CN104742382A - Pressure-assisted VARI (vacuum assisted resin infusion) forming device and method - Google Patents
Pressure-assisted VARI (vacuum assisted resin infusion) forming device and method Download PDFInfo
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- CN104742382A CN104742382A CN201510170911.3A CN201510170911A CN104742382A CN 104742382 A CN104742382 A CN 104742382A CN 201510170911 A CN201510170911 A CN 201510170911A CN 104742382 A CN104742382 A CN 104742382A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
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Abstract
本发明提供了一种压力辅助VARI成型装置及方法,它涉及一种用外加压力辅助VARI成型的装置。压力辅助VARI成型装置包括成型上下模具、上下模具固定装置、加压装置、真空泵和树脂注入装置。本发明解决了现有VARI成型制品由于真空加压不足,造成复合材料纤维体积含量相对不高,制品中存在孔隙、干斑等缺陷,无法满足高性能复合材料结构要求的问题。本发明发挥了热压罐加压固化的优点,弥补了VARI成型真空加压的不足,扬长避短,进而能充分发挥VARI工艺在降低复合材料制造成本及大型构件整体成型方面的优势。
The invention provides a pressure-assisted VARI forming device and method, which relates to a device for assisting VARI forming with external pressure. The pressure-assisted VARI molding device includes molding upper and lower molds, upper and lower mold fixing devices, pressurizing devices, vacuum pumps and resin injection devices. The invention solves the problem that existing VARI shaped products cannot meet the structural requirements of high-performance composite materials because of insufficient vacuum pressure, resulting in relatively low fiber volume content of composite materials, defects such as pores and dry spots in the products. The invention utilizes the advantages of pressurization and solidification in an autoclave, makes up for the deficiency of vacuum pressurization in VARI forming, maximizes strengths and circumvents weaknesses, and furthermore can give full play to the advantages of VARI technology in reducing the manufacturing cost of composite materials and integrally forming large components.
Description
技术领域technical field
本发明涉及一种用外加压力辅助真空灌注工艺成型的装置及方法,属于复合材料成型技术领域。The invention relates to a device and a method for forming with an external pressure-assisted vacuum infusion process, and belongs to the technical field of composite material forming.
背景技术Background technique
由于先进复合材料具有比强度和比模量高、优异的可设计性和良好的抗疲劳性等诸多优点,已广泛应用于航空航天、风机叶片、交通运输、建筑、体育用品及机电工业等领域。就航空航天领域,先进复合材料可以实现飞机结构的整体减重,提高飞机的综合性能,复合材料用量的高低成为衡量飞行器先进性的重要指标。这些为各种新材料、新工艺展现提供了宽广的舞台,但是复合材料面临一个最突出的问题是成本过高,这在一定程度上限制了树脂基复合材料应用的进一步扩大。Because advanced composite materials have many advantages such as high specific strength and specific modulus, excellent designability and good fatigue resistance, they have been widely used in aerospace, fan blades, transportation, construction, sporting goods and electromechanical industries. . In the field of aerospace, advanced composite materials can reduce the overall weight of the aircraft structure and improve the overall performance of the aircraft. The amount of composite materials has become an important indicator to measure the advanced nature of aircraft. These provide a broad stage for the display of various new materials and new processes, but the most prominent problem faced by composite materials is the high cost, which limits the further expansion of the application of resin-based composite materials to a certain extent.
真空辅助树脂灌注成型工艺(真空灌注工艺,以下简称为VARI)以其低成本、高质量、工艺方法灵活的优势逐渐成为制备大尺寸、大厚度复杂制件的新型方法。它是在真空条件下,利用树脂的流动渗透实现对纤维及其织物的浸渍,并在真空下固化的成型方法,该工艺已成功用于舰船、军事设施、国防工程、航空和风电等民用工业领域。但是,现有VARI成型制品由于真空加压不足,造成复合材料纤维体积含量相对不高,制品中存在孔隙、干斑等缺陷,无法满足高性能复合材料结构要求的问题。因此,开发和构建新的复合材料成型工艺方法无疑对复合材料的发展起着重要的作用。Vacuum-assisted resin infusion molding process (vacuum infusion process, hereinafter referred to as VARI) has gradually become a new method for preparing large-size, large-thickness complex parts due to its advantages of low cost, high quality, and flexible process methods. It is a molding method that uses the flow and penetration of resin to impregnate fibers and their fabrics under vacuum conditions and solidify them under vacuum. This process has been successfully used in civilian applications such as ships, military facilities, national defense projects, aviation and wind power. industrial field. However, due to insufficient vacuum pressure, the existing VARI molded products result in relatively low fiber volume content of the composite material, and there are defects such as pores and dry spots in the product, which cannot meet the structural requirements of high-performance composite materials. Therefore, the development and construction of new composite material forming process methods undoubtedly play an important role in the development of composite materials.
