<?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">JMMCE</journal-id><journal-title-group><journal-title>Journal of Minerals and Materials Characterization and Engineering</journal-title></journal-title-group><issn pub-type="epub">2327-4077</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jmmce.2015.31001</article-id><article-id pub-id-type="publisher-id">JMMCE-52698</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><subject> Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Experimental Studies of Self Healing Behaviour of Under-Aged Al-Mg-Si Alloys and 60Sn-40Pb Alloy Reinforced Aluminium Metal-Metal Composites
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>enneth</surname><given-names>Kanayo Alaneme</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Oluwafemi</surname><given-names>Isaac Omosule</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Metallurgical and Materials Engineering, Federal University of Technology, Akure,
Nigeria</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>kalanemek@yahoo.co.uk(EKA)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>26</day><month>12</month><year>2014</year></pub-date><volume>03</volume><issue>01</issue><fpage>1</fpage><lpage>8</lpage><history><date date-type="received"><day>31</day>	<month>October</month>	<year>2014</year></date><date date-type="rev-recd"><day>2</day>	<month>December</month>	<year>2014</year>	</date><date date-type="accepted"><day>15</day>	<month>December</month>	<year>2015</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>
 
 
  Experimental studies to demonstrate self healing potentials of Al-Mg-Si alloy were undertaken in this research work. Self healing exploring secondary precipitation in the Al-Mg-Si alloy and use of low melting metallic alloy reinforcement (60Sn-40Pb alloy) were used as basis for the investigation. For the precipitation study, the Al-Mg-Si alloy was under-aged at temperature of 160
  <sup>o</sup>C for 10 minutes and then subjected to second step ageing treatment at four different temperatures within the range of 25
  <sup>o</sup>C and 70
  <sup>o</sup>C. In the 60Sn-40Pb alloy reinforced Al-Mg-Si alloy study, the samples were prepared in pre-cracked state and then subjected to healing heat-treatment at 250
  <sup>o</sup>C. For all cases tensile test and healing efficiency was used to analyze the results generated. It was observed that a second step thermal ageing at 50
  <sup>o</sup>C resulted in peak improvement in tensile strength, yield strength, toughness and percent elongation while ageing above this temperature lead to a drop in the tensile properties in comparison to that of the sample not subjected to a second ageing treatment. Also the use of 60Sn-40Pb alloy as reinforcement in the Al-Mg-Si alloy resulted in a healing efficiency of 91% after pre-cracking and heat-treatment. The satisfactory bonding between the 60Sn-40Pb alloy and the Al-Mg-Si alloy matrix contributed to the high healing efficiency observed.
 
</p></abstract><kwd-group><kwd>Aluminium Alloys</kwd><kwd> Secondary Precipitation</kwd><kwd> Self Healing Metals</kwd><kwd> Healing Efficiency</kwd><kwd> Mechanical Damage</kwd><kwd> Biomimetics</kwd><kwd> Low Melting Point Reinforcement</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Self healing materials are bio-inspired materials designed to mimic the behaviour of biological systems which have the capacity of self healing after undergoing some form of damage (such as blood clotting to seal up an open wound or cut) [<xref ref-type="bibr" rid="scirp.52698-ref1">1</xref>] . In materials systems, the aim is to be able to restore a substantial level of the original functionality (properties) of the material by a self repair process after it has undergone some form of damage [<xref ref-type="bibr" rid="scirp.52698-ref2">2</xref>] . The damage could be in form of micro-cracks, void or flaws developed from mechanical, thermal and other forms of environmental or in-service factors [<xref ref-type="bibr" rid="scirp.52698-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.52698-ref4">4</xref>] .