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1. 发明申请

US20040148942A1 Method for catalytic combustion in a gas- turbine engine, and applications thereof 审中-公开
标题翻译：燃气涡轮发动机中的催化燃烧方法及其应用
公开(公告)号：US20040148942A1
公开(公告)日：2004-08-05
申请号：US10355145
申请日：2003-01-31
申请人： Capstone Turbine Corporation
发明人： Guillermo Pont , Douglas A. Hamrin , Gregory C. Rouse
IPC分类号： F23R003/40
CPC分类号： F23L15/04 , F02C9/28 , F23N1/02 , F23N5/003 , F23N2023/04 , F23N2023/08 , F23N2041/20 , F23R3/40 , F23R2900/00002 , Y02E20/348 , Y02T50/677
摘要： The present invention provides a method for sustained catalytic combustion of low BTU fuels in a gas-turbine engine, and applications thereof. The method comprises ingesting fuel and combustion air into a catalytic reactor to produce thermal energy and converting the thermal energy to mechanical energy with a turbine. The fuel and the combustion air are mixed to form a fuel-air mixture. The ingested combustion air is used to oxidize the ingested fuel. Fuels having a higher heating value in a range of between 1000 and 5 BTU/scf are mixed with the combustion air and oxidized using the catalytic reactor.
摘要翻译：本发明提供了一种用于燃气涡轮发动机中的低BTU燃料的持续催化燃烧的方法及其应用。该方法包括将燃料和燃烧空气吸入催化反应器以产生热能并将热能转化为具有涡轮的机械能。燃料和燃烧空气混合以形成燃料 - 空气混合物。摄入的燃烧空气用于氧化摄入的燃料。在1000至5BTU / scf范围内具有较高热值的燃料与燃烧空气混合并使用催化反应器进行氧化。

2. 发明申请

US20040160061A1 Gas-turbine engine with catalytic reactor 审中-公开
标题翻译：带催化反应器的燃气轮机
公开(公告)号：US20040160061A1
公开(公告)日：2004-08-19
申请号：US10355142
申请日：2003-01-31
申请人： Capstone Turbine Corporation
发明人： Gregory C. Rouse , Douglas A. Hamrin , Guillermo Pont
IPC分类号： H02P009/04
CPC分类号： F02C9/28 , F02C3/22 , F02C7/08 , F05D2260/85 , F05D2270/02 , F05D2270/303 , F05D2270/304
摘要： The present invention provides a gas-turbine engine and a combustion system that include a catalytic reactor and a turbine. The catalytic reactor oxidizes low BTU fuel to generate thermal energy. The turbine converts the thermal energy produced by the catalytic reactor into mechanical energy. This mechanical energy can be used, for example, to produce electricity. The gas-turbine engine and the catalytic combustion system are capable of oxidizing fuels having a higher heating value in a range of between 1000 and 5 BTU/scf.
摘要翻译：本发明提供一种燃气轮机发动机和包括催化反应器和涡轮机的燃烧系统。催化反应器氧化低BTU燃料以产生热能。涡轮机将由催化反应器产生的热能转化为机械能。这种机械能可以用于例如发电。燃气涡轮发动机和催化燃烧系统能够将具有在1000和5BTU / scf之间的范围内的较高热值的燃料氧化。

3. 发明申请

US20020066270A1 Generated system bottoming cycle 有权
标题翻译：生成系统底循环
公开(公告)号：US20020066270A1
公开(公告)日：2002-06-06
申请号：US09985789
申请日：2001-11-06
申请人： CAPSTONE TURBINE CORPORATION
发明人： Gregory C. Rouse , Bill Treece , Jeff Willis , David Calta
IPC分类号： F01K013/00 , F01K001/00
CPC分类号： F01K23/10 , F01K25/08 , F02C6/18
摘要： A closed loop Rankine bottoming cycle including a heat exchanger coupled to an exhaust port of a first turbogenerator for heating a pressurized refrigerant into a gaseous phase, and a second turbogenerator (e.g., a turbo expander) coupled to the heat exchanger for expanding the gaseous phase so as to create power. Also included is a cooling mechanism coupled to an exhaust of the second turbogenerator for cooling the gaseous phase exhausted by the second turbogenerator into a liquid phase, and a pumping mechanism for pressurizing the liquid phase into the pressurized refrigerant heated by the heat exchanger. A computer program product and method for operating and synchronizing the generator included in the closed loop, so as to optimize the overall system efficiency is also included.
摘要翻译：封闭回路兰金底循环，包括耦合到第一涡轮发电机的排气口的热交换器，用于将加压制冷剂加热成气相;以及第二涡轮发电机（例如，涡轮膨胀机），其连接到热交换器，用于使气相膨胀以创造权力。还包括与第二涡轮发电机的排气相连的冷却机构，用于将由第二涡轮发电机排出的气相冷却成液相;以及泵送机构，用于将液相加压到由热交换器加热的加压制冷剂中。还包括用于操作和同步闭环中包括的发电机的计算机程序产品和方法，以便优化整个系统效率。

4. 发明申请

US20030110773A1 Generated system bottoming cycle 审中-公开
公开(公告)号：US20030110773A1
公开(公告)日：2003-06-19
申请号：US10358060
申请日：2003-02-04
申请人： Capstone Turbine Corporation
发明人： Gregory C. Rouse , Bill Treece , Jeff Willis , David Calta
IPC分类号： F01K001/00 , F01K013/00
CPC分类号： F01K23/10 , F01K25/08 , F02C6/18
摘要： A closed loop Rankine bottoming cycle including a heat exchanger coupled to an exhaust port of a first turbogenerator for heating a pressurized refrigerant into a gaseous phase, and a second turbogenerator (e.g., a turbo expander) coupled to the heat exchanger for expanding the gaseous phase so as to create power. Also included is a cooling mechanism coupled to an exhaust of the second turbogenerator for cooling the gaseous phase exhausted by the second turbogenerator into a liquid phase, and a pumping mechanism for pressurizing the liquid phase into the pressurized refrigerant heated by the heat exchanger. A computer program product and method for operating and synchronizing the generator included in the closed loop, so as to optimize the overall system efficiency is also included.

5. 发明申请

US20020096393A1 Turbogenerator exhaust silencer 审中-公开
标题翻译：涡轮发电机排气消音器
公开(公告)号：US20020096393A1
公开(公告)日：2002-07-25
申请号：US09985435
申请日：2001-11-02
申请人： CAPSTONE TURBINE CORPORATION
发明人： Gregory C. Rouse
IPC分类号： F01N007/00
CPC分类号： F01N13/08 , F01D25/30 , F01N1/24 , F01N13/085 , F02K1/40 , F02K1/827 , F05D2220/32 , F05D2250/70 , F05D2260/96
摘要： An exhaust silencing device and method for silencing a turbogenerator includes a housing, an intake manifold, at least two exhaust outlet ports and flow channels which extend in a bifurcated path from the intake manifold to the exhaust outlet ports and which provide a length to height (or diameter) ratio permitting a compact fluid flow profile.
摘要翻译：用于消音涡轮发电机的排气消音装置和方法包括壳体，进气歧管，至少两个排气出口和流动通道，其在从进气歧管到排气出口端口的分叉路径中延伸，并且提供长度到高度或直径）比允许紧凑的流体流动分布。

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