CN116001312A - A method of manufacturing a slender carbon fiber composite material square tube structure - Google Patents

A method of manufacturing a slender carbon fiber composite material square tube structure Download PDF

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Publication number
CN116001312A
CN116001312A CN202211680162.5A CN202211680162A CN116001312A CN 116001312 A CN116001312 A CN 116001312A CN 202211680162 A CN202211680162 A CN 202211680162A CN 116001312 A CN116001312 A CN 116001312A
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carbon fiber
paving
square tube
fiber composite
equalizing plate
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黄红初
刘影
李跃
龚国宝
万建平
马军
项国辉
刘俊文
郭鹏亮
鄢和庚
郭蕊娜
李燕银
李文辉
万超
钟日良
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Abstract

The invention discloses a manufacturing method of a square tube structural member made of an elongated carbon fiber composite material, which comprises the following steps: the first step: preparing a die: s2: paving and positioning: s3: paving carbon fiber prepreg: s4: and (3) curing and forming parts: s5: and (3) releasing equalizing plates 21 and 22: s6: removing the paving male die: s7: and (3) part detection: s8: and (5) trimming the parts. The invention ensures the precision requirements of the inner and outer molded surfaces of the product, ensures the stability of the demolding quality of the product, adopts flanging for paving in the process of paving the carbon fiber prepreg, plays a role in assisting demolding of the subsequent product, and can slowly demold the male mold by the threaded rod through flanging around the product supported by the ejector rod and the ejector block in the auxiliary tool; after the male die and the slender carbon fiber composite square tube structural member are formed by heating, due to the principles of thermal expansion and cold contraction of the two materials in the curing process, a micro gap can be formed between the inner molded surface of the carbon fiber and the steel male die, and the male die can be slowly pulled out by an auxiliary tool conveniently.

Description

一种细长碳纤维复合材料方管结构件的制作方法A method of manufacturing a slender carbon fiber composite material square tube structure

技术领域technical field

本发明属于复合材料加工技术领域,涉及一种细长碳纤维复合材料方管结构件的制作方法。The invention belongs to the technical field of composite material processing, and relates to a method for manufacturing a square tube structural part of a slender carbon fiber composite material.

背景技术Background technique

碳纤维复合材料凭借它轻质高强、不易腐蚀、成型方便、质量美观等优点已在航天航空产品上广泛应用,复合材料零件应用的结构趋向于简便、轻量化;在现有技术条件下,对复合材料成型工艺有着较大的难度,其中一种细长复合材料管状结构件(参见图1)就属于此类结构;该复合材料零件结构为细长碳纤维复合材料方管结构件,产品四周厚度为等厚度,内腔尺寸偏小;尺寸为(50×60)mm;长度为1000mm左右,细长碳纤维复合材料方管结构件的内外表面要求平整,特别是内表面后续有连接件装配关系,装配精度尺寸要求较高,且复合材料碳纤维结构件主要是靠纤维传递载荷,故装配区域不允许打磨修配,装配区域的内表面尺寸精度要求高,4个R角区域必须符合尺寸要求,所以细长碳纤维复合材料方管结构件的内表面必须依托模具成型,保证该内型面尺寸符合装配要求,但由于该零件的结构方管结构件,在现有复合材料制造工艺方法上比较复杂;主要体现在产品脱模方式上,为了保证结构的要求,现有成型方法主要有以下几种方式:Carbon fiber composite materials have been widely used in aerospace products due to their advantages of light weight, high strength, non-corrosion, convenient molding, and beautiful quality. The structure of composite material parts tends to be simple and lightweight; The material molding process is quite difficult, and one of the slender composite tubular structural parts (see Figure 1) belongs to this type of structure; the composite material part structure is a slender carbon fiber composite square tube structural part, and the thickness around the product is Equal thickness, the inner cavity size is small; the size is (50×60) mm; the length is about 1000mm, the inner and outer surfaces of the slender carbon fiber composite square tube structure are required to be flat, especially the inner surface is followed by the assembly relationship of connectors, assembly The requirements for precision dimensions are high, and the composite carbon fiber structural parts mainly rely on fibers to transmit loads, so grinding and repairing is not allowed in the assembly area, and the dimensional accuracy of the inner surface of the assembly area is high. The inner surface of the carbon fiber composite square tube structural part must be shaped by a mold to ensure that the size of the inner surface meets the assembly requirements. However, due to the structural square tube structural part of the part, the existing composite material manufacturing process is relatively complicated; mainly reflected In terms of product demoulding methods, in order to ensure the structural requirements, the existing molding methods mainly include the following methods:

