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Title: Cooling of integrated combustor nozzle of segmented annular combustion system

Abstract

A segmented annular combustion system includes integrated combustor nozzles, each of which has a fuel injection panel disposed radially between an inner liner segment and an outer liner segment. The fuel injection panel includes an aft end portion, a first side wall, a second side wall, premixing channels defined between the first side wall and the side wall, and injection outlets defined along at least one of the first side wall and the second side wall. The aft end portion defines a turbine nozzle portion. An interior portion between the first side wall and the second side wall includes walls that extend between the first and second side walls, thereby partitioning the interior portion into discrete air cavities. The air cavities and the liner segments may be cooled by impingement inserts or panels.

Inventors:
; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1650855
Patent Number(s):
10641491
Application Number:
15/464,425
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:  
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, and Hughes, Michael John. Cooling of integrated combustor nozzle of segmented annular combustion system. United States: N. p., 2020. Web.
Berry, Jonathan Dwight, Widener, Stanley Kevin, & Hughes, Michael John. Cooling of integrated combustor nozzle of segmented annular combustion system. United States.
Berry, Jonathan Dwight, Widener, Stanley Kevin, and Hughes, Michael John. Tue . "Cooling of integrated combustor nozzle of segmented annular combustion system". United States. https://www.osti.gov/servlets/purl/1650855.
@article{osti_1650855,
title = {Cooling of integrated combustor nozzle of segmented annular combustion system},
author = {Berry, Jonathan Dwight and Widener, Stanley Kevin and Hughes, Michael John},
abstractNote = {A segmented annular combustion system includes integrated combustor nozzles, each of which has a fuel injection panel disposed radially between an inner liner segment and an outer liner segment. The fuel injection panel includes an aft end portion, a first side wall, a second side wall, premixing channels defined between the first side wall and the side wall, and injection outlets defined along at least one of the first side wall and the second side wall. The aft end portion defines a turbine nozzle portion. An interior portion between the first side wall and the second side wall includes walls that extend between the first and second side walls, thereby partitioning the interior portion into discrete air cavities. The air cavities and the liner segments may be cooled by impingement inserts or panels.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2020},
month = {5}
}

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