LOCKING SPACER ASSEMBLY IN GAS TURBINE ENGINE

A locking spacer assembly for filling a final spacer slot in a disk groove between platforms of adjacent rotating blades in a gas turbine engine includes a first side piece having a first outer surface, a second side piece having a second outer surface, a mid-piece disposed between and in contact wi...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DAVIS, Paul, GOSTOMELSKY, Alexander, MILLER, Keith, ZELMER, Dimitri
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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