Menu
Home
People
Places
Arts
History
Plants & Animals
Science
Life & Culture
Technology
Reference.org
Titanium alloys
open-in-new
<h2 id="categories">Categories</h2> <p>Titanium alloys are generally classified into four main categories,<a class="footnote-ref" id="fnref:1" href="#fn:1"><sup>1</sup></a><a class="footnote-ref" id="fnref:2" href="#fn:2"><sup>2</sup></a><a class="footnote-ref" id="fnref:3" href="#fn:3"><sup>3</sup></a><a class="footnote-ref" id="fnref:4" href="#fn:4"><sup>4</sup></a> with a miscellaneous catch-all the fifth. </p> <ul><li>Alpha alloys which contain neutral alloying elements (such as <a href="/facts/Tin/vxbbBgNz">tin</a>) and/ or alpha stabilisers (such as aluminium or <a href="/facts/Oxygen/acyn6o8r">oxygen</a>) only. These are not heat treatable. Examples include:<a class="footnote-ref" id="fnref:5" href="#fn:5"><sup>5</sup></a> Ti-5Al-2Sn-ELI, Ti-8Al-1Mo-1V.</li> <li>Near-alpha alloys contain small amount of <a href="/facts/Ductile/SBJsahEk">ductile</a> beta-phase. Besides alpha-phase stabilisers, near-alpha alloys are alloyed with 1–2% of beta phase stabilizers such as <a href="/facts/Molybdenum/RX6vp2bF">molybdenum</a>, <a href="/facts/Silicon/cgWx0hdr">silicon</a> or <a href="/facts/Vanadium/UvKkKTSm">vanadium</a>. Examples include:<a class="footnote-ref" id="fnref:6" href="#fn:6"><sup>6</sup></a> <a href="/facts/Ti-6Al-2Sn-4Zr-2Mo/64aYjmJR">Ti-6Al-2Sn-4Zr-2Mo</a>, Ti-5Al-5Sn-2Zr-2Mo, IMI 685, Ti 1100.</li> <li>Alpha and beta alloys, which are metastable and generally include some combination of both alpha and beta stabilisers, and which can be heat treated. Examples include:<a class="footnote-ref" id="fnref:7" href="#fn:7"><sup>7</sup></a> <a href="/facts/Ti-6Al-4V/TWYn3qda">Ti-6Al-4V</a>, Ti-6Al-4V-ELI, Ti-6Al-6V-2Sn, <a href="/facts/Ti-6Al-7Nb/b1PNPdlp">Ti-6Al-7Nb</a>, and Ti62A<a class="footnote-ref" id="fnref:8" href="#fn:8"><sup>8</sup></a></li> <li>Beta and near beta alloys, which are <a href="/facts/Metastability/H72SMWof">metastable</a> and which contain sufficient beta stabilisers (such as molybdenum, silicon and vanadium) to allow them to maintain the beta phase when <a href="/facts/Quenching/UUCW0GQD">quenched</a>, and which can also be solution treated and aged to improve strength. Examples include:<a class="footnote-ref" id="fnref:9" href="#fn:9"><sup>9</sup></a> <a href="/facts/Ti-10V-2Fe-3Al/lxxE2Gh1">Ti-10V-2Fe-3Al</a>, Ti–29Nb–13Ta–4.6Zr,<a class="footnote-ref" id="fnref:10" href="#fn:10"><sup>10</sup></a> Ti-13V-11Cr-3Al, Ti-8Mo-8V-2Fe-3Al, Beta C, Ti-15-3.</li> <li>Although uncommercialized in the west, binary titanium alloys with <a href="/facts/Magnesium/XyIhd2FG">magnesium</a>, <a href="/facts/Potassium/5lcumVgo">potassium</a>, <a href="/facts/Calcium/hf252CC0">calcium</a>, <a href="/facts/Lithium/7vXX6BWA">lithium</a> have been produced in an <a href="/facts/Arc_melting/GgYK6Nz1">arc melting</a> pressure vessel at up to 140 atmospheres.<a class="footnote-ref" id="fnref:11" href="#fn:11"><sup>11</sup></a></li></ul> <h3>Alpha-titanium</h3> <h3>Beta-titanium</h3> <p>Beta titanium <a href="/facts/Alloy/I7w7WQWR">alloys</a> exhibit the <a href="/facts/Body-centered_cubic/92Co7BKM">BCC</a> <a href="/facts/Allotropic/2WUdHWxg">allotropic</a> form of <a href="/facts/Titanium/53ArnDoy">titanium</a> (called beta).<a class="footnote-ref" id="fnref:12" href="#fn:12"><sup>12</sup></a> Elements used in this alloy are one or more of the following other than titanium in varying amounts. These are <a href="/facts/Molybdenum/RX6vp2bF">molybdenum</a>, <a href="/facts/Vanadium/UvKkKTSm">vanadium</a>, <a href="/facts/Niobium/3zNI8AKp">niobium</a>, <a href="/facts/Tantalum/VwaxMm33">tantalum</a>, <a href="/facts/Zirconium/y7gsoQFz">zirconium</a>, <a href="/facts/Manganese/j9ELd1TL">manganese</a>, <a href="/facts/Iron/DkICCKIC">iron</a>, <a href="/facts/Chromium/6sVk6Uu7">chromium</a>, <a href="/facts/Cobalt/gqhScEw4">cobalt</a>, <a href="/facts/Nickel/KwMCHYRP">nickel</a>, and <a href="/facts/Copper/I8PEE8oX">copper</a>. </p><p>Beta titanium alloys have excellent formability and can be easily welded.<a class="footnote-ref" id="fnref:13" href="#fn:13"><sup>13</sup></a> </p><p>Beta titanium is nowadays largely utilized in the <a href="/facts/Orthodontic/Np2rL0b4">orthodontic</a> field and was adopted for orthodontics use in the 1980s.<a class="footnote-ref" id="fnref:14" href="#fn:14"><sup>14</sup></a> This type of alloy replaced stainless steel for certain uses, as stainless steel had dominated orthodontics since the 1960s. It has strength/modulus of elasticity ratios almost twice those of 18-8 austenitic stainless steel, larger elastic deflections in springs, and reduced force per unit displacement 2.2 times below those of stainless steel appliances. </p><p>Some of the beta titanium <a href="/facts/Alloy/I7w7WQWR">alloys</a> can convert to hard and brittle <a href="/facts/Hexagonal_crystal_family/sSSok8wo">hexagonal</a> omega-titanium at cryogenic temperatures<a class="footnote-ref" id="fnref:15" href="#fn:15"><sup>15</sup></a> or under influence of ionizing radiation.<a class="footnote-ref" id="fnref:16" href="#fn:16"><sup>16</sup></a> </p> <h3>Omega-titanium</h3> <h2 id="transition-temperature">Transition temperature</h2> <p>The crystal structure of titanium at ambient temperature and pressure is close-packed hexagonal α phase with a c/a ratio of 1.587. At about 890 °C, the titanium undergoes an <a href="/facts/Allotropy/2WUdHWxg">allotropic</a> transformation to a body-centred cubic β phase which remains stable to the melting temperature. </p><p>Some alloying elements, called alpha stabilizers, raise the alpha-to-beta <a href="/facts/Transition_temperature/SHmaYk1q">transition temperature</a>,<a class="footnote-ref" id="fnref:17" href="#fn:17"><sup>17</sup></a> while others (beta stabilizers) lower the transition temperature. Aluminium, <a href="/facts/Gallium/EucevDs9">gallium</a>, <a href="/facts/Germanium/wtoALHGs">germanium</a>, <a href="/facts/Carbon/ukrgQexo">carbon</a>, <a href="/facts/Oxygen/acyn6o8r">oxygen</a> and <a href="/facts/Nitrogen/Nf1QpGDz">nitrogen</a> are alpha stabilizers. <a href="/facts/Molybdenum/RX6vp2bF">Molybdenum</a>, <a href="/facts/Vanadium/UvKkKTSm">vanadium</a>, <a href="/facts/Tantalum/VwaxMm33">tantalum</a>, <a href="/facts/Niobium/3zNI8AKp">niobium</a>, <a href="/facts/Manganese/j9ELd1TL">manganese</a>, <a href="/facts/Iron/DkICCKIC">iron</a>, <a href="/facts/Chromium/6sVk6Uu7">chromium</a>, <a href="/facts/Cobalt/gqhScEw4">cobalt</a>, <a href="/facts/Nickel/KwMCHYRP">nickel</a>, <a href="/facts/Copper/I8PEE8oX">copper</a> and <a href="/facts/Silicon/cgWx0hdr">silicon</a> are beta stabilizers.