<?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">JECTC</journal-id><journal-title-group><journal-title>Journal of Electronics Cooling and Thermal Control</journal-title></journal-title-group><issn pub-type="epub">2162-6162</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/jectc.2016.62004</article-id><article-id pub-id-type="publisher-id">JECTC-67134</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Metal-Ceramic Smart Composite in Ti(C,N)-Ni-Mo-W System
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Z.</surname><given-names>Kovziridze</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>N.</surname><given-names>Nizharadze</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>G.</surname><given-names>Tabatadze</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>E.</surname><given-names>Nikoleishvili</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>M.</surname><given-names>Mshvildadze</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Chemical and Biological Technologies, Georgian Technical University, Tbilisi, Georgia</addr-line></aff><pub-date pub-type="epub"><day>02</day><month>06</month><year>2016</year></pub-date><volume>06</volume><issue>02</issue><fpage>42</fpage><lpage>51</lpage><history><date date-type="received"><day>8</day>	<month>April</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>4</month>	<year>June</year>	</date><date date-type="accepted"><day>7</day>	<month>June</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>
 
 
  Goal: Low wolfram-containing cutting composite was obtained by fusion of titanium carbonitride and high melting temperature binding metallic phase. Method: The composite was obtained via compaction and further sintering in vacuum furnace at 1600
  &amp;#176;C under 10
  <sup>-3</sup> Pa pressure. Phase analysis was performed on X-ray apparatus “DRON-3”; microstructure was determined by electron microscope NANOLAB-7, microhardness by MUCKE-mark microhardness meter; relative resistance of cutters was evaluated at similar modes of cutting according to distances they passed; experiments were carried out on turning lathe. Results: Physical-mechanical characteristics of the obtained composite are: σ
  <sub>bend</sub>, = 1000 - 1150 MPa, σ
  <sub>bend1000</sub>
  &amp;#176;C = 600 MPa, HV = 14 GPa; HV
  <sub>1000</sub>
  &amp;#176;C = 6.5 GPa. High speeds of cutting and high temperatures resistance of cutters made by the obtained composites exceeds 1.5 - 2-folds that of cutters made of the known BK8 and KNT20 hard alloys. Conclusion: Its application is recommended in hot steel treatment by cutting, for removal of the so-called burrs, as well as in steel treatment by cutting during pure and semi-pure operations. It can also be used in jet engines, chemical industry apparatuses, electric-vacuum devices, in industry of responsible details of rockets, nuclear reactors, flying apparatuses.
 
</p></abstract><kwd-group><kwd>Metal-Ceramic</kwd><kwd> Composite</kwd><kwd> Cutting Material</kwd><kwd> High-Temperature</kwd><kwd> Heatproof</kwd><kwd> Micro Hardness</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Up to now the main volume of tool materials is fabricated on the base of wolfram, the reserves of which suffer gradual exhaustion. With this in view, researchers are faced with the problem to create new composite materials without wolfram or to reduce its concentration to its minimum but preserve physical-mechanical and exploitation properties inherent to the composites prepared on the base of wolfram [<xref ref-type="bibr" rid="scirp.67134-ref1">1</xref>] - [<xref ref-type="bibr" rid="scirp.67134-ref6">6</xref>] . To resolve this problem, the researches were in progress in many countries of the world as well as at Georgian Technical University, where the researches in this sphere were initiated by the academician T. Loladze [<xref ref-type="bibr" rid="scirp.67134-ref7">7</xref>] - [<xref ref-type="bibr" rid="scirp.67134-ref16">16</xref>] . T. Loladze contributed greatly to the development of theory of metal treatment by cutting [<xref ref-type="bibr" rid="scirp.67134-ref7">7</xref>] - [<xref ref-type="bibr" rid="scirp.67134-ref11">11</xref>] .