STEAM TURBINE FACILITY
    231.
    发明申请
    STEAM TURBINE FACILITY 有权
    蒸汽涡轮机设施

    公开(公告)号:US20100202876A1

    公开(公告)日:2010-08-12

    申请号:US12674249

    申请日:2009-07-30

    Abstract: Provided is a steam turbine facility capable of suppressing the possibility of vibration occurrence and a drastic increase in facility cost, thereby realizing an increase in size of the facility, even if steam conditions of 650° C. or higher are adopted. In a steam turbine facility including a high-pressure turbine, an intermediate-pressure turbine, and a low-pressure turbine, the intermediate-pressure turbine is separated into a first intermediate-pressure turbine on a high-temperature and high-pressure side and a second intermediate-pressure turbine on a low-temperature and low-temperature side, at least any one of the rotors and casings of the steam-introduction-side turbines into which steam with a temperature of 650° C. or higher is introduced is formed from Ni-based alloy, and at least any one of the overall rotors and the overall casings of the turbines are constructed by joining together a plurality of rotor members or casing members by welding.

    Abstract translation: 提供一种能够抑制振动发生的可能性和设备成本急剧增加的汽轮机设备,即使采用650℃以上的蒸汽条件,也能够实现设备尺寸的增加。 在包括高压涡轮机,中压涡轮机和低压涡轮机的汽轮机设备中,将中压涡轮分离成高温高压侧的第一中压涡轮机, 在低温低温侧的第二中压涡轮机,导入650℃以上的蒸汽的蒸汽导入侧涡轮机的转子和壳体中的至少一个转子和壳体是 由Ni基合金形成,并且通过焊接将多个转子部件或壳体部件接合在一起而构成涡轮机的整体转子和整体壳体中的至少任一个。

    COMPRESSOR SWASH PLATE AND METHOD OF MANUFACTURING THE SAME
    237.
    发明申请
    COMPRESSOR SWASH PLATE AND METHOD OF MANUFACTURING THE SAME 审中-公开
    压缩机刷板及其制造方法

    公开(公告)号:US20090004030A1

    公开(公告)日:2009-01-01

    申请号:US12104539

    申请日:2008-04-17

    Abstract: The invention provides a compressor swash plate which is lead-free and is able to demonstrate a superior durability. A compressor swash plate in the invention includes a base member and a sliding layer being formed on the surface of the base member and constituting at least a sliding surface for allowing a shoe to slide thereon. The sliding layer is formed by thermal spraying Cu-based-MnS by HVOF thermal spraying method. A method of manufacturing the compressor swash plate according to the invention includes a step of thermal spraying powder formed of Cu-based-MnS onto the base member by the HVOF thermal spraying method to form the sliding layer which constitutes at least the sliding surface which allows the shoe to slide thereon on the base member. More specifically, the Cu-based-MnS is Cu-Ni-MnS.

    Abstract translation: 本发明提供一种无铅的压缩机斜盘,能够表现出优异的耐久性。 本发明的压缩机斜盘包括底座件和滑动层,该底座件和滑动层形成在基座件的表面上并至少构成一滑动表面以允许鞋子在其上滑动。 滑动层通过HVOF热喷涂法热喷涂Cu基MnS而形成。 根据本发明的制造压缩机旋转斜盘的方法包括通过HVOF热喷涂法将Cu基MnS形成的粉末热喷涂到基底构件上,以形成至少构成滑动面的滑动层,该滑动层允许 该鞋在基部件上滑动。 更具体地说,Cu系MnS是Cu-Ni-MnS。

    SEALS, SEALED SYSTEMS, AND METHODS FOR SEALING A SHAFT
    238.
    发明申请
    SEALS, SEALED SYSTEMS, AND METHODS FOR SEALING A SHAFT 有权
    密封,密封系统和密封垫片的方法

    公开(公告)号:US20080267767A1

    公开(公告)日:2008-10-30

    申请号:US11742163

    申请日:2007-04-30

    CPC classification number: F01D11/003 F01D25/183 F05C2201/0466 F16J15/0887

    Abstract: In one embodiment, and by way of example only, a seal is provided for sealing a hollow shaft, where the hollow shaft has an inner surface that may be uneven due to shot peening. The seal includes an axially extending ring section having a first end, a second end, an inner surface, and a disk section disposed substantially perpendicular to the ring section inner surface between the ring section first and second ends. The seal conforms to the shaft inner surface to stop oil leakage.

    Abstract translation: 在一个实施例中,仅作为示例,提供用于密封空心轴的密封件,其中空心轴具有由于喷丸硬化而可能不均匀的内表面。 密封件包括轴向延伸的环形部分,其具有第一端,第二端,内表面和与环部分第一端和第二端之间的环部分内表面基本垂直的基板。 密封件符合轴内表面,以防止漏油。

    Dual process nickel alloy crack repair
    240.
    发明申请
    Dual process nickel alloy crack repair 有权
    双工艺镍合金裂纹修复

    公开(公告)号:US20080230156A1

    公开(公告)日:2008-09-25

    申请号:US11638050

    申请日:2007-03-22

    Abstract: A process for repairing cracks in a workpiece, such as a turbine engine component, comprises the steps of: providing a workpiece having a crack to be repaired; applying a nickel or cobalt base alloy material to a root of the crack in an amount sufficient to fill a portion of the crack; subjecting the workpiece with the nickel or cobalt base alloy material to a first heat treatment at a temperature in the range of from about 1950 to 2300° F. for a time period in the range of from about 5.0 to 30 minutes; applying a weld material to the crack; and subjecting the workpiece with the weld material to a second heat treatment.

    Abstract translation: 一种用于修复诸如涡轮发动机部件的工件中的裂纹的方法包括以下步骤:提供具有待修复的裂纹的工件; 将镍或钴基合金材料以足以填充裂纹的一部分的量施加到裂纹的根部; 使工件与镍或钴基合金材料在约1950至2300°F范围内的温度下进行第一次热处理,时间范围为约5.0至30分钟; 对裂缝施加焊接材料; 并且对焊接材料进行第二次热处理。

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