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    Turbine blade with tip shroud cooling passage
    21.
    发明授权
    Turbine blade with tip shroud cooling passage 有权

    公开(公告)号：US11225872B2

    公开(公告)日：2022-01-18

    申请号：US16674059

    申请日：2019-11-05

    Applicant: General Electric Company

    Inventor： Melbourne James Myers ,  Michael Anthony Wondrasek ,  Mary Virginia Holloway ,  Luke C. Sponseller ,  Brandon Joseph Kerins

    IPC: F01D5/18

    Abstract: A turbine blade includes a root for fixing the turbine blade to a turbine rotor; and an airfoil coupled to the root, the airfoil including a suction side and a pressure side, and at least one internal wall defining a coolant chamber in the airfoil for delivering a coolant through the airfoil. A tip shroud is coupled to a radially outer end of the airfoil by a suction side fillet and a pressure side fillet. The tip shroud includes a shroud body defining a substantially trident-shaped shroud cooling passage including: a trunk cooling passage, a center cooling passage in fluid communication with the trunk cooling passage, a suction side cooling passage in fluid communication with the trunk cooling passage, and a pressure side cooling passage in fluid communication with the trunk cooling passage. The center cooling passage is fluidly coupled to the coolant chamber to receive a coolant.

    Tip shroud fillets for turbine rotor blades
    22.
    发明授权
    Tip shroud fillets for turbine rotor blades 有权

    公开(公告)号：US10704392B2

    公开(公告)日：2020-07-07

    申请号：US15933568

    申请日：2018-03-23

    Applicant: General Electric Company

    Inventor： William Scott Zemitis ,  Melbourne James Myers ,  Richard Ryan Pilson ,  Jacob Charles Perry, II

    IPC: F01D5/14 ,  F01D5/22

    Abstract: A turbine rotor blade including an airfoil, tip shroud, and fillet formed therebetween. The fillet defines a fillet profile variable about the intersection for connecting the tip shroud and airfoil and facilitating aerodynamic airflow. The fillet includes a pressure side fillet. The pressure side fillet comprises a pressure side fillet profile per points within a first set of points of X, Y and Z coordinate values in a Cartesian coordinate system, as set forth in Table I, where X, Y and Z are distances in inches from an origin and, when the points are connected by smooth, continuing arcs, the points define the pressure side fillet profile of the pressure side fillet. The first set of points includes points between and including point 1 and point 50 of each reference plane between and including a reference plane H and a reference plane W, as set forth in Table I.

    TIP SHROUD FILLETS FOR TURBINE ROTOR BLADES
    24.
    发明申请
    TIP SHROUD FILLETS FOR TURBINE ROTOR BLADES 审中-公开

    公开(公告)号：US20190292913A1

    公开(公告)日：2019-09-26

    申请号：US15933568

    申请日：2018-03-23

    Applicant: General Electric Company

    Inventor： William Scott Zemitis ,  Melbourne James Myers ,  Richard Ryan Pilson ,  Jacob Charles Perry, II

    IPC: F01D5/14 ,  F01D5/22

    Abstract: A turbine rotor blade including an airfoil, tip shroud, and fillet formed therebetween. The fillet defines a fillet profile variable about the intersection for connecting the tip shroud and airfoil and facilitating aerodynamic airflow. The fillet includes a pressure side fillet. The pressure side fillet comprises a pressure side fillet profile per points within a first set of points of X, Y and Z coordinate values in a Cartesian coordinate system, as set forth in Table I, where X, Y and Z are distances in inches from an origin and, when the points are connected by smooth, continuing arcs, the points define the pressure side fillet profile of the pressure side fillet. The first set of points includes points between and including point 1 and point 50 of each reference plane between and including a reference plane H and a reference plane W, as set forth in Table I.

    METHOD FOR MODIFYING A AIRFOIL SHROUD AND AIRFOIL
    28.
    发明申请
    METHOD FOR MODIFYING A AIRFOIL SHROUD AND AIRFOIL 审中-公开
    用于修改空气动力飞溅和飞行器的方法

    公开(公告)号：US20140147283A1

    公开(公告)日：2014-05-29

    申请号：US13685950

    申请日：2012-11-27

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： John David Ward, Jr. ,  Kelvin Rono Aaron ,  James Ryan Connor ,  Melbourne James Myers ,  Brad Wilson VanTassel

    IPC: F01D5/00 ,  F01D5/22

    CPC classification number: F01D5/005 ,  F01D5/225 ,  F05D2230/80 ,  F05D2240/307 ,  F05D2260/94 ,  F05D2260/941 ,  F05D2270/332 ,  Y10T29/49234 ,  Y10T83/04

    Abstract: According to one aspect of the invention, a method is provided for modifying an airfoil shroud located at a tip of an airfoil of a airfoil, the airfoil shroud having a first end edge, a second end edge, a leading edge and a trailing edge. The method includes locating a reference location in the first end edge of the airfoil shroud, the reference location being proximate a seal rail extending circumferentially from the substantially horizontal surface and forming a relief cut in the airfoil shroud to remove the reference location, wherein a modifying of the airfoil shroud is complete following forming of the relief cut.

    Abstract translation: 根据本发明的一个方面，提供了一种用于修改位于翼型的翼型的尖端处的翼型护罩的方法，所述翼型护罩具有第一端边缘，第二端边缘，前缘和后缘。 该方法包括将参考位置定位在翼型护罩的第一端边缘中，参考位置靠近从基本水平的表面周向延伸的密封轨道，并在翼型护罩中形成浮雕切口以移除参考位置，其中修改 的翼型护罩在形成浮雕切割后完成。

    Rotor blade sealing structures
    29.
    发明授权
    Rotor blade sealing structures 有权

    公开(公告)号：US11566528B2

    公开(公告)日：2023-01-31

    申请号：US16722020

    申请日：2019-12-20

    Applicant: General Electric Company

    Inventor： Martin James Jasper ,  Claire Katherine Naioti ,  Melbourne James Myers ,  William Scott Zemitis ,  Stephen Douglas Shearer

    IPC: F01D11/00 ,  F01D5/22 ,  F01D5/02

    Abstract: A rotor blade is provided. The rotor blade includes a main body having a shank, an airfoil extends radially outwardly from the shank, and a platform. The main body includes a pressure side slash face and a suction side slash face. A slot is defined within each of the pressure side slash face and the suction side slash face. The slot of the pressure side slash face and the slot of the suction side slash face each include an upstream end portion that defines an end and a main body portion extending from the upstream end portion. The upstream end portion tapers from the end to the main body portion. The main body portion further includes a retention wall that covers a portion of the end and that defines an opening. The retention wall further includes an inner retention surface. The retention wall defines an offset from the opening.

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