Drilling Process in γ-TiAl Intermetallic Alloys

Abstract

Gamma titanium aluminides (γ-TiAl) present an excellent behavior under high temperature conditions, being a feasible alternative to nickel-based superalloy components in the aeroengine sector. However, considered as a difficult to cut material, process cutting parameters require special study to guarantee component quality. In this work, a developed drilling mechanistic model is a useful tool in order to predict drilling force (F_z) and torque (T_c) for optimal drilling conditions. The model is a helping tool to select operational parameters for the material to cut by providing the programmer predicted drilling forces (F_z) and torque (T_c) values. This will allow the avoidance of operational parameters that will cause excessively high force and torque values that could damage quality. The model is validated for three types of Gamma-TiAl alloys. Integral hard metal end-drilling tools and different cutting parameters (feeds and cutting speeds) are tested for three different sized holes for each alloy.

1. Introduction

Aeronautics is an emerging sector; aircraft manufacturing predictions estimate doubling of the current fleet by the year 2033, in order to satisfy passenger’s increment demand that grows at a rate of 4.2% per year [1]. Components manufacturing for the aeronautic sector is a high value added process, and, concretely, motor components require special attention because they represent one of the most expensive (20%) components [2]. The aviation industry will try to satisfy manufacturing demand according to regulation requirements regarding efficiency, noise, fuel consumption and contamination. Therefore, new materials and manufacturing processes are under development by aeronautic sector manufacturers. In this sense, γ-TiAl alloys are a feasible replacement for nickel-based alloys frequently used for compressor blades and stator in gas turbine aeroengines [3,4,5]. Moreover, titanium alloys are also interesting for bio-medical engineering, automobile sector and chemical industries [6].

Gamma titanium aluminide intermetallics present excellent strength-weight ratio, and corrosion resistance at high temperature [7,8]. However, it is considered a difficult to cut material [9,10] due to its poor tensile and low room temperature ductility (<2%). Besides, high heat values are generated during γ-TiAl machining due to low thermal conductivity o the material. Consequently, tool and workpiece wear is accelerated [11], tool life is reduced [12] and workpiece integrity is affected [13]. Moreover, γ-TiAl reacts chemically with many materials causing material adhesion.

Several studies have considered γ-TiAl a difficult to cut material regarding turning [14,15], grinding [16], high speed milling [17,18,19], drilling and micro-drilling [20].

In this sense, high machining conditions can cause irreversible consequences such as surface cracking, hardened layers and tensile residual stresses [21]. Optimal machining strategies and parameters are studied for electrochemical machining [22], turning [23,24], and milling [25] related to cutting temperature technique evaluation, and, appropriate machining conditions in order to reduce tool wear and increase tool life. Milling studies have also investigated the effects of operating parameters and conditions on tool life and surface integrity when milling γ-TiAl alloys [26,27,28].

In relation to lubrication techniques, some studies [29] focus on cryogenic lubrication (liquid nitrogen) obtaining cutting feed value increments while tool life is maintained.

Machining processes modelling is also a hot topic for difficult to cut materials. In this sense, two-dimensional models [30] were developed for cutting parameters such as cutting speed and feed influence determination. Numerical and experimental analyses of residual stresses generated in the machining of Ti6A14V titanium alloy are developed [31]. Empirical models are also used for thrust and torque values prediction in composites. Other techniques such as response surface methodology (RSM) and finite element analysis (FEA) are implemented for milling [32] and drilling [33] process parameter analysis. In addition, finite element models are also developed for performance characteristics such as hole quality prediction [34]. Other techniques are focused on the side of monitoring. For instance, power consumption during drilling is a key magnitude in predictive/preventive techniques [35,36].

