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CN114770973A - Bending and torsion-resistant composite molding method and production line for polygonal composite cylinder with long inner ribs - Google Patents

Bending and torsion-resistant composite molding method and production line for polygonal composite cylinder with long inner ribs Download PDF

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Publication number
CN114770973A
CN114770973A CN202210251322.8A CN202210251322A CN114770973A CN 114770973 A CN114770973 A CN 114770973A CN 202210251322 A CN202210251322 A CN 202210251322A CN 114770973 A CN114770973 A CN 114770973A
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layer
fiber
polygonal
layup
fiber cloth
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CN114770973B (en
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张玉井
孙以泽
孟婥
李诗肄
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Donghua University
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • B29C70/32Shaping 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 on a rotating mould, former or core
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • B29C70/34Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/347Shaping 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 combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/523Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement in the die
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545Perforating, cutting or machining during or after moulding

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

The invention provides a bending and twisting resistant composite molding method for a polygonal composite material cylinder. The invention provides a bending-torsion-resistant composite forming production line for a polygonal composite material cylinder, which is characterized by comprising the following steps of: a core mold pulling system; a fiber cloth guide device; a middle layer yarn guiding plate device; a winding device; a ply yarn guiding plate device; a first weaving mechanism; a layer laying mechanism; a second weaving mechanism; a grease injection and curing system; a molded composite product traction device; and a cutting device. In the invention, the polygonal cylinder and the rib plate are formed by pultrusion at one time, so that the production efficiency is high and the labor cost is low; the polygonal barrel adopts a composite molding process of mixed weaving, layer yarn layering, winding yarn and fiber cloth layering, so that the mechanical properties of the barrel, such as axial strength, ring stiffness, bending resistance, torsion resistance, shear resistance and the like, are greatly improved; the transition area between adjacent rib plates adopts the pultrusion process of fiber cloth and ply yarn, so that the connection strength of the rib plates and the cylinder body is increased.

Description

带长内筋的多边型复材筒体抗弯扭复合成型方法及生产线Bending-torsion-resistant composite molding method and production line for polygonal composite cylinder with long inner ribs

技术领域technical field

本发明涉及一种具有长内筋的多边形复材筒体抗弯扭复合成型方法及基于该复合成型方法的具有长内筋的多边形复材筒体抗弯扭复合成型生产线。其中,长内筋指筒体在横截面内侧具有较长突出加强筋形状,加强筋尺寸与筒体横截面尺寸在同一数量级上;多边形指四边形、五边形、六边形、八边形等几何外形;复材指以碳纤维/玻璃纤维等为加强纤维、树脂等为基体复合而成型的复合材料。The invention relates to a bending and torsion-resistant composite molding method for a polygonal composite cylinder with long inner ribs and a bending-torsion-resistant composite molding production line for a polygonal composite cylinder with long inner ribs based on the composite molding method. Among them, the long inner rib means that the cylinder has a long protruding reinforcing rib shape on the inner side of the cross section, and the size of the reinforcing rib is on the same order of magnitude as the cross-sectional size of the cylinder; polygon refers to quadrilateral, pentagon, hexagon, octagon, etc. Geometric shape; composite material refers to a composite material formed by compounding carbon fiber/glass fiber as reinforcing fiber and resin as matrix.

背景技术Background technique

为特殊需求,在市政工程、电力通信、建筑给排水等行业常用到多边型筒体,为加强结构、提高抗弯抗扭性能,常在筒体内壁设计长条状筋板。在国防军工中,筒体内壁的长条状筋板还可作为导轨,筒体内部可以通过导轨输送物资或装置,所以制造具有足够强度、使用寿命和可靠性的带有长条状内筋的多边型筒体十分重要。For special needs, polygonal cylinders are often used in municipal engineering, power communication, building water supply and drainage and other industries. In order to strengthen the structure and improve the bending and torsion resistance, long strip-shaped rib plates are often designed on the inner wall of the cylinder. In the national defense industry, the long rib plate on the inner wall of the cylinder can also be used as a guide rail, and materials or devices can be transported through the guide rail inside the cylinder. The polygonal cylinder is very important.