<a class="footnote-ref" id="fnref:18" href="#fn:18"><sup>18</sup></a> </p> <h2 id="properties">Properties</h2> <p>Generally, beta-phase titanium is the more ductile phase and alpha-phase is stronger yet less ductile, due to the larger number of <a href="/facts/Slip_(materials_science)/P29xbKBu">slip planes</a> in the <a href="/facts/Cubic_crystal_system/92Co7BKM">bcc</a> structure of the beta-phase in comparison to the <a href="/facts/Close-packing_of_equal_spheres/AqL1HUxe">hcp</a> alpha-phase. Alpha-beta-phase titanium has a mechanical property which is in between both. </p><p><a href="/facts/Titanium_dioxide/T0KWmKcz">Titanium dioxide</a> dissolves in the metal at high temperatures, and its formation is very energetic. These two factors mean that all titanium except the most carefully purified has a significant amount of dissolved <a href="/facts/Oxygen/acyn6o8r">oxygen</a>, and so may be considered a Ti–O alloy. Oxide precipitates offer some strength (as discussed above), but are not very responsive to heat treatment and can substantially decrease the alloy's toughness. </p><p>Many alloys also contain titanium as a minor additive, but since alloys are usually categorized according to which element forms the majority of the material, these are not usually considered to be "titanium alloys" as such. See the sub-article on <a href="/facts/Titanium/53ArnDoy">titanium applications</a>. </p><p>Titanium alone is a strong, light metal. It is stronger than common, low-carbon steels, but 45% lighter. It is also twice as strong as weak aluminium alloys but only 60% heavier. Titanium has outstanding corrosion resistance to seawater, and thus is used in propeller shafts, rigging and other parts of boats that are exposed to seawater. Titanium and its alloys are used in airplanes, missiles, and rockets where strength, low weight, and resistance to high temperatures are important.<a class="footnote-ref" id="fnref:19" href="#fn:19"><sup>19</sup></a><a class="footnote-ref" id="fnref:20" href="#fn:20"><sup>20</sup></a><a class="footnote-ref" id="fnref:21" href="#fn:21"><sup>21</sup></a> </p><p>Since titanium does not react within the human body, it and its alloys are used in artificial joints, screws, and plates for fractures, and for other biological implants. See: <a href="/facts/Titanium/53ArnDoy">Titanium orthopedic implants</a>. </p> <h2 id="titanium-grades">Titanium grades</h2> <p>The <a href="/facts/ASTM_International/xzdCexYJ">ASTM International</a> standard on titanium and titanium alloy seamless pipe references the following alloys, requiring the following treatment: </p> <blockquote><p>"Alloys may be supplied in the following conditions: Grades 5, 23, 24, 25, 29, 35, or 36 annealed or aged; Grades 9, 18, 28, or 38 cold-worked and stress-relieved or annealed; Grades 9, 18, 23, 28, or 29 transformed-beta condition; and Grades 19, 20, or 21 solution-treated or solution-treated and aged."<a class="footnote-ref" id="fnref:22" href="#fn:22"><sup>22</sup></a></p></blockquote> <blockquote><p>"Note 1—H grade material is identical to the corresponding numeric grade (that is, Grade 2H = Grade 2) except for the higher guaranteed minimum <a href="/facts/Ultimate_tensile_strength/Cv2jPplR">UTS</a>, and may always be certified as meeting the requirements of its corresponding numeric grade. Grades 2H, 7H, 16H, and 26H are intended primarily for pressure vessel use."<a class="footnote-ref" id="fnref:23" href="#fn:23"><sup>23</sup></a></p></blockquote> <blockquote><p>"The H grades were added in response to a user association request based on its study of over 5200 commercial Grade 2, 7, 16, and 26 test reports, where over 99% met the 58 <a href="/facts/Ksi_(unit)/RMdeTlB0">ksi</a> minimum UTS."<a class="footnote-ref" id="fnref:24" href="#fn:24"><sup>24</sup></a></p></blockquote> Grade 1 is the most ductile and softest titanium alloy. It is a good solution for cold forming and corrosive environments. ASTM/ASME SB-265 provides the standards for commercially pure titanium sheet and plate.<a class="footnote-ref" id="fnref:25" href="#fn:25"><sup>25</sup></a> Grade 2 Unalloyed titanium, standard oxygen. Grade 2H Unalloyed titanium (Grade 2 with 58 ksi minimum UTS). Grade 3 Unalloyed titanium, medium oxygen. Grades 1-4 are unalloyed and considered commercially pure or "CP". Generally the tensile and yield strength goes up with grade number for these "pure" grades. The difference in their physical properties is primarily due to the quantity of <a href="/facts/Interstitial_elements/Io4vS0AS">interstitial elements</a>. They are used for corrosion resistance applications where cost, ease of fabrication, and welding are important. Grade 5 also known as Ti6Al4V, <a href="/facts/Ti-6Al-4V/TWYn3qda">Ti-6Al-4V</a> or Ti 6-4 not to be confused with Ti-6Al-4V-ELI (Grade 23), is the most commonly used alloy. It has a chemical composition of 6% aluminum, 4% vanadium, 0.25% (maximum) <a href="/facts/Iron/DkICCKIC">iron</a>, 0.2% (maximum) <a href="/facts/Oxygen/acyn6o8r">oxygen</a>, and the remainder titanium.<a class="footnote-ref" id="fnref:26" href="#fn:26"><sup>26</sup></a> It is significantly stronger than commercially pure titanium (grades 1-4) while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti).<a class="footnote-ref" id="fnref:27" href="#fn:27"><sup>27</sup></a> Among its many advantages, it is heat treatable. This grade is an excellent combination of strength, corrosion resistance, weld and fabricability. <blockquote><p>"This alpha-beta alloy is the workhorse alloy of the titanium industry. The alloy is fully heat treatable in section sizes up to 15 mm and is used up to approximately 400 °C (750 °F). Since it is the most commonly used alloy – over 70% of all alloy grades melted are a sub-grade of Ti6Al4V, its uses span many aerospace airframe and engine component uses and also major non-aerospace applications in the marine, offshore and power generation industries in particular."<a class="footnote-ref" id="fnref:28" href="#fn:28"><sup>28</sup></a></p></blockquote> <blockquote><p>"<i>Applications</i>: Blades, discs, rings, airframes, fasteners, components. Vessels, cases, hubs, forgings. Biomedical implants."