TURBINE BLADE WITH BLADE TIP EJECTOR

A turbine blade for a gas turbine engine is provided. The turbine blade includes an airfoil having a tip cavity. The tip cavity has a walled bottom. A pocket opening is formed in the wall adjacent to the trailing edge of the turbine blade. A passage carries a cooling medium from an internal cooling...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: CHONG GENE, BERNIER BRYAN, LEE JAE BIN, KIM KIBAEK, KIM SEOKBEOM
Format: Patent
Sprache:eng ; kor
Schlagworte:
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