<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">MSCE</journal-id><journal-title-group><journal-title>Journal of Materials Science and Chemical Engineering</journal-title></journal-title-group><issn pub-type="epub">2327-6045</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/msce.2016.44002</article-id><article-id pub-id-type="publisher-id">MSCE-66113</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject></subj-group></article-categories><title-group><article-title>
 
 
  Hardness Profile Prediction for a 4340 Steel Spline Shaft Heat Treated by Laser Using a 3D Modeling and Experimental Validation
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ahdi</surname><given-names>Hadhri</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Abderazzak</surname><given-names>El Ouafi</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Noureddine</surname><given-names>Barka</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Computer Science and Engineering Department, University of Quebec, Rimouski, Canada</addr-line></aff><pub-date pub-type="epub"><day>25</day><month>04</month><year>2016</year></pub-date><volume>04</volume><issue>04</issue><fpage>9</fpage><lpage>19</lpage><history><date date-type="received"><day>6</day>	<month>April</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>25</month>	<year>April</year>	</date><date date-type="accepted"><day>28</day>	<month>April</month>	<year>2016</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  Laser surface transformation hardening becomes one of the most effective processes used to improve wear and fatigue resistance of mechanical parts. In this process, the material physicochemical properties and the heating system parameters have significant effects on the characteristics of the hardened surface. To appropriately exploit the benefits presented by the laser surface hardening, it is necessary to develop a comprehensive strategy to control the process variables in order to produce desired hardened surface attributes without being forced to use the traditional and fastidious trial and error procedures. The paper presents a study of hardness profile predictive modeling and experimental validation for spline shafts using a 3D model. The proposed approach is based on thermal and metallurgical simulations, experimental investigations and statistical analysis to build the prediction model. The simulation of the hardening process is carried out using 3D finite element model on commercial software. The model is used to estimate the temperature distribution and the hardness profile attributes for various hardening parameters, such as laser power, shaft rotation speed and scanning speed. The experimental calibration and validation of the model are performed on a 3 kW Nd:Yag laser system using a structured experimental design and confirmed statistical analysis tools. The results reveal that the model can provide not only a consistent and accurate prediction of temperature distribution and hardness profile characteristics under variable hardening parameters and conditions but also a comprehensive and quantitative analysis of process parameters effects. The modelling results show a great concordance between predicted and measured values for the dimensions of hardened zones.
 
</p></abstract><kwd-group><kwd>Heat Treatment</kwd><kwd> Laser Surface Transformation Hardening</kwd><kwd> Finite Element Method</kwd><kwd> Hardness  Profile Prediction</kwd><kwd> AISI 4340</kwd><kwd> Nd:Yag Laser System</kwd><kwd> ANOVA</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Surface transformation hardening processes are designed to improve wear and fatigue resistance by hardening the superficial critical areas using brief and localized heat gains. Among these processes, laser surface transformation hardening process is well-known by his capacity in terms of power flux density and is recognized by his fast, local and accurate thermal cycles, while limiting the risks of undesirable distortion and deformation effects. Application of the laser beam rapidly raises the surface temperature (more than to 1000 K/s), resulting in a thin layer that is converted into austenite. Subsequent removal of this energy results in self-quenching caused by the conduction of heat into the relatively cool bulk of the material. This produces a rapidly cooled surface layer and causes a transformation of the austenite into martensite [<xref ref-type="bibr" rid="scirp.66113-ref1">1</xref>] - [<xref ref-type="bibr" rid="scirp.66113-ref5">5</xref>] .