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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 = {Tue Dec 31 00:00:00 EST 2013},
month = {Tue Dec 31 00:00:00 EST 2013}
}

Works referenced in this record:

Dual fuel power generation system
patent, August 2004


Pre-mixing apparatus for a turbine engine
patent, April 2012


Radial lean direct injection burner
patent, September 2012


Sector staging combustor
patent, November 2005


Low emissions combustor premixer
patent, June 2000


Burner with staged fuel injection
patent, March 2007


Lean direct injection diffusion tip and related method
patent, August 2012


Controlled pressure fuel nozzle system
patent, May 2006


Controlled pressure fuel nozzle injector
patent, October 2005


Premixed direct injection nozzle
patent, February 2011


Premixed direct injection disk
patent, April 2013


Premixed Direct Injection Disk
patent-application, September 2010


Burner system with staged fuel injection and method for its operation
patent, May 2003


Automatic combustion control for a gas turbine
patent, April 2005


Premix combustor
patent, July 1978


Bundled Multi-Tube Nozzle For A Turbomachine
patent-application, July 2010


Multiple tube premixing device
patent, December 2012


Premixed charge compression ignition engine with optimal combustion control
patent, July 2005


Two stage V-gutter fuel injection mixer
patent, April 1993


Process for catalytic combustion with staged fuel injection
patent, October 1998