Thermal-Barrier Coatings with an External Magnetron-Sputtered Ceramic Layer for High-Temperature Nickel Alloy Turbine Blades


Дәйексөз келтіру

Толық мәтін

Ашық рұқсат Ашық рұқсат
Рұқсат жабық Рұқсат берілді
Рұқсат жабық Тек жазылушылар үшін

Аннотация

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.

Авторлар туралы

S. Budinovskii

All-Russia Research Institute of Aviation Materials

Хат алмасуға жауапты Автор.
Email: bbssaa55@mail.ru
Ресей, Moscow, 105005

P. Matveev

All-Russia Research Institute of Aviation Materials

Email: bbssaa55@mail.ru
Ресей, Moscow, 105005

A. Smirnov

All-Russia Research Institute of Aviation Materials

Email: bbssaa55@mail.ru
Ресей, Moscow, 105005

D. Chubarov

All-Russia Research Institute of Aviation Materials

Email: bbssaa55@mail.ru
Ресей, Moscow, 105005

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