Gas turbine seal
US-10408077-B2 · Sep 10, 2019 · US
US12146501B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12146501-B2 |
| Application number | US-202318197782-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 16, 2023 |
| Priority date | Jan 4, 2021 |
| Publication date | Nov 19, 2024 |
| Grant date | Nov 19, 2024 |
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In some aspects, the techniques described herein relate to a refrigerant compressor, including: a stator; a rotor configured to rotate with respect to the stator; and at least one step seal between the rotor and the stator, wherein the step seal includes a first tooth and a second tooth extending from the rotor toward the stator, wherein a downstream surface of the first tooth and an upstream surface of the second tooth are arranged at an angle relative to one another, wherein the angle is less than 90°.
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The invention claimed is: 1. A refrigerant compressor, comprising: a stator; a rotor configured to rotate with respect to the stator; and at least one step seal between the rotor and the stator, wherein the step seal comprises a first tooth and a second tooth extending from the rotor toward the stator, wherein a downstream surface of the first tooth and an upstream surface of the second tooth are arranged at an angle relative to one another, wherein the angle is less than 90°, wherein the stator has an abradable portion, wherein the first and second teeth extend toward the abradable portion, wherein the first and second teeth are configured to contact the abradable portion and carve tracks into the abradable portion over time, and wherein each of the tracks carved into the abradable portion exhibits an axial dimension greater than an axial dimension of a tip of a corresponding one of the first and second teeth. 2. The refrigerant compressor as recited in claim 1 , wherein the first tooth and the second tooth comprise a pair of teeth, and the step seal comprises a plurality of pairs of teeth, and wherein each pair of teeth is provided in a stepped arrangement such that each pair of teeth is arranged at a different radial distance from an axis of rotation of the rotor relative to an adjacent pair of teeth. 3. The refrigerant compressor as recited in claim 1 , wherein the first tooth has a first point and the second tooth has a second point, and wherein the first and second points are arranged at a common radial position. 4. The refrigerant compressor as recited in claim 1 , wherein the downstream surface of the first tooth and the upstream surface of the second tooth meet at a curved surface to form a curved cavity. 5. The refrigerant compressor as recited in claim 4 , wherein a radially inner cavity wall is arranged downstream of the second tooth to form a second cavity downstream of the curved cavity. 6. The refrigerant compressor as recited in claim 5 , wherein the second cavity is a curved cavity. 7. The refrigerant compressor as recited in claim 1 , wherein the refrigerant compressor is used in a heating, ventilation, and air conditioning (HVAC) chiller system. 8. The refrigerant compressor as recited in claim 1 , wherein a stator cavity is arranged in the stator, the stator cavity is arranged axially between the first tooth and the second tooth. 9. A refrigeration system, comprising: a condenser; an evaporator; an expansion device; and a compressor, wherein the compressor includes a stator, a rotor configured to rotate with respect to the stator, and at least one step seal between the rotor and the stator, wherein the step seal comprises a first tooth and a second tooth extending from the rotor toward the stator, wherein a downstream surface of the first tooth and an upstream surface of the second tooth are arranged at an angle relative to one another, wherein the angle is less than 90°, wherein an upstream surface of the first tooth and a downstream surface of the second tooth are arranged substantially perpendicular to a radially innermost-portion of a wall of a cavity immediately adjacent one of the first and second teeth. 10. The refrigeration system as recited in claim 9 , wherein the first tooth and the second tooth comprise a pair of teeth, and the step seal comprises a plurality of pairs of teeth, each pair of teeth provided in a stepped arrangement such that each pair of teeth is arranged at a different radial distance from an axis of rotation of the rotor relative to an adjacent pair of teeth. 11. The refrigeration system as recited in claim 9 , wherein the first tooth has a first point and the second tooth has a second point, and wherein the first and second points are arranged at a common radial position. 12. The refrigeration system as recited in claim 9 , wherein the downstream surface of the first tooth and the upstream surface of the second tooth meet at a curved surface to form a curved cavity. 13. The refrigeration system as recited in claim 12 , wherein a radially inner cavity wall is arranged downstream of the second tooth to form a second cavity downstream of the curved cavity. 14. The refrigeration system as recited in claim 13 , wherein the second cavity is a curved or square cavity. 15. The refrigeration system as recited in claim 9 , wherein the stator has an abradable portion, wherein the first and second teeth extend toward the abradable portion, and wherein the first and second teeth are configured to contact the abradable portion and carve tracks into the abradable portion over time, and wherein each of the tracks carved into the abradable portion exhibits an axial dimension greater than an axial dimension of a tip of a corresponding one of the first and second teeth. 16. The refrigerant compressor as recited in claim 1 , wherein an upstream surface of the first tooth and a downstream surface of the second tooth are arranged substantially perpendicular to a radially innermost-portion of a wall of a cavity immediately adjacent one of the first and second teeth. 17. The refrigeration system as recited in claim 9 , wherein the upstream surface of the first tooth and the downstream surface of the second tooth are arranged substantially perpendicular to an axis of rotation of the rotor. 18. The refrigeration system as recited in claim 9 , wherein the second tooth is the closest tooth of the rotor to the first tooth when moving from the first tooth in a downstream direction.
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