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 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).