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1. 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。

2. 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。

3. 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。

4. 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。

5. 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。

6. 发明申请

US20100101203A1 FEED INJECTOR COOLING JACKET 审中-公开
标题翻译：进料注射器冷却夹克
公开(公告)号：US20100101203A1
公开(公告)日：2010-04-29
申请号：US12259631
申请日：2008-10-28
申请人： Monty Lee Harned , Douglas Scott Byrd , Judeth Brannon Corry , Paul Stephen Dimascio , Sunikant Arvindkumar Patel , Shashishekara Sitharamarao Talya
发明人： Monty Lee Harned , Douglas Scott Byrd , Judeth Brannon Corry , Paul Stephen Dimascio , Sunikant Arvindkumar Patel , Shashishekara Sitharamarao Talya
IPC分类号： F02B43/00 , F02C1/00 , B23P17/04
CPC分类号： B01J4/002 , B01J2219/00119 , C10J3/506 , C10J2200/152 , C10J2300/093 , C10J2300/0959 , C10J2300/0976 , C10J2300/1653 , F23D1/005 , F23D2214/00 , Y02E20/16 , Y02E20/18 , Y02E20/366 , Y10T29/49
摘要： A feed injector for providing feed to a gasifier of an integrated gasification combined cycle system includes: a base leading to a body and terminating in a tip, the tip including an exitway for injecting feed into the gasifier; the tip including a mating of an inner shell disposed within a core insert, with an outer shell in which the core insert is disposed; a plurality of spacers disposed between the core insert and inner shell thus providing an inner annular space, and another plurality of spacers disposed between the core insert and outer shell thus providing an outer annular space; the inner annular space and the outer annular space being in fluid communication at the tip and providing for a flow of coolant from the base to the tip and back to the base. A method of fabrication and an integrated gasification combined cycle power plant are also disclosed.
摘要翻译：一种用于向一体化气化联合循环系统的气化器提供进料的进料喷射器包括：通向主体并终止于尖端的底座，所述尖端包括用于将进料注入气化器的出口; 所述尖端包括设置在芯插入件内的内壳的配合与设置所述芯插入件的外壳; 设置在芯插入件和内壳之间的多个间隔件，从而提供内环形空间，以及设置在芯插入件和外壳之间的另外多个间隔件，从而提供外环形空间; 所述内部环形空间和所述外部环形空间在所述尖端处流体连通并且提供冷却剂从所述基部到所述尖端并返回到所述基部的流动。还公开了一种制造方法和一体化气化联合循环发电厂。

7. 发明申请

US20130318993A1 UTILIZATION OF FUEL GAS FOR PURGING A DORMANT FUEL GAS CIRCUIT 有权
标题翻译：用于燃烧多种燃料气体电路的燃料气体的利用
公开(公告)号：US20130318993A1
公开(公告)日：2013-12-05
申请号：US13484410
申请日：2012-05-31
申请人： Dean Matthew Erickson , Robert Lester Brooks , Douglas Scott Byrd , Joseph Robert Law
发明人： Dean Matthew Erickson , Robert Lester Brooks , Douglas Scott Byrd , Joseph Robert Law
IPC分类号： F02C7/232
CPC分类号： F02C7/22 , F02C7/222 , F02C7/232 , F02C9/34 , F23K5/18
摘要： An approach for utilizing fuel gas to purge a dormant fuel gas circuit is disclosed. In one aspect, there is a fuel gas supply that supplies fuel to fuel gas circuits. Gas control valves, each coupled to one of the fuel gas circuits control the flow of fuel gas thereto from the fuel gas supply. A fuel purge system selectively purges fuel gas circuits from the fuel gas circuits that are dormant with fuel gas from the fuel gas supply.
摘要翻译：公开了一种利用燃料气体吹扫休眠燃料气体回路的方法。一方面，存在向燃料气体回路供应燃料的燃料气体供应。每个与燃料气体回路中的一个连接的气体控制阀控制燃料气体从燃料气体供应的流动。燃料净化系统选择性地从燃料气体回路中燃烧气体回路，燃料气体回路与来自燃料气体源的燃料气体休眠。

