Impeller for an exhaust gas turbocharger, exhaust gas turbocharger and method for balancing a rotor arrangement of an exhaust gas turbocharger
A technology for exhaust gas turbines and compressor rotors, which is applied to components of pumping devices for elastic fluids, gas turbine devices, static/dynamic balance testing, etc., to achieve the effect of reducing scrap rate
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[0028] The impeller 1 of a rotor arrangement 2 for an exhaust gas turbocharger 3 according to the prior art is designed according to FIG. 1 . The impeller 1 is designed in the form of a compressor rotor. The rotor arrangement 2 comprises a compressor rotor 1 and a turbine rotor (not shown in detail), which is connected in a rotationally fixed manner to the compressor rotor 1 via a shaft (not shown in detail).
[0029] The rotor arrangement 2 is mounted rotatably in a bearing section (not shown in detail) of the exhaust gas turbocharger 3 about a rotation axis (not shown in detail) of the rotor arrangement 2 . The turbine rotor is accommodated rotatably in a non-detailed exhaust gas guide section of the exhaust gas turbocharger 3 through which flow can flow. The turbine rotor is impinged on and rotated by exhaust gas from an internal combustion engine, not shown in detail, which is flow-through-connected to the exhaust gas turbocharger 3 , via inlet channels (not shown) of the...
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