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    NI-BASED SINGLE CRYSTAL ALLOY
    142.
    发明申请
    NI-BASED SINGLE CRYSTAL ALLOY 审中-公开
    基于NI的单晶合金

    公开(公告)号：US20090214379A1

    公开(公告)日：2009-08-27

    申请号：US12389633

    申请日：2009-02-20

    Applicant: Akira Yoshinari ,  Hideki Tamaki

    Inventor： Akira Yoshinari ,  Hideki Tamaki

    IPC: C22C19/05

    CPC classification number: C22C19/057 ,  F01D5/28 ,  F05C2201/025 ,  F05C2201/0466 ,  F05D2300/11 ,  F05D2300/121 ,  F05D2300/131 ,  F05D2300/132 ,  F05D2300/134 ,  F05D2300/607 ,  Y02T50/671

    Abstract: Disclosed is a single crystal alloy consisting essentially of, by weight, 0.06-0.09% carbon, 0.016-0.035% B, 0.2-0.4% Hf, 0-0.02% Zr, 6.5-8.5% Cr, 0.4-1.0% Mo, 5.5-9.5% W, 1.2-3.1% Re, 8-10% Ta, 0.3-1.0% Nb, 0-0.4% Ti, 4.7-5.4% Al, 0.5-5.0% Co, 0.1-5% Fe, and the balance of Ni and unavoidable impurities. The alloy is free from solidification cracks during casting a large-sized blade of gas turbines, has grain boundary strength sufficient for assuring the reliability during operation, and further has excellent oxidation resistance to a high combustion gas temperature while having excellent high-temperature strength comparable to that of a conventional single crystal alloy.

    Abstract translation: 公开了基本上由0.06-0.09％的碳，0.016-0.035％的B，0.2-0.4％的Hf，0-0.02％的Zr，6.5-8.5％的Cr，0.4-1.0％的Mo，5.5 -9.5％W，1.2-3.1％Re，8-10％Ta，0.3-1.0％Nb，0-0.4％Ti，4.7-5.4％Al，0.5-5.0％Co，0.1-5％Fe，余量 的Ni和不可避免的杂质。 该合金在铸造大型燃气轮机叶片期间没有固化裂纹，具有足够的晶界强度以确保运行时的可靠性，并且还具有优异的耐高温燃烧气体温度的抗氧化性，同时具有优异的高温强度可比性 与传统的单晶合金相比。

    Vacuum pump
    143.
    发明授权
    Vacuum pump 有权
    真空泵

    公开(公告)号：US07572096B2

    公开(公告)日：2009-08-11

    申请号：US11092898

    申请日：2005-03-29

    Applicant: Manabu Nonaka ,  Akihiko Wada

    Inventor： Manabu Nonaka ,  Akihiko Wada

    IPC: F03B11/02

    CPC classification number: F04D19/04 ,  F04D29/023 ,  F05C2201/0466 ,  F05D2230/90 ,  F05D2260/95 ,  F05D2300/16 ,  F05D2300/17 ,  F05D2300/21 ,  F05D2300/611

    Abstract: A vacuum pump is provided in which gas molecules in a vacuum chamber are sucked and exhausted by the rotational motion of a rotor rotatably supported in a pump case. At least one nickel alloy layer is disposed on a surface of at least one component defining a flow path in the vacuum pump for increasing a resistance of the component to corrosion due to a corrosive effect of a gas flowing through the flowpath. A nickel oxide is formed on a surface of the nickel alloy layer and has a higher emissivity than that of the nickel alloy layer for increasing a quantity of heat radiated from the surface of the component when the component is heated during operation of the vacuum pump.

    Abstract translation: 提供一种真空泵，其中真空室中的气体分子通过可旋转地支撑在泵壳中的转子的旋转运动而被吸入和排出。 至少一个镍合金层设置在限定真空泵中的流路的至少一个部件的表面上，用于由于流过流路的气体的腐蚀作用而增加部件对腐蚀的阻力。 在镍合金层的表面上形成氧化镍，并且具有比镍合金层更高的发射率，用于在真空泵的运行期间加热部件时，增加从部件表面辐射的热量。

    Leakage seal for gas path of gas turbine
    145.
    发明授权
    Leakage seal for gas path of gas turbine 有权
    燃气轮机气路泄漏密封

    公开(公告)号：US07389991B2

    公开(公告)日：2008-06-24

    申请号：US11236243

    申请日：2005-09-27

    Applicant: Vincent T. Riggi, Jr. ,  Ronald A. Riggi

    Inventor： Vincent T. Riggi, Jr. ,  Ronald A. Riggi

    IPC: F16J15/16

    CPC classification number: F16J15/3288 ,  F01D11/00 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2250/71 ,  F05D2300/601 ,  F16J15/3284

    Abstract: A leakage seal for use in a gas path between two relatively rotatable members of a gas turbine comprises a foil layer and a cloth layer. The foil layer has two expansive surfaces, a single one of which is covered by the cloth layer. The leakage seal has a proximal end, a distal end, and a generally flat region between the proximal and distal ends. The proximal end is attached to an associated one of the turbine members. The distal end diverges from the generally flat region so as to define a curved hook, along which the cloth portion is wrapped over the foil layer, when the distal end is viewed in cross-section.

    Abstract translation: 用于燃气轮机的两个相对旋转的构件之间的气体路径中的泄漏密封件包括箔层和布层。 箔层具有两个膨胀表面，其中一个被布层覆盖。 泄漏密封件具有近端，远端以及近端和远端之间的大致平坦的区域。 近端附接到相关联的一个涡轮机构件。 远端从大体上平坦的区域分开，以限定弯曲的钩子，当横截面看到远端时，布料部分沿着该部分被卷绕在箔层上。

    Leakage seal for gas path of gas turbine
    148.
    发明申请
    Leakage seal for gas path of gas turbine 有权
    燃气轮机气路泄漏密封

    公开(公告)号：US20070069478A1

    公开(公告)日：2007-03-29

    申请号：US11236243

    申请日：2005-09-27

    Applicant: Vincent Riggi ,  Ronald Riggi

    Inventor： Vincent Riggi ,  Ronald Riggi

    IPC: F16J15/00

    CPC classification number: F16J15/3288 ,  F01D11/00 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2250/71 ,  F05D2300/601 ,  F16J15/3284

    Abstract: A leakage seal for use in a gas path between two relatively rotatable members of a gas turbine comprises a foil layer and a cloth layer. The foil layer has two expansive surfaces, a single one of which is covered by the cloth layer. The leakage seal has a proximal end, a distal end, and a generally flat region between the proximal and distal ends. The proximal end is attached to an associated one of the turbine members. The distal end diverges from the generally flat region so as to define a curved hook, along which the cloth portion is wrapped over the foil layer, when the distal end is viewed in cross-section.

    Abstract translation: 用于燃气轮机的两个相对旋转的构件之间的气体路径中的泄漏密封件包括箔层和布层。 箔层具有两个膨胀表面，其中一个被布层覆盖。 泄漏密封件具有近端，远端以及近端和远端之间的大致平坦的区域。 近端附接到相关联的一个涡轮机构件。 远端从大体上平坦的区域分开，以限定弯曲的钩子，当横截面看到远端时，布料部分沿着该部分被卷绕在箔层上。

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