A rotor blade for an axial flow turbomachine and mounting for such a rotor blade
The invention relates to a rotor blade (10) for an axial flow turbomachine, preferably a turbine, and to a mounting for such a rotor blade (10). In said rotor blade (10), the two opposing lateral walls (20, 22) of the blade base (16) are continuously curved along their extension between platform (14...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention relates to a rotor blade (10) for an axial flow turbomachine, preferably a turbine, and to a mounting for such a rotor blade (10). In said rotor blade (10), the two opposing lateral walls (20, 22) of the blade base (16) are continuously curved along their extension between platform (14) and bottom side (18) of the blade base in order to reduce the mechanical load in the blade base (16) and that of the walls (30, 32) supporting said blade base of a rotor. |
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