CN114311730A - Composite material light shield, forming die and preparation method thereof - Google Patents
Composite material light shield, forming die and preparation method thereof Download PDFInfo
- Publication number
- CN114311730A CN114311730A CN202111582075.1A CN202111582075A CN114311730A CN 114311730 A CN114311730 A CN 114311730A CN 202111582075 A CN202111582075 A CN 202111582075A CN 114311730 A CN114311730 A CN 114311730A
- Authority
- CN
- China
- Prior art keywords
- water
- composite material
- light shield
- holes
- mold
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 53
- 238000002360 preparation method Methods 0.000 title abstract description 10
- 238000000034 method Methods 0.000 claims abstract description 25
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 5
- 239000011347 resin Substances 0.000 claims description 15
- 229920005989 resin Polymers 0.000 claims description 15
- 239000000835 fiber Substances 0.000 claims description 12
- 238000000465 moulding Methods 0.000 claims description 10
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 6
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- XLJMAIOERFSOGZ-UHFFFAOYSA-M cyanate Chemical compound [O-]C#N XLJMAIOERFSOGZ-UHFFFAOYSA-M 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 claims description 3
- 239000003365 glass fiber Substances 0.000 claims description 3
- 239000007769 metal material Substances 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 229920000647 polyepoxide Polymers 0.000 claims description 3
- 229920001721 polyimide Polymers 0.000 claims description 3
- 239000009719 polyimide resin Substances 0.000 claims description 3
- 239000010453 quartz Substances 0.000 claims description 3
- 239000000377 silicon dioxide Substances 0.000 claims description 3
- XQUPVDVFXZDTLT-UHFFFAOYSA-N 1-[4-[[4-(2,5-dioxopyrrol-1-yl)phenyl]methyl]phenyl]pyrrole-2,5-dione Chemical compound O=C1C=CC(=O)N1C(C=C1)=CC=C1CC1=CC=C(N2C(C=CC2=O)=O)C=C1 XQUPVDVFXZDTLT-UHFFFAOYSA-N 0.000 claims 1
- 230000000149 penetrating effect Effects 0.000 claims 1
- 229920003192 poly(bis maleimide) Polymers 0.000 claims 1
- 238000007711 solidification Methods 0.000 claims 1
- 230000008023 solidification Effects 0.000 claims 1
- 230000003014 reinforcing effect Effects 0.000 description 5
- 230000007547 defect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 239000003733 fiber-reinforced composite Substances 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- IWKLZLOHCXIBNS-UHFFFAOYSA-N benzene-1,2-dicarbonyl cyanide Chemical compound N#CC(=O)C1=CC=CC=C1C(=O)C#N IWKLZLOHCXIBNS-UHFFFAOYSA-N 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000002356 single layer Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000003351 stiffener Substances 0.000 description 2
- 238000005056 compaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009415 formwork Methods 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000004046 wet winding Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Landscapes
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
本发明提供了一种复合材料遮光罩、成型模具及其制备方法,包括步骤:S1、按照铺层顺序和铺层角度,在水溶性芯模上铺放至少一层预浸料;S2、将各个水溶性芯模依次利用定位轴进行引导穿插,将穿插有水溶性芯模的定位轴分别与上下模板进行固定;S3、按照铺层顺序和铺层角度在完成固定后的水溶性芯模的外表面及翻边法兰的成型面进行蒙皮的铺放;S4、依次安装外分瓣、外加压圈,完成对复合材料遮光罩成型模具的组装;S5、通过成型模具对复合材料遮光罩进行预压实,并进行固化;S6、完成固化后,对模具进行拆卸并用水溶去水溶性芯模。本发明的遮光罩通过预浸料铺放工艺一体成型制得,得到常规工艺无法制作的小尺度复合材料遮光罩。
The invention provides a composite material light shield, a forming mold and a preparation method thereof, comprising the steps of: S1, laying at least one layer of prepreg on the water-soluble core mold according to the layup sequence and layup angle; S2, placing Each water-soluble mandrel is guided and inserted by the positioning shaft in turn, and the positioning shafts interspersed with the water-soluble mandrel are respectively fixed with the upper and lower templates; The outer surface and the forming surface of the flanging flange are laid for the skin; S4, the outer split and the outer pressure ring are installed in sequence to complete the assembly of the composite material hood forming mold; S5, the composite material is shaded by the forming mold. The cover is pre-compacted and cured; S6. After curing, the mold is disassembled and the water-soluble core mold is removed by dissolving with water. The light shield of the present invention is integrally formed through a prepreg laying process, thereby obtaining a small-scale composite material light shield that cannot be produced by conventional processes.
Description
技术领域technical field
本发明属于复合材料应用技术领域,具体涉及一种复合材料遮光罩、成型模具及其制备方法。The invention belongs to the technical field of composite material application, and in particular relates to a composite material light shield, a forming mold and a preparation method thereof.
