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Simulation of the Resin Film Infusion Process Based on the Finite Element Method
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作者 杨梅 晏石林 《Journal of Wuhan University of Technology(Materials Science)》 SCIE EI CAS 2006年第4期180-182,共3页
A physically accurate and computationally effective pure finite element method (FEM) was developed to simulate the isothermal resin infusing process. The FEM was based on conservation of resin muss at and instant of... A physically accurate and computationally effective pure finite element method (FEM) was developed to simulate the isothermal resin infusing process. The FEM was based on conservation of resin muss at and instant of time and was objective of resin film infusion (RFI) fiber impregnation and mold filling . The developed computer code was able to simulate the resin infusing visually. A numerical example presented here demonstrated that compared with traditional finite element/ control-volume (FE/CV), and FEM was physically accurate and computationally efficient. 展开更多
关键词 resin film infusion finite element method control-volume/finite element
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Formulating Novel Halogen-Free Synergistic Flame Retardant Epoxy Resins for Vacuum Assisted Resin Infusion Composites
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作者 WANG Ming WEI Yi QIU Yiping 《Journal of Donghua University(English Edition)》 CAS 2022年第2期120-127,共8页
The most common process to manufacture advanced composites is the costly autoclave.One of the out-of-autoclave alternatives is the low-cost vacuum assisted resin infusion(VARI)which produces quality parts with less po... The most common process to manufacture advanced composites is the costly autoclave.One of the out-of-autoclave alternatives is the low-cost vacuum assisted resin infusion(VARI)which produces quality parts with less pollution.Epoxy resin is a widely used composite matrix resin,but its high flammability limits its use as interior composite parts for vehicles.The usual flame retardant for epoxy involves halogen,which is effective but has high smoke toxicity.As a result,halogen-free flame retardant epoxy resin systems become dominant.In this paper,phosphorus flame retardant was combined with benzoxazine(BOZ)to produce synergistic effect and achieve satisfactory flame retardance,as well as mechanical improvement for the epoxy resin.Differential scanning calorimetry(DSC),dynamic mechanical analysis(DMA),thermal gravitational analysis(TGA),the cone calorimeter(CC),and limiting oxygen index(LOI)were used to characterize the resins.The results showed significant improvement on the flame retardance of the synergistically modified resins.Specifically,the carbon residue increased by 113.6%,and the char thickness increased by 6 to 7 times,compared to those of the flammable benchmark resin.The LOI reached 33 and passed the UL94 V-0 vertical burn rating.The modified resins also exhibited adequate stability and viscosity suitable for VARI processes. 展开更多