</p><p>The design of self healing materials has become attractive since materials designed using traditional materials design concept of “damage prevention” do eventually fail in service due to damage development. The damage management philosophy explored in the design of self healing materials comes to terms with the inevitability of damage occurring and consequently materials functionality waning [<xref ref-type="bibr" rid="scirp.52698-ref5">5</xref>] . Phenomena such as wear, residual stress development, micro-crack formation, and corrosion are among characteristics processed which can induce materials damage [<xref ref-type="bibr" rid="scirp.52698-ref6">6</xref>] . The damage management design philosophy pursues sustaining materials functionality and properties at levels not below 70% - 80% of its original value through the process of self repair which is triggered once damage occurs in the materials [<xref ref-type="bibr" rid="scirp.52698-ref2">2</xref>] . A wide range of benefits can accrue from the use of this design concept if it can be applied at commercial levels. It has the potential of reducing cost of maintenance if components are made with self healing materials. This will also reflect in reduced production cost and down time of various industrial processes requiring the repair of damaged parts central to its production operations. This would in turn translate to prolonged service life of components and consistent service performance [<xref ref-type="bibr" rid="scirp.52698-ref7">7</xref>] . There is also the attraction of low energy requirement for developing self healing materials and low design cost of fabricating or incorporating self healing agents in traditional materials [<xref ref-type="bibr" rid="scirp.52698-ref8">8</xref>] .</p><p>Despite the huge promise of self healing concept of materials design, the science of self healing is still not thoroughly understood and grossly underutilized [<xref ref-type="bibr" rid="scirp.52698-ref9">9</xref>] . Presently, the most successful application of the self healing concept has been in the development of self healing polymers and polymer based composites [<xref ref-type="bibr" rid="scirp.52698-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.52698-ref11">11</xref>] . This is on account of the high rate of diffusion in polymers due to the presence of cross molecular bonds which facilitates diffusion of healing agents to fill up voids or micro-cracks [<xref ref-type="bibr" rid="scirp.52698-ref10">10</xref>] . In ceramics, some success has been recorded in the development of self healing ceramic systems [<xref ref-type="bibr" rid="scirp.52698-ref12">12</xref>] [<xref ref-type="bibr" rid="scirp.52698-ref13">13</xref>] . However, in metallic material systems which still happen to be the most widely utilized material class, there are still some teething problems [<xref ref-type="bibr" rid="scirp.52698-ref7">7</xref>] . In metals, diffusion rates are significantly lower compared to polymers due to the strong bonds between metal atoms which thus makes self healing much difficult to achieve in metallic systems [<xref ref-type="bibr" rid="scirp.52698-ref14">14</xref>] .</p><p>Currently, there are three main directions which have been taken in the development of self-healing metallic systems [<xref ref-type="bibr" rid="scirp.52698-ref14">14</xref>] . The formation of under aged precipitates in alloys which still retains a substantial amount of solutes in solid solution which can diffuse as secondary precipitates to close defects created by plastic deformation when treated at lower temperatures thus immobilize further defect growth [<xref ref-type="bibr" rid="scirp.52698-ref15">15</xref>] . Materials or alloy matrix reinforcement with microfibers or wires made of a shape-memory alloy (SMA) is another approach currently explored [<xref ref-type="bibr" rid="scirp.52698-ref16">16</xref>] . If the composite undergoes crack formation, heating the material will activate the shape recovery feature of the SMA wires which then shrink applying compressive force at the cracks and close the cracks [<xref ref-type="bibr" rid="scirp.52698-ref17">17</xref>] . The third approach is by incorporating a low-melting temperature alloy that serves as a healing agent in a high- melting temperature alloy which serves as a matrix [<xref ref-type="bibr" rid="scirp.52698-ref14">14</xref>] . When a crack develops in the composites, by heating to the healing temperature the low-melting point alloy embedded in the matrix becomes completely molten, and by capillary pressure and surface tension, flows out and fill in the crack. As the temperature is reduced, the low- melting point healing alloy solidifies and seals the crack [<xref ref-type="bibr" rid="scirp.52698-ref7">7</xref>] .