公开(公告)号：WO2010036432A3

公开(公告)日：2010-04-01

申请号：PCT/US2009/048473

申请日：2009-06-24

Applicant: GENERAL ELECTRIC COMPANY ,  THE UNIVERSITY OF WYOMING ,  ACKERMANN, John, Frederick ,  LEWIS, Randy, Lee ,  BELL, David, Allen ,  ARGYLE, Morris, Dee ,  TOWLER, Brain, Francis ,  FRANER, Matthew, Timothy

Inventor： ACKERMANN, John, Frederick ,  LEWIS, Randy, Lee ,  BELL, David, Allen ,  ARGYLE, Morris, Dee ,  TOWLER, Brain, Francis ,  FRANER, Matthew, Timothy

IPC: F02C3/22 ,  F02C3/34

Abstract: A gas turbine engine system (100) is provided. The gas turbine engine includes a gas turbine engine (10) comprising at least one compressor (14,18,118), at least one combustion chamber (22,120) downstream from the at least one compressor, and at least one turbine (26,30,122) downstream from the at least one combustion chamber, the at least one combustion chamber coupled in flow communication to a source of hydrocarbonaceous fuel (130) and to a source of oxygen (132), the gas turbine engine operable with a working fluid (150) that is substantially nitrogen-free, an exhaust gas (108) conditioning system (112) coupled between a discharge outlet of the gas turbine engine and an inlet of the gas turbine engine, the exhaust gas conditioning system receives all of the exhaust discharged from the gas turbine engine, and a sequestration chamber (142) for storing carbon dioxide, the sequestration chamber coupled to the gas turbine engine for receiving working fluid bled from the turbine upstream from the at least one combustion chamber.

公开(公告)号：WO2013163510A1

公开(公告)日：2013-10-31

申请号：PCT/US2013/038352

申请日：2013-04-26

Applicant: GENERAL ELECTRIC COMPANY

Inventor： RUTHEMEYER, Michael, Anthony ,  SENILE, Darrell, Glenn ,  RENGGLI, Bernard, James ,  LEWIS, Randy, Lee

IPC: F02K1/04 ,  F02K1/80

CPC classification number: F02C7/20 ,  F02K1/04 ,  F02K1/48 ,  F02K1/80 ,  F23R3/007 ,  Y02T50/672

Abstract: A gas turbine engine assembly includes first and second annular members (41, 48) having different first and second thermal expansion coefficients that are connected together with dual arm V brackets (50), where brackets (50) include first and second arms (62, 64) angularly spaced apart from a bracket centerline (70) and extending axially away from bracket bases (72) attached to a first one of the first and second annular members (41, 48), and arms (62, 64) are attached to a second one of the first and second annular members (41, 48).

Abstract translation: 燃气涡轮发动机组件包括具有不同的第一和第二热膨胀系数的第一和第二环形构件（41,48），其与双臂V支架（50）连接在一起，其中支架（50）包括第一和第二臂（62， 64），其与支架中心线（70）成角度地间隔开并且从附接到第一和第二环形构件（41,48）中的第一个的支架底座（72）轴向延伸并且臂（62,64）附接到 第一和第二环形构件（41,48）中的第二个。

公开(公告)号：WO2010039318A1

公开(公告)日：2010-04-08

申请号：PCT/US2009/049856

申请日：2009-07-08

Applicant: GENERAL ELECTRIC COMPANY ,  ACKERMAN, John, Frederick ,  FRANER, Matthew, Timothy ,  TOWLER, Brian, Francis ,  ARGYLE, Morris, Dee ,  BELL, David, Allen ,  LEWIS, Randy, Lee ,  THE UNIVERSITY OF WYOMING-WYOMING RESEARCH PRODUCTS CENTER

Inventor： ACKERMAN, John, Frederick ,  FRANER, Matthew, Timothy ,  TOWLER, Brian, Francis ,  ARGYLE, Morris, Dee ,  BELL, David, Allen ,  LEWIS, Randy, Lee

IPC: F02C3/34 ,  F01K21/04

CPC classification number: F02C3/34

Abstract: 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 hydrocarbonaceous 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.

Abstract translation: 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中的每一个的燃烧室供应烃类燃料， 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：WO2010014324A3

公开(公告)日：2010-02-04

申请号：PCT/US2009/048742

申请日：2009-06-26

Applicant: GENERAL ELECTRIC COMPANY ,  THE UNIVERSITY OF WYOMING ,  FRANER, Matthew, Timothy ,  LEWIS, Randy, Lee ,  BELL, David, Allen ,  ARGYLE, Morris, Dee ,  TOWLER, Brian, Francis ,  ACKERMAN, John, Frederick

Inventor： FRANER, Matthew, Timothy ,  LEWIS, Randy, Lee ,  BELL, David, Allen ,  ARGYLE, Morris, Dee ,  TOWLER, Brian, Francis ,  ACKERMAN, John, Frederick

IPC: F02C3/20 ,  F02C3/34

Abstract: 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.