</p><p>Laser surface transformation hardening offers several advantages: localized treated areas, a relatively small heat affected zone, limited metallurgical changes, reduced residual stresses, very fast thermal cycling and autogenous quenching, and appropriate process for automation and complex production lines when using robots. Despite all its advantages, applications of laser surface treatments represent a very small percentage of industrial plants. Laser surface hardening is still in its infancy, with only a few years of development and it is virtually only developed in the aerospace and automotive industries. This work is a continuing effort to develop power laser applications for surface treatments.</p><p>The modeling of laser heat treatment went through several stages. In the first, researchers were interested in statistical modeling to understand the influence of certain parameters and develop empirical formulas [<xref ref-type="bibr" rid="scirp.66113-ref6">6</xref>] - [<xref ref-type="bibr" rid="scirp.66113-ref8">8</xref>] . Then, other researchers became interested in analytical modeling based on the general equation of heat conduction proposed by Fourier [<xref ref-type="bibr" rid="scirp.66113-ref9">9</xref>] - [<xref ref-type="bibr" rid="scirp.66113-ref11">11</xref>] . During the 90s, advancements in IT brought more powerful computational tools to researchers in all fields. Several numerical modeling platforms made their appearances and greatly accelerated technical developments. These improvements allowed more complex problems to be modeled and solved. According to the literature, there were three methods to model a mobile heat source. The first method was based on the Rosenthal equation of a mobile heat source [<xref ref-type="bibr" rid="scirp.66113-ref12">12</xref>] [<xref ref-type="bibr" rid="scirp.66113-ref13">13</xref>] . The second was to move the source implicitly based on the transport term in the heat equation [<xref ref-type="bibr" rid="scirp.66113-ref14">14</xref>] . The last one was the method of Area Sector Approach. The geometry of the heat treated sample was the main factor in selecting the method of modeling [<xref ref-type="bibr" rid="scirp.66113-ref15">15</xref>] [<xref ref-type="bibr" rid="scirp.66113-ref16">16</xref>] . The second method was efficient only if the geometry was not intricate, and the third was applicable when the movement was simple. The first method was effectual with complex geometries and complex movement, but the challenge was finding the ideal trajectories of the heat source.</p><p>To treat revolutionary geometries, the sample must be rotated, and the laser beam must be in a translational movement as illustrated in <xref ref-type="fig" rid="fig1">Figure 1</xref>. In accordance with the literature, Rahul Patwa and Shin achieved a 3D finite-element model [<xref ref-type="bibr" rid="scirp.66113-ref17">17</xref>] . The model combines a transient digital three-dimensional solution (based on the modeling of Rozzi et al. [<xref ref-type="bibr" rid="scirp.66113-ref18">18</xref>] [<xref ref-type="bibr" rid="scirp.66113-ref19">19</xref>] ) for a rotary cylinder undergoing laser heating by beam translation with a kinetic model. In order to verify the results of the simulation, an experiment is performed. Both researchers reach a depth of 0.54 mm with a hardness of 63 HRC on an AISI 5150 steel sample with a laser (diode) power of 500 W and a rotational speed of 6 RPM [<xref ref-type="bibr" rid="scirp.66113-ref17">17</xref>] . Skvarenina et al. were capable of predicting and experimentally validating a 2.5 mm hardening depth with a uniform hardness of 57 HRC on an AISI 1536 steel cylinder 60 mm in diameter, using a scanning speed of 2.9 mm/s, a diode laser power of 1220 W and a rotation speed of 1 RPM [<xref ref-type="bibr" rid="scirp.66113-ref20">20</xref>] . Another thermal transient 3D model is developed by Leonardo Orazi et al. [<xref ref-type="bibr" rid="scirp.66113-ref21">21</xref>] . The model is based on the geometry of the ring spot and was validated by experimental tests. The advantage of the Leonardo model over other models is that it achieves very high speeds. For a rotational speed of 1140 RPM, a power of 1 kW, a scanning speed of 30 mm/min, and a test piece of AISI 1040 steel 30 mm in diameter, he found a hardness of 690 HV. In general, a second laser pass generates a tempering of the material that is characterized by a drop in micro hardness. In the same context, low processing speeds create a superposition of treatment which gives a non- homogeneous micro hardness.