System and method for reducing combustion dynamics in a combustor
Abstract
A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend from the upstream surface through the downstream surface. A divider inside a tube bundle defines a diluent passage that extends axially through the downstream surface, and a diluent supply in fluid communication with the divider provides diluent flow to the diluent passage. A method for reducing combustion dynamics in a combustor includes flowing a fuel through tube bundles, flowing a diluent through a diluent passage inside a tube bundle, wherein the diluent passage extends axially through at least a portion of the end cap into a combustion chamber, and forming a diluent barrier in the combustion chamber between the tube bundle and at least one other adjacent tube bundle.
- Inventors:
- Issue Date:
- Research Org.:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1213462
- Patent Number(s):
- 9,121,612
- Application Number:
- 13/409,309
- Assignee:
- General Electric Company (Schenectady, NY)
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2012 Mar 01
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Uhm, Jong Ho, Johnson, Thomas Edward, Zuo, Baifang, and York, William David. System and method for reducing combustion dynamics in a combustor. United States: N. p., 2015.
Web.
Uhm, Jong Ho, Johnson, Thomas Edward, Zuo, Baifang, & York, William David. System and method for reducing combustion dynamics in a combustor. United States.
Uhm, Jong Ho, Johnson, Thomas Edward, Zuo, Baifang, and York, William David. Tue .
"System and method for reducing combustion dynamics in a combustor". United States. https://www.osti.gov/servlets/purl/1213462.
@article{osti_1213462,
title = {System and method for reducing combustion dynamics in a combustor},
author = {Uhm, Jong Ho and Johnson, Thomas Edward and Zuo, Baifang and York, William David},
abstractNote = {A system for reducing combustion dynamics in a combustor includes an end cap having an upstream surface axially separated from a downstream surface, and tube bundles extend from the upstream surface through the downstream surface. A divider inside a tube bundle defines a diluent passage that extends axially through the downstream surface, and a diluent supply in fluid communication with the divider provides diluent flow to the diluent passage. A method for reducing combustion dynamics in a combustor includes flowing a fuel through tube bundles, flowing a diluent through a diluent passage inside a tube bundle, wherein the diluent passage extends axially through at least a portion of the end cap into a combustion chamber, and forming a diluent barrier in the combustion chamber between the tube bundle and at least one other adjacent tube bundle.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2015},
month = {9}
}
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Portable burner for fuel gas with two mixer tubes
patent, May 1993
- Jeppesen, Palle
- US Patent Document 5,213,494
Multi-venturi tube fuel injector for gas turbine combustors
patent, January 2006
- Dinu, Constantin; Hu, Iris; Storey, James
- US Patent Document 6,983,600