Turbocharger with air journal bearing and thrust bearing
A turbomachine such as a turbocharger with an air journal bearing and an air thrust bearing arrangement with a fixed air journal bearing connected in series with a floating air journal bearing connected by a hollow spring to supply compressed air from the fixed air journal bearing to the floating air journal bearing, and a forward air thrust bearing and an aft air thrust bearing connected in parallel to a source of compressed air. An air vent cavity is formed between the forward bearing and the aft bearing in which compressed air from all four bearings can be collected and discharged from a housing. Some of the compressed air from the forward thrust bearing is discharged with a compressor outlet, and some of the compressed air from the aft thrust bearing is discharged into a turbine inlet.
1. An air journal bearing assembly for a turbomachine comprising:
a fixed air journal bearing on a rotor;
a floating air journal bearing on the rotor;
a hollow spring connecting the fixed air journal bearing to the floating air journal bearing;
the hollow spring connected to the fixed air journal bearing to support the rotor; and,
the hollow spring supplies compressed air from the fixed air journal bearing in series with the floating air journal bearing to rotatably support the rotor.
2. The air journal bearing of claim 1 , and further comprising:
the fixed air journal bearing includes a radial compressed air inlet passage for compressed air that opens into a plurality of aft bearing pressure pockets;
the fixed air journal bearing also includes an axial compressed air passage connected to the radial compressed air inlet passage and to the hollow spring;
the floating air journal bearing includes a radial compressed air outlet passage connected to a plurality of forward bearing pressure pockets; and,
the floating air journal bearing also includes an axial compressed air passage connecting the hollow spring to the radial compressed air outlet passage.
3. The air journal bearing of claim 2 , and further comprising:
an air vent cavity located between the floating air journal bearing and the fixed air journal bearing to collect some of the compressed air from the forward bearing and the aft bearing pressure pockets.
4. The air journal bearing of claim 2 , and further comprising:
a forward bearing collection groove adjacent to the forward air journal bearing to collect some of the compressed air from the forward bearing pressure pockets;
an aft bearing collection groove adjacent to the aft air journal bearing to collect some of the compressed air from the aft bearing pressure pockets;
a forward bearing return air passage to collect some of the compressed air from the forward bearing pressure pockets;
an aft bearing return air passage to collect some of the compressed air from the aft bearing pressure pockets; and,
an air vent cavity located between the floating air journal bearing and the fixed air journal bearing to collect some of the compressed air from the forward bearing and the aft bearing return air passages.
5. The air journal bearing of claim 1 , and further comprising:
a forward air thrust bearing;
an aft air thrust bearing;
a forward air thrust bearing compressed air supply passage opening into a forward air thrust bearing cavity;
an aft air thrust bearing compressed air supply passage opening into an aft air thrust bearing cavity; and,
a compressed air supply port connected to the forward and aft air thrust bearing compressed air supply passages.
6. The air journal bearing of claim 5 , and further comprising:
a forward bearing compressed air discharge passage connected to the forward air thrust bearing cavity to an outlet of a compressor; and,
an aft bearing compressed air discharge passage connected to the aft air thrust bearing cavity to an inlet of a turbine.
7. The air journal bearing of claim 1 , and further comprising:
the floating air journal bearing is mounted within an annular damper ring that has a stiffness of substantially ten times a stiffness of the hollow spring.
8. A turbomachine comprising:
a compressor connected to a turbine through a rotor;
a housing;
a forward air journal bearing and a forward air thrust bearing to support the rotor on the compressor side;
an aft air journal bearing and an aft air thrust bearing to support the rotor on the turbine side;
the aft air journal bearing being a fixed air journal bearing;
the forward air journal bearing being a floating air journal bearing; and,
a hollow spring connecting the fixed air journal bearing to the floating air journal bearing such that compressed air for the floating air journal bearing flows through the hollow spring from the fixed air journal bearing.
9. The turbomachine of claim 8 , and further comprising:
a first compressed air inlet port on the housing and connected to the fixed air journal bearing; and,
a second compressed air inlet port on the housing and connected in parallel to the forward and the aft air thrust bearings.
10. The turbomachine of claim 9 , and further comprising:
the fixed air journal bearing includes a radial compressed air inlet passage for compressed air that opens into a plurality of aft bearing pressure pockets;
the fixed air journal bearing also includes an axial compressed air passage connected to the radial compressed air inlet passage and to the hollow spring;
the floating air journal bearing includes a radial compressed air outlet passage connected to a plurality of forward bearing pressure pockets; and,
the floating air journal bearing also includes an axial compressed air passage connecting the hollow spring to the radial compressed air outlet passage.
11. The turbomachine of claim 9 , and further comprising:
an air vent cavity located between the floating air journal bearing and the fixed air journal bearing to collect some of the compressed air from the forward bearing and the aft bearing pressure pockets.
12. The turbomachine of claim 8 , and further comprising:
a forward bearing collection groove adjacent to the forward air journal bearing to collect some of the compressed air from the forward bearing pressure pockets;
an aft bearing collection groove adjacent to the aft air journal bearing to collect some of the compressed air from the aft bearing pressure pockets;
a forward bearing return air passage to collect some of the compressed air from the forward bearing pressure pockets;
an aft bearing return air passage to collect some of the compressed air from the aft bearing pressure pockets; and,
an air vent cavity located between the floating air journal bearing and the fixed air journal bearing to collect some of the compressed air from the forward bearing and the aft bearing return air passages.
13. The turbomachine of claim 8 , and further comprising:
a forward air thrust bearing;
an aft air thrust bearing;
a forward air thrust bearing compressed air supply passage opening into a forward air thrust bearing cavity;
an aft air thrust bearing compressed air supply passage opening into an aft air thrust bearing cavity; and,
a compressed air supply port connected to the forward and aft air thrust bearing compressed air supply passages.
14. The turbomachine of claim 13 , and further comprising:
a forward bearing compressed air discharge passage connected to the forward air thrust bearing cavity to an outlet of a compressor; and,
an aft bearing compressed air discharge passage connected to the aft air thrust bearing cavity to an inlet of a turbine.
15. The turbomachine of claim 11 , and further comprising:
an air discharge port on the housing connected to the air vent cavity.
16. The turbomachine of claim 12 , and further comprising:
an air discharge port on the housing connected to the air vent cavity.
17. The turbomachine of claim 8 , and further comprising:
the floating air journal bearing is mounted within an annular damper ring that has a stiffness of substantially ten times a stiffness of the hollow spring.