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Title: Radial inlet guide vanes for a combustor

Abstract

A combustor may include an interior flow path therethrough, a number of fuel nozzles in communication with the interior flow path, and an inlet guide vane system positioned about the interior flow path to create a swirled flow therein. The inlet guide vane system may include a number of windows positioned circumferentially around the fuel nozzles. The inlet guide vane system may also include a number of inlet guide vanes positioned circumferentially around the fuel nozzles and adjacent to the windows to create a swirled flow within the interior flow path.

Inventors:
; ; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1083208
Patent Number(s):
8371101
Application Number:
12/559,522
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

Zuo, Baifang, Simons, Derrick, York, William, and Ziminsky, Willy S. Radial inlet guide vanes for a combustor. United States: N. p., 2013. Web.
Zuo, Baifang, Simons, Derrick, York, William, & Ziminsky, Willy S. Radial inlet guide vanes for a combustor. United States.
Zuo, Baifang, Simons, Derrick, York, William, and Ziminsky, Willy S. Tue . "Radial inlet guide vanes for a combustor". United States. https://www.osti.gov/servlets/purl/1083208.
@article{osti_1083208,
title = {Radial inlet guide vanes for a combustor},
author = {Zuo, Baifang and Simons, Derrick and York, William and Ziminsky, Willy S},
abstractNote = {A combustor may include an interior flow path therethrough, a number of fuel nozzles in communication with the interior flow path, and an inlet guide vane system positioned about the interior flow path to create a swirled flow therein. The inlet guide vane system may include a number of windows positioned circumferentially around the fuel nozzles. The inlet guide vane system may also include a number of inlet guide vanes positioned circumferentially around the fuel nozzles and adjacent to the windows to create a swirled flow within the interior flow path.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Feb 12 00:00:00 EST 2013},
month = {Tue Feb 12 00:00:00 EST 2013}
}

Works referenced in this record:

Gas turbine combustor
patent, February 1996


Perfected combustion system with low polluting emissions for gas turbines
patent, August 1997


Combustor with two stage primary fuel tube with concentric members and flow regulating
patent, November 1999


Rotary ramjet turbo-generator
patent, March 2010


Mixer assembly
patent, August 2010


Partial premix dual circuit fuel injector
patent-application, November 2002


Mixer assembly for combustor of a gas turbine engine having a main mixer with improved fuel penetration
patent-application, February 2007


Methods and Systems to Facilitate Reducing Combustion Systems
patent-application, December 2009