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<article 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" xmlns:ali="http://www.niso.org/schemas/ali/1.0/" article-type="research-article" dtd-version="1.2" xml:lang="en"><front><journal-meta><journal-id journal-id-type="publisher-id">Frontier Materials &amp; Technologies</journal-id><journal-title-group><journal-title xml:lang="en">Frontier Materials &amp; Technologies</journal-title><trans-title-group xml:lang="ru"><trans-title>Frontier Materials &amp; Technologies</trans-title></trans-title-group></journal-title-group><issn publication-format="print">2782-4039</issn><issn publication-format="electronic">2782-6074</issn><publisher><publisher-name xml:lang="en">Togliatti State University</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="publisher-id">912</article-id><article-id pub-id-type="doi">10.18323/2782-4039-2024-1-67-10</article-id><article-categories><subj-group subj-group-type="toc-heading" xml:lang="en"><subject>Articles</subject></subj-group><subj-group subj-group-type="toc-heading" xml:lang="ru"><subject>Статьи</subject></subj-group><subj-group subj-group-type="article-type"><subject>Research Article</subject></subj-group></article-categories><title-group><article-title xml:lang="en">The study of the effect of heat treatment on the properties of the AMg2–10%TiC and AMg6–10%TiC composite materials produced by self-propagating high-temperature synthesis</article-title><trans-title-group xml:lang="ru"><trans-title>Влияние термической обработки на свойства композиционных материалов АМг2–10%TiC и АМг6–10%TiC, полученных методом самораспространяющегося высокотемпературного синтеза</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0002-5451-7107</contrib-id><name-alternatives><name xml:lang="en"><surname>Sherina</surname><given-names>Yuliya V.</given-names></name><name xml:lang="ru"><surname>Шерина</surname><given-names>Юлия Владимировна</given-names></name></name-alternatives><address><country country="RU">Russian Federation</country></address><bio xml:lang="en"><p>postgraduate student of Chair “Metal Science, Powder Metallurgy, Nanomaterials”</p></bio><bio xml:lang="ru"><p>аспирант кафедры «Металловедение, порошковая металлургия, наноматериалы»</p></bio><email>yulya.makhonina.97@inbox.ru</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0001-7889-9931</contrib-id><name-alternatives><name xml:lang="en"><surname>Luts</surname><given-names>Alfiya R.</given-names></name><name xml:lang="ru"><surname>Луц</surname><given-names>Альфия Расимовна</given-names></name></name-alternatives><address><country country="RU">Russian Federation</country></address><bio xml:lang="en"><p>PhD (Engineering), Associate Professor, assistant professor of Chair “Metal Science, Powder Metallurgy, Nanomaterials”</p></bio><bio xml:lang="ru"><p>кандидат технических наук, доцент, доцент кафедры «Металловедение, порошковая металлургия, наноматериалы»</p></bio><email>alya_luts@mail.ru</email><xref ref-type="aff" rid="aff1"/></contrib></contrib-group><aff-alternatives id="aff1"><aff><institution xml:lang="en">Samara State Technical University</institution></aff><aff><institution xml:lang="ru">Самарский государственный технический университет</institution></aff></aff-alternatives><pub-date date-type="pub" iso-8601-date="2024-03-29" publication-format="electronic"><day>29</day><month>03</month><year>2024</year></pub-date><issue>1</issue><issue-title xml:lang="en"/><issue-title xml:lang="ru"/><fpage>105</fpage><lpage>112</lpage><history><date date-type="received" iso-8601-date="2024-03-29"><day>29</day><month>03</month><year>2024</year></date></history><permissions><copyright-statement xml:lang="en">Copyright ©; 2024, Sherina Y.V., Luts A.R.</copyright-statement><copyright-statement xml:lang="ru">Copyright ©; 2024, Шерина Ю.В., Луц А.Р.</copyright-statement><copyright-year>2024</copyright-year><copyright-holder xml:lang="en">Sherina Y.V., Luts A.R.</copyright-holder><copyright-holder xml:lang="ru">Шерина Ю.В., Луц А.Р.