IP Library Granted Patent US 9,382,800
Granted Patent B2
US 9,382,800 · App. 13/813,004 · Granted Jul 5, 2016

Screw type pump or motor

Inventor: Alastair Simpson (Aberdeen, GB)
Assignee: HIVIS PUMPS AS
F01C1/0215F04D3/02F04D5/002F04D7/00
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Quick Facts
Patent No.
US 9,382,800
App. No.
13/813,004
Granted
Jul 5, 2016
Kind
B2
Abstract

A pump assembly comprising a stator and a rotor having vanes of opposite handed thread arrangements is described. A radial gap is located between the stator vanes and the rotor vanes such that rotation of the rotor causes the stator and rotor to co-operate to provide a system for moving fluid longitudinally between them. The operation of the pump results in a fluid seal being is formed across the radial gap. The described apparatus can also be operated as a motor assembly when a fluid is directed to move longitudinally between the stator and rotor. The presence of the fluid seal results in no deterioration of the pump or motor efficiency, even when the radial gap is significantly greater than normal working clearance values. Furthermore, the presence of the radial gap makes the pump/motor assembly ideal for deployment with high viscosity and/or multiphase fluids.

Claims (52)

1. A pump assembly for use with a high viscosity or multiphase hydrocarbon fluid comprising:

a stator having an internal surface of constant diameter and one or more stator vanes extending from the internal surface to a constant stator vane radial height along a length of the stator; and

a rotor having an external surface of constant diameter and one or more rotor vanes extending from the external surface to a constant rotor vane radial height along a length of the rotor,

wherein the one or more stator vanes have an opposite handed thread with respect to a thread of the one or more rotor vanes and the stator and rotor co-operating to provide, on rotation of the rotor, a system for moving the high viscosity or multiphase hydrocarbon fluid longitudinally between them,

wherein a radial gap, having a constant value in the range of 1.28 mm to 10 mm, is located between the constant stator vane radial height and the constant rotor vane radial height along a length of the pump assembly, and

wherein a ratio of the constant rotor vane radial height to the constant stator vane radial height has a constant value in the range of 1.1 to 20 along the length of the pump assembly.

2. A pump assembly as claimed in claim 1 wherein the rotor vanes are arranged on the external surface of the rotor so as to form one or more rotor channels.

3. A pump assembly as claimed in claim 2 wherein a ratio of the volume to cross sectional area of the rotor channels is equal to, or greater than, 200 mm.

4. A pump assembly as claimed in claim 1 wherein the stator vanes are arranged on the internal surface of the stator so as to form one or more stator channels.

5. A pump assembly as claimed in claim 4 wherein a ratio of the volume to cross sectional area of the stator channels is equal to, or greater than, 200 mm.

6. A pump assembly as claimed in claim 1 wherein a helix formed by the rotor vanes has a mean lead angle (α) that is greater than 60° but less than 90°.

7. A pump assembly as claimed in claim 6 wherein the mean lead angle (α) is in the range of 70° to 76°.

8. A pump assembly as claimed in claim 7 wherein the mean lead angle (α) is 73°.

9. A pump assembly as claimed in claim 1 wherein a helix formed by the stator vanes has a mean lead angle (β) that is greater than 60° but less than 90°.

10. A pump assembly as claimed in claim 9 wherein the mean lead angle (β) is in the range of 70° to 76°.

11. A pump assembly as claimed in claim 10 wherein the mean lead angle (β) is 73°.

12. A pump assembly as claimed in claim 1 wherein the ratio of the constant rotor vane radial height to the constant stator vane radial height is in the range 3.5 to 4.5.

13. A pump assembly as claimed in claim 1 wherein the ratio of the constant rotor vane radial height to the constant stator vane radial height is 4.2.

14. A pump assembly as claimed in claim 1 wherein a ratio of a rotor outer diameter to a rotor lead is in the range of 0.5 to 1.5.

