Udimet 188 is a high-temperature aerospace alloy with excellent strength and oxidation resistance. It is used in applications such as gas turbine blades and combustion area parts. The alloy has a tenacious oxide film. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on forming, heat treating, and joining. Filing Code: CO-110. Producer or source: Special Metals Corporation.

chemical composition, combustion parts, creep properties, gas turbine blades, heat treatability, joinability, oxidation resistance, oxide film, physical properties, tensile properties, Udimet 188, workability, thermal properties, UNS R30188
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Copyright © ASM International® 2005
2005
ASM International
Topics
Gas turbines Internal combustion engines Cobalt alloys Chemical composition Oxidation resistance Heat treatability Joinability Workability Creep properties Tensile properties Physical properties Thermal properties
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