IP Library Granted Patent US 10,641,264
Granted Patent B2
US 10,641,264 · App. 15/740,492 · Granted May 5, 2020

Modular thrust-compensating rotor assembly

Inventors: Helmut Engelmann (Radolfzell, DE); Stefan Werner (Allensbach, DE); Yongchun Ma (Allweilerstrasse, DE); Jurgen Broders (Radolfzell, DE)
Assignee: CIRCOR PUMPS NORTH AMERICA, LLC
F04C2/165F01C21/02F04C14/28F04C15/0042F04C2240/54F04C2240/56
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Quick Facts
Patent No.
US 10,641,264
App. No.
15/740,492
Granted
May 5, 2020
Kind
B2
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 (24)

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.

Assignments (7)
GRANT OF SECURITY INTEREST IN PATENT RIGHTS Recorded Nov 4, 2024
From: CIRCOR INTERNATIONAL, INC.; CIRCOR PUMPS NORTH AMERICA, LLC; SPENCE ENGINEERING COMPANY, INC.; CIRCOR AEROSPACE, INC.
To: JEFFERIES FINANCE LLC, AS COLLATERAL AGENT
Reel/Frame 069292/0137 →
RELEASE OF SECURITY INTEREST IN PATENTS, RECORDED AT REEL/FRAME 065300/0544 Recorded Oct 22, 2024
From: ARES CAPITAL CORPORATION, AS COLLATERAL AGENT
To: CIRCOR AEROSPACE, INC.; CIRCOR INTERNATIONAL, INC.; CIRCOR PUMPS NORTH AMERICA, LLC; SPENCE ENGINEERING COMPANY, INC.
Reel/Frame 069227/0202 →
RELEASE OF SECURITY INTEREST Recorded Oct 20, 2023
From: TRUIST BANK, AS COLLATERAL AGENT
To: CIRCOR AEROSPACE, INC.; CIRCOR PRECISION METERING, LL; DELTAVALVE, LLC; TAPCOENPRO, LLC; CIRCOR PUMPS NORTH AMERICA, LLC; CIRCOR INTERNATIONAL, INC.
Reel/Frame 065300/0645 →
SECURITY INTEREST Recorded Oct 20, 2023
From: CIRCOR AEROSPACE, INC.; CIRCOR INTERNATIONAL, INC.; CIRCOR PUMPS NORTH AMERICA, LLC; DELTAVALVE, LLC; SPENCE ENGINEERING COMPANY, INC.; TAPCOENPRO, LLC
To: ARES CAPITAL CORPORATION, AS COLLATERAL AGENT
Reel/Frame 065300/0544 →
SECURITY AGREEMENT Recorded Dec 21, 2021
From: CIRCOR INTERNATIONAL, INC.; CIRCOR AEROSPACE, INC.; CIRCOR PRECISION METERING, LLC; TAPCOENPRO, LLC; DELTAVALVE, LLC; CIRCOR PUMPS NORTH AMERICA, LLC
To: TRUIST BANK
Reel/Frame 058552/0318 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 7, 2018
From: ENGELMANN, HELMUT; WERNER, STEFAN; MA, YONGCHUN; BRODERS, JURGEN
To: IMO INDUSTRIES, INC.
Reel/Frame 046810/0396 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 7, 2018
From: IMO INDUSTRIES, INC.
To: CIRCOR PUMPS NORTH AMERICA, LLC
Reel/Frame 046810/0527 →