发明内容Contents of the invention
本发明要解决的技术问题是进行加压辅助VARI成型,以满足复合材料成型低成本、高性能的要求。The technical problem to be solved by the invention is to carry out pressure-assisted VARI molding to meet the requirements of low cost and high performance for composite material molding.
为了解决上述技术问题,本发明的一个技术方案是提供了一种压力辅助真空灌注工艺成型装置,其特征在于,包括可开合的上模具及下模具,在上模具上设有沿高度方向贯穿整个上模具的压力注入口,真空灌注工艺成型部件位于下模具的腔体内,在下模具位于腔体两侧的部分上分别开有与下模具的型腔相通的树脂注入口及抽真空口,其中,压力注入口与加压装置相连通,树脂注入口与树脂体系相连通,抽真空口经树脂收集器与真空泵相连通。In order to solve the above technical problems, a technical solution of the present invention is to provide a pressure-assisted vacuum infusion process molding device, which is characterized in that it includes an openable upper mold and a lower mold, and the upper mold is provided with a The pressure injection port of the entire upper mold, the vacuum infusion process molding parts are located in the cavity of the lower mold, and the parts of the lower mold located on both sides of the cavity are respectively provided with a resin injection port and a vacuum port communicating with the cavity of the lower mold. , the pressure injection port is connected with the pressurizing device, the resin injection port is connected with the resin system, and the vacuum port is connected with the vacuum pump through the resin collector.
优选地,所述上模具及下模具分别固定在各自的固定装置上,在固定装置处均设置有用于保证上模具的气密性或下模具的气密性的密封条。Preferably, the upper mold and the lower mold are respectively fixed on respective fixing devices, and sealing strips for ensuring the airtightness of the upper mold or the airtightness of the lower mold are provided at the fixing devices.
优选地,所述固定装置为螺栓,在所述上模具或所述下模具的四周分别对应等距预留用于固定螺栓的螺栓孔。Preferably, the fixing device is a bolt, and bolt holes for fixing bolts are correspondingly and equidistantly reserved around the upper mold or the lower mold.
优选地,复合材料部件位于所述下模具腔体内的中央,所述真空灌注工艺成型部件包括自下而上铺放的脱模布及真空袋薄膜一,流动介质位于脱模布与真空袋薄膜一之间。Preferably, the composite material part is located in the center of the lower mold cavity, and the vacuum infusion process forming part includes a release cloth and a vacuum bag film laid from bottom to top, and the flow medium is located between the release cloth and the vacuum bag film. between one.
优选地,所述真空袋薄膜的边缘通过密封胶粘在所述下模具上。Preferably, the edges of the vacuum bag film are glued to the lower mold by sealing glue.
优选地,在所述真空灌注工艺成型装置的外面铺放一层真空袋薄膜二。Preferably, a layer of vacuum bag film 2 is laid on the outside of the vacuum infusion process forming device.
本发明的另一个技术方案是提供了一种基于上述的压力辅助真空灌注工艺成型装置的压力辅助真空灌注工艺成型方法,其特征在于,在所述下模具的腔体中央放置复合材料部件,随后铺放一套完整的真空灌注工艺成型部件,待上模具与下模具合模后,通过抽真空口抽真空,树脂经由树脂注入口注入,完成树脂灌注后,加压装置通过压力注入口加压,直到复合材料固化。Another technical solution of the present invention is to provide a pressure-assisted vacuum infusion process forming method based on the above-mentioned pressure-assisted vacuum infusion process forming device, which is characterized in that a composite material part is placed in the center of the cavity of the lower mold, and then Lay a complete set of vacuum infusion process molding parts. After the upper mold and the lower mold are closed, the vacuum is drawn through the vacuum port, and the resin is injected through the resin injection port. After the resin infusion is completed, the pressurizing device pressurizes through the pressure injection port. until the composite is cured.
