Duplex shear force rotor

• US 6,752,597 B2
• Filed: 09/25/2002
• Issued: 06/22/2004
• Est. Priority Date: 09/27/2001
• Status: Active Grant

• Current Assignee: Discflo Corporation
• Original Assignee: LBT Company
• Inventors: Tybor, Frank J., Pacello, John
• Primary Examiner(s): Nguyen, Ninh H.
• Application Number:
  US10/254,206
• Publication Number:
  US 20030059300A1
• Time in Patent Office: 636 Days
• Field of Search: 416/1, 416/185, 416/186.R, 416/198.R, 416/223.B
• US Class Current: 416/186.00R
• CPC Class Codes: F04D 29/2255 flow-channels with a special cross-section contour, e.g. ejecting, throttling or diffusing effect

Abstract

A single or multi-stage centrifugal pump or mixer duplex shear force rotor. The rotor is circular and consists of two non-parallel shrouds with inner, opposing faces. The driven shroud contains a center opening. The rotor has an open, unobstructed entrance section with no raised ribs and includes a protrusion designed to force-feed the discharge section in a smooth laminar flow pattern. The discharge section incorporates a series of raised ribs. The raised ribs begin at the peripheral edge of the drive and driven shrouds and extend in a direction towards the center of the drive and driven shroud and terminate approximately 50% of the distance from the periphery and the center of the rotor. Cast-in-place spacers space the drive and driven shrouds. Alternatively, the rotor can include no raised ribs. In addition, the raised ribs can have a cross-section that includes a tapered trailing edge to reduce wear. The rotor can also be used without inclusion of the raised ribs. Alternatively, neither the drive or driven shroud are perpendicular to the axis of rotation.

Claims

1. A rotor comprising:

a first shroud with an inner, opposing face;

a second shroud with an inner, opposing face, the second shroud having an opening therethrough;

the first and second shrouds being co-axially disposed and attached for rotation about a common axis;

wherein the second shroud is not parallel to the first shroud;

at least one raised rib mounted on at least one of the first and second shroud faces, the shrould faces having a spacing therebetween and the height of the at least one rib being less than the spacing; and

wherein the at least one rib extends from a radius at least equal to the radius of the second shroud opening to the periphery of the at least one of the first and second shroud faces.

2. The rotor of claim 1 wherein the first shroud inner, opposing face includes a curved, raised protrusion adjacent to the opening.

3. The rotor of claim 2 wherein the at least one raised rib is curved and extends radially from the periphery of the at least one of the first and second shroud faces toward the center of the at least one of the first and second shroud faces.

4. The rotor of claim 3 wherein the at least one raised rib extends from the periphery of the at least one of the first and second shroud faces to between approximately 25% and 75% of the distance to the center of the at least one of the first and second shroud faces.

5. The rotor of claim 4 wherein the at least one raised rib extends from the periphery of the at least one of the first and second shroud faces to approximately 50% of the distance to the center of the first and second shroud faces.

6. The rotor of claim 2 wherein the at least one rib has a cross-section with a tapered trailing edge extending in the direction opposite of rotation.

7. The rotor of claim 2 wherein one of the first and second faces is perpendicular to the axis of rotation.

8. The rotor of claim 2 wherein neither the first or the second face is perpendicular to the axis of rotation.

9. The rotor of claim 1 wherein a rotary drive shaft engages the first shroud.

10. The rotor of claim 1 wherein the center portion of the second shroud curves away from the first shroud.

11. The rotor of claim 10 wherein a rotary drive shaft extends through the first and second shrouds.

12. The rotor of claim 1 wherein the at least one raised rib is curved and extends radially from the periphery of the at least one of the first and second shroud faces toward the center of the at least one of the first and second shroud faces.

13. The rotor of claim 12 wherein the at least one raised rib extends from the periphery of the at least one of the first and second shroud faces to between approximately 25% and 75% of the distance to the center of the at least one of the first and second shroud faces.

14. The rotor of claim 13 wherein the at least one rib extends from the periphery of the at least one of the first and second shroud face to between approximately 50% of the distance to the center of the at least one of the first and second shroud faces.

15. The rotor of claim 1 wherein the at least one rib has a cross-section with a tapered trailing edge extending in the direction opposite of rotation.

16. The rotor of claim 1 wherein the rotor is used in a centrifugal pump.

17. The rotor of claim 16 wherein the pump is used to pump fluids.

18. The rotor of claim 16 wherein the pump is used to pump abrasive fluids.

19. The rotor of claim 16 wherein the pump is used to pump fluids with solids.

20. The rotor of claim 1 wherein one of the first and second faces is perpendicular to the axis of rotation.

21. The rotor of claim 1 wherein neither the first or the second face is perpendicular to the axis of rotation.