System for moving fluid with opposed axial forces
US-2019145415-A1 · May 16, 2019 · US
US11098727B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11098727-B2 |
| Application number | US-201816012952-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 20, 2018 |
| Priority date | Jun 20, 2018 |
| Publication date | Aug 24, 2021 |
| Grant date | Aug 24, 2021 |
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A technique facilitates movement of fluids while reducing axial loading on system components such as thrust bearings. The technique utilizes a system, e.g. a compressor, for moving fluid via counter rotating rotors. By way of example, the rotors may utilize impellers for establishing opposed fluid flows along fluid movement sections. The fluid movement sections may be arranged in a back-to-back configuration such that counter rotation of the rotors causes the impellers to move fluid flows in opposed directions, thus reducing axial loading. The opposed fluid flows ultimately are redirected to an outlet.
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What is claimed is: 1. A system for moving a compressible fluid, comprising: a counter rotating axial compressor having: an inner rotor comprising a plurality of inner impellers, the inner rotor being secured axially by an inner rotor thrust bearing assembly; and an outer rotor comprising a plurality of outer impellers interleaved with the inner impellers, the outer impellers being secured axially via an outer rotor thrust bearing assembly, the outer rotor being rotatable in an opposite direction relative to the inner rotor to draw in the compressible fluid; the inner rotor and the outer rotor forming a first compressor section wherein inner and outer impellers are interleaved and a second compressor section wherein inner and outer impellers are interleaved, the first and second compressor sections being oriented to move the compressible fluid in opposed axial directions along the first compressor section and the second compressor section, respectively, so as to reduce axial loading incurred by the inner rotor thrust bearing assembly and the outer rotor thrust bearing assembly. 2. The system as recited in claim 1 , wherein the inner rotor thrust bearing assembly comprises an inner rotor main thrust bearing, an inner rotor reverse thrust bearing, and an inner rotor thrust disc therebetween. 3. The system as recited in claim 2 , wherein the outer rotor thrust bearing assembly comprises an outer rotor main thrust bearing, an outer rotor reverse thrust bearing, and an outer rotor thrust disc therebetween. 4. The system as recited in claim 1 , wherein rotation of the inner rotor and the outer rotor in opposite directions causes the first compressor section to draw in the compressible fluid through a first compressor inlet and to discharge the compressible fluid through a first compressor outlet. 5. The system as recited in claim 4 , wherein rotation of the inner rotor and the outer rotor in opposite directions causes the second compressor section to draw in the compressible fluid through a second compressor inlet and to discharge the compressible fluid through a second compressor outlet. 6. The system as recited in claim 5 , wherein the compressible fluid discharged through the first compressor outlet is directed into the second compressor inlet. 7. The system as recited in claim 1 , wherein the first compressor section and the second compressor section are aligned axially. 8. The system as recited in claim 1 , further comprising a process cooler through which the compressible fluid is directed to cool the compressible fluid. 9. The system as recited in claim 1 , wherein the counter rotating axial compressor is a multiphase fluid compressor. 10. The system as recited in claim 1 , wherein the counter rotating axial compressor is a dry gas compressor. 11. A system for moving a fluid, comprising: an inner rotor having a plurality of inner impellers, the inner rotor being secured axially by an inner rotor thrust bearing assembly; and an outer rotor having a plurality of outer impellers interleaved with the inner impellers, the outer impellers being secured axially via an outer rotor thrust bearing assembly, the outer rotor being rotatable in an opposite direction relative to the inner rotor to draw in the fluid; the inner rotor and the outer rotor forming a first fluid movement section wherein inner and outer impellers are interleaved and a second fluid movement section wherein inner and outer impellers are interleaved, the first and second fluid movement sections being oriented to move the fluid in opposed axial directions along the first fluid movement section and the second fluid movement section, respectively, so as to reduce axial loading incurred by the inner rotor thrust bearing assembly and the outer rotor thrust bearing assembly. 12. The system as recited in claim 11 , wherein the first fluid movement section is a first compressor section and the second fluid movement section is a second compressor section. 13. The system as recited in claim 12 , wherein the inner rotor thrust bearing assembly comprises an inner rotor main thrust bearing, an inner rotor reverse thrust bearing, and an inner rotor thrust disc therebetween. 14. The system as recited in claim 13 , wherein the outer rotor thrust bearing assembly comprises an outer rotor main thrust bearing, an outer rotor reverse thrust bearing, and an outer rotor thrust disc therebetween. 15. The system as recited in claim 11 , wherein the inner rotor and the outer rotor are powered via at least one electric motor. 16. The system as recited in claim 11 , wherein the inner rotor and the outer rotor are each powered via a corresponding electric motor.
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