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Title: Integrated combustor nozzle for a segmented annular combustion system

Abstract

The present disclosure is directed to an integrated combustor nozzle for a segmented annular combustion system. The integrated combustor nozzle includes an outer liner segment, an inner liner segment, and a fuel injection panel extending radially between the outer liner segment and the inner liner segment. The fuel injection panel includes a first side wall, a second side wall, and a plurality of premixing channels between the first and second side walls, each of the premixing channels having an outlet on one of the first and second side walls. The aft end of the fuel injection panel defines a turbine nozzle.

Inventors:
; ; ; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1637763
Patent Number(s):
10605459
Application Number:
15/464,419
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
F - MECHANICAL ENGINEERING F02 - COMBUSTION ENGINES F02C - GAS-TURBINE PLANTS
DOE Contract Number:  
FE0023965
Resource Type:
Patent
Resource Relation:
Patent File Date: 03/21/2017
Country of Publication:
United States
Language:
English

Citation Formats

Berry, Jonathan Dwight, Widener, Stanley Kevin, Hughes, Michael John, Hafner, Matthew Troy, and Citeno, Joseph Vincent. Integrated combustor nozzle for a segmented annular combustion system. United States: N. p., 2020. Web.
Berry, Jonathan Dwight, Widener, Stanley Kevin, Hughes, Michael John, Hafner, Matthew Troy, & Citeno, Joseph Vincent. Integrated combustor nozzle for a segmented annular combustion system. United States.
Berry, Jonathan Dwight, Widener, Stanley Kevin, Hughes, Michael John, Hafner, Matthew Troy, and Citeno, Joseph Vincent. Tue . "Integrated combustor nozzle for a segmented annular combustion system". United States. https://www.osti.gov/servlets/purl/1637763.
@article{osti_1637763,
title = {Integrated combustor nozzle for a segmented annular combustion system},
author = {Berry, Jonathan Dwight and Widener, Stanley Kevin and Hughes, Michael John and Hafner, Matthew Troy and Citeno, Joseph Vincent},
abstractNote = {The present disclosure is directed to an integrated combustor nozzle for a segmented annular combustion system. The integrated combustor nozzle includes an outer liner segment, an inner liner segment, and a fuel injection panel extending radially between the outer liner segment and the inner liner segment. The fuel injection panel includes a first side wall, a second side wall, and a plurality of premixing channels between the first and second side walls, each of the premixing channels having an outlet on one of the first and second side walls. The aft end of the fuel injection panel defines a turbine nozzle.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2020},
month = {3}
}