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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="other" 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">865</article-id><article-id pub-id-type="doi">10.18323/2782-4039-2023-3-65-2</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></subject></subj-group></article-categories><title-group><article-title xml:lang="en">Development and airworthiness certification of state of art additively manufactured AlSi10Mg mission critical selector valve body part for aerospace</article-title><trans-title-group xml:lang="ru"><trans-title>Разработка и сертификация летной годности современной ответственной детали корпуса переключателя для аэрокосмических систем, изготовленной из сплава AlSi10Mg с помощью аддитивной технологии</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0003-4487-2030</contrib-id><name-alternatives><name xml:lang="en"><surname>Vignesh</surname><given-names>Ponnusamy</given-names></name><name xml:lang="ru"><surname>Вигнеш</surname><given-names>Поннусами</given-names></name></name-alternatives><address><country country="IN">India</country></address><bio xml:lang="en"><p>PhD, Junior Specialist-1</p></bio><bio xml:lang="ru"><p>доктор наук, младший специалист-1</p></bio><email>vigneshpt3532@gmail.com</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><name-alternatives><name xml:lang="en"><surname>Praveen</surname><given-names>K.V.</given-names></name><name xml:lang="ru"><surname>Правин</surname><given-names>К.В.</given-names></name></name-alternatives><address><country country="IN">India</country></address><bio xml:lang="en"><p>Bachelor of Engineering, Technical Assistant</p></bio><bio xml:lang="ru"><p>бакалавр технических наук, технический помощник</p></bio><email>praveenkv61@gmail.com</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><name-alternatives><name xml:lang="en"><surname>Krishnakumar</surname><given-names>Subbulakshmi</given-names></name><name xml:lang="ru"><surname>Кришнакумар</surname><given-names>Суббулакшми</given-names></name></name-alternatives><address><country country="IN">India</country></address><bio xml:lang="en"><p>Bachelor of Engineering, Technical Assistant</p></bio><bio xml:lang="ru"><p>бакалавр технических наук, технический помощник</p></bio><email>krishna.ks0531@gmail.com</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><name-alternatives><name xml:lang="en"><surname>Bhuvaneswari</surname><given-names>Mohanrao Chembu</given-names></name><name xml:lang="ru"><surname>Бхуванесвари</surname><given-names>Моханрао Чембу</given-names></name></name-alternatives><address><country country="IN">India</country></address><bio xml:lang="en"><p>Bachelor of Engineering, Regional Director (Sc ‘F’)</p></bio><bio xml:lang="ru"><p>бакалавр технических наук, региональный директор (сектор ‘F’)</p></bio><email>cm.cemilac@gov.in</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><name-alternatives><name xml:lang="en"><surname>Kale</surname><given-names>Shirish Sharad</given-names></name><name xml:lang="ru"><surname>Кейл</surname><given-names>Шириш Шарад</given-names></name></name-alternatives><address><country country="IN">India</country></address><bio xml:lang="en"><p>Ph.D., Director (Sc ‘G’)</p></bio><bio xml:lang="ru"><p>доктор наук, директор (сектор ‘G’)</p></bio><email>shirish.kale.cemilac@gov.in</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><name-alternatives><name xml:lang="en"><surname>Ram Prabhu</surname><given-names>Theagarajan</given-names></name><name xml:lang="ru"><surname>Рам Прабху</surname><given-names>Тэгараджан</given-names></name></name-alternatives><address><country country="IN">India</country></address><bio xml:lang="en"><p>Ph.D., Joint Director (Sc ‘E’)</p></bio><bio xml:lang="ru"><p>доктор наук, содиректор (сектор ‘E’)</p></bio><email>ramprabhu.t@gmail.com</email><xref ref-type="aff" rid="aff1"/></contrib></contrib-group><aff-alternatives id="aff1"><aff><institution xml:lang="en">RCMA (F&amp;F), CEMILAC, Defence R&amp;D Organization, Bangalore</institution></aff><aff><institution xml:lang="ru">Региональный центр военной полетопригодности (F&amp;F), Центр боевой полетопригодности и сертификации, Организация оборонных исследований и разработок, Бангалор</institution></aff></aff-alternatives><pub-date date-type="pub" iso-8601-date="2023-09-29" publication-format="electronic"><day>29</day><month>09</month><year>2023</year></pub-date><issue>3</issue><issue-title