Radial compressor
A radial compressor having an impeller having a housing with a radially outer and a radially inner insertion section a main flow channel for suppling a medium towards the impeller, a circulation chamber radially outside of the main flow channel separated from the main flow channel by a contour wall and connected to the insertion section via struts. The main flow channel is delimited by the contour wall and by a first segment of the insertion section. The struts engage with a second segment of the insertion section. The second segment of the insertion section engages with a downstream end of the first segment of the insertion section. The upstream end of the first segment of the insertion section protrudes freely in the direction of the contour wall. The first segment of the insertion section has a constant thickness.
1. A radial compressor, comprising:
a rotor-side impeller;
a stator-side housing, comprising:
a radially outer spiral housing section; and
a radially inner insertion section;
a main flow channel configured to supply a medium to be compressed towards the rotor-side impeller;
a contour wall;
a circulation chamber arranged radially outside of the main flow channel, which is separated from the main flow channel by the contour wall, and which is connected to the main flow channel via a circulation opening in an area of the rotor-side impeller;
struts that extend in the circulation chamber and connect the circulation chamber to the insertion section;
a first segment of the insertion section delimits the main flow channel downstream from the contour wall, the main flow channel is delimited by the contour wall upstream of the first segment, wherein the upstream end of the first segment is configured to deform into the circulation chamber upon failure of rotor-side impeller;
a second segment of the insertion section at which the struts engage;
a downstream end of the first segment of the insertion section engages with the second segment of the insertion section;
an upstream end of the first segment of the insertion section protrudes freely towards the contour wall;
wherein viewed in a meridian section, the first segment of the insertion section has an approximately constant thickness with a thickness deviation of maximally 5% across its extension between the downstream end and the upstream end.
2. The radial compressor according to claim 1 , wherein the first segment of the insertion section on a first side, which faces the main flow channel, and on a second side, which faces away from the main flow channel is surface-treated to achieve the approximately constant thickness.
3. The radial compressor according to claim 1 , wherein the first segment of the insertion section has an approximately constant thickness with a thickness deviation of at least one of maximally 2%, and maximally 1%, across its extension between the downstream end and the upstream end.
4. The radial compressor according to claim 1 , wherein a material recess configured as a notch is formed in a transition area between the first segment of the insertion section and the second segment of the insertion section on a side, which faces away from the main flow channel.
5. The radial compressor according to claim 4 , wherein the insertion section is formed integrally.
6. The radial compressor according to claim 4 , wherein the insertion section is of multi-part design.
7. The radial compressor according to claim 4 , wherein the insertion section and the radially outer spiral housing section of the stator-side housing are separated on a component side, and are provided by individual components.
8. The radial compressor according to claim 1 , wherein the radial compressor is a radial compressor of an exhaust turbocharger.
9. The radial compressor according to claim 1 , wherein the first segment has a thickness of 10 mm.
10. The radial compressor according to claim 1 , wherein the first segment has a thickness of 10 mm.
11. The radial compressor according to claim 4 , wherein the material recess is a V-shaped notch.