一、采用阳模成型,这种方式的风险在于零件脱模过程中,由于零件内腔尺寸小,细长结构件,且产品和阳模经过高温高压加温成型,产品和模具比较贴合;现有的成型方法无法使产品和阳模分开,导致产品出现无法脱模的质量问题;1. Using positive mold molding, the risk of this method is that during the part demoulding process, due to the small size of the inner cavity of the part, the slender structural parts, and the product and the male mold are heated and formed at high temperature and high pressure, the product and the mold are relatively close; The existing molding method cannot separate the product from the male mold, resulting in quality problems that the product cannot be demolded;

二、采用阴模成型,这种方式的风险在于外型面的尺寸可以保证,但是根据产品要求的内型面和R角区域尺寸的要求,阴模成型方式无法保证要求,对产品后续装配的配合精度要求无法保证;2. Using female molding, the risk of this method is that the size of the outer surface can be guaranteed, but according to the requirements of the inner surface and the size of the R corner area required by the product, the female molding method cannot guarantee the requirements, and the subsequent assembly of the product The matching accuracy requirements cannot be guaranteed;

三、采用弹性体模具;使用阴阳模成型,其中阳模使用膨胀芯模或气囊芯模代替,用外面的充气源给它们充气使其膨胀,并将压力传递到层合板的表面,这种成型方法对细长碳纤维复合材料方管结构件的成型风险在于,对气囊芯模的成型要求高,气囊芯模需要单独成型,生产组合工艺复杂,提高了生产成本;3. Elastomer molds are used; male and female molds are used for forming, and the male molds are replaced by expansion mandrels or airbag mandrels. They are inflated with an external inflation source to make them expand, and the pressure is transmitted to the surface of the laminate. This kind of molding The risk of forming the slender carbon fiber composite square tube structural parts is that the forming requirements for the airbag mandrel are high, the airbag mandrel needs to be formed separately, the production combination process is complicated, and the production cost is increased;

在这样的技术背景下,对于这种细长碳纤维复合材料方管结构件,产品形状简便、轻量化、内、外表面要求光顺,且内型面尺寸要求符合装配精度的要求,在控制生产成本,提高产品质量的稳定性上;必须在现有的成型工艺上做出突破;本发明采用阳模铺贴、外表面使用均压板成型模组合成型,在保证产品质量的前提线使用脱模辅助工装进行产品脱模;该技术方法完成了细长碳纤维复合材料方管结构件的制造,更好的提高了零件质量,并保证了产品内型面装配精度尺寸要求。Under such a technical background, for this slender carbon fiber composite square tube structure, the product has a simple shape, light weight, smooth inner and outer surfaces, and the size of the inner surface meets the requirements of assembly accuracy. cost, improve the stability of product quality; a breakthrough must be made in the existing molding process; the present invention adopts male die paving, and the outer surface uses pressure equalizing plate molding die to combine molding, and the premise of ensuring product quality is to use stripping Mold-assisted tooling is used to demould the product; this technical method completes the manufacture of slender carbon fiber composite square tube structural parts, better improves the quality of parts, and ensures the assembly accuracy and size requirements of the product's inner surface.

发明内容Contents of the invention

本发明的目的是提供一种细长碳纤维复合材料方管结构件的制作方法,以提高了零件质量,保证产品内型面装配精度尺寸要求,提高生产效率。The purpose of the present invention is to provide a method for manufacturing a slender carbon fiber composite material square tube structure, so as to improve the quality of the parts, ensure the assembly accuracy and size requirements of the inner surface of the product, and improve production efficiency.

本发明技术方案:Technical scheme of the present invention:

一种细长碳纤维复合材料方管结构件的制作方法,该方法的步骤如下:A method for manufacturing a slender carbon fiber composite material square tube structure, the steps of the method are as follows:

S1:制备模具:S1: Prepare the mold:

制作铺贴阳模、均压板成型模和脱模辅助工装,其中,铺贴阳模的一端具有螺纹连接孔,所述均压板成型模由左半均压板和右半均压板组成,在左半均压板和右半均压板的成型面上铺贴膨胀橡胶,铺贴完成后进行组装密封,按照硫化参数固化成型;得到带有膨胀橡胶的左半均压板和右半均压板;所述脱模辅助工装包括顶块、顶杆、螺纹座块、螺纹扳手和螺纹杆,其中,顶块为配合使用部件,所述螺纹座块一侧的四周分别设有顶杆,螺纹座块上安装有螺纹杆,螺纹杆的一端连接有螺纹扳手,螺纹杆的另一端穿过顶块的中心孔与螺纹连接孔配合使用;Make paving and pasting male mold, pressure equalizing plate forming mold and demoulding auxiliary tooling, wherein, one end of paving and pasting male mold has a threaded connection hole, and said pressure equalizing plate forming mold is composed of left half pressure equalizing plate and right half pressure equalizing plate, in the left half Pave expanded rubber on the molding surface of the equalizer plate and the right half equalizer plate, assemble and seal after the paving is completed, and cure and mold according to the vulcanization parameters; obtain the left half equalizer plate and the right half equalizer plate with expanded rubber; the demoulding Auxiliary tooling includes a jacking block, a jacking rod, a threaded seat block, a threaded wrench and a threaded rod. Rod, one end of the threaded rod is connected with a threaded wrench, and the other end of the threaded rod passes through the center hole of the top block to cooperate with the threaded connection hole;

