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<Article>
<Journal>
				<PublisherName>Ferdowsi University of Mashhad Press</PublisherName>
				<JournalTitle>Journal Of Metallurgical and Materials Engineering</JournalTitle>
				<Issn>2008-7462</Issn>
				<Volume>28</Volume>
				<Issue>1</Issue>
				<PubDate PubStatus="epublish">
					<Year>2017</Year>
					<Month>02</Month>
					<Day>19</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Fabrication and Study of Wear Properties of AA8090 Composite Reinforced with SiC Particles after Precipitation Hardening with Directional Quenching</ArticleTitle>
<VernacularTitle>Fabrication and Study of Wear Properties of AA8090 Composite Reinforced with SiC Particles after Precipitation Hardening with Directional Quenching</VernacularTitle>
			<FirstPage>87</FirstPage>
			<LastPage>98</LastPage>
			<ELocationID EIdType="pii">31510</ELocationID>
			
<ELocationID EIdType="doi">10.22067/ma.v28i1.34881</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Amir</FirstName>
					<LastName>Kebriyaei</LastName>
<Affiliation>School of Metallurgy and Materials Engineering, Iran University of Science and Technology, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Hassan</FirstName>
					<LastName>Saghafian</LastName>
<Affiliation>School of Metallurgy and Materials Engineering, Iran University of Science and Technology, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Shamseddin</FirstName>
					<LastName>Mirdamadi</LastName>
<Affiliation>School of Metallurgy and Materials Engineering, Iran University of Science and Technology, Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2014</Year>
					<Month>05</Month>
					<Day>05</Day>
				</PubDate>
			</History>
		    <Abstract>AA8090 is an extra light and deformable group of lithium containing aluminum alloys which have recently replaced some aerospace aluminum alloys, such as 2000 and 7000 series, due to their higher elastic modulus and lower specific weight. In this study, AA8090 matrix composites containing 3, 6 and 9 vol.% SiC were cast using a modified stir casting method. The casting billets were deformed though a hot extrusion operation, followed by a precipitation hardening treatment (T6) with directional quenching and aging at 190 °C. Wear tests were conducted before and after the precipitation hardening (at the peak hardness aging time) using the pin-on-disc method at loads of 10, 20 and 30 N. All samples exhibited a mild wear at 10 and 20 N wear loads, which turned into a sever wear at 30 N. It was shown that increasing the SiC content in the composite samples reduces the wear rate. Also, the wear results after precipitation hardening indicated a decrease in the wear rate only at the wear loads of 10 and 20 N. At the wear load of 30 N, the wear rate increased after precipitation hardening. This behavior was attributed to a transition in the wear mechanism from abrasive to adhesive by increasing the load.</Abstract>
			<OtherAbstract Language="FA">AA8090 is an extra light and deformable group of lithium containing aluminum alloys which have recently replaced some aerospace aluminum alloys, such as 2000 and 7000 series, due to their higher elastic modulus and lower specific weight. In this study, AA8090 matrix composites containing 3, 6 and 9 vol.% SiC were cast using a modified stir casting method. The casting billets were deformed though a hot extrusion operation, followed by a precipitation hardening treatment (T6) with directional quenching and aging at 190 °C. Wear tests were conducted before and after the precipitation hardening (at the peak hardness aging time) using the pin-on-disc method at loads of 10, 20 and 30 N. All samples exhibited a mild wear at 10 and 20 N wear loads, which turned into a sever wear at 30 N. It was shown that increasing the SiC content in the composite samples reduces the wear rate. Also, the wear results after precipitation hardening indicated a decrease in the wear rate only at the wear loads of 10 and 20 N. At the wear load of 30 N, the wear rate increased after precipitation hardening. This behavior was attributed to a transition in the wear mechanism from abrasive to adhesive by increasing the load.</OtherAbstract>
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			<Object Type="keyword">
			<Param Name="value">AA8090</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Composite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Age Hardening</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">directional Quenching</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">wear</Param>
			</Object>
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<ArchiveCopySource DocType="pdf">https://jmme.um.ac.ir/article_31510_5b9a8d01164ae511a4d6f8c83b041556.pdf</ArchiveCopySource>
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