AR093325A1 - SYSTEM AND METHOD FOR DIFFUSION COMBUSTION WITH AN OXIDIZER-DILUENT MIXTURE IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF ESTEQUIOMETRIC EXHAUST GASES - Google Patents

SYSTEM AND METHOD FOR DIFFUSION COMBUSTION WITH AN OXIDIZER-DILUENT MIXTURE IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF ESTEQUIOMETRIC EXHAUST GASES

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Publication number
AR093325A1
AR093325A1 ARP130103999A ARP130103999A AR093325A1 AR 093325 A1 AR093325 A1 AR 093325A1 AR P130103999 A ARP130103999 A AR P130103999A AR P130103999 A ARP130103999 A AR P130103999A AR 093325 A1 AR093325 A1 AR 093325A1
Authority
AR
Argentina
Prior art keywords
turbine
estequiometric
oxidizer
recirculation
gas turbine
Prior art date
Application number
ARP130103999A
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 AR093325A1 publication Critical patent/AR093325A1/en

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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

Abstract

Se proporciona un sistema con una cámara de combustión de turbina que tiene una primera boquilla de combustible de difusión, en donde la primera boquilla de combustible de difusión tiene pasajes primero y segundo que inyectan por separado los flujos respectivos primero y segundo en una cámara de la cámara de combustión de la turbina para producir una llama de difusión. El primer flujo incluye un primer combustible, y el segundo flujo incluye un primer oxidante y un primer diluyente. El sistema incluye una turbina accionada por los productos de combustión de a llama de difusión en la cámara de combustión de la turbina. El sistema también incluye un compresor de gas de escape, en donde el compresor de gas de escape está configurado para comprimir y guiar un gas de escape de la turbina a la cámara de combustión de la turbina a lo largo de una trayectoria de recirculación de gases de escape.A system is provided with a turbine combustion chamber having a first diffusion fuel nozzle, wherein the first diffusion fuel nozzle has first and second passages that separately inject the respective first and second flows into a chamber of the combustion chamber of the turbine to produce a diffusion flame. The first flow includes a first fuel, and the second flow includes a first oxidant and a first diluent. The system includes a turbine driven by diffusion flame combustion products in the combustion chamber of the turbine. The system also includes an exhaust gas compressor, where the exhaust gas compressor is configured to compress and guide an exhaust gas from the turbine to the combustion chamber of the turbine along a gas recirculation path. escape

ARP130103999A 2012-11-02 2013-11-01 SYSTEM AND METHOD FOR DIFFUSION COMBUSTION WITH AN OXIDIZER-DILUENT MIXTURE IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF ESTEQUIOMETRIC EXHAUST GASES AR093325A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US201261722114P 2012-11-02 2012-11-02

Publications (1)

Publication Number Publication Date
AR093325A1 true AR093325A1 (en) 2015-05-27

Family

ID=51797309

Family Applications (1)

Application Number Title Priority Date Filing Date
ARP130103999A AR093325A1 (en) 2012-11-02 2013-11-01 SYSTEM AND METHOD FOR DIFFUSION COMBUSTION WITH AN OXIDIZER-DILUENT MIXTURE IN A GAS TURBINE SYSTEM WITH RECIRCULATION OF ESTEQUIOMETRIC EXHAUST GASES

Country Status (2)

Country Link
AR (1) AR093325A1 (en)
TW (1) TWI644016B (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004029029B4 (en) * 2004-06-09 2018-12-13 Deutsches Zentrum für Luft- und Raumfahrt e.V. Injection head
GB2446164A (en) * 2007-02-05 2008-08-06 Ntnu Technology Transfer As Gas Turbine Emissions Reduction with Premixed and Diffusion Combustion
UY33038A (en) * 2009-11-20 2011-06-30 Rv Lizenz Ag THERMAL AND CHEMICAL USE OF CABONACE SUBSTANCES IN PARTICULAR FOR THE GENERATION OF ENERGY WITHOUT EMISSIONS
WO2012031817A1 (en) * 2010-09-09 2012-03-15 F. Hoffmann-La Roche Ag Determination of abca1 protein levels in cells

Also Published As

Publication number Publication date
TW201432135A (en) 2014-08-16
TWI644016B (en) 2018-12-11

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