ROTOR BLADE

A rotor blade for a gas turbine engine, comprising an aerofoil having pressure and suction surfaces, leading and trailing edges, and an array of passages at a tip region of the aerofoil. The passages extend from the pressure surface to the suction surface of the aerofoil and are disposed so that the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: HARVEY NEIL W, BARALON STEPHANE M. M
Format: Patent
Sprache:eng
Schlagworte:
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