Compressor having a sealing channel
A compressor having a housing and a rotor, the rotor having an impeller at least on one side; a compressor chamber being formed between the impeller and the housing, the rotor being rotationally mounted, an annular sealing channel being formed between the rotor and the housing, the sealing channel being routed from the compressor chamber to a zone having a lower pressure; a throttling section being provided in the sealing channel; the sealing section being configured in closer proximity to the low-pressure zone than to the compression chamber.
1. A compressor, comprising:
a housing;
a rotor having an impeller at least on one side;
wherein a compressor chamber is formed between the impeller and the housing, wherein the rotor is rotationally mounted about an axis of rotation,
wherein an annular sealing channel is formed between the rotor and the housing, and wherein the annular sealing channel is routed from the compressor chamber to a zone having a lower pressure,
wherein a throttling section is in the sealing channel, and
wherein the throttling section is configured in closer proximity to the low-pressure zone than to the compression chamber,
wherein the throttling section is configured in a zone having low-pressure as compared with other zones in the sealing channel having a higher pressure and in which a cross-sectional area of the sealing channel has a smallest cross section,
wherein, on a portion of the sealing channel that is configured from a center plane in a direction of the low-pressure zone, an outer side of a circumferential groove has a greater radial distance to the axis of rotation as compared with a mirror-symmetric side of the circumferential groove.
2. The compressor of claim 1 , wherein the throttling section is configured adjacently to a middle of the sealing channel in a first third of a second half of the sealing channel in closer proximity to the low-pressure zone.
3. The compressor of claim 1 , wherein the rotor has the circumferential groove in the sealing channel, wherein the housing has a circumferential web, wherein the circumferential web engages into the circumferential groove, and wherein at least one of the circumferential web and the circumferential groove are asymmetrically formed relative to a center plane of the circumferential groove so that the throttling section is configured in closer proximity to the low-pressure zone.
4. The compressor of claim 1 , wherein the housing has the circumferential groove, and wherein the rotor has a circumferential web, wherein the circumferential web engages into the circumferential groove, wherein the sealing channel is formed between the circumferential web and the circumferential groove, and wherein at least one of the circumferential web and the circumferential groove is asymmetrically formed relative to a center plane of the circumferential groove so as to allow the throttling section to be configured in closer proximity to the low-pressure zone compared to the compression chamber.
5. The compressor of claim 1 , wherein the impeller is configured on a first side of the rotor, wherein a second impeller is configured on a second side of the rotor, and wherein the impeller and the second impeller represent a first impeller stage and a second impeller stage.
6. The compressor of claim 1 , wherein the rotor is rotationally mounted on a bearing contactlessly, and wherein the bearing is configured between the housing and the rotor in the region of the sealing channel.
7. The compressor of claim 1 , wherein at least one portion of at least one of the housing and the rotor, which is adjacent to the sealing channel, includes a sealing element, which is formed of a softer material than the housing or the rotor.
8. The compressor of claim 1 , wherein at least one of the housing and the rotor in the region of the sealing channel have an asymmetrical shape relative to the center plane of the sealing channel.
9. A compressor, comprising:
a housing;
a rotor having an impeller at least on one side;
wherein a compressor chamber is formed between the impeller and the housing, wherein the rotor is rotationally mounted about an axis of rotation,
wherein an annular sealing channel is formed between the rotor and the housing, and wherein the annular sealing channel is routed from the compressor chamber to a zone having a lower pressure,
wherein a throttling section is in the sealing channel, and
wherein the throttling section is configured in closer proximity to the low-pressure zone than to the compression chamber,
wherein the rotor has a circumferential groove in the sealing channel, wherein the housing has a circumferential web, wherein the circumferential web engages into the circumferential groove, and wherein at least one of the circumferential web and the circumferential groove are asymmetrically formed relative to a center plane of the circumferential groove so that the throttling section is configured in closer proximity to the low-pressure zone,
wherein the circumferential web is laterally bounded by two annular shoulders, a first shoulder being adjacent to the low-pressure zone, a second shoulder being adjacent to a high-pressure zone, and wherein the first shoulder is more radially distant from the axis of rotation than is the second shoulder.