Machining of Titanium Alloys and Composites for Aerospace Applications Edited by R. Zitoune V. Krishnaraj J. Paulo Davim Machining of Titanium Alloys and Composites for Aerospace Applications Special topic volume with invited peer reviewed papers only Edited by R. Zitoune, V. Krishnaraj and J. Paulo Davim Copyright 2013 Trans Tech Publications Ltd, Switzerland All rights reserved. No part of the contents of this publication may be reproduced or transmitted in any form or by any means without the written permission of the publisher. Trans Tech Publications Ltd Kreuzstrasse 10 CH-8635 Durnten-Zurich Switzerland http://www.ttp.net Volume 763 of Materials Science Forum ISSN print 0255-5476 ISSN cd 1662-9760 ISSN web 1662-9752 Full text available online at http://www.scientific.net Distributed worldwide by and in the Americas by Trans Tech Publications Ltd Trans Tech Publications Inc. Kreuzstrasse 10 PO Box 699, May Street CH-8635 Durnten-Zurich Enfield, NH 03748 Switzerland USA Phone: +1 (603) 632-7377 Fax: +41 (44) 922 10 33 Fax: +1 (603) 632-5611 e-mail: [email protected] e-mail: [email protected] Preface A growing concern in the aerospace, automotive and biomedical industrial segments of the manufacturing industry is to build absolute reliability with maximum safety and predictability of the performance of all machined components. This requires development and deployment of predictive models for detailing the effects of varying machining parameters on fatigue life of machined components. The fatigue life is mainly affected by the residual stresses developed during the machining. Residual stresses are produced due to plastic deformation material while machining. The plastic deformation generates cracks and micro structural changes, as well as large micro hardness variations. Residual stresses have consequences on the mechanical behaviour, especially on the fatigue life of the workpieces. Residual stresses are also responsible for the machining distortion phenomenon of the machined parts which lead to difficulties during assembly. The literature detailing the effects of varying operating parameters on tool life when machining Titanium alloy is comprehensive, however, relatively little of this data refers to their effects on machined workpiece surface integrity particularly, residual stress generation and distortion created. Greater knowledge of the effects of operating parameters on surface integrity is critical to the acceptance of new environment, cutting path and cutting sequence strategies on machining of Ti6Al4V aerospace alloys to increase the functional requirements and fatigue life of the milled thin components. In this book four chapters have been included to address the above reported issues. The use of polymer matrix composite materials has significantly increased in the last few years. The aerospace, naval and automotive are the industry’s highly interested in this material, because of its strength/weight ratio which made it very attractive. Edge trimming, cut‐outs and holes exist in most of the composite structures. For example in an aircraft fuselage structure, around 10 million holes are required for joining purposes. However due to their laminated constructions several types of damages like matrix cratering and thermal alterations, fibre pullout and fuzzing, are introduced during machining. Trimming the edges of the composite part is the first and mandatory machining operation carried out after the composite parts are demoulded. This operation is done using conventional machining widely, or in some cases by using abrasive water jet cutting. The heterogeneity and anisotropy of the composite materials made their machining difficult. This has lead to the propagation of many defects. Damages are located at the free edges of the laminate or through the thickness (fibres pull‐out and resin degradation). Few chapters have been dedicated to address the issues of edge trimming and drilling of composite materials. Particularly, the influence of the quality of the machined surfaces (drilling and trimming) on the mechanical behaviour is analysed for different processes of machining. A chapter has been dedicated to address the challenges in drilling of multimaterials. This book will be a useful guide to those who would like to understand the issues in machining of titanium alloys and polymer composite materials. The editors express their sincere thanks to the authors, who contributed papers for this book. Redouane Zitoune Vijayan Krishnaraj J P Davim Table of Contents Preface Turning Investigations on Machining of Ti64 Alloy with Different Cutting Tool Inserts S. Ramesh and L. Karunamoorthy 1 Multi-Objective Optimization on Drilling of Titanium Alloy (Ti6Al4V) A. Prabukarthi, V. Krishnaraj and M. Senthil Kumar 29 Experimental Study on Tool Wear when Machining Super Titanium Alloys: Ti6Al4V and Ti-555 M. Nouari and H. Makich 51 Statistical Approach for Modeling Abrasive Tool Wear and Experimental Validation when Turning the Difficult to Cut Titanium Alloys Ti6Al4V F. Halila, C. Czarnota and M. Nouari 65 Laser Assisted Machining of Titanium Alloys M.W. Norazlan, Z. Mohid and E.A. Rahim 91 Influence of Tool Geometry and Machining Parameters on the Surface Quality and the Effect of Surface Quality on Compressive Strength of Carbon Fibre Reinforced Plastic M. Haddad, R. Zitoune, F. Eyma and B. Castanié 107 Analysis of Stresses in CFRP Composite Plates Drilled with Conventional and Abrasive Water Jet Machining M. Saleem, H. Bougherara, L. Toubal, F. Cénac and R. Zitoune 127 Challenges in Drilling of Multi-Materials V. Krishnaraj, R. Zitoune, F. Collombet and J.P. Davim 145 Materials Science Forum Vol. 763 (2013) pp 1-27 © (2013) Trans Tech Publications, Switzerland doi:10.4028/www.scientific.net/MSF.763.1 Turning Investigations on machining