<?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.2016.47003</article-id><article-id pub-id-type="publisher-id">MSCE-68961</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>
 
 
  Property and Oxidation Behaviours of (Mo,Cr)Si2 + ZrO2 Composite Produced by Pressure-Less Sintering
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Yiming</surname><given-names>Yao</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>Erik</surname><given-names>Ström</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>Xin-Hai</surname><given-names>Li</given-names></name><xref ref-type="aff" rid="aff3"><sup>3</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Qin</surname><given-names>Lu</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Heating Systems Division, Sandvik Heating Technology AB, Hallstahammar, Sweden</addr-line></aff><aff id="aff1"><addr-line>Department of Materials and Manufacturing Technology, Chalmers University of Technology, Gothenburg, Sweden</addr-line></aff><aff id="aff3"><addr-line>Material Technology, Siemens Industrial Turbomachinery AB, Finspong, Sweden</addr-line></aff><pub-date pub-type="epub"><day>25</day><month>07</month><year>2016</year></pub-date><volume>04</volume><issue>07</issue><fpage>15</fpage><lpage>21</lpage><history><date date-type="received"><day>6</day>	<month>May</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>21</month>	<year>July</year>	</date><date date-type="accepted"><day>25</day>	<month>July</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>
 
 
   A composites of (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol% ZrO<sub>2</sub> was prepared with powder metallurgy and Pressure- Less Sintering (PLS) method, aiming at applications of high temperature structural materials. Mechanical properties of the composites were assessed with hardness, indentation fracture toughness K<sub>c</sub> and K<sub>IC</sub> tested using SEVNB, flexure strength at room temperature and 1200?C, and isothermal oxidation at 1400?C. The results showed that the native silica oxide and molybdenum-oxides on the silicide feedstock surface were significantly reduced in terms of Cr-alloying. (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> and its composite also exhibited improved sinterability and grain growth, owing to the presence of (Cr, Mo)<sub>5</sub>Si<sub>3</sub> at grain boundaries. Fracture toughness of the composite was increased by a factor of 1.6 to that in the monolithic silicide. Mechanical property of the composite at high temperature was not affected by Cr addition. However, the high temperature oxidation resistance was greatly improved in the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol% ZrO<sub>2</sub> compared with the non Cr-alloyed counterpart. The Cr-alloying effects on the microstructure, fracture behaviour, and high temperature oxidation resistance were discussed.  
 
</p></abstract><kwd-group><kwd>MoSi2</kwd><kwd> Composite</kwd><kwd> Fracture Toughness</kwd><kwd> Mechanical Property</kwd><kwd> Microstructure</kwd><kwd> High Temperature Oxidation</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Molybdenum disilicide MoSi<sub>2</sub> is a candidate for high-temperature structural materials due to high melting point, high specific strength (strength/density), high thermal conductivity, and excellent oxidation resistance at elevated temperature [<xref ref-type="bibr" rid="scirp.68961-ref1">1</xref>]. However, the properties of fracture toughness and creep resistance have to be improved before engineering applications. Promising approaches include solid solution alloying the silicide (Al, V, Cr, Ta, Nb, and Re, etc.), and composite reinforced with refractory and ceramic particles and fibres (SiC, Si<sub>3</sub>N<sub>4</sub>, Al<sub>2</sub>O<sub>3</sub> and ZrO<sub>2</sub>) [<xref ref-type="bibr" rid="scirp.68961-ref2">2</xref>]. Significant increasing in fracture toughness and strengthening at high temperature has been reported in MoSi<sub>2</sub>-ZrO<sub>2</sub> composites in terms of phase transformation toughening of ZrO<sub>2</sub>, but the degraded oxidation resistance was also observed, especially with a high ZrO<sub>2</sub> content [<xref ref-type="bibr" rid="scirp.68961-ref3">3</xref>] [<xref ref-type="bibr" rid="scirp.68961-ref4">4</xref>].</p><p>In this investigation, Cr alloyed molybdenum disilicide (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub>, and composite (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> were produced with Pressure-Less Sintering (PLS) that was the most economic and practical technique applied popularly in industrial production. The purpose of this study is to investigate the alloying effect of Cr addition on mechanical properties and high temperature oxidation resistance in comparison with the un-al- loyed MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> composite.