VANE ASSEMBLY FOR A GAS TURBINE ENGINE

A vane assembly (10) for a gas turbine engine is disclosed herein. The vane assembly includes an inner platform, an outer platform, and a ceramic-containing airfoil (16) that extends from the inner platform to the outer platform. The ceramic-containing airfoil is manufactured to have radially discon...

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Bibliographische Detailangaben
1. Verfasser:	Walston, Jeffrey A
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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Beschreibung
Zusammenfassung:	A vane assembly (10) for a gas turbine engine is disclosed herein. The vane assembly includes an inner platform, an outer platform, and a ceramic-containing airfoil (16) that extends from the inner platform to the outer platform. The ceramic-containing airfoil is manufactured to have radially discontinuous ribs (25) spaced radially apart from one another between the inner platform and the outer platform.