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结合缩径成形和旋压过程,建立了薄壁管缩径旋压变形力的理论计算模型和旋压力的计算公式, 并对旋压方式、道次压下量Δ及旋轮进给比f等成形工艺参数对滚珠旋压成形的影响进行了试验研究. 相似文献
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三旋轮缩旋时金属变形规律研究 总被引:2,自引:0,他引:2
利用三旋轮自动错距旋压机对管坯进行缩旋成形实验,分别研究了缩径量和旋压道次等工艺参数对缩旋成形的影响规律,并探讨了其变形机理,结果表明,三旋轮缩旋时变形区坯料的壁厚减薄,轴向长度增加,壁厚减薄量与总的缩径量成正比,在缩径量相同的条件下,旋压道次增多,坯料壁厚减薄的程度也增大。 相似文献
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TC4钛合金轮圈热旋成形技术研究 总被引:1,自引:0,他引:1
针对TC4钛合金轮圈的结构特点,设计了钛合金轮圈热旋的模具结构,研究了TC4钛合金的热变形特性,分析了钛合金热旋翻边过程成形缺陷的产生原因,最终获得了钛合金轮圈的合理热旋工艺.研究表明,采用分瓣组合模具是成形钛合金车轮合理的模具结构方案,热旋工艺参数对钛合金轮圈的成形质量有显著的影响.TC4钛合金轮圈的适宜翻边温度为600~700℃,采用略小于坯料壁厚的间隙(小于坯料壁厚的10%左右)及较小的进给比(f≈0.1 mm/r)可有效防止翻边起皱和开裂.直边较短的轮圈采用直线轨迹可一道次翻边成形. 相似文献
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本文借鉴金属零件热校形工艺的经验,利用复合材料在高温下的应力松弛现象,通过热校形工艺修正复合材料零件的形状。制造了碳纤维平纹织物/环氧复合材料L形梁、C形梁,通过自制的热校形模具,以实验方法研究热校形时间、热校形载荷对零件形状的影响,分析复合材料热校形工艺的可行性。研究表明,复合材料热校形工艺中零件变形的主要原因是零件在高温下发生应力松弛,其他因素可以忽略;热校形载荷、热校形时间都对热校形工艺的效果有重要影响。针对特定的复合材料结构,采用合理的热校形工艺过程能够有效地控制构件形状,方便零件的装配。 相似文献
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采用线圈轴向磁场力对压扁量为11mm的20G钢管进行了电磁校形,并以变形量为评价指标,研究了放电电压、放电次数和线圈电感对钢管校形精度的影响。结果表明:虽然线圈电感和放电次数对校形精度有一定的影响,但放电电压是影响校形精度的决定因素;试验还从各种参数对校形的影响关系得到了较优化的工艺参数,以达到提高校形效果的目的。 相似文献
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目的 制备一种热塑性上浆剂,以期改善碳纤维的表面性能以及单丝拉伸性能。方法 通过直接磺化法制备磺化聚醚醚酮水性上浆剂,并通过喷涂法对未上浆的T300碳纤维进行上浆处理,研究制得上浆剂的结构特征、性能以及其对碳纤维性能的影响。结果 制得磺化聚醚醚酮的磺化度约为74%,以此为主浆料配制的水性上浆剂具有良好的成膜性和储存稳定性。经上浆处理后,碳纤维表面形成了连续的磺化聚醚醚酮上浆层,表面官能团含量明显增加,树脂微滴在纤维表面的接触角降低。此外,上浆层可以弥补纤维表面的部分缺陷,使得上浆后碳纤维的单丝拉伸强度提高了5%。结论 磺化聚醚醚酮上浆剂可以有效改善碳纤维的表面性能及单丝拉伸性能。 相似文献
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This work aims at developing a hot sizing process on composite materials to correct the profiles of composite structures during manufacture. Hot sizing experiments were carried out at 150 °C with different sizing loads and hot sizing periods for L-shaped composite beams made of carbon fiber plain-weave fabric and epoxy resin. To predict the springback in hot sizing process, a corresponding finite element simulation method was developed using stress relaxation equations determined at the same temperature. Excellent agreements between the predicted and observed results were obtained. The effects of the component thickness and 45° ply percentage on the springback rate were investigated by simulation. Springback rate in hot sizing process on composite materials ranges from 60% to 95%. In conclusion hot sizing process is proved to be a valid method for compensation for the process-induced deformation (PID) of L-shaped composite beams. 相似文献
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The influence of nano-SiO2 modified epoxy emulsion sizing on the interfacial adhesion properties of carbon fibers reinforced composites was investigated. The interfacial interaction between carbon fibers and the matrix was characterized by X-ray photoelectron spectrometry (XPS), scanning electron microscopy (SEM) and three-point short-beam shear testing. The results showed that the amount of hydroxyl groups was slightly increased on the carbon fibers surface after treatment with nano-SiO2 modified sizing. Compared to the unsized composites, the interlaminar shear strength (ILSS) values for the composites with unmodified sizing and nano-SiO2 modified sizing were increased by 9% and 14%, respectively. The holes and carbon fibers pullout were not observed in their fracture sections. Surprisingly, the fracture section of the composites with nano-SiO2 modified sizing was more compact and the fiber debonding was more difficult. 相似文献
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纤维增强树脂基复合材料机翼结构复杂,往往存在明显的固化变形现象,严重影响机翼的装配和气动特性。本研究目的在于建立大型复合材料复杂结构的热校形工艺方法,解决复合材料机翼制造的变形控制问题。针对复合材料机翼的固化变形特点,设计了新的热校形夹具工装。在评价复合材料应力松弛特性的基础上,建立了大型复合材料机翼结构热校形工艺的有限元模拟方法,实现了对热校形后机翼结构残余变形的有效预报,分析了校形载荷、校形温度等关键工艺参数对校形效果的影响规律,形成优化的热校形工艺方案。模拟及实验结果表明,复合材料热校形工艺可以适用于大型复杂结构,复合材料机翼89.5%的固化变形被热校形工艺的残余变形抵消,达到机翼的装配和气动外形要求。 相似文献
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R.-C. ZhuangJ.-W. Liu R. PlonkaY.-X. Huang E. Mäder 《Composites Science and Technology》2011,71(12):1461-1470
The long term performance of composite materials is highly desired for their expanding application range. Tuning the interphase properties has been proven to be a practical way to enhance the performance of composites. In this study, short glass fibre (GF) reinforced polypropylenes (PPs) with improved hygrothermal durability were obtained by incorporating NaBF4 into the sizing and thus the interphases of GF/PP composites. Detailed investigations were performed on the surface properties of sized GFs and the mechanical properties of virgin and aged composites. It was found that the retention in both ultimate tensile strength and Charpy impact toughness of aged composites monotonically increased with increasing NaBF4 content. The improvement in hygrothermal durability was related to the enhanced fibre/matrix adhesion strength induced by the presence of NaBF4 as indentified by fracture surface analysis using field-emission scanning electron microscopy and single fibre pull-out test. 相似文献
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以酪素(CA)、双丙酮丙烯酰胺(DAAM)、甲基丙烯酸甲酯(MMA)、丙烯酸丁酯(BA)、丙烯腈(AN)为原料,通过无皂乳液聚合制备了酪素接枝丙烯酸酯表面施胶剂,考察了酪素用量对乳液稳定性和纸张施胶度的影响,软硬单体比例和交联单体DAAM的加入量对纸张施胶度和表面物理强度的影响。结果表明,酪素为单体总量30%,软硬单体... 相似文献