</p><p>The study of these self healing approaches in metallic systems is still very limited and is still in need of further investigations to develop a robust science of self healing in metallic systems. In the present study, experimental investigation of self healing in under-aged Al-Mg-Si alloys and Al-Mg-Si alloy reinforced with 60Sn- 40Pb low melting alloy is reported.</p></sec><sec id="s2"><title>2. Materials and Methods</title><sec id="s2_1"><title>2.1. Materials</title><p>The materials used in this research work are: Al-Mg-Si alloy as received in the form of slabs with chemical compositions as presented in <xref ref-type="table" rid="table1">Table 1</xref> and commercial grade tin lead based solders (60Sn-40Pb).</p></sec><sec id="s2_2"><title>2.2. Self Healing Experimental Studies</title><sec id="s2_2_1"><title>2.2.1. Secondary Precipitation Approach</title><p>Precipitation induced self healing was studied following an approach similar to that of Hauta Kangas et al. [<xref ref-type="bibr" rid="scirp.52698-ref18">18</xref>] . The Al-Mg-Si alloy used for the study was machined to specifications for tensile testing with gauge length and diameter of 30 mm and 5 mm respectively. The samples were subjected to solution heat-treatment at 500˚C for 1 hour, and then quenched in water. The samples were then thermally aged at 160˚C for 10 minutes followed by rapid cooling in a water bath. A second ageing treatment was then performed on the test samples at temperatures of 25˚C, 40˚C, 50˚C, 60˚C, and 70˚C for period of 12 hours before quenching in water. Thereafter, the samples were subjected to tensile loading to fracture. The tensile testing was performed at a strain rate of 10<sup>−3</sup>/s and with testing procedures in accordance with ASTM 8M-91 standard [<xref ref-type="bibr" rid="scirp.52698-ref19">19</xref>] . The tests were carried out in triplicates to guarantee the reliability of the results obtained.</p></sec><sec id="s2_2_2"><title>2.2.2. Use of Low Melting Point Reinforcement</title><p>For studies on healing by incorporation of low melting alloy, the tensile samples (<xref ref-type="fig" rid="fig1">Figure 1</xref>) were incorporated with the 60Sn-40Pb based solders fitted within the 3 mm holes bored into them. Three samples of the tensile test specimens had 1 mm holes drilled in the surface of the sample to pierce the low melting point 60Sn-40Pb alloy embedded within the Al matrix. This was done to simulate crack formation (mechanical damage) on the Al based composite. The samples were afterwards subjected to tensile loading to fracture and the tensile properties evaluated. These set of pre-cracked samples subjected to tensile testing were referred to as damaged samples. Another set of pre-cracked 60Sn-40Pb reinforced Al-Mg-Si alloy based composite samples were prepared but this time wrapped with Aluminium foil and heated at a temperature of 250˚C for 10 minutes before air cooling. The samples were then subjected to tensile testing to fracture and its tensile properties evaluated from the stress-</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Chemical composition of the Al-Mg-Si alloy</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >AA6063</th><th align="center" valign="middle" >Si</th><th align="center" valign="middle" >Cu</th><th align="center" valign="middle" >Mn</th><th align="center" valign="middle" >Mg</th><th align="center" valign="middle" >Zn</th><th align="center" valign="middle" >Ti</th><th align="center" valign="middle" >Al</th></tr></thead><tr><td align="center" valign="middle" >Composition (%)</td><td align="center" valign="middle" >0.56</td><td align="center" valign="middle" >0.07</td><td align="center" valign="middle" >0.05</td><td align="center" valign="middle" >0.65</td><td align="center" valign="middle" >0.04</td><td align="center" valign="middle" >0.02</td><td align="center" valign="middle" >bal</td></tr></tbody></table></table-wrap><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Machined Al-Mg-Si alloy samples for the self healing experiment showing (a) The tensile test specimen configuration; (b) tensile sample with drilled hole; and (c) tensile test sample after incorporation of the 60Sn-40Pb solder reinforcement.