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    Gas turbine power augmentation system
    2.
    发明授权
    Gas turbine power augmentation system 有权
    燃气轮机增压系统

    公开(公告)号：US09470150B2

    公开(公告)日：2016-10-18

    申请号：US13873267

    申请日：2013-04-30

    Applicant: General Electric Company

    Inventor： Jianmin Zhang ,  Tailai Hu ,  Bradly Aaron Kippel

    IPC: F02C7/143 ,  F02C7/047 ,  F02C7/08

    CPC classification number: F02C7/143 ,  F02C7/047 ,  F02C7/08

    Abstract: The present application provides a power augmentation system for use with a gas turbine engine. The power augmentation system may include a compressor discharge manifold, an inlet bleed heat system in communication with the compressor discharge manifold via an inlet bleed heat line, and an auxiliary compressor in communication with the compressor discharge manifold via the inlet bleed heat line.

    Abstract translation: 本申请提供了与燃气涡轮发动机一起使用的功率增加系统。 功率增加系统可以包括压缩机排放歧管，通过入口放气热管线与压缩机排放歧管连通的入口放气加热系统，以及经由入口放气加热管路与压缩机排放歧管连通的辅助压缩机。

    Silencing and cooling assembly with fibrous medium
    3.
    发明授权
    Silencing and cooling assembly with fibrous medium 有权
    具有纤维介质的沉默和冷却组件

    公开(公告)号：US09359914B2

    公开(公告)日：2016-06-07

    申请号：US14462845

    申请日：2014-08-19

    Applicant: General Electric Company

    Inventor： Hua Zhang ,  Valery Ivanovich Ponyavin ,  Joshua Shane Sater ,  Jianmin Zhang

    IPC: F02K1/38 ,  F01K7/16 ,  F01D25/12

    CPC classification number: F01K7/16 ,  F01D25/12 ,  F01K23/10 ,  F01K23/14 ,  F02C6/18 ,  F02C7/045 ,  F02C7/143 ,  F05D2250/61 ,  F05D2300/614 ,  Y02E20/16

    Abstract: Embodiments of the present disclosure provide an assembly including a fibrous medium having a plurality of substantially corrugated channels therein, the plurality of substantially corrugated channels being permeable to a flow of fluid therethrough; a distributor in contact with the fibrous medium, and including an aperture therein for transmitting a liquid coolant through the distributor; and at least two acoustic shields coupled to the fibrous medium and proximal to opposing sides of the distributor.

    Abstract translation: 本公开的实施例提供了一种组件，其包括其中具有多个基本波纹通道的纤维介质，所述多个基本上波纹的通道可透过其中的流体流动; 与所述纤维介质接触的分配器，并且在其中包括用于通过所述分配器传输液体冷却剂的孔; 以及耦合到纤维介质并且靠近分配器的相对侧的至少两个声屏蔽。

    Media Pads with Mist Elimination Features
    5.
    发明申请
    Media Pads with Mist Elimination Features 有权
    具有防雾功能的介质垫

    公开(公告)号：US20160108816A1

    公开(公告)日：2016-04-21

    申请号：US14516663

    申请日：2014-10-17

    Applicant: General Electric Company

    Inventor： Jianmin Zhang ,  Bradly Aaron Kippel

    IPC: F02C7/18

    CPC classification number: F02C7/185 ,  B01D45/08 ,  C04B35/565 ,  C04B38/0006 ,  C04B41/009 ,  F01M13/04 ,  F02C7/057

    Abstract: The present application provides a media pad for cooling an inlet air flow to a compressor of a gas turbine engine. The media pad may include a first media sheet with a chevron corrugated surface having a first mist eliminator and a second media sheet with a wavy corrugated surface having a second mist eliminator.

    Abstract translation: 本申请提供了一种用于冷却到燃气涡轮发动机的压缩机的入口空气流的介质垫。 介质垫可以包括具有V形波纹表面的第一介质片，其具有第一除雾器和具有波浪形波纹表面的第二介质片，该第二介质片具有第二除雾器。

    GAS TURBINE INLET HAVING INTEGRATED COILS AND MIST REDUCING VANES
    6.
    发明申请
    GAS TURBINE INLET HAVING INTEGRATED COILS AND MIST REDUCING VANES 审中-公开
    具有集成线圈和减雾器的气体涡轮机入口

