TURBINE CASING COMPRISING A MEANS FOR ATTACHING RING SECTORS

The invention relates to an aircraft turbine casing (30), which is to support a set of ring sectors (28) that partially define a pipe for the flow of a gas stream through the turbine, comprising a means for dynamically adjusting the radial position of the ring sectors (28), an upstream radial lug (3...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CORDIER, JEANRISTOPHE MARC, BONNEAU, DAMIEN, GARIN, FABRICE MARCEL NOEL
Format:	Patent
Sprache:	eng ; fre
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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