目前多边型筒体大多采用金属材料制成,金属材料质量大,筒体内部结构复杂、加工难度大。随着碳纤维、玻璃纤维等高性能纤维的快速发展,其强度大、质量轻的优点近年来逐渐应用于筒体的制备。高性能纤维复合材料制备工艺多样且复杂,很多产品依旧停留在需要大量人力的阶段。At present, most of the polygonal cylinders are made of metal materials. The metal materials are of high quality, the internal structure of the cylinder is complex, and the processing is difficult. With the rapid development of high-performance fibers such as carbon fiber and glass fiber, their advantages of high strength and light weight have been gradually applied to the preparation of cylinders in recent years. The preparation process of high-performance fiber composite materials is diverse and complex, and many products are still at the stage that requires a lot of manpower.

当前在利用高性能纤维制备带导轨筒体时,通常将筒体和长条状筋板分开成型,筒体采用碳纤维轴纱拉挤工艺,长条状筋板采用碳纤维预浸料手糊铺层工艺,两者成型后采用胶粘连接。上述工艺方式存在以下不足:①筒体与长条状筋板分开成型再组装的方式生产效率低,碳纤维预浸料手糊铺层工艺人工成本高;②筒体采用碳纤维轴纱拉挤工艺,制件易分层、不抗剪;③采用胶粘工艺无法保证长条状筋板和筒体的形位误差,有时胶粘后还需要再加工。At present, when using high-performance fibers to prepare a cylinder with a guide rail, the cylinder and the long rib are usually formed separately. The cylinder adopts the carbon fiber shaft yarn pultrusion process, and the long rib adopts the carbon fiber prepreg hand lay-up layer. process, the two are connected by glue after forming. The above-mentioned process has the following shortcomings: 1. The method of forming and reassembling the cylinder body and the elongated rib plate separately is low in production efficiency, and the labor cost of the carbon fiber prepreg hand lay-up process is high; 2. The cylinder body adopts the carbon fiber shaft yarn pultrusion process, The parts are easy to be delaminated and not shear resistant; 3. The shape and position error of the long rib plate and the cylinder cannot be guaranteed by the gluing process, and sometimes it needs to be reprocessed after gluing.

发明内容SUMMARY OF THE INVENTION

本发明的目的是:提供一种能够确保筒体与长条状内筋连接强度且生产效率较高的具有长条状内筋的多边形复合材料筒体的成型工艺以及成型生产线。The purpose of the present invention is to provide a molding process and a molding production line for a polygonal composite material cylinder with elongated inner ribs, which can ensure the connection strength between the cylinder and the elongated inner ribs and has high production efficiency.

为了达到上述目的,本发明的一个技术方案是提供了一种多边形复合材料筒体抗弯扭复合成型方法,采用多边形芯模,多边形芯模的多个角部分别有多个用于成型长条状内筋的长沟槽,其特征在于,复合成型方法包括以下步骤:In order to achieve the above purpose, a technical solution of the present invention is to provide a method for forming a polygonal composite material cylinder with anti-bending and torsion. A polygonal core mold is used, and a plurality of corners of the polygonal core mold are respectively used for forming long strips. The long groove of the inner rib is characterized in that, the composite molding method comprises the following steps:

在多边形芯模的外表面包覆纤维布,形成纤维布层;The outer surface of the polygon core mold is covered with fiber cloth to form a fiber cloth layer;

在纤维布层外侧铺铺层纱形成内层纤维铺层;Lay layup yarns on the outside of the fiber cloth layer to form an inner fiber layup;

将缠绕纱线旋转缠绕到内层纤维铺层外侧,形成缠绕层;Rotate the winding yarn to the outside of the inner fiber layer to form a winding layer;

在缠绕层外侧铺铺层纱形成中间纤维铺层;Lay layup yarns on the outside of the winding layer to form an intermediate fiber layup;

在中间纤维铺层外侧编织形成内层编织层;Weaving on the outside of the intermediate fiber layup to form an inner braided layer;

在内层编织层外侧铺铺层纱形成外侧纤维铺层;Lay layup yarns on the outside of the inner braid to form an outside fiber layup;

在外侧纤维铺层外侧编织形成外层编织层;Weaving on the outside of the outer fiber layup to form an outer braided layer;

