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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">probener</journal-id><journal-title-group><journal-title xml:lang="ru">Известия высших учебных заведений. ПРОБЛЕМЫ ЭНЕРГЕТИКИ</journal-title><trans-title-group xml:lang="en"><trans-title>Power engineering: research, equipment, technology</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1998-9903</issn><issn pub-type="epub">2658-5456</issn><publisher><publisher-name>Kazan State Power Engineering  University</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.30724/1998-9903-2025-27-6-49-71</article-id><article-id custom-type="elpub" pub-id-type="custom">probener-3606</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>ЭЛЕКТРОТЕХНИЧЕСКИЕ КОМПЛЕКСЫ И СИСТЕМЫ</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>ELECTROTECHNICAL COMPLEXES AND SYSTEMS</subject></subj-group></article-categories><title-group><article-title>Разработка и верификация методики проектирования бортовой кабельной сети летательного аппарата с учетом требований электромагнитной совместимости</article-title><trans-title-group xml:lang="en"><trans-title>Designing the electrical complex of an aircraft, taking into account electromagnetic compatibility</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>Мингазов</surname><given-names>А. Л.</given-names></name><name name-style="western" xml:lang="en"><surname>Mingazov</surname><given-names>A. L.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Мингазов Артур Ленарович – аспирант</p><p>г. Казань</p></bio><bio xml:lang="en"><p>Artur L. Mingazov – Kazan National Research Technical University named after A.N. Tupolev – KAI</p><p>Kazan </p></bio><email xlink:type="simple">mingazow.artur@yandex.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>Федоров</surname><given-names>Е. Ю.</given-names></name><name name-style="western" xml:lang="en"><surname>Fedorov</surname><given-names>E. Y.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Федоров Евгений Юрьевич – канд. техн. наук, доцент кафедры «Электрооборудование»</p><p>г. Казань</p></bio><bio xml:lang="en"><p>Evgenii Yu. Fedorov – Kazan National Research Technical University named after A.N. Tupolev – KAI</p><p>Kazan</p></bio><email xlink:type="simple">zhenek_fed@mail.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Казанский национальный исследовательский технический университет им. А.Н. Туполева – КАИ</institution><country>Россия</country></aff><aff xml:lang="en"><institution>Kazan National Research Technical University named after A.N. Tupolev – KAI</institution><country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2025</year></pub-date><pub-date pub-type="epub"><day>19</day><month>12</month><year>2025</year></pub-date><volume>27</volume><issue>6</issue><fpage>49</fpage><lpage>71</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Мингазов А.Л., Федоров Е.Ю., 2025</copyright-statement><copyright-year>2025</copyright-year><copyright-holder xml:lang="ru">Мингазов А.Л., Федоров Е.Ю.</copyright-holder><copyright-holder xml:lang="en">Mingazov A.L., Fedorov E.Y.</copyright-holder><license xml:lang="ru" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>Данная работа распространяется под лицензией Creative Commons Attribution 4.0.</license-p></license><license xml:lang="en" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>This work is licensed under a Creative Commons Attribution 4.0 License.</license-p></license></permissions><self-uri xlink:href="https://www.energyret.ru/jour/article/view/3606">https://www.energyret.ru/jour/article/view/3606</self-uri><abstract><p>ЦЕЛЬ. Рассмотреть проблемы проникновения и распространения электромагнитных помех в отдельных бортовых устройствах электротехнического комплекса летательного аппарата. Провести проверку исследуемого объекта бортового комплекса электрооборудования летательного аппарата на соответствие требованиям нормативных документов в части электромагнитной совместимости. Разработать рекомендации для устранения кондуктивных и индуктивных помех исследуемого объекта бортового комплекса электрооборудования летательного аппарата. МЕТОДЫ. Для решения исследовательских задач использовался комплекс методов, включающий графовое моделирование топологии распространения электромагнитных помех в корпусе летательного аппарата, конечно-элементный анализ электромагнитных полей и методы математического моделирования. РЕЗУЛЬТАТЫ. Исследованы вопросы проникновения и распространения электромагнитных наводок в конструктивных элементах и цепях электротехнических систем воздушного судна. Выполнена верификация соответствия бортового электрооборудования нормативным требованиям по электромагнитной совместимости. Разработана топологическая модель распределения помех внутри корпуса летательного аппарата. Проведен анализ наведенных помех от внешних источников электромагнитного излучения. Сформулированы практические рекомендации по минимизации кондуктивных и индуктивных наводок в бортовом электрооборудовании. ВЫВОДЫ. При проведении исследования на соответствие требованиям нормативных документов в части электромагнитной совместимости исследуемого объекта бортового комплекса электрооборудования летательного аппарата было выявлено, что необходимо дорабатывать способы экранирования чувствительных элементов. Было представлено несколько способов устранения кондуктивных и индуктивных помех исследуемого объекта бортового комплекса электрооборудования летательного аппарата и выбран оптимальный.</p></abstract><trans-abstract xml:lang="en"><p>THE PURPOSE. To consider the problems of the ingress and propagation of electromagnetic interference in individual on-board devices of the electrical complex of the aircraft. To check the object under study of the on-board electrical equipment complex of the aircraft for compliance with the requirements of regulatory documents regarding electromagnetic compatibility. To develop recommendations for the elimination of conductive and inductive interference of the studied object of the on-board complex of electrical equipment of the aircraft. METHODS. To solve the research problems, a set of methods was used, including graph modeling of the topology of electromagnetic interference propagation in the aircraft body, finite element analysis of electromagnetic fields and mathematical modeling methods. RESULTS. The issues of penetration and propagation of electromagnetic interference in structural elements and circuits of electrical systems of an aircraft are investigated. Verification of compliance of on-board electrical equipment with regulatory requirements for electromagnetic compatibility has been performed. A topological model of interference distribution inside the aircraft body has been developed. The analysis of induced interference from external sources of electromagnetic radiation is carried out. Practical recommendations for minimizing conductive and inductive leads in on-board electrical equipment are formulated. CONCLUSION. When conducting a study on compliance with the requirements of regulatory documents in terms of electromagnetic compatibility. It was revealed that it is necessary to refine the methods of shielding sensitive elements of the studied object of the onboard complex of electrical equipment of the aircraft. Several ways to eliminate conductive and inductive interference of the object under study of the on-board complex of electrical equipment of the aircraft were presented and the optimal one was chosen.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>электротехнический комплекс</kwd><kwd>электромагнитная совместимость</kwd><kwd>летательный аппарат</kwd><kwd>зона экранирования</kwd><kwd>кондуктивные помехи</kwd><kwd>индуктивные помехи</kwd><kwd>топологическая модель</kwd></kwd-group><kwd-group xml:lang="en"><kwd>electrical engineering complex</kwd><kwd>electromagnetic compatibility</kwd><kwd>aircraft</kwd><kwd>shielding zone</kwd><kwd>conductive interference</kwd><kwd>inductive interference</kwd><kwd>topological model</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">Нгуен Ван Хой. 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