张红哲,郑植,殷国运,陈晨,邓成林,鲍永杰.碳纤维增强热塑性复合材料螺旋铣磨制孔损伤研究[J].表面技术,2023,52(2):25-34.
ZHANG Hong-zhe,ZHENG Zhi,YIN Guo-yun,CHEN Chen,DENG Cheng-lin,BAO Yong-jie.Hole Damage of Carbon Fiber Reinforced Thermoplastic Composites Using Helical Milling[J].Surface Technology,2023,52(2):25-34 |
| 碳纤维增强热塑性复合材料螺旋铣磨制孔损伤研究 |
| Hole Damage of Carbon Fiber Reinforced Thermoplastic Composites Using Helical Milling |
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| DOI：10.16490/j.cnki.issn.1001-3660.2023.02.003 |
| 中文关键词: 碳纤维增强热塑性复合材料 螺旋铣磨 制孔 切削温度 损伤 冷却辅助 |
| 英文关键词:carbon fiber reinforced thermoplastic composites helical milling hole making cutting temperature damage cooling assistance |
| 基金项目:国家自然科学基金(U21A20165，52105431);大连市科技创新基金(2022JJ12GX033);辽宁省应用基础研究计划(2022JH2/ 101300221) |
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| Author | Institution |
| ZHANG Hong-zhe | Engineering Training Center of Dalian University of Technology, Liaoning Dalian 116023, China |
| ZHENG Zhi | Engineering Training Center of Dalian University of Technology, Liaoning Dalian 116023, China |
| YIN Guo-yun | Marine Engineering College of Dalian Maritime University, Liaoning Dalian 116026, China |
| CHEN Chen | Marine Engineering College of Dalian Maritime University, Liaoning Dalian 116026, China |
| DENG Cheng-lin | Engineering Training Center of Dalian University of Technology, Liaoning Dalian 116023, China |
| BAO Yong-jie | Marine Engineering College of Dalian Maritime University, Liaoning Dalian 116026, China |
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| 中文摘要: |
| 目的 研究碳纤维增强热塑性复合材料(CFRTP)螺旋铣磨制孔的切削温度和切削力的变化趋势，以及典型制孔损伤的特点，并分析切削温度的下降对制孔损伤的影响。方法 采用螺旋铣磨的方法开展CFRTP的制孔试验研究，通过改变工艺参数研究切削温度、切削力的变化趋势，分析各类典型制孔损伤的特点、形成原因及随工艺参数的变化情况，并研究添加冷却辅助降低切削温度对抑制制孔损伤的效果。结果 随着刀具自转转速、公转转速和螺距的升高，切削温度分别升高了约46.43%、12.06%和95.97%;切削力随着自转转速的升高而降低，随着公转转速和螺距的升高而增大。当螺距达到0.45 mm时，轴向力会有所下降。入口损伤和出口损伤主要以毛刺为主，损伤会随着各工艺参数的升高而加剧，孔壁损伤主要表现为涂覆、变形、裂纹等3种形式。添加冷却辅助后，制孔质量得到显著提高，高温下的刀具涂覆问题基本解决。结论 切削温度是影响CFRTP制孔质量的主要因素，切削温度的升高导致树脂基体软化，使得切屑形貌从粉末状转变为连续薄片状，进而对切削力产生影响，树脂软化对制孔损伤有着明显的影响。冷却辅助能够明显地降低切削温度，从而起到抑制损伤的作用。 |
| 英文摘要: |
| In this paper, helical milling experiments were carried out to investigated the hole quality of carbon fiber reinforced thermoplastic composites (CFRTP). The effect of machining parameters such as rotation speed, revolution speed and axial feed depth on cutting temperature, cutting force, characteristics and formation of typical hole damages were investigated. The transition between different damage forms induced by changing machining parameters was also analyzed. Additionally, in order to reduce the effect of cutting temperature on the hole damage, additional cooling assistance technology was proposed. The experimental results showed that increasing rotation speed, revolution speed and axial feed depth increased the cutting temperature by 46.43%, 12.06% and 95.97%, respectively. The cutting force decreased with the increase of rotation speed, but increased with the increase of rotational speed and axial feed depth. However, when the axial feed depth reached 0.45 mm, the axial force decreased to a certain extent, which was related to the softening of the material caused by the continuous contact between the bottom material and the milling tool. Burrs were mainly damage occurred at the entrance and exit of the hole. The entrance damage was caused by the material softening at high temperature during machining and then pushing by the cutting force. Owing to the different thermal conductivity of the carbon fiber and the thermoplastic resin, the resin was easily suffering soften during machining. The softened resin was easily to produce interfacial debonding under the push of the cutting force, so the entrance burr tended to appear in the resin area of the material surface. The exit damage was caused by the bottom material softening during machining and then breaking after reaching yield strength. The exit burr was more obvious because the cutting temperature was higher than that at the entrance. Both entrance damage and exit damage were aggravated with the increase of above machining parameters. The hole wall damages were mainly manifested in three forms:coating, deformation and crack. The phenomenon of coating was more serious at the exit of the hole because the cutting temperature was higher than that at the entrance of the hole. The material which had been softened during machining was pushed by the tool and chip friction, leading to the obvious deformation of the hole wall. When the axial force was large, the tool pushed the material at the hole wall strongly, resulting in cracks. With adding cooling assistance, the heat and chips in the machining area were taken out, so that the cutting temperature decreased greatly, and the phenomenon that the matrix being easily to plasticize by heat was obviously improved. The hole quality was significantly improved, and the chip adhesion on milling tool induced by high temperature basically disappeared. However, there were some phenomena of the machining cylinder adhering due to the insufficient cooling. In conclusion, the cutting temperature is the main factor dominating the hole quality of CFRTP. The increase of cutting temperature will lead to the softening of resin matrix and the variation of chip morphology from powder to continuous slice, which has an impact on the cutting force. The softening of resin has a significant impact on hole damage. The cooling assistance can significantly reduce the cutting temperature and thus inhibit the damage. |
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