在边型芯模外形成由纤维布层、内层纤维铺层、缠绕层、中间纤维铺层、内层编织层、外侧纤维铺层及外层编织层组成的七层混合结构预成型体,在该七层混合结构预成型体中,仅纤维布层及内层纤维铺层位于长条状内筋位置;将包覆有七层混合结构预成型体的多边形芯模被送入外模后,进行高压注脂及固化成型,成型后的产品被不断拉出,每拉出一段距离后,切割得到成型产品。A seven-layer hybrid structure preform consisting of fiber cloth layer, inner fiber layup, winding layer, middle fiber layup, inner braided layer, outer fiber layup and outer braided layer is formed outside the side core mold. In the seven-layer hybrid structure preform, only the fiber cloth layer and the inner layer fiber layup are located at the position of the long strip; the polygonal core mold covered with the seven-layer hybrid structure preform is sent to the outer mold. , carry out high pressure grease injection and curing molding, the molded product is continuously pulled out, and after each pull out for a certain distance, the molded product is obtained by cutting.

优选地,所述七层混合结构预成型体的厚度能够根据需要调节。Preferably, the thickness of the seven-layer hybrid structure preform can be adjusted as required.

本发明的另一个技术方案是提供了一种多边形复合材料筒体抗弯扭复合成型生产线,其特征在于,包括:Another technical solution of the present invention is to provide a polygonal composite material cylinder body bending and torsion-resistant composite molding production line, which is characterized in that, comprising:

芯模牵引系统,用于将多边形芯模推送入外模中;Mandrel pulling system for pushing the polygonal mandrel into the outer mold;

纤维布导向装置,用于将纤维布包覆在多边形芯模的外表面,形成纤维布层;Fiber cloth guiding device, used to wrap the fiber cloth on the outer surface of the polygonal core mold to form a fiber cloth layer;

中间铺层纱引导板装置,用于将铺层纱铺在纤维布层外侧,形成内层纤维铺层;The middle layer yarn guide plate device is used to lay the layer yarn on the outside of the fiber cloth layer to form the inner layer fiber layer;

缠绕装置,用于将缠绕纱线旋转缠绕到内层纤维铺层外侧,形成缠绕层;Winding device, used to rotate the winding yarn to the outside of the inner fiber layer to form a winding layer;

铺层纱引导板装置,用于将铺层纱铺在缠绕层外侧,形成中间纤维铺层;The layered yarn guide plate device is used to lay the layered yarn on the outside of the winding layer to form an intermediate fiber layer;

编织机构一,用于在中间纤维铺层外侧编织形成内层编织层;The first weaving mechanism is used to weave the outer side of the intermediate fiber layup to form the inner braided layer;

铺层机构,用于将铺层纱铺在内层编织层外侧,形成外侧纤维铺层;The layering mechanism is used to lay the layered yarn on the outside of the inner braid to form the outer fiber layer;

编织机构二,用于在外侧纤维铺层外侧编织形成外层编织层;The second weaving mechanism is used to weave the outer layer of the outer fiber layer to form an outer layer of braided layer;

注脂固化系统,用于进行高压注脂及固化成型;Grease injection curing system, used for high pressure grease injection and curing molding;

成型复合材料产品牵引装置,用于将注脂固化系统获得的成型后的产品不断拉出;The forming composite material product pulling device is used to continuously pull out the formed product obtained by the grease injection curing system;

切割装置,每拉出一段距离后,利用切割装置切割得到成型产品。The cutting device is used to cut a shaped product after pulling out a certain distance.

优选地,还包括芯模支撑架,用于在推送过程中支撑多边形芯模。Preferably, a mandrel support frame is also included for supporting the polygonal mandrel during the pushing process.

优选地,所述编织机构一、所述铺层机构以及所述编织机构二为各自独立的机构;或者所述编织机构一、所述铺层机构以及所述编织机构二集成在带铺层混合编织机内;或者所述编织机构一及所述编织机构二集成在三维编织机内。Preferably, the knitting mechanism 1, the laying mechanism and the knitting mechanism 2 are independent mechanisms; or the knitting mechanism 1, the laying mechanism and the knitting mechanism 2 are integrated in the belt-laying hybrid In the knitting machine; or the knitting mechanism 1 and the knitting mechanism 2 are integrated in the three-dimensional knitting machine.