</p></sec><sec id="s2"><title>2. Experimental Methods</title><p>(Mo<sub>0.9</sub>M<sub>0.1</sub>)Si<sub>2</sub> (3.3 at%Cr) and (Mo<sub>0.9</sub>M<sub>0.1</sub>)Si<sub>2</sub> + 15 vol%ZrO<sub>2</sub> composites were prepared using a powder metallurgy process described in an earlier work [<xref ref-type="bibr" rid="scirp.68961-ref4">4</xref>]. The average particle sizes were in a range of 2.3 - 2.6 and 0.87 μm for the Cr-alloyed silicide and un-stabilized ZrO<sub>2</sub> feedstocks, respectively. The powder mixture was milled in gasoline for 4 hours, and pressed to 60% of theoretical density (T.D.) using Cold Isostatic Pressing (CIP) at 200 MPa. PLS process was performed at 1600˚C - 1620˚C in H<sub>2</sub> atmosphere. The sintering density was measured using Archimedes method. Native oxides on the silicide feedstock powder surfaces were examined using X-ray Photoelectron Spectroscopy (XPS). Phases were determined using XRD with Cr-K<sub>α</sub> radiation. The microstructure was characterized with optical microscope and scanning electron microscope (SEM) with Energy Dispersive Spectroscopy (EDS).</p><p>The fracture toughness was measured with two methods: K<sub>c</sub> indentation fracture toughness (IF) calculated with the Anstis formula; K<sub>IC</sub> fracture toughness tested with a standard method of Single Edge V-Notch Beam (SEVNB). The 4-point bending tests were conducted with inner/outer spans of 20/40 mm, and with a cross head speed was 0.2 mm/s. As-sintered surfaces from PLS remained on the testing pieces. The flexure strength was tested at room temperature and at 1200˚C in ambient air. Discontinuous isothermal oxidation test was performed at 1400˚C for 1000 h in flowing air. The weight changes were carefully measured after each exposure with accuracy of 0.1 mg.</p></sec><sec id="s3"><title>3. Results and Discussion</title><sec id="s3_1"><title>3.1. Oxides on Stoking Powder Surfaces</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref> shows XPS spectra of MoSi<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> silicide feedstock at the Si<sub>2p</sub>, Mo<sub>3d</sub> and Cr<sub>3d</sub>. The area ratios of Si<sub>2p</sub> peaks at SiO<sub>2</sub> and MoSi<sub>2</sub> are 2.9 and 1.0 for the MoSi<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> powder surfaces, respectively (<xref ref-type="fig" rid="fig1">Figure 1</xref>(a)). The area ratios of Mo<sub>3d</sub> peaks at Mo-oxides and MoSi<sub>2</sub> are 1.7 and 1.0 in the MoSi<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> powder surfaces, respectively (<xref ref-type="fig" rid="fig1">Figure 1</xref>(b)). The Cr<sub>2p</sub> peak of Cr<sub>2</sub>O<sub>3</sub> was found in the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> powder surface, and the area ratio of Cr<sub>2</sub>O<sub>3</sub> to Cr-silicide is 1.4 (<xref ref-type="fig" rid="fig1">Figure 1</xref>(c)). It is apparent that the formation of silica and Mo-oxides on the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> powder surface are substantially impeded by the formation of Cr-oxides. The oxygen in the sintered bulk is believed to be introduced from the native oxide on the stocking powders. According to the chemical analysis, the oxygen contents were 2.16 and 1.13 wt% in the MoSi<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> sintered bulks. Meanwhile, substantially decreasing of SiO<sub>2</sub> particles was observed in the sintered (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> and composite bulks (see the following section). It was consistently testified that Cr-addition can efficiently reduce silica in molybdenum disilicide. It is widely agreed that low silica at grain boundaries is appreciable to the creep resistance of silicide composites [<xref ref-type="bibr" rid="scirp.68961-ref5">5</xref>]. Thus, Cr-alloying is an alternative approach to reduce the SiO<sub>2</sub> contents of silicide composites, which could contribute to creeping property at elevated temperature.