机械性能,拓展了其应用领域的范围,尤其有助于其向产业用领域的发展。The beneficial effect of the present invention is that it provides a method for forming a woven hollow structure whose surface layer is a multilayer structure, which increases the thickness of the fabric surface layer and improves the resistance of the fabric and its final product after it is compounded with other materials. The physical and mechanical properties such as bending and impact resistance have expanded the scope of its application field, especially helping its development to the industrial field.

附图说明 Description of drawings

下面结合附图和实施例对本发明进一步说明。The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

图1是本发明方法的实施例一的织物结构示意图。Fig. 1 is a schematic diagram of the fabric structure of Embodiment 1 of the method of the present invention.

图2是本发明方法的实施例一的织物结构的纵向横截面图。Fig. 2 is a longitudinal cross-sectional view of the fabric structure of Embodiment 1 of the method of the present invention.

图3是本发明方法的实施例一的各根经纱运动轨迹图。Fig. 3 is a diagram of the trajectory of each warp yarn in Embodiment 1 of the method of the present invention.

图4是本发明方法的实施例一的织物在多臂布机上的织造工艺图。Fig. 4 is a weaving process diagram of the fabric of Embodiment 1 of the method of the present invention on a dobby loom.

图5是本发明方法的实施例二的机织空芯增强体的纵向截面图。Fig. 5 is a longitudinal sectional view of the woven hollow reinforcement body according to the second embodiment of the method of the present invention.

图6是本发明方法的实施例三的机织空芯增强体的纵向截面图。Fig. 6 is a longitudinal cross-sectional view of the woven hollow reinforcement body according to the third embodiment of the method of the present invention.

图中1、2、3、10、11、12为上表面层经纱;4、5、6、13、14、15为下表面层经纱;7、16为上表面层连接经纱;8、17为下表面层连接经纱;9、18为空芯间隔连接经纱;A为上表层结构;C为下表层结构;B为芯部结构。Among the figure 1, 2, 3, 10, 11, 12 are upper surface layer warp yarns; 4, 5, 6, 13, 14, 15 are lower surface layer warp yarns; 7, 16 are upper surface layer connecting warp yarns; 8, 17 are The lower surface layer connects warp yarns; 9 and 18 are empty core spaced connecting warp yarns; A is the upper surface layer structure; C is the lower surface layer structure; B is the core structure.

具体实施方式 Detailed ways

实施例一:Embodiment one:

图1是本发明方法实施例一的织物结构示意图。织物在结构上由三部分组成,一是上表层结构A,由三层组织紧密地连接而成;二是下表层结构C,也由三层组织紧密地连接而成;三是芯部结构B,由芯部接结经以较快的送经速度对上下两表面层的内层进行空芯性连接形成,芯部接结经为V型连接。Fig. 1 is a schematic diagram of the fabric structure of the first embodiment of the method of the present invention. The fabric is composed of three parts in structure, one is the upper surface structure A, which is closely connected by three layers of tissue; the other is the lower surface structure C, which is also closely connected by three layers of tissue; the third is the core structure B , formed by the hollow connection of the inner layers of the upper and lower surface layers by the core binding warp at a faster warp let-off speed, and the core binding warp is a V-shaped connection.

图2是本发明方法实施例一的多根纱线组成织物结构的纵向横截面图。整个织物在结构上由18根纱线织成的三部分组成:上表层结构A、芯部结构B和下表层结构C。与图1所示的相对应,上表层结构A在组成上是再由三层组织通过上表面层连接经纱紧密地贴层连接而成的,下表层结构C在组成上也是再由三层组织通过下表面层连接经纱紧密地贴层连接而成,而芯部结构B由芯部接结经以较快的送经速度对上下两表面层的内层进行空芯性连接形成。Fig. 2 is a longitudinal cross-sectional view of a fabric structure composed of multiple yarns in Embodiment 1 of the method of the present invention. The whole fabric is structurally composed of three parts woven by 18 yarns: upper surface structure A, core structure B and lower surface structure C. Corresponding to that shown in Figure 1, the composition of the upper surface structure A is composed of three layers of weaves connected by the upper surface layer and the warp yarns are tightly attached to each other, and the composition of the lower surface structure C is also composed of three layers of weave It is formed by connecting the warp yarns of the lower surface layer closely, and the core structure B is formed by hollow connection of the inner layers of the upper and lower surface layers by the core binding warp at a faster let-off speed.

