Machinability Study of Steels in Precision Orthogonal Cutting

The miniaturization of components and systems is advancing steadily in many areas of engineering. Consequently, micro-machining is becoming an important manufacture technology due to the increasing demand for miniaturized products in recent years. Precision machining aims the production of advanced components with high dimensional accuracy and acceptable surface integrity. This work presents an experimental study based on Merchant and Lee & Shaffer theories applied to precision radial turning of AISI D2 cold work tool and AISI 1045 medium carbon steels with uncoated carbide tools ISO grade K15. The aim of this study is to evaluate the influence of feed rate on chip compression ratio (R c ), chip deformation ( ε ), friction angle ( ρ ), shear angle ( φ ), normal stress ( σ ) and shear stress ( τ ) for both work materials. The results indicated that the shear angle decreased and chip deformation increased as the chip compression ratio was elevated without significant differences between both materials. Additionally, higher cutting and thrust forces and normal and shear stresses were observed for the tool steel. Finally, the Lee & Shaffer model gave shear plane angle values closer to the experimental data.


Introduction
Micro-machining is becoming an important manufacturing technology due to the increasing demand for miniaturized products in recent years.This is mainly driven by the needs for: greater reduction in size and weight; higher energy efficiency and higher portability in commercial and non-commercial applications.The value of many products can be substantially increased as their size and weight are reduced.The last decade has shown an ever-increasing interest in higher precision and miniaturization in a wide range of manufacturing activities.Many industrial branches require micro-components, for instance, telecommunication, biomedical and micro-intelligent technology.Micromachining by shearing is capable of producing high dimensional and geometric accuracy, surface finish quality and sub-surface integrity at reasonably low costs.Thus, it should be the first choice amongst various manufacturing processes.Furthermore, conventional machining processes such as turning, milling and grinding have already been well established [1][2][3][4] .On the other hand, as the feed rate and depth of cut are reduced, special attention must be paid to the cutting edge preparation, otherwise the chip will not be generated owing to the side flow effect.
Most of the experimental research concerning micromachining has been conducted on either conventional precision machine tools or prototype machine tools built by researchers.Conventional machine tools used to precision machining have improved considerably with regard to motion accuracy, stiffness and capability.In general, micromachining is performed on precision machine tools with power and dimensions typical of conventional machines, however, the required power and the work size are much smaller when micro-machining [5][6] .
Micro-cutting of steel has recently caught research interest with the advent of miniaturized systems using a variety of materials, especially for biomedical applications.The material and geometry of micro-tools are important factors to be considered.The feature size is limited by the size of the micro-tools and tungsten carbide tools are generally suitable for machining a variety of engineering materials.The size and quality of micro-products depends on the properties of the machine tools used to produce them, including their accuracy and their dynamic performance 6 .
The principal difference between conventional and micro-machining resides in the cutting mechanism.In general, the cutting mechanism in conventional machining is mainly shearing of the material ahead of the tool wedge, resulting in chip formation.In contrast, micro-machining relies on more complicated mechanisms depending on the degree of the size effect 5 .In micro-machining the so called OI: D 10.1590/S1516-14392012005000071 The shear plane angle (φ) is the angle at which the shear stress equals the shear strength of the work material, therefore the shear deformation occurs preferably at this angle.Determination of shear angle has been the subject matter of a number of studies.According to Merchant 9,[11][12][13] , it can be calculated by taking the derivative of the shear stress (Equation 3) with respect to φ and considering its value zero (relative maximum of the function τ), see Equation 6: Alternatively, Lee & Shaffer 14 obtained the shear plane relationship presented in Equation 7 by assuming that the material was an ideal rigid-plastic solid and the shear plane would be located in the direction of maximum shear, the work of separation not being included in this derivation.According to 9,[11][12][13] , the mean friction angle (ρ) can be estimated using the cutting and thrust forces (F c and F t ) and the rake angle (γ) as indicated in Equation 8: The aim of this work is to compare the results from the models proposed by both Merchant 9 and Lee & Shaffer 14 with experimental data when precision radial turning AISI D2 cold work tool steel and AISI 1045 medium carbon steel using grade K15 uncoated carbide inserts without chip breaker at various feed rate values under dry cutting.

