DISC FOR A ROTOR OF A GAS TURBINE ENGINE, AND A ROTOR AND A GAS TURBINE COMPRISING THE SAME

A disc of a gas turbine engine (10) system is provided. The disc includes a disc hub (203; 403; 603) including, an interstage coupling (207; 307; 407; 607) disposed on an axially extending surface (212; 312; 412; 612) at a peripheral edge of the disc hub that includes a protrusion that extends axial...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PORTER, Steven D, OREN, Nicholas Waters
Format:	Patent
Sprache:	eng ; fre ; ger
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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