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Influence of tool nose angle on cutting performance in hot machining of Inconel 718

Abstract

Superalloy Inconel718 is an important material for aircraft preparation because of its excellent performance at high temperatures. However, when cutting Inconel718, a large amount of cutting heat will be generated, resulting in excessive tool temperature and serious wear, which accelerates the tool failure. In order to solve this problem, the influence of tool angle on the process of thermal aided machining was studied by simulation model combined with thermal aided machining technology. During the cutting process, the workpiece preheating temperature rises from room temperature 20° C to 500° C, the front tool angle range is − 5° to 10°, and the rear tool angle range is 4° to 16°. By analyzing various parameters, it was found that a smaller tool rake angle can effectively reduce the tool temperature. Additionally, a flank angle of around 12° was found to decrease the maximum wear area of the tool by approximately 10.5%. Moreover, it was observed that implementing heat-assisted machining can result in a significant reduction of tool temperature by 11.1%, as well as a decrease in cutting force ranging from 18 to 22%, particularly at temperatures exceeding 500 °C.

Introduction

Nickel alloys are extensively utilized in industries such as aerospace and precision machinery due to their exceptional properties. However, the high temperatures generated during the cutting process and the challenging nature of processing these alloys make them difficult and costly to machine. Additionally, these conditions can adversely affect the lifespan of the machining tools.

In recent years, there has been a growing interest among researchers in utilizing heat-assisted machining technology for processing nickel alloys. Several studies have shown that this technology can effectively reduce cutting forces and extend the tool life during the hot working process. Venkatesan et al. [1,2,3] conducted research on cutting Inconel 718 using laser heat-assisted technology. They found that this approach could reduce cutting forces, minimize tool wear, and improve the surface roughness of the workpiece. They also discovered that a 60° laser heating angle was particularly effective. Moon and Lee [4] employed plasma thermal machining to mill Inconel 718 and AISI1045 workpieces. Their findings revealed that this method could decrease cutting forces and enhance the surface integrity of the workpiece. Tosun and Ozler [5, 6] utilized liquefied petroleum gas as a heat source to heat the workpiece and cut manganese steel materials. They observed that this technique could improve tool life and reduce the surface roughness of the workpiece. Sofuoğlu M A et al. [7,8,9,10,11] studied the energy consumption factors in thermal-assisted machining of aerospace materials and conducted economic research and optimized the parameters of thermal-assisted machining combined with different simulation software. Parida et al. [12,13,14,15] focused on heat-assisted machining of titanium alloys and nickel-based alloys. Their research indicated that this approach could enhance the chip formation process, reduce cutting forces, and decrease the material’s resistance to machining strength. They also discovered that increasing the hot working temperature further improved these effects.

Despite the increase in cutting temperature associated with heat-assisted machining, researchers continue to explore its application in processing nickel alloys. To address the issue of high temperatures, studies have investigated ways to reduce cutting temperature through different approaches. One aspect researchers have focused on is the tool nose angle, as it has been found to have a significant impact on cutting temperature. By adjusting the tool nose angle, researchers have discovered that it can improve cutting temperature in both roughing and finishing processes of the material. Qu et al. [16] conducted grinding experiments by varying the rake face angle and found that a larger rake angle on the cutting edge effectively reduces surface roughness, improves surface quality, and decreases grinding force and energy consumption. Azaath et al. [17] studied the effect of rake angle and tool geometry on the machining process of AISI4340. They observed that varying the rake angle altered the chip-tool contact, leading to a reduction in tool wear rate. Saptaji et al. [18] investigated the influence of corner angle and tool nose angle in micro-milling and found that increasing the angle effectively reduced burr formation. Anilchandra et al. [19] found that a negative rake angle facilitated chip breakage and minimized the impact of continuous chips on the machined surface. Liu et al. [20] examined the effect of tool nose angle on cutting Al-based SiC materials and discovered that negative chamfers ensured the integrity of the workpiece surface. This is because the angle of the tool tip influences the direction of force acting on the silicon carbide particles. In summary, there are optimal tool nose angles for machining different materials. Researchers have explored and identified these angles to improve the cutting temperature, quality, and efficiency in various machining processes.

