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    Combustor with Fuel Nozzle Liner Having Chevron Ribs
    1.
    发明申请
    Combustor with Fuel Nozzle Liner Having Chevron Ribs 审中-公开
    燃油喷嘴具有雪佛龙肋骨的燃烧器

    公开(公告)号：US20120240592A1

    公开(公告)日：2012-09-27

    申请号：US13069424

    申请日：2011-03-23

    申请人： Mayur Abhay Keny ,  Ronald Chila ,  Vaibhav Nadkarni

    发明人： Mayur Abhay Keny ,  Ronald Chila ,  Vaibhav Nadkarni

    IPC分类号： F02C7/22

    CPC分类号： F23R3/286 ,  F23D11/408

    摘要： The present application and the resultant patent provide a fuel nozzle for mixing a flow of air and a flow of fuel within a combustor. The fuel nozzle may have one or more air passages for the flow of air, one or more fuel pegs for the flow of fuel, and a liner in communication with the air passages and surrounding the fuel pegs. The liner may include a number of ribs thereon so as to promote mixing of the flow of air and the flow of fuel therein.

    摘要翻译： 本申请和所得专利提供了用于混合燃烧器内的空气流和燃料流的燃料喷嘴。 燃料喷嘴可以具有用于空气流动的一个或多个空气通道，用于燃料流的一个或多个燃料栓，以及与空气通道连通并围绕燃料栓的衬垫。 衬垫可以包括多个肋，以便促进空气流与其中的燃料流的混合。

    TURBINE CONDUIT SLEEVE SYSTEM
    2.
    发明申请
    TURBINE CONDUIT SLEEVE SYSTEM 有权
    TURBINE CONDITION SLEEVE系统

    公开(公告)号：US20140044533A1

    公开(公告)日：2014-02-13

    申请号：US13569648

    申请日：2012-08-08

    申请人： Mayur Abhay Keny ,  Josef Scott Cummins ,  Scott Jacob Huth ,  Thangaraj Subbareddyar

    发明人： Mayur Abhay Keny ,  Josef Scott Cummins ,  Scott Jacob Huth ,  Thangaraj Subbareddyar

    IPC分类号： F01D25/24

    CPC分类号： F01D25/243 ,  Y02E20/16

    摘要： Systems and devices configured to shield portions of turbine conduits from contact with a working fluid flow and reduce the associated thermal gradients therein are disclosed. In one embodiment, a sleeve includes: a base portion defining a shield aperture, the base portion including an external surface configured to contact an internal surface of a turbine conduit; and a neck portion connected to the base portion and defining a neck aperture proximate a terminus of the turbine conduit, the neck aperture fluidly connected to the shield aperture.

    摘要翻译： 公开了被配置为屏蔽涡轮管道部分的系统和装置与工作流体流的接触并减少其中相关的热梯度。 在一个实施例中，套筒包括：限定屏蔽孔的基部，所述基部包括构造成接触涡轮导管的内表面的外表面; 以及颈部，其连接到所述基部并且在所述涡轮导管的末端附近限定颈部孔，所述颈部孔与所述屏蔽孔流体连接。

    EXHAUST STRUT AND TURBOMACHINE INCORPRATING SAME
    5.
    发明申请
    EXHAUST STRUT AND TURBOMACHINE INCORPRATING SAME 审中-公开
    排气管和涡轮发动机同时进行

    公开(公告)号：US20130167552A1

    公开(公告)日：2013-07-04

    申请号：US13343115

    申请日：2012-01-04

    申请人： Mayur Abhay Keny ,  Thangaraj Subbareddyar ,  Hariharan Sundaram

    发明人： Mayur Abhay Keny ,  Thangaraj Subbareddyar ,  Hariharan Sundaram

    IPC分类号： F02C7/20

    CPC分类号： F01D5/148 ,  F01D5/28 ,  F05D2300/505

    摘要： An exhaust strut is provided and includes a body having an airfoil-shaped cross-section defining a lead edge portion and a trailing edge portion opposite the lead edge portion, the lead edge portion and the trailing edge portion being connected by a pressure side and a suction side opposite the pressure side, at least the lead edge portion and respective sections of the pressure side and the suction side proximate to the lead edge portion being formed of shape memory alloy, and a temperature control system operably disposed at the lead edge portion and the respective sections of the pressure side and the suction side proximate to the lead edge portion to modify a temperature of the shape memory alloy.

