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1. 发明授权

US08806849B2 System and method of operating a power generation system with an alternative working fluid 有权
标题翻译：用替代工作流体操作发电系统的系统和方法
公开(公告)号：US08806849B2
公开(公告)日：2014-08-19
申请号：US12182837
申请日：2008-07-30
申请人： John Frederick Ackerman , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
发明人： John Frederick Ackerman , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
IPC分类号： F02C3/34 , F02C6/00 , F02C6/18
CPC分类号： F02C3/34
摘要： A method of operating a turbine engine system and a turbine engine system are provided. The method comprises supplying a flow of oxygen to a combustion chamber defined within a plurality of turbines coupled serially together within the turbine engine system, supplying a flow of hydrocarbonaccous fuel to the combustion chambers of each of the plurality of turbines in the turbine engine system, and supplying a working fluid to an inlet of a first turbine engine coupled within the turbine engine system, wherein the working fluid is substantially nitrogen-free and wherein each of the turbines coupled within the turbine engine system is operable with the resulting fuel-oxygen-working fluid mixture.
摘要翻译：提供了一种操作涡轮发动机系统和涡轮发动机系统的方法。该方法包括向在涡轮发动机系统内串联连接的多个涡轮机内限定的燃烧室供应氧气流，向涡轮发动机系统中的多个涡轮机的每一个的燃烧室供应烃类燃料流，以及将工作流体供应到耦合在所述涡轮发动机系统内的第一涡轮发动机的入口，其中所述工作流体基本上是无氮的，并且其中联接在所述涡轮发动机系统内的所述涡轮机中的每一个可利用所得到的燃料 - 工作流体混合物。

2. 发明授权

US6092359A Method for carrying out chemical reactions using a turbine engine 失效
标题翻译：使用涡轮发动机进行化学反应的方法
公开(公告)号：US6092359A
公开(公告)日：2000-07-25
申请号：US917979
申请日：1997-08-27
申请人： John Frederick Ackermann , Randy Lee Lewis , William Randolph Stowell
发明人： John Frederick Ackermann , Randy Lee Lewis , William Randolph Stowell
IPC分类号： B01J10/00 , B01J12/00 , B01J14/00 , F02C6/00
CPC分类号： B01J12/007 , B01J10/007 , B01J14/005
摘要： A process for carrying out chemical reactions in the gas phase or gas-liquid phase comprises feeding the chemical reagents under pressure into the combustion chamber of a turbine engine, where they react to form a desired chemical product. The heat energy evolved in the process can be utilized through the action of the turbine to power auxiliary equipment attached to the turbine engine, such as an electrical generator. In another embodiment, the turbine engine is utilized to carry out at least two reactions: a primary reaction which occurs in the combustion chamber of the engine, and a second reaction which occurs in an augmentor-section of the engine, utilizing the product of the primary reaction as a reagent in the production of a final product.
摘要翻译：在气相或气 - 液相中进行化学反应的方法包括将压力下的化学试剂进料到涡轮发动机的燃烧室中，在那里它们反应以形成所需的化学产品。在该过程中演化的热能可以通过涡轮机的作用来利用附接到涡轮发动机的辅助设备，例如发电机。在另一个实施例中，涡轮发动机用于执行至少两个反应：在发动机的燃烧室中发生的初级反应，以及发生在发动机的增压器部分中的第二反应，利用作为最终产品生产中的试剂的初级反应。

3. 发明申请

US20100024433A1 SYSTEM AND METHOD OF OPERATING A GAS TURBINE ENGINE WITH AN ALTERNATIVE WORKING FLUID 审中-公开
标题翻译：具有替代工作流体的气体涡轮发动机的系统和方法
公开(公告)号：US20100024433A1
公开(公告)日：2010-02-04
申请号：US12182842
申请日：2008-07-30
申请人： John Frederick Ackermann , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
发明人： John Frederick Ackermann , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
IPC分类号： F02C3/00 , F02C7/12
CPC分类号： F02C3/22 , F02C3/34 , F05D2260/61
摘要： A gas turbine engine system is provided. The gas turbine engine system includes a gas turbine engine, an exhaust gas conditioning system, and a sequestration chamber. The gas turbine engine includes at least one compressor, at least one combustion chamber downstream from the compressor, and at least one turbine downstream from the combustion chamber. The combustion chamber is coupled in flow communication to a source of hydrocarbonaceous fuel and to a source of oxygen. The gas turbine engine is operable with a working fluid that is substantially nitrogen-free. The exhaust gas conditioning system is coupled between a discharge outlet and an inlet of the gas turbine engine. The exhaust gas conditioning system receives all of the exhaust discharged from the gas turbine engine. The sequestration chamber stores carbon dioxide and is coupled to the gas turbine engine for receiving working fluid bled from the turbine upstream from combustion chamber.
摘要翻译：提供燃气涡轮发动机系统。燃气涡轮发动机系统包括燃气涡轮发动机，废气调节系统和隔离室。燃气涡轮发动机包括至少一个压缩机，在压缩机下游的至少一个燃烧室和从燃烧室下游的至少一个涡轮机。燃烧室与烃类燃料源和氧气源流连通地联接。燃气涡轮发动机可操作与基本上无氮的工作流体。排气调节系统联接在排气出口和燃气涡轮发动机的入口之间。废气调节系统接收从燃气涡轮发动机排出的所有废气。隔离室存储二氧化碳并且联接到燃气涡轮发动机，用于接收从燃烧室上游的涡轮机排出的工作流体。

