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。

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。

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。

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。