关键词 synergistic flame retardant EPOXY benzoxazine(BOZ) vacuum assisted resin infusion(VARI) composite
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Part Thickness Variation during the Vacuum Assisted Resin Infusion Process
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作者 潘利剑 王英男 +3 位作者 王召召 刘宇婷 段振锦 胡秀凤 《Journal of Donghua University(English Edition)》 EI CAS 2016年第4期673-677,共5页
An experimental procedure was designed to monitor the preform thickness change real-time throughout the vacuum assisted resin infusion( VARI) process. Two kinds of liquid with different viscosity were infused with dif... An experimental procedure was designed to monitor the preform thickness change real-time throughout the vacuum assisted resin infusion( VARI) process. Two kinds of liquid with different viscosity were infused with different post-filling time. The variation of the part thickness during the VARI process was studied. And the effect of the post-filling time on the part thickness was investigated.The results indicate that the compaction behavior of the preform can be divided into three stages,and the fiber volume fraction varies with the post-filling time in a similar sinusoid form. In addition,the post-filling should be overtime for the greatest fiber volume fraction,and when the resin is infused with higher viscosity,the greatest fiber volume fraction is higher. 展开更多
关键词 filling compaction resin viscosity VARI infusion relaxation saturated reservoir inlet
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Rheological Behaviors and Processing Windows of Low Viscosity Epoxy Resin for VIMP 被引量:2
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作者 刘卓峰 《Journal of Wuhan University of Technology(Materials Science)》 SCIE EI CAS 2011年第5期931-934,共4页
The chemorheological behaviors of a low viscosity epoxy resin system (Huntsman 1564/3486) for vacuum infusion moulding process (VIMP) were studied with viscosity experiments.The dual-Arrhenius rheological model an... The chemorheological behaviors of a low viscosity epoxy resin system (Huntsman 1564/3486) for vacuum infusion moulding process (VIMP) were studied with viscosity experiments.The dual-Arrhenius rheological model and the engineering viscosity model were established and compared with the experimental data.The result showed that the viscosity in the earlier stage calculated by dual-Arrhenius model were smaller than the experimental data,while the data calculated by the engineering model were larger.Combining the two models together can predict the rheological behaviors of the resin system in a more credible manner.The processing windows of the resin system for VIMP were determined based on the two models.The optimum processing temperature is 30-45 ℃. 展开更多
关键词 vacuum infusion molding process(VIMP) epoxy resin rheological behaviors