</p><p>The literature review reveals the small number of researches dealing with revolutionarily complex sample processing. The majority of the researchers focused mainly on the study of this phenomenon on gears. Benedict and Eskildsen tested an approach to treat small gears, which proved very promising [<xref ref-type="bibr" rid="scirp.66113-ref22">22</xref>] . In fact, this method consisted of the laser beam scanning from one gear tooth tip to another through variation of the angle of incidence, power, and interaction time (forward speed). In 2003, Zhang et al. used this approach to treat sprockets with 98 mm outside diameters and 23 teeth [<xref ref-type="bibr" rid="scirp.66113-ref23">23</xref>] . They were installed on a mounting allowing the wheel to be moved laterally and be brought into rotation. The results were very conclusive: the cured depth of the flanks was</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Basic configuration of the laser hardening of a cylindrical part</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x7.png"/></fig><p>of a relatively uniform thickness and was not a stressed fusion surface. However, no process modeling was presented. Pretorius and Vollertsen have modeled a form of laser heat treatment on a toothed wheel, where the heat treatment was applied only in the tooth root [<xref ref-type="bibr" rid="scirp.66113-ref24">24</xref>] . The 3D digital model was developed using the SYSWELD package and consisted of modeling the thermal flow, metallurgical transformations, and geometrical. Clearly, the modeling of heat treatment of the revolutionary complex geometry is limited. Among such geometries are spline shafts. Until now, there is no work, neither experimental nor modeling, which presents the laser heat treatment of the spline shaft. Due to its ability to transmit large torques and ease machining, spline shafts have become the essential tools for power transmission. In this work, a method for the prediction of hardened depth using laser heat treatment of a spline shaft with a high speed of revolution is presented.</p><p>The main objective of this work is to develop an integrated approach for hardness profile predictive modeling and experimental validation for spline shafts using a 3D model. The numerical simulation of the hardening process is carried out by 3D finite element model using Comsol Multiphysics software. The model is used to estimate the temperature distribution and the hardness profile attributes for various hardening parameters and material properties. Applied on AISI 4340 steel spline shaft, the experimental calibration and validation of the model is performed on a commercial 3 kW Nd:Yag laser system using a structured experimental design and confirmed statistical analysis tools. The results reveal that the model can provide not only a consistent and accurate prediction of temperature distribution and hardness profile characteristics under variable hardening parameters and conditions but also a comprehensive analysis of process parameters effects. The results show great concordance between predicted and measured values for the dimensions of hardened zones.</p></sec><sec id="s2"><title>2. Finite Element Modeling</title><p>In this study, the laser was modeled as a source of circular Gaussian heat. The laser moves along the spline shaft. The latter is mounted in a test stand that allows it to be turned at rather high rotational speeds.</p><p>In general, non-linear mathematical models of heat transfer by conduction in a homogeneous and isotropic medium take the following form:</p><disp-formula id="scirp.66113-formula1713"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x8.png"  xlink:type="simple"/></disp-formula><p>The volume density of the laser Q (x, y, z, t) applied to the material, is given by:</p><disp-formula id="scirp.66113-formula1714"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x9.png"  xlink:type="simple"/></disp-formula><p>Here Q<sub>0</sub> is the power of laser, A<sub>c</sub> is the coefficient of absorption, R<sub>c</sub> is the coefficient of reflection, W is the radius of the laser beam, and f (x, y, z, t) is the function that describes the shape and the path of the beam, given by:</p><disp-formula id="scirp.66113-formula1715"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x10.png"  xlink:type="simple"/></disp-formula><p>The challenge in modeling the laser heat treatment of splines is that the geometry is complex and the heat source must follow the teeth and the flanks of groove. For this, the solution was to find a mobile frame of vector space at each time t, of which a, b and c are given by:</p><disp-formula id="scirp.66113-formula1716"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x11.png"  xlink:type="simple"/></disp-formula><p>where x<sub>1</sub> is the length travelled by the laser beam, t<sub>f</sub> is the duration of treatment, ω is the rotational speed in rad/s, y<sub>0</sub> and z<sub>0</sub> are the instantaneous positions along y and z, respectively, and are given by Equation (5):</p><disp-formula id="scirp.66113-formula1717"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x12.png"  xlink:type="simple"/></disp-formula><p>The beam should treat tooth and flank, which requires clarified beam position either on the tooth or the flank.