METHOD OF CLEARANCE CONTROL AT TIPS OF TURBINE ROTOR BLADES

FIELD: machine building.SUBSTANCE: method of clearance control between tips of turbine rotor blades of the gas turbine aircraft engine at one side and ring-like bandage of turbine casing enclosing the blades from the other side, wherein the method includes a stage when flow speed and/or temperature...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHAVELO KRISTOF, GOLLI BRJUNO ROBER, OLIVE AMORI, BONNO DAMEN
Format:	Patent
Sprache:	eng ; rus
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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