Dynamic sealing labyrinth seals

1. A compression ring for a shrouded compressor, the compression ring comprising:

a radially inner surface having one or more areas configured to mate flush with one or more portions of a radially outward surface of a shroud of the shrouded compressor;

a radially outer surface located opposite the radially inner surface;

a labyrinth seal located on the radially outer surface;

a groove located within the radially inner surface; and

a load ring located within the groove.

2. The compression ring of claim 1 , wherein the compression ring has a first density and the load ring has a second density that is greater than the first density.

3. The compression ring of claim 1 , wherein the groove and the load ring are located radially inward of the labyrinth seal.

4. The compression ring of claim 1 , wherein the compression ring is composed of three sections including a first section, a second section, and a third section located between the first section and the second section, wherein the labyrinth seal, the groove, and the load ring are located within the first section.

5. The compression ring of claim 4 , wherein the first section has a first average thickness and the third section has a third average thickness, and wherein the first average thickness is less than the third average thickness.

6. A compressor assembly, comprising:

a compressor, comprising:

a central shaft comprising an external surface;

a shroud extending circumferentially around the central shaft, the shroud comprising a radially inward surface and a radially outward surface located opposite the radially inward surface, wherein the external surface of the central shaft and the radially inward surface of the shroud are in a facing spaced relationship forming a core flow path therebetween; and

a plurality of blades extending from the central shaft to the shroud; and

a compression ring extending circumferentially around the shroud, the compression ring comprising:

a radially inner surface;

a radially outer surface located opposite the radially inner surface;

a labyrinth seal located on the radially outer surface;

a groove located within the radially inner surface; and

a load ring located within the groove.

7. The compressor assembly of claim 6 , wherein the compression ring has a first density and the load ring has a second density that is greater than the first density.

8. The compressor assembly of claim 6 , wherein the groove and the load ring are located radially inward of the labyrinth seal.

9. The compressor assembly of claim 6 , wherein the compression ring is composed of three sections including a first section, a second section, and a third section located between the first section and the second section, wherein the labyrinth seal, the groove, and the load ring are located within the first section.

10. The compressor assembly of claim 9 , wherein the first section has a first average thickness and the third section has a third average thickness, and wherein the first average thickness is less than the third average thickness.

11. The compressor assembly of claim 9 , wherein the third section is in contact with the compressor and the first section is not in contact with the compressor.

12. The compressor assembly of claim 6 , wherein the compression ring is in an interference fit with the shroud, and

wherein the compression ring is configured to apply a radially inward compressive force along one or more portions of the radially outward surface of the shroud, the radially inward compressive force is configured to compress the shroud and the plurality of blades into the central shaft.

13. The compressor assembly of claim 6 , wherein the compressor has a first tensile strength, and wherein the compression ring has a second tensile strength that is greater than the first tensile strength.

14. An electrical power generation system, comprising:

a frame;

a labyrinth seal mating ring operably attached to the frame; and

a micro-turbine alternator, comprising:

a combustion chamber;

at least one turbine driven by combustion gases from the combustion chamber;

a compressor operably connected to the combustion chamber to provide a compressed airflow thereto;

one or more shafts connecting the at least one turbine to the compressor such that rotation of the at least one turbine drives rotation of the first stage compressor and the second stage compressor; and

an electric generator disposed along the one or more shafts such that electrical power is generated via rotation of the one or more shafts,

wherein the compressor comprises

a central shaft comprising an external surface;

a shroud extending circumferentially around the central shaft, the shroud comprising a radially inward surface and a radially outward surface located opposite the radially inward surface, wherein the external surface of the central shaft and the radially inward surface of the shroud are in a facing spaced relationship forming a core flow path therebetween; and

a plurality of blades extending from the central shaft to the shroud; and

a compression ring extending circumferentially around the shroud, the compression ring comprising:

a radially inner surface;

a radially outer surface located opposite the radially inner surface;

a labyrinth seal located on the radially outer surface, the labyrinth seal being in a facing spaced relationship with the labyrinth seal mating ring defining a radial gap therebetween;

a groove located within the radially inner surface; and

a load ring located within the groove,

wherein the labyrinth seal is configured reduce the radial gap, using a centrifugal force generated by the load ring as a rotational speed of the compressor assembly increases.

15. The electrical power generation system of claim 14 , wherein the compression ring has a first density and the load ring has a second density that is greater than the first density.

16. The electrical power generation system of claim 14 , wherein the groove and the load ring are located radially inward of the labyrinth seal.

17. The electrical power generation system of claim 14 , wherein the compression ring is composed of three sections including a first section, a second section, and a third section located between the first section and the second section, wherein the labyrinth seal, the groove, and the load ring are located within the first section.

18. The electrical power generation system of claim 17 , wherein the first section has a first average thickness and the third section has a third average thickness, and wherein the first average thickness is less than the third average thickness.

19. The electrical power generation system of claim 17 , wherein the third section is in contact with the compressor and the first section is not in contact with the compressor.

20. The electrical power generation system of claim 14 , wherein the compression ring is in an interference fit with the shroud, and

wherein the compression ring is configured to apply a radially inward compressive force along one or more portions of the radially outward surface of the shroud, the radially inward compressive force is configured to compress the shroud and the plurality of blades into the central shaft.