<?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">MSA</journal-id><journal-title-group><journal-title>Materials Sciences and Applications</journal-title></journal-title-group><issn pub-type="epub">2153-117X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/msa.2014.58053</article-id><article-id pub-id-type="publisher-id">MSA-47069</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>Effects of Heat Treatment on Microhardness of Some Al-Cu Alloy Prepared by Vacuum Coating</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Safdar</surname><given-names>Habibi</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>Babak</surname><given-names>Jaleh</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>Amir</surname><given-names>Namdarmanesh</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Mojtaba</surname><given-names>Shamlo</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Physics Department, Bu Ali Sina University, Hamedan, Iran</addr-line></aff><aff id="aff2"><addr-line>Physics Department, Payam Nour University, Tehran, Iran</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>safdar@basu.ac.ir(SH)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>20</day><month>06</month><year>2014</year></pub-date><volume>05</volume><issue>08</issue><fpage>491</fpage><lpage>495</lpage><history><date date-type="received"><day>16</day>	<month>March</month>	<year>2014</year></date><date date-type="rev-recd"><day>29</day>	<month>April</month>	<year>2014</year>	</date><date date-type="accepted"><day>14</day>	<month>May</month>	<year>2014</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>
	In this paper binary alloy of Al-Cu with composition Al<sub>(100-x)</sub>Cu<sub>x</sub>,
(x = 10, 15, 20) is prepared by thermal evaporation method. The prepared
samples are annealed at different temperatures and investigated by XRD and
microhardness method. XRD has been used to show amorphous state of structures
and microhrdness tester show the increase in hardness due to the increase in
amount of Al in the alloy. SEM and AFM were also used to show information about
the surface of the specimen, resulting some densification and relaxation in
these specimens.
</p></abstract><kwd-group><kwd>Al Alloy</kwd><kwd> Amorphous Materials</kwd><kwd> Microhardness</kwd><kwd> Heat Treatment</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Al and Al alloys are widely used in industry and technology such as aerospace industry because of their unique properties such as good corrosion resistance, light weight and high mechanical hardness [<xref ref-type="bibr" rid="scirp.47069-ref1">1</xref>] . However, despite their unique properties they are normally brittle. Ductility in this material can be improved by 1) addition of certain amounts of Cu and 2) by change in preparation method to avoid crystallization. Since grain boundaries and defects are the main reasons for brittleness in crystalline materials [<xref ref-type="bibr" rid="scirp.47069-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.47069-ref3">3</xref>] . On the other hand, ductility can be improved if the material is prepared in the form of amorphous structure. But amorphous phase usually is a meta-stable phase and needs some heat treatment to get more stability provided that the heat treatment is selected carefully [<xref ref-type="bibr" rid="scirp.47069-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.47069-ref5">5</xref>] . Thermal annealing of amorphous materials can generally make several changes in these alloys. Bulk and surface crystallization, and nanocrystallisation can be imposed on these materials upon thermal annealing [<xref ref-type="bibr" rid="scirp.47069-ref6">6</xref>] -[<xref ref-type="bibr" rid="scirp.47069-ref8">8</xref>] . However low temperature thermal annealing can transfer these alloys to a more stable amorphous state through structural relaxation, enhancing their hardness, ductility and other properties and also increase in density [<xref ref-type="bibr" rid="scirp.47069-ref9">9</xref>] -[<xref ref-type="bibr" rid="scirp.47069-ref11">11</xref>] . In this paper, alloy of Al<sub>(100−x)</sub>Cu<sub>x</sub> with x = 10, 15, 20 is prepared by evaporation method. Then the prepared specimens were annealed at temperatures 200, 250, and 300˚C for one hour. The value of annealing temperatures is chosen quite low as compared to crystalline temperature to avoid any crystallization due to annealing. XRD of the specimens are taken before and after each thermal annealing to show amorphous nature of the prepared and annealed specimens. Microhardness of the specimens is measured using Vickers method. SEM and AFM also are taken to observe surface morphology of the prepared samples. It is found that for x = 15 and annealing time of 200˚C the maximum hardness is obtained.