Evaluation of the possibility of detecting cracks during the control of luminescence on turbine blades after application of complex heat-resistant coatings

Currently, gas turbine engines (GTD) are being improved and made more powerful by increasing the temperature of the gases in front of the turbine and increasing the air compression ratio in the compressor. In the aviation industry, nickel heat-resistant alloys such as ЖС6У-ВІ, ЖС26-ВІ, ЖС32-ВІ, etc....

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Bibliographic Details

Published in:	Авіаційно-космічна техніка та технологія
Main Authors:	Konstantin Balushok, Oleksandr Seliverstov, Oleksandr Prokopenko, Sergii Sakhno
Format:	Article
Language:	English
Published:	National Aerospace University «Kharkiv Aviation Institute» 2024-10-01
Subjects:	покриття комплексні жаростійкі покриття іонно-плазмові покриття лопатки турбіни люмінесцентний контроль тріщини
Online Access:	http://nti.khai.edu/ojs/index.php/aktt/article/view/2581