of Ti64 alloy with different cutting tool Inserts S.Ramesh1,a, L.Karunamoorthy2,b 1Department of Mechanical Engineering, Sona College of Technology, Salem – 636 005, INDIA 2Department of Mechanical Engineering, College of Engineering Guindy Campus, Anna University, Chennai-600 025, INDIA [email protected] (corresponding author) [email protected], Keywords: Machining, Titanium Alloy, Microstructure Studies, Cutting Force, Cutting temperature, Tool wear, Surface roughness, Machining Optimization, Grey Relational Analysis Abstract: Turning operation is fundamental in the manufacturing industry to produce cylindrical parts especially for producing near-nett shape, and aesthetic requirements with good dimensional accuracy. This present research chapter, an attempt has been made to investigate the machining characteristics of titanium alloys. The investigation has been carried out to measure the effect of tool flank wear, surface roughness, cutting force and temperature on different cutting tools by adopting Taguchi’s design of experiment concept. This investigation was set to analyse and develop a mathematical model using response surface methodology, fuzzy logic. The observed responses were optimized using grey relational grade algorithm. Except for a few cases, the experimental results have close proximity (95%) to the predicted value. This validates the model developed in this work. Orthogonal array with grey relational analysis has been successfully implemented for the optimization of the machining parameters. The optimized cutting conditions evolved in this research study will help to achieve better machinability of these advanced materials like titanium alloy. Introduction Titanium is one of the important metals and is used in various fields of engineering and medical sciences. Titanium (Ti), named after the Greek god Titan, was first discovered in 1791 (McQuillan and McQuillan [1]). Although it has been available more than two hundred years, it has only been produced commercially since the 1950s. Titanium is a member of the tin group of the periodic tables. Titanium is a very expensive structural material compared to steel. Titanium shows very good strength to weight ratio at elevated temperatures, and it has exceptional corrosion resistance. These characteristics have been the main cause for the rapid growth of the titanium industry over the last 55 years. The specific weight of titanium is only 2/3rd that of steel and only 60% greater than aluminium. The major application of this material is in aerospace industry, both in air frames and engine components. Non-aerospace applications mainly due to their excellent strength properties as in the case of steam turbine blades, superconductors, missiles etc., or corrosion resistance as in the case of marine services, chemical and petrochemical industries, electronics industry, biomedical instrumentation etc. However, the production and usage of titanium are expensive when compared to many other metals, because of the complexities of the extraction process, difficulty of melting and associated problems during fabrication. On the other hand, the longer service lives and higher property levels counterbalance the high production costs. Machining is important in metal-manufacturing process to achieve near-nett shape, good dimensional accuracy and for aesthetic requirements. The machining of titanium poses many problems. The problems encountered when machining titanium have usually originated in shops working with aircraft alloys. In 1955, Siekmann pointed out that machining of titanium and its alloys would always be a problem. The poor machinability of titanium has led many large companies (such as General Electric) to invest large amount of money in developing techniques in 2 Machining of Titanium Alloys and Composites for Aerospace Applications order to minimize machining costs. Similarly, tool makers are looking for new tool materials which would extend tool life in the presence of such a challenge. The inherent properties of the material make it more difficult to machine. The heat resistance property of the metal proves to be detrimental to the tool life of the cutting tool. Due to its low thermal conductivity, the heat produced during metal cutting accumulates at the small area of the tool-workpiece contact point, resulting in high thermal stresses and frictional forces. At high cutting forces and high cutting temperatures the workpiece material develops higher residual stresses (Guo et al [2] and Manouchehr Vosough [3], Ramesh et al [4]) The chemical reactivity of the material at elevated temperatures makes it easily react with the surrounding atmosphere. Ordinary cutting tools may fail prematurely under these adverse conditions. So, alternate cutting tools which can serve effectively at these severe cutting conditions are to be considered. Cutting parameters have to be carefully selected so as to produce machined surfaces with high level of surface finish at reasonable production rates. The temperature gradients in the tools used for cutting titanium alloys are similar in character to those found when cutting the commercially pure metal (Edward et al [5] and Milton C. Shaw [6]). The present work is aimed at studying the performance of different cutting tool inserts in the machining of Titanium alloy (Ti-64). The work material used for the present investigation is with characteristic microstructures of α + β phase. The machining tests were carried out on lathe. The operations carried out on lathe for the present investigation is turning. Turning is one of the important operations and is backbone of many industrial manufacturing operations. The cutting performance in turning of titanium alloy is evaluated by using the performance investigators such as tool flank wear, surface roughness, and cutting force. In the present work, an attempt has also been made to analyze and optimize the machining parameters in the machining of titanium alloys. Statistics and optimization techniques are important tools used for modeling the machining characteristics and performing the optimization of cutting parameters for achieving the selected objectives. The modeling of machining parameters is carried out using response surface methodology (RSM) and validation of model is done by using fuzzy logic. Grey relational analysis has been used to optimize the machining characteristic with multiple performance characteristics. The effect of temperature on machining of titanium alloy has also been investigated in the present study. 