GAS TURBINE ENGINE WITH A PRE-SWIRL CAVITY

A gas turbine engine comprises a first passage, a second passage and a bypass channel. The first passage transmits a first leakage flow (335) from a bypass channel chamber to a pre-swirl supporting structure (310) and through an inner seal (330). The second passage transmits a second leakage flow (3...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MAY, David, THAM, Kok-Mun
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!