Aerodynamic effervescent fuel/air injection system for a gas turbine combustion chamber

The aerodynamic injection system (2) has an air feed channel (6) to supply air to a tubular structure (4). A fuel passage (8) is connected to a fuel feed channel (10). A gas injection channel (12) injects gas into fuel feed channel at a pressure which is greater than pressure of air supplied to tubu...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MANTCHENKOV, IGOR, PIKALOV, VALERY, NOEL, THOMAS, ROLLIN, GILLES, ORLOV, VLADIMIR, NOVIKOV, ALEXANDER
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION PROCESSES HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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