<?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.2018.911063</article-id><article-id pub-id-type="publisher-id">MSA-88037</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>
 
 
  Investigation of the Boriding Process of the Ti-Al Intermetallic Alloy GE48-2-2 Taking into Account the Probability of the Influence of the Substrate Modification
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Dimitrios</surname><given-names>I. Zagkliveris</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>Georgios</surname><given-names>K. Triantafyllidis</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Chemical Engineering, Aristotle University of Thessaloniki, Thessaloniki, Greece</addr-line></aff><pub-date pub-type="epub"><day>10</day><month>10</month><year>2018</year></pub-date><volume>09</volume><issue>11</issue><fpage>873</fpage><lpage>882</lpage><history><date date-type="received"><day>14,</day>	<month>September</month>	<year>2018</year></date><date date-type="rev-recd"><day>23,</day>	<month>October</month>	<year>2018</year>	</date><date date-type="accepted"><day>26,</day>	<month>October</month>	<year>2018</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>
 
 
  Boriding of the Ti-Al intermetallic GE48-2-2 at 1273 K for 10 hours was performed. In order to ensure that no any serious alteration occurred in the substrate, it was previously examined with X-Ray Diffractometry (XRD), after it has undergone an annealing process at the temperature of boronizing. Subsequently, we examined the coating with XRD and Scanning Electron Microscopy, in order to characterize its structure and morphology. A dense TiΒ
  <sub>2</sub> layer, 10 - 15 μm thick, was formed, but also Cr
  <sub>2</sub>B
  <sub>3</sub> and NbN, BN and some Ti-Al phases were detected. Efforts were undertaken to focus on influence of the substrate modification, towards the quality of the coating.
 
</p></abstract><kwd-group><kwd>Titanium Aluminide</kwd><kwd> Boriding</kwd><kwd> Titanium Boride</kwd><kwd> Substrate Modification</kwd><kwd> Phase Analysis</kwd><kwd> X-Ray Diffraction</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The Ti-Al intermetallics are light, high-temperature oxidation resistant materials and can find application in automotive, aerospace and power industry [<xref ref-type="bibr" rid="scirp.88037-ref1">1</xref>] . They could replace Ni superalloys in these applications [<xref ref-type="bibr" rid="scirp.88037-ref1">1</xref>] , as they have almost two times lower density. They are also more sufficient than pure titanium due to their higher elastic modulus and strength and better oxidation resistance at high temperatures [<xref ref-type="bibr" rid="scirp.88037-ref1">1</xref>] . These properties result from the dominant presence of the γ-TiAl phase. In such a way Ti-Al intermetallic is a promising group of light and high-temperature oxidation and creep resistant materials [<xref ref-type="bibr" rid="scirp.88037-ref1">1</xref>] . Moreover in order to improve these interesting properties, some alloying elements could be added. For instance, Nb and Ta addition improves the oxidation and creep resistance at 1000 K [<xref ref-type="bibr" rid="scirp.88037-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref3">3</xref>] . In particular, Nb hinders dislocation slip resulting to the increase of creep resistance at high temperatures and, additionally, contributes to oxidation resistance by supporting the formation of an Al<sub>2</sub>O<sub>3</sub> film, a kind of passivation [<xref ref-type="bibr" rid="scirp.88037-ref4">4</xref>] .</p><p>In spite of their interesting properties, these materials show insufficient hardness values, so that makes them to be inappropriate for applications towards wear resistance requirements [<xref ref-type="bibr" rid="scirp.88037-ref2">2</xref>] . In order to encounter this weakness, a lot of surface treatments have been developed, included diffusion heat treatments such as aluminizing [<xref ref-type="bibr" rid="scirp.88037-ref5">5</xref>] , nitriding [<xref ref-type="bibr" rid="scirp.88037-ref6">6</xref>] , siliconizing [<xref ref-type="bibr" rid="scirp.88037-ref7">7</xref>] and other techniques as well. Boriding (or boronizing) method is not applied extensively on Ti-Al intermetallics, in spite of this method is widely used in similar applications, even on titanium alloys [<xref ref-type="bibr" rid="scirp.88037-ref8">8</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref9">9</xref>] . By this technique, a layer of metal borides is formed on the surface of the metal with diffusion of boron atoms through the metal lattice.