COOLANT BYPASS CHANNEL FOR GAS TURBINE, INSERTED INTO HOLLOW COOLED TURBINE BLADE

FIELD: machine building.SUBSTANCE: turbine guide blade has a hollow airfoil, in which there is a coolant bypass channel, having inner and outer sides separated by walls. Coolant bypass channel extends from the first component of the gas turbine to the second component of the gas turbine and has mean...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	AKHMAD Fatkhi
Format:	Patent
Sprache:	eng ; rus
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!