</p><disp-formula id="scirp.66113-formula1718"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x13.png"  xlink:type="simple"/></disp-formula><p>Here R<sub>d</sub> is the outer diameter of spline shaft, e is the depth of the groove and H (t) is the position function of the laser beam:</p><disp-formula id="scirp.66113-formula1719"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x14.png"  xlink:type="simple"/></disp-formula><p>where A is a function dependent on the number of teeth.</p></sec><sec id="s3"><title>3. Metallurgical Modeling</title><p>The metallurgical transformation process for the heat treatment of steel occurs over three major steps: the pearlite transformation to austenite (pearlite dissolution), the homogenization of the carbon in austenite, and the austenite transformation to martensitic [<xref ref-type="bibr" rid="scirp.66113-ref25">25</xref>] . By heating the material up to the temperature of eutectoid Ac1, colonies of pearlite in the microstructure are transformed into austenite. The distance between the pearlite plates, which allow colonies pearlite to be completely transformed into austenite, is given by the following formula:</p><disp-formula id="scirp.66113-formula1720"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x15.png"  xlink:type="simple"/></disp-formula><p>where D<sub>0</sub> is the diffusion constant, Q<sub>a</sub> is the activation energy, R the gas constant, T<sub>p</sub> is the temperature of spades, and the two constants c<sub>d</sub> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/2-1740328x16.png" xlink:type="simple"/></inline-formula> are given by Equations (9) and (10):</p><disp-formula id="scirp.66113-formula1721"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x17.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.66113-formula1722"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x18.png"  xlink:type="simple"/></disp-formula><p>Here K the thermal conductivity, V is the scanning speed, T<sub>0</sub> is the initial temperature and R is the reflection coefficient. The homogenization mechanism is simple: around a ferrite grain and a cementite grain, an austenite germ can be created. This germ is formed by eutectoid transformation with a chemical composition of 0.8% C. As the temperature rises it undergoes a systematic change in its composition. Rapid cooling of the austenite, which is formed only within a thin layer during laser hardening due to the self-sealing of the material when the laser beam is moved away, makes it difficult for carbon to diffuse outside its lattice [<xref ref-type="bibr" rid="scirp.66113-ref26">26</xref>] [<xref ref-type="bibr" rid="scirp.66113-ref27">27</xref>] . When the carbon is trapped in the network and cooled, the face-centered cubic crystal structure of austenite is transformed into a hybrid quadratic structure, called martensite [<xref ref-type="bibr" rid="scirp.66113-ref5">5</xref>] . The martensitic volume fraction, f, which is formed on a period T, is given by Equation (11):</p><disp-formula id="scirp.66113-formula1723"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x19.png"  xlink:type="simple"/></disp-formula><p>where f<sub>i</sub> = C/0.8 as the initial volume fraction of pearlite and f<sub>m</sub> is the volume fraction of martensite, given by the following relationship:</p><disp-formula id="scirp.66113-formula1724"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x20.png"  xlink:type="simple"/></disp-formula><p>The hardness of the material is calculated as follows:</p><disp-formula id="scirp.66113-formula1725"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/2-1740328x21.png"  xlink:type="simple"/></disp-formula><p>H<sub>m</sub> and H<sub>f+p</sub> are calculated following Maynier’s equations and taking into account the initial chemical composition [<xref ref-type="bibr" rid="scirp.66113-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.66113-ref11">11</xref>] .</p></sec><sec id="s4"><title>4. Simulation Results</title><p>This study investigates the machine sensitivity parameters of laser heat treatment of an AISI 4340 steel spline shaft. The AISI 4340 steel is very common in the aerospace and automotive industries in the manufacture of propeller shafts, connecting rods, gear shafts and other parts, and automobiles due to its high tensile strength. The AISI 4340 chemical composition is given in <xref ref-type="table" rid="table1">Table 1</xref>. The sample used in the simulations and validation is 15 mm in diameter, 2.5 mm in thickness and is inclined at an angle of 20˚C. Primary results of the simulation of heat treatment showed that there is no heat affected area and the temperature does not exceed 350˚C, even with a speed of 2 mm/s, a power of 2500 W, and rotation speed of 1500 RPM. The results are experimentally validated. To achieve a heat affected zone by the laser beam, it must pass through a preliminary heating. Multiple scanning was carried out to increase the original sample temperature from 20˚C to 500˚C. <xref ref-type="table" rid="table2">Table 2</xref> shows the material properties used for the simulation.