背景技术Background technique
树脂基纤维增强复合材料遮光罩以其轻质高强的力学特性、优异的尺寸稳定性,在航空航天、卫星结构、相机结构等领域均有着广泛的应用。Resin-based fiber reinforced composite hoods are widely used in aerospace, satellite structures, camera structures and other fields due to their lightweight, high-strength mechanical properties and excellent dimensional stability.
传统的复合材料遮光罩制备工艺有金属对模工艺、真空袋工艺、热压罐工艺、真空注塑工艺,上述工艺适用于大尺寸或者中尺寸复合材料遮光罩(直径约大于150mm)制备,这是因为上述工艺均需采用刚性(金属或者其他材料)内模用于遮光罩的成型,中大型尺寸遮光罩内腔空间充裕,可以允许刚性内模分瓣的安装及脱模操作需求,对于小尺寸(直径小于100mm以内)遮光罩而言,遮光罩内腔操作空间小,不足以支撑刚性内模分瓣的安装及脱模操作;同时传统带有内格栅加强筋的遮光罩其一般采用湿法或干法缠绕预浸丝的方式成型,造成内格栅与蒙皮热胀系数不匹配、力学性能差的缺陷。The traditional composite material hood preparation processes include metal mold process, vacuum bag process, autoclave process, and vacuum injection molding process. Because the above processes all need to use rigid (metal or other materials) inner molds for the forming of the hood, the inner cavity space of the medium and large size hoods is abundant, which can allow the installation and demoulding operation requirements of the rigid inner mold split. For the hood (within diameter less than 100mm), the operating space of the inner cavity of the hood is small, which is not enough to support the installation and demoulding operation of the rigid inner mold split; The method of winding the prepreg wire by the method or dry method causes the defects that the thermal expansion coefficient of the inner grid and the skin do not match and the mechanical properties are poor.
发明内容SUMMARY OF THE INVENTION
本发明为了解决上述现有技术中的缺陷,提出了一种复合材料遮光罩、成型模具及其制备方法,能够制备常规工艺无法制作的小尺寸复合材料遮光罩器件,同时相较于传统干法或者湿法缠绕纤维丝成型加强筋的工艺,该方法制备的加强筋热胀系数具有可设计性,其力学性能更佳。为实现上述目的,本发明采用以下具体技术方案:In order to solve the above-mentioned defects in the prior art, the present invention proposes a composite material light shield, a molding die and a preparation method thereof, which can prepare a small-sized composite material light shield device that cannot be produced by a conventional process, and at the same time, compared with the traditional dry method Or the process of forming reinforcing rib by wet winding of filaments, the thermal expansion coefficient of the reinforcing rib prepared by this method can be designed, and its mechanical properties are better. For achieving the above object, the present invention adopts following concrete technical scheme:
一种复合材料遮光罩成型模具,包括:上模板、下模板、外加压圈、外分瓣、水溶性芯模和定位轴;A composite material hood forming mold, comprising: an upper template, a lower template, an outer pressure ring, an outer split, a water-soluble core mold and a positioning shaft;
上模板和下模板的预设区域内均对应设置有加压通孔,合模时通过加压通孔对复合材料遮光罩成型模具的轴向进行加压,预设区域为内径大于外分瓣的外径的环形区域;Pressing through holes are correspondingly arranged in the preset areas of the upper template and the lower template. When the mold is closed, the pressure through holes are used to pressurize the axial direction of the composite material light shield forming mold. The preset area is that the inner diameter is larger than the outer split. the outer diameter of the annular area;
外加压圈的周向均布压圈螺纹孔,压圈螺纹孔用于通过螺纹件对外分瓣进行径向加压;Threaded holes of the outer pressure ring are uniformly distributed in the circumferential direction, and the threaded holes of the pressure ring are used to pressurize the outer splits radially through the threaded parts;
外分瓣的半径与外加压圈的半径相适配,外分瓣至少为三个,置于外加压圈的内侧,周向分布在待成型遮光罩的外圆表面;The radius of the outer split lobe is adapted to the radius of the outer pressure ring, and there are at least three outer split lobes, which are placed on the inner side of the outer pressure ring and circumferentially distributed on the outer surface of the hood to be formed;
水溶性芯模位于周向分布的外分瓣内,水溶性芯模的中心轴处设有连接通孔;The water-soluble mandrel is located in the outer lobes distributed in the circumferential direction, and the central axis of the water-soluble mandrel is provided with a connecting through hole;
定位轴穿过连接通孔,用于连接各个水溶性芯模;The positioning shaft passes through the connecting through hole and is used to connect each water-soluble mandrel;
定位轴分别与上模板和下模板连接。The positioning shafts are respectively connected with the upper template and the lower template.