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基于真空导入工艺的大尺度复合材料异型构件成型技术研究
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作者 丁萍 张作朝 +1 位作者 郑宏雪 柴朋军 《纤维复合材料》 CAS 2024年第1期45-52,共8页
研究了大尺寸复合材料水滴形截面异型构件的成型工艺。在达西定律的基础上采用实验法测得了玻璃纤维织物渗透率,建立了树脂浸润过程的仿真模型。采用仿真软件对典型构件一体成型充模过程进行仿真分析,分别对中心点注射、中心线注射、单... 研究了大尺寸复合材料水滴形截面异型构件的成型工艺。在达西定律的基础上采用实验法测得了玻璃纤维织物渗透率,建立了树脂浸润过程的仿真模型。采用仿真软件对典型构件一体成型充模过程进行仿真分析,分别对中心点注射、中心线注射、单边注射和多线程接力注射方案进行探讨,仿真结果表明,多线程接力注射方案可有效缩短充模时间,满足树脂适用期内完成充模的要求,并达到100%充模率。采用多线程接力注射方案制备了典型构件样机,实际充模时间与理论计算相差约10%,对生产实践具有指导性意义。 展开更多
关键词 复合材料 大尺度 异型构件 SCRIMP 仿真模拟
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孔槽泡沫夹芯复合材料真空辅助树脂传递工艺仿真与优化 被引量:1
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作者 杨张韬 倪爱清 +1 位作者 王继辉 冯雨薇 《材料导报》 EI CSCD 北大核心 2024年第2期249-257,共9页
本工作提出了孔槽泡沫夹芯复合材料的设计方案并针对真空辅助树脂传递(VARI)工艺进行了实验和仿真研究。首先,通过实验测得玻璃纤维织物和树脂的相关参数,利用Hagen-Poiseuill方程和达西定律算出孔洞和沟槽的等效渗透率;接着,利用PAM-RT... 本工作提出了孔槽泡沫夹芯复合材料的设计方案并针对真空辅助树脂传递(VARI)工艺进行了实验和仿真研究。首先,通过实验测得玻璃纤维织物和树脂的相关参数,利用Hagen-Poiseuill方程和达西定律算出孔洞和沟槽的等效渗透率;接着,利用PAM-RTM模拟孔槽泡沫夹芯复合材料的VARI工艺过程,并与实验结果进行对比;然后,使用PAM-RTM研究了芯材加工参数、树脂灌注方式和导流网铺敷区域对成型过程的影响,并选出了最优方案;最后,在此方案的基础上研究了树脂黏度与灌注时间的关系,并拟合得到了预测函数。结果表明:实验结果与仿真结果基本一致;最优灌注方案可显著缩短树脂填充时间并降低整体孔隙率;预测函数可准确预测灌注时间,对实际生产具有一定的指导意义。 展开更多
关键词 夹芯复合材料 等效渗透率 真空辅助树脂传递 芯材加工 工艺优化 孔隙率
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Investigation of carbon fiber composite stiffened skin with vacuum assisted resin infusion/prepreg co-curing process 被引量:6
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作者 MA XuQiang GU YiZhuo +2 位作者 LI Min LI YanXia ZHANG ZuoGuang 《Science China(Technological Sciences)》 SCIE EI CAS 2014年第10期1956-1966,共11页
Co-cured vacuum assisted resin infusion process(co-VARI process),which combined vacuum assisted resin infusion(VARI)with prepreg vacuum bag only process(VBO),was adopted to fabricate T-shaped stiffened skin with non-c... Co-cured vacuum assisted resin infusion process(co-VARI process),which combined vacuum assisted resin infusion(VARI)with prepreg vacuum bag only process(VBO),was adopted to fabricate T-shaped stiffened skin with non-crimp fabric(NCF)stiffener and prepreg skin.During compaction stage of co-VARI process,prepreg resin impregnated fiber fabric under elevated temperature and vacuum pressure.This phenomenon was characterized by fluorescent micrographs with different holding temperature and time.Its influences on processing quality and mechanical performance for co-VARI stiffened skin with different filler materials at triangular region were further analyzed by optical micrographs and pull-off test,respectively.The results show that increasing holding temperature and prolonging holding time can promote prepreg resin impregnation in fiber fabric.Moderate prepreg resin impregnation is favorable to reduce resin rich region and increase fiber volume fraction at prepreg-fabric interface.Moreover,prepreg resin impregnation effect plays significant roles on pull-off performance for co-VARI stiffened skin with fabric filler but has negligible influences on specimens with prepreg filler.In addition,compared with stiffened skin with fabric filler,superior processing quality and pull-off performances are achieved for co-VARI stiffened skin with prepreg core filler.These results are helpful to optimize processing procedures and fabricate composite structure by coVARI process. 展开更多