<a class="footnote-ref" id="fnref:29" href="#fn:29"><sup>29</sup></a></p></blockquote> Generally, Ti-6Al-4V is used in applications up to 400 degrees Celsius. It has a <a href="/facts/Density/92p6hh9I">density</a> of roughly 4420 kg/m3, <a href="/facts/Young%2527s_modulus/MV5JMCIM">Young's modulus</a> of 120 GPa, and <a href="/facts/Tensile_strength/Cv2jPplR">tensile strength</a> of 1000 MPa.<a class="footnote-ref" id="fnref:30" href="#fn:30"><sup>30</sup></a> By comparison, annealed type 316 stainless steel has a density of 8000 kg/m3, modulus of 193 GPa, and tensile strength of 570 MPa.<a class="footnote-ref" id="fnref:31" href="#fn:31"><sup>31</sup></a> Tempered <a href="/facts/6061_aluminium_alloy/UnIooxgV">6061 aluminium alloy</a> has a density of 2700 kg/m3, modulus of 69 GPa, and tensile strength of 310 MPa, respectively.<a class="footnote-ref" id="fnref:32" href="#fn:32"><sup>32</sup></a> Ti-6Al-4V standard specifications include:<a class="footnote-ref" id="fnref:33" href="#fn:33"><sup>33</sup></a><a class="footnote-ref" id="fnref:34" href="#fn:34"><sup>34</sup></a> <ul><li>AMS: 4911, 4928, 4965, 4967, 6930, 6931, T-9046, T9047</li> <li>ASTM: B265, B348, F1472</li> <li>MIL: T9046 T9047</li> <li>DMS: 1592, 1570, 1583</li> <li>Boeing: BMS 7-269</li></ul> Grade 6 contains 5% aluminium and 2.5% tin. It is also known as Ti-5Al-2.5Sn. This alloy is used in airframes and jet engines due to its good weldability, stability and strength at elevated temperatures.<a class="footnote-ref" id="fnref:35" href="#fn:35"><sup>35</sup></a> Grade 7 contains 0.12 to 0.25% <a href="/facts/Palladium/P7y0ESWf">palladium</a>. This grade is similar to Grade 2. The small quantity of palladium added gives it enhanced crevice corrosion resistance at low temperatures and high <a href="/facts/PH/RnSv8D7y">pH</a>.<a class="footnote-ref" id="fnref:36" href="#fn:36"><sup>36</sup></a> Grade 7H is identical to Grade 7 (Grade 7 with 58 ksi minimum UTS). Grade 9 contains 3.0% aluminium and 2.5% vanadium. This grade is a compromise between the ease of welding and manufacturing of the "pure" grades and the high strength of Grade 5. It is commonly used in aircraft tubing for hydraulics and in athletic equipment. Grade 11 contains 0.12 to 0.25% palladium. This grade has enhanced corrosion resistance.<a class="footnote-ref" id="fnref:37" href="#fn:37"><sup>37</sup></a> Grade 12 contains 0.3% molybdenum and 0.8% nickel. This alloy has excellent weldability.<a class="footnote-ref" id="fnref:38" href="#fn:38"><sup>38</sup></a> Grades 13, 14, and 15 all contain 0.5% nickel and 0.05% <a href="/facts/Ruthenium/uzCm4ufn">ruthenium</a>. Grade 16 contains 0.04 to 0.08% palladium. This grade has enhanced corrosion resistance.<a class="footnote-ref" id="fnref:39" href="#fn:39"><sup>39</sup></a> Grade 16H is identical to Grade 16 (Grade 16 with 58 ksi minimum UTS). Grade 17 contains 0.04 to 0.08% palladium. This grade has enhanced corrosion resistance.<a class="footnote-ref" id="fnref:40" href="#fn:40"><sup>40</sup></a> Grade 18 contains 3% aluminium, 2.5% vanadium and 0.04 to 0.08% palladium. This grade is identical to Grade 9 in terms of mechanical characteristics. The added palladium gives it increased corrosion resistance.<a class="footnote-ref" id="fnref:41" href="#fn:41"><sup>41</sup></a> Grade 19 contains 3% aluminium, 8% vanadium, 6% chromium, 4% zirconium, and 4% molybdenum. Grade 20 contains 3% aluminium, 8% vanadium, 6% chromium, 4% zirconium, 4% molybdenum and 0.04% to 0.08% palladium. Grade 21 contains 15% molybdenum, 3% aluminium, 2.7% <a href="/facts/Niobium/3zNI8AKp">niobium</a>, and 0.25% silicon. Grade 23 also known as Ti-6Al-4V-ELI or TAV-ELI <p> contains 6% aluminium, 4% vanadium, 0.13% (maximum) Oxygen. ELI stands for Extra Low Interstitial. Reduced <a href="/facts/Interstitial_elements/Io4vS0AS">interstitial elements</a> <a href="/facts/Oxygen/acyn6o8r">oxygen</a> and <a href="/facts/Iron/DkICCKIC">iron</a> improve ductility and fracture toughness with some reduction in strength.<a class="footnote-ref" id="fnref:42" href="#fn:42"><sup>42</sup></a> TAV-ELI is the most commonly used medical <a href="/facts/Implant_(medicine)/3PKvy4I2">implant</a>-grade titanium alloy.<a class="footnote-ref" id="fnref:43" href="#fn:43"><sup>43</sup></a><a class="footnote-ref" id="fnref:44" href="#fn:44"><sup>44</sup></a> Due to its excellent biocompatibility, corrosion resistance, fatigue resistance, and low <a href="/facts/Elastic_modulus/Et73KjbT">modulus of elasticity</a>, which closely matches human bone,<a class="footnote-ref" id="fnref:45" href="#fn:45"><sup>45</sup></a> TAV-ELI is the most commonly used medical implant-grade titanium alloy.<a class="footnote-ref" id="fnref:46" href="#fn:46"><sup>46</sup></a> </p>Ti-6Al-4V-ELI standard specifications include:<a class="footnote-ref" id="fnref:47" href="#fn:47"><sup>47</sup></a> <ul><li>AMS: 4907, 4930, 6932, T9046, T9047</li> <li>ASTM: B265, B348, F136</li> <li>MIL: T9046 T9047</li></ul> Grade 24 contains 6% aluminium, 4% vanadium and 0.04% to 0.08% palladium. Grade 25 contains 6% aluminium, 4% vanadium and 0.3% to 0.8% nickel and 0.04% to 0.08% palladium. Grades 26, 26H, and 27 all contain 0.08 to 0.14% ruthenium. Grade 28 contains 3% aluminium, 2.5% vanadium and 0.08 to 0.14% ruthenium. Grade 29 contains 6% aluminium, 4% vanadium and 0.08 to 0.14% ruthenium. Grades 30 and 31 contain 0.3% cobalt and 0.05% palladium. Grade 32 contains 5% aluminium, 1% tin, 1% zirconium, 1% vanadium, and 0.8% molybdenum. Grades 33 and 34 contain 0.4% nickel, 0.015% palladium, 0.025% ruthenium, and 0.15% chromium. Both grades are identical but for minor difference in oxygen and nitrogen content.<a class="footnote-ref" id="fnref:48" href="#fn:48"><sup>48</sup></a> These grades contain 6 to 25 times less palladium than Grade 7 and are thus less costly, but offer similar corrosion performance thanks to the added ruthenium.<a class="footnote-ref" id="fnref:49" href="#fn:49"><sup>49</sup></a> Grade 35 contains 4.5% aluminium, 2% molybdenum, 1.6% vanadium, 0.5% iron, and 0.3% silicon. Grade 36 contains 45% niobium. Grade 37 contains 1.5% aluminium. Grade 38 contains 4% aluminium, 2.5% vanadium, and 1.5% iron. This grade was developed in the 1990s for use as an armor plating. The iron reduces the amount of Vanadium needed as a beta stabilizer. Its mechanical properties are very similar to Grade 5, but has good cold workability similar to grade 9.