TURBOMACHINE BLADE WITH TIP FLARE

Certain embodiments of the present disclosure include a system having a turbomachine including a plurality of turbomachine blades coupled to a rotor, wherein each turbomachine blade has a blade base portion and a flared blade tip portion flared relative to the blade base portion. Additionally, a tra...

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Bibliographische Detailangaben
Hauptverfasser: GUSTAFSON ROSS JAMES, PENNY CHRISTOPHER MICHAEL
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:Certain embodiments of the present disclosure include a system having a turbomachine including a plurality of turbomachine blades coupled to a rotor, wherein each turbomachine blade has a blade base portion and a flared blade tip portion flared relative to the blade base portion. Additionally, a trailing edge of each turbomachine blade extends along a common plane.