</p></sec><sec id="s3_2"><title>3.2. Sintering Density</title><p>Theoretical density of MoSi<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> silicides are 6.25 and 6.10 g/cm<sup>3</sup>, respectively, measured from XRD. Theoretical densities of MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> are 6.16 and 6.04 g/cm<sup>3</sup>, calculated from a linear combination rule. The sintering density of different materials is shown in <xref ref-type="table" rid="table1">Table 1</xref>. High sintering density over 98% T.D. was obtained in both Cr-alloyed silicide and composite. Improved sinterability is directly related to the existence of (Cr, Mo)<sub>5</sub>Si<sub>3</sub> type silicide as secondary phase presenting (see the following</p><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title>XPS spectra at (a) Si<sub>2p</sub>; (b) Mo<sub>3d</sub> in the surface of the MoSi<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> feedstock powders, (c) Cr<sub>2p</sub> in the surface of the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> feedstock powder.</title></caption><fig id ="fig1_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x4.png"/></fig><fig id ="fig1_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x5.png"/></fig><fig id ="fig1_3"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x6.png"/></fig></fig-group><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Property of sintered silicides and composites</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Materials</th><th align="center" valign="middle" >Sintering density (g/cm<sup>3</sup>)</th><th align="center" valign="middle" >Relative density (%T.D.)</th><th align="center" valign="middle" >Average grain size (&#181;m)</th><th align="center" valign="middle" >HV10 (GPa)</th></tr></thead><tr><td align="center" valign="middle" >MoSi<sub>2</sub></td><td align="center" valign="middle" >6.01</td><td align="center" valign="middle" >96.2</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >8.7 &#177; 0.3</td></tr><tr><td align="center" valign="middle" >(Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub></td><td align="center" valign="middle" >6.06</td><td align="center" valign="middle" >99.3</td><td align="center" valign="middle" >14</td><td align="center" valign="middle" >7.7 &#177; 0.2</td></tr><tr><td align="center" valign="middle" >MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub></td><td align="center" valign="middle" >5.84</td><td align="center" valign="middle" >95.0</td><td align="center" valign="middle" >4</td><td align="center" valign="middle" >8.7 &#177; 0.2</td></tr><tr><td align="center" valign="middle" >(Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub></td><td align="center" valign="middle" >5.95</td><td align="center" valign="middle" >98.5</td><td align="center" valign="middle" >11</td><td align="center" valign="middle" >7.9 &#177; 0.2</td></tr></tbody></table></table-wrap><p>section). The melting point of CrSi<sub>2</sub> is 1551˚C, nearly 470˚C lower than that of MoSi<sub>2</sub>. According to a quasibinary section phase diagram of MoSi<sub>2</sub>-CrSi<sub>2</sub>, a peritectic reaction exists at 7 at%Cr at 1529˚C, taking place as L + Mo<sub>1?x</sub>Cr<sub>x</sub>Si<sub>2</sub> &#219; Mo<sub>y</sub>Cr<sub>1?y</sub>Si<sub>2</sub> [<xref ref-type="bibr" rid="scirp.68961-ref6">6</xref>]. A liquid phase might appear at the sintering temperature, which may greatly assist mass transport and densification process during sintering at 1600˚C - 1620˚C.</p></sec><sec id="s3_3"><title>3.3. Material Characterization</title><p>The XRD analysis shows that the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> consists of a single-phase of tetragonal C11<sub>b</sub> structure. The Cr solid solubility in the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> is 2.5 - 2.6 at% by EDS, which is lower than the nominal composition of 3.3 at%. Typical microstructures of different materials are shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>. The amount of SiO<sub>2</sub> particles in (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> was reduced to 1.4 vol% compared with 2.2 vol% in MoSi<sub>2</sub>, measured from selected dense areas with imaging process. A small amount of Mo<sub>5</sub>Si<sub>3</sub> was observed in MoS<sub>2</sub> (<xref ref-type="fig" rid="fig2">Figure 2</xref>(a)). In (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub>, the Mo<sub>5</sub>Si<sub>3</sub> phase was replaced by a Cr-rich silicide with a composition of Cr:Mo:Si = 45:15:40 (at%) close to (Cr<sub>0.75</sub>Mo<sub>0.25</sub>)<sub>5</sub>Si<sub>3</sub>. The Cr-rich silicide appears as discrete grains and continuous phase along grain boundaries (<xref ref-type="fig" rid="fig2">Figure 2</xref>(b)). Grain growth is substantial in (Mo<sub>0.9</sub>M<sub>0.1</sub>)Si<sub>2</sub> by a factor of 3 of that in MoSi<sub>2</sub> (<xref ref-type="table" rid="table2">Table 2</xref>), which could be ascribed to the liquid phase sintering effect