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1.发明申请ALLOY MATERIAL HAVING HIGH-TEMPERATURE CORROSION RESISTANCE, THERMAL BARRIER COATING, TURBINE MEMBER, AND GAS TURBINE 有权合金材料具有高温耐腐蚀性，热障涂层，涡轮部件和气体涡轮公开(公告)号：US20100247950A1
公开(公告)日：2010-09-30
申请号：US12741503
申请日：2009-03-13
申请人： Taiji Torigoe , Hidetaka Oguma , Ikuo Okada , Tomoaki Yunomura , Soji Kasumi
发明人： Taiji Torigoe , Hidetaka Oguma , Ikuo Okada , Tomoaki Yunomura , Soji Kasumi
CPC分类号： C23C30/00 , C22C19/058 , C22C19/07 , C22C30/00 , C23C28/321 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2230/90 , Y10T428/12535 , Y10T428/12861 , Y10T428/12931 , Y10T428/12944
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.
摘要翻译： 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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2.发明授权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公开(公告)号：US08409722B2
公开(公告)日：2013-04-02
申请号：US12741503
申请日：2009-03-13
申请人： Taiji Torigoe , Hidetaka Oguma , Ikuo Okada , Tomoaki Yunomura , Soji Kasumi
发明人： Taiji Torigoe , Hidetaka Oguma , Ikuo Okada , Tomoaki Yunomura , Soji Kasumi
CPC分类号： C23C30/00 , C22C19/058 , C22C19/07 , C22C30/00 , C23C28/321 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2230/90 , Y10T428/12535 , Y10T428/12861 , Y10T428/12931 , Y10T428/12944
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.
摘要翻译： 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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公开(公告)号：US20100215148A1
公开(公告)日：2010-08-26
申请号：US12526213
申请日：2008-01-30
申请人： Taiji Torigoe , Masahiro Yamada , Ikuo Okada , Toshio Sakon , Hidetaka Oguma , Takeshi Naito , Koji Takahashi , Soji Kasumi , Keizo Tsukagoshi
发明人： Taiji Torigoe , Masahiro Yamada , Ikuo Okada , Toshio Sakon , Hidetaka Oguma , Takeshi Naito , Koji Takahashi , Soji Kasumi , Keizo Tsukagoshi
CPC分类号： G01N1/286 , G01N2001/2873 , Y10T83/04
摘要： In a specimen collecting method according to the present invention, a specimen is collected from a surface (114a) of a blade. An ultrasonic cutter having a cylindrical cutting blade is fed from the surface (114a) of the blade to a surface (110a) of a base material (100), and thus, a cylindrical incision is formed. After performing cutting to expand the incision outwardly, a rotating cutter (220) having a disc-shaped cutting blade (222) performs cutting inwardly from the cylindrical incision. Thus, a part (20a) situated inside the incision is cut away. The part (20a) becomes the specimen.
摘要翻译： 在根据本发明的样本收集方法中，从叶片的表面（114a）收集样本。 具有圆柱形切割刀片的超声波切割器从叶片的表面（114a）进给到基材（100）的表面（110a），从而形成圆柱形切口。 在执行切割以向外扩张切口之后，具有盘形切割刀片（222）的旋转切割器（220）从圆柱形切口向内切割。 因此，位于切口内部的部分（20a）被切除。 部件（20a）成为样品。
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公开(公告)号：US08287186B2
公开(公告)日：2012-10-16
申请号：US12526213
申请日：2008-01-30
申请人： Taiji Torigoe , Masahiro Yamada , Ikuo Okada , Toshio Sakon , Hidetaka Oguma , Takeshi Naito , Koji Takahashi , Soji Kasumi , Keizo Tsukagoshi
发明人： Taiji Torigoe , Masahiro Yamada , Ikuo Okada , Toshio Sakon , Hidetaka Oguma , Takeshi Naito , Koji Takahashi , Soji Kasumi , Keizo Tsukagoshi
IPC分类号： G01K11/00
CPC分类号： G01N1/286 , G01N2001/2873 , Y10T83/04
摘要： In a specimen collecting method according to the present invention, a specimen is collected from a surface (114a) of a blade. An ultrasonic cutter having a cylindrical cutting blade is fed from the surface (114a) of the blade to a surface (110a) of a base material (100), and thus, a cylindrical incision is formed. After performing cutting to expand the incision outwardly, a rotating cutter (220) having a disc-shaped cutting blade (222) performs cutting inwardly from the cylindrical incision. Thus, a part (20a) situated inside the incision is cut away. The part (20a) becomes the specimen.
