1. 南京航空航天大学机电学院,南京,210016
2. 江苏集萃精密制造研究院有限公司,南京,210016
纸质出版:2026
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李迎港, 陈燕, 杨浩骏, 等. 基于ScCO2低温微量润滑工艺的CFRP/Ti6Al4V叠层结构钻削试验研究[J]. 航空制造技术, 2026,69(1/2).
LI Yinggang, CHEN Yan, YANG Haojun, et al. Experimental Study on Drilling of CFRP/Ti6Al4V Laminates Using ScCO-Based Cryogenic Minimum Quantity Lubrication[J]. Aeronautical Manufacturing Technology, 2026, 69(1/2).
李迎港, 陈燕, 杨浩骏, 等. 基于ScCO2低温微量润滑工艺的CFRP/Ti6Al4V叠层结构钻削试验研究[J]. 航空制造技术, 2026,69(1/2). DOI: 10.16080/j.issn1671-833x.20240423.
LI Yinggang, CHEN Yan, YANG Haojun, et al. Experimental Study on Drilling of CFRP/Ti6Al4V Laminates Using ScCO-Based Cryogenic Minimum Quantity Lubrication[J]. Aeronautical Manufacturing Technology, 2026, 69(1/2). DOI: 10.16080/j.issn1671-833x.20240423.
为了降低CFRP/Ti6Al4V 叠层结构的钻削温度,提高钻削质量,利用超临界二氧化碳(Supercritical carbon dioxide,ScCO
2
)对润滑油具有高溶解性的特点,提出了低温微量润滑(Cryogenic minimum quantity lubrication, CMQL)工艺,进行了CMQL 系统油滴雾化效果测试和输出温度测试,开展了CMQL 条件下CFRP/Ti6Al4V 叠层结构的低频振动钻削试验,分析了CO
2
压力对切削加工性的影响。结果表明,增加CO
2
压力可以提高CMQL 装置的雾化效果和冷却能力,压力增加至8 MPa,CO
2
为超临界态,其输出温度可低至–80 ℃以下;系统压力从5 MPa 增至9 MPa,CFRP 与Ti6Al4V 层的钻削温度分别降低了15.91% 和50.78%,轴向力分别增大了65.22% 和20.26%,扭矩分别减小了23.33% 和16.77%;Ti6Al4V 层的出口毛刺高度降低42.04%,CFRP 出口分层因子减小5.41%;在压力为7 MPa、8 MPa 和9 MPa 时,CFRP/Ti6Al4V 叠层结构可得到较低的孔壁粗糙度。
To reduce drilling temperatures and improve the machining quality of CFRP/Ti6Al4V laminates
this study proposed a cryogenic minimum quantity lubrication (CMQL) technique
utilizing the high solubility of lubricant in supercritical carbon dioxide (ScCO
2
). Tests were conducted on the droplet atomization performance and output temperature of the CMQL system
followed by low-frequency vibration drilling experiments under CMQL conditions for CFRP/Ti6Al4V laminates. The influence of CO
2
pressure on laminate drilling was analyzed. The results demonstrate that increasing CO
2
pressure enhances the atomization and cooling capability of the CMQL system. When the pressure increases to 8 MPa
CO
2
presents as supercritical state
and the output temperature drops to below –80 ℃. As the system pressure rises from 5 MPa to 9 MPa
the drilling temperatures of CFRP and Ti6Al4V layers decrease by 15.91% and 50.78%
axial forces increase by 65.22% and 20.26%
and torques decrease by 23.33% and 16.77%
respectively. Moreover
the burr height at the Ti6Al4V layer exit decreases by 42.04%
the delamination factor at the CFRP layer exit is reduced by 5.41% and a low roughness of borehole wall of CFRP/Ti6Al4V laminates is achieved at pressures of 7 MPa
8 MPa and 9 MPa.
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