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Information × Registration Number 0225U005278, (0125U000636) , R & D reports Title Development of a multilayer composite thermal barrier coating (1200–1300 °C) and vacuum technology for its application to aircraft engine blades popup.stage_title Розробка багатошарового композиційного термобар’єрного покриття (1200–1300 С) та вакуумної технології його нанесення на робочі лопатки авіаційних двигунів Head Klymenko Serhii A., д.т.н. Registration Date 29-12-2025 Organization V. Bakul Institute of superhard material of the National Academy of Sciences of Ukraine popup.description1 Development of a multilayer composite thermal barrier coating that operates at temperatures of 1200–1300 °C, modernization of existing equipment and creation of a vacuum coating technology for aircraft engine blades popup.description2 A multilayer composite thermal barrier coating, resistant to temperatures of 1200–1300 °C, and a vacuum technology for its application to the working aircraft engine blades have been developed. The properties, elemental chemical and phase composition of the heat-resistant alloy ЖС32 and the multilayer coating applied to its surface, obtained by magnetron sputtering using NiCrAlY cathode, the coating deposited using ZrB2 + MoSi2 ceramic cathode, and vacuum-arc oxide coating applied using WTiYTaMo cathode, have been analyzed. A multilayer coating architecture, which consists of alternate heat-resistant NiCrAlY layers and oxide or boride ceramics layers, has been proposed. Samples of engine blades with the multilayer composite thermal barrier coatings have been transferred to the Zaporizhzhia Machine-Building Design Bureau “Progress” LLC named after Academician O.G. Ivchenko" for further testing. Product Description popup.authors Beresniev Viacheslav M. Melnychuk Yurii O. Klymenko Serhii A. Riabchenko Serhii V. Kopieikina Maryna Yu. Manokhin Andrii S. Ryzhov Yurii E. Bondar Ivan V. Chumak Anatolii O. Zharovskyi Hryhorii Ya. Mykola S. Sokolan popup.nrat_date 2025-12-29 Close