优选地,具体包括如下步骤:Preferably, it specifically includes the following steps:
步骤1、在下模具腔体内的中央喷涂脱模剂,将裁剪完毕的碳纤维布铺放在涂有脱模剂的位置上,并铺放脱模布及流动介质,在碳纤维布四周黏上密封胶,之后铺放真空袋薄膜一,形成真空灌注工艺成型部件,预留抽真空口和树脂注入口,检验并保证真空灌注工艺成型部件的气密性,然后,在上模具及下模具上铺放密封胶条,闭合上模具及下模具并将其用固定装置固定;Step 1. Spray the release agent in the center of the lower mold cavity, place the cut carbon fiber cloth on the position coated with the release agent, and lay the release cloth and flow medium, and stick the sealant around the carbon fiber cloth , and then lay the vacuum bag film 1 to form a vacuum infusion process molding part, reserve a vacuum port and a resin injection port, check and ensure the airtightness of the vacuum infusion process molding part, and then lay it on the upper mold and the lower mold Sealing strips, closing the upper mold and the lower mold and fixing them with fixtures;
步骤2、用真空泵对下模具中的真空灌注工艺成型部件抽真空,保压一段时间,检测真空度;Step 2. Use a vacuum pump to evacuate the parts formed by the vacuum infusion process in the lower mold, hold the pressure for a period of time, and detect the degree of vacuum;
步骤3、真空度达标后,从树脂注入口灌入树脂,直到树脂灌满整个碳纤维布;Step 3. After the vacuum reaches the standard, pour resin from the resin injection port until the resin fills the entire carbon fiber cloth;
步骤4、待树脂灌入完毕后,加压装置通过压力注入口加压,直至树脂固化后,形成复合材料部件。Step 4. After the resin is poured in, the pressurizing device pressurizes through the pressure injection port until the resin is solidified to form a composite material part.
本发明的优点是:与现有的VARI成型方式相比,本发明外加了压力辅助装置,其纤维体积含量会明显提高,并且孔隙等缺陷会明显减少;与现有的热压罐成型方法相比,本发明不需要热压设备的高投入,并且成型过程相对简单,可大大减少复合材料成型的成本。所完成的复合材料部件性能明显提高,成本显著下降,具有广阔的应用前景。The advantages of the present invention are: compared with the existing VARI forming method, the present invention adds a pressure auxiliary device, its fiber volume content will be significantly increased, and defects such as pores will be significantly reduced; compared with the existing autoclave forming method Compared with this method, the present invention does not require high investment in hot pressing equipment, and the molding process is relatively simple, which can greatly reduce the cost of composite material molding. The performance of the completed composite material component is obviously improved, the cost is significantly reduced, and the composite material has broad application prospects.
附图说明Description of drawings
图1是本发明压力辅助VARI成型装置示意图;Fig. 1 is the schematic diagram of pressure-assisted VARI forming device of the present invention;
图2是整体成型模具结构示意图;Fig. 2 is a structural schematic diagram of an integral molding die;
图3是下模具中VARI成型示意图;Fig. 3 is a schematic diagram of VARI molding in the lower mold;
其中,1.上模具2.下模具3.压力注入口4.树脂注入口5.抽真空口6.上下模具固定装置7.树脂体系8.加压装置9.树脂收集器10.真空泵11.复合材料部件12.脱模布13.流动介质14.真空袋薄膜15.真空袋薄膜16.密封胶。Among them, 1. Upper mold 2. Lower mold 3. Pressure injection port 4. Resin injection port 5. Vacuum port 6. Upper and lower mold fixing devices 7. Resin system 8. Pressurizing device 9. Resin collector 10. Vacuum pump 11. Composite part 12. Release cloth 13. Flow medium 14. Vacuum bag film 15. Vacuum bag film 16. Sealant.
具体实施方式Detailed ways
为使本发明更明显易懂,兹以优选实施例,并配合附图作详细说明如下。In order to make the present invention more comprehensible, preferred embodiments are described in detail below with accompanying drawings.
请参阅图1,其是本发明压力辅助VARI成型装置示意图。所述压力辅助VARI成型装置包括上模具1、下模具2、压力注入口3、树脂注入口4、抽真空口5,以及上下模具的固定装置6,其中上下模具的固定装置6处均有密封条,并且用等间距的螺栓固定。Please refer to FIG. 1 , which is a schematic diagram of a pressure-assisted VARI forming device of the present invention. The pressure-assisted VARI molding device includes an upper mold 1, a lower mold 2, a pressure injection port 3, a resin injection port 4, a vacuum port 5, and a fixing device 6 of the upper and lower molds, wherein the fixing devices 6 of the upper and lower molds are sealed strips and fastened with equally spaced bolts.
请参阅图2,其是本发明整体成型模具结构示意图。所述的整体成型模具包括树脂体系7、加压装置8、树脂收集器9和真空泵10,其中树脂体系7与树脂注入口4相连,加压装置8与压力注入口3相连,树脂收集器9与抽真空口5相连,并连接至真空泵10上。Please refer to FIG. 2 , which is a structural schematic view of the integral molding die of the present invention. The integral forming mold includes a resin system 7, a pressurizing device 8, a resin collector 9 and a vacuum pump 10, wherein the resin system 7 is connected with the resin injection port 4, the pressurizing device 8 is connected with the pressure injection port 3, and the resin collector 9 It is connected to the vacuum port 5 and connected to the vacuum pump 10.