<a class="footnote-ref" id="fnref:50" href="#fn:50"><sup>50</sup></a> <h2 id="heat-treatment">Heat treatment</h2> <p>Titanium alloys are <a href="/facts/Heat_treating/xR2tVyTU">heat treated</a> for a number of reasons, the main ones being to increase strength by solution treatment and aging as well as to optimize special properties, such as fracture toughness, fatigue strength and high temperature creep strength. </p><p>Alpha and near-alpha alloys cannot be dramatically changed by heat treatment. Stress relief and annealing are the processes that can be employed for this class of titanium alloys. The heat treatment cycles for beta alloys differ significantly from those for the alpha and alpha-beta alloys. Beta alloys can not only be stress relieved or annealed, but also can be solution treated and aged. The alpha-beta alloys are two-phase alloys, comprising both alpha and beta phases at room temperature. Phase compositions, sizes, and distributions of phases in alpha-beta alloys can be manipulated within certain limits by heat treatment, thus permitting tailoring of properties. </p> Alpha and near-alpha alloys The micro-structure of alpha alloys cannot be strongly manipulated by heat treatment since alpha alloys undergo no significant phase change. As a result, high strength can not be acquired for the alpha alloys by heat treatment. Yet, alpha and near-alpha titanium alloys can be stress relieved and annealed. Alpha-beta alloys By working as well as heat treatment of alpha-beta alloys below or above the alpha-beta transition temperature, large micro-structural changes can be achieved. This may give a substantial hardening of the material. Solution treatment plus aging is used to produce maximum strengths in alpha-beta alloys. Also, other heat treatments, including stress-relief heat treatments, are practiced for this group of titanium alloys as well. Beta alloys In commercial beta alloys, stress-relieving and aging treatments can be combined. <h2 id="applications">Applications</h2> <h3>Aerospace structures</h3> <p>Titanium is used regularly in aviation for its resistance to <a href="/facts/Corrosion/lIC7H4we">corrosion</a> and heat, and its high strength-to-weight ratio. Titanium alloys are generally stronger than <a href="/facts/Aluminium_alloys/1EzR3Y4t">aluminium alloys</a>, while being lighter than <a href="/facts/Steel/aN6qWo4H">steel</a>. It has been used in the earliest <a href="/facts/Apollo_Program/IC1Ek1Ao">Apollo Program</a> and <a href="/facts/Project_Mercury/H8zqFzbC">Project Mercury</a>.<a class="footnote-ref" id="fnref:51" href="#fn:51"><sup>51</sup></a> </p><p>The Ti-3Al-2.5V alloy, which consists of 3% <a href="/facts/Aluminum/7wmR8jYE">aluminum</a> and 2.5% <a href="/facts/Vanadium/UvKkKTSm">vanadium</a>, was designed for low-temperature environments, maintaining high toughness and <a href="/facts/Ductility/SBJsahEk">ductility</a> even under <a href="/facts/Cryogenic/cw7dHAkp">cryogenic</a> conditions in space.<a class="footnote-ref" id="fnref:52" href="#fn:52"><sup>52</sup></a> It is used in aerospace components such as aircraft frames and <a href="/facts/Landing_gear/MGt7HeAf">landing gear</a>.<a class="footnote-ref" id="fnref:53" href="#fn:53"><sup>53</sup></a> </p> <h3>Architectural uses</h3> <p>Titanium alloys have been used occasionally in architecture, such as with the cladding of the <a href="/facts/Guggenheim_Museum/rxfpNJyc">Guggenheim Museum</a>, the architect of which being <a href="/facts/Frank_Gehry/tSunALsf">Frank Gehry</a>. </p> <h3>Biomedical</h3> <p>Titanium alloys have been extensively used for the manufacturing of metal orthopedic joint replacements and bone plate surgeries. They are normally produced from wrought or cast bar stock by <a href="/facts/Numerical_control/B2c7UbaX">CNC</a>, <a href="/facts/Computer-aided_design/5gSXrmmN">CAD</a>-driven machining, or <a href="/facts/Powder_metallurgy/tv9uXamF">powder metallurgy</a> production. Each of these techniques comes with inherent advantages and disadvantages. Wrought products come with an extensive material loss during machining into the final shape of the product and for cast samples the acquirement of a product in its final shape somewhat limits further processing and treatment (e.g. <a href="/facts/Precipitation_hardening/hxe4lpBj">precipitation hardening</a>), yet casting is more material effective. Traditional powder metallurgy methods are also more material efficient, yet acquiring fully dense products can be a common issue.<a class="footnote-ref" id="fnref:54" href="#fn:54"><sup>54</sup></a> </p><p>With the emergence of solid freeform fabrication (<a href="/facts/3D_printing/lbvWU3t0">3D printing</a>) the possibility to produce custom-designed biomedical implants (e.g. hip joints) has been realized. Tests show it's 50% stronger than the next strongest alloy of similar density used in aerospace applications.<a class="footnote-ref" id="fnref:55" href="#fn:55"><sup>55</sup></a> While it is not applied currently on a larger scale, freeform fabrication methods offers the ability to recycle waste powder (from the manufacturing process) and makes for selectivity tailoring desirable properties and thus the performance of the implant. <a href="/facts/Electron_beam_additive_manufacturing/KeyGEtuA">Electron Beam Melting</a> (EBM) and <a href="/facts/Selective_laser_melting/7sF4VSuM">Selective Laser Melting</a> (SLM) are two methods applicable for freeform fabrication of Ti-alloys. Manufacturing parameters greatly influence the microstructure of the product, where e.g. a fast cooling rate in combination with low degree of melting in SLM leads to the predominant formation of martensitic alpha-prime phase, giving a very hard product.<a class="footnote-ref" id="fnref:56" href="#fn:56"><sup>56</sup></a> </p> <a href="/facts/Ti-6Al-4V/TWYn3qda">Ti-6Al-4V</a> / Ti-6Al-4V-ELI This alloy has good biocompatibility, and is neither cytotoxic nor genotoxic.<a class="footnote-ref" id="fnref:57" href="#fn:57"><sup>57</sup></a> Ti-6Al-4V suffers from poor shear strength and poor surface wear properties in certain loading conditions:<a class="footnote-ref" id="fnref:58" href="#fn:58"><sup>58</sup></a><blockquote><p><i>Bio compatibility</i>: Excellent, especially when direct contact with tissue or bone is required. Ti-6Al-4V's poor shear strength makes it undesirable for bone screws or plates. It also has poor surface wear properties and tends to seize when in sliding contact with itself and other metals. Surface treatments such as nitriding and oxidizing can improve the surface wear properties.<a class="footnote-ref" id="fnref:59" href="#fn:59"><sup>59</sup></a></p></blockquote> <a href="/facts/Ti-6Al-7Nb/b1PNPdlp">Ti-6Al-7Nb</a> This alloy was developed as a biomedical replacement for Ti-6Al-4V, because Ti-6Al-4V contains vanadium, an element that has demonstrated cytotoxic outcomes when isolated.