Gas Turbine Combustor

A deviation of fuel injection amounts among a plurality of fuel nozzles connected to one fuel header is suppressed while suppressing increases in a manufacturing man-hour count and a pressure loss of a fuel. A gas turbine combustor includes: a liner forming a combustion chamber; a plurality of fuel...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KOGANEZAWA, Tomomi, IGARASHI, Shota, NAGAHASHI, Hiroaki, TERADA, Yoshitaka
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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