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    Blade neck fluid seal
    11.
    发明申请
    Blade neck fluid seal 审中-公开
    刀颈液密封

    公开(公告)号：US20060275106A1

    公开(公告)日：2006-12-07

    申请号：US11146660

    申请日：2005-06-07

    Applicant: Ioannis Alvanos ,  Rajendra Agrawal

    Inventor： Ioannis Alvanos ,  Rajendra Agrawal

    IPC: F03B11/00

    CPC classification number: F01D5/3007 ,  F01D5/082 ,  F01D11/001 ,  F01D11/02

    Abstract: Disclosed are assemblies and articles for restricting leakage of a pressurized fluid from a cavity. In accordance with an embodiment of the invention, a vane support defines a land, and a neck region of a bladed rotor assembly defines a segmented ring. The segmented ring protrudes outward from the bladed rotor assembly in the neck region, spans across the cavity and cooperates with the land to define a seal.

    Abstract translation: 公开了用于限制加压流体从空腔泄漏的组件和制品。 根据本发明的实施例，叶片支撑件限定平台，并且叶片转子组件的颈部区域限定分段环。 分段环从颈部区域中的叶片式转子组件向外突出，跨越空腔并与凸台配合以限定密封。

    TEC mount redundant fastening
    13.
    发明授权
    TEC mount redundant fastening 有权
    TEC安装冗余紧固

    公开(公告)号：US09091210B2

    公开(公告)日：2015-07-28

    申请号：US13456436

    申请日：2012-04-26

    Applicant: Gabriel L. Suciu ,  Ioannis Alvanos

    Inventor： Gabriel L. Suciu ,  Ioannis Alvanos

    IPC: F01D25/28 ,  F02C7/20 ,  B64D27/26

    CPC classification number: F02C7/20 ,  B64D27/26 ,  B64D2027/264

    Abstract: A mounting apparatus for a turbine exhaust case (TEC) is provided. The mounting apparatus may include a neck, support links and a plurality of fastening pins. The neck may include an upper portion that is receivable within a pylon associated with the TEC and at least one neck aperture extending therethrough. The support links may downwardly extend from a lower portion of the neck. The support links may be configured to at least partially receive a section of the TEC. Each support link may include at least one link aperture extending therethrough. The fastening pins may include at least one neck pin extending through the neck aperture and at least one link pin extending through the link aperture of each support link.

    Abstract translation: 提供了一种用于涡轮机排气箱（TEC）的安装装置。 安装设备可以包括颈部，支撑连杆和多个紧固销。 颈部可以包括可接收在与TEC相关联的挂架内的上部和延伸穿过其的至少一个颈孔。 支撑连杆可以从颈部的下部向下延伸。 支持链路可以被配置为至少部分地接收TEC的一部分。 每个支撑连杆可以包括延伸穿过其中的至少一个连杆孔。 紧固销可以包括延伸穿过颈部孔的至少一个颈销和延伸穿过每个支撑连杆的连杆孔的至少一个连杆销。

    TURBINE ENGINE CASE MOUNT AND DISMOUNT
    15.
    发明申请
    TURBINE ENGINE CASE MOUNT AND DISMOUNT 审中-公开
    涡轮发动机壳体安装和配置

    公开(公告)号：US20130232768A1

    公开(公告)日：2013-09-12

    申请号：US13417615

    申请日：2012-03-12

    Applicant: Gabriel L. Suciu ,  Ioannis Alvanos ,  Brian D. Merry

    Inventor： Gabriel L. Suciu ,  Ioannis Alvanos ,  Brian D. Merry

    IPC: B23P17/04

    CPC classification number: F02C7/20 ,  B64D27/10 ,  B64D27/26 ,  B64D2027/262 ,  B64D2027/266 ,  F05D2220/323 ,  F05D2230/60 ,  F05D2240/90 ,  Y02T50/44 ,  Y10T29/49947

    Abstract: A method for mounting a gas turbine engine having a compressor section, a combustor section, a turbine section, a pylon and a rear mount bracket, includes positioning the mounting bracket between the gas turbine engine and the pylon. The mounting bracket is connected to the turbine case reacting a least a vertical load, a side load, a thrust load, and a torque load from the gas turbine engine through the mounting bracket. The mounting bracket is attached to the pylon reacting the same loads from the gas turbine engine.

    Abstract translation: 一种用于安装具有压缩机部分，燃烧器部分，涡轮机部分，塔架和后部安装支架的燃气涡轮发动机的方法，包括将安装支架定位在燃气涡轮发动机和塔架之间。 安装支架连接到涡轮机壳体，使至少垂直载荷，侧向载荷，推力载荷和来自燃气涡轮发动机的转矩载荷通过安装支架反应。 安装支架连接到塔架，使来自燃气涡轮发动机的相同负载反应。

    TURBOMACHINERY SEAL
    16.
    发明申请
    TURBOMACHINERY SEAL 有权
    TURBOMACHINERY密封

    公开(公告)号：US20130119617A1

    公开(公告)日：2013-05-16

    申请号：US13294787

    申请日：2011-11-11

    Applicant: Ioannis Alvanos ,  Gabriel L. Suciu

    Inventor： Ioannis Alvanos ,  Gabriel L. Suciu

    IPC: F16J15/02

    CPC classification number: F01D11/001 ,  F01D11/122 ,  F01D11/127 ,  F05D2230/64 ,  F05D2250/184 ,  F05D2260/38

    Abstract: A seal for sealing a rotor of a rotary machine to a stator thereof which circumscribes the rotor and is separated therefrom by a gap comprises a nonrotational sealing element received within an annular slot in the stator and radially translatable with respect thereto, and extending into the gap for sealing to rotational sealing element carried by the rotor. A resilient biasing element received between the nonrotational sealing element and a floor of the slot biases the nonrotational sealing element radially inwardly toward the rotational sealing element and limits radially outward movement of the nonrotational sealing element. A guide extending into said gap from the slot engages the nonrotational sealing element to prevent axial misalignment thereof with the machine's rotor.

    Abstract translation: 用于将旋转机械的转子密封到其定子上的用于将转子环绕并通过间隙分离的密封件包括：非旋转密封元件，其接收在定子的环形槽内并且可相对于其径向平移并延伸到间隙 用于密封转子承载的旋转密封元件。 容纳在非旋转密封元件和狭槽的底板之间的弹性偏置元件将非旋转密封元件径向向内朝向旋转密封元件偏压并且限制非旋转密封元件的径向向外移动。 从狭槽延伸到所述间隙中的引导件接合非旋转密封元件以防止其与机器转子的轴向不对准。

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