关键词 polymer-matrix composites PREPREG vacuum assisted resin infusion stiffened skin structure CO-CURING
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Liver transplantation following two conversions in a patient with huge hepatocellular carcinoma and portal vein invasion:A case report
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作者 Li-Cong Liang Wen-Sou Huang +6 位作者 Zhao-Xiong Guo Hong-Ji You Yong-Jian Guo Ming-Yue Cai Li-Teng Lin Guo-Ying Wang Kang-Shun Zhu 《World Journal of Gastroenterology》 SCIE CAS 2024年第36期4071-4077,共7页
BACKGROUND Surgical resection and liver transplantation(LT)are the most effective curative options for hepatocellular carcinoma(HCC).However,few patients with huge HCC(>10 cm in diameter),especially those with port... BACKGROUND Surgical resection and liver transplantation(LT)are the most effective curative options for hepatocellular carcinoma(HCC).However,few patients with huge HCC(>10 cm in diameter),especially those with portal vein tumor thrombus(PVTT),can receive these treatments.Selective internal radiation therapy(SIRT)can be used as a conversion therapy for them because it has the dual benefit of shrinking tumors and increasing residual hepatic volume.However,in patients with huge HCC,high lung absorbed dose often prevents them from receiving SIRT.CASE SUMMARY A 35-year-old man was admitted because of emaciation and pain in the hepatic region for about 1 month.The computed tomography scan showed a 20.2 cm×19.8 cm tumor located in the right lobe–left medial lobes with right portal vein and right hepatic vein invasion.After the pathological type of HCC was confirmed by biopsy,two conversions were presented.The first one was drug-eluting bead transarterial chemoembolization plus hepatic arterial infusion chemotherapy and lenvatinib and sintilimab,converted to SIRT,and the second one was sequential SIRT with continued systemic treatment.The tumor size significantly decreased from 20.2 cm×19.8 cm to 16.2 cm×13.8 cm,then sequentially to 7.8 cm×6.8 cm.In the meantime,the ratio of spared volume to total liver volume increased gradually from 34.4%to 55.7%,then to 62.9%.Furthermore,there was visualization of the portal vein,indicating regression of the tumor thrombus.Finally,owing to the new tumor in the left lateral lobe,the patient underwent LT instead of resection without major complications.CONCLUSION Patients with inoperable huge HCC with PVTT could be converted to SIRT first and accept surgery sequentially. 展开更多
