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Title: Gas turbine premixing systems

Abstract

Methods and systems are provided for premixing combustion fuel and air within gas turbines. In one embodiment, a combustor includes an upstream mixing panel configured to direct compressed air and combustion fuel through premixing zone to form a fuel-air mixture. The combustor includes a downstream mixing panel configured to mix additional combustion fuel with the fule-air mixture to form a combustion mixture.

Inventors:
; ; ; ;
Issue Date:
Research Org.:
National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1113536
Patent Number(s):
8616002
Application Number:
12/508,545
Assignee:
General Electric Company (Schenectady, NY)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23N - REGULATING OR CONTROLLING COMBUSTION
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Kraemer, Gilbert Otto, Varatharajan, Balachandar, Evulet, Andrei Tristan, Yilmaz, Ertan, and Lacy, Benjamin Paul. Gas turbine premixing systems. United States: N. p., 2013. Web.
Kraemer, Gilbert Otto, Varatharajan, Balachandar, Evulet, Andrei Tristan, Yilmaz, Ertan, & Lacy, Benjamin Paul. Gas turbine premixing systems. United States.
Kraemer, Gilbert Otto, Varatharajan, Balachandar, Evulet, Andrei Tristan, Yilmaz, Ertan, and Lacy, Benjamin Paul. Tue . "Gas turbine premixing systems". United States. https://www.osti.gov/servlets/purl/1113536.
@article{osti_1113536,
title = {Gas turbine premixing systems},
author = {Kraemer, Gilbert Otto and Varatharajan, Balachandar and Evulet, Andrei Tristan and Yilmaz, Ertan and Lacy, Benjamin Paul},
abstractNote = {Methods and systems are provided for premixing combustion fuel and air within gas turbines. In one embodiment, a combustor includes an upstream mixing panel configured to direct compressed air and combustion fuel through premixing zone to form a fuel-air mixture. The combustor includes a downstream mixing panel configured to mix additional combustion fuel with the fule-air mixture to form a combustion mixture.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2013},
month = {12}
}