AR093324A1 - SYSTEM AND METHOD FOR COMPRESSION OF OXIDIZER IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF EXHAUST GASES ESTEQUIOMETRICO - Google Patents

SYSTEM AND METHOD FOR COMPRESSION OF OXIDIZER IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF EXHAUST GASES ESTEQUIOMETRICO

Info

Publication number
AR093324A1
AR093324A1 ARP130103997A ARP130103997A AR093324A1 AR 093324 A1 AR093324 A1 AR 093324A1 AR P130103997 A ARP130103997 A AR P130103997A AR P130103997 A ARP130103997 A AR P130103997A AR 093324 A1 AR093324 A1 AR 093324A1
Authority
AR
Argentina
Prior art keywords
turbine
exhaust gas
recirculation
compression
combustion chamber
Prior art date
Application number
ARP130103997A
Other languages
Spanish (es)
Original Assignee
Exxonmobil Upstream Res Co
Gen Electric
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, Gen Electric filed Critical Exxonmobil Upstream Res Co
Publication of AR093324A1 publication Critical patent/AR093324A1/en

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engine Equipment That Uses Special Cycles (AREA)
  • Exhaust-Gas Circulating Devices (AREA)

Abstract

Un sistema incluye un sistema de turbina de gas que tiene una cámara de combustión de la turbina, una turbina accionada por los productos de combustión desde la cámara de combustión de la turbina, y un compresor de gas de escape accionado por la turbina. El compresor de gas de escape está configurado para comprimir y suministrar un gas de escape a la cámara de combustión de la turbina. El sistema de turbina de gas también tiene un sistema de recirculación de gases de escape (EGR). El sistema de EGR está configurado para recircular el gas de escape a lo largo de una trayectoria de recirculación de gases de escape de la turbina al compresor de gas de escape. El sistema incluye además un sistema de compresión de oxidante principal que tiene uno o más compresores de oxidantes. Uno o más compresores de oxidantes están separados desde el compresor de gas de escape, y uno o más compresores de oxidantes están configurados para suministrar todo el oxidante comprimido utilizado por la cámara de combustión de la turbina en la generación de los productos de la combustión.One system includes a gas turbine system having a combustion chamber of the turbine, a turbine driven by combustion products from the combustion chamber of the turbine, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compress and supply an exhaust gas to the combustion chamber of the turbine. The gas turbine system also has an exhaust gas recirculation system (EGR). The EGR system is configured to recirculate the exhaust gas along an exhaust gas recirculation path from the turbine to the exhaust gas compressor. The system also includes a main oxidant compression system that has one or more oxidant compressors. One or more oxidant compressors are separated from the exhaust gas compressor, and one or more oxidant compressors are configured to supply all the compressed oxidant used by the combustion chamber of the turbine in the generation of combustion products.

ARP130103997A 2012-11-02 2013-11-01 SYSTEM AND METHOD FOR COMPRESSION OF OXIDIZER IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF EXHAUST GASES ESTEQUIOMETRICO AR093324A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261722118P 2012-11-02 2012-11-02
US201261747192P 2012-12-28 2012-12-28

Publications (1)

Publication Number Publication Date
AR093324A1 true AR093324A1 (en) 2015-05-27

Family

ID=51797311

Family Applications (1)

Application Number Title Priority Date Filing Date
ARP130103997A AR093324A1 (en) 2012-11-02 2013-11-01 SYSTEM AND METHOD FOR COMPRESSION OF OXIDIZER IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF EXHAUST GASES ESTEQUIOMETRICO

Country Status (2)

Country Link
AR (1) AR093324A1 (en)
TW (1) TWI654369B (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2093683C (en) 1992-05-14 2002-10-15 William Miller Farrell Intercooled gas turbine engine
US6012279A (en) 1997-06-02 2000-01-11 General Electric Company Gas turbine engine with water injection
DE102004020753A1 (en) 2004-04-27 2005-12-29 Man Turbo Ag Device for utilizing the waste heat from compressors
US7895822B2 (en) 2006-11-07 2011-03-01 General Electric Company Systems and methods for power generation with carbon dioxide isolation
US8397482B2 (en) 2008-05-15 2013-03-19 General Electric Company Dry 3-way catalytic reduction of gas turbine NOx
MY156099A (en) 2010-07-02 2016-01-15 Exxonmobil Upstream Res Co Systems and methods for controlling combustion of a fuel
US8726628B2 (en) 2010-10-22 2014-05-20 General Electric Company Combined cycle power plant including a carbon dioxide collection system

Also Published As

Publication number Publication date
TW201432137A (en) 2014-08-16
TWI654369B (en) 2019-03-21

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