To study the enhancement mechanism of the combined laser in comparison with the single laser, single laser irradiation was first performed followed by combined laser irradiation. The ablation process and effect were compared and analysed.
3.1. CW Laser
Using a 2-mm thick target and CW laser irradiation for approximately 35 s in the 1-on-1 mode, we obtained the temperature evolution law and ablation morphology characteristics at different times during CW laser ablation, as shown in
Figure 2.
As shown in
Figure 2, according to the increasing temperature law of laser irradiation and the evolution characteristics of ablation morphology, the entire process from initial CW laser irradiation to target burn-through can be divided into four stages. Stage I (0~10.4 s), the solid-state heating stage: owing to the short laser irradiation time, the target had not undergone a phase transition, the temperature increase rate of the test point was approximately 20.7 K/s; the aluminium alloy surface was softened via heating, and an annular plastic strain, such as “annular folds”, was generated under the internal thermal stress, as shown in
Figure 2a. Stage II (10.4~10.8 s), the phase transition stage: the target changed from solid to liquid, with the phase transition lasting for approximately 0.4 s. Stage III (10.4~15.0 s), the liquid heating stage: the metal target experienced a rapid increase in temperature, the laser absorptivity of the liquid aluminium alloy was higher than that of the solid aluminium alloy [
20], leading to the rapid deposition of subsequent laser energy, and the temperature increase rate of the test point increased to 80.1 K/s. Stage IV (15~35 s), the oxidation reaction stage (in which oxygen participates due to ablation in the air): part of the liquid aluminium alloy experienced a violent oxidation reaction, white dust Al
2O
3 was produced during the combustion, and the ablation area was concentrated at the centre of the melted area, as shown in
Figure 2c. At this stage, when the spot thermometer is working, more high-frequency noise may occur because the spattering oxides will interfere with the collection of incident laser and temperature measurement spectrum.
Laser ablation can be divided into longitudinal ablation in the direction of laser transmission and transverse ablation in the direction of the beam radius. The overall ablation and removal of the material can be analysed using Equation (2).
where
is the mass removal or the mass difference of the target before and after laser irradiation,
E is the laser energy,
P is the laser power, and
τ is the duration of CW laser irradiation.
Subsequently, the melting diameter
D_cw (as shown in
Figure 2c), caused by the CW laser on the front surface of the target, and ablation rate were studied, as shown in
Figure 3.
As shown in
Figure 3, an increase in irradiation time resulted in an increase in the melting diameter and a decrease in the ablation rate. The mass ablation rate of the CW laser was low at approximately 0.8–1.3 μg/J. This shows that when CW laser is applied for ablation, the thermal conduction effect will cause diffusion and consumption of the absorbed energy, resulting in less energy being focused on the ablation and removal of the material.
3.2. Ms Pulsed Laser
The characteristics of the hole ablated using the ms pulsed laser indicate the strength of the mechanical effect. In this experiment, the 1-on-1 mode was adopted to study the relationship between the characteristics of the ablated hole in the target under ms pulsed laser irradiation and the pulse energy. The morphology of the ablated hole is shown in
Figure 4.
As shown in
Figure 4, as the energy density of the ms pulsed laser increased, clear differences were found in the morphology of the ablated hole. When heated using the ms pulsed laser, the target melted and vaporised, and the high-temperature steam generated recoil vapour pressure, causing the melted substance to flow out of the melting pool. When the energy density was low, the recoil vapour pressure was small, and the melted substance was only pushed out of the melting pool and resolidified at its edge, as shown in
Figure 4a. As the energy density increased, the range of the melting pool expanded, and the recoil vapour pressure also increased gradually. After the melted substance was pushed out of the melting pool, it resolidified around the pool as a spattering pattern, as shown in
Figure 4b,c. When the energy density reached 1000 J/cm², the recoil vapour pressure enabled the melted substance to overcome the surface tension [
21,
22], which then separated, broke, and flew out of the melting pool opposite to the laser incident direction. The recast layer was barely visible at the edge of the melting pool, as shown in
Figure 4d.
