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

机译:具有外部磁控溅射陶瓷层的热屏障涂层,用于高温镍合金涡轮叶片

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摘要

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.
机译:实验室等温和离子浆热屏障Nicraly(RE,TA,HF)+ alniy(HF)+ Zrygdo涂料的循环耐热试验结果,其施加在含铼的高温VzHM-4合金的样品上 另外,综述钌,含铼和金属间VKNA-1V合金的Vzhm5Y合金。 通过含Y和Gd的锆合金靶标的磁控溅射施加外部陶瓷层(TBC),并具有柱状结构。 研究了TBC对1000℃和900℃的高循环疲劳的长期强度对长期强度的影响。 结果表明,根据测试结果,陶瓷层的最小损坏和在高温合金和VSDP上施加的VSDP-41 + VSDP-16 + VTS-4涂层观察到陶瓷层和最小质量损失 4 + VSDP-23 + VTSS-4涂层在金属间合金上涂覆。

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