优选地,所述纤维布导向装置由四个渐变收缩的异型板材组合而成,异型板材沿周向均匀布置;Preferably, the fiber cloth guiding device is composed of four special-shaped plates with gradual shrinkage, and the special-shaped plates are evenly arranged along the circumferential direction;

每个渐变收缩的异型板材为薄型空间曲面体,该薄型空间曲面体的一端横截面形状为多个周向均布的薄型直板,另一端横截面形状为多个分离的与最终纤维布层的成型形状一致的薄型弯板;薄型空间曲面体的中间为圆滑过渡区域,薄型空间曲面体两端通过该圆滑过渡区域实现圆滑过渡;薄型空间曲面体一端的薄型直板与另一端的薄型弯板的长度相等;Each gradient-shrinking special-shaped sheet is a thin space curved body, one end of the thin space curved body is a plurality of circumferentially evenly distributed thin straight plates, and the other end is a plurality of separate and final fiber cloth layers. Consistent thin curved plate; the middle of the thin space curved body is a smooth transition area, and the two ends of the thin space curved body realize a smooth transition through the smooth transition area; the thin straight plate at one end of the thin space curved body and the thin curved plate at the other end have the same length ;

纤维布根据多边形形状分为多卷,分别铺设在薄型直板上,随着拉挤的进给,纤维布由薄型直板端逐渐经圆滑过渡区域变化并满铺到薄型弯板端表面,从而使纤维布铺成所需形状。The fiber cloth is divided into multiple rolls according to the polygonal shape, which are respectively laid on the thin straight plate. With the feeding of the pultrusion, the fiber cloth gradually changes from the thin straight plate end through the smooth transition area and is fully spread to the thin curved plate end surface, so that the fiber Spread the cloth into the desired shape.

本发明具有如下有益效果:The present invention has the following beneficial effects:

(1)多边型筒体和筋板一次拉挤成型,生产效率高、人工成本低。(1) One-time pultrusion molding of polygonal cylinder and ribs, with high production efficiency and low labor cost.

(2)多边型筒体采用混合编织+铺层纱+缠绕纱+纤维布铺层的复合成型工艺,大大提高了筒体轴向强度、环刚度、抗弯、抗扭、抗剪等力学性能。(2) The polygonal cylinder body adopts the composite molding process of mixed weaving + laying yarn + winding yarn + fiber cloth laying, which greatly improves the mechanical properties of the cylinder body such as axial strength, ring stiffness, bending resistance, torsion resistance, shear resistance, etc. .

(3)相邻筋板间的过渡区域采用纤维布+铺层纱的拉挤工艺,增大了筋板与筒体本体的连接强度。(3) The transition area between adjacent ribs adopts the pultrusion process of fiber cloth + layered yarn, which increases the connection strength between the ribs and the cylinder body.

附图说明Description of drawings

图1为实施例中公开的生产线示意图;Fig. 1 is the production line schematic diagram disclosed in the embodiment;

图2为所使用的多边形芯模的结构示意图;Fig. 2 is the structural representation of the polygon core mold used;

图3为最终获得的产品的截面图;Figure 3 is a sectional view of the final product obtained;

图4为图3中Ⅰ部分的放大示意图;Fig. 4 is the enlarged schematic diagram of part I in Fig. 3;

图5为图3中Ⅱ部分的放大示意图;Fig. 5 is the enlarged schematic diagram of part II in Fig. 3;

图6为空间异形导向结构的正面结构示意图;Fig. 6 is the front structure schematic diagram of the space special-shaped guide structure;

图7为空间异形导向结构的侧面结构示意图。FIG. 7 is a schematic side view of the spatial special-shaped guide structure.

具体实施方式Detailed ways

下面结合具体实施例,进一步阐述本发明。应理解,这些实施例仅用于说明本发明而不用于限制本发明的范围。此外应理解,在阅读了本发明讲授的内容之后,本领域技术人员可以对本发明作各种改动或修改,这些等价形式同样落于本申请所附权利要求书所限定的范围。The present invention will be further described below in conjunction with specific embodiments. It should be understood that these examples are only used to illustrate the present invention and not to limit the scope of the present invention. In addition, it should be understood that after reading the content taught by the present invention, those skilled in the art can make various changes or modifications to the present invention, and these equivalent forms also fall within the scope defined by the appended claims of the present application.

