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    <title>Fracture and Fatigue of the Inertia Welded Titanium Alloy Ti-6Al-2Sn-4Zr-6Mo</title>
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      <item>TN</item>
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    <divisions>10col_ephy</divisions>
    <suggestions>Old embargo - embargo expired 1st Feb 2015

As thesis concerns Rolls Royce option C for 15 years default applied (until Feb 2030). </suggestions>
    <abstract>In this thesis the microstructure, microhardness, and mechanical properties of the α/β alloy Ti-6Al-2Sn-4Zr-6Mo inertia welded to itself using a variety of parameters were assessed. The resultant welds were compared to the parent in both the as-welded and post weld heat treated condition (640°C / 2 hours). The mechanical properties of later welds were evaluated at three different temperatures and R ratios. Welding at process parameters within a defined window has produced welds with satisfactory mechanical properties. These welds are harder than the parent in both the as welded and Post Weld Heat Treated (PWHT) conditions. Post Weld Heat Treating of these welds at 640°C for two hours results in the re-precipitation of secondary α throughout the Central Weld Zone and Heat Affected Zone, leading to a local microhardness increase. The weld is deduced to be more resistant to fatigue crack initiation than the parent material, with all low cycle fatigue samples failing in the parent. The fatigue crack growth resistance of welded and parent samples was comparable at all temperatures tested, with no effects of dwell observed. However, a static (intergranular) mode of failure at room temperature caused rapid acceleration of crack growth at higher ∆K values as the peak value of K approaches the fracture toughness. Hence, the onset of final failure in fatigue crack growth tests is strongly dependent on the R ratio, but at lower ∆K values, crack growth rates are independent of R ratio.</abstract>
    <date>2011-07</date>
    <date_tp>2011-01</date_tp>
    <date_type>graduation</date_type>
    <ub_pri_lang>eng</ub_pri_lang>
    <ub_doc_source>author</ub_doc_source>
    <ub_doc_source_spot>checked</ub_doc_source_spot>
    <copyright_status>This unpublished thesis/dissertation is copyright of the author and/or third parties. The intellectual property rights of the author or third parties in respect of this work are as defined by The Copyright Designs and Patents Act 1988 or as modified by any successor legislation. Any use made of information contained in this thesis/dissertation must be in accordance with that legislation and must be properly acknowledged. Further distribution or reproduction in any format is prohibited without the permission of the copyright holder.</copyright_status>
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      <item>Christopher James Miles</item>
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    <full_text_status>restricted</full_text_status>
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    <department>School of Metallurgy and Materials</department>
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