Alloy, protective coating and component

文件类型：PDF文档
文件大小：265K
Alloy comprises 24-26 wt.%, preferably 25 wt.% of cobalt, 16-25 wt.% of chromium, 9-12 wt.% of aluminum, 0.1-0.7 wt.% of yttrium and/or at least one equivalent metal comprising scandium or rare earth elements, optionally 0.1-0.7 wt.%, preferably 0.6 wt.% of phosphorus, optionally 0.1-0.6 wt.%, preferably 0.5 wt.% of silicon, optionally 1-2 wt.% of rhenium, and nickel making up the remainder. Independent claims are included for : (1) a protective layer (7) for the protection of a device (1) against corrosion and/or oxidation, preferably at high temperature, comprising the alloy; and (2) the device, preferably gas turbine, comprising a substrate (4) on the basis of nickel or cobalt, a protective layer for protection against corrosion and oxidation, and a ceramic heat insulation layer (10).