Considering γ-TiAl promising application possibilities, drilling machinability studies are a focus of interest due to presented machinability problems, drilling being one of the most frequent processes for component assembly. In this work, the developed drilling mechanistic model is a useful tool in order to predict drilling force (F_z) and torque (T_c) for optimal drilling conditions determination. The model is validated for three types of Gamma-TiAl alloys. Integral hard metal end-drilling tools and different cutting parameters (feeds and cutting speeds) are tested for three different sized holes for each alloy.

2. Experimental Procedure

2.1. Material

Four different titanium alloys are tested in performed drilling tests: Ti-6Al-4V and three different γ-TiAl alloys (TNB, extruded MoCuSi and ingot MoCuSi).

Table 1. Mechanical properties comparison between TiAl alloys.

Property	TNB	Ti–6Al–4V (Annealed)	MoCuSi Extruded	MoCuSi Ingot
Density (g/cm3)	3.86	4.49	3.74	3.88
Specific modulus (GPa/(mg·m−3))	43	24	43	37
Tensile strength (MPa)	683	1087	607	689
Specific strength (MPa/(g·cm−3))	192	947	198	180
Yield strength (MPa)	589	942	589	570
Ductility (%)	1.9	7.8	1.7	2.4
Fracture toughness (MPa·m1/2)	23	52	23	20
Thermal conductivity (W/(m·K))	24	8.6	24	19
Maximum operating temperature (°C)	900	615	900	865

shows the tested alloys’ mechanical properties.

γ-TiAl alloys present higher aluminum percentage in comparison to other titanium alloys such as Ti-6Al-4V, 43–48% in γ-TiAl and 6% in Ti-6Al-4V, improving thermal conductivity in γ-TiAl. On the other hand, ductile transition temperature occurring between 600 and 800 °C, depending on the microstructure and grain size alloys, is increased for alloys with higher titanium percentage [12]. The intermetallic TiAl provides low density [37] as well as high mechanical strength under high temperatures and corrosive environments. The intermetallic γ-TiAl superalloys offer excellent mechanical properties [38], with low density (4 gr/cm³), high resistance at high temperatures, low electrical and thermal conductivity, oxidation resistance, ultimate strength of 1000 MPa and Young’ s modulus of 160 GPa.

MoCuSi alloy [Ti-(43–46) Al-(1–2) Mo-(0.2) Si-Cu] is used at low temperatures with high resistance below 650 °C, and, TNB alloy [Ti-(44–45) Al-(5–10) Nb-(0.2–0.4) C] resists very high temperatures maintaining high resistance and oxidation values. Regarding MoCuSi alloys, the material is presented in both, extruded and ingot structure. Extruded alloys present an oriented structure oriented in the extrusion direction whereas melted alloys present a structure without any preferable orientation, typical of no extruded or laminated materials. The ingot structure is directly obtained from the VAR (Vacuum Arc Remelting) process. For extruded structures, material is extruded at 1200 °C and smaller sized grains are obtained with superior creep strain, yield strength and KIC.

2.2. Equipment

Machining tests were performed in a vertical CNC milling machine, Kondia^® model B640 (Kondia, Elgoibar, Spain), with maximum rotational speed of 10,000 rpm and 25 kW. During the tests, process-cutting conditions are measured and recorded. For the axial/thrust (F_z) and radial (F_x, F_y) cutting forces, and, Z axis (T_c) torque measurements, a dynamometric Kistler^® equipment 9257B (Kistler, Winterthur, Switzerland) was used (Figure 1).

2.3. Machining Conditions

Drilling tests were carried out for the described four titanium alloys (Table 1). As can be seen in

Table 2. Machining conditions for the 8.5 mm hole.

