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1. 发明申请

US20160237902A1 GAS TURBINE INLET AIR CONDITIONING COIL SYSTEM 审中-公开
标题翻译：气体涡轮进口空调线圈系统
公开(公告)号：US20160237902A1
公开(公告)日：2016-08-18
申请号：US14768428
申请日：2013-11-05
申请人： Jianmin ZHANG , Bradly Aaron KIPPEL , Yongjiang HAO , Douglas Scott BYRD , Hua ZHANG , General Electric Company
发明人： Jianmin Zhang , Brady Aaron Kippel , Yongjiang Hao , Douglas Scott Byrd , Hua Zhang
IPC分类号： F02C7/143 , F02C7/057
CPC分类号： F02C7/143 , F02C7/057 , F05D2220/32 , F05D2260/20 , Y02T50/675
摘要： A system includes a gas turbine system, including an air intake system that includes a housing, a first plurality of air conditioning coils, a second plurality of air conditioning coils that is downstream relative to the first plurality, and a baffle extending between each of the first and second pluralities of air conditioning coils, wherein the baffle is configured to direct an air flow through the first or second pluralities of air conditioning coils in a closed position, and the baffle is configured to enable air flow to bypass the first and second pluralities of coils in an opened position.
摘要翻译：一种系统包括燃气轮机系统，其包括进气系统，其包括壳体，第一多个空调线圈，相对于第一多个下游的第二多个空调线圈，以及在每个第一和第二多个空调线圈，其中所述挡板构造成在关闭位置引导空气流通过所述第一或第二多个空调线圈，并且所述挡板被配置为使空气流能够绕过所述第一和第二多个空调的线圈处于打开位置。

2. 发明申请

US20160273456A1 GAS TURBINE SYSTEM AND METHOD 审中-公开
标题翻译：气体涡轮机系统和方法
公开(公告)号：US20160273456A1
公开(公告)日：2016-09-22
申请号：US14768431
申请日：2013-10-16
申请人： Hua ZHANG , Wenjie WU , Yongjiang HAO , GENERAL ELECTRIC COMPANY
发明人： Hua Zhang , Wenjie Wu , Yongjiang Hao
IPC分类号： F02C7/32 , F02C7/22 , F02C3/04 , F02C7/36
CPC分类号： F02C7/32 , F02C3/04 , F02C7/22 , F02C7/36 , F05D2220/32 , F05D2220/7642 , F05D2260/85
摘要： A fuel supply system includes a first fuel gas compressor coupled to a fuel gas compressor shaft and configured to pressurize a fuel for a gas turbine system. A clutch is coupled to the fuel gas compressor shaft and is configured to selectively engage the fuel gas compressor shaft with a turbine shaft of the gas turbine system. An electromechanical machine is configured to operator as a motor to drive the fuel gas compressor shaft or to operate as a generator driven by the turbine shaft to generator power, based on an operating condition of the gas turbine system.
摘要翻译：燃料供应系统包括耦合到燃料气体压缩机轴并被配置为对燃气轮机系统的燃料加压的第一燃料气体压缩机。离合器联接到燃料气体压缩机轴并且构造成选择性地将燃料气体压缩机轴与燃气轮机系统的涡轮轴接合。机电机构被配置为基于燃气轮机系统的操作条件，作为电动机操作以驱动燃料气体压缩机轴或作为由涡轮机轴驱动的发电机运行以发电机功率。

