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NANOCARBIDE PRECIPITATION STRENGTHENED ULTRAHIGH-STRENGTH, CORROSION RESISTANT, STRUCTURAL STEELS

机译:纳米碳化物沉淀强化了超高强度,耐腐蚀,结构钢

摘要

A nanocarbide precipitation strengthenedultrahigh-strength, corrosion resistant, structural steelpossesses a combination of strength and corrosion resistancecomprising in combination, by weight, about: 0.1 to 0.3%carbon (C), 8 to 17% cobalt (Co), 5 to 10% nickel (Nl), 6 to12% chromium (Cr), less than 1% silicon (Sl), less than 0.5%manganese (Mn), and less than 0.15% copper (Cu), withadditives selected from the group comprising about: lessthan 3% molybdenum (Mo), less than 0.3% niobium (Nb), lessthan 0.8% vanadium (V), less than 0.2% tantalum (Ta), lessthan 3% tungsten (W), and combinations thereof, withadditional additives selected from the group comprisingabout: less than 0.2% titanium (Ti), less than 0.2%lanthanum (La) or other rare earth elements, less than 0.15%zirconium (Zr), less than 0.005% boron (B), and combinationsthereof, impurities of less than about: 0.02% sulfur (S),0.012% phosphorus (P), 0.015% oxygen (O) and 0.015% nitrogen(N), the remainder substantially iron (Fe), incidentalelements and other impurities. The alloy is strengthened bynanometer scale MZC carbides within a fine lath martensitematrix from which enhanced chemical partitioning of Cr tothe surface provides a stable oxide passivating film forcorrosion resistance. The alloy, with a UTS in excess of280 ksi, is useful for applications such as aircraft landinggear, machinery and tools used in hostile environments, andother applications wherein ultrahigh-strength, corrosionresistant, structural steel alloys are desired.
机译:纳米碳化物沉淀增强超高强度,耐腐蚀,结构钢兼具强度和耐腐蚀性以重量计约占0.1至0.3%碳(C),8至17%的钴(Co),5至10%的镍(Nl),6至12%铬(Cr),少于1%硅(Sl),少于0.5%锰(Mn)和少于0.15%的铜(Cu),选自以下的添加剂:较少钼(Mo)小于3%,铌(Nb)小于0.3%钒(V)小于0.8%,钽(Ta)小于0.2%大于3%的钨(W)及其组合,选自以下的其他添加剂:约:小于0.2%钛(Ti),小于0.2%镧(La)或其他稀土元素,小于0.15%锆(Zr),小于0.005%硼(B)及其组合杂质小于约0.02%的硫(S)0.012%的磷(P),0.015%的氧气(O)和0.015%的氮气(N),其余基本上是铁(Fe),附带元素和其他杂质。合金通过细条状马氏体中的纳米级MZC碳化物Cr增强化学分配的基质表面提供了稳定的氧化物钝化膜,用于耐腐蚀性能。合金,UTS超过280 ksi,适用于飞机降落等应用在敌对环境中使用的齿轮,机械和工具,以及其他超高强度,腐蚀的应用要求有耐腐蚀的结构钢合金。

著录项

  • 公开/公告号CA2475248C

    专利类型

  • 公开/公告日2011-04-05

    原文格式PDF

  • 申请/专利权人 QUESTEK INNOVATIONS LLC;

    申请/专利号CA20032475248

  • 申请日2003-02-07

  • 分类号C22C38/30;C21D6/00;C21D8/00;C22C38/00;C22C38/44;C22C38/52;C22C38/54;

  • 国家 CA

  • 入库时间 2022-08-21 18:02:22

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