Thermal-Barrier Coatings with an External Magnetron-Sputtered Ceramic Layer for High-Temperature Nickel Alloy Turbine Blades
- Authors: Budinovskii S.A.1, Matveev P.V.1, Smirnov A.A.1, Chubarov D.A.1
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Affiliations:
- All-Russia Research Institute of Aviation Materials
- Issue: Vol 2019, No 6 (2019)
- Pages: 617-623
- Section: Hardening and Coating Technologies
- URL: https://journals.rcsi.science/0036-0295/article/view/173294
- DOI: https://doi.org/10.1134/S0036029519060090
- ID: 173294
Cite item
Abstract
The results of laboratory isothermal and cyclic heat-resistance tests of ion-plasma thermal-barrier NiCrAlY (Re, Ta, Hf) + AlNiY (Hf) + ZrYGdO coatings, which were applied on samples of high-temperature VZhM-4 alloy containing rhenium plus ruthenium, VZhM5Y alloy containing rhenium, and intermetallic VKNA-1V alloy, are reported. An external ceramic layer of thermal-barrier coatings (TBCs) is applied by the magnetron sputtering of Y- and Gd-containing zirconium alloy targets and has a columnar structure. The effect of TBCs on the long-term strength at a test temperature of 1000°C and on the high-cycle fatigue at 900°C is studied. It is shown that, according to the test results, the minimum damages of the ceramic layer and the minimum mass losses are observed for the VSDP-41 + VSDP-16 + VTsS-4 coating applied on the high-temperatures alloys and the VSDP-4 + VSDP-23 + VTsS-4 coating applied on the intermetallic alloy.
About the authors
S. A. Budinovskii
All-Russia Research Institute of Aviation Materials
Author for correspondence.
Email: bbssaa55@mail.ru
Russian Federation, Moscow, 105005
P. V. Matveev
All-Russia Research Institute of Aviation Materials
Email: bbssaa55@mail.ru
Russian Federation, Moscow, 105005
A. A. Smirnov
All-Russia Research Institute of Aviation Materials
Email: bbssaa55@mail.ru
Russian Federation, Moscow, 105005
D. A. Chubarov
All-Russia Research Institute of Aviation Materials
Email: bbssaa55@mail.ru
Russian Federation, Moscow, 105005
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