3. 发明授权

US08973366B2 Integrated fuel and water mixing assembly for use in conjunction with a combustor 有权
标题翻译：与燃烧器结合使用的集成燃料和水混合组件
公开(公告)号：US08973366B2
公开(公告)日：2015-03-10
申请号：US13280216
申请日：2011-10-24
申请人： Hua Zhang , Douglas Frank Beadie , Douglas Scott Byrd , Fabien Thibault Codron , James Frederik den Outer , Mark Jason Fisher
发明人： Hua Zhang , Douglas Frank Beadie , Douglas Scott Byrd , Fabien Thibault Codron , James Frederik den Outer , Mark Jason Fisher
IPC分类号： F02C1/00 , F02G3/00 , F23K5/12 , F23K5/06 , F02C3/30 , F02C7/22 , F02C9/40
CPC分类号： F23K5/12 , F02C3/30 , F02C7/222 , F02C9/40 , F05D2210/13 , F05D2260/607 , F23K5/06 , Y02T50/675 , Y10T137/8766 , Y10T137/87668
摘要： A system includes a mixing assembly configured to mix a liquid fuel and a water to generate a fuel mixture. The fuel mixture is configured to combust in a combustor of a gas turbine. The mixing assembly includes a liquid fuel passage disposed in an integrated housing. The liquid fuel passage is configured to flow the liquid fuel and to exclude liquid traps. The mixing assembly also includes a water passage disposed in the integrated housing. The water passage is configured to flow the water and to exclude liquid traps. The mixing assembly also includes a mixer disposed in the integrated housing and coupled to the liquid fuel passage and the water passage. The mixer is configured to mix the liquid fuel and the water to form the fuel mixture.
摘要翻译：一种系统包括配置成混合液体燃料和水以产生燃料混合物的混合组件。燃料混合物构造成在燃气轮机的燃烧器中燃烧。混合组件包括设置在一体化壳体中的液体燃料通道。液体燃料通道构造成流动液体燃料并排除液体捕集阱。混合组件还包括设置在一体式壳体中的水通道。水通道构造成流过水并排除液体捕集阱。混合组件还包括设置在一体式壳体中并耦合到液体燃料通道和水通道的混合器。混合器配置成混合液体燃料和水以形成燃料混合物。

4. 发明申请

US20130097991A1 SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING 有权
标题翻译：涡轮机燃油混合系统
公开(公告)号：US20130097991A1
公开(公告)日：2013-04-25
申请号：US13280216
申请日：2011-10-24
申请人： Hua Zhang , Douglas Frank Beadie , Douglas Scott Byrd , Fabien Thibault Codron , James Frederik den Outer , Mark Jason Fisher
发明人： Hua Zhang , Douglas Frank Beadie , Douglas Scott Byrd , Fabien Thibault Codron , James Frederik den Outer , Mark Jason Fisher
IPC分类号： F02C7/22
CPC分类号： F23K5/12 , F02C3/30 , F02C7/222 , F02C9/40 , F05D2210/13 , F05D2260/607 , F23K5/06 , Y02T50/675 , Y10T137/8766 , Y10T137/87668
摘要： A system includes a mixing assembly configured to mix a liquid fuel and a water to generate a fuel mixture. The fuel mixture is configured to combust in a combustor of a gas turbine. The mixing assembly includes a liquid fuel passage disposed in an integrated housing. The liquid fuel passage is configured to flow the liquid fuel and to exclude liquid traps. The mixing assembly also includes a water passage disposed in the integrated housing. The water passage is configured to flow the water and to exclude liquid traps. The mixing assembly also includes a mixer disposed in the integrated housing and coupled to the liquid fuel passage and the water passage. The mixer is configured to mix the liquid fuel and the water to form the fuel mixture.
摘要翻译：一种系统包括配置成混合液体燃料和水以产生燃料混合物的混合组件。燃料混合物构造成在燃气轮机的燃烧器中燃烧。混合组件包括设置在一体化壳体中的液体燃料通道。液体燃料通道构造成流动液体燃料并排除液体捕集阱。混合组件还包括设置在一体式壳体中的水通道。水通道构造成流过水并排除液体捕集阱。混合组件还包括设置在一体式壳体中并耦合到液体燃料通道和水通道的混合器。混合器配置成混合液体燃料和水以形成燃料混合物。

5. 发明授权

US08083466B2 Turbomachine inlet heating system 有权
标题翻译：涡轮机进气加热系统
公开(公告)号：US08083466B2
公开(公告)日：2011-12-27
申请号：US12403444
申请日：2009-03-13
申请人： Hua Zhang , David Wesley Ball, Jr. , Valery Ivanovich Ponyavin , Douglas Scott Byrd
发明人： Hua Zhang , David Wesley Ball, Jr. , Valery Ivanovich Ponyavin , Douglas Scott Byrd
IPC分类号： F01D21/12
CPC分类号： F02C9/18 , F01D25/10 , F02C7/08 , F05D2260/221 , F05D2270/101
摘要： A turbomachine system includes a compressor having a compressor intake and a compressor extraction outlet, and an inlet system fluidly connected to the compressor intake and the compressor extraction outlet. The inlet system includes a plenum having a first end portion that extends to a second end portion through an intermediate portion. The inlet system also includes a heating system having a plurality of conduits extending horizontally through the intermediate portion of the plenum and arranged in a vertical relationship. Heated air from the compressor extraction outlet passes through the plurality of conduits and raises a temperature of ambient air passing through the plenum and into the compressor intake.
摘要翻译：涡轮机系统包括具有压缩机进气口和压缩机排出口的压缩机，以及与压缩机进气口和压缩机排出口流体连接的入口系统。入口系统包括具有通过中间部分延伸到第二端部的第一端部的增压室。入口系统还包括加热系统，其具有水平延伸通过气室的中间部分并以垂直关系布置的多个管道。来自压缩机排出口的加热空气通过多个管道，并且使经过集气室的环境空气的温度升高并进入压缩机进气口。