优选地,上模板的加压通孔均布于上模板的圆周;Preferably, the pressurized through holes of the upper template are evenly distributed on the circumference of the upper template;
下模板的加压通孔均布于下模板的圆周上,使螺杆依次穿过上模板的加压通孔和下模板的加压通孔,通过与螺母配合实现对复合材料遮光罩成型模具的轴向加压。The pressure through holes of the lower template are evenly distributed on the circumference of the lower template, so that the screw rods pass through the pressure through holes of the upper template and the pressure through holes of the lower template in turn, and the pressure through holes of the composite material hood are realized by cooperating with the nut. Axial compression.
优选地,定位轴的两端均设有定位孔,定位孔用于实现定位轴与上模板和下模板的定位和连接。Preferably, both ends of the positioning shaft are provided with positioning holes, and the positioning holes are used for positioning and connecting the positioning shaft with the upper template and the lower template.
优选地,水溶性芯模的外壁设置有凹槽,凹槽的开槽方向指向水溶性芯模的轴心,凹槽用于形成待成型遮光罩内的加强筋型腔。Preferably, the outer wall of the water-soluble core mold is provided with a groove, and the groove direction is directed to the axis of the water-soluble core mold, and the groove is used to form a reinforcing rib cavity in the light shield to be formed.
优选地,上模板、下模板、外加压圈、外分瓣和定位轴均为金属材料。Preferably, the upper template, the lower template, the outer pressure ring, the outer split lobe and the positioning shaft are all metal materials.
一种复合材料遮光罩制备方法,包括步骤:A method for preparing a composite material light shield, comprising the steps of:
S1、按照第一铺层顺序和铺层角度,在水溶性芯模上铺放预浸料;S1, according to the first layup sequence and layup angle, lay the prepreg on the water-soluble mandrel;
S2、将完成铺放预浸料的各个水溶性芯模利用定位轴进行引导穿插,将穿插有水溶性芯模的定位轴的两端与上模板和下模板进行固定;S2. Use the positioning shaft to guide and insert each water-soluble mandrel on which the prepreg has been laid, and fix the two ends of the positioning shaft with the water-soluble mandrel inserted with the upper template and the lower template;
S3、按照第二铺层顺序和铺层角度在完成固定的水溶性芯模的外表面以及上模板上的翻边法兰的成型面进行蒙皮铺放;S3. According to the second layering sequence and layering angle, the skin is laid on the outer surface of the fixed water-soluble core mold and the forming surface of the flanging flange on the upper template;
S4、依次安装外分瓣、外加压圈,完成对复合材料遮光罩成型模具的组装;S4. Install the outer split valve and the outer pressure ring in sequence to complete the assembly of the composite material hood forming mold;
S5、通过成型模具对复合材料遮光罩进行预压实,并进行固化;S5, pre-compacting and curing the composite material hood through the molding die;
S6、完成固化后,拆卸加压圈、外分瓣、上模板、下模板以及定位轴后用水溶去除水溶性芯模。S6. After curing, remove the pressure ring, the outer split, the upper template, the lower template and the positioning shaft, and then remove the water-soluble mandrel with water.
优选地,预浸料的单层厚度均为0.05mm-0.2mm,预浸料中纤维的体积含量为60±3%。Preferably, the thickness of a single layer of the prepreg is 0.05mm-0.2mm, and the volume content of fibers in the prepreg is 60±3%.
优选地,预浸料的纤维为碳纤维、玻璃纤维、石英纤维、高硅氧纤维中的任意一种;Preferably, the fiber of the prepreg is any one of carbon fiber, glass fiber, quartz fiber, and high silica fiber;
预浸料的树脂为氰酸脂树脂、环氧树脂、双马来酰胺树脂、聚酰亚胺树脂、邻苯二甲氰树脂中的任意一种。The resin of the prepreg is any one of cyanate resin, epoxy resin, bismaleamide resin, polyimide resin, and phthalic cyanide resin.
一种复合材料遮光罩,由上述方法制造。A composite material light shield is manufactured by the above method.
本发明能够取得以下技术效果:The present invention can achieve the following technical effects:
1、本发明的超小尺寸复合材料遮光罩、成型模具及其制备方法,能够制备常规工艺无法制作的小尺度复合材料遮光罩器件,通过预浸料铺放工艺一体成型制得,能够克服传统遮光罩蒙皮与加强筋热胀系数不匹配的缺陷,加强筋与蒙皮具有力学性能更佳的优势。1. The ultra-small size composite material light shield, forming mold and preparation method thereof of the present invention can prepare small-scale composite material light shield devices that cannot be produced by conventional processes. The defect of the mismatch of thermal expansion coefficient between the hood skin and the stiffener, the stiffener and the skin have the advantage of better mechanical properties.
2、本发明的超小尺寸复合材料遮光罩、成型模具结构简单,造价低廉,同时可以应用在其他航空航天领域的小尺寸复合材料零部件制备上。2. The ultra-small-sized composite material light shield and the forming mold of the present invention have simple structure and low cost, and can be applied to the preparation of small-sized composite material parts in other aerospace fields.