</title></caption><fig id ="fig1_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x8.png"/></fig><fig id ="fig1_2"><label> (c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x7.png"/></fig><fig id ="fig1_3"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x6.png"/></fig></fig-group><p>strain plots generated from the testing. The samples were referred to as healed samples. The wrapping with Alu- minium foil was done in other to forestall the draining of the 60Sn-40Pb solder through the drilled hole during the heating process. Finally tensile testing was also conducted on another set of the 60Sn-40Pb reinforced Al- Mg-Si alloy samples which were not pre-cracked; which for the purpose of the experiment were referred to as virgin samples. For all test cases the tensile test was carried out at room temperature with the aid of a universal tensile testing machine. The tensile testing was performed at a strain rate of 10<sup>−3</sup>/s and with testing procedures in accordance with ASTM 8M-91 standard [<xref ref-type="bibr" rid="scirp.52698-ref19">19</xref>] . Repeat tests were performed for all test cases to ensure repeatability and reliability of the data generated.</p><p>The self healing efficiency achieved using the 60Sn-40Pb reinforced Al-Mg-Si alloy based composites was determined using the tensile strength based criterion given by the relation [<xref ref-type="bibr" rid="scirp.52698-ref20">20</xref>] :</p><disp-formula id="scirp.52698-formula85"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-2710272x9.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2710272x10.png" xlink:type="simple"/></inline-formula> is the tensile strength of the virgin specimen and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2710272x11.png" xlink:type="simple"/></inline-formula> is the tensile strength of the healed specimen.</p></sec></sec><sec id="s2_3"><title>2.3. Microstructural Examination</title><p>The microstructures of the 60Sn-40Pb reinforced Al-Mg-Si alloy samples were examined in the as-polished and etched conditions using a metallurgical microscope. The etching of the samples was performed by swabbing using Kellers reagent (consisting of 190 ml distilled water, 5 ml HNO<sub>3</sub>, 3 ml HCl, 2 ml HF).</p></sec></sec><sec id="s3"><title>3. Results and Discussion</title><sec id="s3_1"><title>3.1. Tensile Properties of Precipitation Induced Healing Samples</title><p>The tensile properties of the under-aged samples subjected to a second low temperature ageing treatment within the range of 25˚C and 70˚C are presented in <xref ref-type="fig" rid="fig2">Figure 2</xref>. It is observed from <xref ref-type="fig" rid="fig2">Figure 2</xref>(a) that the samples subjected secondary thermal ageing at 40˚C and 50˚C had higher tensile strength values compared with the sample at room temperature with peak tensile strength observed for second ageing treatment carried out at 50˚C. It is also observed that ageing above 50˚C resulted in reduction in the tensile strength values lower than that observed for the primary aged sample. The same trend was also observed for the yield strength (<xref ref-type="fig" rid="fig2">Figure 2</xref>(b)) and the toughness (<xref ref-type="fig" rid="fig2">Figure 2</xref>(c)). Similar trend with that of the strength parameters and toughness was followed by the % Elongation (<xref ref-type="fig" rid="fig2">Figure 2</xref>(d)) with the exception of the sample treated at 60˚C which had % elongation values higher than that of the primary aged sample (sample that remained at room temperature). This clearly shows that strength, ductility and toughness improvement can be induced in under aged Al-Mg-Si alloy by proper selection of the secondary ageing temperature. The improvement in mechanical properties arises from the secondary precipitation of Mg<sub>2</sub>Si from the under aged Al-Mg-Si alloy which still contains solute atoms in excess of the equilibrium concentration. The secondary precipitates are formed at sites referred to as precipitate free zones (PFZ) which are nucleation sites within the matrix where precipitation did not occur during the under ageing primary precipitation treatment. The process of secondary precipitation is reported to be equally accompanied by the process of grain refinement [<xref ref-type="bibr" rid="scirp.52698-ref21">21</xref>] . The results show that the optimum improvement in mechanical properties from the secondary precipitation process is achieved using a secondary ageing temperature of 50˚C. Ageing above this temperature is observed to result in impoverishment of the mechanical properties of the Al-Mg-Si alloy. This is an indicator that processing Al-Mg-Si alloy in the under-aged condition can help in cases where mechanical damage results from service use. A second ageing treatment can be used to recover substantially a part of the mechanical properties so as to prolong the performance and service life of the components or parts.