<a class="footnote-ref" id="fnref:60" href="#fn:60"><sup>60</sup></a>: 1 Ti-6Al-7Nb contains 6% aluminium and 7% niobium.<a class="footnote-ref" id="fnref:61" href="#fn:61"><sup>61</sup></a>: 18 <blockquote><p>Ti6Al7Nb is a dedicated high strength titanium alloy with excellent biocompatibility for surgical implants. Used for replacement hip joints, it has been in clinical use since early 1986.<a class="footnote-ref" id="fnref:62" href="#fn:62"><sup>62</sup></a></p></blockquote> <h3>Automobile industry</h3> <p>Titanium alloys are used in the automobile industry due to their outstanding characteristics. Key applications include engine components like <a href="/facts/Valves/EwgqAwlJ">valves</a> and <a href="/facts/Connecting_rods/AXp1gPdh">connecting rods</a>, <a href="/facts/Exhaust_systems/p7vXmU4B">exhaust systems</a>, suspension springs, and <a href="/facts/Fasteners/earBwoS6">fasteners</a>.<a class="footnote-ref" id="fnref:63" href="#fn:63"><sup>63</sup></a><a class="footnote-ref" id="fnref:64" href="#fn:64"><sup>64</sup></a> These alloys help reduce vehicle weight, leading to improved <a href="/facts/Fuel_efficiency/URhdQ7Wl">fuel efficiency</a> and performance.<a class="footnote-ref" id="fnref:65" href="#fn:65"><sup>65</sup></a> Additionally, titanium's <a href="/facts/Durability/HPpuqYd2">durability</a> and resistance to <a href="/facts/Corrosion/lIC7H4we">corrosion</a> extend the lifespan of automotive parts. However, the high cost and manufacturing complexity of titanium limit its use mostly to high-performance and <a href="/facts/Luxury_vehicles/nFb5l5kk">luxury vehicles</a>.<a class="footnote-ref" id="fnref:66" href="#fn:66"><sup>66</sup></a> </p> Notes Sources <h2 id="external-links">External links</h2> Wikimedia Commons has media related to Titanium-based alloys. <ul><li><a href="http://www.tifab.com/subpages/tech_spec_grades.htm">Custom Mil-Spec Defense Products</a></li> <li><a href="http://www.azom.com/article.aspx?ArticleID=2591">Datasheet for Beta Titanium</a></li> <li><a href="https://titanium.com.sg/titanium-bars-rods/">Titanium Alloy Bar</a></li> <li><a href="https://link.springer.com/article/10.1007/s11837-015-1411-y">Phase Stability and Stress-Induced Transformations in Beta Titanium Alloys </a></li> <li><a href="https://www.intemetal.com/html_news/?21-Titanium-alloys-and-types-of-titanium-alloys-21.html">Titanium alloy and types of titanium alloy</a></li></ul> <h2 id="references">References</h2> <ol> <li id="fn:1"><p>"Characteristics of Alpha, Alpha Beta and Beta Titanium Alloys". AZO Materials. 17 August 2004. <a href="http://www.azom.com/details.asp?ArticleID=2591" target="_blank">http://www.azom.com/details.asp?ArticleID=2591</a> <a href="#fnref:1" class="footnote-back-ref">↩</a></p></li> <li id="fn:2"><p>"Alpha Titanium Vs. Beta Titanium Vs. Commercially Pure Titanium". <a href="https://www.ulbrich.com/blog/alpha-titanium-vs-beta-titanium-vs-commercially-pure-titanium/" target="_blank">https://www.ulbrich.com/blog/alpha-titanium-vs-beta-titanium-vs-commercially-pure-titanium/</a> <a href="#fnref:2" class="footnote-back-ref">↩</a></p></li> <li id="fn:3"><p>Semiatin, S. L. (2020). "An Overview of the Thermomechanical Processing of α/β Titanium Alloys: Current Status and Future Research Opportunities". Metallurgical and Materials Transactions A. 51 (6): 2593–2625. Bibcode:2020MMTA...51.2593S. doi:10.1007/s11661-020-05625-3. <a href="/wiki/Bibcode_(identifier)" target="_blank">/wiki/Bibcode_(identifier)</a> <a href="#fnref:3" class="footnote-back-ref">↩</a></p></li> <li id="fn:4"><p>Yao, Xin (2016). "Quenching of Titanium and Control of Residual Stresses". Heat Treating of Nonferrous Alloys. pp. 546–554. doi:10.31399/asm.hb.v04e.a0006286. ISBN 978-1-62708-169-6. <a href="978-1-62708-169-6" target="_blank">978-1-62708-169-6</a> <a href="#fnref:4" class="footnote-back-ref">↩</a></p></li> <li id="fn:5"><p>Titanium – A Technical Guide. ASM International. 2000. ISBN 9781615030620. <a href="9781615030620" target="_blank">9781615030620</a> <a href="#fnref:5" class="footnote-back-ref">↩</a></p></li> <li id="fn:6"><p>Titanium – A Technical Guide. ASM International. 2000. ISBN 9781615030620. <a href="9781615030620" target="_blank">9781615030620</a> <a href="#fnref:6" class="footnote-back-ref">↩</a></p></li> <li id="fn:7"><p>Titanium – A Technical Guide. ASM International. 2000. ISBN 9781615030620. <a href="9781615030620" target="_blank">9781615030620</a> <a href="#fnref:7" class="footnote-back-ref">↩</a></p></li> <li id="fn:8"><p>Wang, B.; Zhou, L.; Du, J.; Cao, Y. (January 2023). "Analysis of residual stresses in electron beam welding with filler wire of Ti62A alloy". Journal of Materials Research and Technology. 23: 985–997. doi:10.1016/j.jmrt.2023.01.081. <a href="https://doi.org/10.1016%2Fj.jmrt.2023.01.081" target="_blank">https://doi.org/10.1016%2Fj.jmrt.2023.01.081</a> <a href="#fnref:8" class="footnote-back-ref">↩</a></p></li> <li id="fn:9"><p>Titanium – A Technical Guide. ASM International. 2000. ISBN 9781615030620. <a href="9781615030620" target="_blank">9781615030620</a> <a href="#fnref:9" class="footnote-back-ref">↩</a></p></li> <li id="fn:10"><p>Najdahmadi, A.; Zarei-Hanzaki, A.; Farghadani, E. (1 February 2014). "Mechanical properties enhancement in Ti–29Nb–13Ta–4.6Zr alloy via heat treatment with no detrimental effect on its biocompatibility". Materials & Design. 54: 786–791. doi:10.1016/j.matdes.2013.09.007. ISSN 0261-3069. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:10" class="footnote-back-ref">↩</a></p></li> <li id="fn:11"><p>"INVESTIGATION OF THE BEHAVIOR OF MAGNESIUM IN ARC MELTING OF TITANIUM INGOTS AT PRESSURES OF UP TO 140 ATM" (PDF). BEHAVIOR OF MAGNESIUM IN ARC MELTING. 1980. <a href="https://cdn.ymaws.com/titanium.org/resource/resmgr/ZZ-WTCP1980-VOL3/1980_Vol_3.-5-A-Investation_.pdf" target="_blank">https://cdn.ymaws.com/titanium.org/resource/resmgr/ZZ-WTCP1980-VOL3/1980_Vol_3.-5-A-Investation_.pdf</a> <a href="#fnref:11" class="footnote-back-ref">↩</a></p></li> <li id="fn:12"><p>Schmidt, F. F.; Wood, R. A. (1965). HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS BY (PDF) (TECHNICAL MEMORANDUM X-53445 ed.). GEORGE C. MARSHALL SPACE FLIGHT CENTER: NASA. <a href="https://ntrs.nasa.gov/api/citations/19660015720/downloads/19660015720.pdf" target="_blank">https://ntrs.nasa.gov/api/citations/19660015720/downloads/19660015720.pdf</a> <a href="#fnref:12" class="footnote-back-ref">↩</a></p></li> <li id="fn:13"><p>Goldberg, Jon; Burstone, Charles J. (1979). "An Evaluation of Beta Titanium Alloys for Use in Orthodontic Appliances". Journal of Dental Research. 