Ijraset Journal For Research in Applied Science and Engineering Technology
Authors: Madduleti. M, P. Venkata Ramaiah
DOI Link: https://doi.org/10.22214/ijraset.2022.41052
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The present research looks upon metal matrix composites, namely Aluminum Metal Matrix Composites (AMMCs), as well as modelling and simulation of the orthogonal metal cutting process. A fundamental component of AMMCs is aluminum alloy, which creates a percolating network and acts as the matrix stage. Multiwall nano carbon tubes are another non-metallic component used as reinforcement in the aluminum alloy matrix (CNT). Some of the primary advantages of AMMNCs over unreinforced products are higher strength, high stiffness, decreased weight, improved heat properties, controlled thermal development coefficient, and thermal/heat monitoring. The SHPB test at high stain rates is commonly used to establish the Johnson cook constants for AMMNC work piece material.The Johnson-Cook constitutive model, which estimates flow stress as the product of strain, strain rate, and temperature effects, is used to determine work hardening, strain-rate hardening, and thermal softening. FEM simulations were carried out using 2D-Deform software. When the results of the 2D-Deform software-derived flow stressandtemperature are compared to the findings of the analytical model, the results are satisfactory.
I. INTRODUCTION
The finite element technique is a strong numerical tool for finding solutions to difficult problems because it discretizes the domain into finite elements. The nodes in each element are subjected to boundary conditions and loads. The global stiffness matrix is generated by determining the stiffness matrix for each element in the domain using mathematical methods. The solutions are calculated using the global stiffness matrix and the applied load data. Several scholars have developed finite element codes to solve massive problems, and businesses all around the globe are recognising the significance of such codes in dealing with numerical challenges. FE codes like as Deform, Abacus, Advant Edge, and Third Wave are used to model manufacturing processes (Halil et al 2004). "Deform" is a phrase that is commonly used.
Erol Zeren, Turulzel [1] Cutting processes can be simulated using finite element analysis techniques, which have a number of benefits, including tool force prediction, stress and temperature distribution, tool wear and residual stresses on machined surfaces estimation, and cutting tool geometry and cutting conditions optimization. Under different cutting regimes, the work material flow stress and friction characteristics are not always available. To characterise work material flow stress and friction at primary and secondary deformation zones around the cutting edge, this study uses an Oxley-developed metal cutting model and orthogonal cutting experiments.
Hashem F El-Labban et al. [2] Squeeze casting was used to explore the metallurgical and mechanical characteristics of Al/Al2O3/Ni MMC. They discovered that increasing the Ni content to 10% boosted the composite substance's (UTS), and that combining 2 wt.% nano-Al2O3 with 5 wt.% Ni provided the highest achievable UTS. With the addition of Al2O3 bits and Ni to the base metal, ductility was improved while costs were kept low.
Umbrello, D. [3] D. Umbrello [3] Due to a number of inherent features and their strong reactivity with cutting tools with restricted heat conductivity, titanium alloys are known for being difficult to process, particularly at high cutting speeds. A finite element analysis (FEA) of TiAl6V4 machining for both conventional and high-speed cutting regimes is presented in this paper. Cutting force, chip form, and segmentation are all taken into account when machining these metals since they have such a big impact on machinability and tool wear.
Fang Shao, Zhanqiang Liu, Yi Wan & Zhenyu Shi et al. [4Titanium alloys are characterised as difficult-to-machine materials, especially at higher cutting speeds, due to several intrinsic properties such as limited heat conductivity and significant reactivity with cutting tool materials with low thermal conductivity.
This paper describes a machining finite element analysis (FEA) for Ti-6Al-4V. For both the workpiece and the tool material, the thermodynamical constitutive equation is applied in FEA. It is possible to forecast the temperature of the cutting blade and the depth of tool wear. Differences in cutting temperature and tool wear depth between expected and experimental cutting temperatures and tool wear depth are shown and discussed.
Lee and Lin [5] used regression analysis to identify the parameters for the JC model for Ti6Al4V material from SHPB data. Gray et al (1994) used a computer program based on the optimization routine to fit experimental data to identify material parameters of the JC model..
According to the literature, SHPB data is the most often utilised approach for identifying and optimising flow stress model parameters. The nature of the tests determines flow stress, which is sensitive to material model parameters. The flow stress data for machining must precisely map the deforming material in machining settings, which necessitates either identifying flow stress as a function of the machining process itself or using FEM to modify current parameters to match the deformation processes. Although numerous ways have been utilised to fine tune and improve material properties, most of the models are time intensive and need advanced mathematical abilities.