Heat generation in cutting is primarily influenced by plastic deformation and friction, which are directly related to the rake and relief angles of the tool. Furthermore, the volume of the tool tip plays a crucial role in heat transfer. The volume of the tool tip is also associated with the rake and relief angles of the tool. In this study, the focus is on investigating the effects of different nose angles on various parameters in the cutting process, specifically when thermally assisted machining of nickel alloys is employed. The aim is to understand the relationship between the tool angle and parameters such as cutting temperature and cutting force through range analysis, while ensuring the preservation of the advantageous features of thermal-assisted machining technology.

Experimental

Johnson–cook model for Inconel 718

Given that cutting processes can induce significant thermal strains in the material and are conducted under thermally assisted machining conditions, the Johnson–Cook (J-C) model is chosen as the material model in this study. References [21, 22] demonstrate the simulation results with different J–C model parameters, which confirm the reliability of the model. The model utilized in this study is represented by the following equation:

$$\sigma =\left(1290+895{\varepsilon }^{0.526}\right)\times \left(1+0.016\mathit{ln}\frac{\overline{\varepsilon }}{0.03}\right)\times \left(1-{\left(\frac{T-{T}_{r}}{{T}_{m}-{T}_{r}}\right)}^{1.55}\right)$$

where σ is the flow stress, ɛ is true strain, \(\overline{\varepsilon }\) is true strain-rate, and T, Tm, and Tr are work, material, and melting and room temperature respectively (Tm = 1300 °C, Tr = 20 °C).

The chemical composition and thermo-physical properties of Inconel 718 alloy for the cutting test are shown in Tables 1 and 2.

Table 1 Chemical composition of the Inconel 718 [23]
Table 2 Physical and mechanical properties of Inconel718 at different temperatures

The establishment of the simulation process

The finite element method is employed to analyze heat-assisted processing. In the experimental process, the heating device for the material is depicted in Fig. 1a. Figure 1b illustrates the principle of thermal processing for the material, where a flame torch is used for heating and a temperature detection device monitors the thermal processing temperature.

Fig. 1
figure 1

Hot machining. a Experimental setup [24]. b Schematic diagram. c The boundary and meshing conditions of FE models

The geometric configuration and boundary conditions of the finite element simulation model are presented in Fig. 1c. The workpiece model has a height of 0.7 mm and a length of 3 mm. In the simulation experiment, the workpiece material utilized is Inconel 718, and an adaptive meshing method is applied for workpiece meshing. The minimum mesh size is set to 4 μm, and the maximum mesh size is 70 μm. Higher mesh density is employed based on the relative changes between the workpiece and the tool. The total number of elements in the model amounts to 1668.

The bottom of the workpiece is fixed as a boundary condition, with a constant moving speed of 88 m/min in the X direction and fixed in the Y direction. The depth of cut is 0.1 mm, and the tool material is WC cemented carbide with a nose radius of 20 μm.

Angle analysis

The theoretical force model of the rake angle in different states is illustrated in Fig. 2. When the tool rake angle is negative, the material undergoes compression during the cutting process, causing a downward force component on the workpiece material. When the tool is cutting vertically, the force on the material is solely the cutting force in the horizontal direction, with no vertical cutting force acting on it. Conversely, when the tool rake angle is positive, it can be observed that the cutting force on the material is more pronounced, aiding in the separation of the chips from the workpiece. A comprehensive comparison reveals that when the tool rake angle is negative, the cutting force is greater due to the mutual compression of the material between the tool surface and the workpiece. Therefore, when the tool angle is negative, the overall cutting force during the cutting process is greater compared to the other two conditions. Furthermore, when the rake angle is negative, the compression of the material worsens the heat dissipation conditions during cutting. As a result, the maximum value of the cutting temperature generated during the cutting process theoretically tends to be higher when the tool rake angle is negative compared to the other two conditions.