附图说明Description of drawings
图1是本发明一个实施例的一种复合材料遮光罩成型模具的整体结构示意图;1 is a schematic diagram of the overall structure of a composite material light shield molding die according to an embodiment of the present invention;
图2是图1的A-A处剖视图;Fig. 2 is the sectional view at A-A of Fig. 1;
图3是本发明一个实施例的一种复合材料遮光罩制备方法的流程图;Fig. 3 is a flow chart of a method for preparing a composite light shield according to an embodiment of the present invention;
图4是本发明一个实施例的水溶性芯模上凹槽位置的示意图;Fig. 4 is the schematic diagram of the groove position on the water-soluble mandrel of an embodiment of the present invention;
图5是本发明一个实施例的复合材料遮光罩的示意图。FIG. 5 is a schematic diagram of a composite material light shield according to an embodiment of the present invention.
附图标记:Reference number:
上模板1、下模板2、外加压圈3、压圈螺纹孔31、
外分瓣4、水溶性芯模5、凹槽51、定位轴6、定位孔61、
遮光罩7、加强筋71、凹槽72、翻边8、翻边法兰9、翻边法兰的成型面91。The
具体实施方式Detailed ways
为了使本发明的目的、技术方案及优点更加清楚明白,以下结合附图及具体实施例,对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅用以解释本发明,而不构成对本发明的限制。In order to make the objectives, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.
本发明的目的是提供一种复合材料遮光罩、成型模具及其制备方法。下面将对本发明提供的一种复合材料遮光罩、成型模具及其制备方法,通过具体实施例来进行详细说明。The purpose of the present invention is to provide a composite material light shield, a forming mold and a preparation method thereof. A composite material light shield, a forming mold and a preparation method thereof provided by the present invention will be described in detail below with specific examples.
图1示出了本发明的一种复合材料遮光罩成型模具的整体结构,结合图2,包括:上模板1、下模板2、外加压圈3、外分瓣4、水溶性芯模5和定位轴6;FIG. 1 shows the overall structure of a composite material hood forming mold of the present invention, combined with FIG. 2 , including: an
水溶性芯模5依次串插在定位轴6上,水溶性芯模5及上模板1上的翻边法兰9的外周依次固定有外分瓣4和外加压圈3,外加压圈3通过对外分瓣4的径向加压,实现对水溶性芯模5以及翻边法兰9的径向的紧固;同时通过设置在定位轴6上的定位孔、上模板1和下模板2上的加压通孔,实现上模板1和下模板2的加压和紧固,完成复合材料遮光罩成型模具的组装。The water-
在本发明的一个优选实施例中,水溶性芯模5的中心轴处设置有连接通孔,连接通孔的直径与定位轴6的直径相适配,使各个水溶性芯模5可以串接在定位轴6上。In a preferred embodiment of the present invention, the central axis of the water-
同时,定位轴6的两端设有定位孔,定位孔用于将定位轴6与上模板1和下模板2进行定位,同时利用加压螺栓将三者连接。At the same time, both ends of the
水溶性芯模5的外周设置有三个外分瓣4,三个外分瓣4将水溶性芯模5合围;The outer periphery of the water-
在合围形成的圆柱的三个外分瓣4的外周套有外加压圈3,外加压圈3的周向均布若干个压圈螺纹孔31,压圈螺纹孔31的轴向与外加压圈的径向相同;通过压圈螺纹孔31与相适配的螺栓配合,以及旋紧螺栓实现对外分瓣4的径向加压,使各个外分瓣4与水溶性芯模5间形成的腔体内的复合材料充分接触,保证复合材料成型时的加压压力。An
在上模板1和下模板2的预设区域内对应设置若干个加压通孔,合模时通过加压通孔对复合材料遮光罩成型模具的轴向进行加压,预设区域为内径大于外分瓣4的外径的环形区域;A number of pressurized through holes are correspondingly set in the preset areas of the
在本发明的一个优选实施例中,上模板1的加压通孔均布于上模板1圆周的一个圆上;下模板2的加压通孔均布于下模板2圆周的一个圆上,两个圆上的加压通孔的位置一一对应,使螺杆能够穿过上模板1上的加压通孔、下模板2上的加压通孔,通过与螺母配合实现对复合材料遮光罩成型模具的轴向加压。In a preferred embodiment of the present invention, the pressure through holes of the
为在待成型的遮光罩7内形成如图5所示的加强筋71,在水溶性芯模5的外壁上设置凹槽51,在本发明的一个优选实施例中,如图4所示,将凹槽51设置在水溶性芯模5的两端,以方便在制备遮光罩7时预浸料的铺放。In order to form the reinforcing
为使待成型的遮光罩7具有翻边结构,在上模板1上且与定位轴6固定的一侧,设置翻边法兰。In order to make the
本发明的复合材料遮光罩成型模具的上模板1、下模板2、外加压圈3、外分瓣4和定位轴6均为金属材料,可以选用模具钢或45号钢。The
图3示出了本发明利用上述复合材料遮光罩成型模具制备遮光罩的流程,本发明的复合材料遮光罩通过预浸料铺放工艺一体成型制得,参见图1,包括以下步骤:Fig. 3 shows the process of preparing the light shield by utilizing the above-mentioned composite material light shield molding die of the present invention. The composite material light shield of the present invention is obtained by integral molding through the prepreg laying process. Referring to Fig. 1, the following steps are included:
S1、按照第一铺层顺序和铺层角度,在水溶性芯模上铺放预浸料。S1. Lay the prepreg on the water-soluble mandrel according to the first layup sequence and the layup angle.
