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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">madi</journal-id><journal-title-group><journal-title xml:lang="ru">Автомобиль. Дорога. Инфраструктура. = Avtomobil'. Doroga. Infrastruktura.</journal-title><trans-title-group xml:lang="en"><trans-title>Avtomobil'. Doroga. Infrastruktura.</trans-title></trans-title-group></journal-title-group><issn pub-type="epub">2409-7217</issn><publisher><publisher-name>МАДИ</publisher-name></publisher></journal-meta><article-meta><article-id custom-type="elpub" pub-id-type="custom">madi-444</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>Вопросы транспортного строительства</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>Issues of transport construction</subject></subj-group></article-categories><title-group><article-title>РАСЧЕТ ПРОГИБОВ ПЛИТЫ АЭРОДРОМНОГО ПОКРЫТИЯ С УЧЕТОМ РАЗМЕРА ОТПЕЧАТКА АВИАШИНЫ</article-title><trans-title-group xml:lang="en"><trans-title>CALCULATION DEFLEXION OF AIRFIELD PAVEMENT TAKING INTO ACCOUNT SIZE OF IMPRINT OF AIRTIRE</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>Татаринов</surname><given-names>Владимир Владимирович</given-names></name><name name-style="western" xml:lang="en"><surname>Tatarinov</surname><given-names>Vladimir V.</given-names></name></name-alternatives><bio xml:lang="ru"><p>канд. техн. наук, проф.</p></bio><bio xml:lang="en"><p>Ph. D., professor</p></bio><email xlink:type="simple">tatarinov@madi.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>Фомин</surname><given-names>Андрей Викторович</given-names></name><name name-style="western" xml:lang="en"><surname>Fomin</surname><given-names>Andrey V.</given-names></name></name-alternatives><bio xml:lang="ru"><p>канд. техн. наук, доц.</p></bio><bio xml:lang="en"><p>Ph. D., associate professor</p></bio><email xlink:type="simple">fomin.a@tpr-msk.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru">МАДИ<country>Россия</country></aff><aff xml:lang="en">MADI<country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2017</year></pub-date><pub-date pub-type="epub"><day>27</day><month>12</month><year>2017</year></pub-date><volume>0</volume><issue>4(14)</issue><fpage>4</fpage><lpage>4</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Татаринов В.В., Фомин А.В., 2017</copyright-statement><copyright-year>2017</copyright-year><copyright-holder xml:lang="ru">Татаринов В.В., Фомин А.В.</copyright-holder><copyright-holder xml:lang="en">Tatarinov V.V., Fomin A.V.</copyright-holder><license 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.adi-madi.ru/madi/article/view/444">https://www.adi-madi.ru/madi/article/view/444</self-uri><abstract><p>В статье рассмотрен расчет прогибов армобетонного покрытия аэродрома от колес основной опоры самолета Боинг-747-400. Исследованы решения основной модели жесткого аэродромного покрытия в виде бесконечной пластины на упругом основании и проведен анализ полученных результатов для различного представления подвижной нагрузки от колеса. В качестве примера рассмотрено движение по модели армобетонного покрытия нагрузки от колеса самолета в виде сосредоточенной силы и распределенной по прямоугольному отпечатку.</p></abstract><trans-abstract xml:lang="en"><p>The article describes the calculation of deflections fibercrete pavement of the airfield from the wheels of main landing gear of a Boeing 747-400. We study the solutions of the basic model of rigid airfield pavement in the form of an infinite plate on an elastic foundation and the analysis of the obtained results for different views of the moving load of the wheel. As an example, the considered movement model fibercrete pavement the loads from the wheels of the aircraft in the form of concentrated force and distributed on a rectangular imprint.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>покрытие аэродрома</kwd><kwd>прогиб аэродромного покрытия</kwd><kwd>пластина</kwd><kwd>упругое основание</kwd></kwd-group><kwd-group xml:lang="en"><kwd>airfield pavement</kwd><kwd>deflection of airfield pavement</kwd><kwd>plate</kwd><kwd>elastic foundation</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">СП 121.13330.2012. Аэродромы. Актуализированная редакция СНиП 32-03-96 / Минрегион России. – М., 2012. – 98 с.</mixed-citation><mixed-citation xml:lang="en">Aerodromy, SP 121.13330.2012. Aerodromy. Aktualizirovannaya redaktsiya SNiP 32-03-96 (Aerodromy JV 121.13330.2012. 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