</p></sec><sec id="s2"><title>2. The Major Part</title><p>As is known, cutting tools yield mainly to two types of disintegration which differ by nature: brittle and plastic [<xref ref-type="bibr" rid="scirp.67134-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.67134-ref17">17</xref>] [<xref ref-type="bibr" rid="scirp.67134-ref18">18</xref>] - [<xref ref-type="bibr" rid="scirp.67134-ref24">24</xref>] . At normal conditions of cutting a tool must not yield to deterioration of these types and must possess sufficient plasticity and brittle hardness. Brittle fracture takes place when in the cutting section, that is, in the so-called “dangerous zone” of a tool the main tensile forces reach their limiting value, the limit of strength of the material. Plastic deformation occurs when shearing force in any definite volume of a body exceeds the flow limit and contraction, intense heating and softening commence, which elevate its plasticity. It has been established that cutting tool is able to treat material if its hardness 1.4-times exceeds that of the treated material [<xref ref-type="bibr" rid="scirp.67134-ref7">7</xref>] . Hardness ratio should be preserved at any term of cutting, that is, even at heating of tool material.</p><p>One of the main reasons for plastic collapse of standard hard alloys is heating of contact layers and their softening in the process of cutting. Therefore, great significance is attributed to temperature dependence of hardness of tool material.</p><p>Metal-ceramic cutting composites consist of carbides, nitrides, borides or their solid solutions bound by metallic phase. The so-called ceramic phase of these composites suffers less plastic deformation. The cause of plastic deformation of cutting tools is a binding metal phase. Thus, to elevate plastic hardness we could reduce composition of metal phase, but its decrease would result in a decrease of limit of brittle hardness. Academician Loladze offered an idea [<xref ref-type="bibr" rid="scirp.67134-ref9">9</xref>] , that one of the ways to improve cutting tools would be increase of plastic strength of metal binder. As a result of researches carried out with this in view, some composites were obtained (<xref ref-type="table" rid="table1"><xref ref-type="table" rid="table">Table </xref>1</xref>).</p><p>Batches were ground in vibration grinding mill for 20 - 30 hrs in alcohol medium. After drying of suspension the powder was plasticized in rubber solution dissolved in petrol and was pressed coldly at 1 ton/cm<sup>2</sup> pressure. Compressed and dried specimens were sintered at various temperatures in vacuum furnace at 1600˚C with 50˚-interval. After sintering the specimens were visually inspected and setting, water absorption, density and mechanical properties were determined. From the composites offered in <xref ref-type="table" rid="table1"><xref ref-type="table" rid="table">Table </xref>1</xref>, the best results were revealed by #4 composite, which was subjected to further studies.</p><p>Final baking of the tested composite was performed in vacuum furnace at 1600˚C, under 10<sup>−3</sup> Pa. In the process of sintering as a result of interaction of titanium carbide and titanium nitride we received titanium carbonitride, which was confirmed by X-ray diffraction analysis (<xref ref-type="fig" rid="fig1">Figure 1</xref>).</p><p>Microstructure of the tested composite is mainly homogeneous (<xref ref-type="fig" rid="fig1">Figure 1</xref>(a) and <xref ref-type="fig" rid="fig1">Figure 1</xref>(b)). The selected metal phase binds rather tightly carbonitride grains, which is confirmed by hardness limit at bending σ<sub>bend</sub><sub>.</sub> = 1100 - 1150 MPa (<xref ref-type="table" rid="table2"><xref ref-type="table" rid="table">Table </xref>2</xref>), while limit at bending of titanium carbonitride sintered at the very temperature σ<sub>bend</sub><sub>.</sub> = 500 MPa. Titanium carbonitride grain sizes are within 1 - 2 &#181;m (<xref ref-type="fig" rid="fig2">Figure 2</xref>). Significant impact of sintering temperature on carbonitride grain dimensions has not been fixed, which can be explained by low solubility of carbonitride in Ni-Mo-W metal phase.</p><p>Considering the fact that the hardness value is attributed a great significance for the process of cutting, harnesses were measured at room as well as at high temperatures.</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1"><xref ref-type="table" rid="table">Table </xref>1</xref></label><caption><title> Chemical composition of batches</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  >Batch #</th><th align="center" valign="middle"  colspan="5"  >Batch components, mass. %</th></tr></thead><tr><td align="center" valign="middle" >TiC</td><td align="center" valign="middle" >TiN</td><td align="center" valign="middle" >Ni</td><td align="center" valign="middle" >Mo</td><td align="center" valign="middle" >W</td></tr><tr><td align="center" valign="middle" >1</td><td align="center" valign="middle" >35</td><td align="center" valign="middle" >35</td><td align="center" valign="middle" >10</td><td