6. 发明申请

US20100232945A1 TURBOMACHINE INLET HEATING SYSTEM 有权
标题翻译：涡轮进气加热系统
公开(公告)号：US20100232945A1
公开(公告)日：2010-09-16
申请号：US12403444
申请日：2009-03-13
申请人： Hua Zhang , David Wesley Ball, JR. , Valery Ivanovich Ponyavin , Douglas Scott Byrd
发明人： Hua Zhang , David Wesley Ball, JR. , Valery Ivanovich Ponyavin , Douglas Scott Byrd
IPC分类号： F01D25/08
CPC分类号： F02C9/18 , F01D25/10 , F02C7/08 , F05D2260/221 , F05D2270/101
摘要： A turbomachine system includes a compressor having a compressor intake and a compressor extraction outlet, and an inlet system fluidly connected to the compressor intake and the compressor extraction outlet. The inlet system includes a plenum having a first end portion that extends to a second end portion through an intermediate portion. The inlet system also includes a heating system having a plurality of conduits extending horizontally through the intermediate portion of the plenum and arranged in a vertical relationship. Heated air from the compressor extraction outlet passes through the plurality of conduits and raises a temperature of ambient air passing through the plenum and into the compressor intake.
摘要翻译：涡轮机系统包括具有压缩机进气口和压缩机排出口的压缩机，以及与压缩机进气口和压缩机排出口流体连接的入口系统。入口系统包括具有通过中间部分延伸到第二端部的第一端部的增压室。入口系统还包括加热系统，其具有水平延伸通过气室的中间部分并以垂直关系布置的多个管道。来自压缩机排出口的加热空气通过多个管道，并且使经过集气室的环境空气的温度升高并进入压缩机进气口。

7. 发明申请

US20110099970A1 SYSTEM FOR ICE AND/OR FROST PREVENTION USING GUIDED WAVE ENERGY 有权
标题翻译：使用指导波能量进行冰和/或预防的系统
公开(公告)号：US20110099970A1
公开(公告)日：2011-05-05
申请号：US12611332
申请日：2009-11-03
申请人： Hua Zhang , Jianmin Zhang
发明人： Hua Zhang , Jianmin Zhang
IPC分类号： F02C3/00 , H05B6/64 , F02G3/00
CPC分类号： H05B6/80 , F02C7/047
摘要： An ice and/or frost preventing system for positioning in an airflow tunnel having an air inlet includes a plurality of waveguide passages positioned in the airflow tunnel; an air filter positioned in each waveguide passage; a microwave energy source coupled to each waveguide passage; a first screen positioned in the airflow tunnel upstream of the plurality of waveguide passages; and a second screen positioned in the airflow tunnel downstream of the plurality of waveguide passages. The microwave energy sources and the first and second screens create a guided, standing wave, microwave energy that substantially prevents at least one of ice and frost from forming on the air filters. A turbine system including the ice and/or frost preventing system is also described.
摘要翻译：用于在具有空气入口的气流通道中定位的防冰和/或防霜系统包括位于气流通道中的多个波导通道; 位于每个波导通道中的空气过滤器; 耦合到每个波导通道的微波能源; 位于多个波导通道上游的气流通道中的第一屏幕; 以及位于多个波导通道下游的气流通道中的第二屏幕。微波能量源和第一和第二屏幕产生引导的驻波，微波能量，其基本上防止冰和霜中的至少一种在空气过滤器上形成。还描述了包括冰和/或防霜系统的涡轮机系统。

