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1. 再颁专利

USRE38815E1 Method and apparatus for the destruction of volatile organic compounds 失效
标题翻译：用于破坏挥发性有机化合物的方法和装置
公开(公告)号：USRE38815E1
公开(公告)日：2005-10-11
申请号：US10008676
申请日：2001-12-06
申请人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
发明人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
IPC分类号： F02C3/20 , F02C7/00 , F23G5/46 , F23G7/06
CPC分类号： F23G5/46 , F02C3/20 , F23G7/065 , F23G2209/142 , Y02E20/12
摘要： A system for the destruction of volatile organic compounds while generating power. In a preferred embodiment the system comprises a combustor and a reaction chamber connected to an exit of the combustor. A primary inlet to the combustor supplies a primary fuel to the combustor. A secondary fuel, comprising air and an amount of one or more volatile organic compounds, is supplied to a compressor, which compresses the secondary fuel and directs the secondary fuel to the combustor and the reaction chamber. The system is suitably configured to enable the stoichiometric reaction of the two fuels in a manner sufficient to destroy the volatile organic compounds contained in the secondary fuel and power a turbine engine connected to an exit of the reaction chamber.
摘要翻译：用于在发电时破坏挥发性有机化合物的系统。在优选实施例中，系统包括连接到燃烧器的出口的燃烧器和反应室。燃烧器的主入口向燃烧器提供主要燃料。包含空气和一定量的一种或多种挥发性有机化合物的二次燃料被供应到压缩机，压缩机压缩二次燃料并将二次燃料引导到燃烧器和反应室。该系统适当地构造成使得能够以足以破坏二次燃料中所含的挥发性有机化合物的方式来实现两种燃料的化学计量反应，并为连接到反应室的出口的涡轮发动机供电。

2. 发明授权

US5832713A Method and apparatus for the destruction of volatile organic compounds 失效
公开(公告)号：US5832713A
公开(公告)日：1998-11-10
申请号：US864592
申请日：1997-05-28
申请人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
发明人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
IPC分类号： F02C3/20 , F02C7/00 , F23G5/46 , F23G7/06
CPC分类号： F23G5/46 , F02C3/20 , F23G7/065 , F23G2209/142 , Y02E20/12
摘要： A system for the destruction of volatile organic compounds while generating power. In a preferred embodiment the system comprises a combustor and a reaction chamber connected to an exit of the combustor. A primary inlet to the combustor supplies a primary fuel to the combustor. A secondary fuel, comprising air and an amount of one or more volatile organic compounds, is supplied to a compressor, which compresses the secondary fuel and directs the secondary fuel to the combustor and the reaction chamber. The system is suitably configured to enable the stoichiometric reaction of the two fuels in a manner sufficient to destroy the volatile organic compounds contained in the secondary fuel and power a turbine engine connected to an exit of the reaction chamber.

3. 再颁专利

USRE38784E1 Apparatus for the destruction of volatile organic compounds 失效
标题翻译：用于破坏挥发性有机化合物的装置
公开(公告)号：USRE38784E1
公开(公告)日：2005-08-30
申请号：US10010043
申请日：2001-12-06
申请人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
发明人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
IPC分类号： F02C3/20 , F02C7/00 , F23G5/46 , F23G7/06
CPC分类号： F23G5/46 , F02C3/20 , F23G7/065 , F23G2209/142 , Y02E20/12
摘要： A system for the destruction of volatile organic compounds while generating power. In a preferred embodiment the system comprises a combustor and a reaction chamber connected to an exit of the combustor. A primary inlet to the combustor supplies a primary fuel to the combustor. A secondary fuel, comprising air and an amount of one or more volatile organic compounds, is supplied to a compressor, which compresses the secondary fuel and directs the secondary fuel to the combustor and the reaction chamber. The system is suitably configured to enable the stoichiometric reaction of the two fuels in a manner sufficient to destroy the volatile organic compounds contained in the secondary fuel and power a turbine engine connected to an exit of the reaction chamber.
摘要翻译：用于在发电时破坏挥发性有机化合物的系统。在优选实施例中，系统包括连接到燃烧器的出口的燃烧器和反应室。燃烧器的主入口向燃烧器提供主要燃料。包含空气和一定量的一种或多种挥发性有机化合物的二次燃料被供应到压缩机，压缩机压缩二次燃料并将二次燃料引导到燃烧器和反应室。该系统适当地构造成使得能够以足以破坏二次燃料中所含的挥发性有机化合物的方式来实现两种燃料的化学计量反应，并为连接到反应室的出口的涡轮发动机供电。

