| Combustion chamber comprises sublayer of nickel-cobalt-chromium-aluminum-yttrium alloy and ceramic layer of zirconium dioxide-based material, upper ceramic layer made of gadolinium-zirconium oxide, and intermediate ceramic layer based on zirconium dioxide | |
| 2023-01-30 | |
| 专利权人 | TEHNOLOGICHESKIE SISTEMY ZASHCHITNYH POK (TEHN-Non-standard) |
| 申请日期 | 2023-01-30 |
| 专利号 | RU2023118186-A; RU2836715-C2 |
| 成果简介 | NOVELTY - A combustion chamber with a multilayer coating applied to its inner surface comprises a sublayer of a nickel-cobalt-chromium-aluminum-yttrium alloy and a ceramic layer of a zirconium dioxide-based material, an upper ceramic layer made of gadolinium-zirconium oxide (a) with 20-50 μ m thickness and roughness (Ra) of 4-5 μ m, and an intermediate ceramic layer based on zirconium dioxide is made of zirconium dioxide-dysprosium trioxide having thickness of 200-250 μ m with a roughness (Ra) of 5.5-7 μ m. The sublayer has thickness of 150-200 μ m with a roughness (Ra) of 5-6 μ m. USE - Combustion chamber. DETAILED DESCRIPTION - A combustion chamber with a multilayer coating applied to its inner surface comprises a sublayer of a nickel-cobalt-chromium-aluminum-yttrium (NiCoCrAlY) alloy and a ceramic layer of a zirconium dioxide-based material, an upper ceramic layer made of gadolinium-zirconium oxide of formula: Gd2Zr2O7(a) with 20-50 μ m thickness and roughness (Ra) of 4-5 μ m, and an intermediate ceramic layer based on zirconium dioxide is made of zirconium dioxide (ZrO2)-dysprosium trioxide (Dy2O3) having thickness of 200-250 μ m with a roughness (Ra) of 5.5-7 μ m. The sublayer has thickness of 150-200 μ m with a roughness (Ra) of 5-6 μ m. |
| IPC 分类号 | C23C-014/16 ; C23C-028/02 ; C23C-004/073 ; C23C-004/11 ; C23C-004/134 |
| 国家 | 俄罗斯 |
| 专业领域 | 材料科学 |
| 语种 | 英语 |
| 成果类型 | 专利 |
| 文献类型 | 科技成果 |
| 条目标识符 | http://119.78.100.226:8889/handle/3KE4DYBR/22325 |
| 专题 | 中国科学院新疆生态与地理研究所 |
| 作者单位 | TEHNOLOGICHESKIE SISTEMY ZASHCHITNYH POK (TEHN-Non-standard) |
| 推荐引用方式 GB/T 7714 | BALDAEV L KH,BALDAYEV S L,GIRFANOVA A G,et al. Combustion chamber comprises sublayer of nickel-cobalt-chromium-aluminum-yttrium alloy and ceramic layer of zirconium dioxide-based material, upper ceramic layer made of gadolinium-zirconium oxide, and intermediate ceramic layer based on zirconium dioxide. RU2023118186-A; RU2836715-C2[P]. 2023. |
| 条目包含的文件 | 条目无相关文件。 | |||||
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