Closure unit for the remaining space between the first and the last blades of a bladed ring inserted in a circumferencial slot of a turbomachine, and corresponding turbomachine

The invention relates to a closing assembly (33, 133, 233) for closing the gap (28) remaining between the first and last blade (12a, 12b) of a blade ring that is inserted into a peripheral groove (10) of turbomachinery, said assembly consisting of at least two lateral parts (30, 32, 130, 131, 132, 2...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	QIAN KANG DR, RICHTER CHRISTOPH DR, SCHROEDER PETER, MARTIN SILVIO-ULRICH, SCHNEIDER OLIVER DR, WALTKE ULRICH DR, KRUETZFELDT JOACHIM, MUTKE STEFAN, SCHWARZ MICHAEL DR, KUNZE MARKUS
Format:	Patent
Sprache:	chi ; eng
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!

Beschreibung
Zusammenfassung:	The invention relates to a closing assembly (33, 133, 233) for closing the gap (28) remaining between the first and last blade (12a, 12b) of a blade ring that is inserted into a peripheral groove (10) of turbomachinery, said assembly consisting of at least two lateral parts (30, 32, 130, 131, 132, 230, 231, 232), at least one of which can be hooked onto a projection (20, 22) that forms an undercut (24, 26) in said peripheral groove (10) and at least one securing element (36, 136, 236), which secures the parts (30, 32, 130, 131, 132, 230, 231, 232) from becoming detached from the peripheral groove (10). To provide a particularly reliable closing assembly, the securing element (36, 136, 236) is configured as a pin, joining the parts (30, 32, 130, 131, 132, 230, 231, 232) of the closing assembly (33, 133, 233) in a non-positive fit.