S2:铺贴定位:S2: Paving positioning:

将顶块与铺贴阳模组合,使顶块定位在铺贴阳模的一端;Combine the top block with the paving male mold so that the top block is positioned at one end of the paving male mold;

S3:铺贴碳纤维预浸料:S3: laying carbon fiber prepreg:

将碳纤维预浸料铺贴在铺贴阳模上,铺贴时除成型部分外,朝四周沿顶块侧面翻边铺贴,得到预浸料碳纤维方管;Lay the carbon fiber prepreg on the paving male mold, except for the forming part, pave the four sides along the side of the top block to get the prepreg carbon fiber square tube;

S4:零件固化成型:S4: Part curing molding:

在预浸料碳纤维方管表面铺贴一层脱模布和隔离薄膜,将带有膨胀橡胶的左半均压板和右半均压板进行组合在预浸料碳纤维方管上,然后按照复合材料热压罐成型法的工艺要求进行真空热压成型,得到零件成型体;Lay a layer of release cloth and isolation film on the surface of the prepreg carbon fiber square tube, combine the left half pressure equalizing plate and the right half pressure equalizing plate with expansion rubber on the prepreg carbon fiber square tube, and then heat the The process of the pressure pot forming method requires vacuum hot pressing to obtain a molded part;

S5:脱均压板成型模:S5: Forming mold for de-equalizing plate:

固化成型后去除左半均压板和右半均压板,松动顶块;After curing and forming, remove the left and right equalizing plates, and loosen the top block;

S6:脱铺贴阳模:S6: Take off the pavement and stick the male mold:

将螺纹杆的一端穿过顶块的中心孔后与铺贴阳模的螺纹连接孔连接,使顶杆顶住顶块,通过转动螺纹扳手使得螺纹杆推动铺贴阳模与零件成型体分离,完成脱模;Pass one end of the threaded rod through the center hole of the top block and connect it to the threaded connection hole of the paving male mold, so that the ejector rod withstands the top block, and the threaded rod pushes the paving male mold to separate from the part forming body by turning the threaded wrench. complete demoulding;

S7:零件检测:S7: Part detection:

将零件成型体进行无损检测检查;Carry out non-destructive testing inspection of the molded parts;

S8:修整零件:S8: Trim parts:

按相关技术条件对零件成型体进行加工、修整,得到细长碳纤维复合材料方管结构件。According to the relevant technical conditions, the molded body of the part is processed and trimmed to obtain a slender carbon fiber composite material square tube structural part.

进一步,均压板成型模的型面在碳纤维方管零件外型面基础上每个面扩大0.12mm。Further, the surface of the equalizing plate forming mold is enlarged by 0.12 mm on each surface based on the external surface of the carbon fiber square tube part.

进一步,所述左半均压板和右半均压板的组合面为阶梯型组合面。Further, the combination surface of the left half pressure equalizer plate and the right half pressure equalizer plate is a stepped combination surface.

进一步,所述左半均压板的上表面设有第一外凹台,下表面设有第一内凹台,所述右半均压板的上表面设有与第一外凹台配合的第二内凹台,下表面设有与第一内凹台匹配的第二外凹台。Further, the upper surface of the left half pressure equalizing plate is provided with a first outer concave platform, the lower surface is provided with a first inner concave platform, and the upper surface of the right half pressure equalizing plate is provided with a second concave platform that matches the first outer concave platform. The inner concave platform has a second outer concave platform matching the first inner concave platform on the lower surface.

进一步,S3中,翻边铺贴厚度为细长碳纤维复合材料方管结构件厚度的1.5~2.5倍。Furthermore, in S3, the thickness of the flanging paving is 1.5 to 2.5 times the thickness of the elongated carbon fiber composite square tube structural part.

进一步,所述螺纹杆长1100mm,直径为20mm。Further, the threaded rod has a length of 1100mm and a diameter of 20mm.

