BLADE LEADING EDGE TIP RIB

A rotor blade for a gas turbine engine includes a leading edge tip rib projecting outwardly from an airfoil of the blade at a tip region thereof. The tip rib continuously surrounds a leading edge of the airfoil and extends rearwardly from the leading edge along respective pressure and suction side s...

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Bibliographische Detailangaben
Hauptverfasser: GRIVAS NICOLAS, MARINI REMO, VLASIC EDWARD
Format: Patent
Sprache:eng
Schlagworte:
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