4. 发明申请

US20100024378A1 SYSTEM AND METHOD OF OPERATING A GAS TURBINE ENGINE WITH AN ALTERNATIVE WORKING FLUID 审中-公开
标题翻译：具有替代工作流体的气体涡轮发动机的系统和方法
公开(公告)号：US20100024378A1
公开(公告)日：2010-02-04
申请号：US12182898
申请日：2008-07-30
申请人： John Frederick Ackermann , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
发明人： John Frederick Ackermann , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
IPC分类号： F02C7/141
CPC分类号： F02C3/34 , B01D2256/22 , B01D2257/80 , F02C3/20 , F05D2210/12
摘要： A gas turbine engine system is provided. The gas turbine engine system includes a gas turbine engine and an exhaust gas conditioning system. The gas turbine engine includes at least one combustion chamber and at least one turbine downstream from the combustion chamber. The combustion chamber is coupled in flow communication to a source of hydrocarbonaceous fuel and to a source of oxygen. The gas turbine engine is operable with a working fluid that is substantially nitrogen-free. The exhaust gas conditioning system is coupled between a discharge outlet of the gas turbine engine and an inlet of the gas turbine engine.
摘要翻译：提供燃气涡轮发动机系统。燃气涡轮发动机系统包括燃气涡轮发动机和排气调节系统。燃气涡轮发动机包括至少一个燃烧室和在燃烧室下游的至少一个涡轮机。燃烧室与烃类燃料源和氧气源流连通地联接。燃气涡轮发动机可操作与基本上无氮的工作流体。废气调节系统联接在燃气涡轮发动机的排出口和燃气涡轮发动机的入口之间。

5. 发明授权

US07251941B2 Ablative afterburner 有权
标题翻译：烧蚀助燃剂
公开(公告)号：US07251941B2
公开(公告)日：2007-08-07
申请号：US10797212
申请日：2004-03-10
申请人： John Michael Koshoffer , Randy Lee Lewis
发明人： John Michael Koshoffer , Randy Lee Lewis
IPC分类号： F02K3/11
CPC分类号： F02K3/10 , F02K1/06 , F02K1/822 , F02K9/10 , F02K9/974 , F23M5/00 , F23R3/20
摘要： An afterburner includes an exhaust duct with a fixed area outer nozzle at an aft end thereof, and an ablative inner nozzle therein. The smaller inner nozzle is consumed during reheat operation to expose the larger outer nozzle for increased propulsion thrust.
摘要翻译：加力燃烧器包括在其后端具有固定区域外部喷嘴的排气管道和其中的消融内部喷嘴。在再热操作期间消耗较小的内部喷嘴以暴露较大的外部喷嘴以增加推进推力。

6. 发明申请

US20100024381A1 SYSTEM AND METHOD OF OPERATING A POWER GENERATION SYSTEM WITH AN ALTERNATIVE WORKING FLUID 有权
标题翻译：具有替代工作流体的发电系统的操作系统和方法
公开(公告)号：US20100024381A1
公开(公告)日：2010-02-04
申请号：US12182837
申请日：2008-07-30
申请人： John Frederick Ackermann , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
发明人： John Frederick Ackermann , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
IPC分类号： F02C6/02
CPC分类号： F02C3/34
摘要： A method of operating a turbine engine system and a turbine engine system are provided. The method comprises supplying a flow of oxygen to a combustion chamber defined within a plurality of turbines coupled serially together within the turbine engine system, supplying a flow of hydrocarbonaccous fuel to the combustion chambers of each of the plurality of turbines in the turbine engine system, and supplying a working fluid to an inlet of a first turbine engine coupled within the turbine engine system, wherein the working fluid is substantially nitrogen-free and wherein each of the turbines coupled within the turbine engine system is operable with the resulting fuel-oxygen-working fluid mixture.
摘要翻译：提供了一种操作涡轮发动机系统和涡轮发动机系统的方法。该方法包括向在涡轮发动机系统内串联连接的多个涡轮机内限定的燃烧室供应氧气流，向涡轮发动机系统中的多个涡轮机的每一个的燃烧室供应烃类燃料流，以及将工作流体供应到耦合在所述涡轮发动机系统内的第一涡轮发动机的入口，其中所述工作流体基本上是无氮的，并且其中联接在所述涡轮发动机系统内的所述涡轮机中的每一个可利用所得到的燃料 - 工作流体混合物。