本发明有益效果:Beneficial effects of the present invention:

本发明为了保证产品内型面装配精度要求,采用铺贴阳模成型,为了确保零件的外型面有一个平整的表面质量,定制了一套均压板成型模,为了保证产品脱模质量的稳定性,采用了辅助脱模工装,为了保证产品四周能够平稳的脱模,产品在铺贴过程中采用翻边铺贴,起到后续产品辅助脱模作用,通过辅助工装中的顶杆、顶块顶住产品四周翻边,能够使螺纹杆缓慢将阳模脱模;阳模和细长碳纤维复合材料方管结构件通过加温成型后,由于在固化过程中两种材料热胀冷缩原理,碳纤维内型面和钢质阳模会形成微小间隙,后续可便于辅助工装将阳模缓慢脱出;通过碳纤维复合材料结构件后续的一系列检测,证明了产品质量符合相关技术要求。In order to ensure the assembly accuracy requirements of the inner surface of the product, the present invention adopts a paving male mold for forming. In order to ensure that the outer surface of the part has a smooth surface quality, a set of pressure equalizing plate forming molds is customized. In order to ensure the stability of the demoulding quality of the product In order to ensure that the product can be demoulded smoothly around the product, the product is paved with flanging during the paving process, which plays the role of auxiliary demoulding for subsequent products. Through the ejector pin and the top block in the auxiliary tooling Withstand the flanging around the product, so that the threaded rod can slowly demould the male mold; after the male mold and the slender carbon fiber composite square tube structure are formed by heating, due to the principle of thermal expansion and contraction of the two materials during the curing process, A small gap will be formed between the carbon fiber inner surface and the steel male mold, which will facilitate the auxiliary tooling to slowly release the male mold; through a series of subsequent tests on the carbon fiber composite structural parts, it is proved that the product quality meets the relevant technical requirements.

附图说明Description of drawings

图1为细长碳纤维复合材料方管结构件的结构示意图;Fig. 1 is the structural schematic diagram of the slender carbon fiber composite material square tube structure;

图2为本发明实施例中铺贴阳模的示意图;Fig. 2 is the schematic diagram of paving and pasting male mold in the embodiment of the present invention;

图3为本发明实施例中均压板成型模的示意图;Fig. 3 is the schematic diagram of the molding die of equalizing plate in the embodiment of the present invention;

图4为本发明实施例中脱模辅助工装的结构示意图;Fig. 4 is a schematic structural view of demoulding auxiliary tooling in an embodiment of the present invention;

图5为本发明实施例中脱模辅助工装的另一结构示意图;Fig. 5 is another structural schematic diagram of the demoulding auxiliary tooling in the embodiment of the present invention;

图6为本发明实施例中均压板成型模的组合示意图;Fig. 6 is a combined schematic view of the pressure equalizing plate molding die in the embodiment of the present invention;

图7为本发明实施例的铺贴示意图;Fig. 7 is the paving schematic diagram of the embodiment of the present invention;

图8为本发明实施例的脱模示意图;Fig. 8 is the demoulding schematic diagram of the embodiment of the present invention;

图9为本发明实施例的翻边切除示意图;Fig. 9 is a schematic diagram of flanging cutting according to an embodiment of the present invention;

图中:铺贴阳模1、均压板成型模2,脱模辅助工装3,预浸料碳纤维方管4,翻边切除5,螺纹连接孔11,左半均压板21,右半均压板22,顶块31,顶杆32,螺纹座块33,螺纹扳手34,螺纹杆35,翻边41,左半均压板第一外凹台211,左半均压板第一内凹台212,右半均压板第二内凹台221,右半均压板第二外凹台222。In the figure: paving male mold 1, pressure equalizing plate forming mold 2, demoulding auxiliary tooling 3, prepreg carbon fiber square tube 4, flange cut 5, threaded connection hole 11, left equalizing plate half 21, right half equalizing plate 22 , top block 31, ejector rod 32, threaded seat block 33, threaded wrench 34, threaded rod 35, flange 41, the first outer concave platform 211 of the left half pressure equalizing plate, the first inner concave platform 212 of the left half pressure equalizing plate, the right half The second inner concave platform 221 of the pressure equalizing plate, and the second outer concave platform 222 of the right half pressure equalizing plate.

具体实施方式Detailed ways

本发明通过下面的实施案例可以对本发明做进一步的描述,然而,本发明的范围并不限于下述实施例。The present invention can be further described by the following examples, however, the scope of the present invention is not limited to the following examples.

实施例:如图1所示一种细长碳纤维复合材料方管结构件的制作方法,该方法的步骤如下:Embodiment: As shown in Fig. 1, a kind of manufacturing method of elongated carbon fiber composite material square tube structure, the steps of this method are as follows:

S1:制备模具:S1: Prepare the mold:

