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Title: Transition nozzle combustion system

Abstract

The present application provides a combustion system for use with a cooling flow. The combustion system may include a head end, an aft end, a transition nozzle extending from the head end to the aft end, and an impingement sleeve surrounding the transition nozzle. The impingement sleeve may define a first cavity in communication with the head end for a first portion of the cooling flow and a second cavity in communication with the aft end for a second portion of the cooling flow. The transition nozzle may include a number of cooling holes thereon in communication with the second portion of the cooling flow.

Inventors:
; ;
Issue Date:
Research Org.:
GENERAL ELECTRIC COMPANY, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1333736
Patent Number(s):
9,506,359
Application Number:
13/437,953
Assignee:
GENERAL ELECTRIC COMPANY (Schenectady, NY)
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Apr 03
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING; 33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Kim, Won-Wook, McMahan, Kevin Weston, and Maldonado, Jaime Javier. Transition nozzle combustion system. United States: N. p., 2016. Web.
Kim, Won-Wook, McMahan, Kevin Weston, & Maldonado, Jaime Javier. Transition nozzle combustion system. United States.
Kim, Won-Wook, McMahan, Kevin Weston, and Maldonado, Jaime Javier. Tue . "Transition nozzle combustion system". United States. https://www.osti.gov/servlets/purl/1333736.
@article{osti_1333736,
title = {Transition nozzle combustion system},
author = {Kim, Won-Wook and McMahan, Kevin Weston and Maldonado, Jaime Javier},
abstractNote = {The present application provides a combustion system for use with a cooling flow. The combustion system may include a head end, an aft end, a transition nozzle extending from the head end to the aft end, and an impingement sleeve surrounding the transition nozzle. The impingement sleeve may define a first cavity in communication with the head end for a first portion of the cooling flow and a second cavity in communication with the aft end for a second portion of the cooling flow. The transition nozzle may include a number of cooling holes thereon in communication with the second portion of the cooling flow.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2016},
month = {11}
}

Patent:

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