Title:
代替作動流体でガスタービンエンジンを作動させるシステム及び方法
Document Type and Number:
Japanese Patent JP2011530033
Kind Code:
A
Abstract:
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.
Inventors:
Ackerman, John Frederick
Lewis, Randy Lee
Bell, David Allen
Argyle, Morris Dee
Brain Francis, Tauler
Freina, Matthew Timothy
Lewis, Randy Lee
Bell, David Allen
Argyle, Morris Dee
Brain Francis, Tauler
Freina, Matthew Timothy
Application Number:
JP2011521145A
Publication Date:
December 15, 2011
Filing Date:
June 24, 2009
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
The University of Wyoming
The University of Wyoming
International Classes:
F02C3/30; F02C9/16; F02C6/10; F02C9/18
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Hirokazu Ogura
Toshihisa Kurokawa