摘要翻译： 在根据本发明的样本收集方法中，从叶片的表面（114a）收集样本。 具有圆柱形切割刀片的超声波切割器从叶片的表面（114a）进给到基材（100）的表面（110a），从而形成圆柱形切口。 在执行切割以向外扩张切口之后，具有盘形切割刀片（222）的旋转切割器（220）从圆柱形切口向内切割。 因此，位于切口内部的部分（20a）被切除。 部件（20a）成为样品。
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5.发明申请Oxidation-resistant coating and formation method thereof, thermal barrier coating, heat-resistant member, and gas turbine 审中-公开耐氧化涂层及其形成方法，隔热涂层，耐热构件和燃气轮机公开(公告)号：US20070224443A1
公开(公告)日：2007-09-27
申请号：US11657122
申请日：2007-01-24
申请人： Taiji Torigoe , Ikuo Okada , Tomoaki Yunomura , Hidetaka Oguma , Toshio Sakon , Yutaka Kawata
发明人： Taiji Torigoe , Ikuo Okada , Tomoaki Yunomura , Hidetaka Oguma , Toshio Sakon , Yutaka Kawata
CPC分类号： F02K9/974 , C23C4/073 , C23C10/02 , C23C10/08 , C23C10/26 , C23C28/321 , C23C28/3215 , C23C28/325 , C23C28/3455 , C23C30/00 , F01D5/288 , F05D2230/90 , F05D2260/95 , F05D2300/134 , F05D2300/15 , F05D2300/611 , Y10T428/12611 , Y10T428/12931 , Y10T428/12944
摘要： The present invention provides an oxidation-resistant coating having superior oxidation resistance and superior ductility and toughness for long-term use, and a method for forming the oxidation-resistant coating. An MCrAlY layer primarily containing an MCrAlY alloy (in which M indicates at least one element of Co and Ni) is formed on a substrate formed of a heat-resistant metal by thermal spraying or EB=PVD, and subsequently, aluminum is diffused into a part of the MCrAlY layer in the thickness direction thereof from a side opposite to the substrate.
摘要翻译： 本发明提供了具有优异的抗氧化性和长期使用的优异的延展性和韧性的耐氧化涂层以及形成抗氧化涂层的方法。 通过热喷涂或EB = PVD在由耐热金属形成的基板上形成主要含有MCrAlY合金（其中M表示Co和Ni的至少一种元素）的MCrAlY层，随后将铝扩散到 MCrAlY层的厚度方向的一部分与基板相反的一侧。
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6.发明授权公开(公告)号：US06756131B2
公开(公告)日：2004-06-29
申请号：US10316070
申请日：2002-12-11
申请人： Hidetaka Oguma , Ikuo Okada , Taiji Torigoe , Kouji Takahashi
发明人： Hidetaka Oguma , Ikuo Okada , Taiji Torigoe , Kouji Takahashi
IPC分类号： F03B312
CPC分类号： C23C28/3215 , C22C19/058 , C23C4/02 , C23C4/073 , C23C28/345 , C23C28/3455 , C23C30/00 , Y02T50/67 , Y10T428/12535 , Y10T428/1259 , Y10T428/12611 , Y10T428/12618 , Y10T428/12944
摘要： A high temperature corrosion resistant alloy composition comprising, in addition to Ni, 0.1 to 12% by weight of Co, 10 to 30% by weight of Cr, 4 to 15% by weight of Al, 0.1 to 5% by weight of Y, and 0.5 to 10% by weight of Re. The high temperature corrosion resistant alloy composition has an excellent oxidation resistance and ductility and is suitable for use in a bonding layer of a thermal barrier coating material.