</p><p>The most commonly used technique is conventional powder-pack boriding, which is characterized by its simplicity and cost-effectiveness [<xref ref-type="bibr" rid="scirp.88037-ref10">10</xref>] . It is often performed using a powder that contains the boron agent, an activator and a filler material at a high temperature, which causes the boron to be released from the agent by the activator. After the boron is released, it diffuses interstitially into the titanium aluminide lattice.</p><p>It is important to emphasize that there is not much data related to the boriding process especially on Ti-Al intermetallics. On this topic a rather new and sufficiently comprehensive work it is found at reference [<xref ref-type="bibr" rid="scirp.88037-ref11">11</xref>] . In our work, we investigated the role of the substrate modification, caused by the heat treatment, and the effect of the residual atmospheric gases in the structure and composition of the coating. Such an investigation on a borided Ti-Al intermetallic alloy, focused on the influence of the substrate, is totally absent from literature.</p></sec><sec id="s2"><title>2. Material and Methods</title><sec id="s2_1"><title>2.1. Preliminary Work</title><p>The alloy that used is the GE48-2-2 Ti-Al intermetallic with the chemical composition, as provided by the manufacturer (GfE―Gesellschaft f&#252;r Elektrometallurgie mbH), presented in <xref ref-type="table" rid="table1">Table 1</xref>.</p><p>Ti-Al GE48-2-2 ingots are manufactured by double or triple VAR melting with consumable electrodes. Consumable electrodes are made up of compacted Ti sponge, Aluminum and master alloys [<xref ref-type="bibr" rid="scirp.88037-ref12">12</xref>] .</p><p>The material has been cut into cubic samples with 1 cm long edge. Before boriding process, the samples were ground on SiC papers and then washed and dried.</p><p>At the same time, the boriding powder was prepared. Its composition and grain size information is presented in <xref ref-type="table" rid="table2">Table 2</xref>.</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Chemical composition of the intermetallic GE48-2-2</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Element</th><th align="center" valign="middle" >Ti</th><th align="center" valign="middle" >Al</th><th align="center" valign="middle" >Nb</th><th align="center" valign="middle" >Cr</th><th align="center" valign="middle" >Fe</th><th align="center" valign="middle" >Si</th></tr></thead><tr><td align="center" valign="middle" >wt. % (precise)</td><td align="center" valign="middle" >59.7</td><td align="center" valign="middle" >33.2</td><td align="center" valign="middle" >4.4</td><td align="center" valign="middle" >2.5</td><td align="center" valign="middle" >0.03</td><td align="center" valign="middle" >0.004</td></tr><tr><td align="center" valign="middle" >at. % (nominal)</td><td align="center" valign="middle" >48</td><td align="center" valign="middle" >48</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >2</td><td align="center" valign="middle" >-</td><td align="center" valign="middle" >-</td></tr></tbody></table></table-wrap><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Chemical composition of the intermetallic GE48-2-2</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Substance</th><th align="center" valign="middle" >Weight ratio in the powder</th><th align="center" valign="middle" >Grain size (μm)</th><th align="center" valign="middle" >Purpose of use</th></tr></thead><tr><td align="center" valign="middle" >SiC</td><td align="center" valign="middle" >0.8</td><td align="center" valign="middle" >35 (average)</td><td align="center" valign="middle" >Filling material</td></tr><tr><td align="center" valign="middle" >B<sub>4</sub>C</td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >22 - 59</td><td align="center" valign="middle" >Boron source</td></tr><tr><td align="center" valign="middle" >KBF<sub>4</sub></td><td align="center" valign="middle" >0.1</td><td align="center" valign="middle" >[Undefined]</td><td align="center" valign="middle" >Activator</td></tr></tbody></table></table-wrap></sec><sec id="s2_2"><title>2.2. The Boriding Process</title><p>The sample was placed in a high-temperature resistant porcelain crucible full of the boriding powder. The crucible was sealed in a larger container with a continuous Argon flow, in order to create an inert atmosphere to avoid oxidation.