    摘要翻译： 提供排气支柱，并且包括具有限定引线边缘部分的翼型横截面的主体和与引线边缘部分相对的后缘部分，引线边缘部分和后缘部分通过压力侧和 吸入侧与压力侧相对，至少前缘部分和靠近引线边缘部分的压力侧和吸力侧的各个部分由形状记忆合金形成，并且温度控制系统可操作地设置在引导边缘部分处， 靠近引线边缘部分的压力侧和吸力侧的各个部分，以改变形状记忆合金的温度。

    TURBULATED ARRANGEMENT OF THERMOELECTRIC ELEMENTS FOR UTILIZING WASTE HEAT GENERATED FROM TURBINE ENGINE
    6.
    发明申请
    TURBULATED ARRANGEMENT OF THERMOELECTRIC ELEMENTS FOR UTILIZING WASTE HEAT GENERATED FROM TURBINE ENGINE 失效
    用于利用涡轮发动机产生的废热的热电元件的涡轮机布置

    公开(公告)号：US20120031067A1

    公开(公告)日：2012-02-09

    申请号：US12849517

    申请日：2010-08-03

    申请人： Hariharan Sundaram ,  Mayur Abhay Keny ,  Kathleen Blanche Morey

    发明人： Hariharan Sundaram ,  Mayur Abhay Keny ,  Kathleen Blanche Morey

    IPC分类号： F02C3/00 ,  H01L35/02

    CPC分类号： F02C6/18 ,  F01D25/30 ,  F02C3/00 ,  F05D2220/60 ,  F05D2240/127 ,  H01L35/30

    摘要： Disclosed is a turbulated arrangement of thermoelectric elements for utilizing waste heat generated from a turbine engine. The turbulated arrangement of thermoelectric elements is located within the turbine casing at a heat exhaust end of the turbine engine. The turbulated arrangement of thermoelectric elements convert heat exhaust generated from the turbine engine into electrical energy. In one embodiment, the electrical energy generated from the turbulated arrangement of thermoelectric elements can be used to power electrical components located about the turbine engine.

    摘要翻译： 公开了一种用于利用从涡轮发动机产生的废热的热电元件的混合布置。 热电元件的混浊布置位于涡轮机外壳内，在涡轮发动机的排热端。 热电元件的混合布置将从涡轮发动机产生的热排放转换为电能。 在一个实施例中，从热电元件的混沌布置产生的电能可用于为位于涡轮发动机周围的电气部件供电。

    Turbine conduit sleeve system
    9.
    发明授权
    Turbine conduit sleeve system 有权
    涡轮管套管系统

    公开(公告)号：US09194257B2

    公开(公告)日：2015-11-24

    申请号：US13569648

    申请日：2012-08-08

    申请人： Mayur Abhay Keny ,  Josef Scott Cummins ,  Scott Jacob Huth ,  Thangaraj Subbareddyar

    发明人： Mayur Abhay Keny ,  Josef Scott Cummins ,  Scott Jacob Huth ,  Thangaraj Subbareddyar

    IPC分类号： F01D25/24

    CPC分类号： F01D25/243 ,  Y02E20/16

    摘要： Systems and devices configured to shield portions of turbine conduits from contact with a working fluid flow and reduce the associated thermal gradients therein are disclosed. In one embodiment, a sleeve includes: a base portion defining a shield aperture, the base portion including an external surface configured to contact an internal surface of a turbine conduit; and a neck portion connected to the base portion and defining a neck aperture proximate a terminus of the turbine conduit, the neck aperture fluidly connected to the shield aperture.

    摘要翻译： 公开了被配置为屏蔽涡轮管道部分的系统和装置与工作流体流的接触并减少其中相关的热梯度。 在一个实施例中，套筒包括：限定屏蔽孔的基部，所述基部包括构造成接触涡轮导管的内表面的外表面; 以及颈部，其连接到所述基部并且在所述涡轮导管的末端附近限定颈部孔，所述颈部孔与所述屏蔽孔流体连接。

    Turbine assembly
    10.
    发明授权
    Turbine assembly 有权
    涡轮总成

    公开(公告)号：US09068465B2

    公开(公告)日：2015-06-30

    申请号：US13459931

    申请日：2012-04-30

    申请人： Mayur Abhay Keny ,  Fernando Jorge Casanova ,  Prathap Raj Rajendran

    发明人： Mayur Abhay Keny ,  Fernando Jorge Casanova ,  Prathap Raj Rajendran

    IPC分类号： F01D5/30 ,  F01D5/32

    CPC分类号： F01D5/3038 ,  F01D5/32

    摘要： According to one aspect of the invention, a turbine assembly includes a rotor wheel and a circumferential slot formed in the rotor wheel, the circumferential slot including a uniform cross-section shape for a circumference of the rotor wheel. The assembly also includes a first ring member positioned in the circumferential slot, the first ring member being configured to prevent radial movement of a dovetail attachment when positioned in the circumferential slot, wherein the dovetail attachment is part of a turbine blade.

    摘要翻译： 根据本发明的一个方面，涡轮组件包括转子轮和形成在转子轮中的周向槽，该周向槽包括用于转子轮的圆周的均匀横截面形状。 组件还包括定位在圆周槽中的第一环构件，第一环构件构造成防止燕尾座附件定位在周向槽中时的径向运动，其中燕尾座附件是涡轮叶片的一部分。