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Title: Combustor and combustor screech mitigation methods

Abstract

The present application provides for a combustor for use with a gas turbine engine. The combustor may include a cap member and a number of fuel nozzles extending through the cap member. One or more of the fuel nozzles may be provided in a non-flush position with respect to the cap member.

Inventors:
; ; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1133625
Patent Number(s):
8733108
Application Number:
12/833,237
Assignee:
General Electric Company (Schenectady, NY)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23C - METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  {A CARRIER GAS OR} AIR 
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

Kim, Kwanwoo, Johnson, Thomas Edward, Uhm, Jong Ho, and Kraemer, Gilbert Otto. Combustor and combustor screech mitigation methods. United States: N. p., 2014. Web.
Kim, Kwanwoo, Johnson, Thomas Edward, Uhm, Jong Ho, & Kraemer, Gilbert Otto. Combustor and combustor screech mitigation methods. United States.
Kim, Kwanwoo, Johnson, Thomas Edward, Uhm, Jong Ho, and Kraemer, Gilbert Otto. Tue . "Combustor and combustor screech mitigation methods". United States. https://www.osti.gov/servlets/purl/1133625.
@article{osti_1133625,
title = {Combustor and combustor screech mitigation methods},
author = {Kim, Kwanwoo and Johnson, Thomas Edward and Uhm, Jong Ho and Kraemer, Gilbert Otto},
abstractNote = {The present application provides for a combustor for use with a gas turbine engine. The combustor may include a cap member and a number of fuel nozzles extending through the cap member. One or more of the fuel nozzles may be provided in a non-flush position with respect to the cap member.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2014},
month = {5}
}

Works referenced in this record:

Movable combustion system for a gas turbine
patent, June 1992


Staged fuel delivery system with secondary distribution valve
patent, June 1994


Gas turbine combustor
patent, November 1998


Multiple venturi ultra-low nox combustor
patent, July 1999


Gas turbine combustor
patent, September 2001


Gas turbine combustor
patent, December 2001


Gas turbine combustor
patent, May 2005


Methods and systems for combustion dynamics reduction
patent, August 2009


Gas turbine combustor
patent-application, September 2003


Gas turbine combustor and operating method thereof
patent-application, March 2004


Gas Turbine Combustor and Ignition Method of Igniting Fuel Mixture in the Same
patent-application, July 2008


Swirler, Fuel and Air Assembly and Combustor
patent-application, December 2011