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<article article-type="research-article" dtd-version="1.3" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xml:lang="ru"><front><journal-meta><journal-id journal-id-type="publisher-id">alternative</journal-id><journal-title-group><journal-title xml:lang="ru">Альтернативная энергетика и экология (ISJAEE)</journal-title><trans-title-group xml:lang="en"><trans-title>Alternative Energy and Ecology (ISJAEE)</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1608-8298</issn><publisher><publisher-name>Международный издательский дом научной периодики "Спейс</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.15518/isjaee.2017.25-27.045-059</article-id><article-id custom-type="elpub" pub-id-type="custom">alternative-1183</article-id><article-categories><subj-group subj-group-type="heading"><subject>Research Article</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="ru"><subject>ЭКОЛОГИЧЕСКИЕ АСПЕКТЫ ЭНЕРГЕТИКИ</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>ENVIRONMENTAL ASPECTS OF ENERGY</subject></subj-group></article-categories><title-group><article-title>ИСПАРИТЕЛЬНАЯ СИСТЕМА КРИООБЕСПЕЧЕНИЯ ПРОТЯЖЁННЫХ СИЛОВЫХ ВТСП КАБЕЛЕЙ</article-title><trans-title-group xml:lang="en"><trans-title>EVAPORATIVE CRYOGENIC SYSTEM FOR HIGH POWER HTS LONG EXTENSION CABLES</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Костюк</surname><given-names>В. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Kostyuk</surname><given-names>V. V.</given-names></name></name-alternatives><bio xml:lang="ru"><p>д-р техн. наук, профессор, академик Российской академии наук, советник президента РАН</p></bio><bio xml:lang="en"><p>D.Sc. (engineering), Academician of the Russian Academy of Sciences, the Adviser to the President RAS</p></bio><email xlink:type="simple">cryogen204@mail.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Фирсов</surname><given-names>В. П.</given-names></name><name name-style="western" xml:lang="en"><surname>Firsov</surname><given-names>V. P.</given-names></name></name-alternatives><bio xml:lang="ru"><p>сотрудник кафедры авиационной и космической теплотехники, руководитель отдела криогенных систем</p></bio><bio xml:lang="en"><p>Employee of the Department of Aviation and Space Thermal Engineering, Head of the Cryogenic Systems SIC of Moscow Aviation Institute; scientific experience more than 40 years; a member of working out a number of systems for missile and space programs “NL”, “Proton”, “EnergyBuran”, “Angara”, etc.</p></bio><email xlink:type="simple">cryogen204@mail.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Антюхов</surname><given-names>И. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Antyukhov</surname><given-names>I. V.</given-names></name></name-alternatives><bio xml:lang="ru"><p>научный сотрудник кафедры авиационной и космической теплотехники</p></bio><bio xml:lang="en"><p>Researcher at the Department of Aviation Space Thermotechnics</p></bio><email xlink:type="simple">cryogen204@mail.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Галеев</surname><given-names>А. Г.</given-names></name><name name-style="western" xml:lang="en"><surname>Galeev</surname><given-names>A. G.</given-names></name></name-alternatives><bio xml:lang="ru"><p>д-р техн. наук, профессор, профессор кафедры «Управление эксплуатацией РКС» Московского авиационного института, главный научный сотрудник ФКП «НИЦ РКП», действительный член Российской академии космонавтики им.К.Э. Циолковского</p></bio><bio xml:lang="en"><p>D.Sc. (engineering), Professor, Professor of Management of Operation of RSS department of Moscow Aviation Institute, Chief Researcher of the PCF “SIC RSI”, a Member of the K.E. Tsiolkovsky Russian Academy of Cosmonautics; 40 years of scientific and pedagogical experience; a member of working out a number of systems for missile and space programs “Space-1”, “Space-3”, “N1L3”, “EnergiaBuran”, “GSLV”, “Angara”, etc</p></bio><email xlink:type="simple">cryogen204@mail.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>ФГБОУ ВО Московский авиационный институт (национальный исследовательский университет)</institution><country>Россия</country></aff><aff xml:lang="en"><institution>Moscow aviation Institute (National Research University)</institution><country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2017</year></pub-date><pub-date pub-type="epub"><day>10</day><month>12</month><year>2017</year></pub-date><volume>0</volume><issue>25-27</issue><fpage>45</fpage><lpage>59</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Международный издательский дом научной периодики "Спейс, 2017</copyright-statement><copyright-year>2017</copyright-year><copyright-holder xml:lang="ru">Международный издательский дом научной периодики "Спейс</copyright-holder><copyright-holder xml:lang="en">Международный издательский дом научной периодики "Спейс</copyright-holder><license xlink:href="https://www.isjaee.com/jour/about/submissions#copyrightNotice" xlink:type="simple"><license-p>https://www.isjaee.com/jour/about/submissions#copyrightNotice</license-p></license></permissions><self-uri xlink:href="https://www.isjaee.com/jour/article/view/1183">https://www.isjaee.com/jour/article/view/1183</self-uri><abstract><p>Проведен анализ результатов теоретических и экспериментальных исследований испарительной системы криообеспечения применительно к протяженным каналам термостатирования высокотемпературных сверхпроводящих кабелей и гибридных энергетических магистралей, а также систем поддержания теплового режима компонентов криогенного топлива в баках летательных аппаратов при длительных космических полётах. Представлены экспериментальные данные, полученные на азоте и водороде. Показана важность таких исследований для практического применения при создании современных систем криостатирования. Рассмотрена конструкция экспериментальной гибридной энергетической магистрали для исследования процессов термостатирования сверхпроводящих кабельных линий высокой мощности. Магистраль состоит из трех участков с различными типами теплоизоляции и токовых вводов, которые обеспечивают подвод электрического тока большой мощности к сверхпроводящим жилам с минимальным внешним теплопритоком. Получены уникальные экспериментальные данные по теплопритокам с внешней поверхности магистрали на разных ее участках. Показано, что на участке с испарительной системой криостатирования возможно полностью компенсировать внешний теплоприток в криогенную магистраль и при необходимости понизить температуру криогенного теплоносителя. С помощью математической модели, описывающей физические процессы в канале термостатирования с испарительной системой криостатирования, были проведены оценочные расчеты при использовании в качестве рабочего тела жидкого азота и жидкого водорода для различных массовых расходов подачи хладагента с целью определения возможной длины рабочей зоны криостатирования протяженного сверхпроводящего кабеля. Получены расчетные данные по изменению по длине протяженного криостата температуры, давления и холодопроизводительности испарительной системы криостатирования.</p><p> </p></abstract><trans-abstract xml:lang="en"><p>The article analyzes the results of theoretical and experimental studies of the evaporative cryogenic system for extended temperature control channels of high-temperature superconducting cables and hybrid power lines as well as systems for maintaining the thermal regime of cryogenic fuel components in the tanks of aircraft during long space flights. Experimental data obtained with nitrogen and hydrogen are presented. The importance of such studies for practical use in the development of modern cryostat systems is shown. The design of the experimental hybrid power line for studying the processes of thermostating of superconducting cable lines of high power is considered. The main line consists of three sections with different types of thermal insulation and current inputs which provide the supply of an electric current of high power to superconducting veins with a minimum external heat input. Unique experimental data on heat inflows from the outer surface of the main line at various sites have been obtained. The article shows it is possible to fully compensate external heat input into the cryogenic line, and, if necessary, to lower the temperature of the cryogenic coolant in the section with the evaporative cryostat system. With the help of a mathematical model describing the physical processes in the thermostatic channel with the evaporative cryostat system, the estimates were made using liquid nitrogen and liquid hydrogen as the working fluid for various mass flow rates of the coolant supply in order to determine the possible length of the cryostat working zone of the extended superconducting cable. Calculated data are obtained on the change in temperature, pressure, and cooling capacity of an evaporative cryostat system along the length of an extended cryostat.</p><p> </p></trans-abstract><kwd-group xml:lang="ru"><kwd>криостат</kwd><kwd>жидкий азот</kwd><kwd>жидкий водород</kwd><kwd>теплоприток</kwd><kwd>теплоизоляция</kwd><kwd>система криостатирования</kwd><kwd>теплообменный аппарат</kwd></kwd-group><kwd-group xml:lang="en"><kwd>cryostat</kwd><kwd>liquid nitrogen</kwd><kwd>liquid hydrogen</kwd><kwd>heat transfer</kwd><kwd>heat insulation</kwd><kwd>cryostat system</kwd><kwd>heat exchange</kwd></kwd-group></article-meta></front><back><ref-list><title>References</title><ref id="cit1"><label>1</label><citation-alternatives><mixed-citation xml:lang="ru">Grant, P.M. Will MgB2 Work [Text] / P.М. Grant // The Industrial Physicist. – 2001. – Oct-Nov. – P. 22–23.</mixed-citation><mixed-citation xml:lang="en">Grant P.M. Will MgB2 Work. 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