4. 发明授权

US5673553A Apparatus for the destruction of volatile organic compounds 失效
标题翻译：用于破坏挥发性有机化合物的装置
公开(公告)号：US5673553A
公开(公告)日：1997-10-07
申请号：US538308
申请日：1995-10-03
申请人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
发明人： Luis R. Maese , Ram Srinivasan , Stephen R. Thomas
IPC分类号： F02C3/20 , F02C7/00 , F23G5/46 , F23G7/06
CPC分类号： F23G5/46 , F02C3/20 , F23G7/065 , F23G2209/142 , Y02E20/12
摘要： A system for the destruction of volatile organic compounds while generating power. In a preferred embodiment the system comprises a combustor and a reaction chamber connected to an exit of the combustor. A primary inlet to the combustor supplies a primary fuel to the combustor. A secondary fuel, comprising air and an amount of one or more volatile organic compounds, is supplied to a compressor, which compresses the secondary fuel and directs the secondary fuel to the combustor and the reaction chamber. The system is suitably configured to enable the stoichiometric reaction of the two fuels in a manner sufficient to destroy the volatile organic compounds contained in the secondary fuel and power a turbine engine connected to an exit of the reaction chamber.
摘要翻译：用于在发电时破坏挥发性有机化合物的系统。在优选实施例中，系统包括连接到燃烧器的出口的燃烧器和反应室。燃烧器的主入口向燃烧器提供主要燃料。将包含空气和一定量的一种或多种挥发性有机化合物的二次燃料供应到压缩机，压缩机压缩二次燃料并将二次燃料引导到燃烧器和反应室。该系统适当地构造成使得能够以足以破坏二次燃料中所含的挥发性有机化合物的方式来实现两种燃料的化学计量反应，并为连接到反应室的出口的涡轮发动机供电。

5. 发明授权

US5237663A Low cost diagnostic/configuration interface 失效
标题翻译：低成本诊断/配置界面
公开(公告)号：US5237663A
公开(公告)日：1993-08-17
申请号：US675238
申请日：1991-03-26
申请人： Ram Srinivasan
发明人： Ram Srinivasan
IPC分类号： G06F3/023 , G06F13/38 , H04B10/00
CPC分类号： H04B10/801 , G06F13/385 , G06F3/0231
摘要： A computing system has a wireless interface, for example an infrared interface. The infrared interface is used to directly transmit configuration information to and/or receive configuration from a configuration storage device without going through the standard I/O interfaces of the computing system. This is done by connecting the infrared interface directly to the configuration storage device. Alternately, the infrared interface is used to allow direct connection to a memory bus without using an I/O bus. This allows the computing system to send out diagnostic information without using the I/O bus. The infrared interface can be full duplex allowing requests for diagnostic information to be made by a handheld computing system such as a handheld computer or a calculator. The infrared interface may also be used to download data and programming code to a handheld computing system and for receiving data from the handheld computing system.
摘要翻译：计算系统具有无线接口，例如红外接口。红外线接口用于直接从配置存储设备传送配置信息和/或从配置存储设备接收配置，而无需通过计算系统的标准I / O接口。这通过将红外接口直接连接到配置存储设备来实现。或者，红外线接口用于在不使用I / O总线的情况下直接连接到存储器总线。这允许计算系统在不使用I / O总线的情况下发送诊断信息。红外线接口可以是全双工的，允许由诸如手持计算机或计算器的手持计算系统进行诊断信息的请求。红外线接口还可用于将数据和编程代码下载到手持计算系统并用于从手持计算系统接收数据。