图3是本发明方法实施例一的经纱运动轨迹图,表示了各根经纱对纬纱的围绕或运动方式,这种围绕方式就构成了织物结构。因为在图2中,织物的纵向横截面图是由多根纱线共同组成的,因为纱线间存在着重叠,不易进行清楚的叙述,所以,以图3来准确清晰地表示。图中,各根经纱按布机上的穿综顺序排列。图3不但表示了本发明方法实施例一的各根纱线组成整体织物结构的详细结构方式,而且,这种方式也正是针对本发明方法实施例一的作为织机主要成布机件的综框的运动方式。图3中表示出:上表层经纱1、2、3、10、11、12形成上表层的三片组织,而上表层连接经纱7、16则形成对上表层的三片组织的贯穿式连接,将上表层的三片组织紧密地连成一体;相应地,下表层经纱4、5、6、13、14、15形成下表层的三片组织,而下表层连接经纱8、17则形成对下表层的三片组织的贯穿式连接,将下表层的三片组织紧密地连成一体;空芯间隔连接经纱9、18位于上、下表层之间,形成对上表层和下表层的空芯形式的连接,在织物结构上,形成上、下表层间的空芯部分。表层连接经纱7、8、16、17以相对于空芯间隔连接经纱9、18的较慢的速度进行送经。对图3的综合,就形成了图1、2所示的表面层为多层组织的机织空芯结构的织物。Fig. 3 is the locus diagram of the warp thread of the method embodiment 1 of the present invention, has shown each warp thread around or the mode of movement of weft yarn, and this kind of around mode has just constituted fabric structure. Because in Figure 2, the longitudinal cross-sectional view of the fabric is composed of multiple yarns, because there is overlap between the yarns, it is difficult to describe clearly, so it is accurately and clearly shown in Figure 3. In the figure, each warp yarn is arranged according to the drawing-in order on the loom. Fig. 3 has not only represented the detailed structural mode that each yarn of the present invention's method embodiment one forms the whole fabric structure, and, this mode is also exactly for the present invention's method embodiment one as the main fabric-forming mechanism of the loom Movement of the heald frame. Shown in Fig. 3: upper surface warp yarns 1, 2, 3, 10, 11, 12 form three tissue of upper surface, and upper surface connecting warp yarns 7, 16 then form the penetrating connection to the three tissue of upper surface, The three tissues of the upper surface are tightly connected into one; correspondingly, the warp yarns 4, 5, 6, 13, 14, and 15 of the lower surface form the three tissues of the lower surface, and the connecting warp yarns 8 and 17 of the lower surface form a pair of lower surface layers. The penetrating connection of the three pieces of tissue on the surface tightly connects the three pieces of tissue on the lower surface into one; the hollow core spacer connecting warp yarns 9 and 18 are located between the upper and lower surface layers, forming a hollow form for the upper surface layer and the lower surface layer The connection of the fabric structure forms a hollow part between the upper and lower skins. The surface layer connecting warp yarns 7, 8, 16, 17 are let off at a slower speed than the hollow space connecting warp yarns 9, 18. The synthesis of Fig. 3 has just formed the fabric of the woven hollow core structure that the surface layer shown in Fig. 1, 2 is a multi-layer structure.

图4是本发明方法实施例一的织物在多臂布机上的织造工艺图。图4中的左图表示了实施例一中的各根经纱的穿综图,采用18页综框,18根经纱从左至右1、2、3等顺序地穿综。图4中的右图表示了实施例一中控制多臂机构的纹版图。穿综图和纹版图是织造的最主要的工艺技术图纸,是实现织物特定组织结构的关键,按工艺图对织机进行相应的技术设置,就可织造出相应的织物。Fig. 4 is a weaving process diagram of the fabric of the method embodiment 1 of the present invention on the dobby loom. The left figure in Fig. 4 shows the drawing-in diagram of each warp yarn in embodiment one, adopts 18 pages of heald frames, and 18 warp yarns are drawn in order from left to right 1, 2, 3, etc. The right figure in Fig. 4 shows the pattern pattern of the control dobby mechanism in the first embodiment. The drafting diagram and pattern diagram are the most important technical drawings for weaving, and are the key to realizing the specific structure of the fabric. The corresponding technical settings of the loom can be made according to the technical diagram, and the corresponding fabric can be woven.

