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1. 发明申请

US20090038313A1 METHOD AND APPARATUS FOR SUPPLYING PRESSURE FOR SPRAY INLET TEMPERATURE SUPPRESSOR OF GAS TURBINES 有权
标题翻译：用于喷射喷嘴喷射压力抑制器的压力的方法和装置
公开(公告)号：US20090038313A1
公开(公告)日：2009-02-12
申请号：US11834958
申请日：2007-08-07
申请人： David Wesley Ball, JR. , Leroy Omar Tomlinson , Douglas Frank Beadie
发明人： David Wesley Ball, JR. , Leroy Omar Tomlinson , Douglas Frank Beadie
IPC分类号： F02C3/30 , F02C7/143
CPC分类号： F02C7/1435 , F01K21/047 , F02C3/305 , F05D2260/20 , Y02E20/16
摘要： An apparatus for supplying water to a misting system for an inlet of a gas turbine, includes a diversion of heated feedwater from a loop and to a pump, the pump providing high-pressure feedwater to the misting system. A combined cycle power plant and a method for supplying water are provided.
摘要翻译：一种用于向用于燃气轮机入口的雾化系统供水的设备包括将加热的给水从环路引导到泵，该泵向雾化系统提供高压给水。提供了一种联合循环发电厂和一种供水方法。

2. 发明申请

US20100024424A1 CONDENSER FOR A COMBINED CYCLE POWER PLANT 审中-公开
标题翻译：一个组合循环电厂的冷凝器
公开(公告)号：US20100024424A1
公开(公告)日：2010-02-04
申请号：US12181741
申请日：2008-07-29
申请人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, JR.
发明人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, JR.
IPC分类号： F01K13/00
CPC分类号： F01K9/00 , F01K11/02 , F01K23/106 , F28B1/00 , F28D15/02 , Y02E20/16
摘要： A combined cycle power plant includes a steam turbine section having an inlet section and an outlet section. The steam turbine section passes steam from the inlet section toward the outlet section. The combined cycle power plant also includes a condenser fluidly connected to the outlet section of the steam turbine section. The condenser includes a plurality of heat pipes configured to extract latent heat from steam passing from the steam turbine section to form condensed water.
摘要翻译：联合循环发电厂包括具有入口部分和出口部分的汽轮机部分。蒸汽轮机部分将来自进口部分的蒸汽传送到出口部分。联合循环发电厂还包括流体连接到蒸汽涡轮机部分的出口部分的冷凝器。冷凝器包括多个热管，其构造成从蒸汽涡轮机部分抽出的蒸气中提取潜热，形成冷凝水。

3. 发明申请

US20130098038A1 SYSTEM FOR HEATING A FUEL 有权
标题翻译：燃料加热系统
公开(公告)号：US20130098038A1
公开(公告)日：2013-04-25
申请号：US13280659
申请日：2011-10-25
申请人： Timothy Russell Bilton , David Wesley Ball, JR. , Brian Michael Gallagher , Korey Frederic Rendo , Gary Cletus Mobley, JR.
发明人： Timothy Russell Bilton , David Wesley Ball, JR. , Brian Michael Gallagher , Korey Frederic Rendo , Gary Cletus Mobley, JR.
IPC分类号： F02C6/18
CPC分类号： F02C7/141 , F02C7/224 , F05D2260/213
摘要： An embodiment of the present invention takes the form of a system that uses exhaust from the combustion turbine engine to heat the fuel gas consumed by a combustion turbine engine. The benefits of the present invention include reducing the need to use a parasitic load to heat the fuel gas.
摘要翻译：本发明的实施例采用使用来自燃气涡轮发动机的排气来加热燃气涡轮发动机所消耗的燃料气体的系统的形式。本发明的优点包括减少使用寄生负载来加热燃料气体的需要。

4. 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。

5. 发明申请

US20100028140A1 HEAT PIPE INTERCOOLER FOR A TURBOMACHINE 有权
标题翻译：热管式热交换器用于涡轮发动机
公开(公告)号：US20100028140A1
公开(公告)日：2010-02-04
申请号：US12181756
申请日：2008-07-29
申请人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, JR.
发明人： Hua Zhang , Jatila Ranasinghe , David Wesley Ball, JR.
IPC分类号： F01D25/12
CPC分类号： F02C7/143 , F05D2260/208 , F05D2260/211
摘要： A turbomachine includes a compressor having an intake portion and an outlet portion. The compressor compresses air received at the intake portion to form a compressed airflow that is passed from the outlet portion. The turbomachine also includes an intercooler operatively connected downstream from the compressor. The intercooler includes a plurality of heat pipes that are configured to extract heat from the compressed airflow.
摘要翻译：涡轮机包括具有进气部分和出口部分的压缩机。压缩机压缩容纳在进气部分处的空气，以形成从出口部分通过的压缩空气流。涡轮机还包括可操作地连接在压缩机下游的中间冷却器。中间冷却器包括被配置为从压缩空气流中提取热量的多个热管。