6. 发明授权

US06374615B1 Low cost, low emissions natural gas combustor 失效
标题翻译：低成本，低排放天然气燃烧器
公开(公告)号：US06374615B1
公开(公告)日：2002-04-23
申请号：US09493646
申请日：2000-01-28
申请人： Frank J. Zupanc , Rudolph Dudebout , John J. Lipinski , Ram Srinivasan
发明人： Frank J. Zupanc , Rudolph Dudebout , John J. Lipinski , Ram Srinivasan
IPC分类号： F02C100
CPC分类号： F23R3/286 , F23R3/14 , F23R3/343
摘要： A combustor dome for use in a combustor has an igniter mounted in a central bore. Moving outward from the bore is a concentric pilot fuel passageway. Concentric about the pilot fuel passageway is an air passageway. Lastly, concentric about the air passageway is a premix passageway. The outlets of the pilot fuel passageway, the air passageway, and the premix passageway are generally coplanar.
摘要翻译：用于燃烧器的燃烧器穹顶具有安装在中心孔中的点火器。从钻孔向外移动是一个同心的导向燃料通道。关于飞行员燃料通道的同心是空气通道。最后，与空气通道同心的是预混通道。导向燃料通道，空气通道和预混通道的出口通常是共面的。

7. 发明申请

US20080066468A1 Splash plate dome assembly for a turbine engine 有权
标题翻译：用于涡轮发动机的飞溅板式圆顶组件
公开(公告)号：US20080066468A1
公开(公告)日：2008-03-20
申请号：US11898679
申请日：2007-09-14
申请人： Les Faulder , Mario Abreu , Ram Srinivasan , Michael Lane
发明人： Les Faulder , Mario Abreu , Ram Srinivasan , Michael Lane
IPC分类号： F02C1/00
CPC分类号： F23R3/002 , F23R3/10 , F23R3/283 , F23R2900/03044
摘要： A splash plate dome assembly for a combustion liner of a turbine engine is disclosed. The splash plate may include an outer periphery having a plurality of corners and an inner periphery defining an aperture and an annular flange. The splash plate may include a plurality of first flow guides extending from the outer periphery to the inner periphery. The splash plate may further include a plurality of second flow guides extending from the outer periphery to a location intermediate the inner periphery and the outer periphery. The splash plate, annular flange, first flow guides, and second flow guides may be integrally formed by casting. The splash plate may be mounted to a combustion dome having a plurality of distributed through holes for forming impingement jets on an upstream face of the splash plate.
摘要翻译：公开了一种用于涡轮发动机的燃烧衬套的飞溅板圆顶组件。溅溅板可以包括具有多个拐角的外周边和限定孔的内周边和环形凸缘。溅溅板可以包括从外周延伸到内周的多个第一流动引导件。溅溅板还可以包括多个第二流动引导件，该第二流动引导件从外周边延伸到内周边和外周边之间的位置。溅溅板，环形凸缘，第一流动引导件和第二流动引导件可以通过铸造一体地形成。飞溅板可以安装到具有多个分布通孔的燃烧穹顶上，用于在飞溅板的上游面上形成冲击射流。

8. 发明授权

US06286300B1 Combustor with fuel preparation chambers 有权
标题翻译：带燃料准备室的燃烧器
公开(公告)号：US06286300B1
公开(公告)日：2001-09-11
申请号：US09492678
申请日：2000-01-27
申请人： Joseph Zelina , Geoffrey D. Myers , Ram Srinivasan , Robert S. Reynolds
发明人： Joseph Zelina , Geoffrey D. Myers , Ram Srinivasan , Robert S. Reynolds
IPC分类号： F23R330
CPC分类号： F23R3/14 , Y02T50/675
摘要： An annular combustor having fuel preparation chambers mounted in the dome of the combustor. The fuel preparation chamber comprises an annular wall extending axially from an inlet to an exit that defines a mixing chamber. Mounted to the inlet are an air swirler and a fuel atomizer. The air swirler provides swirled air to the mixing chamber while the atomizer provides a fuel spray. On the downstream side of the exit, the fuel preparation chamber has an inwardly extending conical wall that compresses the swirling mixture of fuel and air exiting the mixing chamber.
摘要翻译：具有安装在燃烧器的圆顶中的燃料准备室的环形燃烧器。燃料制备室包括从入口轴向延伸到限定混合室的出口的环形壁。安装到入口的是空气旋流器和燃料雾化器。空气旋流器为混合室提供旋转空气，而雾化器提供燃料喷雾。在出口的下游侧，燃料准备室具有向内延伸的锥形壁，其压缩离开混合室的燃料和空气的旋转混合物。

