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    AIRFOIL SHAPE FOR THIRD STAGE COMPRESSOR STATOR VANE
    42.
    发明申请
    AIRFOIL SHAPE FOR THIRD STAGE COMPRESSOR STATOR VANE 审中-公开

    公开(公告)号：US20180094642A1

    公开(公告)日：2018-04-05

    申请号：US15285258

    申请日：2016-10-04

    Applicant: General Electric Company

    Inventor： Moorthi Subramaniyan ,  John David Dyer

    IPC: F04D29/54 ,  F04D29/38 ,  F04D29/32 ,  F02C3/06

    CPC classification number: F04D29/544 ,  F01D5/141 ,  F04D29/324 ,  F05D2250/74 ,  Y02T50/673

    Abstract: A system is provided, including an airfoil. The airfoil includes a first suction portion of a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z of a suction side as set forth in TABLE I to a maximum of three decimal places, wherein the X and Y values of the suction side are coordinate values that couple together to define suction side sections of the first suction portion of the nominal airfoil profile at each Z coordinate value, the suction side sections of the first suction portion of the nominal airfoil profile are coupled together to define the first suction portion, the airfoil includes an airfoil length along a Z axis, the first suction portion comprises a first portion length along the Z axis, the first portion length is less than or equal to the airfoil length, and the Cartesian coordinate values of X, Y, and Z are non-dimensional values convertible to dimensional distances.

    TURBINE BUCKET PLATFORM FOR CONTROLLING INCURSION LOSSES
    46.
    发明申请
    TURBINE BUCKET PLATFORM FOR CONTROLLING INCURSION LOSSES 审中-公开
    用于控制损失的涡轮机底盘平台

    公开(公告)号：US20160258295A1

    公开(公告)日：2016-09-08

    申请号：US14635352

    申请日：2015-03-02

    Applicant: General Electric Company

    Inventor： Moorthi Subramaniyan ,  Rohit Chouhan ,  Prabakaran Modachur Krishnan

    IPC: F01D5/14

    CPC classification number: F01D5/143 ,  F01D5/145 ,  F01D11/001 ,  F05D2220/31 ,  F05D2220/32 ,  F05D2240/24 ,  F05D2240/80 ,  F05D2260/97

    Abstract: Embodiments of the invention relate generally to rotary machines and, more particularly, to the reducing mixing of packing leakage and the main flow of hot gas or steam in gas and steam turbines, respectively. In one embodiment, the invention provides a turbine bucket comprising: a platform portion; an airfoil extending radially outward from the platform portion; and at least one recess extending radially inward into the platform portion, the at least one recess being disposed at an angle relative to a leading edge of the platform portion.

    Abstract translation: 本发明的实施方案一般涉及旋转机器，更具体地，涉及分别在气体和蒸汽涡轮机中的填料泄漏和热气体或蒸汽的主流的减少混合。 在一个实施例中，本发明提供一种涡轮机桶，包括：平台部分; 从平台部分径向向外延伸的翼型件; 以及至少一个向内延伸到所述平台部分内的凹部，所述至少一个凹部相对于所述平台部分的前缘以一定角度设置。

    Exhaust diffuser arrangement for a turbine system and method of redirecting a flow
    48.
    发明授权
    Exhaust diffuser arrangement for a turbine system and method of redirecting a flow 有权
    用于涡轮机系统的排气扩散器布置和重新定向流动的方法

    公开(公告)号：US09388710B2

    公开(公告)日：2016-07-12

    申请号：US13632752

    申请日：2012-10-01

    Applicant: General Electric Company

    Inventor： Sachin Kumar Rai ,  Richa Awasthi ,  Shruti Kulkarni ,  Moorthi Subramaniyan

    IPC: F01D25/30

    CPC classification number: F01D25/30 ,  F05D2240/12

    Abstract: An exhaust diffuser arrangement for a turbine system includes an inlet for receiving a flow proximate a last stage bucket of the turbine system, the flow flowing in a first flow direction. Also included is a flow redirecting component. The flow redirecting component includes a first wall having a first side of a concave surface geometry for redirecting the flow and a second side of a convex surface geometry. The flow redirecting component also includes a second wall spaced downstream of the first wall and having at least one flow exit for reducing a boundary layer along the second side of the first wall.

