NON-INTEGRAL FAN BLADE PLATFORM

Described are a gas turbine engine fan blade platform, related rotor assembly and gas turbine engine, as well as a method of assembling the same. The platform has a forward portion proximal to an axis of rotation, an aft portion, and a transition portion between the forward and aft portions. The for...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PAULEY GERALD ALEXANDER, WILKIN, II DANIEL ALLEN, XIE MING, LAMBOY JORGE ORLANDO, KRAY NICHOLAS JOSEPH, GANN MATTHEW GLEN
Format:	Patent
Sprache:	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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