7. 发明授权

US08726670B2 Ejector purge of cavity adjacent exhaust flowpath 有权
标题翻译：喷射器吹扫腔邻近排气流路
公开(公告)号：US08726670B2
公开(公告)日：2014-05-20
申请号：US12822519
申请日：2010-06-24
申请人： Frank Gerald Bachman , Randy Lee Lewis , Robert Steven Bockwich , Shane Bunnag
发明人： Frank Gerald Bachman , Randy Lee Lewis , Robert Steven Bockwich , Shane Bunnag
IPC分类号： F02K3/10
CPC分类号： F23R3/18 , F02K1/822 , F23R3/06 , F23R2900/03044 , Y02T50/675
摘要： A gas turbine engine augmentor includes an inter-liner cavity including an axially extending annular gap separating augmentor and tailpipe liners. A purge flow cavity is in fluid communication with a fan bypass duct and with the cavity. An ejector in fluid communication with the bypass duct includes an ejector nozzle positioned and aimed to direct an ejector nozzle flow from inside the ejector nozzle across the cavity. The purge flow cavity may be bifurcated into forward and aft purge flow cavities which are in fluid communication with the ejector and inter-liner cavity respectively. An annular dividing wall having ejector metering apertures may be disposed between the forward purge flow cavity and an ejector plenum of the ejector. An annular trapped vortex cavity pilot may be located upstream of the annular gap. The aft purge flow cavity may be outwardly bounded by a seal having purge metering apertures disposed therethrough.
摘要翻译：燃气涡轮发动机增压器包括内衬腔，其包括分离增压器和排气管线的轴向延伸的环形间隙。吹扫流动空腔与风扇旁路管道和空腔流体连通。与旁路管道流体连通的喷射器包括喷射器喷嘴，喷射器喷嘴被定位并且旨在引导喷射器喷嘴从喷射器喷嘴内部流过空腔。吹扫流动腔可以分叉成分别与喷射器和内衬空腔流体连通的向前和向后吹扫流动空腔。具有喷射器计量孔的环形分隔壁可以设置在前吹扫流动空腔和喷射器的喷射器气室之间。环形捕获涡流腔引导件可以位于环形间隙的上游。后吹扫流动腔可以通过具有穿过其设置的清洗计量孔的密封件向外限定。

8. 发明申请

US20110315789A1 EJECTOR PURGE OF CAVITY ADJACENT EXHAUST FLOWPATH 有权
标题翻译：排气孔排气流程
公开(公告)号：US20110315789A1
公开(公告)日：2011-12-29
申请号：US12822519
申请日：2010-06-24
申请人： Frank Gerald Bachman , Randy Lee Lewis , Robert Steven Bockwich , Shane Bunnag
发明人： Frank Gerald Bachman , Randy Lee Lewis , Robert Steven Bockwich , Shane Bunnag
IPC分类号： B63H25/46
CPC分类号： F23R3/18 , F02K1/822 , F23R3/06 , F23R2900/03044 , Y02T50/675
摘要： A gas turbine engine augmentor includes an inter-liner cavity including an axially extending annular gap separating augmentor and tailpipe liners. A purge flow cavity is in fluid communication with a fan bypass duct and with the cavity. An ejector in fluid communication with the bypass duct includes an ejector nozzle positioned and aimed to direct an ejector nozzle flow from inside the ejector nozzle across the cavity. The purge flow cavity may be bifurcated into forward and aft purge flow cavities which are in fluid communication with the ejector and inter-liner cavity respectively. An annular dividing wall having ejector metering apertures may be disposed between the forward purge flow cavity and an ejector plenum of the ejector. An annular trapped vortex cavity pilot may be located upstream of the annular gap. The aft purge flow cavity may be outwardly bounded by a seal having purge metering apertures disposed therethrough.
摘要翻译：燃气涡轮发动机增压器包括内衬腔，其包括分离增压器和排气管的轴向延伸的环形间隙。吹扫流动空腔与风扇旁路管道和空腔流体连通。与旁路管道流体连通的喷射器包括喷射器喷嘴，喷射器喷嘴被定位并且旨在引导喷射器喷嘴从喷射器喷嘴内部流过空腔。吹扫流动腔可以分叉成分别与喷射器和内衬空腔流体连通的向前和向后吹扫流动空腔。具有喷射器计量孔的环形分隔壁可以设置在前吹扫流动空腔和喷射器的喷射器气室之间。环形捕获涡流腔引导件可以位于环形间隙的上游。后吹扫流动腔可以通过具有穿过其设置的清洗计量孔的密封件向外限定。

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