局部加压对合金飞轮外微观结构和机械性能的影响 复杂形状的飞轮外
Qiang Chen1, Ning Ge2, Jufu Jiang2
1Southwest Technology and Engineering Research Institute, Chongqing 400039, China.
Materials (Basel, Switzerland)
|January 11, 2024
概括
挤压造AlSi9Mg合金飞轮外与局部加压改善了表面质量和减少了缺陷. 最佳参数产生了高抗拉强度,但强制养效应在厚的部分是有限的.
科学领域:
- 材料科学 材料科学 材料科学
- 制造业 工程 制造工程
背景情况:
- 飞轮外需要高完整性,因为要求高的汽车应用.
- 复杂的形状和组件中巨大的墙壁厚度差异给造带来了挑战,导致像收缩孔隙性这样的缺陷.
研究的目的:
- 研究复杂的飞轮外的AlSi9Mg合金压.
- 评估过程参数和局部加压对造缺陷,微观结构和机械性能的影响.
主要方法:
- 对具有不同壁厚的AlSi9Mg合金组件进行压试验.
- 将局部加压应用于厚壁部分,以减轻造缺陷.
- 在不同的工艺条件下分析了微观结构和机械性能.
主要成果:
- 通过优化挤压造参数 (650°C造,48 MPa特定压力,220°C模具温度) 实现了良好的表面质量.
- 当地加压有效地减少了厚壁的收缩缺陷,尽管其范围有限.
- 最佳参数的最终拉伸强度为201 MPa,强度为103 MPa,延长率为5.1%.
结论:
- 使用优化参数和局部加压的压是生产复杂AlSi9Mg组件的有效方法.
- 局部加压影响固化,导致塑性变形,并有助于强制养,但有局限性.
- 微观结构分析显示了细小的,粉丝圈/均的α-Al颗粒和容易分离的针状欧性.
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