Material	vc [m/min]	n [rev/min]	f [mm/rev]	f [mm/rev]
Ti-6Al-4V	50	1874	0.05	0.1
TNB	15	1874	0.05	0.1
MoCuSi Extruded	15	562	0.05	0.1
MoCuSi Ingot	15	562	0.05	0.1

, for each material, tested feed values are 0.05 and 0.1 mm/rev for calibration tests and 0.06 and 0.08 mm/rev for validation tests, and, D = 3, 4, 5, 6, 7 mm (pilot holes) and 8.5 mm holes (final holes) were drilled in each case (Figure 2). The drilled depth is 20 mm. D = 3, 4, 5, 6, 7 mm (pilot holes) and 8.5 mm holes (final holes) are used for calibration, and, D = 4–6 mm (pilot holes) and 8.5 mm holes (final holes) are used for the validation tests.

The selected tool is a solid carbide drill (Mitsubishi^®, Tokyo, Japan, MPS0850S-DIN-C, Figure 3). During the machining operations, cutting forces, torque and power consumption were recorded.

One of the critical aspects when drilling γ-TiAl is chip evacuation and heat dissipation. Internal lubrication is directly applied on the cutting edge, due to the poor thermal conductivity of these alloys. Specially designed for low machinability materials, Rhenus^® FU W (

Table 3. Properties of Rhenus^® FU 70 W coolant.

Concentrated		Emulsion
Viscosity 20 °C (mm2/s)	Content of mineral oil %	pH Value 5% concentration	Protection against corrosion (DIN 51360/1)
Approx. 150	Approx. 33	Approx. 9,0	Note 0 al 2%

, Rhenus, Mönchengladbach, Germany) coolant was used. Internal coolant pressure is set to 8.5 bar.

3. Cutting Forces Prediction Mechanistic Model

Predictive cutting forces mechanistic models help programmers with cutting parameter selection. Especially when drilling low machinability titanium alloys, it is interesting to simulate different machining conditions in order to decide whether the estimated cutting forces values lead to an optimum machining process.

This section explains the modelling of cutting forces and torque in drilling. Since the cutting speed varies along the drill’s lips, the way the cutting force coefficients are introduced inside the model is a crucial issue. There have been a number of attempts based on orthogonal-oblique transformation [39] and mechanistic models [40].

The cutting edge is divided into discrete elements in the drill axis (j = 1 to n elements) and the global cutting force and torque are obtained by summing the elemental contributions along each lip (i = 1 to Z). As it can be seen in Figure 4, while F_x and F_y are coupled due to tool rotation leading to the radial Fr and tangential Ft cutting force components, F_z is directly obtained from the axial component Fa. Here, we will focus on the thrust force (Equation (1)) in Z direction and torque (Equation (2)), which are critical parameters when characterizing tool life. These magnitudes are calculated as:

$$F_z\left(t\right)=\sum _{i=1}^Z\sum _{j=1}^n{K}_{c,z}\left(h,r\right)\cdot \Delta z\cdot h$$

(1)

$$T_c\left(t\right)=\sum _{i=1}^Z\sum _{j=1}^n{K}_{t,z}\left(h,r\right)\cdot \Delta z\cdot h\cdot r$$

(2)

where K_z and K_T are the corresponding thrust force and torque coefficients, Δz is the axial width of a differential element, h the chip thickness (here, h = 0.5f·sin70°) and r the tool radius. As usual, the thrust cutting force and torque coefficients need to be calibrated. Here, 4 different titanium alloys were tested: (1) Ti-6Al-4V, taken as reference; (2) TNB and MoCuSi types, (3) extruded and (4) ingot types. Under this approach, the cutting force coefficients were assumed a function of the feedrate (or h) and radial distance of the cutting point to drill axis as quadratic functions. First, a₀-a₅ and b₀-b₅ coefficients in Equations (3) and (4) are identified from a linear regression for the four types of materials from a set of experiments.

$$K_z\left(h,r\right)=a_0+a_1\cdot h+a_2\cdot r+a_3\cdot hr+a_4\cdot r^2+a_5\cdot h^2$$

(3)

$$K_T\left(h,r\right)=b_0+b_1\cdot h+b_2\cdot r+b_3\cdot hr+b_4\cdot r^2+b_5\cdot h^2$$

(4)

4. Results

The mechanistic model is valid for v_c = 50 m/min (Ti-6Al-4V), and v_c = 15 m/min (TNB, and extruded/ingot types), the cutting speed at the tool diameter D. To identify the cutting coefficients, 10 tests were done. After a pilot hole, the hole was finished at D = 8.5 mm. Five different pilot hole diameters (D₀ = 3, 4, 5, 6, 7 mm) and two feed rates (f = 0.05–0.1 mm) were programmed.