8. 发明申请

US20140069076A1 GAS TURBINE INLET FOGGING SYSTEM USING ELECTROHYDRODYNAMIC (EHD) ATOMIZATION 审中-公开
标题翻译：使用电动力学（EHD）原理的气体涡轮入口喷雾系统
公开(公告)号：US20140069076A1
公开(公告)日：2014-03-13
申请号：US13607849
申请日：2012-09-10
申请人： Valery Ivanovich Ponyavin , Gilbert Otto Kraemer , Hua Zhang , Jianmin Zhang
发明人： Valery Ivanovich Ponyavin , Gilbert Otto Kraemer , Hua Zhang , Jianmin Zhang
IPC分类号： F02C3/30
CPC分类号： F02C3/305 , F02C7/1435
摘要： A gas turbine inlet fogging system using electrohydrodynamic (EHD) atomization is disclosed. In one embodiment, the inlet fogging system includes: a gas turbine system including an air inlet duct, and a plurality of electrohydrodynamic (EHD) nozzles coupled to a water supply, the plurality of EHD nozzles configured to provide a water-spray for reducing a temperature of inlet air drawn into the air inlet duct. In another embodiment, an inlet fogging system for a gas turbine system includes: a plurality of electrohydrodynamic (EHD) nozzles, and a water supply in fluid communication with the plurality of EHD nozzles.
摘要翻译：公开了一种使用电动力学（EHD）雾化的燃气轮机入口雾化系统。在一个实施例中，入口雾化系统包括：燃气涡轮机系统，其包括空气入口管道和联接到水源的多个电动力学（EHD）喷嘴，所述多个EHD喷嘴被配置为提供喷水以减少吸入空气入口管道的入口空气温度。在另一个实施例中，用于燃气轮机系统的入口雾化系统包括：多个电动力学（EHD）喷嘴，以及与多个EHD喷嘴流体连通的供水。

9. 发明授权

US08505273B2 System for ice and/or frost prevention using guided wave energy 有权
标题翻译：使用导波能量进行冰和/或霜预防的系统
公开(公告)号：US08505273B2
公开(公告)日：2013-08-13
申请号：US12611332
申请日：2009-11-03
申请人： Hua Zhang , Jianmin Zhang
发明人： Hua Zhang , Jianmin Zhang
IPC分类号： F02G3/00
CPC分类号： H05B6/80 , F02C7/047
摘要： An ice and/or frost preventing system for positioning in an airflow tunnel having an air inlet includes a plurality of waveguide passages positioned in the airflow tunnel; an air filter positioned in each waveguide passage; a microwave energy source coupled to each waveguide passage; a first screen positioned in the airflow tunnel upstream of the plurality of waveguide passages; and a second screen positioned in the airflow tunnel downstream of the plurality of waveguide passages. The microwave energy sources and the first and second screens create a guided, standing wave, microwave energy that substantially prevents at least one of ice and frost from forming on the air filters. A turbine system including the ice and/or frost preventing system is also described.
摘要翻译：用于在具有空气入口的气流通道中定位的防冰和/或防霜系统包括位于气流通道中的多个波导通道; 位于每个波导通道中的空气过滤器; 耦合到每个波导通道的微波能源; 位于多个波导通道上游的气流通道中的第一屏幕; 以及位于多个波导通道下游的气流通道中的第二屏幕。微波能量源和第一和第二屏幕产生引导的驻波，微波能量，其基本上防止冰和霜中的至少一种在空气过滤器上形成。还描述了包括冰和/或防霜系统的涡轮机系统。

10. 发明申请

US20130199150A1 STEAM INJECTION ASSEMBLY FOR A COMBINED CYCLE SYSTEM 审中-公开
标题翻译：用于组合循环系统的蒸汽注入装置
公开(公告)号：US20130199150A1
公开(公告)日：2013-08-08
申请号：US13365580
申请日：2012-02-03
申请人： Jianmin Zhang , Kihyung Kim , Brad Aaron Kippel , Hua Zhang
发明人： Jianmin Zhang , Kihyung Kim , Brad Aaron Kippel , Hua Zhang
IPC分类号： F02C6/00 , F01K23/00
CPC分类号： F01K23/10 , F01K17/06 , Y02E20/16
摘要： A steam injection assembly for a combined cycle system includes a heat recovery system having at least one superheater configured to generate a steam supply. Also included is a gas turbine system having an inlet and a compressor, wherein the inlet receives an air supply and the steam supply for combined injection into the compressor.
摘要翻译：一种用于组合循环系统的蒸汽注入组件包括热回收系统，该系统具有至少一个过热器，其配置成产生蒸汽供应。还包括具有入口和压缩机的燃气轮机系统，其中入口接收空气供应和用于组合喷射到压缩机中的蒸汽供应。

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