Rotor blade with air flow passages

A rotor blade 2 for a turbo machine, such as a gas turbine engine, comprising an aerofoil 6 having pressure and suction surfaces 8,10, leading and trailing edges 12, 14, and an array of passages 20 at a tip region 18 of the aerofoil, where the passages extend from the pressure surface to the suction...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	STEPHANE MICHEL MARCEL BARALON, NEIL WILLIAM HARVEY
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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