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    Moving blade for a turbomachine and turbomachine
    161.
    发明授权
    Moving blade for a turbomachine and turbomachine 失效
    用于涡轮机和涡轮机的移动叶片

    公开(公告)号：US06827556B2

    公开(公告)日：2004-12-07

    申请号：US10379987

    申请日：2003-03-05

    Applicant: Volker Simon

    Inventor： Volker Simon

    IPC: F01D528

    CPC classification number: F01D5/147 ,  B22F2998/00 ,  F01D5/28 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2260/203 ,  F05D2300/612 ,  B22F7/006

    Abstract: A novel blade configuration does not exceed the permitted stresses for particular loads, especially as a result of centrifugal forces and which at the same time, allows the turbomachine to function with a high degree of efficiency. To this end, a moving blade for the turbomachine contains at least partially a cellular material, especially a foamed metal. The cellular material can be provided e.g. in the hollowed-out part of the moving blade.

    Abstract translation: 新颖的叶片结构不会超过特定载荷的允许应力，特别是由于离心力而同时允许涡轮机以高效率起作用。 为此，用于涡轮机的移动叶片至少部分地包含多孔材料，特别是泡沫金属。 细胞材料可以例如提供。 在动叶片的中空部分。

    Lubricating system for thermal medium delivery parts in a gas turbine
    165.
    发明申请
    Lubricating system for thermal medium delivery parts in a gas turbine 失效
    燃气轮机中热介质输送部件的润滑系统

    公开(公告)号：US20010022934A1

    公开(公告)日：2001-09-20

    申请号：US09769749

    申请日：2001-01-26

    Inventor： Thomas Charles Mashey

    IPC: F01D005/08 ,  F01D005/14

    CPC classification number: C23C28/321 ,  C23C28/34 ,  C23C28/347 ,  F01D5/084 ,  F01D9/06 ,  F01D25/18 ,  F05C2201/0463 ,  F05D2230/90 ,  F05D2300/21 ,  F05D2300/509 ,  F05D2300/611 ,  F16L58/08 ,  F16L58/14

    Abstract: Cooling steam delivery tubes extend axially along the outer rim of a gas turbine rotor for supplying cooling steam to and returning spent cooling steam from the turbine buckets. Because of the high friction forces at the interface of the tubes and supporting elements due to rotor rotation, a low coefficient of friction coating is provided at the interface of the tubes and support elements. On each surface, a first coating of a cobalt-based alloy is sprayed onto the surface at high temperature. A portion of the first coating is machined off to provide a smooth, hard surface. A second ceramic-based solid film lubricant is sprayed onto the first coating. By reducing the resistance to axial displacement of the tubes relative to the supporting elements due to thermal expansion, the service life of the tubes is substantially extended.

    Abstract translation: 冷却蒸汽输送管沿着燃气涡轮机转子的外缘轴向延伸，用于将冷却蒸汽供给并从涡轮机叶返回废冷却蒸汽。 由于由于转子旋转而在管和支撑元件的界面处的高摩擦力，所以在管和支撑元件的界面处提供了低摩擦系数涂层。 在每个表面上，钴基合金的第一涂层在高温下喷涂到表面上。 第一涂层的一部分被加工以提供光滑的硬表面。 将第二陶瓷基固体膜润滑剂喷涂到第一涂层上。 通过由于热膨胀减小管相对于支撑元件的轴向位移的阻力，管的使用寿命显着延长。

    Method of forming high-temperature components and components formed thereby
    166.
    发明授权
    Method of forming high-temperature components and components formed thereby 失效
    形成高温部件和由此形成的部件的方法

    公开(公告)号：US5960249A

    公开(公告)日：1999-09-28

    申请号：US35802

    申请日：1998-03-06

    Applicant: Ann Melinda Ritter ,  Paul Leonard Dupree ,  Melvin Robert Jackson ,  Donald Norman Wemple, Jr.