</p><p>It is clear in <xref ref-type="fig" rid="fig2">Figure 2</xref> that the laser is in the process of turning around the spline shaft, treating both the tooth and the flank. The temperature rises to 837˚C with a rotational speed of 1000 RPM, a scanning speed of 5 mm/s, and a power of 2200 W. Note that the austenitizing temperature is 790˚C.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref> and <xref ref-type="fig" rid="fig4">Figure 4</xref> show that the temperature progressively increases approaching the measurement point,</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Material chemical composition of 4340 steel</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Element</th><th align="center" valign="middle" >Content (wt%)</th></tr></thead><tr><td align="center" valign="middle" >C</td><td align="center" valign="middle" >0.38 - 0.43</td></tr><tr><td align="center" valign="middle" >Cr</td><td align="center" valign="middle" >0.70 - 0.90</td></tr><tr><td align="center" valign="middle" >Mn</td><td align="center" valign="middle" >0.60 - 0.80</td></tr><tr><td align="center" valign="middle" >Mo</td><td align="center" valign="middle" >0.20 - 0.30</td></tr><tr><td align="center" valign="middle" >Ni</td><td align="center" valign="middle" >1.65 - 2.00</td></tr><tr><td align="center" valign="middle" >P</td><td align="center" valign="middle" >0.040 max</td></tr><tr><td align="center" valign="middle" >Si</td><td align="center" valign="middle" >0.20 - 0.35</td></tr><tr><td align="center" valign="middle" >S</td><td align="center" valign="middle" >0.040 max</td></tr><tr><td align="center" valign="middle" >Fe</td><td align="center" valign="middle" >Balance</td></tr></tbody></table></table-wrap><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Distribution of temperature</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x22.png"/></fig><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Distribution of heat flux</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x23.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> The evolution of temperature versus time (x = 5, y = 0, z = 15)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x24.png"/></fig><p>then gradually decreases away from the measurement point. It is clear that the temperature increases and decreases when the laser beam turns around the spline shaft.</p></sec><sec id="s5"><title>5. Experimental Validation</title><p>A Yag laser with a maximum power of 3 KW was used to validate the finite element model. The laser head is mounted on a Fanuc robot with six degrees of freedom (see <xref ref-type="fig" rid="fig5">Figure 5</xref> left). The laser beam diameter is evaluated at 1.08 mm when focused. The specimens are treated by a hardening and tempering process to ensure a core hardness of 35 HRC. The latter is the untreated area. The prediction algorithm is intended to look at the hardened area. Two validation tests shown in <xref ref-type="table" rid="table3">Table 3</xref>, are performed to validate the hardened depth at the tooth (D<sub>t</sub>) and the flank (D<sub>f</sub>).</p><p>The curve describing the hardness profile is divided into three zones. The first is the hardened zone, consisting of 100% martensite. The second is the transition zone, consisting of ferrite, perlite and martensite. The third</p><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Material properties of 4340 steel</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Property</th><th align="center" valign="middle" >Symbol</th><th align="center" valign="middle" >Unit</th><th align="center" valign="middle" >Value</th></tr></thead><tr><td align="center" valign="middle" >Reflexion coefficient</td><td align="center" valign="middle" >Rc</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >0.6</td></tr><tr><td align="center" valign="middle" >Steel absorptivity</td><td align="center" valign="middle" >Ac</td><td align="center" valign="middle" >m<sup>−</sup><sup>1 </sup></td><td align="center" valign="middle" >800</td></tr><tr><td align="center" valign="middle" >Eutectoid temperature</td><td align="center" valign="middle" >Ac1</td><td align="center" valign="middle" >K</td><td align="center" valign="middle" >996</td></tr><tr><td align="center" valign="middle" >Austenitization temperature</td><td align="center" valign="middle" >Ac3</td><td align="center" valign="middle" >K</td><td align="center" valign="middle" >1063.15</td></tr><tr><td align="center" valign="middle" >Austenite grain size (assumed)</td><td