具体的,分别在水溶性芯模上铺放至少一层预浸料,在本发明的一个优选的实施例中,预浸料为树脂基纤维增强复合材料。Specifically, at least one layer of prepreg is respectively laid on the water-soluble mandrel. In a preferred embodiment of the present invention, the prepreg is a resin-based fiber reinforced composite material.
预浸料的纤维为碳纤维、玻璃纤维、石英纤维、高硅氧纤维中的任意一种;预浸料的树脂为氰酸脂树脂、环氧树脂、双马来酰胺树脂、聚酰亚胺树脂、邻苯二甲氰树脂中的任意一种;预浸料的单层厚度均为0.05mm-0.2mm,预浸料中纤维的体积含量为60±3%。The fiber of the prepreg is any one of carbon fiber, glass fiber, quartz fiber and high silica fiber; the resin of the prepreg is cyanate resin, epoxy resin, bismaleamide resin, polyimide resin , any one of phthalic cyanide resin; the thickness of the single layer of the prepreg is 0.05mm-0.2mm, and the volume content of the fiber in the prepreg is 60±3%.
S2、将完成铺放预浸料的各个水溶性芯模利用定位轴进行引导穿插,将穿插有水溶性芯模的定位轴与上模板和下模板进行固定。S2. Use the positioning shaft to guide and insert each water-soluble mandrel on which the prepreg has been laid, and fix the positioning shaft inserted with the water-soluble mandrel to the upper template and the lower template.
在本发明的一个优选实施例中,为了使遮光罩7能够与其它部件进行连接,在上模板的一侧设置翻边法兰,使翻边法兰与定位轴上的外分瓣抵接,形成遮光罩7的翻边8。In a preferred embodiment of the present invention, in order to enable the
进一步的,通过定位轴上的定位孔,利用螺栓完成对水溶性芯模同上模板和下模板的固定。Further, through the positioning holes on the positioning shaft, the fixing of the water-soluble mandrel to the upper template and the lower template is completed by using bolts.
S3、按照第二铺层顺序和铺层角度在完成固定水溶性芯模的外表面以及翻边法兰的成型面进行蒙皮的铺放。S3. Lay the skin on the outer surface of the fixed water-soluble core mold and the forming surface of the flanging flange according to the second layering sequence and the layering angle.
在本发明的一个优选实施例中,如图2所示,翻边法兰的成型面91为与外分瓣4相抵接的面。In a preferred embodiment of the present invention, as shown in FIG. 2 , the forming
蒙皮的第二铺层顺序和铺层角度可以同步骤S1中的第一铺层顺序和铺层角度相同或不同,蒙皮为与预浸料组份相同的树脂基纤维增强复合材料。The second layering sequence and layering angle of the skin can be the same as or different from the first layering sequence and layering angle in step S1, and the skin is a resin-based fiber reinforced composite material with the same composition as the prepreg.
S4、依次安装外分瓣、外加压圈,完成对复合材料遮光罩成型模具的组装。S4. Install the outer split valve and the outer pressure ring in sequence to complete the assembly of the composite material hood forming mold.
在完成蒙皮的铺放后,在与上模板和下模板固定的定位轴的外周安装三个外分瓣,在三个外分瓣形成的圆柱体的外表面安装外加压圈,通过压圈螺纹孔,旋紧螺栓对外分瓣进行加压。After the laying of the skin is completed, three outer lobes are installed on the outer circumference of the positioning shaft fixed with the upper template and the lower template, and an outer pressure ring is installed on the outer surface of the cylinder formed by the three outer lobes. Circle the threaded holes, and tighten the bolts to pressurize the outer split.
S5、通过成型模具对复合材料遮光罩进行预压实,并进行固化。S5 , pre-compacting and curing the composite material light shield through a molding die.
在本发明的一个优选实施例中,通过旋紧与压圈螺纹孔配合的螺栓,旋紧与穿过上模板和下模板的螺杆配合的螺母,在径向和轴向上同时实现对复合材料遮光罩的预压实。In a preferred embodiment of the present invention, by tightening the bolts matched with the threaded holes of the pressure ring, and tightening the nuts matched with the screws passing through the upper template and the lower template, the composite material can be compressed in the radial and axial directions at the same time. Pre-compaction of the hood.
