Modular thrust-compensating rotor assembly

• US 10,641,264 B2
• Filed: 05/11/2016
• Issued: 05/05/2020
• Est. Priority Date: 04/29/2016
• Status: Active Grant

• Current Assignee: Circor Pumps North America LLC (Circor International Incorporated)
• Original Assignee: Circor Pumps North America LLC (Circor International Incorporated)
• Inventors: Engelmann, Helmut, Werner, Stefan, Ma, Yongchun, Broders, Jurgen
• Primary Examiner(s): Davis, Mary
• Application Number:
  US15/740,492
• Publication Number:
  US 20180187675A1
• Time in Patent Office: 1,455 Days
• CPC Class Codes: F01C 21/02 Arrangements of bearings bearing constructions F16C
• CPC Class Codes: F04C 14/28 Safety arrangements; Monitoring
• CPC Class Codes: F04C 15/0003 Sealing arrangements in rotary-piston machines or pumps sealing in general F16J
• CPC Class Codes: F04C 15/0042 Systems for the equilibration of forces acting on the machines or pump interstice adjustment other than by fluid pressure F01C21/102
• CPC Class Codes: F04C 2/084 Toothed wheels
• CPC Class Codes: F04C 2/165 having more than two rotary pistons with parallel axes
• CPC Class Codes: F04C 2240/54 Hydrostatic or hydrodynamic bearing assemblies specially adapted for rotary positive displacement pumps or compressors
• CPC Class Codes: F04C 2240/56 Bearing bushings or details thereof

Abstract

A modular rotor assembly for a screw pump including a power rotor and an idler rotor having respective first ends adapted to be disposed in a suction side of the screw pump and respective second ends adapted to be disposed in a discharge side of the screw pump, the power rotor including a balance piston adapted to be disposed within a pump housing of the screw pump with a radial clearance between an entire circumference of the balance piston and the pump housing is in a range between 1 micron and 200 microns, wherein the power rotor is provided with a tapered bearing surface configured to define a wedge-shaped, radial gap axially intermediate the power rotor and the idler rotor.

Claims

1. A screw pump comprising:

a pump housing; and

a rotor set disposed within the pump housing, the rotor set including a power rotor and an idler rotor having radially intermeshing threaded portions, the power rotor including a balance piston enclosed by the pump housing, wherein a radial clearance between an entire circumference of the balance piston and the pump housing is in a range between 1 micron and 200 microns;

wherein the power rotor is provided with a tapered bearing surface configured to define a wedge-shaped, radial gap axially intermediate the power rotor and the idler rotor.

2. The screw pump of claim 1, wherein the tapered bearing surface is a downstream face of a thrust disc that extends radially from the power rotor.

3. The screw pump of claim 2, wherein the tapered bearing surface of the thrust disc confronts a tapered bearing surface defined by an upstream face of the idler rotor.

4. The screw pump of claim 3, wherein an angle of the tapered bearing surface of the thrust disc is greater than the angle of the tapered bearing surface of the idler rotor.

5. The screw pump of claim 1, further comprising a thrust disc extending radially from the power rotor into an annular groove in the idler rotor, wherein the annular groove is bounded by a downstream face of the threaded portion of the idler rotor and an upstream face of a flanged end of the idler rotor, and wherein at least one of the downstream face of the threaded portion, the upstream face of the flanged end, a downstream face of the thrust disc, and an upstream face of the thrust disc is tapered for defining a wedge-shaped, radial gap axially intermediate the power rotor and the idler rotor.

6. The screw pump of claim 5, wherein the thrust disc and the annular groove are located at a discharge side of the screw pump.

7. The screw pump of claim 1, wherein the tapered bearing surface is a downstream face of a thrust disc that extends radially from the power rotor at a suction side of the screw pump.

8. The screw pump of claim 1, the idler rotor having a tapped end extending into a complementary recess in a discharge side of the pump housing, the tapped end having a cavity formed in a downstream face thereof.

9. The screw pump of claim 8, further comprising a balance bushing disposed within the recess and confronting the tapped end for channeling fluid into the cavity.

10. The screw pump of claim 1, wherein the tapered bearing surface is an upstream face of a thrust disc that extends radially from the power rotor at a discharge side of the screw pump.

11. A rotor set for a screw pump, the rotor set comprising:

a power rotor and an idler rotor having respective first ends adapted to be disposed in a suction side of the screw pump and respective second ends adapted to be disposed in a discharge side of the screw pump, the power rotor including a balance piston adapted to be disposed within a pump housing of the screw pump with a radial clearance between an entire circumference of the balance piston and the pump housing is in a range between 1 micron and 200 microns;

wherein the power rotor is provided with a tapered bearing surface configured to define a wedge-shaped, radial gap axially intermediate the power rotor and the idler rotor.

12. The rotor set of claim 11, wherein the tapered bearing surface is a downstream face of a thrust disc that extends radially from the power rotor.

13. The rotor set of claim 12, wherein the tapered bearing surface of the thrust disc confronts a tapered bearing surface defined by an upstream face of the idler rotor.

14. The rotor set of claim 13, wherein an angle of the tapered bearing surface of the thrust disc is greater than the angle of the tapered bearing surface of the idler rotor.

15. The rotor set of claim 11, further comprising a thrust disc extending radially from the power rotor into an annular groove in the idler rotor, wherein the annular groove is bounded by a downstream face of a threaded portion of the idler rotor and an upstream face of a flange at the second end of the idler rotor, and wherein at least one of the downstream face of the threaded portion, the upstream face of the flange, a downstream face of the thrust disc, and an upstream face of the thrust disc is tapered for defining a wedge-shaped, radial gap axially intermediate the power rotor and the idler rotor.

16. The rotor set of claim 15, wherein the thrust disc and the annular groove are located at the second end of the power rotor and the second end of the idler rotor, respectively.

17. The rotor set of claim 11, wherein the tapered bearing surface is a downstream face of a thrust disc that extends radially from the first end of the power rotor.

18. The rotor set of claim 11, wherein the second end of the idler rotor is tapped with a cavity formed in a downstream face thereof.

19. The rotor set of claim 11, wherein the tapered bearing surface is an upstream face of a thrust disc that extends radially from the second end of the power rotor.