COMBUSTOR FOR GAS TURBINE

A combustor includes a combustion chamber; a nozzle supplied with fuel and air to produce a mixed gas of the fuel and the air and configured to inject the mixed gas into the combustion chamber; a fuel supply section coupled to the nozzle casing and configured to supply the fuel to the nozzle; a fuel...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	Uhm, Jong Ho
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A combustor includes a combustion chamber; a nozzle supplied with fuel and air to produce a mixed gas of the fuel and the air and configured to inject the mixed gas into the combustion chamber; a fuel supply section coupled to the nozzle casing and configured to supply the fuel to the nozzle; a fuel conditioner that includes a fuel flow path having a serpentine shape and is disposed between the fuel supply section and the nozzle, the fuel conditioner configured to guide the fuel supplied from the fuel supply section to the nozzle along the fuel flow path; and a nozzle casing having an opening into which the nozzle is inserted. The fuel conditioner extends from a first side of the nozzle casing toward a second side. The fuel conditioner and the nozzle casing form a first passage through which fuel may flow to the nozzle.