</p></sec><sec id="s2"><title>2. Experimental Procedure</title><p>Al and Cu are used in the form of powder. The required amount of Al and Cu in the form of powder is used to prepare initial samples. Then by evaporation method in vacuum of 10<sup>−5</sup> torr is deposited on glass substrate. Prepared samples are annealed in vacuum of 10<sup>−3</sup> torr at temperatures 200, 250 and 300˚C for 1 hour. Structure is characterized using X ray diffraction (XRD) with Cu-K<sub>a</sub> radiation with wavelength = 1.5405 angstrom. Microhardness measurements are done using Buehler microhardness tester, with diamond pyramid, load of 10 grams and pressing time of 15 seconds. More than 10 measurements are performed and their average is considered. Jeol SEM is used to observe surface morphology and AFM is used to observe surface roughness of the samples.</p></sec><sec id="s3"><title>3. Results and Discussions</title><sec id="s3_1"><title>3.1. XRD Study</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref> show the XRD patterns of all prepared specimens before and after thermal annealing. It clearly shows broad halos typical for an amorphous structure. Specimens with compositions Al<sub>90</sub>Cu<sub>10</sub> and Al<sub>80</sub>Cu<sub>20</sub> show some crystalline phases, but the specimen with composition Al<sub>85</sub>Cu<sub>15</sub> seems to be quite amorphous in structure without presence of any crystalline phase.</p></sec><sec id="s3_2"><title>3.2. Microhardness Measurements</title><p>Microhardness of the specimens is measured before and after thermal annealing. <xref ref-type="fig" rid="fig2">Figure 2</xref> shows the obtained microhardness values as a function of annealing temperatures.</p><p>It is observed that there is some increase in hardness of the all specimens due to thermal annealing, which can be related to densification of specimens. It can be considered that increase in hardness due to annealing is highest for sample with composition Al<sub>85</sub>Cu<sub>15</sub> annealed at 200˚C which may be related to its amorphous structure. Thermal annealing of other specimens cannot make such amount of increase in the microhardness.</p></sec><sec id="s3_3"><title>3.3. SEM Study</title><p>We have studied the sample with composition Al<sub>85</sub>Cu<sub>15</sub> because of its good increase in amount of microhardness after thermal annealing. <xref ref-type="fig" rid="fig3">Figure 3</xref> shows micrographs of specimen obtained by SEM.</p><p>It shows clearly that the inter-atomic distances are decreasing or, one can say that the density of the specimen is increases upon thermal annealing which is in good agreement with our earlier result [<xref ref-type="bibr" rid="scirp.47069-ref11">11</xref>] .</p></sec><sec id="s3_4"><title>3.4. AFM Results</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref> shows the surface roughness of the specimen by using AFM.</p><p>It shows that upon annealing the surface of the specimen becomes smoother due to structural relaxation occurred in the specimen after annealing. This phenomenon which arises due to low temperature thermal annealing can increase the density of the specimens and increase its hardness.</p></sec></sec><sec id="s4"><title>4. Conclusion</title><p>The effects of thermal annealing on prepared amorphous samples with composition Al<sub>100−x</sub>Cu<sub>x</sub> were studied using XRD, microhardness tester, SEM and AFM. It is observed that sample with composition Al<sub>85</sub>Cu<sub>15</sub> can give</p><fig-group id="fig1"> <caption><title>Figure 1</title><p> XRD patterns of samples before and after thermal annealing for different alloy compositions a: (Al<sub>80</sub>Cu<sub>20</sub>), b: (Al<sub>85</sub>Cu<sub>15</sub>), c: (Al<sub>90</sub>Cu<sub>10</sub>)</p></caption><fig id ="fig1_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\6397b403-c1bd-4a1c-a007-862c59334557.png"/></fig><fig id ="fig1_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\91c114fc-34c3-4fa8-a2f4-4a92edb2039f.png"/></fig><fig id ="fig1_3"><label>(c)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\830e78ba-66b4-48b7-a01d-c9c04428769a.png"/></fig></fig-group><fig-group id="fig2"> <caption><title>Figure 2</title><p> Microhardnes of the samples as a function of