58 (2): 593–599. doi:10.1177/00220345790580020901. PMID 283089. S2CID 29064479. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:13" class="footnote-back-ref">↩</a></p></li> <li id="fn:14"><p>Goldberg, Jon; Burstone, Charles J. (1979). "An Evaluation of Beta Titanium Alloys for Use in Orthodontic Appliances". Journal of Dental Research. 58 (2): 593–599. doi:10.1177/00220345790580020901. PMID 283089. S2CID 29064479. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:14" class="footnote-back-ref">↩</a></p></li> <li id="fn:15"><p>De Fontaine§§, D.; Paton, N.E.; Williams, J.C. (November 1971). "Transformation de la phase omega dans les alliages de titane comme exemple de reactions controlees par deplacement Die omega-phasenumwandlung in titanlegierungen als beispiel einer verschiebungskontrollierten reaktion". Acta Metallurgica. 19 (11): 1153–1162. doi:10.1016/0001-6160(71)90047-2. Retrieved 27 April 2020. <a href="https://www.sciencedirect.com/science/article/abs/pii/0001616071900472" target="_blank">https://www.sciencedirect.com/science/article/abs/pii/0001616071900472</a> <a href="#fnref:15" class="footnote-back-ref">↩</a></p></li> <li id="fn:16"><p>Ishida, Taku; Wakai, Eiichi; Makimura, Shunsuke; Casella, Andrew M.; Edwards, Danny J.; Senor, David J.; Ammigan, Kavin; Hurh, Patrick G.; Densham, Christopher J.; Fitton, Michael D.; Bennett, Joe M.; Kim, Dohyun; Simos, Nikolaos; Hagiwara, Masayuki; Kawamura, Naritoshi; Meigo, Shin-ichiro; Yohehara, Katsuya (2020). "Tensile behavior of dual-phase titanium alloys under high-intensity proton beam exposure: Radiation-induced omega phase transformation in Ti-6Al-4V". Journal of Nuclear Materials. 541: 152413. arXiv:2004.11562. Bibcode:2020JNuM..54152413I. doi:10.1016/j.jnucmat.2020.152413. S2CID 216144772. <a href="/wiki/ArXiv_(identifier)" target="_blank">/wiki/ArXiv_(identifier)</a> <a href="#fnref:16" class="footnote-back-ref">↩</a></p></li> <li id="fn:17"><p>In a titanium or titanium alloy, alpha-to-beta transition temperature is the temperature above which the beta phase becomes thermodynamically favorable. <a href="#fnref:17" class="footnote-back-ref">↩</a></p></li> <li id="fn:18"><p>Vydehi Arun Joshi. Titanium Alloys: An Atlas of Structures and Fracture Features. CRC Press, 2006. doi:10.1201/9781420006063 ISBN 978-0-429-12327-6 <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:18" class="footnote-back-ref">↩</a></p></li> <li id="fn:19"><p>Nyamekye, Patricia; Rahimpour Golroudbary, Saeed; Piili, Heidi; Luukka, Pasi; Kraslawski, Andrzej (2023-05-01). "Impact of additive manufacturing on titanium supply chain: Case of titanium alloys in automotive and aerospace industries". Advances in Industrial and Manufacturing Engineering. 6: 100112. doi:10.1016/j.aime.2023.100112. ISSN 2666-9129. <a href="https://doi.org/10.1016%2Fj.aime.2023.100112" target="_blank">https://doi.org/10.1016%2Fj.aime.2023.100112</a> <a href="#fnref:19" class="footnote-back-ref">↩</a></p></li> <li id="fn:20"><p>Gerdemann, Steven J. (2001-07-01). "TITANIUM: Process Technologies". Advanced Materials & Processes. 159 (7): 41. <a href="https://go.gale.com/ps/i.do?p=AONE&sw=w&issn=08827958&v=2.1&it=r&id=GALE%7CA76881053&sid=googleScholar&linkaccess=abs" target="_blank">https://go.gale.com/ps/i.do?p=AONE&sw=w&issn=08827958&v=2.1&it=r&id=GALE%7CA76881053&sid=googleScholar&linkaccess=abs</a> <a href="#fnref:20" class="footnote-back-ref">↩</a></p></li> <li id="fn:21"><p>"Titanium (Ti) - Chemical properties, Health and Environmental effects". www.lenntech.com. Retrieved 2023-05-11. <a href="https://www.lenntech.com/periodic/elements/ti.htm" target="_blank">https://www.lenntech.com/periodic/elements/ti.htm</a> <a href="#fnref:21" class="footnote-back-ref">↩</a></p></li> <li id="fn:22"><p>ASTM B861 – 10 Standard Specification for Titanium and Titanium Alloy Seamless Pipe (Grades 1 to 38) <a href="http://www.astm.org/Standards/B861.htm" target="_blank">http://www.astm.org/Standards/B861.htm</a> <a href="#fnref:22" class="footnote-back-ref">↩</a></p></li> <li id="fn:23"><p>ASTM B861 – 10 Standard Specification for Titanium and Titanium Alloy Seamless Pipe (Grades 1 to 38) <a href="http://www.astm.org/Standards/B861.htm" target="_blank">http://www.astm.org/Standards/B861.htm</a> <a href="#fnref:23" class="footnote-back-ref">↩</a></p></li> <li id="fn:24"><p>ASTM B861 – 10 Standard Specification for Titanium and Titanium Alloy Seamless Pipe (Grades 1 to 38) <a href="http://www.astm.org/Standards/B861.htm" target="_blank">http://www.astm.org/Standards/B861.htm</a> <a href="#fnref:24" class="footnote-back-ref">↩</a></p></li> <li id="fn:25"><p>Titanium Grades, Application <a href="http://www.unisteelsengg.com/titanium-alloys-grades-properties-and-application.html" target="_blank">http://www.unisteelsengg.com/titanium-alloys-grades-properties-and-application.html</a> <a href="#fnref:25" class="footnote-back-ref">↩</a></p></li> <li id="fn:26"><p>"Titanium-6-4". Retrieved 2009-02-19. <a href="http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641" target="_blank">http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641</a> <a href="#fnref:26" class="footnote-back-ref">↩</a></p></li> <li id="fn:27"><p>Compare Materials: Commercially Pure Titanium and 6Al-4V (Grade 5) Titanium <a href="http://www.makeitfrom.com/compare/Grade-1-3.7025-R50250-Titanium/Grade-5-Ti-6Al-4V-3.7165-R56400-Titanium/" target="_blank">http://www.makeitfrom.com/compare/Grade-1-3.7025-R50250-Titanium/Grade-5-Ti-6Al-4V-3.7165-R56400-Titanium/</a> <a href="#fnref:27" class="footnote-back-ref">↩</a></p></li> <li id="fn:28"><p>Titanium Alloys – Ti6Al4V Grade 5 <a href="http://www.azom.com/details.asp?ArticleID=1547" target="_blank">http://www.azom.com/details.asp?ArticleID=1547</a> <a href="#fnref:28" class="footnote-back-ref">↩</a></p></li> <li id="fn:29"><p>"Titanium-6-4". Retrieved 2009-02-19. <a href="http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641" target="_blank">http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641</a> <a href="#fnref:29" class="footnote-back-ref">↩</a></p></li> <li id="fn:30"><p>Material Properties Data: 6Al-4V (Grade 5) Titanium Alloy <a href="http://www.makeitfrom.com/material-properties/Grade-5-Ti-6Al-4V-3.7165-R56400-Titanium/" target="_blank">http://www.makeitfrom.com/material-properties/Grade-5-Ti-6Al-4V-3.7165-R56400-Titanium/</a> <a href="#fnref:30" class="footnote-back-ref">↩</a></p></li> <li id="fn:31"><p>Material Properties Data: Marine Grade Stainless Steel <a href="http://www.makeitfrom.com/material-properties/AISI-316-1.4401-1.4436-S31600-Stainless-Steel/" target="_blank">http://www.makeitfrom.com/material-properties/AISI-316-1.4401-1.4436-S31600-Stainless-Steel/</a> <a href="#fnref:31" class="footnote-back-ref">↩</a></p></li> <li id="fn:32"><p>Material Properties Data: 6061-T6 Aluminum <a href="http://www.makeitfrom.com/material-properties/6061-T6-Aluminum/" target="_blank">http://www.makeitfrom.com/material-properties/6061-T6-Aluminum/</a> <a href="#fnref:32" class="footnote-back-ref">↩</a></p></li> <li id="fn:33"><p>"6Al-4V Titanium". Performance Titanium Group. 