align="center" valign="middle" >g</td><td align="center" valign="middle" >&#181;m</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle" >Activation energy of carbon diffusion in ferrite</td><td align="center" valign="middle" >Q</td><td align="center" valign="middle" >KJ/mol</td><td align="center" valign="middle" >10</td></tr><tr><td align="center" valign="middle" >Pre-exponential for diffusion of carbon</td><td align="center" valign="middle" >D0</td><td align="center" valign="middle" >m<sup>2</sup>/s</td><td align="center" valign="middle" >80</td></tr><tr><td align="center" valign="middle" >Gas constant</td><td align="center" valign="middle" >R</td><td align="center" valign="middle" >J/mol・K</td><td align="center" valign="middle" >6.10<sup>−</sup><sup>5 </sup></td></tr><tr><td align="center" valign="middle" >Steel carbon content</td><td align="center" valign="middle" >C</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >0.34%</td></tr><tr><td align="center" valign="middle" >Austenite carbon content</td><td align="center" valign="middle" >Ce</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >0.8%</td></tr><tr><td align="center" valign="middle" >Ferrite carbon content</td><td align="center" valign="middle" >Cf</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >0.01%</td></tr><tr><td align="center" valign="middle" >Critical value of carbon content</td><td align="center" valign="middle" >Cc</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >0.05%</td></tr><tr><td align="center" valign="middle" >Volume fraction of pearlite colonies</td><td align="center" valign="middle" >fi</td><td align="center" valign="middle" ></td><td align="center" valign="middle" >0.5375</td></tr></tbody></table></table-wrap><table-wrap id="table3" ><label><xref ref-type="table" rid="table3">Table 3</xref></label><caption><title> Numerical model validation tests</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Test</th><th align="center" valign="middle" >P (W)</th><th align="center" valign="middle" >V (mm/s)</th><th align="center" valign="middle" >W (RPM)</th></tr></thead><tr><td align="center" valign="middle" >1</td><td align="center" valign="middle" >2500</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >1500</td></tr><tr><td align="center" valign="middle" >2</td><td align="center" valign="middle" >2200</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >2000</td></tr></tbody></table></table-wrap><fig-group id="fig5"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Experimental setup and example of hardness profile.</title></caption><fig id ="fig5_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x25.png"/></fig><fig id ="fig5_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x26.png"/></fig></fig-group><p>zone is the untreated area. The transition zone is not considered in the modeling. The modeling of the transition zone with precision depends on two main parameters: the cooling rate and the initial hardness of the material [<xref ref-type="bibr" rid="scirp.66113-ref26">26</xref>] [<xref ref-type="bibr" rid="scirp.66113-ref27">27</xref>] . In the Figures 5-7, we can see that the error of modeling the martensitic area is below 15%. The tests show that the flank hardened depth is always less than or equal to the depth of the hardened tooth.</p></sec><sec id="s6"><title>6. Statistical Analysis</title><p>The objective of this part is to identify the influence of various system parameters on the hardened depth. This is carried out with the help of experiment designs, consisting in producing a series of N experiments and determining the value of the response function for these N configurations. So, in this case, the selected solution is the profile of the hardened depth shown by the tow characteristic measurements {D<sub>t</sub>, D<sub>f</sub>}. The experiments are carried</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Sample of hardness profile-2200 W, 4 mm/s and 2000 RPM</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x27.png"/></fig><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Sample of hardness profile-2200 W, 4 mm/s and 2000 RPM</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x28.png"/></fig><p>out using a 3D model with COMSOL software (see <xref ref-type="fig" rid="fig2">Figure 2</xref>). The factors to be examined in this study are power, rotary speed and scanning speed. Taguchi proposed that in order to optimize a process or a product, experiments should be carried out in a three-step approach, i.e. system design, parameter design, and tolerance design [<xref ref-type="bibr" rid="scirp.66113-ref28">28</xref>] . The Taguchi orthogonal designs offer minimizes the effect of aliases and measures error with minimum testing. In this context, aL9 orthogonal array of 3 factors and 3 levels was chosen (see <xref ref-type="table" rid="table4">Table 4</xref>).