首页> 外国专利> Articles made of nickel-based superalloys, nickel-based superalloy, the heat treatment method of the nickel-based alloy cast article, the columnar grain nickel-based superalloy cast article manufacturing method and a columnar grain nickel base superalloy gas turbine engine turbine blades method of manufacturing a cast member

Articles made of nickel-based superalloys, nickel-based superalloy, the heat treatment method of the nickel-based alloy cast article, the columnar grain nickel-based superalloy cast article manufacturing method and a columnar grain nickel base superalloy gas turbine engine turbine blades method of manufacturing a cast member

机译:镍基高温合金制成的物品,镍基高温合金,镍基合金铸造物品的热处理方法,柱状晶粒镍基高温合金铸造物品的制造方法以及柱状晶粒镍基高温合金燃气涡轮发动机的涡轮叶片方法铸件的制造

摘要

One form of an improved cast, hollow, columnar grain nickel base alloy article is provided with outstanding elevated temperature stability as represented by oxidation resistance, an improved combination of longitudinal and transverse stress rupture properties, and a thin wall of less than about 0.035 inch, substantially free of cracks. Described is a heat treatment in combination with an alloy for providing such an article. The alloy contains essentially in weight percent: C 0.1-0.15 Hf 0.3-2 Co 11-14 Ta 5-9 V no more than 1 Zr less than .05 Cr 5-10 Mo 0.5-3 W 4-7 Ti no more than 1 Al 5-7 Re 1.5-4 B .005-.03 Cb 0-1.5 Y 0-0.5 Ni Rest Articles produced in the alloy may be solution annealed at 2025-2075 DEG F (1246-1293 DEG C) and aged in a multi-step aging process.
机译:一种形式的改进的铸造空心空心柱状晶粒镍基合金制品具有出色的高温稳定性,表现为抗氧化性,纵向和横向应力断裂性能的改进组合以及小于约0.035英寸的薄壁,基本上没有裂缝。描述了与合金组合的热处理以提供这种制品。该合金的重量百分比基本上为:C 0.1-0.15 Hf 0.3-2 Co 11-14 Ta 5-9 V不大于1 Zr小于0.05 Cr 5-10 Mo 0.5-3 W 4-7 Ti不大于1 Al 5-7 Re 1.5-4 B .005-.03 Cb 0-1.5 Y 0-0.5 Ni残余物合金中生产的制品可在2025-2075 F(1246-1293 C)下固溶退火并在一个多步骤的老化过程。

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