15 May 2015. <a href="https://performancetitanium.com/6al-4v-grade5/" target="_blank">https://performancetitanium.com/6al-4v-grade5/</a> <a href="#fnref:33" class="footnote-back-ref">↩</a></p></li> <li id="fn:34"><p>"Ti-6Al-4V Titanium Grade 5". Service Steel Aerospace Corporation. 6 October 2020. <a href="https://www.ssa-corp.com/en/Ti-6Al-4V-Titanium-AMS-4928-UNSR56400.php" target="_blank">https://www.ssa-corp.com/en/Ti-6Al-4V-Titanium-AMS-4928-UNSR56400.php</a> <a href="#fnref:34" class="footnote-back-ref">↩</a></p></li> <li id="fn:35"><p>"Titanium Ti-5Al-2.5Sn (Grade 6) - Material Web". <a href="http://matweb.com/search/DataSheet.aspx?MatGUID=e234a0ea74ea4680b116a1bccd59ca00" target="_blank">http://matweb.com/search/DataSheet.aspx?MatGUID=e234a0ea74ea4680b116a1bccd59ca00</a> <a href="#fnref:35" class="footnote-back-ref">↩</a></p></li> <li id="fn:36"><p>"Titanium Grade 7 (Titanium Palladium alloy, Ti-IIPd)-Metals, Alloys, and Sputtering Targets". Archived from the original on 2012-04-26. Retrieved 2011-12-19. <a href="https://web.archive.org/web/20120426062139/http://www.uctend.com/products-more.asp?id=589&sid=777" target="_blank">https://web.archive.org/web/20120426062139/http://www.uctend.com/products-more.asp?id=589&sid=777</a> <a href="#fnref:36" class="footnote-back-ref">↩</a></p></li> <li id="fn:37"><p>"Titanium Grade Overview". Archived from the original on 2023-03-26. <a href="https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php" target="_blank">https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php</a> <a href="#fnref:37" class="footnote-back-ref">↩</a></p></li> <li id="fn:38"><p>"Titanium Grade Overview". Archived from the original on 2023-03-26. <a href="https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php" target="_blank">https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php</a> <a href="#fnref:38" class="footnote-back-ref">↩</a></p></li> <li id="fn:39"><p>"Active Atom Materials - Titanium Group". <a href="https://www.activeatom.com/materials-titanium.php" target="_blank">https://www.activeatom.com/materials-titanium.php</a> <a href="#fnref:39" class="footnote-back-ref">↩</a></p></li> <li id="fn:40"><p>"Active Atom Materials - Titanium Group". <a href="https://www.activeatom.com/materials-titanium.php" target="_blank">https://www.activeatom.com/materials-titanium.php</a> <a href="#fnref:40" class="footnote-back-ref">↩</a></p></li> <li id="fn:41"><p>"Active Atom Materials - Titanium Group". <a href="https://www.activeatom.com/materials-titanium.php" target="_blank">https://www.activeatom.com/materials-titanium.php</a> <a href="#fnref:41" class="footnote-back-ref">↩</a></p></li> <li id="fn:42"><p>"Titanium Grade Overview". Archived from the original on 2023-03-26. <a href="https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php" target="_blank">https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php</a> <a href="#fnref:42" class="footnote-back-ref">↩</a></p></li> <li id="fn:43"><p>"Titanium Grade Overview". Archived from the original on 2023-03-26. <a href="https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php" target="_blank">https://web.archive.org/web/20230326023104/http://www.supraalloys.com/titanium-grades.php</a> <a href="#fnref:43" class="footnote-back-ref">↩</a></p></li> <li id="fn:44"><p>"6Al-4V-ELI Titanium". Performance Titanium Group. 15 May 2015. <a href="https://performancetitanium.com/6al-4v-eli/" target="_blank">https://performancetitanium.com/6al-4v-eli/</a> <a href="#fnref:44" class="footnote-back-ref">↩</a></p></li> <li id="fn:45"><p>Dallago, M.; Fontanari, V. (2018). "Fatigue and biological properties of Ti-6Al-4V ELI cellular structures with variously arranged cubic cells made by selective laser melting". Journal of the Mechanical Behavior of Biomedical Materials. 78: 381–394. doi:10.1016/j.jmbbm.2017.11.044. hdl:11572/190389. PMID 29220822. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:45" class="footnote-back-ref">↩</a></p></li> <li id="fn:46"><p>"Precision Engineering with Grade 23 Titanium: Ti-6Al-4V-ELI's Role in High-Performance Machinery". Stanford Powders. Retrieved Aug 25, 2024. <a href="https://powder.samaterials.com/grade-23-titanium-ti-6al-4v-eli-role-in-machinery.html" target="_blank">https://powder.samaterials.com/grade-23-titanium-ti-6al-4v-eli-role-in-machinery.html</a> <a href="#fnref:46" class="footnote-back-ref">↩</a></p></li> <li id="fn:47"><p>"6Al-4V-ELI Titanium". Performance Titanium Group. 15 May 2015. <a href="https://performancetitanium.com/6al-4v-eli/" target="_blank">https://performancetitanium.com/6al-4v-eli/</a> <a href="#fnref:47" class="footnote-back-ref">↩</a></p></li> <li id="fn:48"><p>"Active Atom Materials - Titanium Group". <a href="https://www.activeatom.com/materials-titanium.php" target="_blank">https://www.activeatom.com/materials-titanium.php</a> <a href="#fnref:48" class="footnote-back-ref">↩</a></p></li> <li id="fn:49"><p>T. Lian; T. Yashiki; T. Nakayama; T. Nakanishi; R. B. Rebak (2006-07-23). Comparative corrosion behavior of two palladium-containing titanium alloys. ASME Pressure Vessels and Piping Conference. Vancouver. <a href="https://www.osti.gov/servlets/purl/888858" target="_blank">https://www.osti.gov/servlets/purl/888858</a> <a href="#fnref:49" class="footnote-back-ref">↩</a></p></li> <li id="fn:50"><p>"Grade 38 Titanium: A High-Strength and Corrosion-Resistant Alloy". Stanford Advanced Materials. <a href="https://www.samaterials.com/grade-38-titanium-a-high-strength-and-corrosion-resistant-alloy.html" target="_blank">https://www.samaterials.com/grade-38-titanium-a-high-strength-and-corrosion-resistant-alloy.html</a> <a href="#fnref:50" class="footnote-back-ref">↩</a></p></li> <li id="fn:51"><p>"Preparations for the First Manned Apollo Mission". NASA. Retrieved June 26, 2024. <a href="https://www.hq.nasa.gov/pao/History/SP-4205/ch8-7.html" target="_blank">https://www.hq.nasa.gov/pao/History/SP-4205/ch8-7.html</a> <a href="#fnref:51" class="footnote-back-ref">↩</a></p></li> <li id="fn:52"><p>Trento, Chin (Apr 12, 2024). "Titanium Used in the Aerospace Industry". Stanford Advanced Materials. Retrieved June 26, 2024. <a href="https://www.samaterials.com/content/which-titanium-is-used-in-aircrafts.html" target="_blank">https://www.samaterials.com/content/which-titanium-is-used-in-aircrafts.html</a> <a href="#fnref:52" class="footnote-back-ref">↩</a></p></li> <li id="fn:53"><p>Zhao, Qinyan; Sun, Qiaoyan (2022). "High-strength titanium alloys for aerospace engineering applications: A review on melting-forging process". Materials Science and Engineering. 