关键词 Hepatocellular carcinoma Two conversions Liver transplantation Yttrium-90 resin microspheres Transarterial chemoembolization Hepatic arterial infusion chemotherapy Case report
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Stiffness of In-Situ Formed Interleaving Polymeric Nanofiber-Epoxy Nanocomposites
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作者 Farzin Javanshour Kaan Bilge +1 位作者 Abdul Bari Abdul Raheman Melih Papila 《Open Journal of Composite Materials》 2024年第4期147-157,共11页
This study proposes a facile, but precise method to back-calculate the effective modulus of nanocomposite interleaving plies. Adaptation of a conventional dry-reinforcement resin film infusion (RFI) approach allows in... This study proposes a facile, but precise method to back-calculate the effective modulus of nanocomposite interleaving plies. Adaptation of a conventional dry-reinforcement resin film infusion (RFI) approach allows interleaving neat epoxy layers (NE) with the epoxy-infused nanofibrous plies (XE) of constant thickness. The final cured nanocomposite laminate thus has the form (NE/XE)n, where “n” denotes the number of the repeats and enables clear distinction of the nanocomposite interlayers through the thickness. Mechanical testing of neat epoxy and laminated nanocomposite specimens can be coupled with the classical lamination theory for back-calculating in-plane elastic modulus of the individual epoxy-infused nanofibrous plies (EXE). Finite element analysis (FEA) and testing the laminated nanocomposite subject to flexural loading (3-point bending) are proposed to validate the analytically back-calculated EXE. It is shown that the FEA prediction incorporating EXE and testing for flexural modulus of (NE/XE)20 laminated nanocomposites correlate well and the results are within 5%. This finding suggests that the back-calculation scheme reported herein would be attractive for accurately determining the properties of an individual nanocomposite building block layer. The proposed framework is beneficial for modelling laminated structural composites incorporating XE-like nanocomposite interlayers. 展开更多
关键词 Lamination Theory resin Film infusion Electrospun Nanofibers Mechanical Properties
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基于VARI工艺的碳纤维复合材料快速修理飞机铝合金裂纹的研究
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作者 汪愿 孙运刚 +3 位作者 符彬 刘文浩 宣善勇 刘鹏 《材料导报》 EI CAS CSCD 北大核心 2024年第6期205-210,共6页
考虑到飞机战伤抢修需求,在现有的复合材料胶接修理基础上提出了一种基于真空辅助树脂灌注(VARI)工艺的金属裂纹快速修理方法,通过静力拉伸和疲劳实验将VARI修理工艺与传统湿法胶接修理工艺、机械补强修理工艺进行对比,获得了不同修理... 考虑到飞机战伤抢修需求,在现有的复合材料胶接修理基础上提出了一种基于真空辅助树脂灌注(VARI)工艺的金属裂纹快速修理方法,通过静力拉伸和疲劳实验将VARI修理工艺与传统湿法胶接修理工艺、机械补强修理工艺进行对比,获得了不同修理工艺下实验件的静强度恢复率、疲劳寿命、修理时间及比静拉伸强度恢复率,借助有限元分析法深入研究了VARI修理件的损伤过程,并以比静拉伸强度恢复率为指标,利用Design Expert软件进一步优化了修理补片参数。结果表明:在三种修理工艺中,VARI修理工艺效果最佳,采用VARI修理的实验件静强度能恢复至完好实验件的90.3%,疲劳寿命相比未修理实验件增长了31.4倍;与传统湿法胶接修理相比,采用VARI修理可将修理时间缩短60.2%;与机械补强修理相比,采用VARI修理可将实验件增重降低53.5%,比静拉伸强度恢复率提高146.6%;对于长度为20 mm的裂纹,补片长度60 mm、宽度64.8 mm、铺层数目四层(即补片厚度1 mm)为最优补片参数。 展开更多