2. Literature Review The demand for machining of titanium alloy has been increased in recent years (Klaus Gebauer [7] and Kennametal [8]). In order to understand and access the current status of research in machining of titanium alloys, an extensive literature review has been carried out. The selected literature reviews for the present investigations are given hereunder: 2.1. Machining of Titanium Alloys The present study is focused on the machining characteristics of titanium alloy. In general, a finish machining of a titanium component will be necessary, because of the requirement of exact dimensional accuracy, surface quality and material homogeneity. Machining of titanium alloy poses considerable problem due to its poor machinability (Komanduri [9] and Awopetu [10]). The poor machinability of titanium has led many large companies (for example Rolls-Royce and General Electric) to invest large amount of money in developing techniques to minimize machining costs. Similarly, tool makers are looking for new tool materials which can extend tool life in the presence of such a challenge (Machado and Wallbank [11], Ramesh et al [12, 13]). Materials Science Forum Vol. 763 3 From the available literature, it has been noticed that the first literature on machining of titanium alloy was presented by Siekmann [14]. It has been pointed out that machining of titanium and its alloys will always be a problem no matter what technique is employed to transform this metal into chips. Komanduri and Reed [9] have commented that the machining difficulty of titanium alloy is still true as far as cutting tool materials are concerned. While improving the machining rates will go a long way towards increasing the usage of the material, it must be noted that this is only one of the number of factors affecting the use of the material. Others, which include material cost, must also be considered in any specific application. The Metals Handbook [15] gives detailed information about the alpha-beta alloy, Ti-64 which accounts for about 45% of the total titanium production while unalloyed grades comprise about 30%. All the other alloys comprise of the remaining 25%. Michael Field [16] has set some guidelines for improving surface integrity as a new requirement for improving reliability of Aerospace hardware. Komanduri et al [17] presented some new observations on the mechanism of chip formation to increase productivity when machining Titanium alloys and reported interesting findings towards the goal. Hartung et al [18] have investigated turning test on Ti-64 with conventional (Carboloy 820 and Kennametal K68) grade cemented carbides. They analyzed and suggested that tool wear rate of tool materials, which maintain a stable reaction layer, is limited by the diffusion rate of tool constituents from the tool-chip interface. The diffusion flux correlates well with the observed wear rate. Bhaumik et al [19] has developed a wurtzite boron nitride–cubic boron nitride (wBN-cBN) composite tool obtained by high pressure/high temperature sintering for machining Ti-64 alloys. In their investigation they indicated that this composite tool can be used economically to machine titanium alloys. Bayoumi et al [20] have studied the behavior of chip formation using various metallurgical analysis techniques. Obikawa et al [21] has studied the computational machining of titanium alloy using finite element analysis. They have used finite element modeling to simulate the serrated chip formation similar to that found by actual cutting. Kitagawa et al [22] have carried out high speed machining on Inconel 718 and Ti-6Al-6V-2Sn alloys from a thermal point of view. They have studied the temperature and wear of the cutting tools by means of cutting experiments and numerical analysis up to a cutting speed of around 600 m/min. Toru Okabe et al [22] have explored the present status of titanium castings in the field of biomaterials as dental casting. Zoya and Krishnamurthy [24] have discussed the factors that affect the machining of titanium and its alloys. They have stated that the machining of titanium alloys is a thermally dominant process. With the increase in cutting speed, the temperature produced also increased. They observed that surface roughness increased with increasing cutting speed in the range of 150-350 m/min at 0.5 mm depth of cut. Barry et al [25] have carried out some observations on chip formation and acoustic emission in machining Ti-64 alloy. They have found that the degree of welding between the chip and the tool increases with cutting speed. Shane et al [26] have reported how the temperature affects Ti-64 alloy properties and they have proposed a new economical cryogenic cooling approach. Shuting Lei et al [27] have invented a new generation driven rotary lathe tool for high-speed machining of titanium alloy, Ti-64. They have found that the tool can significantly increase tool life and achieved more than 60 times. Corduan et al [28] have presented the interactions between Polycrystalline Diamond (PCD), Cubic Boron Nitride (cBN) and TiB2 -coated carbide with