</p><p>The present study used ANOVA to determine the optimum combination of process parameters more accurately by investigating the relative importance of each parameter [<xref ref-type="bibr" rid="scirp.66113-ref29">29</xref>] . <xref ref-type="table" rid="table5">Table 5</xref> presents the results of ANOVA for the tooth hardened depth (D<sub>t</sub>). It is observed from the results (<xref ref-type="table" rid="table5">Table 5</xref> and <xref ref-type="fig" rid="fig8">Figure 8</xref>) that the scanning speed (68.66%) is the most significant parameter, followed by power (25.14%). The rotary speed has the smallest effect (3.02%) in hardened depth. Statistically, the F-test determines whether the parameters are significantly different. A larger F value shows a greater impact on the machining performance characteristics [<xref ref-type="bibr" rid="scirp.66113-ref29">29</xref>] . Larger F- values are observed for scanning speed, as 25.24, and for power, as 7.18.</p><p>As seen from the ANOVA results in <xref ref-type="table" rid="table6">Table 6</xref> and <xref ref-type="fig" rid="fig9">Figure 9</xref>, the influence of the scanning speed (66.06%) in the hardened depth of the flank is significantly larger. The power (27.28%) is the second most significant factor. Again, the rotary speed has the least effect (3.45%) on D<sub>f</sub>. It is also observed that there is an error contribution of 3.21% in the hardened depth on the flank.</p></sec><sec id="s7"><title>7. Conclusion</title><p>In this paper, an integrated approach used to build a hardness profile prediction model for AISI 4340 spline shafts heat treated by laser is presented. Numerical simulation carried out through 3D finite element model using Comsol Multiphysics software is discussed. A commercial 3 kW Nd:Yag laser system, a structured experimental</p><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Effect of the parameters on the depth (D<sub>t</sub>)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x29.png"/></fig><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Effect of the parameters on the depth (D<sub>f</sub>)</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1740328x30.png"/></fig><table-wrap id="table4" ><label><xref ref-type="table" rid="table4">Table 4</xref></label><caption><title> Experimental planning</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Test</th><th align="center" valign="middle" >P (W)</th><th align="center" valign="middle" >V (mm/s)</th><th align="center" valign="middle" >W (RPM)</th><th align="center" valign="middle" >P<sub>d</sub> (&#181;m)</th><th align="center" valign="middle" >P<sub>f</sub> (&#181;m)</th></tr></thead><tr><td align="center" valign="middle" >1</td><td align="center" valign="middle" >1900</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >1500</td><td align="center" valign="middle" >340</td><td align="center" valign="middle" >144</td></tr><tr><td align="center" valign="middle" >2</td><td align="center" valign="middle" >1900</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >2000</td><td align="center" valign="middle" >111</td><td align="center" valign="middle" >56</td></tr><tr><td align="center" valign="middle" >3</td><td align="center" valign="middle" >1900</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >2500</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0</td></tr><tr><td align="center" valign="middle" >4</td><td align="center" valign="middle" >2200</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >2000</td><td align="center" valign="middle" >695</td><td align="center" valign="middle" >308</td></tr><tr><td align="center" valign="middle" >5</td><td align="center" valign="middle" >2200</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >2500</td><td align="center" valign="middle" >260</td><td align="center" valign="middle" >106</td></tr><tr><td align="center" valign="middle" >6</td><td align="center" valign="middle" >2200</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >1500</td><td align="center" valign="middle" >63</td><td align="center" valign="middle" >54</td></tr><tr><td align="center" valign="middle" >7</td><td align="center" valign="middle" >2500</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >2500</td><td align="center" valign="middle" >923</td><td align="center" valign="middle" >407</td></tr><tr><td align="center" valign="middle" >8</td><td align="center" valign="middle" >2500</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >1500</td><td align="center" valign="middle" >325</td><td align="center" valign="middle" >154</td></tr><tr><td align="center" valign="middle" >9</td><td align="center" valign="middle" >2500</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >2000</td><td align="center" valign="middle" >156</td><td