</p><p>The sample with the above described boriding experimental plant was put into a CARBOLITE™ CWF 1300 furnace. The boriding process was carried out for 10 hours at 1273 K. After the end of the cycle, the specimens were left to cool down slowly in the furnace. The boriding conditions selected after a literature research in boronizing studies on Ti-Al and Ti alloys [<xref ref-type="bibr" rid="scirp.88037-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref11">11</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref13">13</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref14">14</xref>] .</p></sec><sec id="s2_3"><title>2.3. XRD Analysis</title><p>XRD analysis method was selected to characterize the crystal structure of the substrate, with and without the thermal cycle. Also, Ti boride formation was verified via this method.</p><p>The measurements were carried out with a Bruker D8 ADVANCE device. A Cu Ka tube with 1.54060 Å wave length was used. The measurements were taken within a 2θ angle range of 25 - 85 degrees with a step of 0.02 degrees and 1.0 sec time exposure for every measured angle.</p><p>We also carried out extra measurements within a sub-range of 2θ angle with the same step, but 5.000 sec time exposure. Thereby, we achieved to produce a high quality pattern at the sub-range that includes the majority of the information of the whole pattern.</p><p>The evaluation of the patterns was carried out via Bruker’s DIFFRAC.EVA V.4.2.0.31 suite, drawing data from Crystallographic Open Database (COD-2016).</p></sec><sec id="s2_4"><title>2.4. SEM Analysis</title><p>As a complementary characterization method, Scanning Electron Microscopy was used for taking high resolution images of the coating layer and for having a semi-quantitative chemical analysis for the area of the coating and below it.</p></sec></sec><sec id="s3"><title>3. Results and Discussion</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref> shows XRD pattern of the substrate material GE48-2-2 Titanium Aluminide before any treatment.</p><p>In order to separate overlapping peaks, we proceeded to an additional measurement with five times larger exposure time (5.0 sec) within a 2θ range of 36 - 48 degrees, which is shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>. It is clear that, in the pre-treatment substrate, the dominant phase is the γ-Titanium Aluminide (γ-TiAl), but there is a presence of another equilibrium Ti-Al phase consisted of α<sub>2</sub>-Ti<sub>3</sub>Al. These preliminary measurements were carried out for two reasons: first, to detect the initial phases of the raw material and, second, to have a reference to evaluate the possible modification of the substrate after the boronizing treatment.</p><p>In <xref ref-type="fig" rid="fig3">Figure 3</xref> the XRD spectrum of the substrate metal after 10 hours non-boriding annealing treatment at 1073 K, 1173 K and 1273 K is presented. The measurements, which were carried out at room temperature, showed that the substrate was modified and transformed into a pure γ-TiAl material, ensuring that during boriding the substrate consists of just one single phase.</p><p>In <xref ref-type="fig" rid="fig4">Figure 4</xref> the XRD spectrum of borided layer is presented. In <xref ref-type="fig" rid="fig5">Figure 5</xref> the pattern of limited 2θ range from 33 to 47 degrees for better analysis is presented. This layer was created with boronizing treatment at 1273 K for 10 hours.</p><p>Moreover, a variety of secondary phases was revealed such as TiAl<sub>2</sub> and Ti<sub>5</sub>Al<sub>11</sub>. During the boriding process, a diffusion mechanism seems to hold near the surface, leading to an alteration of the local equilibrium composition, which in turn results in formation of the mentioned above Al-rich phases, appeared to be formed between the TiB<sub>2</sub> needles. It is more probably that the Al-rich phases were formed because of the fact that a part of the Ti atoms was consumed for the formation mainly of TiB<sub>2</sub>.</p><p>There is no evidence of TiB formation, in spite that elsewhere was referred to be observed [<xref ref-type="bibr" rid="scirp.88037-ref14">14</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref15">15</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref16">16</xref>] . Contrariwise, only TiB<sub>2</sub> was formed as it is clearly observable in <xref ref-type="fig" rid="fig4">Figure 4</xref> and <xref ref-type="fig" rid="fig5">Figure 5</xref>. This is a very important detail that contributes to the evaluation of the quality of the coating, because the mechanical properties of TiB phase are inferior in comparison to TiB<sub>2</sub> [<xref ref-type="bibr" rid="scirp.88037-ref17">17</xref>] . The absence of TiB is probably due to the fact that the diffusion of boron was not facilitated through the coating<sub> </sub>layer. The Boron also seems to form a small amount of a</p><p>boride with Chromium, Cr<sub>2</sub>B<sub>3</sub> (<xref ref-type="fig" rid="fig5">Figure 5</xref>). The Cr<sub>2</sub>B<sub>3</sub> is a hard phase that enhances the quality of the coating [<xref ref-type="bibr" rid="scirp.88037-ref18">18</xref>] . Moreover, NbN (<xref ref-type="fig" rid="fig5">Figure 5</xref>) was probably formed, which contributes to the superficial strengthening of the material [<xref ref-type="bibr" rid="scirp.88037-ref19">19</xref>] .