Cast heat-resistant nickel alloy with monocrystal structure, intended for casting gas turbine engine blades
2024-04-01
专利权人TECHNOLOGIES SPECIAL METALLURGY SCI (TECH-Non-standard)
申请日期2024-04-01
专利号RU2828002-C1
成果简介NOVELTY - Invention relates to metallurgy, namely to casting heat-resistant nickel alloys with a single-crystal structure, intended for casting gas turbine engine blades, which operate for a long time at temperatures of order of 1,050-1,100 °C. Cast heat-resistant nickel alloy with monocrystal structure contains, wt.%: carbon 0.002-0.05, chromium 1.0-3.0, cobalt 2.0-4.0, tungsten 0.4-2.0, molybdenum 1.0-3.5, aluminium 5.5-6.5, tantalum 3.8-5.0, hafnium 0.05-0.6, rhenium 10.0-11.5, boron 0.005-0.02, zirconium 0.005-0.03, cerium 0.001-0.1, lanthanum 0.001-0.1, yttrium 0.001-0.1, magnesium 0.01-0.03, manganese 0.01-0.2, silicon 0.01-0.2, vanadium 0.05-0.6, scandium 0.005-0.03, praseodymium 0.005-0.05, nickel – balance. Heat resistance of alloy is provided. USE - Metallurgy. ADVANTAGE - Alloy has high heat resistance while maintaining specific weight at level of 8,88 g/cm3. 2 cl, 1 dwg, 2 tbl, 3 ex
IPC 分类号C22C-019/05
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/17439
专题中国科学院新疆生态与地理研究所
作者单位
TECHNOLOGIES SPECIAL METALLURGY SCI (TECH-Non-standard)
推荐引用方式
GB/T 7714
DANILOV D V,LOGUNOV A V,MIKHAYLOV A M,et al. Cast heat-resistant nickel alloy with monocrystal structure, intended for casting gas turbine engine blades. RU2828002-C1[P]. 2024.
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