annealing temperatures for different alloy compositions, a: (Al<sub>80</sub>Cu<sub>20</sub>), b: (Al<sub>85</sub>Cu<sub>15</sub>) and c: (Al<sub>90</sub>Cu<sub>10</sub>)</p></caption><fig id ="fig2_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\1fa806a8-daad-463e-967a-1408cc30025e.png"/></fig><fig id ="fig2_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\8f31024e-5e99-423a-a3a8-ae61eba86b45.png"/></fig><fig id ="fig2_3"><label>(c)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\bf4a991c-2d91-4e97-8580-aa0bab7e0a48.png"/></fig></fig-group><fig-group id="fig3"><caption><title>Figure 3</title><p> SEM micrographs of the sample Al<sub>85</sub>Cu<sub>15</sub> before (a) and after thermal annealing b (200), c (250) and d (300˚C)</p></caption><fig id ="fig3_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\206c8fd8-f2bd-4963-ac8f-8d0df4116ce7.png"/></fig><fig id ="fig3_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\30f86038-4d5e-471d-809d-97b89202186b.png"/></fig><fig id ="fig3_3"><label>(c)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\26d0e2c3-92a3-4724-8ae5-789102aa268a.png"/></fig><fig id ="fig3_4"><label>(d)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\dc396a3d-6fe2-4699-af09-3e29fffb5062.png"/></fig></fig-group><fig-group id="fig4"><caption><title>Figure 4</title><p> AFM of the sample Al<sub>85</sub>Cu<sub>15</sub> before (a) and after thermal annealing b (200), c (250) and d (300˚C)</p></caption><fig id ="fig4_1"><label>(a)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\73ded12a-dd48-4ccb-80ca-9693917da66d.png"/></fig><fig id ="fig4_2"><label>(b)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\fc94493f-fd63-4ef7-9cac-77cee6261ac4.png"/></fig><fig id ="fig4_3"><label>(c)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\4f75c54e-ecd3-43e0-8583-501f9e164c2e.png"/></fig><fig id ="fig4_4"><label>(d)</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\2-7701238x\fc73d247-8b99-437b-9287-50931f3896f4.png"/></fig></fig-group><p>the best amorphous structure. Thermal annealing at temperature 200 C for one hour can make maximum increase in microhardness of the specimen. And thermal annealing at selected temperatures can relax the specimen and densify it without occurrence of crystallization, hence better ductility can be achieved.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.47069-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">JIANG, W.H. AND ATZMON, M. (2006) MECHANICALLY-ASSISTED NANOCRYSTALLIZATION AND DEFECTS IN AMOURPHOUS ALLOYS, SCRIPTA MATERIALIA, 54, 333-336. HTTP://DX.DOI.ORG/10.1016/J.SCRIPTAMAT.2005.09.052</mixed-citation></ref><ref id="scirp.47069-ref2"><label>2</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>WANG</surname><given-names> X.F.</given-names></name>,<name name-style="western"><surname> WU</surname><given-names> X.Q.</given-names></name>,<name name-style="western"><surname> LIN</surname><given-names> J.G. </given-names></name>,<name name-style="western"><surname> MA</surname><given-names> M. </given-names></name>,<etal>et al</etal>. (<year>2007</year>)<article-title>THE INFLUENCE OF HEAT TREATMENT ON THE CORROSION BEHAVIOUR OF AS-SPUN AMORPHOUS AL88NI6LA6 ALLOY IN 0.01 M NACL SOLUTION</article-title><source> MATERIALS LETTERS</source><volume> 61</volume>,<fpage> 1715</fpage>-<lpage>1717</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/J.MATLET.2006.07.186</pub-id></mixed-citation></ref><ref id="scirp.47069-ref3"><label>3</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>WU</surname><given-names> X.Q. </given-names></name>,<name name-style="western"><surname> XIE</surname><given-names> C.Q. </given-names></name>,<etal>et al</etal>. (<year>2008</year>)<article-title>INFLUENCE OF CRYSTALLIZATION ON CORROSION RESISTANCE OF AL86NI6LA6CU2 AMORPHOUS ALLOY</article-title><source> JOURNAL OF RARE EARTHS</source><volume> 26</volume>,<fpage> 745</fpage>-<lpage>748</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/S1002-0721(08)60175-1</pub-id></mixed-citation></ref><ref id="scirp.47069-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">TAN, C.-G., JIANG, W.-J., WU, X.-Q., WANG, X.-F. AND LIN, J.-G. (2007) EFFECT OF CRYSTALLIZATION ON CORROSION RESISTANCE OF CU22.5TI30ZR11.5NI6 BULK AMORPHOUS ALLOY. TRANSACTIONS OF NONFERROUS METALS SOCIETY OF CHINA, 17, 751754.</mixed-citation></ref><ref id="scirp.47069-ref5"><label>5</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>JIANG</surname><given-names> W.H.