Exhaust gas duct for a gas turbine with heat resistant liner and gas turbine having such a gas duct

The gas channel (17) has concentric inner housing (19) that is surrounded by outer housing (18), through which exhaust gases from gas turbine are discharged outside. The inner housing and outer casing are interconnected by several radial supports (20). The supports, outer housing and inner housing a...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Steffen, Tobias, Krautzig, Joachim, Pacholleck, Jürgen, Rauch, Marc, Busekros, Amin
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS 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!

Beschreibung
Zusammenfassung:	The gas channel (17) has concentric inner housing (19) that is surrounded by outer housing (18), through which exhaust gases from gas turbine are discharged outside. The inner housing and outer casing are interconnected by several radial supports (20). The supports, outer housing and inner housing are equipped with refractory linings (19a,20a) for protection against hot exhaust gases. The linings are releasably fastened to support structure, such that stress-free thermal expansion of linings is ensured in all operating conditions.