A. Research Gaps
B. Objectives
II. MATERIAL SELECTION AND METHODS
A. Material
In this study, the Al/ MWCNT composite is used as the workpiece material to investigate its machinability. The workpieces employed in this experiment were diameter of 36 mm and length of 200 mm. Physical and mechanical features of multi-walled carbon nanotube reinforcement, chemical composition of aluminum 7075 alloys are shown in Tables 1 and 2.
Table 1. Chemical composition (wt. %) of Al
Aluminum 7075 |
Zn |
Mg |
Cr |
Ti |
Mn |
Si |
Fe |
Ti |
others |
Al |
Wt.% of composition |
5.64 |
2.2 |
0.2 |
0.045 |
0.04 |
0.054 |
0.21 |
0.043 |
0.027 |
Reminder |
Table 2. Properties of multi-walled carbon nanotube
Reinforcement Material |
Young’s modulus (GPa) |
Thermal expansion (10-6/K) |
Thermal conductivity (W/m K) |
Density (g/cc) |
Melting Point temp(0C) |
MWCNT |
450 |
6.0 |
3000 |
1.9 |
2800 |
B. Fabrication Of Metal Matrix Nanocomposites
The most recent fabrication procedures for MMNCs have been developed in the last few years. The development of composite component processing leads to a cost-effective method. Despite the fact that MMNCs may be manufactured using a variety of ways. All of these approaches are dependent on the reinforcement and matrix materials chosen.
III. METALCUTTING
Metal cutting is a common occurrence in the manufacturing business, as material processing accounts for the majority of a product's cost. In the recent century, there has been a revolution in the processes and techniques used to machine a wide range of materials. Material behaviour at the microscopic and macroscopic levels are important determinants in machining ease. Because materials' metallurgical properties vary, a detailed examination of their machining characteristics is required to optimise cutting conditions, tools, and production processes. Analytically, experimentally, and numerically, machining characteristics can be determined. Analytical and experimental approaches have mostly been used to determine cutting conditions and material machinability.Due of the increased expense and time involved in these trials, the finite element (FE) approach was developed, which has since transformed the manufacturing sector. It has aided in the understanding of the machining behaviour of a variety of materials as well as the micro-level understanding of the complicated metal cutting process.
Experimental and analytical models are good at predicting cutting forces and chip shape at the global level, but they can't assess or forecast local phenomena like stress, strain, strain rate, and temperature distribution in the cutting process. To examine the machining process in depth and propose answers to problems related to design optimization and failure analysis, FE tools are necessary. There has been a surge in its use in machining simulations in the recent decade, but it has been fraught with challenges. Despite the apparent benefits of the FE tool, there remain challenges in critical areas of machining process modelling.Selecting the appropriate material flow stress model to represent the machining deformation behaviour of the material being machined, modelling the correct friction and fracture conditions and criteria as applicable to machining, and applying the appropriate chip separation criterion for the chip formation process are the key aspects. The goal of this research is to improve the accuracy of FE predictions by optimising the flow stress data input.
A. Turning Experiment
Turning experiments were conducted on AMMNC cylindrical work piece having a diameter of 36 mm according to Taguchi orthogonal array L16. The cutting conditions employed for turning of AMMNC material are cutting speed, feed and depth of cut at four different levels.
The responses cutting force, thrust force are measured using lathe tool dynamometer and temperature is measured with temperature gun. Orthogonal cutting test output values are recorded for different speeds, feeds and depth of cuts as in the Table 3.