of the existence of the (Cr, Mo)<sub>5</sub>Si<sub>3</sub> silicide with lower melting point. ZrO<sub>2</sub> particles were well-dispersed in both composites (<xref ref-type="fig" rid="fig3">Figure 3</xref>(c) and <xref ref-type="fig" rid="fig3">Figure 3</xref>(d)), and grain sizes in both composites were refined owing to the dispersion of ZrO<sub>2</sub> particles (<xref ref-type="table" rid="table2">Table 2</xref>). The Mo<sub>5</sub>Si<sub>3</sub> grains are still visible in MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> (<xref ref-type="fig" rid="fig2">Figure 2</xref>(c)), but the (Cr ,Mo)<sub>5</sub>Si<sub>3</sub> is hardly recognized in (Mo<sub>0.9</sub>M<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> composite from the contrast in SEM images (<xref ref-type="fig" rid="fig2">Figure 2</xref>(d)).</p></sec><sec id="s3_4"><title>3.4. Mechanical Property</title><p>Mechanical properties are shown in <xref ref-type="table" rid="table1">Table 1</xref> and <xref ref-type="table" rid="table2">Table 2</xref>. The average hardness values of the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> matrix phase and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> composite are 10% lower than their un-Cr alloyed counterparts (<xref ref-type="table" rid="table1">Table 1</xref>), which might result from the softening effect of the Cr-addition. The fracture toughness K<sub>IC</sub> of the two composites are comparable, which are higher than the monolithic silicides in a factor of 1.4 - 1.6 (<xref ref-type="table" rid="table2">Table 2</xref>). The fracture toughness values from indentation fracture (K<sub>c</sub>) and SEVBN (K<sub>IC</sub>) methods are close in MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub>. However, the K<sub>c</sub> value is too high over K<sub>IC</sub> in the (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2 </sub>composite, which</p><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Microstructure of as-sintered silicides and composites (a) MoSi<sub>2</sub>, (b) (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub>, (c) MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub>, and (d) (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub>.</title></caption><fig id ="fig2_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x7.png"/></fig><fig id ="fig2_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x8.png"/></fig><fig id ="fig2_3"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x9.png"/></fig><fig id ="fig2_4"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x10.png"/></fig></fig-group><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Mechanical property of silicides and composites</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Materials</th><th align="center" valign="middle" >K<sub>c</sub> (98N) (MPa.m<sup>1/2</sup>)</th><th align="center" valign="middle" >K<sub>IC</sub> (SEVNB) (MPa.m<sup>1/2</sup>)</th><th align="center" valign="middle" >s<sub>f</sub> (Room temp.)(MPa)</th><th align="center" valign="middle" >s<sub>f</sub> (high temp.) (MPa)</th></tr></thead><tr><td align="center" valign="middle" >MoSi<sub>2</sub></td><td align="center" valign="middle" >3.0 &#177; 0.2</td><td align="center" valign="middle" >3.0 &#177; 0.2</td><td align="center" valign="middle" >450 &#177; 40</td><td align="center" valign="middle" >≥330 (1100˚C)</td></tr><tr><td align="center" valign="middle" >MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub></td><td align="center" valign="middle" >4.7 &#177; 0.6</td><td align="center" valign="middle" >4.2 &#177; 0.2</td><td align="center" valign="middle" >325 &#177; 40</td><td align="center" valign="middle" >334 &#177; 14 (1200˚C)</td></tr><tr><td align="center" valign="middle" >(Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub></td><td align="center" valign="middle" >6.4 &#177; 0.4</td><td align="center" valign="middle" >4.7 &#177; 0.3</td><td align="center" valign="middle" >293 &#177; 25</td><td align="center" valign="middle" >200 &#177; 27 (1200˚C)</td></tr></tbody></table></table-wrap><p>is caused by the uncertainty in determination of the crack length. <xref ref-type="fig" rid="fig3">Figure 3</xref> shows typical indentation cracks in the composites. The primary median cracks from the indent corners in MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> are deflected (D), branched (Bra), bridged (Bri) by the dispersed ZrO<sub>2</sub> additives (<xref ref-type="fig" rid="fig3">Figure 3</xref>(a)), which dissipates and absorbs the energy for crack propagation. In contrast, multi-cracks are developed around the indent edges in (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> (<xref ref-type="fig" rid="fig3">Figure 3</xref>(b)). In such a case, the measured crack length is not reliable and inaccurate, which results in the overestimated K<sub>c</sub> result. It is implied that the indentation fracture method is not suitable to describe the fracture toughness property of the composite (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub>, therefore, a verification with a standard method has to be considered. The room temperature flexural strength s<sub>f</sub> of the composites is lower than that of MoSi<sub>2</sub> (<xref ref-type="table" rid="table2">Table 2</xref>). The s<sub>f</sub> of (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub>is substantially reduced at 1200˚C compared with MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub>. It is believed that interfacial fracture energy is changed between the alloyed silicide matrix and ZrO<sub>2</sub> particles [<xref ref-type="bibr" rid="scirp.68961-ref7">7</xref>], and grain boundaries can be weakened by the present of the (Cr, Mo)<sub>5</sub>Si<sub>3</sub> phase in (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> at elevated temperatures.</p></sec><sec id="s3_5"><title>3.5. High Temperature Oxidation Test</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref> shows time dependence of mass change after isothermal exposure at 1400˚C in air. All the samples present with parabolic kinetics in the steady oxidation stage, indicating the formation of protective oxide scales and diffusion controlled oxidation. Total weight gains in (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> and MoSi<sub>2</sub> are 1.7 and 3.6 mg/cm<sup>2</sup> after 1000 h exposure, inferring that the thickness of the SiO<sub>2</sub> layer on the Cr-alloyed silicide (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> is thinner than that on MoSi<sub>2</sub>. The performance of (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> composite is similar to that of monolithic</p><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Cracks at indents in the composites (a) MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub>, and (b) (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub>.</title></caption><fig id ="fig3_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x11.png"/></fig><fig id ="fig3_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x12.png"/></fig></fig-group><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Exposure time dependence on weight change at 1400˚C in air</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x13.png"/></fig><p>MoSi<sub>2</sub>. In contrast, an erratic weight loss occurred in un-alloyed composite MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub>in the initial oxidation stage within 50 h. A parabolic weight-gain in MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> is established when a continuous silica layer is formed. The rate constants in the steady oxidation stage (after 50 h) are 0.0014 and 0.0006 (mg<sup>2</sup>∙cm<sup>−</sup><sup>4</sup>∙h<sup>−</sup><sup>1</sup>) in MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub>, respectively. Obviously, the oxidation rate is substantially decreased in the Cr-alloyed composite.</p><p>The oxide scales on both composites consist of tetragonal ZrSiO<sub>4</sub> and α-SiO<sub>2</sub> by XRD. Typical morphologies of the composite surfaces after 1000 h exposure are shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>. The scale on MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> surface contains large amounts of smaller zircon particles with a size of 1 - 2 mm (<xref ref-type="fig" rid="fig5">Figure 5</xref>(a)). In contrast, the surface of (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> is comprised zircon particles with a size of 3 - 5 mm (<xref ref-type="fig" rid="fig5">Figure 5</xref>(c)). Scale thickness is between 50 - 60 and 20 - 30 &#181;m in MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> and (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub>, respectively. SEM cross sectional images show that Mo<sub>5</sub>Si<sub>3</sub> grains are located at the interface between the base silicide and oxide scale of MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> (<xref ref-type="fig" rid="fig5">Figure 5</xref>(b)). The fine zircon particle network in the scale of MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> can provide fast diffusion paths for oxygen to the interface of scale-base silicide, which results in higher oxidation rate. In comparison, the oxide scale of (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> consists of nearly pure silica. Some large zircon particles mainly appear on the outermost surface of this composite. A few small discrete Cr<sub>2</sub>O<sub>3</sub> grains were found at the interface (<xref ref-type="fig" rid="fig5">Figure 5</xref>(d)), which resulted from the outer diffusion and oxidation of Cr from the alloyed base silicide after the formation of the protective silica scale.