首先为了确保细长碳纤维复合材料方管结构件内型面装配尺寸精度符合要求,定制了铺贴阳模1(参见图2),铺贴阳模1的一端具有螺纹连接孔11;为了确保零件的外型面有一个平整的表面质量,定制了一套均压成型模2和成型后膨胀橡胶软模(参见图3和图6),均压板成型模2的型面在碳纤维方管4零件的外型面基础上每个面扩大0.12mm,均压板由左半均压板21和右半均压板22组成,在左半均压板21和右半均压板22上铺贴膨胀橡胶,铺贴完成后按照相关的工艺文件要求进行组装密封,然后使用相关的加温设备按照软模的硫化参数进行固化成型,得到带有膨胀橡胶的左半均压板21和右半均压板22,其中,左半均压板21和右半均压板22的组合面为阶梯型组合面,左半均压板21的上表面设有第一外凹台211,下表面设有第一内凹台212,所述右半均压板22的上表面设有与第一外凹台211配合的第二内凹台221,下表面设有与第一内凹台212匹配的第二外凹台222;为了确保细长碳纤维复合材料方管结构件顺利脱模,定制了一套辅助脱模工装(参见图4和图5),脱模辅助工装3包括顶块31、顶杆32、螺纹座块33、螺纹扳手34和螺纹杆35,其中,顶块31为配合使用部件,所述螺纹座块33一侧的四周分别设有顶杆32,螺纹座块33上安装有螺纹杆35,螺纹杆35的一端连接有螺纹扳手34,螺纹杆35的另一端穿过顶块31的中心孔(图中未示出)与螺纹连接孔11配合使用。First of all, in order to ensure that the dimensional accuracy of the internal surface assembly of the slender carbon fiber composite square tube structure meets the requirements, a paving male mold 1 (see Figure 2) is customized. One end of the paving male mold 1 has a threaded connection hole 11; in order to ensure that the parts The outer surface of the pressure equalizing plate has a flat surface quality, and a set of pressure equalizing molding die 2 and soft expansion rubber mold after molding are customized (see Figure 3 and Figure 6). On the basis of the exterior surface, each surface is enlarged by 0.12mm. The equalizing plate is composed of the left half equalizing plate 21 and the right half equalizing plate 22. The expansion rubber is laid on the left half equalizing plate 21 and the right half equalizing plate 22, and the paving is completed. Finally, assemble and seal according to the requirements of relevant process documents, and then use relevant heating equipment to perform curing and molding according to the vulcanization parameters of the soft mold, and obtain the left half equalizing plate 21 and the right half equalizing plate 22 with expanded rubber, wherein, the left half The combined surface of the pressure equalizing plate 21 and the right half of the pressure equalizing plate 22 is a stepped combination surface, the upper surface of the left half of the pressure equalizing plate 21 is provided with a first outer concave platform 211, and the lower surface is provided with a first inner concave platform 212. The upper surface of the pressure equalizing plate 22 is provided with a second inner concave platform 221 matched with the first outer concave platform 211, and the lower surface is provided with a second outer concave platform 222 matched with the first inner concave platform 212; in order to ensure that the elongated carbon fiber composite The material square tube structure was successfully demoulded, and a set of auxiliary demoulding tooling was customized (see Figure 4 and Figure 5). Rod 35, wherein, jacking block 31 is the part that cooperates to use, described threaded seat block 33 sides are respectively provided with ejector bar 32, and threaded seat block 33 is equipped with threaded rod 35, and one end of threaded rod 35 is connected with threaded wrench 34. The other end of the threaded rod 35 passes through the center hole (not shown in the figure) of the top block 31 to cooperate with the threaded connection hole 11.

S2:铺贴定位:S2: Paving positioning:

将顶块31与铺贴阳模1组合,使顶块31定位在铺贴阳模1的一端;具体地可通过双面胶将顶块31固定在阳模铺贴工装一头(参见图7)。Combine the jacking block 31 with the paving male mold 1, so that the jacking block 31 is positioned at one end of the paving male mold 1; specifically, the jacking block 31 can be fixed at one end of the male paving tooling with double-sided adhesive (see Figure 7) .

S3:铺贴碳纤维预浸料:S3: laying carbon fiber prepreg:

按照细长碳纤维复合材料方管结构件的相关要求在铺贴阳模1进行碳纤维预浸料铺贴,铺贴过程中需要在顶块31四周翻边41进行整体铺贴,得到预浸料碳纤维方管4;翻边41铺贴厚度为细长碳纤维复合材料方管结构件厚度的1.5~2.5倍,优选为2倍厚度,通过设置翻边41可以起到传递载荷作用,有利于后续产品的脱模,(参见图7)。According to the relevant requirements of the slender carbon fiber composite material square tube structural parts, the carbon fiber prepreg is laid on the laying male mold 1. During the laying process, the flanging 41 around the top block 31 needs to be laid as a whole to obtain the prepreg carbon fiber. The square tube 4; the thickness of the flanging 41 is 1.5 to 2.5 times the thickness of the slender carbon fiber composite square tube structure, preferably 2 times the thickness. By setting the flanging 41, the load can be transferred, which is conducive to the development of subsequent products. Unmold, (see Figure 7).