上述4个图完整地表示了本发明的实施例一的织物结构和织造技术。The above four figures completely represent the fabric structure and weaving technology of Embodiment 1 of the present invention.

实施例二:Embodiment two:

图5是本发明方法的实施例二的机织空芯结构的纵向截面图,表示了形成的是表面层为三层组织,芯部接结经为W型连接的机织空芯结构。其中,图5的左图中,上表层经纱1、2、3、10、11、12与纬纱交织形成上表面层的三层互相平行的织物,下表层经纱4、5、6、13、14、15与纬纱交织形成下表面层的三层互相平行的织物;上表层接结经7、11一隔一轮流贯穿于上表面层的最上层和最下层,下表层接结经8、17一隔一轮流贯穿于下表面层的最上层和最下层,也如图5的中图所示,形成紧密的上下表面层的接结三层组织;空芯间隔连接经纱9、18以W型规律轮流出现在上下表面层的最内层,如图5中的右图所示,将上下表面层的内层组织连接起来,如此,形成整体间隔空芯结构。Fig. 5 is a longitudinal sectional view of the woven hollow structure of the second embodiment of the method of the present invention, showing that the surface layer is a three-layer structure, and the core is connected by a W-shaped woven hollow structure. Wherein, in the left figure of Fig. 5, the upper surface layer warp yarns 1, 2, 3, 10, 11, 12 are interwoven with the weft yarns to form three layers of parallel fabrics on the upper surface layer, and the lower surface layer warp yarns 4, 5, 6, 13, 14 , 15 interweaves with weft yarns to form three layers of fabric parallel to each other on the lower surface layer; the upper surface layer binding warp 7, 11 runs through the uppermost layer and the lowermost layer of the upper surface layer alternately, and the lower surface layer binding warp 8, 17- It runs through the uppermost layer and the lowermost layer of the lower surface layer alternately, as shown in the middle figure of Figure 5, forming a tight three-layer structure of the upper and lower surface layers; the hollow cores connect the warp yarns 9 and 18 in a W-shaped pattern They appear in the innermost layer of the upper and lower surface layers in turn, as shown in the right figure in Figure 5, connecting the inner layers of the upper and lower surface layers, thus forming an overall spaced hollow core structure.

图5的实施例二与图1-图4的实施例一的主要区别在于芯部接结经的连接形式不同,实施例一为V型连接,而实施例二为W型连接,在实现及技术上属同一类的,其叙述类同,故从略。The main difference between the second embodiment of Fig. 5 and the first embodiment of Figs. Those that belong to the same category technically have similar descriptions, so they are omitted.

实施例三:Embodiment three:

图6是本发明方法的实施例三的机织空芯增强体的纵向截面图。图6中左图表示的是表面层为二层组织,芯部接结经为V型连接的机织空芯结构。上表层经纱1、2、10、11与纬纱交织形成上表面层的二层互相平行的织物,下表层经纱4、5、13、14与纬纱交织形成下表面层的二层互相平行的织物,上表层接结经7、11一隔一轮流贯穿于上表面层的最上层和最下层,下表层接结经8、17一隔一轮流贯穿于下表面层的最上层和最下层,也如图6的中图所示,形成紧密的上下表面层的接结二层组织;空芯间隔连接经纱9、18以V型规律轮流出现在上下表面层的最内层,如图6中的右图所示,将上下表面层的内层组织连接起来,如此,形成整体间隔空芯结构的织物。Fig. 6 is a longitudinal cross-sectional view of the woven hollow reinforcement body according to the third embodiment of the method of the present invention. The left figure in Fig. 6 shows a woven hollow core structure in which the surface layer is a two-layer structure and the core joint is V-shaped. Upper surface warp yarns 1, 2, 10, 11 interweave with weft yarns to form two layers of parallel fabrics on the upper surface layer, and lower surface layer warp yarns 4, 5, 13, 14 interweave with weft yarns to form two layers of parallel fabrics on the lower surface layer, The junction of the upper surface layer runs through the uppermost layer and the lowermost layer of the upper surface layer through 7 and 11 alternately, and the junction of the lower surface layer passes through the uppermost layer and the lowermost layer of the lower surface layer through 8 and 17 alternately. As shown in the middle figure of Fig. 6, a tight joint two-layer structure of the upper and lower surface layers is formed; the hollow-core interval connecting warp yarns 9 and 18 appear in the innermost layer of the upper and lower surface layers in turn in a V-shaped pattern, as shown on the right in Fig. 6 As shown in the figure, the inner layers of the upper and lower surface layers are connected, so that a fabric with an integral spaced hollow core structure is formed.

