CMC VANE WITH FLANGE HAVING SLOPED RADIAL FACE

A vane arc segment (60) includes a ceramic matrix composite fairing (62) that has first and second platforms (64, 66) and an airfoil section (68) that extends in a radial direction (RD) there between. Each of the first and second platforms (64, 66) includes axially-facing leading and trailing sides...

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Bibliographische Detailangaben
Hauptverfasser:	LILES, Howard J, KIM, Russell
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 arc segment (60) includes a ceramic matrix composite fairing (62) that has first and second platforms (64, 66) and an airfoil section (68) that extends in a radial direction (RD) there between. Each of the first and second platforms (64, 66) includes axially-facing leading and trailing sides (70c, 70d), a core gaspath side (70a), and a non-core gaspath side (70b). The non-core gaspath side (70b) of the first platform (64) has a flange (72) that projects radially there from and extends adjacent the trailing side (70d). The flange (72) has a radial face (72a) that is sloped with respect to the radial direction (RD).