Fig. 2
figure 2

The state of cutting force components at different nose angles

The influence of the relief angle on the cutting temperature and cutting force is not significant compared with the rake angle, but it will still have different degrees of influence on the quality of the machined surface of the material and the degree of heat dissipation.

Take into account that in the cutting process, the tool geometry angles required for roughing and finishing are different. In this paper, four different rake angles and knife relief angles were selected. And compared with 4 different heat-assisted processing temperatures, the combination is shown in Table 3.

Table 3 Parameters for the cutting simulation

Friction model

The primary source of friction encountered in the cutting process arises from the relative motion that occurs when the cutting tool and the surface of the workpiece come into contact. Accurately predicting and describing the friction behavior between the tool and the workpiece surface is a challenging issue that needs to be addressed in the current field of cutting. Successfully resolving this problem is essential for ensuring the precision of cutting simulation outcomes. In a study conducted by Özel et al. [25], the researchers examined the impact of different friction models on the cutting process. The friction model using the hybrid model is \(\tau =\mathrm{\mu k}\). The value of μ is shown in Table 4.

Table 4 Friction and wear parameter

Wear model

In this study, the Usui wear model was employed, and the finite element-based tool wear prediction method developed by Yen et al. [26] was utilized in a two-dimensional model. The simulation results obtained using the Usui wear model were compared with experimental data in this paper, and its reliability was confirmed by Malakizadi et al. in their research [27]. The Usui wear model is represented by the following equation.

$$\omega =\int {apVe}^{-b/T}dt$$

where p is interface pressure, V is sliding velocity, T is interface temperature, dt is time increment, and a and b are experimentally calibrated coefficients. And a and b are set to 1 × 10−5 and 1000 respectively.

Results and discussion

Simulation and experiment comparison

Figure 3 presents a comparison of cutting forces and specific cutting energy during the cutting of nickel-based alloys under thermally assisted machining conditions. The results indicate a close resemblance between the simulated results obtained using the power exponential J–C model and the experimental data. This result shows the cutting force and specific cutting energy state at different cutting depths (specifically 0.1 mm and 0.15 mm) at a cutting speed of 66 m/min, and the simulation results are very close to the experimental results.

Fig. 3
figure 3

Comparison of experimental [24] and simulated data. a Cutting forces. b Specific cutting energy

Figure 4 illustrates a comparison between the simulated results obtained using the power function J–C model and the experimental cutting results. In the experiment, the tool had a rake angle of 20°, relief angle of 7°, and a cutting edge with a blunt round radius of 20 μm. The findings indicate a close agreement between the simulation and experimental results, particularly in terms of chip thickness and cutting thickness.

Fig. 4
figure 4

Simulated and measured [23] chip morphology

Result data

The cutting simulation is carried out according to the combination scheme given in Table 3, and the cutting parameters are set as fixed values. The cutting speed is 88 m per minute, and the depth of cut is 0.1 mm. Tables 5, 6, 7, and 8 show the resulting data for different tool nose angles at different heat-assisted machining temperatures.

Table 5 Cutting data results for different nose angles at 20 °C
Table 6 Cutting data results for different nose angles at 100 °C
Table 7 Cutting data results for different nose angles at 300 °C
Table 8 Cutting data results for different nose angles at 500 °C

In this paper, the temperature change, cutting force, and wear state caused by tool angle change in the cutting process are analyzed.

Cutting temperature

In the cutting process, the cutting temperature plays a crucial role in determining the quality of the cut, while the temperature of the tool itself affects tool wear and service life. Figure 5 displays the temperature distribution variations across the rake angle during thermally assisted machining. Under different heat-assisted machining temperature conditions, it is observed that both the maximum cutting temperature and the high-temperature range decrease as the rake angle increases. This implies that as the rake angle increases, the extrusion effect of the tool on the workpiece material decreases, leading to an expanded temperature diffusion area and subsequently reducing the cutting temperature. Additionally, as the rake angle increases, the chip shape transitions from a continuous shape to a sawtooth shape. However, once the heat-assisted processing temperature surpasses 500 °C, the chip shape remains continuous without further changes, presumably due to the softening of the workpiece material at higher temperatures, eliminating serration. Furthermore, it can be noted that as the thermally assisted machining temperature increases, the influence of the tool nose angle on the cutting temperature gradually diminishes. Nevertheless, increasing the rake angle still contributes to lowering the maximum cutting temperature.

