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US08409722B2 Alloy material having high-temperature corrosion resistance, thermal barrier coating, turbine member, and gas turbine 有权
具有耐高温腐蚀性的合金材料，隔热涂层，涡轮部件和燃气轮机

Alloy material having high-temperature corrosion resistance, thermal barrier coating, turbine member, and gas turbine
摘要：
An alloy material having high-temperature corrosion resistance, which exhibits excellent oxidation resistance and ductility and can be applied to gas turbines used at ultra high temperatures, and a thermal barrier coating, a turbine member and a gas turbine each comprising the alloy material. An alloy material having high-temperature corrosion resistance, comprising, by weight, Co: 15 to 30%, Cr: 10 to 30%, Al: 4 to 15%, Y: 0.1 to 3%, and Re: 0.1 to 1%, with the balance being substantially Ni. Also, an alloy material having high-temperature corrosion resistance, comprising, by weight, Ni: 20 to 40%, Cr: 10 to 30%, Al: 4 to 15%, Y: 0.1 to 3%, and Re: 0.1 to 5%, with the balance being substantially Co.
摘要（中）：

具有高温耐腐蚀性的合金材料，其具有优异的抗氧化性和延展性，并且可以应用于在超高温下使用的燃气轮机，以及每个包含合金材料的隔热涂层，涡轮机构件和燃气轮机。 Co：15〜30％，Cr：10〜30％，Al：4〜15％，Y：0.1〜3％，Re：0.1〜1％的耐高温性的合金材料， ，其余为Ni。 另外，具有高温耐腐蚀性的合金材料中，Ni：20〜40％，Cr：10〜30％，Al：4〜15％，Y：0.1〜3％，Re：0.1〜 5％，余额基本为公司

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