The corresponding functions for the cutting coefficients are summarized in Table 8 with the obtained coefficients of polynomial functions K_z and K_T in Equations (3) and (4).

4.1. Results for Ti-6Al-4V Alloy

As can be seen, both experimental and the predicted thrust force and torque values are higher for higher feed rate values (Figure 5).

Table 4. Experimental results for F_z [N] and T_c [Nm] in Ti-6Al-4V alloy.

D0 [mm]	Fz [N]		Tc [Nm]
	f [mm/rev]		f [mm/rev]
	0.05	0.1	0.05	0.1
3	591	723	3.1	3.9
4	460	565	2.4	3.7
5	319	440	2.1	3.4
6	242	332	1.9	3.2
7	169	225	1.8	3.1

shows the experimental data for both variables during the calibration of the cutting coefficients. While the curve F_z reflects almost a linear tendency, the torque is approximated as a curve with an inflexion (third order). At the same time, the higher the dispersion, the lower is the difference between the pilot and final hole diameters.

4.2. Results for TNB Alloy

Thrust force values (Figure 6a) show higher values for higher feed rate values but are not doubled when doubling the feed rate. However, the cutting tool behaved correctly despite that the cutting force increased ×1.33 and cutting torque increased ×1.5–2, with respect to Ti4Al6V. When feed rates values are multiplied ×2, torque values are multiplied ×1.3 approximately.

Table 5. Experimental results for F_z [N] and T_c [Nm] in TNB alloy.

D0 [mm]	Fz [N]		Tc [Nm]
	f [mm/rev]		f [mm/rev]
	0.05	0.1	0.05	0.1
3	802	954	5.8	7.0
4	631	765	5.3	6.7
5	476	575	4.3	6.1
6	343	421	4.0	6.0
7	240	259	3.5	5.7

shows again the experimental data necessary to obtain the polynomials of the cutting coefficients. A higher dispersion is seen for the cutting torque T_c as the pilot hole diameter approaches the final hole diameter (Figure 6b).

4.3. Results for Ingot MoCuSi Alloy

Ingot MoCuSi alloys are harder Ti-6Al-4V alloys and TNB alloys.

Table 6. Experimental results for F_z [N] and T_c [Nm] in ingot MoCuSi alloy.

D0 [mm]	Fz [N]		Tc [Nm]
	f [mm/rev]		f [mm/rev]
	0.05	0.1	0.05	0.1
3	852	906	6.0	8.7
4	702	775	5.5	8.3
5	525	600	4.8	7.5
6	419	466	4.6	7.3
7	275	290	4.0	7.0

shows the main values. This statement was verified on sight of Figure 7. The axial force F_z and cutting torque T_c are higher regarding previous alloys. Focusing on cutting torque (Figure 7b), when the feed rate value is multiplied ×2, torque values are multiplied ×1.1 approximately.

4.4. Results for Extruded MoCuSi Alloy

MoCuSi extruded alloys present the highest hardness values in comparison to the latter ones. While the results for the cutting torque T_c are quite similar to the ingot MoCuSi alloy (both results are almost identical), the thrust force is more dramatic for the extruded MoCuSi alloy. Regarding cutting torque (Figure 8b), when the feed rate value is multiplied by two, torque values are multiplied ×1.2 approximately (see also results in

Table 7. Experimental results for F_z [N] and T_c [Nm] in extruded MoCuSi alloy.

