<?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">OJMetal</journal-id><journal-title-group><journal-title>Open Journal of Metal</journal-title></journal-title-group><issn pub-type="epub">2164-2761</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojmetal.2013.32003</article-id><article-id pub-id-type="publisher-id">OJMetal-32778</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>
 
 
  Technological Basics for Production of Low-Temperature Superconductors
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>erman</surname><given-names>Leonidovich Kolmogorov</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>Victor</surname><given-names>Nicolaevich Trofimov</given-names></name></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Tatyana</surname><given-names>Vyacheslavovna Chernova</given-names></name></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Natalia</surname><given-names>Alexandrovna Kosheleva</given-names></name></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Yulia</surname><given-names>Alexandrovna Burdina</given-names></name></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Marina</surname><given-names>Victorovna Snigireva</given-names></name></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Natalya</surname><given-names>Fridrihovna Bolshakova</given-names></name></contrib></contrib-group><aff id="aff1"><addr-line>Department Dynamics and Strength of Machines, Perm National Research Polytechnic University, Perm, Russia</addr-line></aff><pub-date pub-type="epub"><day>08</day><month>06</month><year>2013</year></pub-date><volume>03</volume><issue>02</issue><fpage>19</fpage><lpage>22</lpage><history><date date-type="received"><day>February</day>	<month>3,</month>	<year>2013</year></date><date date-type="rev-recd"><day>March</day>	<month>10,</month>	<year>2013</year>	</date><date date-type="accepted"><day>March</day>	<month>21,</month>	<year>2013</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>
 
 
  The technological principles of low-temperature superconductor production for the magnetic system of the International Thermonuclear Experimental Reactor (ITER) that provides continuity of a superconductor billet in the superconductor production are considered.
   
 
</p></abstract><kwd-group><kwd>Superconducting Materials; Optimization; Thermoelastic State; Plastic Deformation; Drawing</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Now, in Russia, industrial production of low-temperature superconducting materials (LTSM) for the magnetic system of the international thermonuclear experimental reactor (ITER), the construction of which started in the Atomic Center of Cadarache in France [<xref ref-type="bibr" rid="scirp.32778-ref1">1</xref>] is organized. This production is directly relevant to the field of modern nanotechnologies. The total number of superconducting materials for the ITER magnetic system is over 700 tons [<xref ref-type="bibr" rid="scirp.32778-ref2">2</xref>].</p><p>Technical superconducting cables are complex composite structures made of dissimilar materials with ultrathin fibers (fractions of microns) of the superconducting material. <xref ref-type="fig" rid="fig1">Figure 1</xref> shows the structure of one of the superconductors. For the ITER, it is planned to produce low-temperature superconductors based on Nb-Ti and Nb<sub>3</sub>Sn.</p><p>Composite superconductors are transversely-isotropic medium consisting of a core which comprises superconducting fibers, and a current-stabilizing shell of ultrapure copper. The basic mechanical and thermal characteristics of the transversely-isotropic medium are defined by equations [<xref ref-type="bibr" rid="scirp.32778-ref3">3</xref>] of composite mechanics.</p></sec><sec id="s2"><title>2. Technological Basics</title><p>The manufacturing technology of superconductors is the plastic deformation of metals using metal forming methods, in particular, extrusion of a combined billet and its</p><p>repeated drawing. The highest labour input is accounted for drawing. The drawing process means drawing a billet through a conical drawing tool, and the total number of stages in superconductor production reaches several dozens.</p><p>In drawing the plastic deformation is characterized by the draw ratio that for random i-th pass is as follows:</p><disp-formula id="scirp.32778-formula53824"><label>(1)</label><graphic position="anchor" xlink:href="2-1840047\aad269f7-43c0-4e2f-8ecf-b727b734407f.