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    • 7. 发明授权
    • Gas turbine nozzle
    • 燃气轮机喷嘴
    • US4283234A
    • 1981-08-11
    • US102828
    • 1979-12-12
    • Yutaka FukuiHiromi Kagohara
    • Yutaka FukuiHiromi Kagohara
    • F01D9/02C22C19/05F02C7/00
    • C22C19/052
    • A gas turbine nozzle made of a cast material having a chemical composition which contains 0.2 to 1 wt% carbon, 0.1 to 2 wt% silicon, 0.1 to 2 wt% manganese, 20 to 40 wt% chromium, 0.001 to 0.1 wt% boron, 5 to 20 wt% of at least one of tungsten and molybdenum and the remainder nickel. The material can contain at least one of carbide former which forms MC type carbides, e.g. titanium, niobium, hafnium, tantalum, zirconium and vanadium. The content of the carbide formers is between 0.1 and 2 wt%. Further, the material can contain 0.005 to 2 wt% of at least one of yttrium and aluminum. The material has a heat-treated structure in which eutectic carbides and secondary carbides are dispersed. The gas turbine nozzle made of this cast material exhibits a strength against thermal shock greater than that of conventional gas turbine nozzle made of a cobalt base alloy. Also, corrosion resistance, creep rupture strength, rupture strength and reduction of area are equivalent to or greater than those of the conventional gas turbine nozzle.
    • 一种由铸造材料制成的燃气轮机喷嘴,其具有含有0.2〜1重量%的碳,0.1〜2重量%的硅,0.1〜2重量%的锰,20〜40重量%的铬,0.001〜0.1重量%的硼, 5至20重量%的钨和钼中的至少一种,其余为镍。 该材料可以含有形成MC型碳化物的碳化物形成体中的至少一种,例如。 钛,铌,铪,钽,锆和钒。 碳化物前体的含量为0.1〜2重量%。 此外,该材料可以含有0.005〜2重量%的钇和铝中的至少一种。 该材料具有分散有共晶碳化物和二次碳化物的热处理结构。 由这种铸造材料制成的燃气轮机喷嘴表现出比由钴基合金制成的常规燃气轮机喷嘴的热冲击强度大。 此外,耐腐蚀性,蠕变断裂强度,断裂强度和面积的减少等于或大于常规燃气轮机喷嘴的抗腐蚀性。