本实施例公开了一种具有长条状内筋的多边形复合材料筒体抗弯扭复合成型方法,采用多边形芯模2,多边形芯模2的多个角部分别有多个用于成型长条状内筋的长沟槽,则复合成型方法具体包括以下步骤:This embodiment discloses a method for bending and torsion-resistant composite molding of a polygonal composite material cylinder with elongated inner ribs. A polygonal core mold 2 is used, and multiple corners of the polygonal core mold 2 are respectively used for forming long strips. If the long groove of the inner rib is formed, the composite molding method specifically includes the following steps:

由芯模牵引系统1将多边形芯模2推送入外模中,在推送过程中:The polygonal mandrel 2 is pushed into the outer mold by the mandrel pulling system 1. During the pushing process:

步骤1、纤维布3通过纤维布导向装置4包覆在多边形芯模2的外表面,形成纤维布层A,为第一层;Step 1. The fiber cloth 3 is wrapped on the outer surface of the polygonal core mold 2 through the fiber cloth guide device 4 to form a fiber cloth layer A, which is the first layer;

步骤2、通过中间铺层纱引导板装置5将放置在铺层纱架6上的第一部分铺层纱铺在纤维布层A外侧,形成内层纤维铺层B,为第二层;Step 2, laying the first part of the layup yarn placed on the layup creel 6 on the outer side of the fiber cloth layer A through the intermediate layup yarn guide plate device 5 to form the inner layer fiber layup layer B, which is the second layer;

步骤3、缠绕装置7将缠绕纱线旋转缠绕到内层纤维铺层B外侧,形成缠绕层C,为第三层;Step 3, the winding device 7 rotates the winding yarn to the outside of the inner fiber layer B to form the winding layer C, which is the third layer;

步骤4、通过铺层纱引导板装置8将放置在铺层纱架6上的第二部分铺层纱铺在缠绕层C外侧,形成中间纤维铺层D,为第四层;Step 4, laying the second part of the layup yarn placed on the layup creel 6 on the outside of the winding layer C through the layup yarn guide plate device 8 to form an intermediate fiber layup D, which is the fourth layer;

步骤5、利用带铺层混合编织机9的内圈锭子在中间纤维铺层D外侧编织形成内层编织层E,为第五层;Step 5, using the inner ring spindle of the hybrid braiding machine 9 with a layer to weave on the outer side of the intermediate fiber layer D to form an inner layer braid E, which is the fifth layer;

步骤6、利用带铺层混合编织机9的中间铺层将将放置在铺层纱架6上的第二部分铺层纱铺在内层编织层E外侧,形成外侧纤维铺层F,为第六层;Step 6. Use the middle layer of the hybrid braiding machine 9 with the layer to lay the second part of the lay-up yarn placed on the lay-up creel 6 on the outside of the inner woven layer E to form the outer fiber lay-up layer F, which is the first six layers;

步骤7、利用带铺层混合编织机9的外圈锭子在外侧纤维铺层F外侧编织形成外层编织层G,为第七层;Step 7, using the outer ring spindle of the hybrid braiding machine 9 with a layer to weave on the outer side of the outer fiber layer F to form an outer braid G, which is the seventh layer;

由此,在多边形芯模2外形成由纤维布层A、内层纤维铺层B、缠绕层C、中间纤维铺层D、内层编织层E、外侧纤维铺层F及外层编织层G组成的七层混合结构预成型体,在该七层混合结构预成型体中,仅纤维布层A及内层纤维铺层B位于长条状内筋位置;将包覆有七层混合结构预成型体的多边形芯模2被送入外模后,利用注脂固化系统10进行高压注脂及固化成型,成型后的产品11通过成型复合材料产品牵引装置12不断拉出,每拉出一段距离后,利用切割装置13切割得到成型产品,从而获得具有一定长度的最终产品。As a result, a fiber cloth layer A, an inner fiber layer B, a winding layer C, an intermediate fiber layer D, an inner woven layer E, an outer fiber layer F, and an outer woven layer G are formed outside the polygonal core mold 2. The seven-layer hybrid structure preform is composed, in the seven-layer hybrid structure preform, only the fiber cloth layer A and the inner layer fiber laying layer B are located at the position of the long strip; After the polygonal core mold 2 of the molded body is sent into the outer mold, the grease injection and curing system 10 is used to perform high-pressure grease injection and curing molding. Then, the shaped product is obtained by cutting by the cutting device 13, so as to obtain the final product with a certain length.

