钻孔参数和工具直径对分层和推力力的影响,用于钻孔高性能玻璃/环氧复合材料,用于航空航天结构,使用新设计钻孔
Bekir Yalçın1, Çağın Bolat2, Berkay Ergene3
1Department of Mechanical Engineering, Faculty of Technology, Afyon Kocatepe University, 03200 Afyonkarahisar, Türkiye.
Polymers
|November 9, 2024
概括
优化航空航天复合材料的干钻是非常重要的. 这项研究发现,中等线速度,低料率和小工具直径可以最大限度地减少推力和分层,从而提高结构完整性.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 复合材料由于其高性能,在航空航天领域至关重要.
- 确保组装性能和复合材料组件的连接性能至关重要.
- 干钻是复合结构的常见制造工艺.
研究的目的:
- 为了优化玻璃增强环氧矩阵复合材料的干式钻井过程.
- 为了研究轴速度,料速度和工具直径对推力和分层的影响.
- 为了确定航空航天复合材料应用的最佳钻井参数.
主要方法:
- 使用定制设计的钻头工具进行实验分析.
- 实验的塔古奇设计的应用.
- 螺旋转速 (1000-5750rpm),料速度 (0.2-0.8mm/rev) 和工具直径 (3-5mm) 的系统变化.
主要成果:
- 确定了最小化推力和分层的最佳条件.
- 发现中等螺旋速度 (2250-4000rpm) 是有益的.
- 较低的进料速率 (0.2 mm/rev) 和较小的工具直径 (3 mm) 显著减少了钻探引起的损坏.
结论:
- 该研究为改善钻孔航空航天复合材料组件的结构完整性提供了可操作的见解.
- 优化的干式钻井参数提高了航空航天结构的性能和可靠性.
- 通过改进复合材料制造,这些发现为航空航天和国防工业带来了进步.
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