align="center" valign="middle" >10</td><td align="center" valign="middle" >10</td></tr><tr><td align="center" valign="middle" >2</td><td align="center" valign="middle" >40</td><td align="center" valign="middle" >40</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >7</td></tr><tr><td align="center" valign="middle" >3</td><td align="center" valign="middle" >45</td><td align="center" valign="middle" >45</td><td align="center" valign="middle" >5</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >3</td></tr><tr><td align="center" valign="middle" >4</td><td align="center" valign="middle" >34</td><td align="center" valign="middle" >34</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >12</td><td align="center" valign="middle" >12</td></tr><tr><td align="center" valign="middle" >5</td><td align="center" valign="middle" >42</td><td align="center" valign="middle" >35</td><td align="center" valign="middle" >6</td><td align="center" valign="middle" >8</td><td align="center" valign="middle" >9</td></tr></tbody></table></table-wrap><fig-group id="fig1"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> X-ray phase analysis of the process of sintering of low-wolfram containing tested composite: (a) in the presence of metal Ni-Mo-W phase and (b) without metal phase.</title></caption><fig id ="fig1_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x6.png"/></fig></fig-group><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Microstructure of the Composite T</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x7.png"/></fig><table-wrap id="table2" ><label><xref ref-type="table" rid="table2"><xref ref-type="table" rid="table">Table </xref>2</xref></label><caption><title> Mechanical characteristics of tested and standard composites at room temperature</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Composite name</th><th align="center" valign="middle" >Strength at bending, σ<sub>bend</sub><sub>.</sub><sub>,</sub>MPa</th><th align="center" valign="middle" >HRA</th><th align="center" valign="middle" >HV, GPa at 5N load</th><th align="center" valign="middle" >HV, GPa at 15N load</th><th align="center" valign="middle" >HV, GPa at 50N load</th></tr></thead><tr><td align="center" valign="middle" >T</td><td align="center" valign="middle" >900 - 1150</td><td align="center" valign="middle" >88 - 89</td><td align="center" valign="middle" >9 - 10</td><td align="center" valign="middle" >8 - 9</td><td align="center" valign="middle" >7 - 8</td></tr><tr><td align="center" valign="middle" >BK8</td><td align="center" valign="middle" >1400 - 1500</td><td align="center" valign="middle" >89 - 90</td><td align="center" valign="middle" >10 - 11</td><td align="center" valign="middle" >11 - 12</td><td align="center" valign="middle" >11 - 12</td></tr><tr><td align="center" valign="middle" >KNT20</td><td align="center" valign="middle" >1300 - 1400</td><td align="center" valign="middle" >89 - 90</td><td align="center" valign="middle" >15 - 16</td><td align="center" valign="middle" >16 - 17</td><td align="center" valign="middle" >14 - 15</td></tr></tbody></table></table-wrap><p>Hardness at room temperature was measured by Rockwell’s method as well as at various loading by Vickers. Just for comparison simultaneously we measured characteristics of the standard alloys BK8 (WC92-Co 8%); and KNT20 (TiCN80-(Ni, Mo) 20%). Micro-hardness was measured at the Chair of Ceramics of Clausthal Technical University (Germany).</p><p>Results of measuring of micro-hardness at room temperature are offered in <xref ref-type="table" rid="table2"><xref ref-type="table" rid="table">Table </xref>2</xref> and Figures 3-5.</p><fig-group id="fig3"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Graphs for micro-hardness and distance passed by indenter for 5N load. (a) for tested T composite; (b) for BK8 and (c) for KNT20 alloys.</title></caption><fig id ="fig3_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x8.png"/></fig><fig id ="fig3_2"><label> (c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x9.png"/></fig></fig-group><fig-group id="fig4"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Graph for microhardness and distance passed by indenter for 50N load. (a) for tested T composite; (b) for KNT20 alloys.</title></caption><fig id ="fig4_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x10.png"/></fig></fig-group><fig-group id="fig5"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Graphs for micro-hardness and distance passed by indenter at 100N load. (a) for tested T composite; (b) for KNT20 alloys.