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="2-1840047\0f8c3cef-30cf-4b3a-b493-3736023b61da.jpg" /> and <img src="2-1840047\f225af8d-74f7-46b6-b219-2186a5db9c10.jpg" /> are cross-sectional area before and after the pass; <img src="2-1840047\3a7422d4-18eb-496e-ad63-975413a5c74a.jpg" />is the diameter of the billet before entering the drawing tool; <img src="2-1840047\e6f05755-ad53-4ceb-902a-e0c3a355bad3.jpg" />is the diameter of the billet at the output of the tool.</p><p>In repeated drawing the aggregate draw is determined by the area ratio of the original superconductor billet <img src="2-1840047\f5474db1-a23f-4055-bb37-89ad0bb25348.jpg" /> and the finished superconductor of cross Section<img src="2-1840047\78433acf-8936-454f-9f3b-243f7437077f.jpg" />; the aggregate draw being determined through draw ratios for individual passes by the relation:</p><disp-formula id="scirp.32778-formula53825"><label>(2)</label><graphic position="anchor" xlink:href="2-1840047\20135657-4ec3-4992-9df9-bb982e0a7648.jpg"  xlink:type="simple"/></disp-formula><p>where n is the total number of passes in drawing.</p><p>To assess the manufacturing complexity of superconductor products, in the case of realization of equal draw ratios on the route of multiple deformation of the superconductor billet, the averaged around technological cycle draw ratio λ<sub>av</sub> is introduced. Then from equation (2) for the averaged draw ratio the aggregate draw will be:</p><disp-formula id="scirp.32778-formula53826"><label>(3)</label><graphic position="anchor" xlink:href="2-1840047\6eef59ef-f0c5-4ad3-9431-bf67db998be1.jpg"  xlink:type="simple"/></disp-formula><p>From equation (3) the number of repeated drawing passes required to produce a superconducting product is determined</p><disp-formula id="scirp.32778-formula53827"><label>(4)</label><graphic position="anchor" xlink:href="2-1840047\44c0eb1b-677e-4322-aa07-58a1c69370e1.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="2-1840047\2bdc9dbd-4aea-4588-aac4-76b21c465aeb.jpg" /> and <img src="2-1840047\c3c9f171-216e-4c28-ab86-5184321d9335.jpg" /> are diameters of the superconductor billet and the finished superconductor respectively.</p><p>From (4) it follows that with the increase of single drawing the number of passes is reduced which is more technologically advanced and cost effective. However, single drawing increases danger of breakage of the billet front end to which the drawing force is applied.</p><p>Following are the calculated values of the number of passes depending on the values of single drawing by the billet deformation after pressing from the diameter d<sub>0</sub> = 70 mm to the final diameter of the superconducting product <img src="2-1840047\2bafa6cf-f44c-432b-a63b-9e5fc6edc69d.jpg" /> mm.</p><p><img src="2-1840047\a4531289-bc24-4aed-a2a4-7d8091c95c29.jpg" /></p><p>Taking into account the complex structure of the superconductor billet, the draw recommended while manufacturing is<img src="2-1840047\7783b4fe-321d-4e9e-9520-d8ed2ff7c94c.jpg" />.</p><p>From Equation (1) for the given <img src="2-1840047\10bb51c8-f093-462c-9d90-58dc341b3a7b.jpg" /> pass routes are defined:</p><disp-formula id="scirp.32778-formula53828"><label>(5)</label><graphic position="anchor" xlink:href="2-1840047\a9f2b474-b599-4852-a83a-f066aca6b075.jpg"  xlink:type="simple"/></disp-formula><p>Optimization of drawing routs allows you to achieve the following objectives:</p><p>• reduce the number of the route passes;</p><p>• avoid breakage of long-length billets;</p><p>• improve quality of the surface of superconductor products;</p><p>• increase durability of the drawing tool.</p><p>In the processing of metals by pressure it is the deformation degree that largely defines energy-power and technological parameters of plastic deformation.</p><p>In [<xref ref-type="bibr" rid="scirp.32778-ref4">4</xref>] there is a formula proposed for determining the average over cross section deformation degree in drawing axisymmetric superconductor products:</p><disp-formula id="scirp.32778-formula53829"><label>(6)</label><graphic position="anchor" xlink:href="2-1840047\79c2d06f-ea11-411e-a319-d241b3b22d55.jpg"  xlink:type="simple"/></disp-formula><p>where α<sub>v</sub> is the inclination angle of a forming of the tool to the drawing axis; <img src="2-1840047\83a1104a-6877-4b4d-b433-87d7d8bd19f7.jpg" />is the outer diameter before the pass; <img src="2-1840047\8a07ac4b-f3ea-4119-8071-079aab8e4fab.jpg" />is the outer diameter after the pass.