High-pressure turbine rotor, and method for the production...

B - Operations – Transporting – 22 – F

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Details

B22F 3/105 (2006.01) B22F 5/00 (2006.01) B22F 5/04 (2006.01) F01D 5/02 (2006.01)

Patent

CA 2665069

The invention relates to a method for producing a high-pressure turbine rotor, wherein this turbine rotor is designed as a blisk (i.e., bladed disk) and forms a radially inward disk and several vanes or blades that project from said disk, wherein the turbine rotor has an internal duct system for air cooling, and wherein at least one section of said turbine rotor is manufactured in a generative production process, as well as a turbine rotor.

La présente invention concerne un procédé de réalisation d'un rotor de turbine haute pression qui se présente sous la forme d'un disque à aubes (b

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