Experimental cutting model of metal matrix composites (MMCs)
Introduction
Recently, the use of metal matrix composites (MMCs) has increased in various areas of science and technology due to their special mechanical and physical properties. MMCs are characterized by having a combination of light weight, very high strength and a high stiffness. Therefore, MMCs tend to replace conventional materials in various fields of application such as aeronautical, aerospace, automotive, mechanical engineering, as well as in other industries because of its own properties. As result of these properties and potential applications, a great necessity exits to understand the questions associated with the production and machining of such materials. Machining MMCs is a rather complex task owing to its heterogeneity and to the fact that reinforcements are extremely abrasive [1], [2], [3], [4], [5], [6].
The machinability of MMCs reinforced with particles of SiC (20%) using PCD tools was studied having in consideration the evolution of the cutting time of the tool wear, the cutting forces and the surface roughness workpieces [1], [2], [3]. Later, was evaluated the performance of the CVD diamond tools in machining of these composites [4]. A machinability study of MMCs reinforced with particles of SiC (5%) using cemented carbide tools were studied having in consideration the tool wear and the surface roughness workpieces [5]. The optimization of cutting parameters in this type of composites was makes using FEM models [6].
The orthogonal model, presented by Merchant (Fig. 1) can be used to approximate turning, and certain other single-point machining operations, as long as the feed in these operations is small relative to depth of cut [7], [8].
The undeformed chip thickness (e) can be calculated from the cutting edge angle (χ) and the feed rate (f) with the following equation:
The chip compression ratio, as defined by Merchant, is [7], [8]:being e′ the chip thickness after cutting.
The shear plane angle (ϕ) can be calculated from the chip compression ratio by the following equation [7], [9], [10]:being γ the rake angle and Rc obtained by Eq. (2).
From the cutting forces and the shear plane angle, the shear and normal stresses (N/mm2) along shear plane can be calculated [7], [9], [10]:being Fc the cutting force (N), Ft the thrust force (N), c the width of cut (mm) and e the undeformed chip thickness (mm).
The chip deformation (ɛ) can be obtained from the values of Rc and γ [9]:
The shear plane angle (ϕ) is the angle at which the shear stress equals the shear strength of the work material, and so the shear deformation occurs preferably at this angle. The shear plane angle can be determined by taking the derivative of the shear stress (Eq. (4)) with respect to ϕ and setting the derivative to zero (relative maximum of the function τ), according to Merchant [7], [9], [10]:
The mean friction angle (ρ) can be estimated from the cutting forces (Fc and Ft) and the rake angle (γ) by the following equation [7], [9], [10]:
The objective of this experimental work is to compare the results of the Merchant equation with the experimental cutting model during the turning MMCs with PCD cutting tools.
Section snippets
Materials and experimental details
Aluminium alloy reinforced with 20% of SiC particulates (A356/20/SiCp-T6) has been tested. A typical microstructure of this material is shown in Fig. 2. The chemical composition of the A356 aluminium matrix is aluminium with 7.0% Si and 0.4% Mg. The average dimension of the SiC particles is about 20 μm.
The experiments were carried out using MMCs appropriate workpieces with a diameter of 60 mm and a length of 200 mm, using a PCD tool (TCMW 16T3 04 FP CD10). A type STGCL 2020 K16 tool holder was
Results and discussion
Taking into account the chip thickness value measured after the cutting operation on the metal matrix composite, it was possible to obtain the chip compression ratio (Rc) (Eq. (2)), the shear plane angle (ϕ) (Eq. (3)) and the chip deformation (ɛ) (Eq. (6)), as presented in Table 2.
In Fig. 3 it is possible to observe that the value of the shear plane angle (ϕ) decreases with the increase of the chip compression ratio (Rc). By linear regression for the shear plane angle (ϕ) as a function of the
Conclusions
Correlations between the chip compression ratio and shear plane angle or chip deformation have been obtained in MMCs turning. The shear angle decreased with the chip compression ratio. On the contrary the chip deformation increased with chip compression ratio.
The Merchant model gives, in general, an overestimation of the shear plane angle value in cutting of aluminium matrix composites. The exceptions are the cases of the simultaneous utilization of the more severe cutting parameters,
References (10)
Diamond tool performance in machining metal-matrix composites
J. Mater. Process. Technol., Elsevier Science
(2002)- et al.
Study of tool wear and surface roughness in machining of homogenized SiC-p reinforced aluminium metal matrix composite
J. Mater. Process. Technol., Elsevier Science
(2005) - et al.
Machining of aluminium/silicon carbide particulate metal matrix composites: part IV. Residual stress in machined workpiece
J. Mater. Process. Technol., Elsevier Science
(2004) - et al.
Relationship between cutting force and PCD cutting tool in machining silicon carbide reinforced aluminium
J. Mater. Process. Technol., Elsevier Sci.
(2000) Turning particulate metal matrix composites. Experimental study of the evolution the cutting forces, tool wear and workpiece surface roughness with the cutting time
J. Eng. Manuf., Proc. Instn. Mech. Eng. Part B
(2001)
Cited by (45)
Establishment of scratching force model for micro-removal of SiCp/Al composites by ultrasonic vibration
2022, Journal of Materials Processing TechnologyAluminium 6082-boron carbide composite materials preparation and investigate mechanical-electrical properties with CNC turning
2020, Materials Today: ProceedingsCitation Excerpt :These boron carbide materials are used in aerospace, defense, automobile and other industrial fields [4]. The composite materials have high particular properties, high warm resistance, good damping limits and high particular firmness [5,6]. The most commonly used composite materials are aluminium alloy reinforced with hard ceramic particles such as silicon carbide, fly ash, alumina and soft particles (graphite).
Experimental investigation on machinability of in situ formed TiB<inf>2</inf> particles reinforced Al MMCs
2016, Journal of Manufacturing ProcessesCitation Excerpt :Chip breaking criteria based on the mechanical properties of SiC/Al MMCs was developed. Davim et al. [23] studied the relationship between chip formation and chip compression ratio. It was found that the chip deformation increased with chip compression ratio which cutting SiC/Al MMCs.
A novel in-situ polymer derived nano ceramic MMC by friction stir processing
2015, Materials and DesignRigorous treatment of dry cutting of FRP - Interface consumption concept: A review
2014, International Journal of Mechanical Sciences