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Title: Apparatus and method for mixing fuel in a gas turbine nozzle

Abstract

A nozzle includes a fuel plenum and an air plenum downstream of the fuel plenum. A primary fuel channel includes an inlet in fluid communication with the fuel plenum and a primary air port in fluid communication with the air plenum. Secondary fuel channels radially outward of the primary fuel channel include a secondary fuel port in fluid communication with the fuel plenum. A shroud circumferentially surrounds the secondary fuel channels. A method for mixing fuel and air in a nozzle prior to combustion includes flowing fuel to a fuel plenum and flowing air to an air plenum downstream of the fuel plenum. The method further includes injecting fuel from the fuel plenum through a primary fuel passage, injecting fuel from the fuel plenum through secondary fuel passages, and injecting air from the air plenum through the primary fuel passage.

Inventors:
; ;
Issue Date:
Research Org.:
National Energy Technology Laboratory (NETL), Pittsburgh, PA, Morgantown, WV (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1150213
Patent Number(s):
8800289
Application Number:
12/877,385
Assignee:
General Electric Company (Schenectady, NY)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
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

Johnson, Thomas Edward, Ziminsky, Willy Steve, and Berry, Jonathan Dwight. Apparatus and method for mixing fuel in a gas turbine nozzle. United States: N. p., 2014. Web.
Johnson, Thomas Edward, Ziminsky, Willy Steve, & Berry, Jonathan Dwight. Apparatus and method for mixing fuel in a gas turbine nozzle. United States.
Johnson, Thomas Edward, Ziminsky, Willy Steve, and Berry, Jonathan Dwight. Tue . "Apparatus and method for mixing fuel in a gas turbine nozzle". United States. https://www.osti.gov/servlets/purl/1150213.
@article{osti_1150213,
title = {Apparatus and method for mixing fuel in a gas turbine nozzle},
author = {Johnson, Thomas Edward and Ziminsky, Willy Steve and Berry, Jonathan Dwight},
abstractNote = {A nozzle includes a fuel plenum and an air plenum downstream of the fuel plenum. A primary fuel channel includes an inlet in fluid communication with the fuel plenum and a primary air port in fluid communication with the air plenum. Secondary fuel channels radially outward of the primary fuel channel include a secondary fuel port in fluid communication with the fuel plenum. A shroud circumferentially surrounds the secondary fuel channels. A method for mixing fuel and air in a nozzle prior to combustion includes flowing fuel to a fuel plenum and flowing air to an air plenum downstream of the fuel plenum. The method further includes injecting fuel from the fuel plenum through a primary fuel passage, injecting fuel from the fuel plenum through secondary fuel passages, and injecting air from the air plenum through the primary fuel passage.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Aug 12 00:00:00 EDT 2014},
month = {Tue Aug 12 00:00:00 EDT 2014}
}

Works referenced in this record:

Rotary Engine
patent, November 1973


Heavy fuel combustor
patent, November 1983


Fuel/oxidizer premixing combustion chamber
patent, August 1994


Pre-mixing injection system for a turbojet engine
patent, January 1997


Circulating fluidized bed reactor having extensions to its heat exchange area
patent, January 1998


Premixing fuel injector with improved secondary fuel-air injection
patent, August 2000


Self-cooled oxygen-fuel burner for use in high-temperature and high-particulate furnaces
patent, September 2000


Method and apparatus for a fuel-rich catalytic reactor
patent, May 2002


Swozzle based burner tube premixer including inlet air conditioner for low emissions combustion
patent, August 2002


High capacity/low NOx radiant wall burner
patent, September 2004


Method and apparatus for reducing gas turbine engine emissions
patent, November 2005


Multi-venturi tube fuel injector for gas turbine combustors
patent, January 2006


Multi-sided diffuser for a venturi in a fuel injector for a gas turbine
patent, February 2006


Method and apparatus for reducing gas turbine engine emissions
patent, August 2007


Controlled pilot oxidizer for a gas turbine combustor
patent, July 2010


Fuel Injector for Low NOx Furnace
patent-application, December 2009


Pre-Mixing Apparatus for a Turbine Engine
patent-application, January 2010


Turbomachine Injection Nozzle Including a Coolant Delivery System
patent-application, February 2010


Multi-tube Thermal Fuse for Nozzle Protection from a Flame Holding or Flashback Event
patent-application, June 2010


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


Premixed Direct Injection Disk
patent-application, September 2010


Premixing Direct Injector
patent-application, October 2010


Staged Multi-Tube Premixing Injector
patent-application, April 2011


    Works referencing / citing this record:

    Fuel nozzle for use in a turbine engine and method of assembly
    patent, March 2017


    Micromixing cap assembly
    patent, January 2017


    Combustor cap having non-round outlets for mixing tubes
    patent, December 2016


    System having a combustor cap
    patent, December 2016


    System having multi-tube fuel nozzle with floating arrangement of mixing tubes
    patent, December 2016


    Combustor end cover with fuel plenums
    patent, June 2016


    End cover configuration and assembly
    patent, May 2016