在上述方法中,可以根据需要调节七层混合结构预成型体的厚度;带铺层混合编织机9也可以是三维编织机或普通单层编织机。在所得到的最终产品中,最内层的多块纤维布在筋板根部与多边形筒体内表面形成了完整的加强层,可显著加强筒体内长条状内筋根部抗弯性和整体抗扭性。In the above method, the thickness of the seven-layer hybrid structure preform can be adjusted as required; the hybrid braiding machine 9 with layers can also be a three-dimensional braiding machine or a common single-layer braiding machine. In the final product obtained, the innermost fiber cloth forms a complete reinforcing layer at the root of the rib plate and the inner surface of the polygonal cylinder, which can significantly enhance the bending resistance and overall torsion resistance of the long strip inner rib in the cylinder. sex.

本发明提供的一种具有长条状内筋的多边形复合材料筒体抗弯扭复合成型生产线,采用上述复合成型方法,除包括芯模牵引系统1、多边形芯模2、纤维布导向装置4、中间铺层纱引导板装置5、铺层纱架6、缠绕装置7、铺层纱引导板装置8、带铺层混合编织机9、注脂固化系统10、成型复合材料产品牵引装置12及切割装置13外,还包括:The present invention provides a production line for bending and torsion-resistant composite molding of polygonal composite material cylinders with long inner ribs. The composite molding method described above is adopted, except that it includes a core mold traction system 1, a polygonal core mold 2, a fiber cloth guide device 4, Middle layup yarn guide plate device 5, layup creel 6, winding device 7, layup yarn guide plate device 8, belt layup hybrid braiding machine 9, grease injection curing system 10, forming composite material product pulling device 12 and cutting In addition to device 13, it also includes:

芯模支撑架14,用于在推送过程中支撑多边形芯模2。The mandrel support frame 14 is used to support the polygonal mandrel 2 during the pushing process.

本实施例中,由于筒体结构复杂,最内层的碳布层铺设难度较大,纤维布导向装置4设计采用特殊空间异形导向结构,由4个渐变收缩的异型板材4-1组合而成,异型板材4-1沿周向均匀布置。该渐变收缩的异型板材4-1为薄板经冲压/折弯等加工而成的薄型空间曲面体。该薄型空间曲面体的一端横截面形状为多个周向均布的薄型直板,另一端横截面形状为多个分离的与最终纤维布层A的成型形状一致的薄型弯板。薄型空间曲面体的中间为圆滑过渡区域,薄型空间曲面体两端通过该圆滑过渡区域实现圆滑过渡。薄型空间曲面体一端的薄型直板与另一端的薄型弯板的长度相等。纤维布3根据多边形形状分为多卷,分别铺设在薄型直板上,随着拉挤的进给,由薄型直板端逐渐经圆滑过渡区域变化并满铺到薄型弯板端表面。通过这样的引导区域,可使纤维布3顺利铺成所需形状。In this embodiment, due to the complex structure of the cylinder body, the laying of the innermost carbon cloth layer is relatively difficult. The fiber cloth guide device 4 is designed to adopt a special spatial special-shaped guide structure, which is composed of four gradient-shrinking special-shaped plates 4-1. , the special-shaped plates 4-1 are evenly arranged along the circumferential direction. The gradient-shrinking special-shaped plate 4-1 is a thin space curved body formed by stamping/bending a thin plate. The cross-sectional shape of one end of the thin space curved body is a plurality of thin straight plates uniformly distributed in the circumferential direction, and the cross-sectional shape of the other end is a plurality of separated thin curved plates consistent with the final forming shape of the fiber cloth layer A. The middle of the thin space curved body is a smooth transition area, and the two ends of the thin space curved body realize smooth transition through the smooth transition area. The length of the thin straight plate at one end of the thin space curved body and the thin curved plate at the other end is equal. The fiber cloth 3 is divided into multiple rolls according to the polygonal shape, which are respectively laid on the thin straight plate. With the feeding of the pultrusion, the end of the thin straight plate gradually changes through the smooth transition area and is fully spread to the surface of the thin curved plate end. Through such a guide area, the fiber cloth 3 can be smoothly laid into a desired shape.

