Rotor blade for an axial flow turbomachine and mounting for such a rotor blade

A rotor blade for an axial flow turbomachine, preferably a turbine, and to a mounting for such a rotor blade is provided. In the rotor blade, the two opposing lateral walls of the blade base are continuously curved along their extension between platform and bottom side of the blade base in order to...

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Bibliographic Details
Main Authors AHMAD FATHI, WALZ GÜNTHER
Format Patent
LanguageEnglish
Published 10.02.2015
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Summary:A rotor blade for an axial flow turbomachine, preferably a turbine, and to a mounting for such a rotor blade is provided. In the rotor blade, the two opposing lateral walls of the blade base are continuously curved along their extension between platform and bottom side of the blade base in order to reduce the mechanical load in the blade base and that of the walls supporting the blade base of a rotor.
Bibliography:Application Number: US201013378453