| 摘要 |
The invention relates to a turbocharger (1) with variable turbine geometry (VTG), comprising a multiplicity of guide blades (7). Each guide blade (7) has a blade lever (19, 19′), wherein the center plane (Em2) of an intermediate region (24; 24′) of the blade lever (19, 19′) is arranged so as to be offset axially along a blade shaft longitudinal axis (L) at a distance (a) from the center plane (Em1) of a first end region (20; 20′) of the blade lever (19, 19′) and of a second end region (23; 23′) of the blade lever (19, 19′), and wherein a recess (26; 26′) is arranged adjacent to the intermediate region (24; 24′) between the first end region (20; 20′) and the second end region (23; 23′).
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