摘要翻译： 一种高温耐腐蚀合金组合物，除了Ni之外还包含0.1〜12重量％的Co，10〜30重量％的Cr，4〜15重量％的Al，0.1〜5重量％的Y， 和0.5〜10重量％的Re。 高温耐腐蚀合金组合物具有优异的抗氧化性和延展性，并且适用于热障涂层材料的粘合层。
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公开(公告)号：US07261758B2
公开(公告)日：2007-08-28
申请号：US11012222
申请日：2004-12-16
申请人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Masahiko Onda , Takeshi Seto
发明人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Masahiko Onda , Takeshi Seto
CPC分类号： B23P6/002 , B22F1/0003 , B22F2998/00 , B22F2999/00 , C22C1/0433 , B22F3/1035
摘要： Disclosed is a Ni-based sintered alloy used for preparing a high temperature part utilized under a high temperature gas atmosphere, characterized in that the Ni-based sintered alloy is prepared by mixing and heating two kinds of Ni alloy powders differing from each other in the melting point.
摘要翻译： 公开了一种用于制备在高温气氛下使用的高温部分的Ni基烧结合金，其特征在于，Ni基烧结合金通过混合和加热两种相互不同的Ni合金粉末 熔点
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公开(公告)号：US20050097986A1
公开(公告)日：2005-05-12
申请号：US11012222
申请日：2004-12-16
申请人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Mashiko Onda , Takeshi Seto
发明人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Mashiko Onda , Takeshi Seto
CPC分类号： B23P6/002 , B22F1/0003 , B22F2998/00 , B22F2999/00 , C22C1/0433 , B22F3/1035
摘要： Disclosed is a Ni-based sintered alloy used for preparing a high temperature part utilized under a high temperature gas atmosphere, characterized in that the Ni-based sintered alloy is prepared by mixing and heating two kinds of Ni alloy powders differing from each other in the melting point.
摘要翻译： 公开了一种用于制备在高温气氛下使用的高温部分的Ni基烧结合金，其特征在于，Ni基烧结合金通过混合和加热两种相互不同的Ni合金粉末 熔点
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公开(公告)号：US06884275B2
公开(公告)日：2005-04-26
申请号：US10425830
申请日：2003-04-30
申请人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Masahiko Onda , Takeshi Seto
发明人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Masahiko Onda , Takeshi Seto
CPC分类号： B23P6/002 , B22F1/0003 , B22F2998/00 , B22F2999/00 , C22C1/0433 , B22F3/1035
摘要： Disclosed is a Ni-based sintered alloy used for preparing a high temperature part utilized under a high temperature gas atmosphere, characterized in that the Ni-based sintered alloy is prepared by mixing and heating two kinds of Ni alloy powders differing from each other in the melting point.
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公开(公告)号：US20050005733A1
公开(公告)日：2005-01-13
申请号：US10425830
申请日：2003-04-30
申请人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Masahiko Onda , Takeshi Seto
发明人： Ikuo Okada , Kei Ohsawa , Hidetaka Oguma , Koji Takahashi , Masahiko Onda , Takeshi Seto
CPC分类号： B23P6/002 , B22F1/0003 , B22F2998/00 , B22F2999/00 , C22C1/0433 , B22F3/1035
摘要： Disclosed is a Ni-based sintered alloy used for preparing a high temperature part utilized under a high temperature gas atmosphere, characterized in that the Ni-based sintered alloy is prepared by mixing and heating two kinds of Ni alloy powders differing from each other in the melting point.
摘要翻译： 公开了一种用于制备在高温气氛下使用的高温部分的Ni基烧结合金，其特征在于，Ni基烧结合金通过混合和加热两种相互不同的Ni合金粉末 熔点
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