Table: 3 orthogonal cutting test values
S.NO |
Speed (rpm) |
Depth of cut (mm) |
Feed (mm) |
Cutting force (N) |
Thrust force. (N) |
Temperature (OC) |
1 |
280 |
0.2 |
0.2 |
39.24 |
9.81 |
36.8 |
2 |
280 |
0.4 |
25 |
88.29 |
19.62 |
37.2 |
3 |
280 |
0.6 |
0.32 |
137.34 |
29.43 |
39.2 |
4 |
280 |
0.8 |
0.36 |
176.58 |
39.24 |
39.6 |
5 |
450 |
0.2 |
0.2 |
39.24 |
9.81 |
36.8 |
6 |
450 |
0.4 |
25 |
68.67 |
9.81 |
38.8 |
7 |
450 |
0.6 |
0.32 |
78.48 |
19.62 |
37 |
8 |
450 |
0.8 |
0.36 |
137.34 |
19.62 |
36.5 |
9 |
710 |
0.2 |
0.2 |
49.05 |
9.81 |
36.8 |
10 |
710 |
0.4 |
25 |
78.48 |
9.81 |
37.4 |
11 |
710 |
0.6 |
0.32 |
137.34 |
19.62 |
39 |
12 |
710 |
0.8 |
0.36 |
186.39 |
39.24 |
39.8 |
13 |
1120 |
0.2 |
0.2 |
39.24 |
9.81 |
36.7 |
14 |
1120 |
0.4 |
25 |
88.29 |
19.62 |
36.8 |
15 |
1120 |
0.6 |
0.32 |
127.53 |
19.62 |
37 |
16 |
1120 |
0.8 |
0.36 |
166.77 |
29.43 |
38.3 |
IV. JOHNSON COOK MODEL
The Johnson-Cook constitutive model Eq. (1), which produces the flow stress as the product of strain, strain rate, and temperature, results in work hardening, strain-rate hardening, and thermal softening.
σ = [A+Bεn ] [1+Cln(?/ε0)] {1? [(T _ T0)/(Tm –T0)]m} (1)
In the equation above, A represents the material's initial yield strength at room temperature. To standardise the similar plastic strain rate, a reference strain rate of 0 is employed. Tm is the melting temperature of the material, and T0 is ambient temperature. Parameter n considers the strain hardening effect, parameter m considers the thermal softening impact, and parameter C considers strain rate sensitivity.
A. Split Hopkinson Pressure Bar Test
Typically, the SHPB test (Figure.2) is used to estimate the Johnson cook constant for AMMNC work piece material at high stain rates. Between the event and transmission bars, the work sample is put. Gas pressure propels the incident bar towards the transmission bar. The compression wave propagates through the sample towards the transmission bar as a result of the effect of the incidence bar on the sample, and signals are transferred to the amplifier, where the JC constants are derived using these signals from the PC. The numbers are listed in a table.
V. SIMULATION IN DEFORM
To perform a simulation, a database containing the process data and simulation controls is prepared. The database is created using the above preprocessor inputs. The control, material, object and inter-object options of the preprocessor allow for interactive input of the simulation parameters. The specified database is executed as simulation steps are generated. The output is written back into the database file. The basic equation of equilibrium, constitutive relationship and boundary conditions are converted to non-linear algebraic equations. All the input and output data are stored in binary form and are accessed through the post processor. The results of the simulation are displayed in graphical and alphanumeric form. It is important to note that this module only reads the results of the database file and no modifications can be executedhere.
A. DEFORM- Model
DEFORM- is a Finite Element Method-based three-dimensional (2D) metal cutting process simulation system (FEM). It provides critical material and heat flow information throughout the cutting process, making product design and tooling easier.
DEFORM 2D- has been utilised by companies all around the world to investigate turning, milling, drilling, finishing, and a range of other metal cutting processes.
DEFORM 2D offers state-of-the-art process simulation technology. Its powerful simulation engine can examine complicated interactions of several deforming objects with varying material properties throughout the metal cutting process.
This makes it possible to simulate the metal cutting process in a real-world context in a realistic and exact manner. Its clever mesh generator creates an optimal mesh system automatically as needed. By evaluating the solution behaviour, the mesh generator develops finer components in regions where improved solution accuracy is required, reducing the total problem size and processing requirements. It offers a comprehensive and adaptable graphical user interface that makes preparing input data and analysing output data a snap.
B. StepBy Step Procedure of Analysis Performed on 2-Deform
a. The name of the operation, the machining type, process setup, and process condition are all specified at the operation setup stage of the analysis.
b. Turning, Milling, Boring, Drilling, and Grooving procedures are among the machining types offered.
c. Cutting speed, rotating speed, depth of cut, and Feed rate are all parameters that may be specified under the Process setup settings.
d. Temperature, Shear friction factor, and Heat transfer coefficient are assigned under the Process condition choice.