9. 发明申请

US20140000274A1 METHODS AND APPARATUS FOR CO-FIRING FUEL 审中-公开
标题翻译：燃烧燃料的方法和装置
公开(公告)号：US20140000274A1
公开(公告)日：2014-01-02
申请号：US13538099
申请日：2012-06-29
申请人： Ram Srinivasan , Colin John Etheridge
发明人： Ram Srinivasan , Colin John Etheridge
IPC分类号： F02C3/20
CPC分类号： F02C3/22 , F02C3/24 , F02C9/40 , F05D2220/75 , F23C2900/9901 , F23R3/36 , F23R2900/00002
摘要： A method of co-firing fuel within a gas turbine engine. The method may include injecting a first fuel into a combustion system of a gas turbine engine. The first fuel may include a high energy liquid fuel. The method may also include injecting a second fuel into the combustion system. The second fuel may include a gaseous low Wobbe fuel. Only the first fuel may be injected during a first mode of operation. The first fuel and the second fuel may be injected simultaneously and discretely during a second mode of operation.
摘要翻译：一种在燃气涡轮发动机内共燃燃料的方法。该方法可以包括将第一燃料喷射到燃气涡轮发动机的燃烧系统中。第一燃料可以包括高能液体燃料。该方法还可以包括将第二燃料喷射到燃烧系统中。第二种燃料可以包括一种低挥发性的沃博（Wobbe）燃料。在第一种操作模式下，只能喷射第一种燃料。第一燃料和第二燃料可以在第二操作模式期间同时和离散注入。

10. 发明授权

US07730725B2 Splash plate dome assembly for a turbine engine 有权
标题翻译：用于涡轮发动机的飞溅板式圆顶组件
公开(公告)号：US07730725B2
公开(公告)日：2010-06-08
申请号：US11898679
申请日：2007-09-14
申请人： Les Faulder , Mario E. Abreu , Ram Srinivasan , Michael A. Lane
发明人： Les Faulder , Mario E. Abreu , Ram Srinivasan , Michael A. Lane
IPC分类号： F23R3/50
CPC分类号： F23R3/002 , F23R3/10 , F23R3/283 , F23R2900/03044
摘要： A splash plate dome assembly for a combustion liner of a turbine engine is disclosed. The splash plate may include an outer periphery having a plurality of corners and an inner periphery defining an aperture and an annular flange. The splash plate may include a plurality of first flow guides extending from the outer periphery to the inner periphery. The splash plate may further include a plurality of second flow guides extending from the outer periphery to a location intermediate the inner periphery and the outer periphery. The splash plate, annular flange, first flow guides, and second flow guides may be integrally formed by casting. The splash plate may be mounted to a combustion dome having a plurality of distributed through holes for forming impingement jets on an upstream face of the splash plate.
摘要翻译：公开了一种用于涡轮发动机的燃烧衬套的飞溅板圆顶组件。溅溅板可以包括具有多个拐角的外周边和限定孔的内周边和环形凸缘。溅溅板可以包括从外周延伸到内周的多个第一流动引导件。溅溅板还可以包括多个第二流动引导件，该第二流动引导件从外周边延伸到内周边和外周边之间的位置。溅溅板，环形凸缘，第一流动引导件和第二流动引导件可以通过铸造一体地形成。飞溅板可以安装到具有多个分布通孔的燃烧穹顶上，用于在飞溅板的上游面上形成冲击射流。

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