    Abstract translation: 用于涡轮机系统的排气扩散器装置包括用于接收靠近涡轮机系统的最后级桶的流体的入口，流体沿第一流动方向流动。 还包括流重定向组件。 流动重定向部件包括第一壁，其具有用于重新定向流动的凹面几何形状的第一侧面和凸面几何形状的第二侧面。 流动重定向部件还包括在第一壁的下游间隔开的第二壁，并具有至少一个流出口，用于沿第一壁的第二侧减小边界层。

    FLOW MANIPULATING ARRANGEMENT FOR A TURBINE EXHAUST DIFFUSER
    49.
    发明申请
    FLOW MANIPULATING ARRANGEMENT FOR A TURBINE EXHAUST DIFFUSER 审中-公开
    用于涡轮排气歧管的流量控制装置

    公开(公告)号：US20140314549A1

    公开(公告)日：2014-10-23

    申请号：US13864748

    申请日：2013-04-17

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Srinivas Rao Pakkala ,  Manjunath Bangalore Chengappa ,  Kamlesh Mundra ,  Antanu Sadhu ,  Kunal Upendra Sakekar ,  Moorthi Subramaniyan ,  Lisa Anne Wichmann

    IPC: F01D9/02

    CPC classification number: F01D9/02 ,  F01D5/146 ,  F01D17/162 ,  F01D25/30

    Abstract: A flow manipulating arrangement for a turbine exhaust diffuser includes a strut having a leading edge and a trailing edge, the strut disposed within the turbine exhaust diffuser. Also included is a plurality of rotatable guide vanes disposed in close proximity to the strut and configured to manipulate an exhaust flow, wherein the plurality of rotatable guide vanes is coaxially aligned and circumferentially arranged relative to each other. Further included is an actuator in operative communication with the plurality of rotatable guide vanes and configured to actuate an adjustment of the plurality of rotatable guide vanes. Yet further included is a circumferential ring operatively coupling the plurality of rotatable guide vanes, wherein the actuator is configured to directly actuate rotation of one of the rotatable guide vanes, and wherein the circumferential ring actuates rotation of the plurality of rotatable guide vanes upon rotational actuation by the actuator.

    Abstract translation: 用于涡轮机排气扩散器的流动操纵装置包括具有前缘和后缘的支柱，支柱设置在涡轮排气扩散器内。 还包括多个可旋转导向叶片，其布置成紧邻支柱并且构造成操纵排气流，其中多个可旋转的导向叶片相对于彼此同轴对准并且周向布置。 还包括与多个可旋转导向叶片可操作地连通并被构造成致动多个可旋转导向叶片的调节的致动器。 还包括一个可操作地连接多个可旋转的导向叶片的周向环，其中致动器构造成直接致动可转动导向叶片中的一个的旋转，并且其中周向环在旋转致动时致动多个可旋转导向叶片的旋转 由致动器。

    EXHAUST DIFFUSER
    50.
    发明申请
    EXHAUST DIFFUSER 有权
    排气歧管

    公开(公告)号：US20140096500A1

    公开(公告)日：2014-04-10

    申请号：US13646003

    申请日：2012-10-05

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Manjunath Bangalore Chengappa ,  Moorthi Subramaniyan ,  Vignesh Radhakrishnan

    IPC: F02C7/00 ,  F02C3/04 ,  F01N13/00

    CPC classification number: F01D5/145 ,  F01D25/30 ,  F05D2240/127

    Abstract: An exhaust diffuser includes an outer shroud and an inner shroud radially separated from the outer shroud so as to define a fluid passage between the outer shroud and the inner shroud. A strut extends between the outer shroud and the inner shroud. The strut generally includes an outer surface, a leading edge, a trailing edge, a first side and a second side. At least one turbulator may be positioned along a radial span of the strut. The at least one turbulator extends generally outwardly from the strut outer surface. The turbulator extends across the leading edge of the strut from the first side to the second side of the strut.

    Abstract translation: 排气扩散器包括外护罩和与外护罩径向分离的内护罩，以便在外护罩和内护罩之间限定流体通道。 支柱在外护罩和内护罩之间延伸。 支柱通常包括外表面，前缘，后缘，第一侧和第二侧。 至少一个湍流器可以沿着支柱的径向跨度定位。 至少一个湍流器从支柱外表面大致向外延伸。 湍流器从支柱的前缘延伸穿过支柱的第一侧到第二侧。

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