Gas turbine stationary blade insert installation method and application

The invention relates to the technical field of gas turbine hollow blade cooling, and particularly discloses a gas turbine stationary blade insert installation method which is applied to installationof heavy-duty gas turbine hollow blade inserts or aviation turbine engine hollow blade inserts. The m...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SU PENGFEI, KONG XIANGLIN, ZHOU NA, LI JINHONG, CAI GUOHUANG, LU HANG, YIN ZHENGFA, ZHAO SHIQUAN, LUO TAO
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	COMBINED OPERATIONS MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PERFORMING OPERATIONS TRANSPORTING UNIVERSAL MACHINE TOOLS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!