Claims (6)

1.一种多边形复合材料筒体抗弯扭复合成型方法,采用多边形芯模,多边形芯模的多个角部分别有多个用于成型长条状内筋的长沟槽,其特征在于,复合成型方法包括以下步骤:1. a polygonal composite material cylinder anti-bending torsion composite molding method, adopts a polygonal core mold, and a plurality of corners of the polygonal core mold respectively have a plurality of long grooves for forming elongated inner ribs, it is characterized in that, The composite molding method includes the following steps: 在多边形芯模的外表面包覆纤维布,形成纤维布层;The outer surface of the polygon core mold is covered with fiber cloth to form a fiber cloth layer; 在纤维布层外侧铺铺层纱形成内层纤维铺层;Lay layup yarns on the outside of the fiber cloth layer to form an inner fiber layup; 将缠绕纱线旋转缠绕到内层纤维铺层外侧,形成缠绕层;Rotate the winding yarn to the outside of the inner fiber layer to form a winding layer; 在缠绕层外侧铺铺层纱形成中间纤维铺层;Lay layup yarns on the outside of the winding layer to form an intermediate fiber layup; 在中间纤维铺层外侧编织形成内层编织层;Weaving on the outside of the intermediate fiber layup to form an inner braided layer; 在内层编织层外侧铺铺层纱形成外侧纤维铺层;Lay layup yarns on the outside of the inner braid to form an outside fiber layup; 在外侧纤维铺层外侧编织形成外层编织层;Weaving on the outside of the outer fiber layup to form an outer braided layer; 在边型芯模外形成由纤维布层、内层纤维铺层、缠绕层、中间纤维铺层、内层编织层、外侧纤维铺层及外层编织层组成的七层混合结构预成型体,在该七层混合结构预成型体中,仅纤维布层及内层纤维铺层位于长条状内筋位置;将包覆有七层混合结构预成型体的多边形芯模被送入外模后,进行高压注脂及固化成型,成型后的产品被不断拉出,每拉出一段距离后,切割得到成型产品。A seven-layer hybrid structure preform consisting of fiber cloth layer, inner fiber layup, winding layer, middle fiber layup, inner braided layer, outer fiber layup and outer braided layer is formed outside the side core mold. In the seven-layer hybrid structure preform, only the fiber cloth layer and the inner layer fiber layup are located at the position of the long strip; the polygonal core mold covered with the seven-layer hybrid structure preform is sent to the outer mold. , carry out high pressure grease injection and curing molding, the molded product is continuously pulled out, and after each pull out for a certain distance, the molded product is obtained by cutting. 2.如权利要求1所述的一种多边形复合材料筒体抗弯扭复合成型方法,其特征在于,所述七层混合结构预成型体的厚度能够根据需要调节。2 . The bending and torsion-resistant composite molding method for a polygonal composite material cylinder according to claim 1 , wherein the thickness of the seven-layer hybrid structure preform can be adjusted as required. 3 . 3.一种多边形复合材料筒体抗弯扭复合成型生产线,其特征在于,包括:3. A polygonal composite material cylinder body bending and torsion-resistant composite molding production line is characterized in that, comprising: 芯模牵引系统,用于将多边形芯模推送入外模中;Mandrel pulling system for pushing the polygonal mandrel into the outer mold; 纤维布导向装置,用于将纤维布包覆在多边形芯模的外表面,形成纤维布层;Fiber cloth guiding device, used to wrap the fiber cloth on the outer surface of the polygonal core mold to form a fiber cloth layer; 中间铺层纱引导板装置,用于将铺层纱铺在纤维布层外侧,形成内层纤维铺层;The middle layer yarn guide plate device is used to lay the layer yarn on the outside of the fiber cloth layer to form the inner layer fiber layer; 缠绕装置,用于将缠绕纱线旋转缠绕到内层纤维铺层外侧,形成缠绕层;Winding device, used to rotate the winding yarn to the outside of the inner fiber layer to form a winding layer; 铺层纱引导板装置,用于将铺层纱铺在缠绕层外侧,形成中间纤维铺层;The layered yarn guide plate device is used to lay the layered yarn on the outside of the winding layer to form an intermediate fiber layer; 编织机构一,用于在中间纤维铺层外侧编织形成内层编织层;The first weaving mechanism is used to weave the outer side of the intermediate fiber layup to form the inner