</p></sec><sec id="s3_2"><title>3.2. Tensile Property Results for Samples Incorporated with Low Melting 60Sn-40Pb Alloy</title><p>The tensile properties of the Al-Mg-Si alloy samples incorporated with low melting 60Sn-40Pb alloys are presented in <xref ref-type="table" rid="table2">Table 2</xref>. It is observed that the pre-cracked sample (damaged sample) had tensile strength value of 43.4 MPa which is 20% reduction from that of the virgin sample with tensile strength of 54.5 MPa. Conducting the self healing treatment at 250˚C for 10 minutes followed by air cooling, resulted in tensile strength increase from 43.4 MPa (damaged state) to 49.4 MPa (healed state). In comparison with the tensile strength of the virgin</p><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Tensile properties of the Al-Mg-Si alloy subjected to double ageing treatment showing (a) Tensile Strength; (b) Yield Strength; (c) Toughness; and (d) % Elongation.</title></caption><fig id ="fig2_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x12.png"/></fig><fig id ="fig2_2"><label>(c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x13.png"/></fig><fig id ="fig2_3"><label>(d)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x14.png"/></fig><fig id ="fig2_4"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x15.png"/></fig></fig-group><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Optical micrograph of (a) as-polished; and (b) etched sample of the Al-Mg-Si alloy reinforced with 60Sn-40Pb low melting alloy.</title></caption><fig id ="fig3_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x16.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-2710272x17.png"/></fig></fig-group><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Tensile strength and self healing efficiency data for the 60Sn-40Pb reinforced Al-Mg-Si alloy based composite</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Tensile Strength (MPa) (Virgin Sample)</th><th align="center" valign="middle" >Tensile Strength (MPa) (Damaged Sample)</th><th align="center" valign="middle" >Tensile Strength (MPa) (Healed Sample)</th><th align="center" valign="middle" >Self Healing Efficiency <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-2710272x18.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >54.5 &#177; 0.15</td><td align="center" valign="middle" >43.4 &#177; 0.30</td><td align="center" valign="middle" >49.4 &#177; 0.50</td><td align="center" valign="middle" >91%</td></tr></tbody></table></table-wrap><p>sample and the use of Equation (1), a healing efficiency of 91% was achieved. The experimental results are testaments to the promise that self healing (using a low melting alloy as reinforcement) holds to restoring mechanical damage of metallic materials in service. This is achievable particularly if good wetting between the matrix and reinforcement is attained. In the present case, it can be observed from <xref ref-type="fig" rid="fig3">Figure 3</xref> that satisfactory bonding between the 60Sn-40Pb solder (dark phase) and the Al-Mg-Si alloy matrix (lighter phase) was achieved as the matrix/reinforcement interface show considerable closure.</p></sec></sec><sec id="s4"><title>4. Conclusions</title><p>Experimental studies to demonstrate self healing potentials of Al-Mg-Si alloy by exploring secondary precipitation and use of low melting metallic alloy reinforcement (60Sn-40Pb alloy) were investigated. From the results the following conclusions are drawn:</p><p>・ Second step thermal ageing at 50˚C resulted in peak improvement in tensile strength, yield strength, toughness and percent elongation while ageing above this temperature lead to a drop in the tensile properties in comparison to that of the sample not subjected to a second ageing treatment.</p><p>・ The use of 60Sn-40Pb alloy as reinforcement in the Al-Mg-Si alloy resulted in a healing efficiency of 91% after pre-cracking and heat-treatment. Satisfactory bonding between the 60Sn-40Pb alloy and the Al-Mg-Si alloy matrix contributed to the high healing efficiency.</p></sec><sec id="s5"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.52698-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Van der Zwaag, S. (2007) Self-Healing Materials. An Alternative Approach to 20th Centuries of Materials Science. 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