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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">zldm</journal-id><journal-title-group><journal-title xml:lang="ru">Заводская лаборатория. Диагностика материалов</journal-title><trans-title-group xml:lang="en"><trans-title>Industrial laboratory. Diagnostics of materials</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1028-6861</issn><issn pub-type="epub">2588-0187</issn><publisher><publisher-name>ООО «Издательство «ТЕСТ-ЗЛ»</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.26896/1028-6861-2022-88-2-64-70</article-id><article-id custom-type="elpub" pub-id-type="custom">zldm-1602</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>МЕХАНИКА МАТЕРИАЛА: ПРОЧНОСТЬ, РЕСУРС, БЕЗОПАСНОСТЬ</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>MATERIALS MECHANICS: STRENGTH, DURABILITY, SAFETY</subject></subj-group></article-categories><title-group><article-title>Исследование пластической деформации металла методом индентирования</article-title><trans-title-group xml:lang="en"><trans-title>Study of the plastic deformation of metals by indentation method</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>Орешко</surname><given-names>Е. И.</given-names></name><name name-style="western" xml:lang="en"><surname>Oreshko</surname><given-names>E. I.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Евгений Игоревич Орешко</p><p>105005, Москва, ул. Радио, д. 17</p></bio><bio xml:lang="en"><p>Evgeny I. Oreshko</p><p>17, ul. Radio, Moscow, 105005</p></bio><email xlink:type="simple">89639619741@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>Яковлев</surname><given-names>Н. О.</given-names></name><name name-style="western" xml:lang="en"><surname>Yakovlev</surname><given-names>N. O.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Николай Олегович Яковлев</p><p>105005, Москва, ул. Радио, д. 17</p></bio><bio xml:lang="en"><p>Nikolai O. Yakovlev</p><p>17, ul. Radio, Moscow, 105005</p></bio><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Ерасов</surname><given-names>В. С.</given-names></name><name name-style="western" xml:lang="en"><surname>Erasov</surname><given-names>V. S.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Владимир Сергеевич Ерасов</p><p>105005, Москва, ул. Радио, д. 17</p></bio><bio xml:lang="en"><p>Vladimir S. Erasov</p><p>17, ul. Radio, Moscow, 105005</p></bio><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Уткин</surname><given-names>Д. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Utkin</surname><given-names>D. A.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Денис Антонович Уткин</p><p>105005, Москва, ул. Радио, д. 17</p></bio><bio xml:lang="en"><p>Denis A. Utkin</p><p>17, ul. Radio, Moscow, 105005</p></bio><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Всероссийский научно-исследовательский институт авиационных материалов</institution><country>Россия</country></aff><aff xml:lang="en"><institution>All-Russian Scientific Research Institute of Aviation Materials</institution><country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2022</year></pub-date><pub-date pub-type="epub"><day>23</day><month>02</month><year>2022</year></pub-date><volume>88</volume><issue>2</issue><fpage>64</fpage><lpage>70</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Орешко Е.И., Яковлев Н.О., Ерасов В.С., Уткин Д.А., 2022</copyright-statement><copyright-year>2022</copyright-year><copyright-holder xml:lang="ru">Орешко Е.И., Яковлев Н.О., Ерасов В.С., Уткин Д.А.</copyright-holder><copyright-holder xml:lang="en">Oreshko E.I., Yakovlev N.O., Erasov V.S., Utkin D.A.</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.zldm.ru/jour/article/view/1602">https://www.zldm.ru/jour/article/view/1602</self-uri><abstract><p>Один из видов повреждения материала — пластическая деформация, которая может нарушить нормальную работу конструкции. В связи с этим разработана методика оценки степени повреждаемости металла. Для ее реализации изготовлен корсетный образец на растяжение из алюминиевого сплава системы Al – Zn – Mg – Cu. Из-за переменного поперечного сечения рабочей зоны образца при растяжении в нем возникало неоднородное напряженное состояние, для моделирования которого использован конечно-элементный комплекс ANSYS. Сначала измеряли твердость корсетного образца, затем его испытывали на растяжение до момента начала образования шейки и падения нагрузки на диаграмме деформирования. После разгрузки образца вдоль его рабочей зоны измеряли твердость по методу Бринелля и шероховатость поверхности. Результаты измерений твердости показали, что в зонах образца, где напряжения при растяжении ниже условного предела текучести материала, она соответствовала твердости исходного материала. В области образца, где при растяжении напряжения выше условного предела текучести, твердость повышалась и достигала максимума в центре образца, зоне минимального поперечного сечения. Таким образом, определяя изменение твердости и шероховатости поверхности по длине образца, связывали его с повреждаемостью материала. По результатам инструментального сферического индентирования разработана методика оценки механических характеристик материала. Она заключалась в испытании одного образца на твердость и на растяжение. По полученным экспериментальным результатам строили корреляционные зависимости нагрузок при растяжении и индентировании. Эти зависимости позволили по диаграммам вдавливания исследуемого материала получать расчетные диаграммы растяжения.</p></abstract><trans-abstract xml:lang="en"><p>All-Russian Scientific Research Institute of Aviation Materials, 17, ul. Radio, Moscow, 105005 Russia; e-mail: 89639619741@mail.ru</p><p>Plastic deformation is a type of material damage which can disrupt the normal operation of the structure. In this regard, the method for assessing the degree of damage to a metal sample has been developed. A corset sample for tensile tests was made from an aluminum alloy of the Al – Zn – Mg – Cu system. The ANSYS finite element complex was used to simulate an inhomogeneous stress state occurred in the sample working zone due to the variable cross-section upon tension. First, the hardness of the corset sample was measured, then it was tested for tension until the onset of necking and the load drop on the deformation diagram. After unloading along the sample working area, the Brinell hardness and surface roughness were measured. The results of the hardness measurements showed that in the areas where the tensile stresses are below the conditional yield stress of the material, the hardness value corresponds to the hardness of the starting material. In the areas where the tensile stresses are higher than the conventional yield stress, the hardness increases and reaches the maximum value in the center of the specimen, i.e., in the zone of the minimum cross-section. Thus, the damageability of the material can be assessed through the change in the hardness and roughness of the surface along the sample length. Proceeding from the results of instrumental spherical indentation, a technique for assessing the mechanical characteristics of the material was developed. The method consists in testing one sample for hardness and tensile strength with subsequent construction of the correlation dependences of tensile and indentation loads using the experimental results to obtain calculated tensile diagrams from the indentation diagrams of the material under study.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>твердость</kwd><kwd>повреждаемость</kwd><kwd>индентирование</kwd><kwd>деформация</kwd><kwd>напряжения</kwd><kwd>вдавливание</kwd><kwd>расчет</kwd></kwd-group><kwd-group xml:lang="en"><kwd>hardness</kwd><kwd>damage</kwd><kwd>indentation</kwd><kwd>deformation</kwd><kwd>stress</kwd><kwd>indentation</kwd><kwd>calculation</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">Solntsev Yu. P., Pryakhin E. I. Materials science: the textbook for higher education institutions. 7th edition. — St. Petersburg: Khimizdat, 2020. — 784 p. 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