关键词 飞机铝合金裂纹 真空辅助树脂灌注修理 疲劳寿命 比静拉伸强度恢复率 有限元模拟
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等温DSC法研究RFI用环氧树脂固化动力学 被引量:52
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作者 代晓青 肖加余 +3 位作者 曾竟成 刘钧 尹昌平 刘卓峰 《复合材料学报》 EI CAS CSCD 北大核心 2008年第4期18-23,共6页
为了预测固化反应的进程,采用STA 449C型差示扫描量热仪,用等温DSC法研究了室温下成膜、中温固化的RFI工艺用(E-44/E-21(6/4,质量比))/GA-327=100/40(质量比)环氧树脂体系在80、90、100、110、120℃下的固化过程,通过Matlab数据拟合良... 为了预测固化反应的进程,采用STA 449C型差示扫描量热仪,用等温DSC法研究了室温下成膜、中温固化的RFI工艺用(E-44/E-21(6/4,质量比))/GA-327=100/40(质量比)环氧树脂体系在80、90、100、110、120℃下的固化过程,通过Matlab数据拟合良好性统计法得到了n级固化模型、自催化模型及复合模型方程中的各个参数值。根据R2和离差平方和SSE确定了适合的动力学模型。研究表明:该树脂体系的固化反应具有自催化和扩散控制的特征,低温下受扩散控制的影响更大;该体系的固化反应动力学符合自催化反应动力学模型,其表观活化能Ea为56.7 kJ/mol,指前因子A为1.18×107s-1,固化反应的反应级数m、n分别为0.529和1.561。 展开更多
关键词 等温DSC 树脂膜熔渗(RFI)工艺 环氧树脂 固化动力学 数据拟合
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新型树脂传递模塑技术 被引量:18
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作者 齐燕燕 刘亚青 张彦飞 《化工新型材料》 CAS CSCD 北大核心 2006年第3期36-38,共3页
概述了传统树脂传递模塑(RTM)及在其基础上发展起来的新型RTM工艺,包括真空辅助树脂传递模塑(VARTM)、Seemann复合材料树脂浸渍模塑成型工艺(SCRIMP)和树脂膜渗透成型工艺(RFI)的成型原理、优点,并指出目前存在的缺点及解决方法。
关键词 树脂传递模塑 真空辅助树脂传递模塑 Seemann复合材料树脂浸渍模塑 树脂膜渗透
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三维整体夹芯织物增强复合材料的研制 被引量:12
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作者 祝成炎 陈俊俊 +2 位作者 朱俊萍 谭冬宜 徐国平 《纺织学报》 EI CAS CSCD 北大核心 2007年第1期56-59,共4页
用玻璃纤维在普通二维织机上分别试制经向为V形、X形和蜂窝形3种典型三维整体夹芯织物,利用真空辅助成型工艺研制复合材料夹芯板。为使树脂能较好地渗入织物和纤维内部,对灌注用树脂胶液的组成、配制比例以及树脂黏度等进行了研究,并讨... 用玻璃纤维在普通二维织机上分别试制经向为V形、X形和蜂窝形3种典型三维整体夹芯织物,利用真空辅助成型工艺研制复合材料夹芯板。为使树脂能较好地渗入织物和纤维内部,对灌注用树脂胶液的组成、配制比例以及树脂黏度等进行了研究,并讨论了三维空芯结构织物中树脂胶液流动过程及气泡形成原因。该复合材料成型工艺能有效地排除在成型过程中产生于织物纤维束之间和纤维束内的气泡。研究结果表明所研制的板材保持了夹芯织物原有的孔形结构、形状与较好的力学性能。 展开更多
关键词 三维整体央芯织物 蜂窝 基体树脂 真空辅助成型
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复合材料的真空辅助成型工艺研究 被引量:21
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作者 张锐 郑威 +2 位作者 袁秀梅 高泉喜 王昭亮 《工程塑料应用》 CAS CSCD 北大核心 2005年第6期33-35,共3页
研究了导流介质、脱模介质等工艺要素对真空辅助成型工艺的影响。结果表明,高渗透率的导流介质和脱模介质均能有效提高树脂的充模速度;所研制的新型导流介质能够有效控制树脂的流动状态。采用真空辅助成型工艺成型的复合材料的性能与模... 研究了导流介质、脱模介质等工艺要素对真空辅助成型工艺的影响。结果表明,高渗透率的导流介质和脱模介质均能有效提高树脂的充模速度;所研制的新型导流介质能够有效控制树脂的流动状态。采用真空辅助成型工艺成型的复合材料的性能与模压工艺成型的复合材料的性能相当。 展开更多
关键词 复合材料 工艺研究 真空辅助成型工艺 工艺成型 工艺要素 流动状态 有效控制 介质 导流 渗透率 脱模 树脂 性能 充模 模压
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复合材料RFI成形的树脂膜揭取性研究 被引量:5
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作者 唐邦铭 梁子青 +2 位作者 蔡杉 张子龙 益小苏 《材料工程》 EI CAS CSCD 北大核心 2005年第3期43-47,共5页
采用树脂膜/离型纸的T型剥离实验方法来表征RFI树脂膜操作过程中的揭取特性,实验研究了几种基本RFI树脂膜的T形剥离载荷 位移关系在不同加载速度及不同实验温度下的表现形式。结果显示内聚破坏与界面破坏情况下载荷位移曲线有明显不同... 采用树脂膜/离型纸的T型剥离实验方法来表征RFI树脂膜操作过程中的揭取特性,实验研究了几种基本RFI树脂膜的T形剥离载荷 位移关系在不同加载速度及不同实验温度下的表现形式。结果显示内聚破坏与界面破坏情况下载荷位移曲线有明显不同的形式。提高温度有利于出现内聚破坏,而提高实验速度则易于出现界面破坏。进一步从实验数据总结出树脂膜揭取的工艺范围应当在出现界面破坏的温度范围内。 展开更多
关键词 复合材料 树脂膜渗透成形 树脂膜 揭取特性 工艺范围
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改性双马来酰亚胺树脂在RFI工艺中的应用 被引量:5
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作者 曹魏 陈立新 +2 位作者 梁滨 董建娜 宋家乐 《航空材料学报》 EI CAS CSCD 北大核心 2009年第2期66-70,共5页