Under ms pulsed laser irradiation, the evolution of the ablated hole size and the ablation rate were closely related to the pulsed laser energy, which are shown in
Figure 5.
As shown in
Figure 5, before the target was perforated, the diameter, depth, and ablation rate of the ablated hole all increased with laser energy density. Their trends maintained a rapid then gradual increase before becoming flat. This indicates that ms pulsed laser ablation increased the depth and diameter of the ablated hole at the same time, thus enhancing the utilisation of laser energy compared with that of the CW laser. When the energy density was approximately 1000 J/cm², the target was perforated, and part of the laser energy passed through the ablated hole, resulting in a reduction in the ablation rate. In general, under the irradiation of the ms pulsed laser (5 mm spot diameter), the diameter of the ablated hole ranges from 0 to 3 mm, and the ablation rate ranges from 8 to 110.7 μg/J. The ablation rate is well consistent with the earlier work of Gao et al., in which the experiment result is 6.7–121.8 μg/J [
23].
3.3. CW/ms Combined Laser
The CW/ms combined laser damage experiment included two modes of parameter matching. First, time matching: the ms pulsed laser energy was kept constant (205.2 J/cm²) to study the effect of CW laser irradiation time (τ: 5~25 s) on ablation efficiency. Second, energy matching: the CW laser irradiation time was kept constant (13 s) to study the effect of ms pulsed laser energy on ablation efficiency.
Figure 6 shows the ablation rate results in the four cases: the CW laser, ms pulsed laser, combined laser time matching, and combined laser energy matching.
As shown in
Figure 6, when the 205.2 J/cm² ms pulsed laser was used alone, the ablation rate was 75.7 μg/J. However, under the irradiation of the CW/ms combined laser, the ablation rate of the ms pulsed laser was greatly enhanced to 170.4~1928.8 μg/J, with a maximum increase of 24.5 times.
Under combined laser irradiation, mass ablation rate can be greatly enhanced, and there are significant differences in ablation morphology. Tests were conducted on the damage morphologies generated by the CW laser (5~25 s, with an interval of 5 s), the ms pulsed laser (205.2 J/cm²), and a combination of the two under different time matchings, as shown in
Figure 7.
As shown by the damage morphology in
Figure 7, the combined laser had greater damage efficiency than the single laser. Based on the damage morphology evolution characteristics of the combined laser under different time matchings, the ablation mechanism could be classified into three types, as shown in
Figure 7c. Type I, insufficient thermal effect: when the CW laser preheating time was short (≤10 s), the target did not melt. Thus, when the pulsed laser irradiated, part of the energy was used to form a melting pool, whereas the other part was converted into the mechanical effect acting on the melting pool and causing mass removal. The thermomechanical coupling efficiency of the combined laser was low, and the target was not perforated. Type II, effectively matched thermomechanical effect: when the CW laser preheating time was moderate (13~15 s), the mechanical effect of the ms pulsed laser could completely flush the melted substance out of the melting pool and remove it from the target surface, resulting in a smooth through-hole morphology and perforated target. Type III, insufficient mechanical effect: when the CW laser preheating time was long (≥20 s), the melting pool caused by the CW laser was too large. The mechanical effect of the ms pulsed laser could only flush part of the melted substance out of the melting pool, resulting in an irregular through-hole morphology and perforated target.
To further clarify the causes of the three typical ablation mechanisms of the combined laser, research was conducted on the CW laser melting pool diameter (
D_cw), the pulsed laser ablated hole diameter (
D_pulsed), and the combined laser ablated hole diameter (
D_combined), as shown in
Figure 8. In general, the diameter of the pulsed laser ablated hole is approximately 2 mm. The CW laser melting pool diameter (with a maximum value of 7 mm) increased gradually with irradiation time. Under combined laser irradiation, the diameter of the ablated hole on the front surface of the target first increased and then decreased, ranging from 2 to 4 mm.