S6、完成固化后,拆卸加压圈、外分瓣、上模板、下模板以及定位轴后用水溶去水溶性芯模。S6. After curing, remove the pressure ring, the outer split, the upper template, the lower template and the positioning shaft, and then dissolve the water-soluble mandrel with water.
在本发明的一个优选实施例中,待遮光罩的固化过程完毕后,旋松螺栓,依次拆卸掉加压圈、外分瓣、上模板、下模板以及定位轴,然后用水溶去水溶性芯模,得到如图5所示的超小尺寸复合材料遮光罩。In a preferred embodiment of the present invention, after the curing process of the hood is completed, the bolts are loosened, the pressure ring, the outer splitter, the upper template, the lower template and the positioning shaft are removed in sequence, and then the water-soluble core is removed by dissolving with water. mold to obtain an ultra-small size composite material light shield as shown in Figure 5.
一种复合材料遮光罩,利用上述复合材料遮光罩成型模具,使用上述复合材料遮光罩制备方法制备。A composite material light shield is prepared by using the above-mentioned composite material light shield forming mold and the above-mentioned composite material light shield preparation method.
在本说明书的描述中,参考术语“一个实施例”、“一些实施例”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施例或示例中。在本说明书中,对上述术语的示意性表述不必须针对的是相同的实施例或示例。而且,描述的具体特征、结构、材料或者特点可以在任一个或多个实施例或示例中以合适的方式结合。此外,在不相互矛盾的情况下,本领域的技术人员可以将本说明书中描述的不同实施例或示例以及不同实施例或示例的特征进行结合和组合。In the description of this specification, description with reference to the terms "one embodiment," "some embodiments," "example," "specific example," or "some examples", etc., mean specific features described in connection with the embodiment or example , structure, material or feature is included in at least one embodiment or example of the present invention. In this specification, schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, those skilled in the art may combine and combine the different embodiments or examples described in this specification, as well as the features of the different embodiments or examples, without conflicting each other.
尽管上面已经示出和描述了本发明的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本发明的限制,本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型。Although the embodiments of the present invention have been shown and described above, it should be understood that the above embodiments are exemplary and should not be construed as limiting the present invention. Embodiments are subject to variations, modifications, substitutions and variations.
以上本发明的具体实施方式,并不构成对本发明保护范围的限定。任何根据本发明的技术构思所作出的各种其他相应的改变与变形,均应包含在本发明权利要求的保护范围内。The above specific embodiments of the present invention do not constitute a limitation on the protection scope of the present invention. Any other corresponding changes and modifications made according to the technical concept of the present invention shall be included in the protection scope of the claims of the present invention.
Claims (9)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202111582075.1A CN114311730A (en) | 2021-12-22 | 2021-12-22 | Composite material light shield, forming die and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202111582075.1A CN114311730A (en) | 2021-12-22 | 2021-12-22 | Composite material light shield, forming die and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN114311730A true CN114311730A (en) | 2022-04-12 |
Family
ID=81054373
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202111582075.1A Pending CN114311730A (en) | 2021-12-22 | 2021-12-22 | Composite material light shield, forming die and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114311730A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117656539A (en) * | 2024-02-02 | 2024-03-08 | 哈尔滨远驰航空装备有限公司 | Composite material adapter, forming die and method |
Citations (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10233697A1 (en) * | 2002-12-05 | 2004-02-19 | East-4D-Gmbh Lightweight Structures | Centrifuge body for laboratory and industrial centrifuges is made from a material containing axially/radially and tangentially arranged reinforcing fibers |
CN101450533A (en) * | 2007-11-30 | 2009-06-10 | 航天材料及工艺研究所 | Carbon fiber reinforcement resin base composite material lattice structural-component conforming die and method |
CN101697035A (en) * | 2009-11-03 | 2010-04-21 | 哈尔滨玻璃钢研究院 | Forming method of fiber reinforced resin base compound material hood with inner grating |
CN201471634U (en) * | 2009-09-09 | 2010-05-19 | 哈尔滨玻璃钢研究院 | Forming die of hollow enclosed element of inner grid reinforced composite material |
CN103407175A (en) * | 2013-07-30 | 2013-11-27 | 北京航空航天大学 | Integrally-forming method of wing box made of fiber reinforced resin matrix composites |
CN103722753A (en) * | 2014-01-02 | 2014-04-16 | 厦门欧势复材科技有限公司 | Production technology of carbon fibre composite material rim |
