FAN BLADE TIP AS A CUTTING TOOL

FAN BLADE TIP AS A CUTTING TOOL An airfoil for a gas turbine engine is disclosed. The airfoil may include a first side, and a second side opposite the first side. The first side and the second side may extend axially from a leading edge to a trailing edge and radially from a base to a tip. The tip m...

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Hauptverfasser:	CHANGSHENG GUO, JAMES O. HANSEN
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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Beschreibung
Zusammenfassung:	FAN BLADE TIP AS A CUTTING TOOL An airfoil for a gas turbine engine is disclosed. The airfoil may include a first side, and a second side opposite the first side. The first side and the second side may extend axially from a leading edge to a trailing edge and radially from a base to a tip. The tip may include an oblique surface between the first side and the second side. [No suitable figure]