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Inconel 625 was designed as a solid solution strengthened material with no significant microstructure. This holds true at low and high temperatures, but there is a region (923 to 1148 K) where precipitates form that are detrimental to the creep properties, and thus the strength, of the alloy.
Nimonic alloys typically consist of more than 50% nickel and 20% chromium with additives such as titanium and aluminium. The main use is in gas turbine components and extremely high performance reciprocating internal combustion engines.
Inconel 617: Solid solution strengthened (nickel-chromium-cobalt-molybdenum), high-temperature strength, corrosion and oxidation resistant, high workability and weldability. [66] Incorporated in ASME Boiler and Pressure Vessel Code for high temperature nuclear applications such as molten salt reactors c. April, 2020. [67]
High-temperature. Can be used for brazing tungsten. 2.2: Nb 97.8: Nb 80 Ti 20 [5] – High-temperature. Can be used for brazing tungsten. 20: Nb 80: Pt 85 W 11 B 4 [5] – High-temperature. Joint remelt temperature 2200 °C. Can be used for brazing tungsten. 85: 11: 4: W 75 Os 25 [5] – Very-high-temperature. Requires very intense heating, e.g ...
Nickel superalloy jet engine turbine blade. A superalloy, or high-performance alloy, is an alloy with the ability to operate at a high fraction of its melting point. [1] Key characteristics of a superalloy include mechanical strength, thermal creep deformation resistance, surface stability, and corrosion and oxidation resistance.
Alloy 230 is a nickel alloy, made up of mostly nickel and chromium, with smaller amounts of tungsten and molybdenum.This combination of metals results in a number of desirable properties including excellent strength, oxidation resistance at temperatures of up to 2,100 °F (1,150 °C) and nitriding-resistance.
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