| 摘要 |
An alloy steel for high temperature applications, such as for compressor and turbine discs in gas turbines consists essentially of: 0.02-0.25 percent carbon, 0.05-1.5 percent silicon, 0.1-1.5 percent manganese, 7.0-12.0 percent chromium, 0.2-4.0 percent nickel, 0.2-5.0 percent molybdenum, 0.10-0.60 percent vanadium, 0.05-0.70 percent niobium, up to 7.0 percent cobalt, up to 5.0 percent copper, 0.002-0.03 percent boron, at least 0.010 percent but less than 0.050 percent nitrogen, the balance, apart from incidental impurities being iron.
|
