F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 3/22 (2006.01) F02C 3/34 (2006.01) F02C 7/12 (2006.01)
Patent
CA 2732176
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.
Linvention concerne un système de turbine à gaz (100). La turbine à gaz consiste en une turbine à gaz (10) comprenant au moins un compresseur (14, 18, 118), au moins une chambre de combustion (120) en aval du ou des compresseurs, et au moins une turbine (26, 30) en aval de la ou des chambres de combustion, la ou les chambres de combustion étant en communication d'écoulement avec une source de carburant hydrocarboné (130) et avec une source d'oxygène (132), la turbine à gaz pouvant fonctionner avec un fluide de travail (150) sensiblement non azoté, un système de conditionnement de gaz d'échappement (108) étant accouplé entre une évacuation de la turbine à gaz et une admission de la turbine à gaz, le système de conditionnement de gaz d'échappement recevant tous les gaz déchappement évacués de la turbine à gaz, et une chambre d'isolement (142) permettant de stocker du dioxyde de carbone, la chambre disolement étant accouplée à la turbine à gaz afin de recevoir un fluide de travail purgé de la turbine en amont de la ou des chambres de combustion.
Ackerman John Frederick
Argyle Morris Dee
Bell David Allen
Franer Matthew Timothy
Lewis Randy Lee
Company General Electric
Craig Wilson And Company
The University Of Wyoming
LandOfFree
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