Composite airfoil assembly with dovetail portion

A composite blade assembly for a turbine engine has a core and a laminated skin. The core has a composite structure. The laminated skin has at least one composite ply. The laminated skin has a first portion forming a first angle with respect to a horizontal plane and a second portion forming a secon...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	FRANKS MICHAEL JOHN, KRAY NICHOLAS JOSEPH
Format:	Patent
Sprache:	chi ; 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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