ENSEMBLE COMPRISING A FUEL INJECTION SYSTEM FOR AN AIRCRAFT TURBOMACHINE COMBUSTION CHAMBER AND A FUEL INJECTOR

An assembly includes an injection system and an injector for an aircraft turbomachine combustion chamber. The system includes an aerodynamic bowl including a first end widening toward the downstream end and centered on a central axis of the injection system, this also including a central body along...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MERY, Yoann, LEPAROUX, Julien, BIDART, Olivier
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING REGULATING OR CONTROLLING COMBUSTION WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!