</p><p>Realizing the technology of drawing superconductor composite billets requires knowledge of deformation temperature conditions. In repeated drawing, the billet temperature changes due to the deformation heat up in each pass and it is determined by the terms of cooling between passes. Knowledge of the temperature mode is necessary to assess the thermoelastic state of a multi-component billet and prevent possible shell detachment from the core.</p><p>To determine the heat of the metal wire under deformation it is necessary to define the work spent on the deformation, as</p><disp-formula id="scirp.32778-formula53830"><label>(7)</label><graphic position="anchor" xlink:href="2-1840047\eeb9dd24-d237-4de2-bf1f-b3f142ccd232.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="2-1840047\3bef33fa-8125-4c49-b851-46a2f72175dd.jpg" /> is resistance to deformation generally based on the deformation degree.</p><p>If you accept that all plastic deformation work goes into heat, then the temperature raise for a volume unit of the material element during the adiabatic process of deformation is defined by the equation:</p><disp-formula id="scirp.32778-formula53831"><label>(8)</label><graphic position="anchor" xlink:href="2-1840047\f4414662-4ff8-4d96-9c30-a4b64108a8fe.jpg"  xlink:type="simple"/></disp-formula><p>where c is the specific heat of the drawn metal; <img src="2-1840047\9089ba88-8886-4fea-becc-9a0f35468e2d.jpg" />is the metal density.</p><p>In deformation heat up the shell may be detached from the core due to the difference of thermophysical properties of their materials. To evaluate possible detachment and prevent it in the manufacturing process the thermoelastic state of the bimetallic superconductor billet is considered (see <xref ref-type="fig" rid="fig1">Figure 1</xref>).</p><p>The thermoelastic state of an axisymmetric body is described by equations of the elasticity theory [<xref ref-type="bibr" rid="scirp.32778-ref5">5</xref>], and the strain tensor components are as follows:</p><disp-formula id="scirp.32778-formula53832"><label>(9)</label><graphic position="anchor" xlink:href="2-1840047\c8f491ea-5d0e-42c9-b926-155ad5b7a55e.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="2-1840047\4d65f9a5-a456-423e-908b-f101f046ef90.jpg" /> are normal stress tensor components; <img src="2-1840047\239850c9-c8d3-4362-9346-eabf529847bf.jpg" />are relative deformations in the corresponding direction; α is thermal expansion coefficient; T is temperature; E is modulus of elasticity; ν is Poisson’s ratio.</p><p>Because of symmetry shear strains and shear stresses equal zero. In the manufacture of long-length products axial deformation also equals zero<img src="2-1840047\1753f0e3-fdce-4007-80ab-3e6d5170748c.jpg" />. From this condition it follows that:</p><disp-formula id="scirp.32778-formula53833"><label>(10)</label><graphic position="anchor" xlink:href="2-1840047\3a5dcce7-e4ac-4182-a4bf-e4e7e7df9364.jpg"  xlink:type="simple"/></disp-formula><p>In view of equation (10) the Ratios (9) are converted to the following:</p><disp-formula id="scirp.32778-formula53834"><label>(11)</label><graphic position="anchor" xlink:href="2-1840047\47bd1300-6504-4968-8393-7f41f8db0bf5.jpg"  xlink:type="simple"/></disp-formula><p>Under the action of temperature in the axisymmetrical billet radial displacements arise defining the components of the radial deformation tensor:</p><disp-formula id="scirp.32778-formula53835"><label>(12)</label><graphic position="anchor" xlink:href="2-1840047\6e5dd334-25b2-4ed0-b213-71b95aefe56e.jpg"  xlink:type="simple"/></disp-formula><p>where u is displacement; r is radial coordinate.</p><p>The differential equation for radial displacements in the axisymmetrical problem of thermoelasticity [<xref ref-type="bibr" rid="scirp.32778-ref5">5</xref>] is as follows:</p><disp-formula id="scirp.32778-formula53836"><label>(13)</label><graphic position="anchor" xlink:href="2-1840047\0da67a1a-269b-492c-bbf0-6c20098c353b.jpg"  xlink:type="simple"/></disp-formula><p>Equation (13) is addressed separately for the core, with the average temperature over the cross section T<sub>c</sub> and for the shell, with the average temperature over thickness T<sub>0</sub>. Temperatures T<sub>c</sub> and T<sub>0</sub> are determined from the deformation conditions in the technological tool, with the different ratio of temperatures T<sub>c</sub> and T<sub>0</sub> depending on the thermal and mechanical properties of bimetallic billet components.