请参阅图3,其是本发明下模具2中VARI成型示意图。所述的VARI成型示意图包括复合材料部件11、脱模布12、流动介质13、真空袋薄膜一14、真空袋薄膜二15、密封胶16。Please refer to FIG. 3 , which is a schematic diagram of VARI forming in the lower mold 2 of the present invention. The VARI forming schematic diagram includes a composite material part 11 , a release cloth 12 , a flow medium 13 , a vacuum bag film one 14 , a vacuum bag film two 15 , and a sealant 16 .
复合材料部件在下模具2中进行VARI成型,并通过上模具1中的加压装置8实现对VARI成型的加压固化。其具体步骤如下:The composite material part is subjected to VARI molding in the lower mold 2, and the pressure curing of the VARI molding is realized through the pressing device 8 in the upper mold 1. The specific steps are as follows:
步骤1、提供包括密封胶条、固定装置6、形状尺寸合适的成型模具;Step 1, providing a forming mold including a sealing strip, a fixing device 6, and a suitable shape and size;
步骤2、在下模具2中央喷涂脱模剂,将裁剪完毕的碳纤维布铺放涂有脱模剂的位置,并铺放脱模布12、流动介质13,在碳纤维布四周黏上密封胶16,之后铺放真空袋薄膜一14及真空袋薄膜二15,预留抽真空口5和树脂注入口4,检验并保证装置的气密性;然后在上模具1及下模具2上铺放密封胶条,闭合上模具1、下模具2并将其用固定装置6固定。Step 2. Spray the release agent on the center of the lower mold 2, lay the cut carbon fiber cloth on the position coated with the release agent, and lay the release cloth 12, the flow medium 13, and stick the sealant 16 around the carbon fiber cloth, Lay vacuum bag film one 14 and vacuum bag film two 15 afterwards, reserve vacuum port 5 and resin injection port 4, check and ensure the airtightness of the device; then lay sealant on upper mold 1 and lower mold 2 strip, close the upper mold 1, the lower mold 2 and fix it with the fixture 6.
步骤3、用真空泵10对下模具2中的VARI装置抽真空,保压一段时间,检测真空度。Step 3, vacuumize the VARI device in the lower mold 2 with a vacuum pump 10, keep the pressure for a period of time, and check the degree of vacuum.
步骤4真空度达标后,从树脂注入口4灌入树脂,直到树脂灌满整个碳纤维布。Step 4: After the vacuum reaches the standard, pour resin from the resin injection port 4 until the resin fills the entire carbon fiber cloth.
步骤5待树脂灌入完毕,从压力注入口3打压力。Step 5 After the resin is poured in, apply pressure from the pressure injection port 3.
步骤6固化树脂,形成复合材料部件。Step 6 Cures the resin to form the composite part.
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CN104999675A (en) * | 2015-07-06 | 2015-10-28 | 湖北三江航天红阳机电有限公司 | Preparation method of small-sized thermal protective composite material screws |
CN106338417A (en) * | 2015-09-01 | 2017-01-18 | 湖北航天化学技术研究所 | Solid propellant pressure curing detection sample die tool |
CN107914406A (en) * | 2017-11-16 | 2018-04-17 | 江苏恒神股份有限公司 | A kind of new vacuum imports shaping big height difference product device and process |
CN108162433A (en) * | 2018-03-01 | 2018-06-15 | 江苏金风科技有限公司 | Priming by vacuum auxiliary device and vacuum perfusion process |
CN109177236A (en) * | 2018-11-05 | 2019-01-11 | 陕西碳能新材料有限责任公司 | A kind of abnormity composite material battery case molding die and forming method |
CN112644040A (en) * | 2020-12-29 | 2021-04-13 | 百佳瑞航天航空新材料(苏州)有限公司 | Low-cost liquid forming test plate manufacturing process |
CN114102802A (en) * | 2021-11-29 | 2022-03-01 | 航天特种材料及工艺技术研究所 | A large-sized special-shaped thermal insulation member forming device and preparation method |
CN114102802B (en) * | 2021-11-29 | 2023-01-20 | 航天特种材料及工艺技术研究所 | Forming device and preparation method of large-size special-shaped heat insulation component |
CN117532912A (en) * | 2023-11-27 | 2024-02-09 | 江苏赛欧环保设备有限公司 | Vacuum filling process for processing air duct |
CN117532912B (en) * | 2023-11-27 | 2024-04-26 | 江苏赛欧环保设备有限公司 | Vacuum filling process for processing air duct |
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