Drilling Machinability of Glass, Basalt, and Hybrid Epoxy Composites: Thrust Force, Thermal Load, and Hole Quality

玻璃、玄武岩和混合环氧复合材料的钻孔加工性能:推力、热载荷和孔质量

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Abstract

The drilling machinability of glass fiber G(14), basalt fiber B(14), and two hybrid laminates (B(4)G(6)B(4), G(4)B(6)G(4)) was evaluated through 36 full-factorial experiments employing an HSS-G drill, three spindle speeds (715, 1520, 3030 rpm), and three feed rates (0.1-0.3 mm rev(-1)). Peak thrust force varied from 65.8 N for B14 at 0.1 mm rev(-1) to 174.3 N for G(14) at 0.3 mm rev(-1); hybrids occupied the intermediate range of 101-163 N. Infra-red thermography recorded maximum drill temperatures of 110-120 °C for G(14), almost double those of B(14), while both hybrids attenuated hotspots to below 90 °C. ANOVA attributed 73.4% of thrust force variance to feed rate, with material type and spindle speed contributing 15.5% and 1.7%, respectively; for temperature, material type governed 41.5% of variability versus 17.0% for speed. Dimensional quality tests revealed that the symmetric hybrid G(4)B(6)G(4) maintained entrance and exit diameters within ±2% of the nominal 6 mm, whereas B(4)G(6)B(4) over-expansion exceeded 8% at the lowest feed and G(14) exit diameters grew to 6.1 mm at 0.3 mm rev(-1). Integrating basalt compliance with glass stiffness, therefore, halves thrust force relative to G(14), suppresses delamination and overheating, and offers a practical strategy to prolong tool life and improve hole quality in multi-material composite structures. These insights guide parameter selection for lightweight hybrid composites in aerospace, renewable-energy installations, and marine components worldwide.

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