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

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
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