align="center" valign="middle" >108</td></tr></tbody></table></table-wrap><table-wrap id="table5" ><label><xref ref-type="table" rid="table5">Table 5</xref></label><caption><title> Variance analysis case of depth (D<sub>t</sub>)</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Source</th><th align="center" valign="middle" >DF</th><th align="center" valign="middle" >Sum of Squares</th><th align="center" valign="middle" >Mean Square</th><th align="center" valign="middle" >F-Value</th><th align="center" valign="middle" >P-Value</th><th align="center" valign="middle" >C (%)</th></tr></thead><tr><td align="center" valign="middle" >P</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >153188</td><td align="center" valign="middle" >76594</td><td align="center" valign="middle" >7.18</td><td align="center" valign="middle" >0.122</td><td align="center" valign="middle" >25.14</td></tr><tr><td align="center" valign="middle" >V</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >538255</td><td align="center" valign="middle" >269127</td><td align="center" valign="middle" >25.24</td><td align="center" valign="middle" >0.038</td><td align="center" valign="middle" >68.66</td></tr><tr><td align="center" valign="middle" >W</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >34514</td><td align="center" valign="middle" >17257</td><td align="center" valign="middle" >1.62</td><td align="center" valign="middle" >0.382</td><td align="center" valign="middle" >3.02</td></tr><tr><td align="center" valign="middle" >Error</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >21323</td><td align="center" valign="middle" >10661</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >3.18</td></tr><tr><td align="center" valign="middle" >Total</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >747280</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >100</td></tr></tbody></table></table-wrap><table-wrap id="table6" ><label><xref ref-type="table" rid="table6">Table 6</xref></label><caption><title> Variance analysis case of depth (D<sub>f</sub>)</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Source</th><th align="center" valign="middle" >DF</th><th align="center" valign="middle" >Sum of Squares</th><th align="center" valign="middle" >Mean Square</th><th align="center" valign="middle" >F-Value</th><th align="center" valign="middle" >P-Value</th><th align="center" valign="middle" >C (%)</th></tr></thead><tr><td align="center" valign="middle" >P</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >36910</td><td align="center" valign="middle" >18455</td><td align="center" valign="middle" >8.47</td><td align="center" valign="middle" >0.105</td><td align="center" valign="middle" >27.28</td></tr><tr><td align="center" valign="middle" >V</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >89375</td><td align="center" valign="middle" >44687</td><td align="center" valign="middle" >20.56</td><td align="center" valign="middle" >0.046</td><td align="center" valign="middle" >66.06</td></tr><tr><td align="center" valign="middle" >W</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >4667</td><td align="center" valign="middle" >2333</td><td align="center" valign="middle" >1.07</td><td align="center" valign="middle" >0482</td><td align="center" valign="middle" >3.45</td></tr><tr><td align="center" valign="middle" >Error</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >4347</td><td align="center" valign="middle" >2173</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >3.21</td></tr><tr><td align="center" valign="middle" >Total</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >135298</td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" >100</td></tr></tbody></table></table-wrap><p>design and confirmed statistical analysis tools are used to conduct the experimental study for the prediction model calibration and validation. The results reveal that the numerical simulation can effectively lead to a consistent and accurate model and provide an appropriate prediction of the hardness profile attributes under variable hardening parameters and conditions. With a maximumerror less than 15%, the validation process shows great concordance between predicted and experimental results.</p></sec><sec id="s8"><title>Cite this paper</title><p>Mahdi Hadhri,Abderazzak El Ouafi,Noureddine Barka, (2016) Hardness Profile Prediction for a 4340 Steel Spline Shaft Heat Treated by Laser Using a 3D Modeling and Experimental Validation. Journal of Materials Science and Chemical Engineering,04,9-19. doi: 10.4236/msce.2016.44002</p></sec><sec id="s9"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.66113-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Kannatey-Asibu Jr., E. (2009) Principles of Laser Materials Processing. 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