2014
DOI: 10.1016/j.procir.2014.04.068
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Influence of Lay-up Configuration and Feed Rate on Surface Integrity when Drilling Carbon Fibre Reinforced Plastic (CFRP) Composites

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Cited by 34 publications
(12 citation statements)
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“…When the load exceeds the fiber yield strength, failure occurs below the cutting plane/surface with the debris removed as the tool passes, which creates cavities or grooves onto the surface. [ 38 ] Additionally, fiber pullouts owing to the fiber/matrix interface debonding and fiber fragments inserting inside the interlayers are prevalent in the drilling process of carbon/PI composites. The phenomenon is attributed to the inherent brittleness of the carbon/PI material which involves the brittle‐fracture dominated chip removal mode leading to the powdery chip formation.…”
Section: Resultsmentioning
confidence: 99%
“…When the load exceeds the fiber yield strength, failure occurs below the cutting plane/surface with the debris removed as the tool passes, which creates cavities or grooves onto the surface. [ 38 ] Additionally, fiber pullouts owing to the fiber/matrix interface debonding and fiber fragments inserting inside the interlayers are prevalent in the drilling process of carbon/PI composites. The phenomenon is attributed to the inherent brittleness of the carbon/PI material which involves the brittle‐fracture dominated chip removal mode leading to the powdery chip formation.…”
Section: Resultsmentioning
confidence: 99%
“…Previous work reported that instantaneous cutting forces (frequency and magnitude) varied with the varying fibre orientation and relative position between the cutting edge and the fibres, which affected the machined surface quality [32]. Additional studies showed that the cutting forces and surface roughness developed in the machining of composites depend on the orientation of the fibres and the way in which fibres are cut [33,34], and that angle ply laminates are easier to machine than unidirectional ones [35].…”
Section: Analysis Of the Thrust Force Fz And Torque Mzmentioning
confidence: 99%
“…The CFRP composites are being introduced in the fabrication of major structural members of aircrafts with floor beams, frame panels and significant portion of the tail sections being the specific examples. 6 CFRP members in these applications are typically joined through mechanical fastening, i.e. riveting and bolting, requiring as much as tens of thousands of drilled holes for the complete assembly.…”
Section: Introductionmentioning
confidence: 99%