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Title: System for dissipating fuel egress in fuel supply conduit assemblies

Abstract

A system for dissipating fuel egress includes a fuel injector and a fuel supply assembly. The fuel supply assembly has a fuel supply line that provides fuel and a purge air conduit arranged co-axially around the fuel supply line, thereby defining an annular channel around the fuel supply line. The fuel injector includes a perimeter body, a fuel injection port associated with the perimeter body, and an internal mixing chamber downstream of the fuel injection port in a direction of fuel flow. The fuel supply line provides fuel to the fuel injection port. The perimeter body of the fuel injector defines a fuel egress passage therethrough, which has an inlet in fluid communication with the annular channel and an outlet in fluid communication with the mixing chamber. A gas turbine combustor having an axial fuel staging (AFS) system with the present fuel egress dissipation system is also provided.

Inventors:
;
Issue Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1600421
Patent Number(s):
10,513,987
Application Number:
15/395,282
Assignee:
General Electric Company (Schenectady, NY)
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 12/30/2016
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS

Citation Formats

Hughes, Michael John, and Natarajan, Jayaprakash. System for dissipating fuel egress in fuel supply conduit assemblies. United States: N. p., 2019. Web.
Hughes, Michael John, & Natarajan, Jayaprakash. System for dissipating fuel egress in fuel supply conduit assemblies. United States.
Hughes, Michael John, and Natarajan, Jayaprakash. Tue . "System for dissipating fuel egress in fuel supply conduit assemblies". United States. https://www.osti.gov/servlets/purl/1600421.
@article{osti_1600421,
title = {System for dissipating fuel egress in fuel supply conduit assemblies},
author = {Hughes, Michael John and Natarajan, Jayaprakash},
abstractNote = {A system for dissipating fuel egress includes a fuel injector and a fuel supply assembly. The fuel supply assembly has a fuel supply line that provides fuel and a purge air conduit arranged co-axially around the fuel supply line, thereby defining an annular channel around the fuel supply line. The fuel injector includes a perimeter body, a fuel injection port associated with the perimeter body, and an internal mixing chamber downstream of the fuel injection port in a direction of fuel flow. The fuel supply line provides fuel to the fuel injection port. The perimeter body of the fuel injector defines a fuel egress passage therethrough, which has an inlet in fluid communication with the annular channel and an outlet in fluid communication with the mixing chamber. A gas turbine combustor having an axial fuel staging (AFS) system with the present fuel egress dissipation system is also provided.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2019},
month = {12}
}

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Works referenced in this record:

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patent, June 2016


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patent, June 2016


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patent, June 2018


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patent, April 2016


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patent, July 2014


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patent, June 2014


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patent, February 2016


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