THERMAL MANAGEMENT FOR GAS TURBINE ENGINE

A gas turbine engine has an inlet duct, which is configured to communicate with an inlet to a compressor. The inlet duct is further configured to communicate air outwardly of an outer casing of the gas turbine engine, and to pass the air along an axial length of the gas turbine engine to cool a comp...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	THAYALAKHANDAN, NAGAMANY, ALEXANDER, ERIC J, TRAVELBEE, CHARLES BRIAN, JONES, ANTHONY C, LYDON, PATRICK M
Format:	Patent
Sprache:	eng ; fre
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!