</title></caption><fig id ="fig5_1"><label> (b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x11.png"/></fig></fig-group><p>As is seen from the <xref ref-type="table" rid="table">Table </xref>linear relation between micro-hardness and load value was not uniquely fixed. Definite deviations are conditioned by various factors, which affect the numerical value of hardness, material non-homogeneity, grain sizes, errors at measuring and others [<xref ref-type="bibr" rid="scirp.67134-ref25">25</xref>] - [<xref ref-type="bibr" rid="scirp.67134-ref27">27</xref>] .</p><p>In the process of micro-hardness measuring, with load and unload, we tried to characterize the value of flexible deformation by comparison of distance passed by an indenter, which was computed in percentages of difference between them. It turned out that for standard alloys it used to change within the limits of 22% - 38%, while for tested composite it was not fixed at all.</p><p>Consideration of indenter impression showed (<xref ref-type="fig" rid="fig6">Figure 6</xref>) that the limits of the tested composite are perturbed in the cases of all loading forces, while in the case of standard BK8 fracture is fixed only after 15N load and in case of KNT20 alloy, which contains 20% nickel-molybdenum metal binder, perturbation of impression limits is fixed at higher, 50 N loading force, which, according to our opinion refers to deficiency of flexibility deformation in tested composite, compared to standard alloys.</p><p>Determination of hardness indices at high temperatures (<xref ref-type="table" rid="table">Table </xref>3) prove that the tested composite preserves hardness up to a rather high temperature, while standard composites with cobalt or nickel-molybdenum metal binder are markedly inferior, and that it was conditioned by the increase of heat resistance of binding metal phase, thanks to introduction of metallic wolfram in it.</p><p>Measuring of strength at bending at high temperatures showed that strength of the tested low-wolfram composite almost doesn’t suffer change up to 1000˚C, while at further increase of sample testing temperature the limit of strength at bending slowly falls, but at 1200˚C, still preserves 400 - 600 MPa (<xref ref-type="fig" rid="fig7">Figure 7</xref>).</p><p>After investigation of specimens for strength at bending we carried out electron microscopy study for fracture (<xref ref-type="fig" rid="fig8">Figure 8</xref>). Case of a specimen fractured at room temperature (<xref ref-type="fig" rid="fig8">Figure 8</xref>(a)) shows that fault occurs via inter- grain and trans-crystallite mechanism, while at high temperatures it occurs via the inter-grain metal phase (<xref ref-type="fig" rid="fig8">Figure 8</xref>(b)).</p><p>Results of experiments for resistance [<xref ref-type="bibr" rid="scirp.67134-ref28">28</xref>] - [<xref ref-type="bibr" rid="scirp.67134-ref30">30</xref>] of carbon, alloyed steels and thermally stable alloys at the treatment by cutting showed that resistance of tested composite exceeds 1.5 - 2-times the resistance of standard composites. (Figures 9(a)-(c)).</p><p>At the treatment of steel 45 (HRC-45) at low speeds of cutting, resistance value (<xref ref-type="fig" rid="fig9">Figure 9</xref>(a)) for all composites is more or less similar, and is determined according to brittle adhesive wear and tear and crumbling, since they have almost similar limit of strength. At the treatment of iron at low cutting speed v = 5 - 10 m/min (<xref ref-type="fig" rid="fig9">Figure 9</xref>(b)) resistance is approximately the same, while at v = 5 - 10 m/min speeds the resistance of T composite greatly exceeds those of BK8 and KNT20, similar is in the case of treatment of stainless steel (<xref ref-type="fig" rid="fig9">Figure 9</xref>(c)).</p><p>Addition of high melting temperature wolfram to metal binder of the tested composite results in increase of plastic strength of the composite and it is expressed in its advantage at cutting at high speeds [<xref ref-type="bibr" rid="scirp.67134-ref31">31</xref>] .</p><p>Marked advantage of the tested low-wolfram composite to BK8 and KNT20 was fixed due to high plastic strength and diffuse resistance for the operations of removal of inner and external burrs of pipes welded by hot steel cutting, when cutting temperature reached 900˚C - 950˚C.</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Indenter impression images at 5, 15, 50N loading forces</title></caption>
<table-wrap id="table_fig1" >
<object-id pub-id-type="pii">
<xref ref-type="table" rid="table1">
<xref ref-type="table" rid="table">Table </xref>1</xref></object-id>