Fig. 5
figure 5

Temperature distribution for different nose angles and heat assist temperatures (relief angle = 4°)

While the influence of the flank angle on the cutting temperature may not be readily apparent, it does have a considerable impact on the temperature distribution within the machined workpiece. Figure 6 displays the temperature distribution of the machined workpiece for various flank angles. It is observed that as the flank angle increases, the range of the high-temperature area within the machined part gradually diminishes. This can be attributed to the fact that a smaller flank angle results in greater surface extrusion, thereby generating more frictional heat and facilitating a higher rate of temperature diffusion.

Fig. 6
figure 6

Temperature distribution of machined surface at different relief angles (rake angle = 0°)

Table 9 demonstrates that regardless of the thermally assisted machining temperature conditions employed, the change in rake angle has a more pronounced effect on the temperature of the heated tool compared to the change in flank angle. Furthermore, apart from the optimal tool angle choice of a rake angle of 5° and relief angle of 8° at room temperature, the optimal tool angle selection under other thermally assisted machining temperature conditions is a rake angle of 5° and relief angle of 4°. At room temperature, there is a temperature difference of 0.25 °C between the relief angle of 4° and relief angle of 8°. Consequently, the lowest tool temperature solution is achieved with a rake angle of 5° and relief angle of 4°. This is owing to the fact that an excessively large tool nose angle results in a smaller tool volume, causing the same amount of heat to be concentrated within a smaller volume, leading to elevated temperatures. Conversely, a tool angle that is too small allows for wider temperature dispersion within the tool, thereby reducing the average tool temperature.

Table 9 Temperature range analysis table

Figure 7 illustrates the variation in average tool temperature as the tool angle changes. It is evident that as both the rake angle and flank angle increase, the tool temperature also rises. This phenomenon arises because, while increasing the rake angle can reduce the heat generated from cutting, it also reduces the volume of the tool tip and consequently hampers heat dissipation. Thus, an excessively large rake angle fails to effectively lower the tool tip temperature. Notably, at heat-assisted machining temperatures of 300 °C and 500 °C, the tool temperature is notably lower compared to other heat-assisted temperatures. This implies that an increase in heat-assisted machining temperature can contribute to a certain extent in reducing tool temperature.

Fig. 7
figure 7

Average tool temperature at different nose angles

Cutting force

The cutting force is another important parameter in the cutting process, and its magnitude is related to tool life. Figure 8 reveals that the cutting force gradually decreases with an increase in rake angle, in line with the previous analysis of tool angle. Meanwhile, when the rake angle is negative, the cutting force increases due to material extrusion between the tool surface and the workpiece. As the rake angle increases, less material is extruded, resulting in a corresponding reduction in cutting force. On the other hand, the change in flank angle does not significantly affect the cutting force. Notably, at thermally assisted machining temperatures of 300 °C and 500 °C, the cutting force is significantly reduced. This observation correlates with the decrease in tool temperature as the thermally assisted machining temperature increases. Figure 9 illustrates the heat transfer states under different contact conditions. When the cutting force is substantial, as shown in Fig. 9a, the tool and the chip are in complete contact, facilitating significant heat transfer. However, as the cutting force decreases, the contact force between the tool surface and the chip diminishes, creating a larger gap as depicted in Fig. 9b. This gap accelerates the transfer of cutting temperature to the air, thereby reducing the temperature transferred to the tool.