CN104385624A (en) * | 2014-09-29 | 2015-03-04 | 北京空间机电研究所 | Forming method for composite material barrel shell employing horizontal installation |
CN204398343U (en) * | 2014-12-05 | 2015-06-17 | 上海复合材料科技有限公司 | Frame-type light shield shaping mould |
CN105128355A (en) * | 2015-08-26 | 2015-12-09 | 航天材料及工艺研究所 | Auxiliary integral forming method for composite material bearing cylinder soft mould with light baffle ring |
CN106976250A (en) * | 2017-04-10 | 2017-07-25 | 江苏恒神股份有限公司 | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product and uses step |
CN108274780A (en) * | 2018-04-02 | 2018-07-13 | 天津工业大学 | A kind of forming method of hollow composite |
CN108501398A (en) * | 2018-03-16 | 2018-09-07 | 航天材料及工艺研究所 | A kind of composite material casing, molding die and the forming method of the window containing in-flanges |
CN108705785A (en) * | 2018-05-03 | 2018-10-26 | 航天特种材料及工艺技术研究所 | A composite material spiral tube, forming mold and forming process |
CN208083251U (en) * | 2018-03-28 | 2018-11-13 | 东莞市正太合众金属包装自动化设备有限公司 | A kind of tank body expansion hemmer |
CN108891040A (en) * | 2018-06-21 | 2018-11-27 | 西安爱生技术集团公司 | A kind of small and medium size unmanned aerial vehicles composite horizontal empennage manufacturing method |
CN108928013A (en) * | 2018-07-12 | 2018-12-04 | 台州市中冠模业有限公司 | A kind of variable cross-section shaped spiral housing mold |
JP2018202753A (en) * | 2017-06-05 | 2018-12-27 | 株式会社岩間工業所 | Method for manufacturing carbon fiber reinforced resin member |
CN109249627A (en) * | 2018-08-17 | 2019-01-22 | 武汉源海博创科技有限公司 | A kind of carbon fibre composite propeller die press technology for forming |
CN109895417A (en) * | 2019-03-27 | 2019-06-18 | 成都联科航空技术有限公司 | The variable cross-section hollow structure composite material parts forming method of high-precision outer surface |
CN110312613A (en) * | 2017-02-09 | 2019-10-08 | 中车青岛四方机车车辆股份有限公司 | By fibrous composite manufacture hollow beam method, be configured to ducted body core and its application and the hollow beam made of fibrous composite application |
CN110561782A (en) * | 2019-08-26 | 2019-12-13 | 长春长光宇航复合材料有限公司 | Composite material secondary curing molding method based on internal grid rib structure and application |
CN110978562A (en) * | 2019-11-28 | 2020-04-10 | 长春长光宇航复合材料有限公司 | Preparation method of high-temperature-resistant composite material cabin section |
CN111959002A (en) * | 2020-07-02 | 2020-11-20 | 林书伟 | Method for manufacturing bicycle parts made of composite materials |
CN113510939A (en) * | 2021-08-10 | 2021-10-19 | 上海复合材料科技有限公司 | Diaphragm type lens hood forming die |
-
2021
- 2021-12-22 CN CN202111582075.1A patent/CN114311730A/en active Pending
Patent Citations (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10233697A1 (en) * | 2002-12-05 | 2004-02-19 | East-4D-Gmbh Lightweight Structures | Centrifuge body for laboratory and industrial centrifuges is made from a material containing axially/radially and tangentially arranged reinforcing fibers |
CN101450533A (en) * | 2007-11-30 | 2009-06-10 | 航天材料及工艺研究所 | Carbon fiber reinforcement resin base composite material lattice structural-component conforming die and method |
CN201471634U (en) * | 2009-09-09 | 2010-05-19 | 哈尔滨玻璃钢研究院 | Forming die of hollow enclosed element of inner grid reinforced composite material |
CN101697035A (en) * | 2009-11-03 | 2010-04-21 | 哈尔滨玻璃钢研究院 | Forming method of fiber reinforced resin base compound material hood with inner grating |
CN103407175A (en) * | 2013-07-30 | 2013-11-27 | 北京航空航天大学 | Integrally-forming method of wing box made of fiber reinforced resin matrix composites |
CN103722753A (en) * | 2014-01-02 | 2014-04-16 | 厦门欧势复材科技有限公司 | Production technology of carbon fibre composite material rim |
CN104385624A (en) * | 2014-09-29 | 2015-03-04 | 北京空间机电研究所 | Forming method for composite material barrel shell employing horizontal installation |
CN204398343U (en) * | 2014-12-05 | 2015-06-17 | 上海复合材料科技有限公司 | Frame-type light shield shaping mould |
CN105128355A (en) * | 2015-08-26 | 2015-12-09 | 航天材料及工艺研究所 | Auxiliary integral forming method for composite material bearing cylinder soft mould with light baffle ring |
CN110312613A (en) * | 2017-02-09 | 2019-10-08 | 中车青岛四方机车车辆股份有限公司 | By fibrous composite manufacture hollow beam method, be configured to ducted body core and its application and the hollow beam made of fibrous composite application |
CN106976250A (en) * | 2017-04-10 | 2017-07-25 | 江苏恒神股份有限公司 | It is molded the Wound Dies of inside grid reinforced cylindrical shell structure product and uses step |