</table-wrap><p><xref ref-type="fig" rid="fig6">Figure 6</xref>. Indenter impression images at 5, 15, 50N loading forces.</p><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Curves of temperature dependence of limit of strength at bending of T and KNT 20 composites</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x21.png"/></fig><fig-group id="fig7"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Electron microscopic image of T composite fracture after testing for limit of strength at bending: (a) at room temperature; (b) at 800˚C; (c) at 1200˚C.</title></caption><fig id ="fig7_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x22.png"/></fig><fig id ="fig7_2"><label> (c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x23.png"/></fig></fig-group><fig-group id="fig8"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Curves of T, BK and KNTcomposites resistance at the treatment of various materials by cutting. (a) steel HRC = 45; (b) iron and (c) stainless steel. (α = α = 9˚; φ = 45˚;φ<sub>1</sub> = 35; λ= 0˚; t = 1 mm; S = 0.21 mm/rev.).</title></caption><fig id ="fig8_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x24.png"/></fig><fig id ="fig8_2"><label>(c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x25.png"/></fig><fig id ="fig8_3"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/2-1520077x26.png"/></fig></fig-group><table-wrap id="table3" ><label><xref ref-type="table" rid="table">Table </xref>3</label><caption><title> Composite hardness-temperature dependence</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  >Temperature , T ˚C</th><th align="center" valign="middle"  colspan="3"  >Hardness HV, GPa</th></tr></thead><tr><td align="center" valign="middle" >Tested T composite</td><td align="center" valign="middle" >WC 92-Co 8</td><td align="center" valign="middle" >Ti(C, N) 80-Co 20</td></tr><tr><td align="center" valign="middle" >200</td><td align="center" valign="middle" >14.0</td><td align="center" valign="middle" >13.0</td><td align="center" valign="middle" >14.0</td></tr><tr><td align="center" valign="middle" >400</td><td align="center" valign="middle" >13.0</td><td align="center" valign="middle" >10.5</td><td align="center" valign="middle" >11.5</td></tr><tr><td align="center" valign="middle" >600</td><td align="center" valign="middle" >11.0</td><td align="center" valign="middle" >8.0</td><td align="center" valign="middle" >8.5</td></tr><tr><td align="center" valign="middle" >800</td><td align="center" valign="middle" >9.0</td><td align="center" valign="middle" >5.5</td><td align="center" valign="middle" >6.0</td></tr><tr><td align="center" valign="middle" >1000</td><td align="center" valign="middle" >6.5</td><td align="center" valign="middle" >3.5</td><td align="center" valign="middle" >4.0</td></tr></tbody></table></table-wrap></fig></sec><sec id="s3"><title>3. Conclusion</title><p>Results of the researches enable us to make conclusion that low-wolfram containing cutting composite obtained by fusion of titanium carbonitride and high melting point binding metal phase can be used at pure and semi-pure treatment of steels by cutting. Its application is recommended also in hot steel treatment by cutting, for removal of the so-called hot burrs. Besides, it can be used in jet engines, chemical industry apparatuses, electric-vacuum devices, in industry of responsible details of rockets, nuclear reactors, flying apparatuses.</p></sec><sec id="s4"><title>Acknowledgements</title><p>We express our gratitude to the Institute of Nonmetallic Materials, Technical University Clausthal, Germany and Prof. Dr.-Ing. Jurgen G. Heinrich for the support rendered in scientific experiments.</p></sec><sec id="s5"><title>Cite this paper</title><p>Z. Kovziridze,N. Nizharadze,G. Tabatadze,E. Nikoleishvili,M. Mshvildadze, (2016) Metal-Ceramic Smart Composite in Ti(C,N)-Ni-Mo-W System. Journal of Electronics Cooling and Thermal Control,06,42-51. doi: 10.4236/jectc.2016.62004</p></sec></body><back><ref-list><title>References</title><ref id="scirp.67134-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Shlishevsky, B.E. and Larina, T.C. (2007) Wolframfree Solid Alloys and Prospects of Their Application in Optic Sphere of Instrument Engineering. Interexpo Geo Siberia, 4, 1-7.</mixed-citation></ref><ref id="scirp.67134-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Grubyj, S.V. (1984) Elevation of Efficiency of Lathe Treatment of Steels by Cutting Tools Made of Wolframfree Solid Alloys. Abstract of a Thesis for a Scientific Degree of a Candidate of Technical Sciences, Moscow.</mixed-citation></ref><ref id="scirp.67134-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Zubkov, N.N. 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