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
Summary
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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