SILENCER DUCT HAVING SILENCING ELEMENT AND COUPLERS
    114.
    发明申请
    SILENCER DUCT HAVING SILENCING ELEMENT AND COUPLERS 审中-公开
    带防静电元件和联轴器的保护罩

    公开(公告)号:US20170074289A1

    公开(公告)日:2017-03-16

    申请号:US14855902

    申请日:2015-09-16

    Abstract: A silencer duct that may be part of, for example, a turbomachine inlet and may include a duct body, and a silencer element extending axially through the duct body. A first portion of a coupler may extend axially from a first side of the duct body. A second portion of a coupler may extend axially from a second side of the duct body. At least one of the first portion of the coupler and the second portion of the coupler are configured to couple to at least one of an adjacent silencer duct and an inlet.

    Abstract translation: 可以是例如涡轮机入口的一部分的消音器管道,并且可以包括管道主体和沿轴向延伸穿过管道主体的消音器元件。 耦合器的第一部分可以从导管主体的第一侧轴向延伸。 耦合器的第二部分可以从导管主体的第二侧轴向延伸。 耦合器的第一部分和耦合器的第二部分中的至少一个被配置成耦合到相邻的消声器导管和入口中的至少一个。

    HEAVY DUTY GAS TURBINE INLET SYSTEM
    115.
    发明申请
    HEAVY DUTY GAS TURBINE INLET SYSTEM 有权
    重型燃气轮机入口系统

    公开(公告)号:US20160258357A1

    公开(公告)日:2016-09-08

    申请号:US14638472

    申请日:2015-03-04

    CPC classification number: F02C7/045 B64D29/00 F02C3/30 F02C7/047 F05D2260/96

    Abstract: A silencer apparatus for a gas turbine inlet system ducting is disclosed. The inlet ducting contains a main silencer and a pre-silencer, and Inlet Bleed Heat (“IBH”) located between the silencers. The pre-silencer decreases the noise level from the turbine compressor and makes the air flow/temperature profiles more uniform. The main silencer reduces noise from the IBH and the remaining noise from the compressor to an appropriate level. The main silencer is comprised of a first plurality of sound-absorbing splitters disposed along the gas flow direction in the gas turbine inlet ducting. The pre-silencer is comprised of a second plurality of sound-absorbing splitters disposed along the gas flow direction in the gas turbine inlet ducting, but staggered with respect to the first plurality of splitters to thereby block a direct line of travel for noise acoustical waves from the compressor travelling opposite the gas flow direction in the inlet ducting.

    Abstract translation: 公开了一种用于燃气轮机入口系统管道的消声器装置。 入口管道包含一个主消音器和一个预消声器,以及位于消音器之间的入口泄放热(“IBH”)。 预消声器降低了来自涡轮压缩机的噪音水平,使气流/温度曲线更加均匀。 主消声器将IBH的噪音和压缩机的噪音降低到适当的水平。 主消声器包括沿燃气轮机入口管道中的气流方向设置的第一组多个吸声分离器。 预消音器由在气体涡轮机入口管道中沿着气体流动方向设置的第二多个吸声分离器组成,但是相对于第一多个分离器交错,从而阻挡用于噪声声波的直线行进 从压缩机在入口管道中与气体流动方向相反地行进。

    Silencing and cooling assembly with fibrous medium
    116.
    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

    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。

    COOLING APPARATUS FOR TURBOMACHINERY WITH METHOD OF INSTALLATION
    117.
    发明申请
    COOLING APPARATUS FOR TURBOMACHINERY WITH METHOD OF INSTALLATION 有权
    用于安装方法的涡轮机的冷却装置

    公开(公告)号:US20160146043A1

    公开(公告)日:2016-05-26

    申请号:US14550946

    申请日:2014-11-22

    Abstract: Embodiments of the present disclosure provide cooling systems for turbomachinery and methods of installation. In an embodiment, an apparatus of the present disclosure can include a ventilation conduit for routing a cooling air from a compressor of a power generation system to a turbine component of the power generation system; and a nozzle in fluid communication with the ventilation conduit, wherein the nozzle delivers water from a water supply into the ventilation conduit.

    Abstract translation: 本公开的实施例提供了用于涡轮机械的冷却系统和安装方法。 在一个实施例中,本公开的装置可以包括用于将冷却空气从发电系统的压缩机路由到发电系统的涡轮机部件的通风管道; 以及与所述通气导管流体连通的喷嘴,其中所述喷嘴将水从供水部分输送到所述通气导管中。

    SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING
    118.
    发明申请

    公开(公告)号:US20160084160A1

    公开(公告)日:2016-03-24

    申请号:US14961131

    申请日:2015-12-07

    CPC classification number: F02C3/30 F23K5/005 F23K5/12 F23L7/002 F23R3/36

    Abstract: A system includes a plurality of interconnected mixing assemblies configured to mix a first fuel and water to generate a first mixture, and mix a second fuel and the water to generate a second mixture. The first and second fuel mixtures are configured to combust in a plurality of combustors of a gas turbine. The interconnected mixing assemblies include first and second fuel passages, a water passage, first and second mixers, first and second fuel valves, and first and second water valves disposed in an integrated housing. The first fuel valve has a first fuel flow coefficient between approximately 1.0 to 1.5, the second fuel valve has a second fuel flow coefficient between approximately 3.0 to 5.0, the first water valve has a first water flow coefficient between approximately 0.4 to 0.55, and the second water valve has a second water flow coefficient between approximately 3.5 to 5.0.

    SYSTEM AND METHOD FOR OPERATING A POWER PLANT
    120.
    发明申请
    SYSTEM AND METHOD FOR OPERATING A POWER PLANT 有权
    用于操作发电厂的系统和方法

    公开(公告)号:US20140238039A1

    公开(公告)日:2014-08-28

    申请号:US14037268

    申请日:2013-09-25

    CPC classification number: F02C7/236 F02C3/04 F02C3/045 F02C7/22 F02C9/40

    Abstract: A system including a fuel-supply system including, an auxiliary-fuel-gas compressor configured to compress a fuel for use by a gas-turbine system, an expander configured to generate power by expanding an oxidant from the gas-turbine system, and a motor/generator configured to function in a motor mode and in a generator mode, wherein the motor/generator drives fuel compression with the auxiliary fuel-gas compressor in the motor mode, and the motor/generator generates power in the generator mode as the expander uses oxidant from the gas-turbine system to drive the motor/generator

    Abstract translation: 一种包括燃料供给系统的系统,包括:构造成压缩由燃气轮机系统使用的燃料的辅助燃料气体压缩机;膨胀机,其构造成通过从所述燃气轮机系统膨胀氧化剂而发电;以及 电动机/发电机被配置为在电动机模式和发电机模式下起作用,其中电动机/发电机在电动机模式下利用辅助燃料气体压缩机驱动燃料压缩,并且电动发电机以发电机模式发电,作为膨胀机 使用来自燃气轮机系统的氧化剂来驱动电动机/发电机

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