图6的实施例三与图1-图4的实施例一的主要区别在于上下表面层的层数不同,实施例一的上下表面层的层数为3层,而实施例三的上下表面层的层数为2层,在实现及技术上的叙述类同,故从略。The main difference between embodiment three of Fig. 6 and embodiment one of Fig. 1-Fig. 4 is that the number of layers of the upper and lower surface layers is different. The number of layers is 2, and the descriptions in terms of implementation and technology are similar, so they are omitted.

Claims (8)

1. a high-strength woven hollow strengthens the weaving method of body, it is characterized in that: core is woven as access node when hollow connects up and down two superficial layers, and two superficial layers itself are woven into access node through multilayer tissue that paste layer connects up and down.
2. formation method according to claim 1 is characterized in that: the tissue that constitutes the upper and lower surfaces layer can adopt any monolayer organization.
3. high-strength woven hollow according to claim 1 strengthens the weaving method of body, it is characterized in that: upper surface layer or undersurface layer are carried out access node that paste layer connects through weaving motion with the mode that runs through upper surface layer or undersurface layer.
4. high-strength woven hollow according to claim 1 strengthens the weaving method of body, it is characterized in that: the core access node connects through the internal layer of two superficial layers is up and down carried out hollow.
5. high-strength woven hollow according to claim 1 strengthens the weaving method of body, it is characterized in that: the core access node connects through with the V-type motion mode two superficial layers up and down being carried out hollow.
6. high-strength woven hollow according to claim 1 strengthens the weaving method of body, it is characterized in that: the core access node connects through with W type motion mode two superficial layers up and down being carried out hollow.
7. high-strength woven hollow according to claim 1 strengthens the weaving method of body, it is characterized in that: the access node of upper surface layer or undersurface layer is through carrying out the paste layer connection with the V-type motion mode to upper surface layer or undersurface layer.
8. high-strength woven hollow according to claim 1 strengthens the weaving method of body, it is characterized in that: the access node of upper surface layer or undersurface layer is through carrying out the paste layer connection with W type motion mode to upper surface layer or undersurface layer.
CN2010105785062A 2010-12-08 2010-12-08 Weaving method of high-strength woven hollow-core reinforcer Pending CN102560808A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103171175A (en) * 2013-04-08 2013-06-26 漯河天英材料高科有限公司 Composite component unit with delamination resistance and composite containing same
CN106012237A (en) * 2016-08-14 2016-10-12 谢强 3d interval woven fabric
CN106467991A (en) * 2015-08-18 2017-03-01 浙江英诺威纺织有限公司 A kind of hollow double wall inflation tatting base fabric and its method for weaving
CN108697054A (en) * 2016-02-22 2018-10-23 M·布罗瓦 Drainage element for plants and its use
CN111886307A (en) * 2018-03-02 2020-11-03 塞托普拉特胶带技术有限公司 Adhesive tape

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103171175A (en) * 2013-04-08 2013-06-26 漯河天英材料高科有限公司 Composite component unit with delamination resistance and composite containing same
CN103171175B (en) * 2013-04-08 2015-12-16 漯河君叁材料高科有限公司 There is the composite element unit of anti-hierarchical nature and contain this unit composite
CN106467991A (en) * 2015-08-18 2017-03-01 浙江英诺威纺织有限公司 A kind of hollow double wall inflation tatting base fabric and its method for weaving
CN106467991B (en) * 2015-08-18 2018-05-01 浙江英诺威纺织有限公司 A kind of hollow double wall inflation tatting base fabric and its method for weaving
CN108697054A (en) * 2016-02-22 2018-10-23 M·布罗瓦 Drainage element for plants and its use
CN106012237A (en) * 2016-08-14 2016-10-12 谢强 3d interval woven fabric
CN111886307A (en) * 2018-03-02 2020-11-03 塞托普拉特胶带技术有限公司 Adhesive tape

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Application publication date: 20120711