6. 发明申请

US20100229524A1 LOW HEATING VALUE FUEL GAS BLENDING CONTROL 有权
标题翻译：低加热燃料气体混合控制
公开(公告)号：US20100229524A1
公开(公告)日：2010-09-16
申请号：US12401512
申请日：2009-03-10
申请人： Ajanta Bhatnagar , David Wesley Ball, JR. , Kelvin Rafael Estrada , John Reuben Aiton
发明人： Ajanta Bhatnagar , David Wesley Ball, JR. , Kelvin Rafael Estrada , John Reuben Aiton
IPC分类号： F02C3/20
CPC分类号： F02C9/40 , C10K3/06 , F02C3/28 , F02C9/26 , F05D2220/75 , Y02E20/16 , Y02E50/12
摘要： A method includes blending a first fuel with a second fuel in a ratio to produce a third mixed fuel. The first fuel has a first heating value, the second fuel has a second heating value, and the third mixed fuel has a third heating value. In addition, the first heating value is different than the second heating value. The method also includes feedforward controlling the third heating value of the third mixed fuel via prediction and correction of a fuel flow rate of the first and/or second fuels to adjust the ratio of the first and second fuels based at least in part on a comparison between a measurement and a target for the third heating value.
摘要翻译：一种方法包括以一定比例混合第一燃料和第二燃料以产生第三混合燃料。第一燃料具有第一加热值，第二燃料具有第二加热值，第三混合燃料具有第三加热值。此外，第一加热值不同于第二加热值。该方法还包括通过预测和校正第一和/或第二燃料的燃料流量来控制第三混合燃料的第三热值的前馈，以至少部分地基于比较来调节第一和第二燃料的比率在第三加热值的测量和目标之间。

7. 发明申请

US20100054926A1 SYSTEM AND METHOD FOR THERMAL MANAGEMENT OF A GAS TURBINE INLET 审中-公开
标题翻译：一种气体涡轮机入口热管理系统及方法
公开(公告)号：US20100054926A1
公开(公告)日：2010-03-04
申请号：US12201491
申请日：2008-08-29
申请人： Hua Zhang , David Wesley Ball, JR.
发明人： Hua Zhang , David Wesley Ball, JR.
IPC分类号： F02C7/141
CPC分类号： F02C7/10
摘要： A thermal management system includes: a turbine assembly including an inlet housing, a compressor in fluid communication with the inlet housing, a power turbine in fluid communication with the compressor, and an exhaust assembly in fluid communication with the power turbine; and at least one heat pipe having a first portion disposed in thermal communication with the inlet housing and a second portion disposed in thermal communication with the exhaust assembly, the at least one heat pipe configured to transfer thermal energy from the exhaust assembly to at least one of input gas entering the inlet housing and at least one component of the inlet housing.
摘要翻译：热管理系统包括：涡轮组件，其包括入口壳体，与入口壳体流体连通的压缩机，与压缩机流体连通的动力涡轮机和与动力涡轮机流体连通的排气组件; 以及至少一个热管，其具有设置成与所述入口壳体热连通的第一部分和设置成与所述排气组件热连通的第二部分，所述至少一个热管被配置为将热能从所述排气组件传递到至少一个输入气体进入入口壳体和入口壳体的至少一个部件。

8. 发明申请

US20100018180A1 APPARATUS AND METHOD FOR COOLING TURBOMACHINE EXHAUST GAS 有权
标题翻译：用于冷却涡轮机排气的装置和方法
公开(公告)号：US20100018180A1
公开(公告)日：2010-01-28
申请号：US12177919
申请日：2008-07-23
申请人： Hua Zhang , David Wesley Ball, JR. , Thomas Francis Taylor
发明人： Hua Zhang , David Wesley Ball, JR. , Thomas Francis Taylor
IPC分类号： F02C7/141
CPC分类号： F01D25/30 , F01N3/05 , F02C6/00 , F05D2250/232 , F05D2260/601 , F05D2270/082
摘要： Disclosed is a turbomachine including at least one exhaust pathway along which exhaust is directed and released to ambient and at least one exhaust processor capable of removing regulated substances from the exhaust. One or more ambient air inlets are located at the at least one exhaust pathway upstream of the at least one exhaust processor. The at least one exhaust pathway is configured such that ambient air is capable of being urged into the at least one exhaust pathway through the one or more ambient air inlets by an acceleration of the exhaust along the at least one exhaust pathway. The ambient air urged into the at least one exhaust pathway reduces a temperature of the exhaust to increase effectiveness of the at least one exhaust processor. Further disclosed is a method for releasing turbomachine exhaust to ambient.
摘要翻译：公开了一种涡轮机，其包括至少一个排气通道，排气被引导并释放到环境中，并且至少一个排气处理器能够从排气中去除受调节的物质。一个或多个环境空气入口位于至少一个废气处理器上游的至少一个排气路径处。至少一个排气通道被构造成使得环境空气能够通过沿着至少一个排气通道的排气的加速被推入通过一个或多个环境空气入口的至少一个排气通道中。被推入至少一个排气通道中的环境空气降低了排气的温度，以提高至少一个废气处理器的有效性。进一步公开了一种将涡轮机排气释放到环境中的方法。

