Journal and thrust gas bearing

1. A bearing, comprising:

a thrust gas bearing attached to a journal bearing; and

two or more converging-diverging orifices defined in a surface of at least one of the thrust gas bearing and the journal bearing,

wherein the converging-diverging orifices supply at least one pressurized gas to an interior of the bearing, and

wherein the thrust gas bearing is configured to accommodate a hydrostatic injection of the at least one pressurized gas to form a gas seal within the thrust gas bearing.

2. The bearing according to claim 1 , wherein the at least one pressurized gas comprises a process gas.

3. The bearing according to claim 1 , wherein the converging-diverging orifices each comprise a throat, each orifice being configured to cause a flow of the at least one pressurized gas in the throat of the orifice to have a velocity of Mach 1 and to cause a flow of the at least one pressurized gas beyond the throat to have a supersonic velocity.

4. The bearing according to claim 1 , wherein the thrust gas bearing comprises hydrodynamic lifting grooves on a surface of the thrust gas bearing, the hydrodynamic lifting grooves being configured to create a gas seal.

5. The bearing according to claim 1 , wherein an edge of an inner surface of the journal bearing comprises a plurality of grooves defined therein, the grooves having a geometry that creates a high pressure region at the edge of the journal bearing.

6. The bearing according to claim 1 , wherein the converging-diverging orifices comprise at least one inboard orifice and at least one outboard orifice and the at least one pressurized gas comprises a process gas supplied through the at least one inboard orifice and a clean air gas supplied through the at least one outboard orifice, and

wherein when the process gas has a higher pressure than the clean air gas, the process gas prevents the clean air gas from leaking into the bearing.

7. The bearing according to claim 1 , wherein the converging-diverging orifices comprise at least one inboard orifice and at least one outboard orifice and the at least one pressurized gas comprises a process gas supplied through the at least one inboard orifice and a clean air gas supplied through the at least one outboard orifice, and

wherein when the clean air gas has a higher pressure than the process gas, the clean air gas prevents the process gas from leaking out of the bearing.

8. The bearing according to claim 1 , wherein the converging-diverging orifices comprise at least one inboard orifice, at least one outboard orifice, and at least one seal gas orifice located between the at least one inboard orifice and the at least outboard orifice, and the at least one pressurized gas comprises a process gas supplied through the at least one inboard orifice, a clean air gas supplied through the at least one outboard orifice, and a seal gas supplied through the at least one seal gas orifice, and

wherein when the seal gas has a higher pressure than the process gas and the clean air gas, the seal gas prevents the process gas from leaking out of the bearing.

9. The bearing according to claim 1 , wherein a metal mesh damper is provided on an outside surface of the bearing.

10. A turbomachine, comprising:

a casing having an inlet end and an outlet end opposite the inlet end along a longitudinal axis of the casing;

a shaft disposed within the casing, the shaft extending from the inlet end to the outlet end of the casing;

at least one rotor extending radially outward from the shaft; and

at least one bearing, the at least one bearing comprising:

a thrust gas bearing attached to a journal bearing; and

two or more converging-diverging orifices defined in a surface of at least one of the thrust gas bearing and the journal bearing,

wherein the converging-diverging orifices supply at least one pressurized gas to an interior of the bearing,

wherein the rotor is encased within the thrust gas bearing,

wherein the shaft is at least partially encased within the journal bearing, and

wherein the thrust gas bearing is configured to accommodate a hydrostatic injection of the at least one pressurized gas to form a gas seal within the thrust gas bearing.

11. The turbomachine according to claim 10 , wherein the at least one pressurized gas comprises a process gas.

12. The turbomachine according to claim 10 , wherein the converging-diverging orifices each comprise a throat, each orifice being configured to cause a flow of the at least one pressurized gas in the throat of the orifice to have a velocity of Mach 1 and to cause a flow of the at least one pressurized gas beyond the throat to have a supersonic velocity.

13. The turbomachine according to claim 10 , wherein the thrust gas bearing comprises hydrodynamic lifting grooves on a surface of the thrust gas bearing, the hydrodynamic lifting grooves being configured to create a gas seal.

14. The turbomachine according to claim 10 , wherein an edge of an inner surface of the journal bearing comprises a plurality of grooves defined therein, the grooves having a geometry that creates a high pressure region at the edge of the journal bearing.

15. The turbomachine according to claim 10 , wherein the converging-diverging orifices comprise at least one inboard orifice and at least one outboard orifice and the at least one pressurized gas comprises a process gas supplied through the at least one inboard orifice and a clean air gas supplied through the at least one outboard orifice, and

wherein when the process gas has a higher pressure than the clean air gas, the process gas prevents the clean air gas from leaking into the bearing.

16. The turbomachine according to claim 10 , wherein the converging-diverging orifices comprise at least one inboard orifice and at least one outboard orifice and the at least one pressurized gas comprises a process gas supplied through the at least one inboard orifice and a clean air gas supplied through the at least one outboard orifice, and

wherein when the clean air gas has a higher pressure than the process gas, the clean air gas prevents the process gas from leaking out of the bearing.

17. The turbomachine according to claim 10 , wherein the converging-diverging orifices comprise at least one inboard orifice, at least one outboard orifice, and at least one seal gas orifice located between the at least one inboard orifice and the at least outboard orifice, and the at least one pressurized gas comprises a process gas supplied through the at least one inboard orifice, a clean air gas supplied through the at least one outboard orifice, and a seal gas supplied through the at least one seal gas orifice, and

wherein when the seal gas has a higher pressure than the process gas and the clean air gas, the seal gas prevents the process gas from leaking out of the bearing.

18. The turbomachine according to claim 10 , further comprising a metal mesh damper provided on an outside surface of the bearing.