xml:lang="en"/><issue-title xml:lang="ru"/><fpage>19</fpage><lpage>30</lpage><history><date date-type="received" iso-8601-date="2023-09-29"><day>29</day><month>09</month><year>2023</year></date></history><permissions><ali:free_to_read xmlns:ali="http://www.niso.org/schemas/ali/1.0/"/></permissions><self-uri xlink:href="https://vektornaukitech.ru/jour/article/view/865">https://vektornaukitech.ru/jour/article/view/865</self-uri><abstract xml:lang="en"><p>Aerospace applications can benefit from additive manufacturing (AM), which is highly advantageous for prototyping and rapid manufacturing. It also offers cost and weight savings, as well as integrated design capabilities. As of now, there are only a few AM standards available, many materials and equipment are involved, resulting in many variables that hinder certification and adoption. As a result, nonstandard testing is making AM in the airborne materials less appealing due to its costly and time-consuming nature. The main objective of this work is to manufacture the Selector Valve Body parts of military and civil aircraft through Laser Powder Bed Fusion (LPBF) process using AlSi10Mg powder. Further, this paper has been carried out the metallurgical properties, non-destructive and destructive testing as well as the clear explanation about the certification procedures. Moreover, this underscores the need for the developing guidelines, and standards that cover all aspects of manufacturing from design to manufacturing to operation. A comprehensive analysis from liquid penetration test shows defects are within the permissible level. In addition, it exhibits higher yield strength, ultimate strength, and elongation of (259±4) MPa, (323±4) MPa, and (12.5±1.5) % respectively, along with factual evidence that the precipitation hardened AlSi10Mg indigenously developed and produced is equal in properties to the equivalent precipitation hardening aluminium alloys produced by internationally renowned manufacturers. </p></abstract><trans-abstract xml:lang="ru"><p>Аддитивные технологии (АТ) очень эффективны для макетирования и быстрого производства, поэтому их применение выгодно для аэрокосмической отрасли. Они позволяют сэкономить средства, а также облегчить конструкции, подходят для комплексного проектирования. Однако на данный момент доступно лишь несколько стандартов аддитивных технологий, требуется много материалов и оборудования, что приводит к возникновению затруднений с сертификацией и внедрением АТ. Нестандартные испытания приводят к тому, что АТ в аэрозольных материалах оказываются менее привлекательными из-за их дороговизны и трудоемкости. Целью работы является изготовление деталей корпуса переключателя военных и гражданских самолетов методом лазерного сплавления порошкового слоя (LPBF) с применением порошка AlSi10Mg. Выявлены физико-химические свойства материала, проведены неразрушающие и разрушающие испытания, а также даны четкие разъяснения процедур сертификации. Сделан упор на необходимости разработки руководств и стандартов, охватывающих все аспекты производства – от проектирования до изготовления и эксплуатации продукта. Комплексный анализ испытаний на проникновение жидкости показывает, что дефекты находятся в пределах допустимого уровня. AlSi10Mg демонстрирует более высокие показатели предела текучести, предела прочности и относительного удлинения, равные (259±4) МПа, (323±4) МПа и (12,5±1,5) % соответственно. Показано, что дисперсионно-твердеющий AlSi10Mg, разработанный и производящийся в Индии, по свойствам не уступает аналогичным дисперсионно-твердеющим алюминиевым сплавам всемирно известных производителей.</p></trans-abstract><kwd-group xml:lang="en"><kwd>additive manufacturing</kwd><kwd>AlSi10Mg</kwd><kwd>Al alloy</kwd><kwd>precipitate hardening</kwd><kwd>development and certification</kwd></kwd-group><kwd-group xml:lang="ru"><kwd>аддитивное производство</kwd><kwd>AlSi10Mg</kwd><kwd>алюминиевый сплав</kwd><kwd>дисперсионное твердение</kwd><kwd>разработка и сертификация</kwd></kwd-group><funding-group/></article-meta></front><body></body><back><ref-list><ref id="B1"><label>1.</label><citation-alternatives><mixed-citation xml:lang="en">Bradford R.L., Cao L., Klosterman D., Herman F., Forman L., Browning C. A metal–metal powder formulation approach for laser additive manufacturing of difficult-to-print high-strength aluminum alloys. 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