    Inventor： Ann Melinda Ritter ,  Paul Leonard Dupree ,  Melvin Robert Jackson ,  Donald Norman Wemple, Jr.

    IPC: B22F3/12 ,  B22F5/04 ,  B22F7/06 ,  B23P15/04 ,  F01D5/18 ,  F01D5/28 ,  G22B7/00

    CPC classification number: F01D5/18 ,  B22F3/1208 ,  B22F5/04 ,  B22F7/062 ,  B23P15/04 ,  F01D5/28 ,  F01D5/282 ,  B22F2998/00 ,  B22F2998/10 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2230/20 ,  F05D2230/22 ,  F05D2300/603 ,  Y10T428/12028

    Abstract: A method for forming an exterior surface of a high-temperature component, such as a blade or vane of a gas turbine engine. The method entails forming a shell by a powder metallurgy technique that yields an airfoil whose composition can be readily tailored for the particular service conditions of the component. The method generally entails providing a pair of inner and outer mold members that form a cavity therebetween. One or more powders and any desired reinforcement material are then placed in the cavity and then consolidated at an elevated temperature and pressure in a non-oxidizing atmosphere. Thereafter, at least the outer mold member is removed to expose the consolidated powder structure. By appropriately shaping the mold members to tailor the shape of the cavity, the consolidated powder structure has the desired shape for the exterior shell of a component, such that subsequent processing of the component does not require substantially altering the configuration of the exterior shell. The airfoil can be produced as a free-standing article or produced directly on a mandrel that subsequently forms the interior structure of the component. In one embodiment, an airfoil is configured to have double walls through which cooling air flows.

    Abstract translation: 一种用于形成诸如燃气轮机的叶片或叶片的高温部件的外表面的方法。 该方法需要通过粉末冶金技术形成壳体，该技术产生的翼型件的组合可以容易地根据部件的特定使用条件进行定制。 该方法通常需要提供一对在其间形成空腔的内部和外部模具构件。 然后将一种或多种粉末和任何所需的增强材料置于空腔中，然后在非氧化性气氛中在升高的温度和压力下固化。 此后，至少移除外模构件以暴露固结的粉末结构。 通过适当地成型模具以适应空腔的形状，固结的粉末结构具有用于组件的外壳的期望的形状，使得组件的后续处理不需要基本上改变外壳的构造。 翼型件可以作为独立制品生产，或直接制造在随后形成部件的内部结构的心轴上。 在一个实施例中，翼型构造成具有双壁，冷却空气流过该壁。

    葉片屈從填隙片
    169.
    发明专利
    葉片屈從填隙片 失效
    叶片屈从填隙片

    公开(公告)号：TW567276B

    公开(公告)日：2003-12-21

    申请号：TW090125538

    申请日：2001-10-16

    Applicant: 哈尼威爾國際公司

    Inventor： 麥克 柯洛里傑 ,  布魯斯D 威爾森

    IPC: F01D

    CPC classification number: F01D5/28 ,  F01D5/3092 ,  F05C2201/0463 ,  F05D2230/90 ,  F05D2250/71 ,  F05D2260/30 ,  F05D2300/611

    Abstract: 一種屈從填隙片，供在一燃氣輪機轉子圓盤，在一燃氣輪機風扇葉片之根部與一鳩尾槽之間使用，以減低其間之磨損。屈從填隙片有第一及第二切口，供貼合自風扇葉片根部延伸之凸片。切口及凸片合作，以在引擎操作時固持填隙片。一氧化作用層覆蓋屈從填隙片。

    Abstract in simplified Chinese: 一种屈从填隙片，供在一燃气轮机转子圆盘，在一燃气轮机风扇叶片之根部与一鸠尾槽之间使用，以减低其间之磨损。屈从填隙片有第一及第二切口，供贴合自风扇叶片根部延伸之凸片。切口及凸片合作，以在发动机操作时固持填隙片。一氧化作用层覆盖屈从填隙片。

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