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US4174213A Highly ductile alloys of iron-nickel-chromium-molybdenum system for gas turbine combustor liner and filler metals 失效
用于燃气轮机燃烧器衬套和填充金属的铁镍铬铬钼体系的高度延性合金

Highly ductile alloys of iron-nickel-chromium-molybdenum system for gas
turbine combustor liner and filler metals
摘要:
The present alloys of iron-nickel-chromium-molybdenum system are alloys having high strength and ductility, comprising 0.03-0.2% by weight of carbon, not more than 2% by weight of silicon, not more than 2% by weight of manganese, 42-70% by weight of nickel, 15-35% by weight of chromium, 4.5-15% by weight of molybdenum, 0.05-1.0% by weight of at least one of Ti and Nb as additive elements, and 7.5-35% by weight of iron, the balance being incidental impurities, or further contain 0.1-10% by weight of at least one of tungsten and cobalt as reinforcing elements.
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