</p><p>Finally, there is a strong evidence of the formation of a hexagonal (graphite-like) Boron Nitride, h-BN (<xref ref-type="fig" rid="fig4">Figure 4</xref>). Normally, the BN is formed in the case that an NH<sub>4</sub>Cl activator is used [<xref ref-type="bibr" rid="scirp.88037-ref10">10</xref>] . However, in our case is obvious that the presence of BN in the coating is caused by the atmospheric Nitrogen traces, as we did not use a Nitrogen containing activator. The substrate is not sufficiently approachable from the X-ray beam, so the γ-TiAl phase peaks on XRD pattern (<xref ref-type="fig" rid="fig4">Figure 4</xref> &amp; <xref ref-type="fig" rid="fig5">Figure 5</xref>) are not enough intense [<xref ref-type="bibr" rid="scirp.88037-ref20">20</xref>] [<xref ref-type="bibr" rid="scirp.88037-ref21">21</xref>] .</p><p>For additional aspect of the coating, a metallographic image is presented in <xref ref-type="fig" rid="fig6">Figure 6</xref>.</p><p>In <xref ref-type="fig" rid="fig7">Figure 7</xref> a SEM image of the coating layer is presented.</p><p>The image (<xref ref-type="fig" rid="fig7">Figure 7</xref>) revealed a 10 - 15 μm thick TiB<sub>2</sub> layer. Moreover, the linear chemical profile across the coating layer for the elements Ti (light blue), Al (purple), Nb (red), Cr (green) is presented. The coating layer, as shown clearly in <xref ref-type="fig" rid="fig6">Figure 6</xref>, seems to consist of two phases. The atomic ratio Al:Ti in the coating, as extracted from elemental analysis via SEM (<xref ref-type="fig" rid="fig7">Figure 7</xref>), is significantly diminished. The majority of Ti atoms have being consumed in the formation of the TiB<sub>2</sub> phase. Thus, a large amount of Al atoms were deliberated from the initial γ-TiAl phase. Part of these Al atoms seemed to form the detected via XRD Al-rich phases TiAl<sub>2</sub> and Ti<sub>5</sub>Al<sub>11</sub>. The rest of the Al atoms have been moved towards the surface, following a reverse diffusion path. After that, an oxidation reaction of Al atoms took place and the oxide that was formed peeled off due to its weak adhesion with the coating layer.</p></sec><sec id="s4"><title>4. Conclusions</title><p>From the above described results we deduce the following:</p><p>・ The boronizing treatment leads to the formation of a coating layer, that includes the desirable TiB<sub>2</sub> phase with sufficient hardness (up to HV = 1400).</p><p>・ The TiB phase is totally absent from the spectrum.</p><p>・ The substrate undergoes a modification during the boronizing process, being transformed into a pure γ-TiAl material.</p><p>・ The same modification is present during non-boriding annealing of the pure substrate at the same time and temperature conditions. Consequently, this modification is independent of the presence of Boron.</p></sec><sec id="s5"><title>Acknowledgements</title><p>The authors acknowledge Mrs. Dabou Xanthi for carrying out the XRD measurements and Assoc. Prof. Pavlidou Eleni for conducting the SEM measurements. This research has been financially supported by General Secretariat for Research and Technology (GSRT) and the Hellenic Foundation for Research and Innovation (HFRI) (Scholarship Code: 530).</p></sec><sec id="s6"><title>Conflicts of Interest</title><p>The authors declare no conflicts of interest regarding the publication of this paper.</p></sec><sec id="s7"><title>Cite this paper</title><p>Zagkliveris, D.I. and Triantafyllidis, G.K. (2018) Investigation of the Boriding Process of the Ti-Al Intermetallic Alloy GE48-2-2 Taking into Account the Probability of the Influence of the Substrate Modification. Materials Sciences and Applications, 9, 873-882. https://doi.org/10.4236/msa.2018.911063</p></sec></body><back><ref-list><title>References</title><ref id="scirp.88037-ref1"><label>1</label><mixed-citation publication-type="book" xlink:type="simple">Appel, F. and Oehring, M. (2003) γ-Titanium Aluminide Alloys: Alloy Design and Properties. 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