</copyright-holder><ali:free_to_read xmlns:ali="http://www.niso.org/schemas/ali/1.0/"/><license><ali:license_ref xmlns:ali="http://www.niso.org/schemas/ali/1.0/">https://creativecommons.org/licenses/by/4.0</ali:license_ref></license></permissions><self-uri xlink:href="https://vektornaukitech.ru/jour/article/view/912">https://vektornaukitech.ru/jour/article/view/912</self-uri><abstract xml:lang="en"><p>Dispersion-strengthened composite materials belong to the group of promising structural materials characterised by a diverse combination of properties. The paper considers examples of the creation and heat treatment of composite materials based on aluminium alloys strengthened by the titanium carbide dispersed phase characterised by high hardness, elastic modulus, and good melt wettability. At present, self-propagating high-temperature synthesis (SHS) is the most accessible, inexpensive and effective way to obtain them. The authors substantiate the expediency and show their successful experience of the formation in the composition of the AMg2 and AMg6 industrial alloys of a titanium carbide dispersed phase with a particle size of 130 nm in an amount of up to 10 wt. % using the SHS method, which makes it possible to increase the hardness of the alloys. Additional heating of the AMg2–10%TiC and AMg6–10%TiC samples after synthesis also contributes to the further increase in hardness. The complex of studies of physical, mechanical and operational characteristics presented in the paper was carried out to compare the properties of the work-hardened matrix alloys and the samples of composite materials before and after heating. The test results showed that heat treatment reduces the porosity of the composites and significantly increases their hardness and microhardness. A slight decrease in compressive strength at a significant increase in wear resistance is observed. It was found that composite materials are characterised by high corrosion resistance to carbon dioxide and hydrogen sulfide corrosion corresponding to the level of matrix alloys. The results obtained allow recommending the developed materials for the production of parts of the connecting rod and piston group, bearings and other wear-resistant parts of friction units.</p></abstract><trans-abstract xml:lang="ru"><p>Дисперсно-упрочненные композиционные материалы относятся к группе перспективных конструкционных материалов, отличающихся разнообразным сочетанием свойств. В работе рассмотрены примеры создания и термической обработки композиционных материалов на основе алюминиевых сплавов, упрочненных дисперсной фазой карбида титана, для которой характерны высокая твердость, модуль упругости и хорошая смачиваемость расплавом. В настоящее время наиболее доступным, недорогим и эффективным способом получения этих материалов является самораспространяющийся высокотемпературный синтез (СВС). Обоснована целесообразность и показан собственный успешный опыт формирования в составе промышленных сплавов АМг2 и АМг6 дисперсной фазы карбида титана с размером частиц от 130 нм в количестве до 10 мас. % методом СВС, что позволяет увеличить твердость сплавов. Проведение после синтеза дополнительного нагрева образцов АМг2–10%TiC и АМг6–10%TiC также способствует последующему повышению твердости. Представленный в статье комплекс исследований физических, механических и эксплуатационных характеристик выполнен с целью сравнения свойств матричных сплавов в нагартованном состоянии и образцов композиционных материалов до и после нагрева. Результаты испытаний показали, что проведение термической обработки способствует снижению пористости композитов и значительному повышению их твердости и микротвердости. Наблюдается также незначительное снижение прочности на сжатие при существенном повышении износостойкости. Установлено, что композиционные материалы характеризуются высокой коррозионной стойкостью к углекислотной и сероводородной коррозии, соответствующей уровню матричных сплавов. Полученные результаты позволяют рекомендовать разработанные материалы для изготовления деталей шатунно-поршневой группы, подшипников и других износостойких деталей узлов трения.</p></trans-abstract><kwd-group xml:lang="en"><kwd>composite material</kwd><kwd>AMg2–10%TiC</kwd><kwd>AMg6–10%TiC</kwd><kwd>titanium carbide</kwd><kwd>heat treatment</kwd><kwd>self-propagating high-temperature synthesis</kwd></kwd-group><kwd-group xml:lang="ru"><kwd>композиционный материал</kwd><kwd>АМг2–10%TiC</kwd><kwd>АМг6–10%TiC</kwd><kwd>карбид титана</kwd><kwd>термическая обработка</kwd><kwd>самораспространяющийся высокотемпературный синтез</kwd></kwd-group><funding-group><funding-statement xml:lang="en">The paper was written on the reports of the participants of the XI International School of Physical Materials Science (SPM-2023), Togliatti, September 11–15, 2023.</funding-statement><funding-statement xml:lang="ru">Статья подготовлена по материалам докладов участников XI Международной школы «Физическое материаловедение» (ШФМ-2023), Тольятти, 11–15 сентября 2023 года.</funding-statement></funding-group></article-meta></front><body></body><back><ref-list><ref id="B1"><label>1.</label><citation-alternatives><mixed-citation xml:lang="en">Panfilov A.A., Prusov E.S., Kechin V.A. 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