Fig. 8
figure 8

Average cutting force at different nose angles

Fig. 9
figure 9

Heat transfer in different contact states

Wear

The change in tool angle, particularly the rake angle, has a significant impact on the chip flow state. Figure 10 depicts the cutting process, wherein some materials tend to flow slowly or even stagnate near the tool tip’s corner, resulting in the formation of a built-up edge known as the dead metal zone (DMZ) [28]. The presence of the DMZ enhances the strength of the cutting edge near it, but it also increases the cutting force. Notably, as shown in Fig. 10, the DMZ is located at the upper part of the tool nose angle [29], and its position does not vary significantly with changes in the thermally assisted machining temperature. This phenomenon has been demonstrated in previous studies as well [30]. Figure 11 illustrates that the minimum wear depth of the tool is situated near the DMZ, while the deepest wear area is near the flank face. As a result, changes in the tool rake angle have no noteworthy effect on the deepest wear area of the tool. However, according to Table 10, increasing the heat-assisted machining temperature helps reduce the deepest wear depth when choosing a larger rake angle.

Fig. 10
figure 10

The position of dead metal zone. a Simulation. b Experimental [24]

Fig. 11
figure 11

Tool wear status

Table 10 Wear range analysis table

Figure 12 indicates that the smallest deepest wear value is observed when the flank angle is set at 8° and 12°. Therefore, a suitable flank angle falls within the range of approximately 8°–12°. At a heat-assisted machining temperature of 100 °C, the wear depth is higher compared to that at room temperature. This can be attributed to the increased cutting temperature resulting from elevated heat-assisted temperature. However, the cutting force does not decrease significantly, leading to an increased tool wear rate. On the other hand, at a heat-assisted machining temperature of 500 °C, the wear depth is notably reduced. This reduction can be attributed to the decrease in cutting force, which leads to reduced heat transfer from the chip to the tool, resulting in decreased friction force and subsequent reduction in tool wear.

Fig. 12
figure 12

Average tool wear at different relief angles

Conclusions

Through the establishment of a simulation model for the cutting process of Inconel 718, a difficult-to-machine material, and the investigation and analysis of the influence of cutting process parameters, the following conclusions can be drawn:

  • 1. The tool angle exhibits a positive correlation with tool temperature. A smaller tool nose angle can effectively reduce the tool temperature, but it may result in an increase in cutting temperature. When roughing materials that can withstand high temperatures, a smaller tool nose angle can be chosen. When finishing, it can be paired with a larger tool nose angle and a thermally assisted processing temperature above 300 °C. This approach ensures processing accuracy while reducing tool temperature.

  • 2. The change in flank angle does not have a significant effect on cutting force. Cutting force decreases as the rake angle increases. Increasing the heat-assisted processing temperature can effectively reduce cutting force, with a reduction of 10.8% at 300 °C and 22% at 500 °C.

  • 3. The smallest wear depth under different heat-assisted processing temperatures is observed when the flank angle is approximately 8°–12°. To minimize tool wear, a flank angle of about 8°–12° is recommended.

  • 4. When machining Inconel 718, it is essential to consider tool temperature, cutting force, and tool wear comprehensively. Selecting a rake angle of 5°–10°, a flank angle of 8°–12°, and a heat-assisted processing temperature of 300 °C or higher can effectively improve the cutting conditions and prolong tool life.

Availability of data and materials

The material and data in this paper are obtained by software simulation and quoting other people’s experimental data.

Abbreviations

DMZ:

Dead metal zone

J-C model:

Johnson-Cook model

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Acknowledgements

Thanks to Professor Zhicheng Zhang and Professor Xiaofei Cheng for their suggestions on the revision of the article, so as to make the content of the article more abundant and standardized.

Funding

This work is supported by the Youth Fund of Shandong Agriculture and Engineering University (QNKJZ202301).

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Xiaoliang Lin and Xiaowei Jia analyzed and verified the usability and accuracy of the model. Xin Liu modeled the tool and analyzed the performance comparison of different texture tools and the effect of texture on the tool. All authors read and approved the final manuscript. Yueyang Li and Changfeng Shao contributed to the content structure and language polishing of the article.

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Correspondence to Xin Liu or Yueyang Li.

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Liu, X., Lin, X., Jia, X. et al. Influence of tool nose angle on cutting performance in hot machining of Inconel 718. J. Eng. Appl. Sci. 71, 90 (2024). https://doi.org/10.1186/s44147-024-00423-9

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