S4:零件固化成型:S4: Part curing molding:

在预浸料碳纤维方管4表面铺贴一层脱模布和隔离薄膜、带有膨胀橡胶的左半均压板21和右半均压板22进行组合压在预浸料碳纤维方管4上,然后按照复合材料热压罐成型法的一般工艺要求对其进行真空袋工艺组合操作;按照碳纤维预浸料的工艺参数进热压罐进行加温固化,得到零件成型体。Lay a layer of release cloth and isolation film on the surface of the prepreg carbon fiber square tube 4, and combine the left half pressure equalizing plate 21 and the right half pressure equalizing plate 22 with expanded rubber to press on the prepreg carbon fiber square tube 4, and then According to the general process requirements of the autoclave forming method of composite materials, the vacuum bag process combination operation is carried out; according to the process parameters of the carbon fiber prepreg, it is heated and cured in an autoclave to obtain a molded part.

S5:脱均压板成型模:S5: Forming mold for de-equalizing plate:

去除真空袋和均压左半均压板21和右半均压板22;松动顶块31靠近零件成型体的一端,确保顶块31与铺贴阳模1处于松动状态(参见图8);Remove the vacuum bag and equalize the left half of the pressure equalizing plate 21 and the right half of the pressure equalizing plate 22; loosen the end of the top block 31 close to the molded body of the part, and ensure that the top block 31 and the paving male mold 1 are in a loose state (see Figure 8);

S6:脱铺贴阳模:S6: Take off the pavement and stick the male mold:

将螺纹杆35的一端穿过顶块31的中心孔后与铺贴阳模1的螺纹连接孔11连接,使顶杆2顶住顶块31,通过转动螺纹扳手34使得螺纹杆35推动铺贴阳模1与零件成型体分离,完成脱模;Pass one end of the threaded rod 35 through the center hole of the top block 31 and connect it to the threaded connection hole 11 of the paving male mold 1, so that the ejector rod 2 withstands the top block 31, and the threaded rod 35 is pushed by turning the threaded wrench 34 The male mold 1 is separated from the molded body of the part to complete demoulding;

S7:零件检测:S7: Part detection:

将零件成型体进行无损检测检查;Carry out non-destructive testing inspection of the molded parts;

S8:修整零件:S8: Trim parts:

按相关技术条件对产品进行加工、修整(参见图9对零件成型体带有翻边的一端进行切除),得到细长碳纤维复合材料方管结构件。The product is processed and trimmed according to the relevant technical conditions (refer to Figure 9 to cut off the end of the part molded body with flanging), and a slender carbon fiber composite material square tube structural part is obtained.

以上显示和描述了本发明的基本原理和主要特征和本发明的优点,对于本领域技术人员而言,显然本发明不限于上述示范性实施例的细节,而且在不背离本发明的精神或基本特征的情况下,能够以其它的具体形式实现本发明。因此,无论从哪一点来看,均应将实施例看作是示范性的,而且是非限制性的,本发明的范围由所附权利要求而不是上述说明限定,因此旨在将落在权利要求的等同要件的含义和范围内的所有变化囊括在本发明内。不应将权利要求中的任何附图标记视为限制所涉及的权利要求。The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above. For those skilled in the art, it is obvious that the present invention is not limited to the details of the above-mentioned exemplary embodiments, and without departing from the spirit or basic principles of the present invention. The present invention can be embodied in other specific forms without using the features described above. Accordingly, the embodiments should be regarded in all points of view as exemplary and not restrictive, the scope of the invention being defined by the appended claims rather than the foregoing description, and it is therefore intended that the scope of the invention be defined by the appended claims rather than by the foregoing description. All changes within the meaning and range of equivalents of the elements are embraced in the present invention. Any reference sign in a claim should not be construed as limiting the claim concerned.

此外,应当理解,虽然本说明书按照实施方式加以描述,但并非每个实施方式仅包含一个独立的技术方案,说明书的这种叙述方式仅仅是为清楚起见,本领域技术人员应当将说明书作为一个整体,各实施例中的技术方案也可以经适当组合,形成本领域技术人员可以理解的其它实施方式。In addition, it should be understood that although this specification is described according to implementation modes, not each implementation mode only contains an independent technical solution, and this description in the specification is only for clarity, and those skilled in the art should take the specification as a whole , the technical solutions in the various embodiments can also be properly combined to form other implementations that can be understood by those skilled in the art.