Experimental Procedure
Bars of AISI D2 cold work die steel and AISI 1045 medium carbon steel were used as work materials.Table 1 presents the chemical compositions and mechanical properties of these materials.
Radial turning tests were carried out using ISO grade K15 uncoated cemented carbide inserts (Sandvik Coromant geometry N151.2-540-40-3B and grade H13A).The experimental setup is shown in Figure 1.The inserts were mounted on a tool holder coded LF 151.22-2020-40, thus resulting in the following angles: clearance angle α = 0°, cutting edge inclination angle λ = 0° and rake angle γ = 0°.A fresh cutting edge was used for each test, therefore, tool wear was considered negligible throughout the "size effect" is identified as critical in defining process performance.Size effects refers to the phenomenon whereby the reduction of the undeformed chip thickness to levels below the cutting edge radius, or gain size of the workpiece material begins to influence workpiece material deformation mechanisms, chip formation and flow 7 .
Davim et al. 8 compared finite element model (FEM) simulations with experimental and analytical findings concerning precision radial turning of AISI D2 steel using uncoated carbide cutting tools.FEM machining simulation employs a Lagrangian finite element based machining model applied to predict cutting and thrust forces, cutting temperature and plastic strain distribution.The results show that the difference between the experimental and simulated cutting force was approximately 20% and was not drastically affected by the friction coefficient employed in the FEM model.
The model proposed by Merchant 9 has been extensively applied to metal cutting since its advent owing to the fact that it provides quite reliable data with regard to the plastic deformation in the primary shear plane, thus allowing the prediction of the imposed forces and stresses.
The chip compression ratio (R c ), as defined by Merchant [9][10] , is given by: Where t' is the chip thickness and t is the undeformed chip thickness, i.e., t = f for orthogonal cutting.The shear plane angle (φ) can be determined experimentally from the chip compression ratio 9, 11-13 using Equation 2: Where γ is the rake angle.
From the cutting forces and the shear plane angle, the shear and normal stresses along the shear plane can be calculated 9,[11][12][13] using, respectively, Equations 3 and 4: Where F c is the cutting force (N), F t is the thrust force (N) and c is the width of cut (mm).As a result, the chip deformation (ε) can be obtained from R c and γ 11 : linearity lower than 1% and sensitivity of -3,8 pC.N -1 for F c and -7,9 pC.N -1 for F t .Chip thickness (t') measurement was undertaken with a Mitutoyo ® digital micrometer (range of 0-25 mm and resolution of 1 µm).