9. 发明申请

US20120117977A1 METHOD AND SYSTEM FOR CONTROLLING A SET POINT FOR EXTRACTING AIR FROM A COMPRESSOR TO PROVIDE TURBINE COOLING AIR IN A GAS TURBINE 有权
标题翻译：用于控制从压缩机提取空气以在气体涡轮机中提供涡轮冷却空气的设定点的方法和系统
公开(公告)号：US20120117977A1
公开(公告)日：2012-05-17
申请号：US12120621
申请日：2008-05-14
申请人： Priscilla Childers , Mark Disch , Curtis Newton, III , David Wesley Ball, JR. , Kenneth Neil Whaling , Alan Meier Truesdale
发明人： Priscilla Childers , Mark Disch , Curtis Newton, III , David Wesley Ball, JR. , Kenneth Neil Whaling , Alan Meier Truesdale
IPC分类号： F02C6/08
CPC分类号： F02C9/18 , F02C6/08 , F02C7/18
摘要： A method for controlling the generation of turbine cooling air from air extracted from a compressor of a gas turbine including: extracting compressed air from a low pressure and a high pressure stage of the compressor; adding in an ejector the compressed air from the low pressure stage to the air from the high pressure stage and discharging the combined air as turbine cooling air; bypassing the ejector with a bypass portion of the extracted compressed air from the high pressure stage; in response to turning on the flow of extracted compressed air from the low pressure stage, changing a set point for an actual pressure ratio that includes a pressure of the turbine cooling air, and adjusting the bypass flow in response to the changed set point to cause the actual pressure ratio to approach the changed set point.
摘要翻译：一种用于控制从燃气轮机压缩机抽出的空气产生涡轮机冷却空气的方法，包括：从压缩机的低压级和高压级抽出压缩空气; 将压缩空气从低压级喷射到来自高压级的空气并将组合的空气作为涡轮冷却空气排出; 绕过来自高压级的提取的压缩空气的旁路部分的喷射器; 响应于从低压级引起提取的压缩空气的流动，改变包括涡轮机冷却空气的压力的实际压力比的设定点，并且响应于改变的设定点来调节旁路流，导致实际压力比接近改变的设定点。

10. 发明申请

US20110056212A1 SYSTEM AND METHOD FOR APPLYING ENERGY EXTERNALLY FOR FUEL GAS FOR DEW POINT HEATING IN GAS TURBINE POWER PLANT 有权
标题翻译：用于燃气涡轮发电厂柴油机加热能源的系统和方法
公开(公告)号：US20110056212A1
公开(公告)日：2011-03-10
申请号：US12556153
申请日：2009-09-09
申请人： Hua Zhang , Dean Erickson , David Wesley Ball, JR.
发明人： Hua Zhang , Dean Erickson , David Wesley Ball, JR.
IPC分类号： F02C7/26 , H05B3/06
CPC分类号： F02C7/22 , F02C3/22 , F05D2260/20 , F05D2260/85
摘要： In a gas turbine power plant, pressurized fuel gas undergoes pressure reduction and gas expansion before being provided to a gas turbine. Condensations, which can damage the turbine, can form as the fuel gas cools when the fuel gas undergoes the pressure reduction and expansion. An electric startup heater is used to superheat the fuel gas to substantially prevent the condensations from forming. The electric startup heater includes band heaters wrapped externally to a fuel gas pipe to heat the fuel gas from outside in. Compared to conventional heaters which provide superheating through internal heating elements, the electric startup heater reduces costs and provides increased safety, flexibility, operational efficiency and ability to adapt to varying fuel gas characteristics.
摘要翻译：在燃气轮机发电厂中，加压燃料气体在提供给燃气轮机之前经历减压和气体膨胀。当燃料气体经历减压和膨胀时，当燃料气体冷却时，可能形成可能损坏涡轮机的冷凝物。使用电启动加热器来使燃料气体过热，从而基本上防止冷凝物形成。电启动加热器包括从外部包裹的燃气管道的带式加热器，以从外部加热燃料气体。与通过内部加热元件提供过热的常规加热器相比，电启动加热器降低成本并提供增加的安全性，灵活性，运行效率以及适应不同燃料气体特性的能力。

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