JP2018202753A (en) * | 2017-06-05 | 2018-12-27 | 株式会社岩間工業所 | Method for manufacturing carbon fiber reinforced resin member |
CN108501398A (en) * | 2018-03-16 | 2018-09-07 | 航天材料及工艺研究所 | A kind of composite material casing, molding die and the forming method of the window containing in-flanges |
CN208083251U (en) * | 2018-03-28 | 2018-11-13 | 东莞市正太合众金属包装自动化设备有限公司 | A kind of tank body expansion hemmer |
CN108274780A (en) * | 2018-04-02 | 2018-07-13 | 天津工业大学 | A kind of forming method of hollow composite |
CN108705785A (en) * | 2018-05-03 | 2018-10-26 | 航天特种材料及工艺技术研究所 | A composite material spiral tube, forming mold and forming process |
CN108891040A (en) * | 2018-06-21 | 2018-11-27 | 西安爱生技术集团公司 | A kind of small and medium size unmanned aerial vehicles composite horizontal empennage manufacturing method |
CN108928013A (en) * | 2018-07-12 | 2018-12-04 | 台州市中冠模业有限公司 | A kind of variable cross-section shaped spiral housing mold |
CN109249627A (en) * | 2018-08-17 | 2019-01-22 | 武汉源海博创科技有限公司 | A kind of carbon fibre composite propeller die press technology for forming |
CN109895417A (en) * | 2019-03-27 | 2019-06-18 | 成都联科航空技术有限公司 | The variable cross-section hollow structure composite material parts forming method of high-precision outer surface |
CN110561782A (en) * | 2019-08-26 | 2019-12-13 | 长春长光宇航复合材料有限公司 | Composite material secondary curing molding method based on internal grid rib structure and application |
CN110978562A (en) * | 2019-11-28 | 2020-04-10 | 长春长光宇航复合材料有限公司 | Preparation method of high-temperature-resistant composite material cabin section |
CN111959002A (en) * | 2020-07-02 | 2020-11-20 | 林书伟 | Method for manufacturing bicycle parts made of composite materials |
CN113510939A (en) * | 2021-08-10 | 2021-10-19 | 上海复合材料科技有限公司 | Diaphragm type lens hood forming die |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117656539A (en) * | 2024-02-02 | 2024-03-08 | 哈尔滨远驰航空装备有限公司 | Composite material adapter, forming die and method |
CN117656539B (en) * | 2024-02-02 | 2024-04-19 | 哈尔滨远驰航空装备有限公司 | Composite material adapter, forming die and method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN110722811B (en) | Integrated forming method for composite skirt and shell of solid rocket engine | |
CN108501398B (en) | A composite material shell containing an inner flanging window, a molding die and a molding method | |
CN101870172B (en) | Preparation mould of carbon fiber composite material casing of airplane and aircraft and forming method thereof | |
CN110355333A (en) | One kind being used for solid rocket motor case forming metal core mold structure | |
US5474721A (en) | Method of forming an expanded composite | |
CN105252751A (en) | Winding forming die for cylinder | |
JP2017530882A (en) | Method for releasing a composite material having an organic matrix | |
CN111745996B (en) | Preparation method of fiber-wound solid rocket engine shell | |
JP6367242B2 (en) | Injection mold for producing rotating parts, especially gas turbine casings, made of composite material with external flange | |
CN114311730A (en) | Composite material light shield, forming die and preparation method thereof | |
CN111376389A (en) | A kind of cylindrical composite material component forming mold with flange and preparation method | |
CN112644039A (en) | Large-opening composite material shell, forming method and forming tool | |
CN113650199A (en) | A split composite mandrel for solid rocket motor casing winding | |
CN110815851A (en) | A kind of molding method of revolving body composite material component | |
CN215397021U (en) | Big open-ended combined material casing and shaping frock | |
CN110524915A (en) | A kind of socket forming frock and socket forming method | |
US4248649A (en) | Method for producing a composite structure | |
CN114375251A (en) | Method for closing injection molding mold using anti-pinching tape | |
CN106217902A (en) | A kind of automatically spread the device twining technique for Composites Lattice Structure | |
JP4227299B2 (en) | Manufacturing method of flanged tubular product made of fiber reinforced plastic | |
CN112060617A (en) | Composite hollow curved tube, forming die and preparation method | |
CN114951555B (en) | Tandem type water-soluble sand core mould and manufacturing method thereof | |
CN205185294U (en) | Barrel winding forming die | |
CN111196045B (en) | Integral winding forming method suitable for hollow structure and hollow structure | |
CN107901448B (en) | Large-diameter composite skirt compression curing method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20220412 |