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}
}
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