主权项 |
1. A mixed flow turbine wheel (1) for a turbocharger comprising:
a hub (6) extending in an axial direction between a nose (10) and a partial back wall (9), said back wall (9) including a peripheral edge (11), wherein said hub (6) defines an axis of rotation (4) extending in said axial direction; a plurality of turbine blades (7), which extend beyond said peripheral edge (11) of said partial back wall (9) are coupled to said hub (6) and disposed in a circumferential direction generally at equal intervals around said axis of rotation (4); and at least one scallop cut (5) formed in said peripheral edge (11) of said partial back wall (9) for balancing said turbine wheel (1), wherein said at least one scallop cut (5) is positioned along said peripheral edge (11) such that said peripheral edge (11) is not symmetrical in said circumferential direction about said axis of rotation (4). |