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A process for the increase of the fatigue strength in the case of high temperature stress of as a single crystal or with microstructures castings produced from nickel-based superalloys
A process for the increase of the fatigue strength in the case of high temperature stress of as a single crystal or with microstructures castings produced from nickel-based superalloys
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机译:在单晶或由镍基高温合金制成的微结构铸件承受高温应力的情况下提高疲劳强度的方法
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摘要
1,260,195. Unidirectionally solidified Ni-base superalloys. UNITED AIRCRAFT CORP. April 16, 1969 [May 1, 1968], No.19539/69. Heading C7A. A Ni base superalloy comprising a dispersion of Ni 3 (Al 1 Ti 1 Nb) in a Ni-Cr solid solution matrix has its C content limited to 0À01% max. and is unidirectionally solidified to form a single crystal or columnar-grained article. The superalloy preferably comprises:- the balance, apart from the 0-0À01% C, being Ni.
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机译:1,260,195。单向凝固的镍基高温合金。联合飞机公司1969年4月16日[1968年5月1日],编号19539/69。标题C7A。包含Ni 3(Al 1 Ti 1 Nb)在Ni-Cr固溶体基质中的分散体的Ni基超合金的C含量限制为最大0‑01%。并单向固化形成单晶或柱状颗粒制品。超级合金优选地包括:-除0-0-01%的C外,其余为Ni。
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