2. Insert Setup Tool setup
a. Geometry, Meshing, Boundary Conditions, and Material Selection are all part of this configuration.
b. The geometry stage is critical because we must design the tool to the desired dimensions.
c. The created tool's meshing is based on the geometry's size. Set the tool's Boundary Conditions.
d. Load the correct material for the tool.
3. Work Piece Setup: Steps involving work piece setup resembles same as tool setup. At final work piece material loaded from material library available.
4. Position: The work piece and tool positioned according to the depth of cut required as shown in the figure 6.1.
5. Simulator: Simulator is the major keys for generated data base, simulator work carry out after completion of preprocess. At simulator window by switching the run simulator, the simulation process begins. It will take minimum of 2 to 3 hours’ time for generating the animation.
6. Post process: This post process controls the generated output animation. The output animation, tool and work piece positioning as shown in figure 5.
C. Simulation For Ammnc With Tungsten Carbide Tool
Simulations have been performed using 2D-Deform software at different cutting conditions on work piece material as in the following sections.
In this paper, FEA Simulations have been performed using 2-Deform software at different cutting conditions on workpiece material as in the following.
a. Input Conditions
Machining type : Turning
Speed : 280 rpm
Feed : 0.2mm
Depth of cut : 0.2mm
Tool material : Tungsten Carbide
Work piece Material : AMMNC
b. Output
Friction range : 0.000 to 1.46
Effective Stress : 0.000 to 127 (N/mm2)
Temperature : 20.0 to 63.5 0C
The 2D-Deform software at different cutting conditions on work piece material are shown in Fig (6 and7).
VI. RESULTS
By conducting the orthogonal cutting process, the machining responses are taken.Johnson cook constants are substituted in the Johnson cook model, to determine the flow stresses values.
The output responses flow stress and temperature are recorded from 2D Deform simulation.
Comparison of constitutive model values and 2D- deform model values as following
A. Flow Stress and Temperature
Comparing the flow stress values obtained from the Johnson cook model and 2D- Deform software model are given in Table 9 and 10.
B. Comparison of Flow Stress and Temperature obtained from constitutive models and 2d- Deform software
The machining reactions are obtained by using the orthogonal cutting method. The output parameters are determined using these values instead of Oxley's model. To obtain the flow stresses values, the Oxley's output values and Johnson cook constants are inserted in the Johnson cook model. The output responses of the 2D Deform simulation are flow stress and temperature.
2. Temperature
Fig (6-7) shows predicted, flow stress andtemperature at secondary zone values for aluminum nanocomposite material are compared with the results obtained from Johnson cook model and 2D-Deform software, and comparison is satisfactory.
The current research makes use of an enlarged metal cutting model developed by Oxley and colleagues, as well as a novel method for expanding the Johnson-Cook material model\'s applicability to cutting situations. Using constitutive models, the dynamic parameters Flow stress and Temperature distribution are predicted in this study. To acquire dynamic parameters, the orthogonal test values of speed, feed, and depth of cut are fed into the 2D-Deform software. The findings of the 2D-Deform software are compared to the predicted Flow stress and Temperature values for AMMNC, and the comparison is satisfactory. A. CRediT authorship contribution statement M. Madduleti: preparation of work material, turning operation, numerical modeling, investigation and validation, original draft preparation. P. Venkataramaiah: Conceptualization, Data curation, Formal analysis, Project administration, Writing - review & editing, Supervision. B. Declaration of Competing Interest The authors declare no conflict of interest. C. Acknowledgement Authors acknowledge support from MrDhanunjay, Research scholar, SVU College of Engineering. Dr. S. Suresh acknowledges the support from the Department of Mechanical Engineering, SIETK, Puttur, India. D. Current Funding Sources Funding information is not applicable / No funding was received. E. Data Availability The raw/processed data needed to replicate these findings is not available at this time because it is part of a current investigation. F. Ethical Approval No animals were used in any of the studies. G. Consent to Participate No humans have been used in any experiments. H. Consent to Publish The author certifies that the work described has not been published before (except as an abstract or as part of a published lecture, review, or thesis); that it is not under consideration for publication elsewhere; that it has been approved for publication by all co-authors, if any; and that it has been approved (tacitly or explicitly) by the responsible authorities at the institution where the work is performed.
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Copyright © 2022 Madduleti. M, P. Venkata Ramaiah. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Paper Id : IJRASET41052
Publish Date : 2022-03-28
ISSN : 2321-9653
Publisher Name : IJRASET
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