TURBINE VANE AIRFOIL PROFILE

A turbine vane (32b) for a gas turbine engine (10) has an airfoil (50) including leading and trailing edges (54, 56) joined by spaced-apart pressure and suction sides (62, 64) to provide an external airfoil surface (52). The surface (52) is formed in substantial conformance with multiple cross-secti...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MARINI, Remo, TARDIF, Marc, GILLESPIE, Jason
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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