    公开(公告)号：US20150308338A1

    公开(公告)日：2015-10-29

    申请号：US14117661

    申请日：2013-01-11

    Applicant: General Electric Company

    Inventor： Yongjiang Hao ,  Doug Scott Byrd ,  Brad Aaron Kippel ,  Jianmin Zhang

    IPC: F02C7/12 ,  F01D25/32

    CPC classification number: F02C7/12 ,  F01D25/32 ,  F28F1/32 ,  F28F17/00

    Abstract: An integrated coil and fin system in a gas turbine inlet. The integrated system includes at least one wavy, non-planar, fin integrated with at least one heating/cooling coil, wherein the at least one coil is configured to heat or cool air moving through the gas turbine inlet, and wherein the at least one non-planar fin is configured to remove moisture in the air moving through the gas turbine inlet. In one embodiment, at least one hook can be included at an end or along a length of at least one non-planar fin.

    Abstract translation: 燃气轮机入口中的集成线圈和翅片系统。 集成系统包括与至少一个加热/冷却盘管集成的至少一个波浪形非平面翅片，其中至少一个线圈构造成加热或冷却通过燃气轮机入口移动的空气，并且其中至少一个 非平面翅片构造成去除移动通过燃气轮机入口的空气中的水分。 在一个实施例中，至少一个钩可以包括在至少一个非平面翅片的一端或一段长度上。

    GAS TURBINE ON-LINE WATER WASH SYSTEM AND METHOD
    7.
    发明申请
    GAS TURBINE ON-LINE WATER WASH SYSTEM AND METHOD 有权
    气体涡轮在线水洗系统及方法

    公开(公告)号：US20150000693A1

    公开(公告)日：2015-01-01

    申请号：US13932467

    申请日：2013-07-01

    Applicant: General Electric Company

    Inventor： Doug Scott BYRD ,  Gilbert Otto Kraemer ,  Hua Zhang ,  Jianmin Zhang ,  Valery Ivanovich Ponyavin

    IPC: F01D25/00

    CPC classification number: F01D25/002 ,  B08B7/00 ,  F05D2270/172

    Abstract: An on-line wash system for a compressor including: a nozzle including a flow passage for wash liquid, wherein the flow passage is configured to be coupled to a source of a wash liquid and includes a discharge outlet arranged to project the wash liquid into a stream of working fluid for the turbomachine; an electrode proximate to the flow passage of the nozzle, wherein the electrode is configured to form an electrical field sufficient to charge the wash liquid flowing through the passage and the charge applied to the wash liquid is of a first polarity, and a surface of the compressor charged with the first polarity, wherein the surface is exposed to the stream of working fluid and downstream of the nozzle.

    Abstract translation: 一种用于压缩机的在线洗涤系统，包括：喷嘴，其包括用于洗涤液体的流动通道，其中所述流动通道被配置为联接到洗涤液体源并且包括排出口，所述排出出口布置成将所述洗涤液体投射到 用于涡轮机的工作液流; 靠近所述喷嘴的流动通道的电极，其中所述电极被配置为形成足以对流过所述通道的洗涤液体充电的电场，并且施加到所述洗涤液体的电荷具有第一极性，并且所述表面 带有第一极性的压缩机，其中表面暴露于工作流体流并且在喷嘴的下游。

    Gas turbine on-line water wash system and method
    9.
    发明授权
    Gas turbine on-line water wash system and method 有权

    公开(公告)号：US09951646B2

    公开(公告)日：2018-04-24

    申请号：US13932467

    申请日：2013-07-01

    Applicant: General Electric Company

    Inventor： Doug Scott Byrd ,  Gilbert Otto Kraemer ,  Hua Zhang ,  Jianmin Zhang ,  Valery Ivanovich Ponyavin

    IPC: F01D25/00 ,  B08B7/00

    CPC classification number: F01D25/002 ,  B08B7/00 ,  F05D2270/172

    Abstract: An on-line wash system for a compressor including: a nozzle including a flow passage for wash liquid, wherein the flow passage is configured to be coupled to a source of a wash liquid and includes a discharge outlet arranged to project the wash liquid into a stream of working fluid for the turbomachine; an electrode proximate to the flow passage of the nozzle, wherein the electrode is configured to form an electrical field sufficient to charge the wash liquid flowing through the passage and the charge applied to the wash liquid is of a first polarity, and a surface of the compressor charged with the first polarity, wherein the surface is exposed to the stream of working fluid and downstream of the nozzle.

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