Rotor for a centrifugal flow machine and a centrifugal flow machine

Patent metadata

Field	Value
Publication number	US-9631633-B2
Application number	US-201414899920-A
Country	US
Kind code	B2
Filing date	Jun 16, 2014
Priority date	Jul 2, 2013
Publication date	Apr 25, 2017
Grant date	Apr 25, 2017

Abstract

A rotor structure for a centrifugal flow machine includes working vanes attached to the hub of the rotor without any support disc or shroud. Additionally, the vane has a device for efficiently flushing the sealing chamber behind the rotor.

First claim

The invention claimed is:

1. A rotor for a centrifugal flow machine, the rotor comprising:
a hub with an axis and device configured to couple the rotor, when in use, on a shaft of the flow machine including a sealing chamber; and
at least one working vane extending outwardly from the hub, the working vane having a front edge, a leading edge, a trailing edge, a rear face, a leading surface and a trailing surface, the rear face, when in use, facing the sealing chamber, the working vane being formed of a root portion and a vane portion integrated to one another, the working vane being fastened to the hub solely by the root portion, the root portion having, when joined to the hub, a substantially trapezoidal or triangular cross section having sides representing a leading face, a trailing face, a rounded front edge between the leading face and the trailing face and the rear face opposite to the front edge of the root portion, the rear face of the at least one working vane forming a sharp angle with a circumferential direction, the sharp angle opening in a direction of rotation of the rotor for pumping fluid towards the sealing chamber for flushing the sealing chamber.

2. The rotor as recited in claim 1 , wherein
the rounded front edge has a thickness equal to a thickness of the vane portion at a position where the vane portion joins the root portion.

3. The rotor as recited in claim 2 , wherein
a thickness of the root portion is at the rear face adjacent the hub equal to 2*S-5*S, where S is an average thickness of the working vane at the vane portion.

4. The rotor as recited in claim 2 , wherein the edges have a radius of ¼*S-½*S where S is an average thickness of the edge after rounding.

5. The rotor as recited in claim 1 , wherein
the leading face and the trailing face are arranged adjacent the hub at an angle between 5 and 45 degrees.

6. The rotor as recited in claim 1 , wherein
the root portion has a centerline running via the front edge and, at the rear face, a thickness measured in a direction perpendicular to the centerline of the root portion, the thickness representing a largest thickness dimension of the root portion of the working vane.

7. The rotor as recited in claim 6 , wherein the centerline is arranged at an angle in relation to an axial direction, the angle being between +/−45 degrees.

8. The rotor as recited in claim 6 , wherein
a transitional line or curve is at the trailing surface of the working vane, a thickness of the working vane increasing from that at the transitional curve to that at the rear face of the working vane.

9. The rotor as recited in claim 8 , wherein
a blunt angle γ between 135-180 degrees is at the transitional line or curve between main directions of the trailing surface and the trailing face of the working vane in a plane perpendicular to the leading surface or the working vane and parallel with the axis of the rotor.

10. The rotor as recited in claim 1 , wherein
the working vane has a trapezoidal or triangular cross section in a plane perpendicular to the leading surface of the working vane and parallel with the axis of the rotor, the cross section having sides representing the front edge, a leading surface, a trailing surface and a rear face of the working vane.

11. The rotor as recited in claim 10 , wherein
at least one of the sides of the trapezoidal or triangular cross section representing the front edge, the leading edge of the working vane and the rear face is rounded.

12. The rotor as recited in claim 11 , wherein
the edges have a radius of ¼*S-½*S where S is an average thickness of the edge after rounding.

13. The rotor as recited in claim 10 , wherein
at least one of the sides of the trapezoidal or triangular cross section representing the leading surface and the trailing surface is curved.

14. The rotor as recited in claim 1 , wherein
the root portion of the working vane extends at the rear face at least to a distance of 0.5* the radius of the rotor from the axis of the rotor.

15. A centrifugal flow machine comprising the rotor of claim 1 .

16. The centrifugal flow machine as recited in claim 15 , wherein
the centrifugal flow machine has a shaft sealing with a rotary sealing member coupled to the hub of the rotor, the rotary sealing member having a diameter and the hub having a diameter, and that the diameter of the hub is equal or smaller than that of the rotary sealing member.

17. The centrifugal flow machine as recited in claim 16 , wherein
the flow machine is a centrifugal pump or a blower.

18. The centrifugal flow machine as recited in claim 15 , wherein
the flow machine is a centrifugal pump or a blower.

Assignees

• Sulzer Management Ag

Inventors

• Manninen Heikki

Classifications

• F04D29/2233 Primary

  entirely open or stamped from one sheet · CPC title

• F04D29/2266 Primary

  for sealing or thrust balance (F04D29/04 and F04D29/16 take precedence) · CPC title

• F04D29/126

  especially adapted for liquid pumps · CPC title

• F04D29/28

  for centrifugal or helico-centrifugal pumps {for radial-flow or helico-centrifugal pumps} · CPC title

• F04D1/00

  Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps (adapted for pumping specific fluids F04D7/00; priming or boosting F04D9/00) · CPC title