Abstract

Carbon fibre reinforced polymer composites (CFRPs) can be costly to manufacture, but they are typically used anywhere a high strength-to-weight ratio and a high steadiness (rigidity) are needed in many industrial applications, particularly in aerospace. Drilling composites with a laser tends to be a feasible method since one of the composite phases is often in the form of a polymer, and polymers in general have a very high absorption coefficient for infrared radiation. The feasibility of sequential laser–mechanical drilling for a thick CFRP is discussed in this article. A 1 kW fibre laser was chosen as a pre-drilling instrument (or initial stage), and mechanical drilling was the final step. The sequential drilling method dropped the overall thrust and torque by an average of 61%, which greatly increased the productivity and reduced the mechanical stress on the cutting tool while also increasing the lifespan of the bit. The sequential drilling (i.e., laser 8 mm and mechanical 8 mm) for both drill bits (i.e., 2- and 3-flute uncoated tungsten carbide) and the laser pre-drilling techniques has demonstrated the highest delamination factor (SFDSR) ratios. A new laser–mechanical sequence drilling technique is thus established, assessed, and tested when thick CFRP composites are drilled.

Highlights

  • IntroductionThe Airbus A350 XWB is made of carbon fibre reinforced polymer composites (CFRP)

  • The Airbus A350 XWB is made of carbon fibre reinforced polymer composites (CFRP)(52% fuselage components and wing spars) [1], which overtake the Boeing 787 Dreamliner for the highest weight ratio of a CFRP aircraft, which was previously 50% [2]

  • 8 mm for both tools and laser pre-drilled strategies (i.e., single-side (SS) and double-side (DS)). This observation is present in the experimental work of Sobri et al [6]. This result could be due to the presence of the pre-drilled holes, because the drill bit tool diameter has the same diameter and is unable to eliminate the heat-affected zone (HAZ) contributed by the laser beam

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Summary

Introduction

The Airbus A350 XWB is made of carbon fibre reinforced polymer composites (CFRP). (52% fuselage components and wing spars) [1], which overtake the Boeing 787 Dreamliner for the highest weight ratio of a CFRP aircraft, which was previously 50% [2]. This was one of the first commercial aircraft with composite wing spars. The Airbus A380 was one of the first commercial aircrafts to have a central CFRP wing box. It was the first aircraft to have a smooth wing section rather than wings that are divided into sections span-wise. The appropriate tool geometry, combined with the proper process conditions and ideal machining efficiency, can result in an acceptable level of damage [4]

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