This study focused on analyzing the size, shape, and frequency of harmful dust particles from an exhaust filter generated at different drilling speeds, cemented carbide cutting tool wear, and the resulting delamination.
This study was divided into two main parts. The first part focused on the effect of changing cutting conditions (vc = 15, 35, 55 m/min, fn = 0.1 mm/rev.) on the size, shape, and frequency of harmful dust particles. The second part focused on the effect of the wear of the cutting tool with the proportion of CFRP delamination on the size, shape, and frequency of generated dust particles from the filter of the extraction device.
3.1. Effect of Cutting Conditions on the Size of Dust Particles
Table 5 shows the average values of the frequency of individual sizes of dust particles on the filter for the intervals of drilled holes. Particles were detected using confocal microscope and SEM images.
The percentage of particles smaller than ten μm in size was monitored during the analysis of harmful dust particles. This is the limit value for inhaling particles that are harmful to human health.
From the collected dust particles, it was found that for the cutting speed vc = 15 m/min, the proportion of particles smaller than five μm was 51%. For the cutting speeds vc = 35 and 55 m/min, it was 58%. The analysis shows that an increase in the cutting speed promotes an increase in the amount of harmful dust particles smaller than five μm in size. Cutting speeds vc = 35 and 55 m/min generate more dangerous dust particles, which are more harmful to human health.
The SEM analysis shown in
Figure 4 found that the carbon fibers broke at an angle or perpendicular to the longitudinal axis of the fibers. No longitudinal fiber breaks were evident. The fibers had a diameter of 6 μm, and their length ranged from units to tens of micrometers. Carbon fibers were split transversely or at 40–60° angles, i.e., with a pointed end. In addition, they also chipped off at the ends, creating the smallest dust particles. Despite the temperature that is generated when drilling the holes, there is no thermal effect on the shape and length of the particle characters. Epoxy resin, as a reactive plastic matrix, fractures brittlely and small fragments tend to aggregate. The emerging temperature does not affect the refractive character of the thermally conductive carbon fibers.
From a detailed analysis of the dust particles captured on the filter using a confocal microscope and SEM, the presence of four types of dust particles was proven:
fine dust (mixture of matrix and fibers) with dimensions from 1 μm to 5 μm,
free fibers with dimensions from 10 μm to 400 μm,
matrix pieces with dimensions from 5 μm to 40 μm,
fragments (matrix + fibers) measuring 100 μm to 500 μm.
From the results in
Table 6, as the cutting speed increases, the size of the dust particles decreases, and the frequency of the generated dust particles increases. The most significant amount of generated chips of the most diminutive dimensions was created at a cutting speed of
vc = 55 m/min. On the contrary, the smallest particles were made at a cutting speed of
vc = 15 m/min. At the same time, at the highest cutting speed,
vc = 55 m/min, the average size of the dust particles was 7.30 μm, while at the lowest cutting speed,
vc = 15 m/min, the average size of dust particles was 9.01 μm.
Elevated cutting speeds during CFRP machining significantly affect dust particle generation by enhancing brittle fracture behavior in both carbon fibers and the polymer matrix. The associated increase in cutting temperature reduces the mechanical strength of the matrix, promoting micro-fracturing and particle detachment. Moreover, higher cutting speeds concentrate the mechanical and thermal energy within a smaller interaction zone, resulting in intensified material disintegration. Consequently, higher cutting speeds lead to the formation of a greater number of ultrafine dust particles, which increases occupational health risks and necessitates effective dust extraction and filtration systems.
The measurements performed show that the size and frequency of dust particles are significantly influenced by the size of the cutting speed (
Figure 5). As the cutting speed increased from 15 to 55 m/min, smaller dust particles formed, and their frequency increased.
This means that a combination of a high cutting speed of 55 m/min and a feed of 0.1 mm/rev creates small, tiny, hazardous harmful dust particles (5 and 10 µm settle in the area of the nasopharynx or larynx, 2 and 5 µm settle between the trachea and bronchi, and particles smaller than 2 µm can then reach the bloodstream) [
1,
2].