braided layer; 铺层机构,用于将铺层纱铺在内层编织层外侧,形成外侧纤维铺层;The layering mechanism is used to lay the layered yarn on the outside of the inner braid to form the outer fiber layer; 编织机构二,用于在外侧纤维铺层外侧编织形成外层编织层;The second weaving mechanism is used to weave the outer layer of the outer fiber layer to form an outer layer of braided layer; 注脂固化系统,用于进行高压注脂及固化成型;Grease injection curing system, used for high pressure grease injection and curing molding; 成型复合材料产品牵引装置,用于将注脂固化系统获得的成型后的产品不断拉出;The forming composite material product pulling device is used to continuously pull out the formed product obtained by the grease injection curing system; 切割装置,每拉出一段距离后,利用切割装置切割得到成型产品。The cutting device is used to cut a shaped product after pulling out a certain distance. 4.如权利要求3所述的一种多边形复合材料筒体抗弯扭复合成型生产线,其特征在于,还包括芯模支撑架,用于在推送过程中支撑多边形芯模。4 . The bending and torsion-resistant composite molding production line for a polygonal composite material cylinder according to claim 3 , further comprising a core mold support frame for supporting the polygonal core mold during the pushing process. 5 . 5.如权利要求3所述的一种多边形复合材料筒体抗弯扭复合成型生产线,其特征在于,所述编织机构一、所述铺层机构以及所述编织机构二为各自独立的机构;或者所述编织机构一、所述铺层机构以及所述编织机构二集成在带铺层混合编织机内;或者所述编织机构一及所述编织机构二集成在三维编织机内。5. The anti-bending and torsion-resistant composite molding production line for a polygonal composite cylinder body according to claim 3, wherein the first weaving mechanism, the layering mechanism and the second weaving mechanism are independent mechanisms; Alternatively, the first knitting mechanism, the layering mechanism, and the second knitting mechanism are integrated into a hybrid knitting machine with layering; or the first knitting mechanism and the second knitting mechanism are integrated into a three-dimensional knitting machine. 6.如权利要求3所述的一种多边形复合材料筒体抗弯扭复合成型生产线,其特征在于,所述纤维布导向装置由四个渐变收缩的异型板材组合而成,异型板材沿周向均匀布置;6 . The anti-bending and torsion composite molding production line for a polygonal composite cylinder body according to claim 3 , wherein the fiber cloth guiding device is composed of four special-shaped plates with gradual shrinkage, and the special-shaped plates are along the circumferential direction. 7 . evenly arranged; 每个渐变收缩的异型板材为薄型空间曲面体,该薄型空间曲面体的一端横截面形状为多个周向均布的薄型直板,另一端横截面形状为多个分离的与最终纤维布层的成型形状一致的薄型弯板;薄型空间曲面体的中间为圆滑过渡区域,薄型空间曲面体两端通过该圆滑过渡区域实现圆滑过渡;薄型空间曲面体一端的薄型直板与另一端的薄型弯板的长度相等;Each gradient-shrinking special-shaped sheet is a thin space curved body, one end of the thin space curved body is a plurality of circumferentially evenly distributed thin straight plates, and the other end is a plurality of separate and final fiber cloth layers. Consistent thin curved plate; the middle of the thin space curved body is a smooth transition area, and the two ends of the thin space curved body realize a smooth transition through the smooth transition area; the thin straight plate at one end of the thin space curved body and the thin curved plate at the other end have the same length ; 纤维布根据多边形形状分为多卷,分别铺设在薄型直板上,随着拉挤的进给,纤维布由薄型直板端逐渐经圆滑过渡区域变化并满铺到薄型弯板端表面,从而使纤维布铺成所需形状。The fiber cloth is divided into multiple rolls according to the polygonal shape, which are respectively laid on the thin straight plate. With the feeding of the pultrusion, the fiber cloth gradually changes from the thin straight plate end through the smooth transition area and is fully spread to the thin curved plate end surface, so that the fiber Spread the cloth into the desired shape.
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