Claims (6)

1. A manufacturing method of a slender carbon fiber composite square tube structural member is characterized by comprising the following steps: the method comprises the following steps:
s1: preparing a die:
manufacturing a paving male die, a uniform pressure plate forming die and a demolding auxiliary tool, wherein one end of the paving male die is provided with a threaded connection hole, the uniform pressure plate forming die consists of a left half uniform pressure plate and a right half uniform pressure plate, expanded rubber is paved on forming surfaces of the left half uniform pressure plate and the right half uniform pressure plate, assembly sealing is carried out after paving is completed, and curing molding is carried out according to vulcanization parameters; obtaining a left half equalizing plate and a right half equalizing plate with expanded rubber; the demolding auxiliary tool comprises a jacking block, an ejector rod, a threaded seat block, a threaded wrench and a threaded rod, wherein the jacking block is a matched part, the ejector rod is arranged around one side of the threaded seat block respectively, the threaded seat block is provided with the threaded rod, one end of the threaded rod is connected with the threaded wrench, and the other end of the threaded rod penetrates through a central hole of the jacking block to be matched with the threaded connecting hole;
s2: paving and positioning:
combining the top block with the paving male die to enable the top block to be positioned at one end of the paving male die;
s3: paving carbon fiber prepreg:
spreading the carbon fiber prepreg on a spreading male die, and spreading the carbon fiber prepreg along the side edge of the top block towards the periphery except the forming part during spreading to obtain a prepreg carbon fiber square tube;
s4: and (3) curing and forming parts:
paving a layer of release cloth and an isolating film on the surface of the prepreg carbon fiber square tube, combining a left half-equalizing plate and a right half-equalizing plate with expansion rubber on the prepreg carbon fiber square tube, and then carrying out vacuum hot-press molding according to the technological requirements of a composite material autoclave molding method to obtain a part molded body;
s5: and (3) removing the equalizing plate forming die:
removing the left half uniform pressure plate and the right half uniform pressure plate after solidification molding, and loosening the top block;
s6: removing the paving male die:
one end of the threaded rod penetrates through the center hole of the ejector block and then is connected with the threaded connection hole of the paving male die, so that the ejector rod is propped against the ejector block, and the threaded rod pushes the paving male die to be separated from the part forming body through rotating the threaded wrench, so that demolding is completed;
s7: and (3) part detection:
performing nondestructive inspection on the part molded body;
s8: trimming parts:
and (3) processing and trimming the part forming body according to related technical conditions to obtain the slender carbon fiber composite square tube structural member.
2. The method for manufacturing the square tube structural member made of the slender carbon fiber composite material according to claim 1, wherein the method comprises the following steps: the molded surface of the equalizing plate molding die expands 0.12mm on the basis of the outer surface of the carbon fiber square tube part.
3. The method for manufacturing the square tube structural member made of the slender carbon fiber composite material according to claim 1, wherein the method comprises the following steps: the combined surface of the left half pressure equalizing plate and the right half pressure equalizing plate is a stepped combined surface.
4. A method of making an elongated carbon fiber composite square tube structural member according to claim 3, wherein: the upper surface of half equalizing plate in left side is equipped with first outer concave station, and the lower surface is equipped with first concave station, the upper surface of half equalizing plate in right side be equipped with first outer concave station complex second concave station, the lower surface be equipped with first concave station matched second outer concave station.
5. The method for manufacturing the square tube structural member made of the slender carbon fiber composite material according to claim 1, wherein the method comprises the following steps: and S3, the thickness of the flange is 1.5-2.5 times of that of the square tube structural member made of the slender carbon fiber composite material.
6. The method for manufacturing the square tube structural member made of the slender carbon fiber composite material according to claim 1, wherein the method comprises the following steps: the length of the threaded rod is 1100mm, and the diameter of the threaded rod is 20mm.
CN202211680162.5A 2022-12-26 2022-12-26 A method of manufacturing a slender carbon fiber composite material square tube structure Pending CN116001312A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116552738A (en) * 2023-07-04 2023-08-08 东莞市聚力复合材料科技有限公司 Sail control rod and manufacturing process thereof
CN116945645A (en) * 2023-07-28 2023-10-27 江西昌河航空工业有限公司 Method for improving edge thickness qualification rate of composite honeycomb sandwich component
CN117140997A (en) * 2023-08-28 2023-12-01 江苏新扬新材料股份有限公司 A method of forming an integrated composite material mounting base with an internal thread structure
CN119974591A (en) * 2025-01-08 2025-05-13 威海光威复合材料科技有限公司 A forming die and manufacturing method of a composite material polygonal tube

