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Title: Transition duct with late injection in turbine system

Abstract

A system for supplying an injection fluid to a combustor is disclosed. The system includes a transition duct comprising an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The passage defines a combustion chamber. The system further includes a tube providing fluid communication for the injection fluid to flow through the transition duct and into the combustion chamber.

Inventors:
; ; ; ;
Issue Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1215539
Patent Number(s):
9,133,722
Application Number:
13/459,516
Assignee:
General Electric Company (Schenectady, NY) NETL
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Apr 30
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

LeBegue, Jeffrey Scott, Pentecost, Ronnie Ray, Flanagan, James Scott, Kim, Won -Wook, and McMahan, Kevin Weston. Transition duct with late injection in turbine system. United States: N. p., 2015. Web.
LeBegue, Jeffrey Scott, Pentecost, Ronnie Ray, Flanagan, James Scott, Kim, Won -Wook, & McMahan, Kevin Weston. Transition duct with late injection in turbine system. United States.
LeBegue, Jeffrey Scott, Pentecost, Ronnie Ray, Flanagan, James Scott, Kim, Won -Wook, and McMahan, Kevin Weston. Tue . "Transition duct with late injection in turbine system". United States. https://www.osti.gov/servlets/purl/1215539.
@article{osti_1215539,
title = {Transition duct with late injection in turbine system},
author = {LeBegue, Jeffrey Scott and Pentecost, Ronnie Ray and Flanagan, James Scott and Kim, Won -Wook and McMahan, Kevin Weston},
abstractNote = {A system for supplying an injection fluid to a combustor is disclosed. The system includes a transition duct comprising an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The passage defines a combustion chamber. The system further includes a tube providing fluid communication for the injection fluid to flow through the transition duct and into the combustion chamber.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2015},
month = {9}
}

Patent:

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