D0 [mm]	Fz [N]		Tc [Nm]
	f [mm/rev]		f [mm/rev]
	0.05	0.1	0.05	0.1
3	925	1050	6.5	9.3
4	751	860	6.1	8.6
5	550	621	5.5	8.0
6	427	475	4.7	7.7
7	280	292	4.0	7.5

).

Using the above experimental results, the coefficients in Equations (3) and (4) are obtained and then the corresponding polynomial functions are built (

Table 8. Obtained coefficients for the polynomials in Equations (3) and (4).

Materials	Kz(h,r)						KT(h,r)
	a0	a1	a2	a3	a4	a5	b0	b1	b2	b3	b4	b5
Ti-6Al-4V	13,159	−93,861	−3,225	−10,986	977.11	−7,056.0	39.646	−68.280	−21.597	−41.882	5.253	−5.171
TNB	19,860	−217,630	−3,830	17,235	855.42	−16,347.1	77.853	−283.109	−36.204	−61.168	8.334	−21.331
MoCuSi (ingot)	23,445	−270,543	−4,028	20,962	688.07	−20,320	90.152	−274.538	−45.120	−17.808	9.663	−20.703
MoCuSi (extruded)	24,016	−282,289	−4,270	24,114	860.73	−21,202	84.201	−120.895	−45.120	−17.808	9.663	−20.703

).

For model validation, different combinations of parameters were tested within the window parameters. New pilot hole drills and final drill of D = 8.5 mm were used for these tests. Eight different tests were programmed to put the model to work.

Table 9. Cutting conditions for the validation tests.

Materials	Vc [m/min]	D0 [m/min]	f [mm/rev]	# Test
Ti-6Al-4V	50	4	0.06	1
		6	0.08	2
TNB	15	4	0.06	3
		6	0.08	4
MoCuSi (ingot)	15	4	0.06	5
		6	0.08	6
MoCuSi (extruded)	15	4	0.06	7
		6	0.08	8

presents the conditions for these validation tests.

Figure 9 shows the results from the simulated values using the model described and the experimentally measured values. The model presents a good correlation with the real thrust forces and cutting torques. For the cutting forces, the maximum relative error between the predicted and measured values was 8% while for the cutting torque the worst case was found to be 13%. The model behaves well in the targeted interval of feed rates, with higher deviations, the higher is the programmed feed. On the other hand, the mechanistic model seems less sensitive to the range of tested pilot hole diameters and final hole diameters. A higher dispersion is seen also in the torque values with respect to thrust forces that can be predicted with very good agreement.

5. Conclusions

This work presents the machinability results for four different titanium alloys. Currently there are few data about machining of γ-TiAl. The obtained results reflect that:

• These alloys present a much smaller machinability than conventional titanium alloys.
• The presented mechanistic stationary model is capable of simulating the thrust force and cutting torque in the drilling process. The influence of vibratory effects, lateral vibrations or runout was not considered. After model calibration, validation tests were done, showing a good agreement.
• Experimental drilling tests done to evaluate the machinability of these difficult-to-cut materials (the high cost of the tested materials (approx. 400 €/kg) limited the number of tests and a stronger experimental design) show that the obtained cutting coefficients present a quasi-linear dependence on the pilot hole D₀ for the axial force F_z, while a cubic is more suitable in the case of T_c.
• Machining problems during drilling tests confirm that these are very brittle materials, so operational parameter determination is essential for chipping and cracking avoidance of components during machining processes [41,42].
• Experiments demonstrated large differences between the more conventional Ti6Al4V alloy and the three γ-TiAl intermetallic alloys. As the mechanical properties of extruded/ingot alloys are higher than those of the TNB alloy, this trend is inversely true for the machinability grade. Tests proved that MoCuSi alloys are the toughest materials.
• Despite the good results during the validation, a statistical approach would be desirable to test any differences in material series, machine tools, as well as to build more complete models. Wear studies including process damping effects can be subjects for future research works.