Industria De Turbo Propulsores, S.a.

Roque Corral Garcia

Juan Manuel Gallardo Antolín

Juan Manuel Gallardo Antolin

The present invention relates to a rotor for gas or steam turbines having a disk (), an outer cover () and a plurality of blades (). The disk () defines the portion of less diameter of the rotor and has an inner surface configured to be coupled on a shaft () of the turbine or connected to an axially adjacent disk (&#x2033;); an outer surface configured for housing a plurality of blades (). The outer cover () defines the portion of greater diameter of the rotor. The blades () have a root () configured to be coupled on the disk () and a tip () opposite to the outer cover (). Between these blades there is a plurality of blades () welded together at the tip () to form groups of blades () and individual blades () intercalated between groups of blades ().

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Madrid, Spain

Roque Corral Garcia