As shown in
Figure 8, when the CW laser preheating time was less than 10 s, the thermal effect of the CW laser was insufficient, and
η =
D_cw /
D_pulsed = 0. At this time, the damage morphology of the combined laser was similar to that of the pulsed laser, resulting in Type I ablation. The size of the ablated hole caused by the combined laser was slightly larger than that of the ablated hole caused by the ms pulsed laser because CW laser preheating increases subsequent laser absorptivity. Between the preheating times of 13 s and 15 s, the diameter of the melting pool caused by the CW laser was larger than that of the ablated hole caused by the pulsed laser, and
η ∊ [1.7,1.9]. The impact of the pulsed laser acted entirely on the melting pool, and the melted substance could be completely ejected from the pool under the impact pressure of vaporisation, realising efficient coupling in the thermomechanical effect of the combined laser. At these times, the diameter of the ablated hole caused by the combined laser was equivalent to the range of the melting pool caused by the CW laser, forming the Type II damage morphology. When the preheating time further increased, the range of the melting pool caused by the CW laser became too large and
η ≥ 2.4. The impact pressure could not completely remove the melt, resulting in a Type III damage morphology. As the melting pool expanded, the size of the through-hole first increased and then decreased. It can be concluded that the time matching of the combined laser can be regarded as the matching of the impact pressure of the pulsed laser with the range of the melting pool. Under the parameters used in this study, when the diameter of the melting pool caused by the CW laser did not exceed 1.9 times the diameter of the ablated hole caused by the pulsed laser, the mechanical effect of the pulsed laser could completely remove the melt.
By monitoring the temperature at the centre of the melting pool, it can be verified whether melting is completely removed.
Figure 9a shows the variation in temperature with time at the centre point of the front surface under combined laser irradiation. The target was firstly heated under CW laser irradiation. At 13 s, the target temperature increased sharply owing to the application of the ms pulsed laser (Point A) and rapidly decreased to 828.8 K after pulsed laser irradiation ceased (Point B). Because the melting point of the 7075 aluminium alloy ranges from 748 to 908 K, the temperature measured by the spot thermometer at this time was that of the solid–liquid interface. Therefore, it was speculated that the impact pressure of the ms pulsed laser would remove almost all the melted substance from the melting pool. As shown in
Figure 9b, which is a plot of the centre-point temperature at the end of pulsed laser irradiation (Point B) under different time matchings, when the preheating time did not exceed 15 s, the temperature of the melting pool under ms pulsed laser irradiation was always maintained within the melting point range of the material, indicating that the mechanical effect of the pulsed laser could completely remove the melt from the melting pool; when the preheating time was greater than 15 s, the test result of the spot thermometer was greater than the melting point range, indicating that the melted substance had not been completely removed. This is consistent with the results of previous analyses.
3.4. CW/ns Combined Laser
An aluminium alloy with a thickness of 1 mm was adopted as the experimental target.
Figure 10 shows the ablation rate of the target under four irradiation conditions: that is, the CW laser, ns pulsed laser, combined laser time matching, and combined laser energy matching. As shown in
Figure 10, the ablation rate of the aluminium alloy irradiated by the CW laser ranged from 1.54 to 1.79 μg/J, and the ablation rate of the aluminium alloy irradiated by the ns pulsed laser ranged from 6.54 to 26.26 μg/J. After CW laser preheating, the ablation rate of the ns pulsed laser was enhanced to 1228.92~22319.47 μg/J, with a maximum increase of 849.9 times that of the ns pulsed laser alone.
The CW/ns combined laser greatly improved the ablation rate of the ns laser pulse and presented new features in the ablation morphology, as shown in
Figure 11.
Figure 11 shows the damage morphologies of the target in three cases, namely, with the CW laser (irradiation time of 8 s), ns pulsed laser (48.7 J/cm²), and a combination of the two. When the CW laser irradiated the target for 8 s, a melting pool with a range of approximately 10 mm was generated on the target. A ns pulse was then added. Under its mechanical effect, the centre of the melting pool was perforated, with a perforation size of approximately 2 mm, equivalent to the spot size of the ns pulsed laser. At the same time, the entire melting pool sunk towards the rear surface, resulting in a height difference (∆h) from the front surface of the target. This occurred because of the laser-supported detonation wave (LSDW) under ns pulsed laser irradiation, and the mechanical effect of LSDW diffusion caused the entire melting pool to sink towards the rear surface [
24].