Stepped double head annular combustor

The ring-shaped staged combustion chamber (1) is for a gas turbine of an aircraft engine and comprises a pilot head (12) with several injection systems (16) spread over the base of the pilot head chamber (8) connecting a longitudinal internal wall (4) of the chamber to a longitudinal external wall (...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	COMMARET, PATRICE, VIGUIER, CHRISTOPHE, BOUDOIN, CHRISTOPHE, LE LETTY, ERIC
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 WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!