15. A pump assembly as claimed in claim 14 wherein the ratio of the rotor outer diameter to the rotor lead is 1.0.

16. A pump assembly as claimed in claim 1 wherein a ratio of a stator inner diameter to a stator lead is in the range of 0.5 to infinity.

17. A pump assembly as claimed in claim 16 wherein the ratio of the stator inner diameter to the stator lead is 1.0.

18. A pump assembly as claimed in claim 1 wherein one or more anti-rotation tabs are located at each end of the stator.

19. A pump assembly as claimed in claim 1 wherein the assembly further comprises a cylindrical housing within which the rotor and stator are located.

20. A pump assembly as claimed in claim 1 wherein the rotor is connected to a motor by means of a central shaft such that operation of the motor induces relative rotation between the rotor and the stator.

21. A pump assembly as claimed in any claim 1 wherein the assembly further comprises a first bearing which defines an inlet for the device.

22. A pump assembly as claimed in claim 21 wherein the assembly further comprises a second bearing, longitudinally spaced from the first bearing, which defines an outlet for the device.

23. A pump assembly as claimed in claim 1 wherein a stator vane thickness is greater than a rotor vane thickness.

24. A pump assembly as claimed in claim 1 wherein the rotor is coated with an erosion resistant, corrosion resistant and/ or drag resistant coating.

25. A pump assembly as claimed in claim 1 wherein the stator is coated with an erosion resistant, corrosion resistant and/ or drag resistant coating.

26. A multistage pump wherein the multistage pump comprises two or more pump assemblies, and wherein at least one of the two or more pump assemblies comprises:

a stator having an internal surface of constant diameter and one or more stator vanes extending from the internal surface to a constant stator vane radial height along the length of the stator; and

a rotor having an external surface of constant diameter and one or more rotor vanes extending from the external surface to a constant rotor vane radial height along the length of the rotor,

wherein the one or more stator vanes have an opposite handed thread with respect to the thread of the one or more rotor vanes and the stator and rotor cooperating to provide, on rotation of the rotor, a system for moving a high viscosity or multiphase hydrocarbon fluid longitudinally between them;

wherein a radial gap, having a constant value in the range of 1.28 mm to 10 mm, is located between the constant stator vane radial height and the constant rotor vane radial height along a length of the pump assembly, and

a ratio of the constant rotor vane radial height to the constant stator vane radial height has a constant value in the range of 1.1 to 20 along the length of the pump assembly.

27. A multistage pump as claimed in claim 26 wherein the two or more pump assemblies are deployed on opposite sides of a central inlet aperture.

28. A multistage pump as claimed in claim 26 wherein the diameter of the two or more pump assemblies differs along the length of the multistage pump.

29. A motor assembly for use with a high viscosity and or multiphase hydrocarbon fluid comprising:

a stator having an internal surface of constant diameter and one or more stator vanes extending from the internal surface to a constant stator vane radial height along a length of the stator; and

a rotor having an external surface of constant diameter and one or more rotor vanes extending from the external surface to a constant rotor vane radial height along a length of the rotor,

wherein the one or more stator vanes have an opposite handed thread with respect to the thread of the one or more rotor vanes and the stator and rotor cooperating to provide, on the high viscosity or multiphase hydrocarbon fluid moving longitudinally between them, relative rotation of the rotor and stator,

wherein a radial gap, having a constant value in the range of 1.28 mm to 10 mm, is located between the constant stator vane radial height and the constant rotor vane radial height along a length of the motor assembly, and

a ratio of the constant rotor vane radial height to the constant stator vane radial height has a constant value in the range of 1.1 to 20 along the length of the motor assembly.

