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    • 10. 发明公开
    • Method of controlling and refining final grain size in supersolvus heat treated nickel-base superalloys
    • Verfahren zur Steuerung derEndkorngrößebeisupersolvuswärmebehandeltenLegierungen auf Nickelbasis
    • EP2295612A1
    • 2011-03-16
    • EP10167751.6
    • 2010-06-29
    • General Electric Company
    • Mourer, David PaulBain, Kenneth Rees
    • C22C19/05C22F1/10F01D5/02
    • C22C19/056C22C19/03C22C19/057C22F1/10F05B2230/21
    • A gamma prime precipitation-strengthened nickel-base superalloy and method of forging an article (10) from the superalloy to promote a low cycle fatigue resistance and high temperature dwell behavior of the article (10). The superalloy has a composition of, by weight, 16.0-22.4% cobalt, 6.6-14.3% chromium, 2.6-4.8% aluminum, 2.4-4.6% titanium, 1.4-3.5% tantalum, 0.9-3.0% niobium, 1.9-4.0% tungsten, 1.9-3.9% molybdenum, 0.0-2.5% rhenium, greater than 0.05% carbon, at least 0.1% hafnium, 0.02-0.10% boron, 0.03-0.10% zirconium, the balance nickel and incidental impurities. A billet is formed of the superalloy and worked at a temperature below the gamma prime solvus temperature of the superalloy so as to form a worked article (10), which is then heat treated above the gamma prime solvus temperature of the superalloy to uniformly coarsen the grains of the article (10), after which the article (10) is cooled to reprecipitate gamma prime. The article (10) has an average grain size of not coarser than ASTM 7 and is substantially free of critical grain growth.
    • γ型析出强化镍基超级合金和从超合金锻造制品(10)的方法,以促进制品(10)的低循环耐疲劳性和高温停留行为。 超合金具有重量百分比为16.0-22.4%的钴,6.6-14.3%的铬,2.6-4.8%的铝,2.4-4.6%的钛,1.4-3.5%的钽,0.9-3.0%的铌,1.9-4.0% 钨,1.9-3.9%钼,0.0-2.5%铼,大于0.05%的碳,至少0.1%的铪,0.02-0.10%的硼,0.03-0.10%的锆,余量的镍和附带的杂质。 一个坯料由超级合金制成,并在低于该高合金的γ'固溶温度的温度下加工,以便形成一个加工制品(10),然后在超高温合金的γ'固溶温度之上进行热处理,以均匀地粗化 制品(10)的颗粒,之后将制品(10)冷却以再沉淀γ'。 制品(10)的平均粒径不比ASTM 7粗,并且基本上没有临界晶粒生长。