ROTOR BLADE FOR A TURBOMACHINE AND CORRESPONDING TURBOMACHINE
Rotor blades (30) and turbomachines are provided. The rotor blade (30) includes a main body (35) having a shank (38), an airfoil (36) extending radially outwardly from the shank (38), and a platform (42). The main body (35) further includes a pressure-side slash face (56) and a suction-side slash fa...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | Rotor blades (30) and turbomachines are provided. The rotor blade (30) includes a main body (35) having a shank (38), an airfoil (36) extending radially outwardly from the shank (38), and a platform (42). The main body (35) further includes a pressure-side slash face (56) and a suction-side slash face (58). Each of the pressure-side slash face (56) and the suction-side slash face (58) includes a damper land (90), (120) and defines a slot (70). The damper land (90), (120) is disposed radially inward from the slot (70). |
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