Centrifugal compressor with heat exchanger

1. A centrifugal compressor comprising:

a rotary shaft of a compressor impeller;

a gas bearing structure that supports the rotary shaft, wherein the gas bearing structure includes a thrust bearing and a radial bearing;

a motor that rotates the rotary shaft;

a motor housing that houses the motor;

a compressor housing that houses the compressor impeller and includes a discharge port configured to discharge compressed gas;

a gas bleed port fluidly coupled to the discharge port in the compressor housing;

a bearing cooling line that fluidly couples the gas bleed port to the gas bearing structure, wherein the bearing cooling line includes a first cooling path that passes through the thrust bearing, and a second cooling path that passes through the radial bearing, wherein an outlet of the first cooling path and an outlet of the second cooling path are formed at the motor housing, and wherein a cross-sectional flow area at the outlet of the second cooling path is smaller than a cross-sectional flow area at the outlet of the first cooling path; and

a heat exchanger including a gas flow passage that forms a portion of the bearing cooling line, wherein the heat exchanger is mounted on at least one of the motor housing and the compressor housing, and wherein the heat exchanger is configured to remove heat from the compressed gas that passes through the gas flow passage.

2. The centrifugal compressor according to claim 1 ,

wherein the heat exchanger further includes a refrigerant flow passage configured to contain a refrigerant that is maintained at a lower temperature than the compressed gas contained in the gas flow passage,

wherein the gas flow passage includes an inlet and an outlet for the compressed gas, and

wherein a distance between the inlet and the compressor impeller is less than a distance between the outlet and the compressor impeller, in a direction along the rotary shaft.

3. The centrifugal compressor according to claim 1 ,

wherein the thrust bearing is located on an opposite side of the motor from the radial bearing, and

wherein the second cooling path passes through the radial bearing without passing through the thrust bearing.

4. The centrifugal compressor according to claim 3 ,

wherein the gas bearing structure includes a second radial bearing located between the motor and the thrust bearing along an axial direction of the rotary shaft, and

wherein the first cooling path passes through both the thrust bearing and the second radial bearing.

5. The centrifugal compressor according to claim 1 ,

wherein a first end of the motor housing is located adjacent the compressor housing, and

wherein the outlet of the first cooling path and the outlet of the second cooling path are located at a second end of the motor housing that is opposite the first end of the motor housing along an axial direction of the rotary shaft.

6. The centrifugal compressor according to claim 1 , further comprising a first orifice that is located at the outlet of the first cooling path and a second orifice that is located at the outlet of the second cooling path,

wherein an orifice diameter of the first orifice is larger than an orifice diameter of the second orifice.

7. A centrifugal compressor comprising:

a rotary shaft of a compressor impeller;

a motor that rotates the rotary shaft;

a motor housing that houses the motor;

a gas bearing structure that supports the rotary shaft, wherein the gas bearing structure includes a thrust bearing and a radial bearing, and wherein the thrust bearing is located on an opposite side of the motor from the radial bearing;

a compressor housing that houses the compressor impeller and includes a discharge port configured to discharge compressed gas;

a gas bleed port fluidly coupled to the discharge port in the compressor housing; and

a bearing cooling line that fluidly couples the gas bleed port to the gas bearing structure,

wherein the bearing cooling line includes a first cooling path and a second cooling path that are fluidly coupled to a shaft space within the motor housing which at least partially surrounds the rotary shaft,

wherein the first cooling path passes through the thrust bearing and through a first end portion of the shaft space which surrounds the rotary shaft at a first end of the motor housing that is adjacent the compressor housing,

wherein the second cooling path passes through the radial bearing and through a second end portion of the shaft space which surrounds the rotary shaft at a second end of the motor housing that is opposite the first end of the motor housing along an axial direction of the rotary shaft, and

wherein an outlet of each of the first cooling path and the second cooling path is located at the second end of the motor housing.

8. The centrifugal compressor according to claim 7 , further comprising a turbine housing,

wherein both the first cooling path and the second cooling path fluidly couple the turbine housing to the shaft space, and

wherein the second end of the motor housing is adjacent the turbine housing.

9. The centrifugal compressor according to claim 7 ,

wherein the motor housing comprises a bearing housing that houses the thrust bearing,

wherein the thrust bearing comprises a thrust collar fixed to the rotary shaft, and an annular bearing body fixed to the bearing housing,

wherein the first cooling path passes through a gap formed between the thrust collar and the annular bearing body, and

wherein the second cooling path passes through the radial bearing without passing through the thrust bearing.

