对钉挤压力的分析建模,考虑到航空结构中钉的不均变形
Yonggang Kang1, Siren Song1, Tianyu Wang1
1School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072, China.
Materials (Basel, Switzerland)
|June 19, 2024
概括
这项研究通过考虑非均的钉变形来增强飞机钉挤压力建模. 新型号提高了航空航天应用的精度.
科学领域:
- 机械工程 机械工程
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
背景情况:
- 对于飞机子挤压力的现有分析模型通常假定子变形均.
- 在挤压过程中现实世界的钉变形是不均的,影响模型的准确性.
研究的目的:
- 开发一种高质量的挤压力模型,以解决非均的钉变形问题.
- 提高飞机结构组装分析模型的准确性.
主要方法:
- 在压力方程中引入了库伦摩擦.
- 整合了四个关键调整:不均的干扰,驱动的头桶,弹背面,和修改的尺寸.
- 考虑了驱动头的凸起结构和修改了板孔扩展.
主要成果:
- 与现有方法相比,拟议的模型显示了明显提高的准确性.
- 在航空航天工业中常见的挤压比率上,提高的精度尤其值得注意.
结论:
- 开发的模型提供了更现实的钉挤压力的表现.
- 准确建模变形对于确保飞机结构的完整性至关重要.
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