Results and Discussion
Using the chip thickness value it is possible to calculate the chip compression ratio (R c ) using Equation 1, the shear plane angle (φ) through Equation 2and finally the chip deformation (ε) using Equation 5. Table 2 gives the values of chip compression ratio, shear plane angle and chip deformation as a function of feed rate when precision radial turning AISI 1045 and AISI D2 steels.
It can be noticed in Figure 3 that the value of the experimental shear plane angle (φ) decreases as the chip compression ratio (R c ) increases.The value of chip compression ratio and therefore of the shear plane angle provide an indicative of the amount of plastic deformation at the shear zone, i.e., low φ values (high R c values) mean large amounts of strain in the shear plane.
Figure 4 presents the influence of the chip compression ratio (R c ) on the chip deformation value (ε), where it can be seen a smooth increase in ε as R c is elevated, irrespectively of the work material.The cutting and thrust force values recorded at distinct feed rate values (10, 20, 40 and 80 µm.rev - ) are presented in Figure 5.It can be noticed that when machining AISI D2 steel, the cutting and thrust forces present higher values owing to its superior hardness and tensile strength (see Table 1).The cutting force values increase drastically with feed rate and the thrust force component increases slightly.In addition to that, the forces recorded when cutting the tool steel present less scatter compared with the carbon steel.experimental program.An average of three measurements was taken for making graphics and Table 2 and 3.
Dry radial turning experiments were conducted on a Kingsbury MHP 50 CNC lathe with 18 kW power and maximum spindle speed of 4500 rpm.Constant cutting speed (v c ) of 70 m/min and width of cut (c) of 2.7 mm values were used, while the following feed rates (f) were tested: 10, 20, 40 and 80 µm.rev - .
The tool holder was mounted on a Kistler ® piezoelectric dynamometer model 9121 with a load amplifier connected to a computer which was used for the acquisition of the cutting (F c ) and thrust (F t ) forces, as shown in Figure 2. Kistler Dynoware ® software was used for data acquisition.The equipment, provided with a static and dynamic calibration record, presents a working range from 0 to 600 N to F c and from 0 to 300 N to F t .Moreover, the above mentioned dynamometer possesses a natural frequency of 1kHz,   the rake and friction angles.Table 3 presents the results obtained through both methods and Figure 7 compares the values for the shear plane angle (φ) obtained by the three methods.It can be seen that both materials presented significant difference between experimental and analytical values, possibly due to the low feed rate values used, which provided larger deformation, associated to the fact that both methods do not take work hardening into account.
The values predicted by Lee & Shaffer 14 tend to be closer to the experimental data, nevertheless, differences are to be expected owing to the fact that elastic strain and the influence of temperature are neglected.In addition to that, according to Lee & Shaffer 14 model the shear stress should equal the normal stress on the shear plane, however this is not observed.According to Bil et al. 15 , Lee & Shaffer 14 model, which is relatively simpler than the others, gives good predictions.These authors found simulated similar to with those given by Lee & Shaffer 14 model, especially for a rake angle of 20°.Furthermore, the shear plane angle calculated according to Merchant model considers the shear stress value constant, which may not be accurate.According to Childs et al. 16 , although Merchant 9 and Lee & Shaffer 14 models correctly show that the shear plane angle increases as the rake angle is elevated and the friction angle is reduced, this universal relationship is not supported experimentally.
Shaw 10 regards Lee & Shaffer 14 model as the best starting point due to the fact that it considers the least objectionable assumptions.In spite of that, correction factors encompassing the presence of built up edge, the size of the secondary shear zone, chip curl, tool wear and strain hardening should be incorporated in the model.
Through Equations 3 and 4 it is possible to obtain the normal stress (σπ) and the shear stress (τπ) values.Figures 8  and 9 show, respectively, the evolution of the normal stress (σπ) and the shear stress (τπ) values as feed rate increases.It can be observed that the normal stress (σπ) is always lower than the shear stress (τπ), both stresses tending to reduce as the feed rate is elevated.Moreover, higher normal and shear stress values are obtained during the machining of AISI D2 steel, in spite of the reduction in the difference recorded for both materials as feed rate is elevated.This can be explained by the higher experimental shear plane Figure 6 presents the evolution of the average cutting and thrust forces as a function of feed rate when turning both materials, where it can be observed that the cutting and thrust forces increases drastically with feed rate.Nevertheless, the difference between the forces recorded when turning die steel and carbon steel tend to decrease as feed rate is elevated.
From Equation 6, concerned with Merchant model, it is possible to obtain the value of the shear plane angle (φ M ) from the friction angle value (ρ) calculated from Equation 8.This procedure allows a comparison between the experimental values and those derived from both Merchant 9 and Lee & Shaffer 14 models, both analytical models depending on

Conclusions
After precision radial turning of AISI D2 cold work tool steel and AISI 1045 medium carbon steel the following conclusions can be drawn: • Correlations between the chip compression ratio and shear plane angle or chip deformation were obtained for both materials.The shear angle decreased with angle values observed for the tool steel at feed rates of 40 and 80 µm.rev - .Summarizing the above considerations, it can be concluded that each observed cutting model reflects a particular aspect of metal cutting practice, in reality, the cutting conditions may be created where one or another model is valid, but no one model covers the whole variation of cutting conditions.• Higher shear stress values were obtained in comparison with the normal stress.Both stresses values were reduced as feed rate was elevated.

Figure 1 .
Figure 1.Workpiece and cutting tool used in the experimental work.

Figure 3 .
Figure 3. Experimental shear plane angle versus chip compression ratio.

Figure 6 .
Figure 6.Effect of feed rate on average cutting and thrust forces when machining of AISI 1045 and AISI D2 steels at v c = 70 m/min with K15 uncoated cemented carbide tool.

Figure
Figure Effect of feed rate on normal stress.Figure9.Effect of feed rate on shear stress.

Figure 9 .
Figure Effect of feed rate on normal stress.Figure9.Effect of feed rate on shear stress.

Table 1 .
Chemical composition in % weight and mechanical properties of work materials.

Table 2 .
Values of chip compression ratio (R c ), experimental shear plane angle (φ) and chip deformation (ε) as functions of feed rate when precision turning of AISI 1045 and AISI D2 steels.

Table 3 .
Values of the friction angle (ρ), experimental shear plane angle (φ) and Merchant(φ M ) and Lee & Shaffer (φ LS ) shear plane angle as functions of feed rate.