TURBINE ENGINE AIRFOIL ASSEMBLY

An airfoil assembly for a turbine engine includes an airfoil with an outer wall having a pressure side and a suction side, the airfoil extending axially between a leading edge and a trailing edge to define a chord-wise direction and also extending radially between a root and a tip to define a span-w...

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Bibliographische Detailangaben
Hauptverfasser: Davis, Tod Winton, Farson, Max Robert, Cotten, Stephanie Glynn, Bryant, JR., Gary Willard, Ingling, Theodore Robert, Brown, James Francis
Format: Patent
Sprache:eng
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Zusammenfassung:An airfoil assembly for a turbine engine includes an airfoil with an outer wall having a pressure side and a suction side, the airfoil extending axially between a leading edge and a trailing edge to define a chord-wise direction and also extending radially between a root and a tip to define a span-wise direction. An aperture and at least one slot can define at least a portion of a release plane extending through the outer wall.