| 摘要 |
A disc damper for a charge air line of an internal combustion engine that has a turbocharger. The disc damper includes an inlet, an outlet, and at least one slit chamber disposed between the inlet and outlet. Starting from the inlet, at least two gap chambers are provided downstream of the slit chamber and disposed axially one after the other. At least one of the following features is fulfilled: a) the slit chamber has a radial inner dimension that changes in the circumferential direction and/or b) the slit chamber has axial inner dimensions that change in the circumferential direction, and/or at least one gap chamber comprises radial inner dimensions that change in the circumferential direction.
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