Gas turbine engine system and method for controlling a temperature of a conduit in a gas turbine engine system

According to one aspect of the invention, an engine system includes one or more fuel circuits (102) configured to provide gaseous fuel from a fuel source for combustion. The system further comprises a conduit (110) in fluid communication with the one or more fuel circuits (102), wherein the conduit...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	Widener, Stanley Kevin
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	According to one aspect of the invention, an engine system includes one or more fuel circuits (102) configured to provide gaseous fuel from a fuel source for combustion. The system further comprises a conduit (110) in fluid communication with the one or more fuel circuits (102), wherein the conduit (110) is configured to receive a first gaseous fuel flow (117) and an oxidant flow (150) for a reaction within the conduit (110), wherein a temperature of the conduit (110) is controlled by a second gaseous fuel flow (118) along an outer wall of the conduit (110).