COOLING ARRANGEMENT FOR PLATFORM REGION OF TURBINE ROTOR BLADE

A platform cooling arrangement in a turbine rotor blade having a platform at an interface between an airfoil and a root. The platform may include a pressure side slashface and a suction side slashface. The platform cooling arrangement may include: a cooling channel formed within the interior of the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BENSON ADEBUKOLA OLUWASEUN, SAMPAYO CAMILO ANDRES, KESTER CHRISTOPHER WILLIAM, ZHANG XIUZHANG JAMES
Format: Patent
Sprache:eng
Schlagworte:
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