MX357226B - System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system. - Google Patents

System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system.

Info

Publication number
MX357226B
MX357226B MX2015005603A MX2015005603A MX357226B MX 357226 B MX357226 B MX 357226B MX 2015005603 A MX2015005603 A MX 2015005603A MX 2015005603 A MX2015005603 A MX 2015005603A MX 357226 B MX357226 B MX 357226B
Authority
MX
Mexico
Prior art keywords
exhaust gas
turbine
oxidant
gas turbine
oxidant compression
Prior art date
Application number
MX2015005603A
Other languages
Spanish (es)
Other versions
MX2015005603A (en
Inventor
F Mittricker Franklin
K Starcher Loren
A Huntington Richard
K Dhanuka Sulabh
M O'dea Dennis
D Draper Samuel
M Hansen Christian
Denman Todd
A West James
Original Assignee
Exxonmobil Upstream Res Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Exxonmobil Upstream Res Co filed Critical Exxonmobil Upstream Res Co
Priority claimed from PCT/US2013/067803 external-priority patent/WO2014071037A2/en
Publication of MX2015005603A publication Critical patent/MX2015005603A/en
Publication of MX357226B publication Critical patent/MX357226B/en

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Landscapes

  • Exhaust-Gas Circulating Devices (AREA)

Abstract

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
MX2015005603A 2012-10-29 2013-10-31 System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system. MX357226B (en)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US201214066579A 2012-10-29 2012-10-29
US201261722115P 2012-11-02 2012-11-02
US201261722114P 2012-11-02 2012-11-02
US201261722111P 2012-11-02 2012-11-02
US201261722118P 2012-11-02 2012-11-02
US201261747192P 2012-12-28 2012-12-28
PCT/US2013/067803 WO2014071037A2 (en) 2012-11-02 2013-10-31 System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system

Publications (2)

Publication Number Publication Date
MX2015005603A MX2015005603A (en) 2016-02-05
MX357226B true MX357226B (en) 2018-06-29

Family

ID=55959540

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2015005603A MX357226B (en) 2012-10-29 2013-10-31 System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system.

Country Status (1)

Country Link
MX (1) MX357226B (en)

Also Published As

Publication number Publication date
MX2015005603A (en) 2016-02-05

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