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钻削CFRP/Ti合金叠层时钻头温度、几何误差及热膨胀对钻孔精度影响的试验研究

Experimental Study of Drilling Temperature, Geometrical Errors and Thermal Expansion of Drill on Hole Accuracy When Drilling CFRP/Ti Alloy Stacks.

作者信息

Kolesnyk Vitalii, Peterka Jozef, Kuruc Marcel, Šimna Vladimír, Moravčíková Jana, Vopát Tomáš, Lisovenko Dmytro

机构信息

Sumy State University, Rymskogo-Korsakova Str., 2, 40007 Sumy, Ukraine.

Faculty of Materials Science and Technology, Slovak University of Technology in Bratislava, Vazovova 5, 81243 Bratislava, Slovakia.

出版信息

Materials (Basel). 2020 Jul 20;13(14):3232. doi: 10.3390/ma13143232.

Abstract

The drilling of holes in CFRP/Ti (Carbon Fiber-Reinforced Plastic/Titanium alloy) alloy stacks is one of the frequently used mechanical operations during the manufacturing of fastening assemblies in temporary civil aircraft. A combination of inhomogeneous behavior and poor machinability of CFRP/Ti alloy stacks in one short drilling brought challenges to the manufacturing community. The impact of the drilling temperature and time delay factor under various cutting conditions on hole accuracy when machining CFRP/Ti alloy stacks is poorly studied. In this paper, the drilling temperature, the phenomenon of thermal expansion of the drill tool, and hole accuracy are investigated. An experimental study was carried out using thermocouples, the coordinate measuring machine method, and finite element analysis. The results showed that the time delay factor varied from 5 (s) to 120 (s), influences the thermal-dependent properties of CFRP, and leads to an increase in hole roundness. Additionally, the thermal expansion of the drill significantly contributes to the deviation of the hole diameter in Ti alloy.

摘要

在临时民用飞机紧固组件制造过程中,在碳纤维增强塑料/钛合金(CFRP/Ti)叠层上钻孔是常用的机械操作之一。在一次短时间钻孔中,CFRP/Ti合金叠层的不均匀行为和较差的可加工性给制造领域带来了挑战。目前对各种切削条件下钻孔温度和时间延迟因素对加工CFRP/Ti合金叠层时孔精度的影响研究较少。本文对钻孔温度、钻具热膨胀现象和孔精度进行了研究。采用热电偶、坐标测量机方法和有限元分析进行了实验研究。结果表明,时间延迟因素在5(秒)至120(秒)之间变化,会影响CFRP的热相关性能,并导致孔圆度增加。此外,钻头的热膨胀对钛合金中孔直径的偏差有显著影响。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cabd/7411704/12b7aec86112/materials-13-03232-g001.jpg

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