| 분류 | 표면기술 |
|---|---|
| 기술명 | EBPVD_TBCs for Blades of Aircraft Gas Turbine Engines |
| 연구자 | Sung-hun Lee |
| 특허출원번호 | KR10-1438799 |
| 개요 | The thermal barrier coatings (TBCs) offer the potential to improve efficiencies of aero engines significantly.
TBCs, typically consisting of an yttria-stabilized zirconia top coat and a metallic bond coat deposited onto a superalloy substrate, are mainly used to extend a lifetime of gas turbine engine parts. TBCs fabricated by EB-PVD are favored for high-performance applications, because of reduced thermal conductivity, increased temperature capability, life prediction modeling, process modeling, bond coat oxidation, and hot corrosion resistance as well as improved erosion behavior. |
| 첨부파일 |  088_EBPVD_TBCs_for_Blades_of_Aircraft_Gas_Turbine_Engines.jpg (586.3K) [14] DATE : 2018-02-09 17:28:52 |
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