As part of the study, the effect of the cutting speed on the amount of captured dust particles on the filter was also monitored. Dust particles caught on the extraction device’s filter and the machined CFRP were weighed on a calibrated laboratory scale, T-SCALE Electronics MFG—NHB-1500+. The dust particles caught on the extraction device’s filter and the machined material were weighed, and the percentage ratios, which are listed in
Table 7, were then calculated from these values.
As the cutting speed increases, the suction device’s efficiency increases noticeably. At the lowest cutting speed, vc = 15 m/min, the average ratio of extracted dust was only 26.1%. The rest of the chips remained trapped in the jig, on the machine plate, and scattered in the air. In contrast, at the highest cutting speed, vc = 55 m/min, the average ratio of extracted dust was up to 92.5%, i.e., a difference of up to 66.4%.
This phenomenon occurs because, at a higher cutting speed, the tool rotates so fast that the dust particles are more dispersed into the air, and thus, the extraction system can extract them better. At a low cutting speed, the chips tend to fall into the fixture onto the machine plate, and they are not dispersed into the air as much.
3.2. Effect of Cutting Tool Wear on the Size of Dust Particles and the Issue of Delamination
The wear values of the cutting tool were measured after 50 drilled holes. It follows from the performed measurement that as the cutting speed increases, so does the value of the wear of the cutting tool,
Table 8. The wear of the cutting tool was realized in the form of abrasion following Kroisova et al. [
17,
18], caused by abrasive carbon fibers acting on the tool as a polishing medium. The chips acted on the back of the cutting tool, resulting in a smooth and rounded area above the cutting edge,
Figure 6. On the surface of the cutting tool, tiny grooves and small local potholes were always formed, which were caused by the bending and deflection mechanism of the carbon fiber from the cutting point [
6,
8].
3.2.1. Effect of Cutting Tool Wear on the Frequency of Generated Harmful Dust Particles
The measurements clearly show that as the number of drilled holes increases, i.e., the tool wear increases, the frequency of harmful dust particles with a size of 1–5 μm also increases (
Table 9).
As the tool wears, the frequency of dust particles with a size of 1–5 μm increases by more than twofold. The matrix and the fibers were crushed into tiny pieces and mixed to form a finer dust dangerous to human health. It was shown that the wear of the cutting tool affected the frequency of hazardous dust particles. While the new, unworn tool tended to cut the fibers, the worn edge bent, broke, and crushed the fibers into finer dust that is very dangerous to human health.
3.2.2. Issues of Sample Delamination at the Entrance/Exit and Inside the Drilled Hole
Due to the negative effect of delamination on the structural quality, especially the integrity of laminates, and on the shape, size, and frequency of dust particles, this study also focused on this influencing factor.
Delamination is commonly defined as the separation of composite plies by the formation of interlaminar cracks. It is the most dominant machining defect in the drilling of thermoset CFRP, as it is often considered a limiting factor for machining tolerances and the reliability of drilled CFRP parts. Delamination occurs at both the tool entry and exit sides of the drilled hole. At the entry side, delamination happens due to peeling up the fibers as a result of a peeling force applied in an upright direction, which causes the debonding of either single fibers or the whole upper ply. However, the more severe damage happens on the exit side. There, the drill pushes the last remaining plies downward when the drilling process is getting to its end. Under this applied deformation, the thrust force may exceed the interlaminar bond strength of the laminate, leading to a separation of plies. Hence, this kind of delamination is called push-down delamination. The model of the delamination mechanism is shown in detail in
Figure 7 [
7,
19].
The delamination of the evaluated samples caused by drilling was monitored during the study using a stereomicroscope (
Figure 8, SEM
Figure 9) and computed tomography (CT—
Figure 10).