</given-names></name>,<name name-style="western"><surname> PINKERTON</surname><given-names> F.E. </given-names></name>,<name name-style="western"><surname> ATZMON</surname><given-names> M. </given-names></name>,<etal>et al</etal>. (<year>2003</year>)<article-title>DEFORMATION-INDUCED NANOCRYSTALLIZATION IN AN AL-BASED AMORPHOUS ALLOY AT A SUBAMBIENT TEMPERATURE</article-title><source> SCRIPTA MATERIALIA</source><volume> 48</volume>,<fpage> 1195</fpage>-<lpage>1200</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/S1359-6462(02)00568-7</pub-id></mixed-citation></ref><ref id="scirp.47069-ref6"><label>6</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>NASIR</surname><given-names> M.</given-names></name>,<name name-style="western"><surname> KHAN</surname><given-names> M. A. M.</given-names></name>,<name name-style="western"><surname> HUSAIN</surname><given-names> M. </given-names></name>,<name name-style="western"><surname> ZULFEQUAR</surname><given-names> M. </given-names></name>,<etal>et al</etal>. (<year>2011</year>)<article-title>THERMAL PROPERTIES OF SE100-XZNX GLASSY SYSTEM</article-title><source> MATERIALS SCIENCES AND APPLICATION</source><volume> 2</volume>,<fpage> 289</fpage>-<lpage>298</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.4236/MSA.2011.25038</pub-id></mixed-citation></ref><ref id="scirp.47069-ref7"><label>7</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>KAMRUZZAMAN</surname><given-names> M.</given-names></name>,<name name-style="western"><surname> ABU SAYEM KARAL</surname><given-names> M.</given-names></name>,<name name-style="western"><surname> SAHA</surname><given-names> D.K. </given-names></name>,<name name-style="western"><surname> KHAN</surname><given-names> F.A. </given-names></name>,<etal>et al</etal>. (<year>2012</year>)<article-title>KAMRUZZAMAN, M., ABU SAYEM KARAL, M., SAHA, D.K. AND KHAN, F.A.  CRYSTALLIZATION, TRANSPORT AND MAGNETIC PROPERTIES OF THE AMORPHOUS (FE1-XMNX)75P15C10 ALLOYS</article-title><source> JOURNAL OF CRYSTALLIZATION PROCESS AND TECHNOLOGY</source><volume> 2</volume>,<fpage> 105</fpage>-<lpage>110</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.47069-ref8"><label>8</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>GOGEBAKAN</surname><given-names> M. </given-names></name>,<name name-style="western"><surname> OKUMUS</surname><given-names> M. </given-names></name>,<etal>et al</etal>. (<year>2009</year>)<article-title>GOGEBAKAN, M. AND OKUMUS, M.  STRUCTURE AND CRYSTALLIZATION KINETICS OF AMORPHOUS AL-NI-SI ALLOY</article-title><source> MATERIALS SIENCE-POLAND</source><volume> 37</volume>,<fpage> 79</fpage>-<lpage>87</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.47069-ref9"><label>9</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>MUNOZ-MORRIS</surname><given-names> M.A. </given-names></name>,<name name-style="western"><surname> MORRIS</surname><given-names> D.G. </given-names></name>,<etal>et al</etal>. (<year>2010</year>)<article-title>SEVERE PLASTIC DEFORMATION PROCESSING OF AL-CU-LI ALLOY FOR ENHANCING STRENGTH WHILE MAINTAINING DUCTILITY</article-title><source> SCRIPTA MATERIALIA</source><volume> 63</volume>,<fpage> 304</fpage>-<lpage>307</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/J.SCRIPTAMAT.2010.04.022</pub-id></mixed-citation></ref><ref id="scirp.47069-ref10"><label>10</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>GAO</surname><given-names> M.C.</given-names></name>,<name name-style="western"><surname> ET AL. </surname><given-names>  </given-names></name>,<etal>et al</etal>. (<year>2008</year>)<article-title>DEVELOPMENT OF FCC-AL NANOCRYSTALS IN AL-NI-GD METALLIC GLASSES DURING CONTINUOUS HEATING DSC SCAN</article-title><source> MATERIALS SCIENCE AND ENGINEERING A</source><volume> 485</volume>,<fpage> 532</fpage>-<lpage>543</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/J.MSEA.2007.08.009</pub-id></mixed-citation></ref><ref id="scirp.47069-ref11"><label>11</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>HABIBI</surname><given-names> S. </given-names></name>,<name name-style="western"><surname> SOUDM</surname><given-names></given-names></name>,<name name-style="western"><surname> M. </surname><given-names>  </given-names></name>,<etal>et al</etal>. (<year>2004</year>)<article-title>STUDY OF STRUCTURAL RELAXATION IN ALLOYS OF METALLIC GLASSES</article-title><source> SURFACE AND INTERFACE ANALYSIS</source><volume> 36</volume>,<fpage> 929</fpage>-<lpage>930</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1002/SIA.1802</pub-id></mixed-citation></ref></ref-list></back></article>