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机身大型蒙皮件拉形新工艺可行性研究
英文标题:Feasibility study on the new technology of large skin stretch forming
作者:李荣 孙志莹 郎利辉 
单位:西安飞机工业(集团) 有限责任公司 
关键词:大型蒙皮件 凹模纵向拉形 拉形工艺 回弹量 
分类号:
出版年,卷(期):页码:2014,39(10):47-51
摘要:

针对机身长宽比例差距较大的大型铝合金蒙皮件冷拉成形工艺研究,结合传统拉形工艺对比分析,提出一种新的蒙皮加工工艺—凹模纵向拉伸成形。采用数值模拟与实验相结合的方式对蒙皮拉形工艺加工过程中的缺陷进行分析。分析结果表明,对于长宽比例大于5的机身蒙皮零件,采用凹模纵向拉伸成形工艺方案,其板料承受的等效应力分布均匀且可以达到屈服,有利于减小回弹,回弹量可以控制在0.5 mm内。因此,利用凹模纵向冷拉成形工艺方案制造长宽比例大的铝合金蒙皮件,不仅可以节省材料、降低对设备的要求,而且可以获得高精度、高质量的铝合金蒙皮件。

Based on the study of stretch forming process of large aluminum alloy skin with a large length to width ratio and the analysis and comparison of traditional stretch forming process, a new process of skin stretch forming of longitudinal stretch forming with die was proposed. The forming defect during the skin stretch forming process was analyzed by combining the numerical simulation with experiments. Simulation results show that equivalent stresses are distributed uniformly and up to the yield limit so as to reduce the springback effectively. The springback can be controlled within 0.5 mm for skin, whose length to width ratio is larger than five. Therefore, aluminum alloy skin with large length to width ratio can be manufactured by longitudinal stretch forming with die, which not only saves materials and reduces requirements on equipment, but also obtains high precision and high-quality skin parts.

基金项目:
作者简介:
李荣(1979-),男,硕士,工程师
参考文献:
[1]张彦敏,周贤宾.蒙皮拉形加载轨迹优化[J].北京航空航天大学学报,2007,2):201-205.

Zhang Y MZhou X B.Optimization of loading trajectory in skin stretch forming process[J].Journal of Beijing University of Aeronautics and Astronautics2007,2):201-205.

[2]徐龙,熊杰,郑堂介,等.复杂蒙皮拉形工艺有限元仿真与试验研究[J].塑性工程学报,2011,183):118-121.

Xu LXiong JZheng T J,et al. FEM simulation and experimental analysis on complicated skin stretch forming[J].Journal of Plasticity Engineering2011,183):118-121.

[3]彭静文,李卫东,万敏,等.机翼前缘蒙皮拉形工艺参数优化与试验[J].塑性工程学报,2011184):74-78.

Peng J WLi W DWan M, et al.Optimization and experimental research of processing parameters in stretch forming of wing leading edge skin[J].Journal of Plasticity Engineering2011184):74-78.

[4]He D HLi X QLi D S, et al. Process design for multi-stage stretch forming of aluminium alloy aircraft skin[J]. Transactions of Nonferrous Metals Society of China, 2010(6): 1053-1058.

[5]He D HLi D SLi X Q, et al. Optimization on springback reduction in cold stretch forming of titanium-alloy aircraft skin[J]. Transactions of Nonferrous Metals Society of China, 2010,(12): 2350-2357.

[6]Murugan S, Flores E S, Adhikari S, et al. Optimal design of variable fiber spacing composites for morphing aircraft skins[J].Composite Structures, 2012, 94(5): 1626-1633.

[7]Zhu J H, Gu X J, Zhang W H, et al. Structural design of aircraft skin stretch-forming die using topology optimization[J]. Journal of Computational and Applied Mathematics, 2013, 246: 278-288.

[8]周朝晖,蔡中义,李明哲.多点模具拉形中回弹的数值分析[J].锻压技术,2006,262):94-97.

Zhou Z H,Cai Z Y,Li M Z.Numerical analysis of the springback in stretching of sheet metal based on multi-point die[J].Forging & Stamping Technology2006262):94-97.

[9]刘晓兰,束飞,黄旭林.进气道马鞍形蒙皮件成形工艺与模具设计[J].模具工业,2012,388):39-41.

Liu X LShu FHuang X L.Forming process and design of die for saddle-shaped inlet panel[J].Die & Mould Industry2012388):39-41.

[10]彭赫力.柔性夹钳拉形过程及其数值模拟研究[D].吉林:吉林大学,2013.

Peng H L.Research on Process and Numerical Simulation of Flexible Clamp Stretch Forming[D].Jilin: Jilin University2013.
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