</p><p>From Equation (13) taking into account Ratios (11) and (12) it follows that:</p><disp-formula id="scirp.32778-formula53837"><label>(14)</label><graphic position="anchor" xlink:href="2-1840047\3cc92e84-2a16-4239-9d0b-57425c71a359.jpg"  xlink:type="simple"/></disp-formula><p>Expressions (14) are used independently for the core and for the shell. The constants of integration <img src="2-1840047\e6e7eb7f-3b32-48ae-920a-82fdc761bf60.jpg" /> and <img src="2-1840047\659e2c96-4bc8-4770-8a4a-f96c026de7fd.jpg" /><sub> </sub>&#160;are determined from the corresponding boundary conditions. For example, for the core we believe <img src="2-1840047\2e72ed7f-7df8-47b4-9190-3f57526ac018.jpg" />because <img src="2-1840047\67c73fa6-789e-4c96-a11a-fa34e0f4791d.jpg" /> when<img src="2-1840047\ba7e0a06-d02e-40c5-a62d-6da2c7fb3aea.jpg" />. We also assume that at the output of the drawing tool the core and the shell contact without force interaction, i.e.<img src="2-1840047\f6ba4bfd-3802-4bbf-9567-a1222b314016.jpg" />. Defining constants <img src="2-1840047\68c9bb8e-a4f2-4d1e-85c9-bf31a9140633.jpg" /> and<img src="2-1840047\400b04e7-e43e-4127-88ac-9eb390783b84.jpg" />, we obtain the formula for the core:</p><disp-formula id="scirp.32778-formula53838"><label>(15)</label><graphic position="anchor" xlink:href="2-1840047\71ef8773-1511-4a65-a7b1-a5170940564f.jpg"  xlink:type="simple"/></disp-formula><p>Accordingly for the shell we use boundary conditions to determine integration constants<img src="2-1840047\11807991-9775-4562-b240-7a35a64bd19c.jpg" />.</p><p>After determining the integration constants we obtain expressions for the shell:</p><disp-formula id="scirp.32778-formula53839"><label>(16)</label><graphic position="anchor" xlink:href="2-1840047\58fa66d6-f5e7-4462-b828-7d05a24c2eef.jpg"  xlink:type="simple"/></disp-formula><p>Possible gap between the core and the shell is determined by the size of radial displacements at the core-shell edge. From equation system (15) for r = r<sub>(c)</sub> we have</p><disp-formula id="scirp.32778-formula53840"><label>(17)</label><graphic position="anchor" xlink:href="2-1840047\97ca7613-1cb0-44ed-8d4c-49c1f31da91d.jpg"  xlink:type="simple"/></disp-formula><p>Respectively of the expressions (16) for the shell when r = r<sub>(c)</sub> we get:</p><disp-formula id="scirp.32778-formula53841"><label>(18)</label><graphic position="anchor" xlink:href="2-1840047\ce88fc38-462e-456f-831c-4d1593c51314.jpg"  xlink:type="simple"/></disp-formula><p>In case of equality of displacements <img src="2-1840047\f129c02d-61c6-4c48-ac40-4a0573b1e6c6.jpg" /><sub> </sub>the contact in the bimetallic billet is maintained. When <img src="2-1840047\042b0a49-7102-4cfc-a0ed-e3c553759f5c.jpg" /> there appears a gap which is undesirable. The most favorable condition is<img src="2-1840047\f156d539-7fcc-4cf3-b6c9-7802a44f8fab.jpg" />. It provides contact radial compressive stresses that help increase the metal core plasticity in deformation on subsequent passes. Thus, from the standpoint of thermoelasticity of bimetallic billets in drawing the most favorable ratio is [<xref ref-type="bibr" rid="scirp.32778-ref6">6</xref>].</p><disp-formula id="scirp.32778-formula53842"><label>(19)</label><graphic position="anchor" xlink:href="2-1840047\ffe4039c-925c-48fe-9d76-0353d30c6a69.jpg"  xlink:type="simple"/></disp-formula><p>Ratio (19) is recommended for technological calculations in order to preserve the continuity of a bimetallic billet while being drawn. Equations (15) and (16) may be used to determine the stress state of bimetallic billet components.</p></sec><sec id="s3"><title>3. Conclusion</title><p>The technological principles of low-temperature superconductor production for the magnetic system of the International thermonuclear experimental reactor (ITER) are outlined. Based on thermoelasticity equations, temperature modes in the superconductor production are established, which provides continuity of a bimetallic superconductor billet.</p></sec><sec id="s4"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.32778-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Chepetsky Mechanical Plant, “Superconductivity: The Experience of Organization of the High-Tech Production Capacities in JSC Chepetsky Mechanical Plant,” Nanotechnology, Environmental Science, No. 1, 2009, pp. 80-83.</mixed-citation></ref><ref id="scirp.32778-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">A. K. Shikov, A. D. Nikulin and A. G. Silaev, “Development of Superconductors for ITER Magnet System in Russia,” Izvestia Vyssih Ucebnyh Zavedenij. 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