Filter muffler for an exhaust gas turbocharger of an internal combustion engine

1. A filter muffler arranged on an intake side of a compressor of an exhaust gas turbocharger for an internal combustion engine, the filter muffler comprising:

a front element,

a rear element, and

a plurality of damping elements arranged between the front element and the rear element,

wherein the damping elements are arranged radially around a central axis of the filter muffler such that a flow channel is formed between adjacent damping elements, wherein respective outflow-side ends of the damping elements have a diffuser element which has an outflow-side tapering toward the central axis, wherein the outflow-side tapering is continuous and meets to form the outflow-side ends, and wherein an angle α between two opposite sides of the diffuser element is selected from a range of 1°≤α≤8°.

2. The filter muffler of claim 1 , wherein the flow channel has an increasing flow cross-section on the outflow side.

3. The filter muffler of claim 1 , wherein the flow channel is delimited by respective involute contours of adjacent damping elements over at least 40% of the flow channel length.

4. The filter muffler of claim 3 , wherein the respective involute contours of the damping elements are formed between a radially outer inflow-side end and a radially inner outflow-side end of the damping elements.

5. The filter muffler of claim 4 , wherein the respective inflow-side ends of the damping elements, in relation to the respective involute contours, have a rear curvature in the circumferential direction.

6. The filter muffler of claim 1 , wherein the tapering runs toward an outflow edge of the diffuser element and leads at the outflow edge to a reduction in thickness of the damping element of at least 50%.

7. The filter muffler of claim 1 , wherein the damping elements are configured such that a cross-section of an inflow region of the respective flow channels between adjacent damping elements becomes smaller in the direction of flow.

8. The filter muffler of claim 1 , wherein the damping elements are configured such that a cross-section of the respective flow channels in a region which is delimited by involute contours of adjacent damping elements is constant in the direction of flow.

9. The filter muffler of claim 1 , wherein the damping elements are configured such that a cross-section of an outflow region of the respective flow channels between adjacent damping elements becomes larger in the direction of flow.

10. The filter muffler of claim 1 , wherein the flow channel is delimited by respective involute contours of adjacent damping elements over at least 50% of the flow channel length.

11. The filter muffler of claim 3 , wherein a distance D between the respective involute contours of adjacent damping elements is selected from a range of 2 mm≤D≤30 mm.

12. The filter muffler of claim 1 , wherein the respective damping elements have a first involute contour and a second involute contour parallel to the first involute contour, and wherein a distance T between the first involute contour and the second involute contour is selected from a range of 6 mm≤T≤50 mm.

13. The filter muffler of claim 1 , wherein respective inflow-side ends of the damping elements have a rear curvature in the circumferential direction.

14. The filter muffler of claim 1 , wherein the tapering runs toward an outflow edge of the diffuser element and leads at the outflow edge to a reduction in thickness of the damping element of at least 20%.

15. The filter muffler of claim 14 , wherein the damping elements are configured such that a cross-section of an outflow region of the respective flow channels between adjacent damping elements becomes larger in the direction of flow.

16. The filter muffler of claim 6 , wherein the damping elements are configured such that a cross-section of an outflow region of the respective flow channels between adjacent damping elements becomes larger in the direction of flow.

17. The filter muffler of claim 1 , wherein the flow channel is delimited by respective involute contours of adjacent damping elements over at least 65% of the flow channel length.

18. The filter muffler of claim 3 , wherein a distance D between the respective involute contours of adjacent damping elements is selected from a range of 5 mm≤D≤25 mm.

19. An exhaust gas turbocharger for an internal combustion engine, the gas turbocharger comprising:

a compressor having an intake side, and

a filter muffler arranged on the intake side of the compressor, the filter muffler comprising a front element, a rear element, and a plurality of damping elements arranged between the front element and the rear element, wherein the damping elements are arranged radially around a central axis of the filter muffler such that a flow channel is formed between adjacent damping elements, wherein respective outflow-side ends of the damping elements have a diffuser element which has an outflow-side tapering toward the central axis, wherein the outflow-side tapering is continuous and meets to form the outflow-side ends, and wherein an angle α between two opposite sides of the diffuser element is selected from a range of 1°≤α≤8°.

20. An internal combustion engine comprising:

an exhaust gas turbocharger comprising:

a compressor having an intake side, and

a filter muffler arranged on the intake side of the compressor, the filter muffler comprising a front element, a rear element, and a plurality of damping elements arranged between the front element and the rear element, wherein the damping elements are arranged radially around a central axis of the filter muffler such that a flow channel is formed between adjacent damping elements, wherein respective outflow-side ends of the damping elements have a diffuser element which has an outflow-side tapering toward the central axis, wherein the outflow-side tapering is continuous and meets to form the outflow-side ends, and wherein an angle α between two opposite sides of the diffuser element is selected from a range of 1°≤α≤8°.