共查询到20条相似文献,搜索用时 581 毫秒
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以铝合金半球壳体为研究对象,分析了铝合金半球壳体冲压预成形和旋压成形工艺。结果表明,旋压件和冲压预成形件的形状越接近,冲压预成形件的工作效率也就越高,冲压件成形工艺优势也就越明显。在旋压成形过程中,5A06铝合金的类似环筋结构具有较大的变形抗力,一道次普旋成形的结果是变形过程中零件发生了反挤现象;为了改进成形工艺,可以增大减薄率,将普旋道次增加到3次,同时向前移动普旋起点。 相似文献
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采用多道次有芯复合旋压工艺,成功地加工出了30CrMnSiA薄壁偏心异形件,并探讨了这种非对称工件旋压成形的规律。 相似文献
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薄壁筒形件多道次滚珠旋压成形机理研究 总被引:4,自引:0,他引:4
为研究多道次成形条件下薄壁筒形件滚珠旋压的成形机理,采用实验和有限元法相结合对薄壁筒形件多道次滚珠旋压的应力应变、旋压力和成形性进行了分析。结果表明:各道次下的等效应力和等效应变都是由旋压件的内表面向外表面逐渐增大,且随着旋压道次数的增加,等效应力和等效应变也都是逐渐增大;每道次的轴向旋压力随着滚珠行程的增加而增大,且各道次的旋压力也逐渐增大;多道次滚珠旋压时,由于采用较小的壁厚减薄量和材料的加工硬化,金属易于稳定流动,能够保证管坯的轴向伸长。因此,通过多道次滚珠旋压可实现大减薄量薄壁筒形件的旋压成形。 相似文献
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框架式三旋轮错距旋压成形装置的研制 总被引:1,自引:0,他引:1
采用分层错距进行旋压成形时,工件厚度逐渐减小,增大了道次减薄率,减少了加工道次,可显著提高旋压件的加工精度和生产效率。本文根据齿轮旋压成形工艺要求、旋压成形原理及三旋轮错距旋压工艺特点,设计了一种框架式三旋轮错距旋压成形装置,重点介绍了旋轮座、旋轮径向进给及轴向、径向错距量调整等结构的设计方案,并对蜗杆传动进行了强度设计。 相似文献
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Xu Hengqiu Li Mingzhe Zhang Rui Wang Dali Hou Fengyan Li Linlin Fan Guisen Shen Yujing Jilin University Changchun China Changchun Institute of Equipment Technology Changchun 《稀有金属材料与工程》2011,(Z3):78-81
In this paper, the process of thermal conventional spinning of Ti-6Al-4V alloy complex shape shell is studied by experiment. Billet for Ti-6Al-4V alloy board is headed in the spinning process for multi-pass conventional spinning forming. With two spinning mandrel, the first is conventional spinning pre-forming and the second is conventional end forming, vacuum heat treatment after each spinning forming. As results, the mandrel preheating temperature impacts the spinning and the appropriate temperature range plays an important role in the process of spinning. With supplemental heating means and infrared thermometer measurement ensure a stable temperature. Multi-passing thermal spinning Ti-6Al-4V alloy thins the billet thickness, using the feature obtaining the wanting complex shape shell of thick bottom and thin mouth. The spinning track, the number of spinning pass, feed rate affect the billet thinning. During thermal spinning process Ti-6Al-4V alloy rebound severe. The size reduction and feed have impact on the rebound. By modifying the spinning parameters and the mandrel repair to ensure the dimensional accuracy of workpiece. Spinning workpiece has fine grain and high strength. 相似文献
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大型复杂薄壁壳体多道次旋压过程中的壁厚变化 总被引:4,自引:1,他引:3
基于ABAQUS/Explicit和Standard建立的包含回弹与退火的大型复杂薄壁壳体多道次旋压全过程模拟模型,分析了该过程中壁厚的分布与变化及工艺参数对壁厚的影响规律。结果表明,壁厚减薄经历了剪切减薄和拉薄两个阶段,壁厚剧烈减薄部位位于旋轮后方的环带并向工件口部移动,而且其值逐渐减小;壁厚沿工件母线方向分布不均匀,沿周向分布较均匀;回弹对壁厚的分布影响不大。摩擦系数在一定范围内的增大,可以有效地抑制第一道次旋压过程中壁厚过度减薄的发生,使壁厚分布更均匀;而旋轮进给比对工件壁厚的影响与摩擦系数的作用相反。在后续道次旋压过程中,工件壁厚差随着摩擦系数的增大先减小后增大,随着旋轮进给比的增大逐渐减小。这些结果可为大型复杂薄壁壳体多道次旋压成形参数的确定和优化设计提供理论依据。 相似文献
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A new approach to optimal design of multi-stage metal forming processes with micro genetic algorithms 总被引:3,自引:0,他引:3
S. Roy S. Ghosh R. Shivpuri 《International Journal of Machine Tools and Manufacture》1997,37(1):29-44
This paper describes a new method for design optimization of process variables in multi-stage metal forming processes. The selected forming processes are multi-pass cold wire drawing, multi-pass cold drawing of a tubular profile and cold forging of an automotive outer race preform. An adaptive micro genetic algorithm (μGA) scheme has been implemented for minimizing a wide variety of objective-cost functions relevant to the respective processes. The chosen design variables are die geometry, area reduction ratios and the total number of forming stages. Significant improvements in the simulated product quality and reduction in the number of passes has been observed as a result of the micro genetic algorithms-based optimization process. 相似文献
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介绍了半锥角<1°的LF6合金锥筒旋压成形过程。实验表明,LF6合金小锥度铝筒零件,用筒形锻坯在直筒芯模上变薄旋压,再用小锥度芯模普旋收锥成形是可行的。文章分别对确定初始锻坯尺寸、室温下强旋变薄铝筒、加热普旋成锥形零件以及实验中出现的问题进行了说明。实验为LF6合金小角度无缝锥筒塑性加工成形提供了参考。 相似文献