STATIONARY BLADE FOR GAS TURBINE

PURPOSE:To reduce radiation heat transfer quantity by constituting a stationary blade, stated in the title, of a combustor, etc., with a mandril coated with a heat reflecting film on its surface loosely fitted in a cavity of a blade part made of ceramics having a cavity inside thereof. CONSTITUTION:...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: FURUSE YUTAKA, MIYAZAKI SHOGO
Format: Patent
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!