ATI Nickel ATI C-263™
Precipitation Hardenable Nickel-Base Superalloy
The ATI C-263™ (UNS N07263) alloy is a high-temperature alloy commonly used in aircraft turbine engines and land-based gas turbines. It is typically supplied in the solution-annealed condition and then age-hardened by the customer after fabrication. The alloy is nickel based, but it also contains a significant amount of cobalt, which gives it superior high-temperature strength over other superalloys such as Types 718 and 625.
Typical applications require high strength at temperatures up to 1500°F (816°C) or oxidation resistance up to a temperature of 2000°F (1093°C). In addition to turbine engines, ATI C-263 alloy has also been used for components in automotive turbochargers.
The ATI C-263™ (UNS N07263) alloy is a high-temperature alloy commonly used in aircraft turbine engines and land-based gas turbines. It is typically supplied in the solution-annealed condition and then age-hardened by the customer after fabrication. The alloy is nickel based, but it also contains a significant amount of cobalt, which gives it superior high-temperature strength over other superalloys such as Types 718 and 625.
Typical applications require high strength at temperatures up to 1500°F (816°C) or oxidation resistance up to a temperature of 2000°F (1093°C). In addition to turbine engines, ATI C-263 alloy has also been used for components in automotive turbochargers.
一般属性
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物料形态
已商用：当前有效
文档
description
Technical Datasheet (English)
下载文档可用性
北美洲, 非洲和中东, 拉丁美洲, 欧洲, 亚太地区
其他属性
Applicable Specifications, Forms Available, Metal Type, Alloy Identification, Type Analysis, 密度, Tensile Strength (Ultimate), Tensile Strength (Yield), 0.2%, Tensile Elongation (Break), 硬度, 拉伸模量
加工
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