845. doi:10.1016/j.msea.2022.143260. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:53" class="footnote-back-ref">↩</a></p></li> <li id="fn:54"><p>Murr, L. E.; Quinones, S. A.; Gaytan, S. M.; Lopez, M. I.; Rodela, A.; Martinez, E. Y.; Hernandez, D. H.; Martinez, E.; Medina, F. (2009-01-01). "Microstructure and mechanical behavior of Ti–6Al–4V produced by rapid-layer manufacturing, for biomedical applications". Journal of the Mechanical Behavior of Biomedical Materials. 2 (1): 20–32. doi:10.1016/j.jmbbm.2008.05.004. PMID 19627804. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:54" class="footnote-back-ref">↩</a></p></li> <li id="fn:55"><p>Noronha, Jordan; Dash, Jason; Rogers, Jason; Leary, Martin; Brandt, Milan; Qian, Ma (2024-01-07). "Titanium Multi-Topology Metamaterials with Exceptional Strength". Advanced Materials. 36 (34): e2308715. Bibcode:2024AdM....3608715N. doi:10.1002/adma.202308715. ISSN 0935-9648. PMID 38160263. <a href="https://doi.org/10.1002%2Fadma.202308715" target="_blank">https://doi.org/10.1002%2Fadma.202308715</a> <a href="#fnref:55" class="footnote-back-ref">↩</a></p></li> <li id="fn:56"><p>Murr, L. E.; Quinones, S. A.; Gaytan, S. M.; Lopez, M. I.; Rodela, A.; Martinez, E. Y.; Hernandez, D. H.; Martinez, E.; Medina, F. (2009-01-01). "Microstructure and mechanical behavior of Ti–6Al–4V produced by rapid-layer manufacturing, for biomedical applications". Journal of the Mechanical Behavior of Biomedical Materials. 2 (1): 20–32. doi:10.1016/j.jmbbm.2008.05.004. PMID 19627804. <a href="/wiki/Doi_(identifier)" target="_blank">/wiki/Doi_(identifier)</a> <a href="#fnref:56" class="footnote-back-ref">↩</a></p></li> <li id="fn:57"><p>Velasco-Ortega, E (Sep 2010). "In vitro evaluation of cytotoxicity and genotoxicity of a commercial titanium alloy for dental implantology". Mutat. Res. 702 (1): 17–23. Bibcode:2010MRGTE.702...17V. doi:10.1016/j.mrgentox.2010.06.013. PMID 20615479. <a href="/wiki/Bibcode_(identifier)" target="_blank">/wiki/Bibcode_(identifier)</a> <a href="#fnref:57" class="footnote-back-ref">↩</a></p></li> <li id="fn:58"><p>"Titanium-6-4". Retrieved 2009-02-19. <a href="http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641" target="_blank">http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641</a> <a href="#fnref:58" class="footnote-back-ref">↩</a></p></li> <li id="fn:59"><p>"Titanium-6-4". Retrieved 2009-02-19. <a href="http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641" target="_blank">http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641</a> <a href="#fnref:59" class="footnote-back-ref">↩</a></p></li> <li id="fn:60"><p>The fatigue resistance of commercially pure titanium(grade II), titanium alloy (Ti6Al7Nb) and conventional cobalt-chromium cast clasps by Mali Palanuwech; Inaugural-Dissertation zur Erlangung des Doktorgrades der Zahnheilkunde der Medizinschen Fakultät der Eberhard-Karls-Universität zu Tübingenvorgelegt; Munich (2003). Retrieved 8 September 2012 <a href="http://tobias-lib.uni-tuebingen.de/volltexte/2003/844/pdf/palanuwech_complete.pdf" target="_blank">http://tobias-lib.uni-tuebingen.de/volltexte/2003/844/pdf/palanuwech_complete.pdf</a> <a href="#fnref:60" class="footnote-back-ref">↩</a></p></li> <li id="fn:61"><p>The fatigue resistance of commercially pure titanium(grade II), titanium alloy (Ti6Al7Nb) and conventional cobalt-chromium cast clasps by Mali Palanuwech; Inaugural-Dissertation zur Erlangung des Doktorgrades der Zahnheilkunde der Medizinschen Fakultät der Eberhard-Karls-Universität zu Tübingenvorgelegt; Munich (2003). Retrieved 8 September 2012 <a href="http://tobias-lib.uni-tuebingen.de/volltexte/2003/844/pdf/palanuwech_complete.pdf" target="_blank">http://tobias-lib.uni-tuebingen.de/volltexte/2003/844/pdf/palanuwech_complete.pdf</a> <a href="#fnref:61" class="footnote-back-ref">↩</a></p></li> <li id="fn:62"><p>Titanium Alloys – Ti6Al7Nb Properties and Applications. Retrieved 8 September 2012 <a href="http://www.azom.com/article.aspx?ArticleID=2064" target="_blank">http://www.azom.com/article.aspx?ArticleID=2064</a> <a href="#fnref:62" class="footnote-back-ref">↩</a></p></li> <li id="fn:63"><p>"Applications Of Titanium Alloy In The Automobile Industry". Advanced Refractory Metals. March 2018. Retrieved July 6, 2024. <a href="https://www.refractorymetal.org/applications-of-titanium-alloy-in-automobile-industry/" target="_blank">https://www.refractorymetal.org/applications-of-titanium-alloy-in-automobile-industry/</a> <a href="#fnref:63" class="footnote-back-ref">↩</a></p></li> <li id="fn:64"><p>Ian Polmear (2005). Light Alloys: From Traditional Alloys to Nanocrystals. Elsevier. p. 361. ISBN 978-0-7506-6371-7. <a href="978-0-7506-6371-7" target="_blank">978-0-7506-6371-7</a> <a href="#fnref:64" class="footnote-back-ref">↩</a></p></li> <li id="fn:65"><p>Yamashita, Yoshito; Takayama, Isamu (2002). "Applications and Features of titanium for automobile industry" (PDF). Nippon Steel. Retrieved July 6, 2024. <a href="https://www.nipponsteel.com/en/tech/report/nsc/pdf/8503.pdf" target="_blank">https://www.nipponsteel.com/en/tech/report/nsc/pdf/8503.pdf</a> <a href="#fnref:65" class="footnote-back-ref">↩</a></p></li> <li id="fn:66"><p>Nyamekye, Patricia; Golroudbary, S. R. (2023). "Impact of additive manufacturing on titanium supply chain: Case of titanium alloys in automotive and aerospace industries". Advances in Industrial and Manufacturing Engineering. 6. doi:10.1016/j.aime.2023.100112. <a href="https://doi.org/10.1016%2Fj.aime.2023.100112" target="_blank">https://doi.org/10.1016%2Fj.aime.2023.100112</a> <a href="#fnref:66" class="footnote-back-ref">↩</a></p></li> </ol>