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06106632A (en) * 1992-09-30 1994-04-19 Sakura Rubber Kk Method for molding composite material product
JP2007076202A (en) * 2005-09-15 2007-03-29 Toho Tenax Co Ltd Molding method of frp-made square pipe
CN103029307A (en) * 2012-12-12 2013-04-10 江西洪都航空工业集团有限责任公司 Manufacture method of box-shaped structural main beam made from composite material
CN104552991A (en) * 2014-11-25 2015-04-29 中材科技股份有限公司 De-molding device for large-length-diameter-ratio composite material thin wall pipe and de-molding method of de-molding device
CN105500730A (en) * 2015-12-24 2016-04-20 中航复合材料有限责任公司 High-precision forming mold and method for thickly-laid composite material boxes
CN106182805A (en) * 2016-09-09 2016-12-07 西安爱生技术集团公司 A kind of manufacturing process of the isometrical tubular structure of carbon fibre composite
CN106393743A (en) * 2016-11-30 2017-02-15 江西洪都航空工业集团有限责任公司 Composite material intake way forming mold
CN107738386A (en) * 2017-11-10 2018-02-27 江苏恒神股份有限公司 Stripper apparatus of the carbon fiber ring to U-shaped part
CN212472170U (en) * 2020-06-29 2021-02-05 北京尚方达科技发展有限公司 Demoulding device for compression molding of composite square tube
CN215319520U (en) * 2021-03-08 2021-12-28 江苏埃菲尔实业有限公司 Novel tubular pile steel mould structure
CN113977984A (en) * 2021-10-15 2022-01-28 江西洪都航空工业集团有限责任公司 Preparation method of tubular double-curved-surface composite material structural member
CN114834062A (en) * 2022-03-29 2022-08-02 天津爱思达新材料科技有限公司 Forming process of special-shaped airplane air inlet channel
CN115464899A (en) * 2022-08-24 2022-12-13 南京晨光集团有限责任公司 A method for forming composite materials with a hollow rotary body structure with front and rear ends

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06106632A (en) * 1992-09-30 1994-04-19 Sakura Rubber Kk Method for molding composite material product
JP2007076202A (en) * 2005-09-15 2007-03-29 Toho Tenax Co Ltd Molding method of frp-made square pipe
CN103029307A (en) * 2012-12-12 2013-04-10 江西洪都航空工业集团有限责任公司 Manufacture method of box-shaped structural main beam made from composite material
CN104552991A (en) * 2014-11-25 2015-04-29 中材科技股份有限公司 De-molding device for large-length-diameter-ratio composite material thin wall pipe and de-molding method of de-molding device
CN105500730A (en) * 2015-12-24 2016-04-20 中航复合材料有限责任公司 High-precision forming mold and method for thickly-laid composite material boxes
CN106182805A (en) * 2016-09-09 2016-12-07 西安爱生技术集团公司 A kind of manufacturing process of the isometrical tubular structure of carbon fibre composite
CN106393743A (en) * 2016-11-30 2017-02-15 江西洪都航空工业集团有限责任公司 Composite material intake way forming mold
CN107738386A (en) * 2017-11-10 2018-02-27 江苏恒神股份有限公司 Stripper apparatus of the carbon fiber ring to U-shaped part
CN212472170U (en) * 2020-06-29 2021-02-05 北京尚方达科技发展有限公司 Demoulding device for compression molding of composite square tube
CN215319520U (en) * 2021-03-08 2021-12-28 江苏埃菲尔实业有限公司 Novel tubular pile steel mould structure
CN113977984A (en) * 2021-10-15 2022-01-28 江西洪都航空工业集团有限责任公司 Preparation method of tubular double-curved-surface composite material structural member
CN114834062A (en) * 2022-03-29 2022-08-02 天津爱思达新材料科技有限公司 Forming process of special-shaped airplane air inlet channel
CN115464899A (en) * 2022-08-24 2022-12-13 南京晨光集团有限责任公司 A method for forming composite materials with a hollow rotary body structure with front and rear ends

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
蒋建军,李玉军: "树脂基复合材料成型原理与工艺", vol. 1, 31 May 2022, 西北工业大学出版社, pages: 175 - 176 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116552738A (en) * 2023-07-04 2023-08-08 东莞市聚力复合材料科技有限公司 Sail control rod and manufacturing process thereof
CN116552738B (en) * 2023-07-04 2023-11-14 东莞市聚力复合材料科技有限公司 Sail control rod and manufacturing process thereof
CN116945645A (en) * 2023-07-28 2023-10-27 江西昌河航空工业有限公司 Method for improving edge thickness qualification rate of composite honeycomb sandwich component
CN116945645B (en) * 2023-07-28 2025-11-04 江西昌河航空工业有限公司 A method for improving the edge thickness qualification rate of composite honeycomb sandwich components
CN117140997A (en) * 2023-08-28 2023-12-01 江苏新扬新材料股份有限公司 A method of forming an integrated composite material mounting base with an internal thread structure
CN119974591A (en) * 2025-01-08 2025-05-13 威海光威复合材料科技有限公司 A forming die and manufacturing method of a composite material polygonal tube
CN119974591B (en) * 2025-01-08 2025-11-11 威海光威复合材料科技有限公司 Composite polygonal pipe forming die based on autoclave forming and manufacturing method

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