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Title: Gas turbine premixer with internal cooling

Abstract

A system that includes a turbine fuel nozzle comprising an air-fuel premixer. The air-fuel premixed includes a swirl vane configured to swirl fuel and air in a downstream direction, wherein the swirl vane comprises an internal coolant path from a downstream end portion in an upstream direction through a substantial length of the swirl vane.

Inventors:
; ; ;
Issue Date:
Research Org.:
National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1082352
Patent Number(s):
8333075
Application Number:
12/425,293
Assignee:
General Electric Company (Schenectady, NY)
Patent Classifications (CPCs):
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

York, William David, Johnson, Thomas Edward, Lacy, Benjamin Paul, and Stevenson, Christian Xavier. Gas turbine premixer with internal cooling. United States: N. p., 2012. Web.
York, William David, Johnson, Thomas Edward, Lacy, Benjamin Paul, & Stevenson, Christian Xavier. Gas turbine premixer with internal cooling. United States.
York, William David, Johnson, Thomas Edward, Lacy, Benjamin Paul, and Stevenson, Christian Xavier. Tue . "Gas turbine premixer with internal cooling". United States. https://www.osti.gov/servlets/purl/1082352.
@article{osti_1082352,
title = {Gas turbine premixer with internal cooling},
author = {York, William David and Johnson, Thomas Edward and Lacy, Benjamin Paul and Stevenson, Christian Xavier},
abstractNote = {A system that includes a turbine fuel nozzle comprising an air-fuel premixer. The air-fuel premixed includes a swirl vane configured to swirl fuel and air in a downstream direction, wherein the swirl vane comprises an internal coolant path from a downstream end portion in an upstream direction through a substantial length of the swirl vane.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Dec 18 00:00:00 EST 2012},
month = {Tue Dec 18 00:00:00 EST 2012}
}

Works referenced in this record:

Burner Development and Operability Issues Associated with Steady Flowing Syngas Fired Combustors
journal, May 2008