Turbomachine blade tip shroud

Embodiments of the present disclosure are directed toward systems including a turbomachine blade tip shroud having a pressure side portion and a suction side portion. The pressure side portion and the suction side portion are divided by a mean camber line of a turbomachine blade, and the pressure si...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Soni, Sumeet, Chouhan, Rohit, Smith, Paul Kendall, Bommanakatte, Harish, Kareff, Spencer Aaron, Pierre, Sylvain, Jayana, Srinivasa Govardhan
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:Embodiments of the present disclosure are directed toward systems including a turbomachine blade tip shroud having a pressure side portion and a suction side portion. The pressure side portion and the suction side portion are divided by a mean camber line of a turbomachine blade, and the pressure side portion has a greater surface area than the suction side portion.