30. A multistage motor wherein the multistage motor comprises two or more motor assemblies, wherein at least one of the two motor assemblies comprises:

a stator having an internal surface of constant diameter and one or more stator vanes extending from the internal surface to a constant stator vane radial height along a length of the stator; and

a rotor having an external surface of constant diameter and one or more rotor vanes extending from the external surface to a constant rotor vane radial height along a length of the rotor,

wherein the one or more stator vanes have an opposite handed thread with respect to the thread of the one or more rotor vanes and the stator and rotor co-operating to provide, on a high viscosity or multiphase hydrocarbon fluid moving longitudinally between them, relative rotation of the rotor and stator,

wherein a radial gap, having a constant value in the range of 1.28 mm to 10 mm, is located between the constant stator vane radial height and the constant rotor vane radial height along a length of the motor assembly, and

a ratio of the constant rotor vane radial height to the constant stator vane radial height has a constant value in the range of 1.1 to 20 along the length of the motor assembly.

31. A multistage motor as claimed in claim 30 wherein the two or more motor assemblies are deployed on opposite sides of a central inlet aperture.

32. A pump assembly for use with a high viscosity or multiphase hydrocarbon fluid comprising a stator and a rotor, each one being provided with one or more vanes having an opposite handed thread with respect to a thread of the one or more vanes on the other, the stator and rotor co-operating to provide, on rotation of the rotor, a system for moving the high viscosity or multiphase hydrocarbon fluid longitudinally between them, wherein: a radial gap, in the range of 1.28 mm to 10 mm, is located between the one or more stator vanes and the one or more rotor vanes along a length of the pump assembly, and a ratio of a radial height of the one or more rotor vanes to a radial height of the one or more stator vanes is in the range of 3.5 to 4.5 along the length of the pump assembly.

Assignments (12)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 5, 2024
From: EXTRACT MANAGEMENT COMPANY, LLC; EXTRACT PRODUCTION SERVICES LLC; EXTRACT SURFACE SYSTEMS LLC
To: EXTRACT COMPANIES LLC
Reel/Frame 066028/0513 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 17, 2023
From: SIMPSON, ALASTAIR
To: HIVIS PUMPS AS
Reel/Frame 065595/0469 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 13, 2022
From: EXTRACT PRODUCTION SERVICES, LLC
To: EXTRACT MANAGEMENT COMPANY, LLC
Reel/Frame 061074/0304 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 20, 2022
From: VERE TECHNOLOGY LLC
To: EXTRACT PRODUCTION SERVICES, LLC
Reel/Frame 058707/0441 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 20, 2021
From: HIVIS PUMPS AS
To: VERE TECHNOLOGY LLC
Reel/Frame 058435/0233 →
CHANGE OF ADDRESS Recorded Dec 20, 2021
From: HIVIS PUMPS AS
To: HIVIS PUMPS AS
Reel/Frame 058549/0966 →
NULLIFICATION OF NAME CHANGE DOCUMENTS RECORDED AT REEL/FRAME: 048323/0254; 048339/0326; 048359/0216; 048371/0844 Recorded Oct 24, 2019
From: HIVIS PUMPS AS
To: HIVIS PUMPS AS
Reel/Frame 051885/0164 →
CHANGE OF NAME Recorded Feb 19, 2019
From: VERETEK LLC
To: VERE TECHNOLOGY LLC
Reel/Frame 048371/0844 →
CHANGE OF NAME Recorded Feb 18, 2019
From: VERETEK MULTIPHASE LLC
To: VERETEK LLC
Reel/Frame 048359/0216 →
CHANGE OF NAME Recorded Feb 14, 2019
From: ELITE MULTIPHASE SOLUTIONS, LLC
To: VERETEK MULTIPHASE LLC
Reel/Frame 048339/0326 →
CHANGE OF NAME Recorded Feb 13, 2019
From: HIVIS PUMPS AS
To: ELITE MULTIPHASE SOLUTIONS, LLC
Reel/Frame 048323/0254 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 29, 2013
From: SIMPSON, ALASTAIR
To: HIVIS PUMPS AS
Reel/Frame 029713/0743 →
Priority Claims (1)
GB 1012792.6 · Jul 30, 2010 · national
Continuity (1)
Related Publication 20130136639A1 · May 30, 2013