8. 发明申请

US20120088197A1 SYSTEM AND METHOD FOR DETERMINING A FLAME CONDITION IN A COMBUSTOR 审中-公开
标题翻译：用于确定燃烧器中火焰条件的系统和方法
公开(公告)号：US20120088197A1
公开(公告)日：2012-04-12
申请号：US12900668
申请日：2010-10-08
申请人： Douglas Scott Byrd , Joseph Robert Law
发明人： Douglas Scott Byrd , Joseph Robert Law
IPC分类号： F23C99/00
CPC分类号： F23N5/16 , F02C9/28 , F02C9/50 , F05D2260/80 , F05D2270/083 , F05D2270/301 , F23N5/242 , F23N2029/00 , F23N2031/06 , F23N2041/20
摘要： A system for determining a flame condition in a combustor includes a pressure sensor that generates a pressure signal reflective of a pressure in the combustor. A controller receives the pressure signal and generates a flame signal reflective of the flame condition in the combustor. A method for determining a flame condition in a combustor includes measuring a pressure in the combustor, comparing the measured pressure in the combustor to a predetermined limit, and generating a flame signal based on the comparison of the measured pressure in the combustor to the predetermined limit, wherein the flame signal reflects the flame condition in the combustor.
摘要翻译：用于确定燃烧器中的火焰状态的系统包括产生反映燃烧器中的压力的压力信号的压力传感器。控制器接收压力信号并产生反映燃烧器中的火焰状态的火焰信号。一种用于确定燃烧器中的火焰状态的方法，包括测量燃烧器中的压力，将燃烧器中的测量压力与预定极限进行比较，并且基于将燃烧器中的测量压力与预定极限的比较来产生火焰信号其中火焰信号反映燃烧器中的火焰状态。

9. 发明申请

US20090053040A1 APPARATUS AND METHOD FOR PRESSURIZED INLET EVAPORATIVE COOLING OF GAS TURBINE ENGINES 有权
标题翻译：气体涡轮发动机压缩式进气冷却装置及方法
公开(公告)号：US20090053040A1
公开(公告)日：2009-02-26
申请号：US11843060
申请日：2007-08-22
申请人： Rahul Jaikaran Chillar , Douglas Scott Byrd
发明人： Rahul Jaikaran Chillar , Douglas Scott Byrd
IPC分类号： F01D1/00
CPC分类号： F02C7/1435 , F02C3/305 , Y02T50/675
摘要： An apparatus for cooling air for an intake to a gas turbine, is provided and includes a pressurized water piping and nozzle apparatus for producing a water spray in an airflow to the intake; and evaporative media for receiving the spray and causing a pressurizing of the air in the airflow.
摘要翻译：提供了一种用于将用于进气到燃气轮机的空气的冷却装置，并且包括用于在进气口的气流中产生喷水的加压水管道和喷嘴装置; 以及用于接收喷雾并引起气流中的空气加压的蒸发介质。

10. 发明授权

US09376931B2 Turbomachine passage cleaning system 有权
标题翻译：涡轮机通道清洗系统
公开(公告)号：US09376931B2
公开(公告)日：2016-06-28
申请号：US13359962
申请日：2012-01-27
申请人： Arun Meenakshinatha Iyer , Douglas Scott Byrd , Gary Michael Itzel , Jaime Javier Maldonado
发明人： Arun Meenakshinatha Iyer , Douglas Scott Byrd , Gary Michael Itzel , Jaime Javier Maldonado
IPC分类号： F04D29/58 , F01D25/00
CPC分类号： F01D25/002 , F04D29/5846 , F05D2210/13 , F05D2260/2322 , F05D2260/607
摘要： A turbomachine passage cleaning system includes a first airflow passage having a first inlet configured and disposed to fluidly connect to a compressor portion, a first outlet configured and disposed to fluidly connect to a turbine portion, and a first intermediate portion including a first strainer. A second airflow passage is fluidly coupled to the first airflow passage. The second airflow passage has a second intermediate portion having second strainer. A first valve is arranged in the first intermediate portion upstream from the first strainer, and a second valve is arranged in the second intermediate portion upstream from the second strainer. The first and second valves are selectively operated to control fluid flow into respective ones of the first and second airflow passages to filter air passing from a turbomachine compressor portion to a turbomachine turbine portion.
摘要翻译：涡轮机通道清洁系统包括第一气流通道，其具有构造和设置成流体连接到压缩机部分的第一入口，被配置和设置成流体连接到涡轮机部分的第一出口和包括第一过滤器的第一中间部分。第二气流通道流体地联接到第一气流通道。第二气流通道具有具有第二过滤器的第二中间部分。第一阀布置在第一过滤器上游的第一中间部分中，并且第二阀布置在第二过滤器上游的第二中间部分中。选择性地操作第一阀和第二阀以控制流入第一和第二气流通道中的相应流体的流体，以过滤从涡轮机压缩机部分流到涡轮机涡轮机部分的空气。

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