Figure 8 shows pull-out, push-down, and inside-the-hole delamination. Delamination is a very complex problem that includes the mechanics of delamination, the quality of the bond between the reinforcing fibers and the matrix, and the influence of the textile bond [
7,
18,
19]. During drilling, heterogeneous material (fibers, matrix) is removed.
The removed material is ground during drilling. The fibers and the matrix are crushed, affecting the character of the surface inside the hole. The character of the fibers is clearly visible in the images from the electron microscope (
Figure 4). They are shortened, broken, and chipped at the ends. This crushed material, generated during drilling, further destroys the material inside the holes.
The obtained results,
Figure 9 and
Figure 10, are in accordance with
Figure 11 [
20] about the occurrence of different levels of delamination in individual layers of the composite system.
As is evident, the issue of drilling composite materials is very complicated and includes many parameters that interact with each other. As shown in
Figure 7 [
7,
19], multiple types of delamination occur when drilling a multilayer composite system. Peel-up delamination on the surface is created by pulling the fibers upward as the drill bit passes through the composite system. The threads will break and create an unwanted burr on the surface of the hole.
When the drill bit passes through the material, the resin matrix is crushed, and the fibers are cut, broken, and pulled out according to how they are placed in the direction of the drill bit movement. The fibers released in this way simultaneously enter the space between the drill bit and the wall of the material and are further ground and crushed. Due to the mechanical parameters of carbon fibers, this crushed material can have a very destructive effect on the used drill, whose blade becomes dull. Chipping of submicrometer/nanometer particles from the ends of the carbon fibers is likely to occur at this stage. These particles, on the one hand, stick to the inner surface of the holes, and on the other hand, they are sucked out during drilling. This study confirmed previous research results that the greatest delamination occurs in the middle of the thickness of the evaluated sample [
20]. This fact is probably correlated with the distribution of the carbon reinforcing fibers, the highest stiffness of the system, and the highest energy that the drill has to develop to pass through the material. Delamination in this central part of the sample,
Figure 10, is then the cause of reduced integrity around the drilled hole or the integrity and stability of the entire system. It can be seen from
Figure 10 that the delamination between the layers detected by CT analysis reaches a length of 2.59 mm. The thickness of the sample is 4.5 mm.
When the drill bit passes through the lower part of the composite material, the fibers are pushed out on one side and separated from the matrix. The tensile load of the fibers increases, causing their subsequent destruction. This delamination is called push-down and is characterized by the simultaneous creation of a cavity between the final and penultimate layers of the composite system (
Figure 10 and
Figure 11). After passing the drill, the fibers break due to their tensile strength limit being exceeded and create visible burrs on the lower surface of the sample, which makes it difficult to perform other technological operations (
Figure 10).
From the above analysis, it is clear that the drill’s passage through the central part of the system has the greatest impact on the formation of micrometer/submicrometer and nanometer particles dangerous to human health [
21] (
Figure 12). This part is also the most problematic in terms of reducing the integrity of the material caused by the failure of the composite system’s cohesion layers (
Figure 7,
Figure 8 and
Figure 9). The presence of fine particles is all the more dangerous the smaller and lighter they are, as they can then move in the air for longer periods of days or weeks and can be transported over distances of hundreds of kilometers. Based on these facts, it is clear how essential it is to incorporate filtration equipment into plant machining composite systems, particularly with carbon fiber, to minimize the release of these particles into the environment and maximize human protection. Even the simplest extraction equipment that is co-joined with the drilling area of composite systems will provide at least partial protection for the operator. There may also be opportunities to minimize dust particles and delamination in new equipment and new processes [
12,
13,
14].
The issue of studying the drilling of composite systems is interesting both from the point of view of setting optimal cutting conditions and minimizing tool wear, as well as from the point of view of minimizing the formation of dust particles during machining. No less important is the study of the possibilities of influencing the delamination process by setting the technological conditions and any subsequent operation, which could minimize or eliminate the resulting defects.