</p><p>It is known that the formation of protective silica on MoSi<sub>2</sub> at high temperature surface is implemented by selective oxidation of Si: MoSi<sub>2</sub> + O<sub>2</sub> &#174; MoO<sub>3</sub>(g) + SiO<sub>2</sub> at high pO<sub>2</sub>; and MoSi<sub>2</sub> + O<sub>2</sub>(g) &#174; Mo<sub>5</sub>Si<sub>3</sub> + SiO<sub>2</sub>, at low pO<sub>2</sub>. In the latter case, and silica can form at surface and Mo<sub>5</sub>Si<sub>3</sub> silicide usually form at the interface between scale and base silicide as oxygen diffuses through the surface oxide layer. In presence of ZrO<sub>2</sub> additives, SiO<sub>2</sub> will react with ZrO<sub>2</sub> to form zircon: SiO<sub>2</sub> +ZrO<sub>2</sub> = ZrSiO<sub>4</sub>, thus, the resultant zircon particles are retained in</p><fig-group id="fig5"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Plane view and cross section of the composites after exposure at 1400˚C for 1000 h, (a) and (b) MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub>, and (c) and (d) (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZO<sub>2</sub>.</title></caption><fig id ="fig5_1"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x14.png"/></fig><fig id ="fig5_2"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x15.png"/></fig><fig id ="fig5_3"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x16.png"/></fig><fig id ="fig5_4"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/68961x17.png"/></fig></fig-group><p>the oxide scale. The improved oxidation behaviour of the Cr- alloyed composite can be attributed to the chemistry change at the as received surfaces sintered in reduced atmosphere. It was reported that as-sintered surface of PLSed MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> is comprised with a silicon depleted silicide (Mo-Zr-Si) [<xref ref-type="bibr" rid="scirp.68961-ref8">8</xref>]. The substantial weight loss presenting in initial oxidation occurred in this composite was ascribed to the rapid oxidation of the high Zr-content silicide in the outermost surface. In comparison, the PLS sintered (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> surface consists of Cr-rich silicide with a low Zr content. It is believed that this silicide in the as-sintered surface could assists the formation of SiO<sub>2</sub> scale with a favourable microstructure (showed in <xref ref-type="fig" rid="fig5">Figure 5</xref>(d)) at relative lower temperature. The outer diffusion of Cr can also promote the mobility and diffusion of Si at high temperature in the Cr-alloyed composite. The investigation details will be published in a later paper.</p></sec></sec><sec id="s4"><title>4. Conclusion</title><p>(Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol% ZrO<sub>2</sub> composite with high sintering density 99% T.D. was prepared with pressure-less sintering method. The native silica and Mo-oxides in the Cr-alloyed silicide feed stocking surface was substantially reduced by means of forming Cr-oxides. As a result, the amount of silica particles in the sintered silicide bulk was reduced by 50%. The sinterablity of the composite was improved considerably due to the existence of small amounts of (Cr<sub>0.75</sub>Mo<sub>0.25</sub>)Si<sub>2</sub> silicide at grain boundaries. Toughening effect of the composite was not influenced by Cr-addition, and flexure strength was 200 MPa at 1200˚C. However, the as-sintered (Mo<sub>0.9</sub>Cr<sub>0.1</sub>)Si<sub>2</sub> + 15vol%ZrO<sub>2</sub> composite exhibited an excellent oxidation behaviour at 1400˚C, and the weight loss occurred at the starting oxidation in the as-sintered MoSi<sub>2</sub> + 15vol%ZrO<sub>2</sub> was avoided.</p></sec><sec id="s5"><title>Acknowledgement</title><p>The research was financially supported by Svenska Elf&#246;retagens Forsknings-och Utvecklings Elforsk-AB (KME), Sandvik Heating Technology AB, and Siemens Industrial Turbomachinery AB.</p></sec><sec id="s6"><title>Cite this paper</title><p>Yiming Yao,Erik Str&#246;m,Xin-Hai Li,Qin Lu, (2016) Property and Oxidation Behaviours of (Mo,Cr)Si2 + ZrO2 Composite Produced by Pressure-Less Sintering. 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