LOW NOX COMBUSTOR FOR GAS TURBINE ENGINE

PROBLEM TO BE SOLVED: To contribute to the reduction of discharging of NOx in a gas turbine engine by a method wherein the air stream of a specified amount is introduced from the air port of a combustor at the downstream of a dome by a specified distance into a fuel air spray pattern. SOLUTION: A co...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	STURGESS GEOFFREY J, SMITH REID D C, SISKIND KENNETH S, SEGALMAN IRVING, HOKE JAMES B
Format:	Patent
Sprache:	eng
Schlagworte:	AIR BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN WEAPONS
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