Turbomachine blade with tip flare

Certain embodiments of the present disclosure include a system having a turbomachine including a plurality of turbomachine blades (22) coupled to a rotor (24), wherein each turbomachine blade (22) has a blade base portion (52) and a flared blade tip portion (50) flared relative to the blade base por...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	Gustafson, Ross James, Penny, Christopher Michael
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:	Certain embodiments of the present disclosure include a system having a turbomachine including a plurality of turbomachine blades (22) coupled to a rotor (24), wherein each turbomachine blade (22) has a blade base portion (52) and a flared blade tip portion (50) flared relative to the blade base portion (52). Additionally, a trailing edge (60) of each turbomachine blade (22) extends along a common plane (70).