通过在改性双马来酰亚胺5405树脂中加入耐高温热塑性塑料聚芳醚砜(PES),获得了满足RFI工艺要求、具有良好成膜性的5405A树脂膜。该树脂膜在室温不粘手,能够任意弯曲。在熔渗温度(130℃)下,低黏度(≤500mPa.s)的保持时间长达70min。在室... 通过在改性双马来酰亚胺5405树脂中加入耐高温热塑性塑料聚芳醚砜(PES),获得了满足RFI工艺要求、具有良好成膜性的5405A树脂膜。该树脂膜在室温不粘手,能够任意弯曲。在熔渗温度(130℃)下,低黏度(≤500mPa.s)的保持时间长达70min。在室温存放3个月后,不溶物含量由1.25%变化为2.02%,DSC曲线表明反应的峰始温度和峰顶温度与放置前无明显差异,130℃凝胶时间由137min变化为135min。参照5405树脂的固化工艺,制备了5405A树脂浇铸体和单向碳纤维帘子布(G0827)增强5405A复合材料,并对性能进行了评价。对比5405和5405A树脂树脂浇铸体的性能表明,5405A力学性能稍有降低,但韧性得到了明显提高。 展开更多
关键词 树脂膜熔渗 改性双马来酰 肚胺 低黏发 复合材料 件能
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RFI工艺用环氧基树脂膜的研制 被引量:8
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作者 张国利 李嘉禄 +1 位作者 杨彩云 李学明 《固体火箭技术》 EI CAS CSCD 北大核心 2006年第2期142-145,共4页
据RFI工艺用环氧树脂基树脂膜低温成膜性、高温流动性和浸渗性的技术性能要求,设计了在一定温度内具有低反应活性的GY6010型高粘度液态双酚A二缩水甘油醚环氧树脂、HT907型六氢邻苯二甲酸酐和DY062型苄基二甲胺树脂膜制备体系。根据等... 据RFI工艺用环氧树脂基树脂膜低温成膜性、高温流动性和浸渗性的技术性能要求,设计了在一定温度内具有低反应活性的GY6010型高粘度液态双酚A二缩水甘油醚环氧树脂、HT907型六氢邻苯二甲酸酐和DY062型苄基二甲胺树脂膜制备体系。根据等当量反应计算理论和浇注体的力学性能,确定了树脂膜制备体系的最佳混合比例,利用加热聚合、流延成膜和快速冷却方法,制备了具有低固化度的BS-1型环氧树脂基树脂膜。经测试该树脂膜成膜性、弯曲性良好;在80℃的融渗温度下粘度为645 mPa.s,低粘度区域宽度(粘度小于1 000 mPa.s)达25 m in,凝胶时间达56 m in。采用该树脂膜制备的RFI叠层板试件空隙含量(0.8%)极低,与模压试件相比,RFI试件拉伸强度、弯曲强度和层间剪切强度分别提高4.57%、6.26%和21.88%。 展开更多
关键词 复合材料 环氧树脂基树脂膜 树脂膜融渗成型工艺
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碳纳米管/玻纤/环氧层板超声真空灌注工艺及性能研究 被引量:4
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作者 赵艳文 叶宏军 +3 位作者 翟全胜 顾轶卓 李敏 张佐光 《航空材料学报》 EI CAS CSCD 北大核心 2013年第4期58-63,共6页
针对碳纳米管/玻璃纤维/环氧树脂体系,采用传统的真空灌注工艺和超声波辅助真空灌注工艺制备复合材料层板,分析不同工艺方法下层板缺陷状况,测试层板的弯曲性能和层间剪切性能,考察树脂性能和纤维/树脂界面黏结状况,探讨碳管及工艺方法... 针对碳纳米管/玻璃纤维/环氧树脂体系,采用传统的真空灌注工艺和超声波辅助真空灌注工艺制备复合材料层板,分析不同工艺方法下层板缺陷状况,测试层板的弯曲性能和层间剪切性能,考察树脂性能和纤维/树脂界面黏结状况,探讨碳管及工艺方法对层合板性能的影响。结果表明:与传统的真空罐注工艺相比,超声波辅助真空罐注工艺能增强树脂在纤维内部的流动,提高树脂对纤维的浸润,减少层合板的孔隙缺陷;添加0.05%(质量分数)的CNT后层合板的力学性能提高,使用超声波辅助真空罐注工艺制造的层板性能提高得更为明显;制造工艺对层合板性能的影响与纤维织物的结构紧密相关。 展开更多
关键词 复合材料 真空灌注工艺 碳纳米管 环氧树脂
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真空导入模塑工艺树脂流动规律研究 被引量:22
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作者 杨金水 肖加余 +1 位作者 曾竟成 刘钧 《宇航材料工艺》 CAS CSCD 北大核心 2007年第5期22-26,共5页
研究了导流介质、重力、注射方式和注射管径等工艺参数对真空导入模塑工艺中树脂流动行为的影响。结果表明,真空导入模塑工艺中,主导树脂充模流动速度的是导流介质的渗透率;注射方式改变时,树脂的流动模式和流动速度发生改变;树脂的充... 研究了导流介质、重力、注射方式和注射管径等工艺参数对真空导入模塑工艺中树脂流动行为的影响。结果表明,真空导入模塑工艺中,主导树脂充模流动速度的是导流介质的渗透率;注射方式改变时,树脂的流动模式和流动速度发生改变;树脂的充模流动速度随着注射管径的增大而增大;树脂的流动倾角越接近竖直方向重力对树脂流动的影响越大。 展开更多
关键词 真空导入模塑工艺 导流介质 树脂流动 达西定律
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RFI工艺过程的数值模拟 被引量:5
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作者 杨梅 晏石林 谭华 《武汉理工大学学报》 CAS CSCD 北大核心 2005年第12期10-13,共4页
针对RFI工艺过程中的树脂在复杂形状预制件中的流动行为和固化过程进行数值分析,分别编写了基于控制体/有限元法和基于纯有限元法的流动模拟程序和固化程序。通过计算实例可见,所编写的有限元程序能很好地预测充模时间、各个时刻树脂的... 针对RFI工艺过程中的树脂在复杂形状预制件中的流动行为和固化过程进行数值分析,分别编写了基于控制体/有限元法和基于纯有限元法的流动模拟程序和固化程序。通过计算实例可见,所编写的有限元程序能很好地预测充模时间、各个时刻树脂的流动前沿位置、模腔中的压力分布和温度分布,树脂的固化反应程度及粘度变化情况。这对于优化成型工艺参数、控制残余应力以及提高产品质量具有重要的指导意义。 展开更多
关键词 RFI工艺 树脂流动 固化 数值模拟
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