Guide blade carrier

A guide blade carrier (1), particularly for a gas turbine (101), comprising a number of axial segments (2), is intended to attain a particularly high degree of operational reliability and long service life. To this end, two neighboring axial segments (2) are connected to a number of tie rods (8), ea...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	BRYK RODERICH, STROHMEIER OLIVER
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 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:	A guide blade carrier (1), particularly for a gas turbine (101), comprising a number of axial segments (2), is intended to attain a particularly high degree of operational reliability and long service life. To this end, two neighboring axial segments (2) are connected to a number of tie rods (8), each enclosed by a support tube (14), wherein a spherical disk (16) is arranged on at least one end of the respective support tube (14) and mounted in a conical socket (18) supported on the respective axial segment (2).