09599070 is referenced by 4 patents and cites 722 patents.

A system includes a gas turbine system having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compress and supply an exhaust gas to the turbine combustor. The gas turbine system also has an exhaust gas recirculation (EGR) system. The EGR system is configured to recirculate the exhaust gas along an exhaust recirculation path from the turbine to the exhaust gas compressor. The system further includes a main oxidant compression system having one or more oxidant compressors. The one or more oxidant compressors are separate from the exhaust gas compressor, and the one or more oxidant compressors are configured to supply all compressed oxidant utilized by the turbine combustor in generating the combustion products.

Title
System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
Application Number
14/66579
Publication Number
9599070 (B2)
Application Date
October 29, 2013
Publication Date
March 21, 2017
Inventor
James A West
Liberty Township
OH, US
Todd Denman
Greenville
SC, US
Christian M Hansen
Greenville
SC, US
Samuel D Draper
Simpsonville
SC, US
Dennis M O Dea
Somerset
NJ, US
Sulabh K Dhanuka
Houston
TX, US
Loren K Starcher
Sugar Land
TX, US
Franklin F Mittricker
Jamul
CA, US
Richard A Huntington
Houston
TX, US
Agent
Fletcher Yoder P C
Assignee
ExxonMobil Upstream Research Company
TX, US
General Electric Company
NY, US
IPC
F02C 7/36
F02C 3/34
F02C 3/107
F02M 25/07
F02C 1/00
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