Abradable labyrinth seal for refrigerant compressors
A compressor according to an exemplary aspect of the present disclosure includes, among other things, a rotor configured to rotate with respect to a stator, the stator having an abradable portion. At least one labyrinth seal is between the rotor and the stator, wherein the labyrinth seal comprises a plurality of teeth extending from the rotor toward the abradable portion.
1. A compressor, comprising:
a rotor configured to rotate with respect to a stator, the stator having an abradable portion;
at least one labyrinth seal between the rotor and the stator, wherein the labyrinth seal comprises a plurality of teeth extending from the rotor toward the abradable portion.
2. The compressor as recited claim 1 , wherein the plurality of teeth are provided in a stepped arrangement.
3. The compressor as recited in claim 1 , wherein the plurality of teeth are arranged in three groups separated by radial steps.
4. The compressor as recited in claim 1 , wherein the abradable portion is made of one of PTFE, polyamide, and a low strength alloy.
5. The compressor as recited in claim 1 , wherein the plurality of teeth are configured to contact the abradable portion and carve tracks into the abradable portion over time.
6. The compressor as recited in claim 1 , wherein a flow path is defined through the labyrinth seal and a discharge path is arranged downstream of the labyrinth seal.
7. The compressor as recited in claim 1 , wherein a flow path is defined through the labyrinth seal and a debris trap is arranged downstream of the labyrinth seal.
8. The compressor as recited claim 1 , wherein the labyrinth seal is arranged at a first location, and a second labyrinth seal is arranged at a second location between the rotor and the stator.
9. The compressor as recited in claim 1 , wherein the rotor comprises an impeller, the stator is a housing, and the labyrinth seal is arranged between an outer diameter of the impeller and the housing.
10. The compressor as recited in claim 1 , wherein the rotor comprises an impeller and the labyrinth seal is arranged at an inner diameter of the impeller.
11. The compressor as recited in claim 1 , wherein the rotor rotates on a shaft that is driven by a motor.
12. The compressor as recited in claim 1 , wherein the compressor is a two stage compressor.
13. The compressor as recited in claim 1 , wherein the compressor is used in a heating, ventilation, and air conditioning (HVAC) chiller system.
14. The compressor as recited in claim 1 , wherein the plurality of teeth are configured to rotate together with the rotation of the rotor to gradually wear away the abradable portion.
15. The compressor as recited in claim 14 , wherein the plurality of teeth are configured to rotate together with the rotation of the rotor to gradually form tracks in the abradable portion.
16. The compressor as recited in claim 1 , wherein the plurality of teeth and the rotor are formed of the same material.
17. The compressor as recited in claim 16 , wherein the plurality of teeth and the rotor are formed of a different material than the abradable portion.
18. A refrigerant system comprising:
a main refrigerant loop including a compressor, a condenser, an evaporator, and an expansion device, wherein the compressor includes:
a rotor configured to rotate with respect to a stator, the stator having an abradable portion; and
at least one labyrinth seal between the rotor and the stator, wherein the labyrinth seal comprises a plurality of teeth extending from the rotor toward the abradable portion.
19. The refrigerant system of claim 18 , wherein the plurality of teeth are provided in a stepped arrangement.
20. The refrigerant system of claim 19 , wherein the plurality of teeth are arranged in at least two groups separated by radial steps.
21. The refrigerant system of claim 18 , wherein the teeth are configured to contact the abradable portion and carve tracks into the abradable portion over time.
22. The refrigerant system of claim 18 , wherein a flow path is defined through the labyrinth seal and at least one of a discharge path and a debris trap is arranged downstream of the labyrinth seal.
23. The refrigerant system of claim 18 , comprising a second labyrinth seal between the rotor and the stator.
24. The refrigerant system of claim 18 , wherein the compressor is a two stage centrifugal compressor.