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Title: Fuel injection assembly for use in turbine engines and method of assembling same

Abstract

A fuel injection assembly for use in a turbine engine is provided. The fuel injection assembly includes a plurality of tube assemblies, wherein each of the tube assemblies includes an upstream portion and a downstream portion. Each tube assembly includes a plurality of tubes that extend from the upstream portion to the downstream portion or from the upstream portion through the downstream portion. At least one injection system is coupled to at least one tube assembly of the plurality of tube assemblies. The injection system includes a fluid supply member that extends from a fluid source to the downstream portion of the tube assembly. The fluid supply member includes a first end portion located in the downstream portion of the tube assembly, wherein the first end portion has at least one first opening for channeling fluid through the tube assembly to facilitate reducing a temperature therein.

Inventors:
;
Publication Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1174216
Patent Number(s):
8,984,888
Application Number:
13/281,679
Assignee:
General Electric Company (Schenectady, NY) NETL
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2011 Oct 26
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Uhm, Jong Ho, and Johnson, Thomas Edward. Fuel injection assembly for use in turbine engines and method of assembling same. United States: N. p., 2015. Web.
Uhm, Jong Ho, & Johnson, Thomas Edward. Fuel injection assembly for use in turbine engines and method of assembling same. United States.
Uhm, Jong Ho, and Johnson, Thomas Edward. Tue . "Fuel injection assembly for use in turbine engines and method of assembling same". United States. doi:. https://www.osti.gov/servlets/purl/1174216.
@article{osti_1174216,
title = {Fuel injection assembly for use in turbine engines and method of assembling same},
author = {Uhm, Jong Ho and Johnson, Thomas Edward},
abstractNote = {A fuel injection assembly for use in a turbine engine is provided. The fuel injection assembly includes a plurality of tube assemblies, wherein each of the tube assemblies includes an upstream portion and a downstream portion. Each tube assembly includes a plurality of tubes that extend from the upstream portion to the downstream portion or from the upstream portion through the downstream portion. At least one injection system is coupled to at least one tube assembly of the plurality of tube assemblies. The injection system includes a fluid supply member that extends from a fluid source to the downstream portion of the tube assembly. The fluid supply member includes a first end portion located in the downstream portion of the tube assembly, wherein the first end portion has at least one first opening for channeling fluid through the tube assembly to facilitate reducing a temperature therein.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Mar 24 00:00:00 EDT 2015},
month = {Tue Mar 24 00:00:00 EDT 2015}
}

Patent:

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