10. A centrifugal compressor comprising:

a rotary shaft of a compressor impeller;

a gas bearing structure that supports the rotary shaft;

a bearing housing that houses the gas bearing structure;

a motor that rotates the rotary shaft;

a motor housing that houses the motor, wherein the motor housing comprising a stator housing that houses a stator of the motor;

a compressor housing that at least partially houses the compressor impeller;

a bearing cooling line configured to supply compressed gas from the compressor impeller to the gas bearing structure; and

a heat exchanger including a gas flow passage that forms a portion of the bearing cooling line,

wherein an inlet of the gas flow passage is connected to the bearing housing,

wherein an outlet of the gas flow passage is connected to the stator housing,

wherein the heat exchanger is mounted on at least one of the motor housing and the compressor housing, and

wherein the heat exchanger is configured to remove heat from the compressed gas that passes through the gas flow passage.

11. The centrifugal compressor according to claim 10 ,

wherein the heat exchanger is mounted on the motor housing so as to extend across the stator housing and the bearing housing along an axial direction of the rotary shaft.

12. The centrifugal compressor according to claim 10 ,

wherein the gas bearing structure includes a thrust bearing and a radial bearing, and

wherein the bearing cooling line includes a first cooling path that passes through the thrust bearing, and a second cooling path that passes through the radial bearing.

13. The centrifugal compressor according to claim 12 ,

wherein the thrust bearing is located on an opposite side of the motor from the radial bearing, and

wherein the second cooling path passes through the radial bearing without passing through the thrust bearing.

14. The centrifugal compressor according to claim 12 ,

wherein the thrust bearing comprises a thrust collar fixed to the rotary shaft, and an annular bearing body fixed to the bearing housing, and

wherein the first cooling path passes through a gap formed between the thrust collar and the annular bearing body.

15. A centrifugal compressor comprising:

a rotary shaft of a compressor impeller;

a turbine including a turbine impeller configured to rotate the rotary shaft;

a turbine housing that houses the turbine impeller;

a gas bearing structure that supports the rotary shaft;

a motor that rotates the rotary shaft;

a motor housing that houses the motor;

a compressor housing that at least partially houses the compressor impeller; and

a bearing cooling line configured to supply compressed gas from the compressor impeller to the gas bearing structure,

wherein the bearing cooling line includes a first cooling path and a second cooling path that are fluidly coupled to a shaft space within the motor housing which at least partially surrounds the rotary shaft,

wherein the first cooling path passes through a first end portion of the shaft space which surrounds the rotary shaft at a first end of the motor housing that is adjacent the compressor housing,

wherein the second cooling path passes through a second end portion of the shaft space which surrounds the rotary shaft at a second end of the motor housing that is opposite the first end of the motor housing along an axial direction of the rotary shaft,

wherein an outlet of each of the first cooling path and the second cooling path is located at the second end of the motor housing that is adjacent the turbine housing, and

wherein both the first cooling path and the second cooling path fluidly couple the turbine housing to the shaft space.

16. The centrifugal compressor according to claim 15 ,

wherein the first cooling path and the second cooling path fluidly couple the turbine housing to the gas bearing structure.

17. The centrifugal compressor according to claim 16 ,

wherein a second cross-sectional flow area at the outlet of the second cooling path is smaller than a first cross-sectional flow area at the outlet of the first cooling path so as to reduce a flow rate of the compressed gas through the second cooling path as compared to the first cooling path.

18. The centrifugal compressor according to claim 17 , further comprising an orifice located in the second cooling path and having the second cross-sectional flow area.

19. The centrifugal compressor according to claim 16 ,

wherein the gas bearing structure comprises a radial bearing and a thrust bearing that is disposed between the radial bearing and the compressor impeller along the axial direction of the rotary shaft,

wherein the motor housing comprises a bearing housing that houses the thrust bearing and the radial bearing,

wherein the thrust bearing comprises a thrust collar fixed to the rotary shaft, and an annular bearing body fixed to the bearing housing, and

wherein the first cooling path passes through a gap formed between the thrust collar and the annular bearing body.

20. The centrifugal compressor according to claim 19 ,

wherein the motor housing comprising a stator housing that houses a stator of the motor,

wherein the gas bearing structure includes a second radial bearing located in the stator housing, and

wherein the second cooling path passes through the second radial bearing without passing through the gap formed between the thrust collar and the annular bearing body, and without passing through the radial bearing located in the bearing housing.