研究冷成形过程的条纹为托架的杆太空建筑的杆
Xingwen Yang1,2, Jingtao Han1,3, Ruilong Lu1
1School of Materials Science and Engineering, University of Science and Technology Beijing, Beijing 100083, China.
Materials (Basel, Switzerland)
|December 23, 2023
概括
这项研究引入了太空杆的轨道冷成型,优化了滚动间隙和间距. 最佳参数 (0.4毫米卷隙,100毫米间距) 确保成功地形成条纹,防止边缘波等缺陷.
科学领域:
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
- 制造过程 制造过程 制造过程
背景情况:
- 空间杆结构需要特殊的组件,如冷成型杆.
- 在轨道上的制造对材料加工提出了独特的挑战.
- 现有的冷成型技术需要适应太空应用.
研究的目的:
- 开发和研究一种用于轨道上冷成型太空杆的新技术.
- 分析卷间隙和卷间距对不对称横截面薄条的冷成型的影响.
- 为了确定最佳的过程参数,以成功制造太空杆杆.
主要方法:
- 使用ABAQUS有限元素分析 (FEA) 进行模拟.
- 进行模拟结果的实验验证.
- 研究了不同卷间距 (0.3-0.5毫米) 和卷间距 (100-140毫米) 的影响.
主要成果:
- 在成型过程中,应力和张力集中在特定的角落 (2/4/6).
- 大约0.4毫米的卷隙提供了最佳的条形形成.
- 100毫米的滚筒间距平衡了纵向应变波动,制造成本和体积.
- 实验验证证了成功准备带的0.4毫米滚动间隔和100毫米滚动间隔.
- 0.3毫米的滚动间隙会导致边缘波和潜在的撕裂缺陷.
结论:
- 拟议的轨道冷成型技术对于太空杆是可行的.
- 优化参数 (0.4毫米卷隙,100毫米卷隙) 对于无缺陷成型至关重要.
- 结合实验,FEA有效指导太空应用冷成型工艺的优化.
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