In China, mainly detailed research for high temperature alloys and completely . Other high temperature different alloys are not strengthened with bond ordered deposits on high-temperature alloy Cobalt-Chromium Alloy, but small amount of carbide distribution is enhanced by FCC austenite solid solution matrix and matrix composition. Casting a Cobalt-Chromium Alloy superalloy depends primarily on silicon carbide strengthening. Pure cobalt crystal is less than 417 ° C. Crystal structure C, FCC of hexagonal close packed (HCP) is converted at higher temperature. To avoid Cobalt-Chromium Alloy transitions in such superalloys, in fact, all of the nickel alloy Cobalt-Chromium Alloy section, melting point occurs during use, so as to stabilize the temperature range of the tissue at room temperature. It is possible to have it because there is an upper high chromium containing alloy, such as alloy, which has been shown that the Cobalt-Chromium Alloy-temperature relationship with plane fracture stress has an excellent high temperature other than high temperature corrosion resistance at 1000 ° C .
Cobalt-base superalloys generally have low and moderate high temperature strength (nickel-based alloys of only 50 to 75 percent) at temperatures above 980 ° C lack coherent reinforcing phase, but high strength, good heat Fatigue and corrosion resistance Wear resistance performance, and with excellent weldability. Suitable for manufacturing aircraft jet engines, industrial gas turbines, marine gas turbine blades and nozzle guide vanes and diesel engine nozzles.
Pure cobalt crystal is less than 417 ° C. Crystal structure C, FCC of hexagonal close packed (HCP) is converted at higher temperature. To avoid Cobalt-Chromium Alloy transitions in such superalloys, in fact, all of the nickel alloy Cobalt-Chromium Alloy section, melting point occurs during use, so as to stabilize the temperature range of the tissue at room temperature. It is possible to have it because there is an upper high chromium containing alloy, such as alloy, which has been shown that the Cobalt-Chromium Alloy-temperature relationship with plane fracture stress has an excellent high temperature other than high temperature corrosion resistance at 1000 ° C .
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