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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">caht</journal-id><journal-title-group><journal-title xml:lang="ru">Научный вестник МГТУ ГА</journal-title><trans-title-group xml:lang="en"><trans-title>Civil Aviation High Technologies</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">2079-0619</issn><issn pub-type="epub">2542-0119</issn><publisher><publisher-name>Moscow State Technical University of Civil Aviation (MSTU CA)</publisher-name></publisher></journal-meta><article-meta><article-id custom-type="elpub" pub-id-type="custom">caht-334</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>Статьи</subject></subj-group></article-categories><title-group><article-title>Диагностика срыва горения в камере сгорания с помощью тепловизионной техники</article-title><trans-title-group xml:lang="en"><trans-title>Diagnosis of failure of combustion in the combustion chamber with a thermovision equipment</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>Воробьев</surname><given-names>С. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Vorobiev</surname><given-names>S. V.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.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>Павлов</surname><given-names>Ю. И.</given-names></name><name name-style="western" xml:lang="en"><surname>Pavlov</surname><given-names>Yu. I.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.ru</email><xref ref-type="aff" rid="aff-2"/></contrib></contrib-group><aff xml:lang="ru" id="aff-1"><institution>ФГУП ЦИАМ им. П.И. Баранова</institution><country>Russian Federation</country></aff><aff xml:lang="ru" id="aff-2"><institution>МАТИ</institution><country>Russian Federation</country></aff><pub-date pub-type="collection"><year>2014</year></pub-date><pub-date pub-type="epub"><day>07</day><month>11</month><year>2016</year></pub-date><volume>0</volume><issue>208</issue><fpage>104</fpage><lpage>108</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Воробьев С.В., Павлов Ю.И., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Воробьев С.В., Павлов Ю.И.</copyright-holder><copyright-holder xml:lang="en">Vorobiev S.V., Pavlov Y.I.</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://avia.mstuca.ru/jour/article/view/334">https://avia.mstuca.ru/jour/article/view/334</self-uri><abstract><p>Рассматривается применение тепловизионной техники для диагностики срыва горения при испытании жаровой трубы основной камеры сгорания газотурбинного двигателя (ГТД). Регистрация теплового излучения струи продуктов сгорания и внутренних элементов осуществлялась с помощью коротковолновой тепловизионной системы AGA-782 с применением спектральных фильтров в нескольких диапазонах от 3,2 до 5,6 мкм. Тепловизор устанавливался по оси жаровой трубы. Выходной сигнал записывался и обрабатывался на компьютере в режиме реального времени, что позволяло контролировать процесс горения и тепловое состояние объекта во время эксперимента.</p></abstract><trans-abstract xml:lang="en"><p>The use of thermovision technology to diagnose failure of the combustion flame test tube of the main combustion chamber gas turbine engine is deal with in the article. Join the thermal radiation of the jet of combustion products and the internal elements was carried out using short-wave thermovision system AGA-782 with spectral spectral filters in several ranges from 3.2 to 5.6 microns. Thermovision is mounted on the axis of the flame tube. The output signal was recorded and processed on a computer in real time, allowing monitor the combustion process and the thermal state of the object during the experiment.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>тепловое излучение</kwd><kwd>тепловизор</kwd><kwd>камера сгорания</kwd></kwd-group><kwd-group xml:lang="en"><kwd>thermal radiation</kwd><kwd>thermal imager</kwd><kwd>a combustion chamber</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">Блох А.Г. Основы теплообмена излучением. - М.: Госэнергоиздат, 1962</mixed-citation><mixed-citation xml:lang="en">Блох А.Г. Основы теплообмена излучением. - М.: Госэнергоиздат, 1962</mixed-citation></citation-alternatives></ref></ref-list><fn-group><fn fn-type="conflict"><p>The authors declare that there are no conflicts of interest present.</p></fn></fn-group></back></article>
