OUTFLOW REGION OF A COMPRESSOR, COMPRESSOR HAVING AN OUTFLOW REGION OF SAID TYPE, AND TURBOCHARGER HAVING THE COMPRESSOR
Disclosed is an outflow region of a compressor. The outflow region comprises a flow channel delimited by a side wall at a shroud side and a side wall at a hub side. The side wall at the hub side has, in a region of the compressor wheel outlet, a contour configured such that, in a flow direction, the...
Saved in:
Main Author | |
---|---|
Format | Patent |
Language | English |
Published |
02.11.2023
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | Disclosed is an outflow region of a compressor. The outflow region comprises a flow channel delimited by a side wall at a shroud side and a side wall at a hub side. The side wall at the hub side has, in a region of the compressor wheel outlet, a contour configured such that, in a flow direction, the cross-sectional areas of the flow channel decrease, pass through a minimum and increase again. In the region of the compressor wheel outlet, the flow channel has a length L which extends from a compressor wheel outlet edge to a diffuser blade inlet edge of a diffuser region. The diffuser region adjoins the region of the compressor wheel outlet and has multiple diffuser blades. Also disclosed is a compressor with the outflow region according to the invention, and to a turbocharger having the compressor. |
---|---|
Bibliography: | Application Number: US202117791331 |