Pressure screen

Abstract

A pressure screen for cleaning a fibrous stock including a screen element which has a rotationally symmetrical configuration about a screen axis. The screen element divides the pressure screen into an inlet chamber and an accepted stock chamber. The inlet chamber is connected at a first axial end with a suspension inlet and at a second axial end with a reject outlet. The accepted stock chamber is connected with an accepted stock outlet. The pressure screen also includes a rotor situated in the inlet chamber and including a plurality of rotor blades. The rotor rotates about the rotational axis relative to the screen element. The plurality of rotor blades is arranged on a plurality of circumferential planes of the rotor. The width of an annular gap between the rotor and the screen element decreases from the suspension inlet to the reject outlet.

Claims

1. A pressure screen for cleaning a fibrous stock, comprising: a screen element which has a rotationally symmetrical configuration about a screen axis, said screen element dividing the pressure screen into an inlet chamber and an accepted stock chamber, said inlet chamber being connected at a first axial end with a suspension inlet and at a second axial end with a reject outlet, said accepted stock chamber being connected with an accepted stock outlet; and a rotor situated in said inlet chamber and including a plurality of rotor blades, said rotor having a rotational axis which corresponds to said screen axis, and said rotor rotating about said rotational axis relative to said screen element, said plurality of rotor blades being arranged on a plurality of circumferential planes of said rotor which run perpendicular with respect to said rotational axis, wherein a width of an annular gap between said rotor and said screen element decreases from said suspension inlet to said reject outlet such that said width of the annular gap decreases in steps, and wherein a radial extension of said plurality of rotor blades decreases from the suspension inlet to the reject outlet.

2. The pressure screen according to claim 1, wherein the radial extension of said plurality of rotor blades decreases in steps.

3. The pressure screen according to claim 1, wherein the radial extension of said plurality of rotor blades decreases continuously.

4. The pressure screen according to claim 1, wherein said rotor includes at least one recess between said plurality of rotor blades in at least one of said plurality of circumferential planes.

5. The pressure screen according to claim 1, wherein said rotor has at least three circumferential planes with said plurality of rotor blades.

6. The pressure screen according to claim 1, wherein each of said plurality circumferential planes includes two rotor blades respectively.

7. The pressure screen according to claim 1, wherein said plurality of rotor blades of adjacent said plurality of circumferential planes are arranged offset to one another in a circumferential direction.

8. The pressure screen according to claim 1, wherein each of said plurality of rotor blades has an identical shape.

9. The pressure screen according to claim 1, wherein the rotational axis is positioned perpendicular to a machine plane.

10. The pressure screen according to claim 1, wherein said rotor is located inside said screen element.

11. The pressure screen according to claim 10, wherein said screen element is cylindrical and said rotor is a cylindrical drum.

12. The pressure screen according to claim 1, wherein said suspension inlet is arranged below said reject outlet.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The above-mentioned and other features and advantages of this invention, and the manner of attaining them, will become more apparent and the invention will be better understood by reference to the following description of an embodiment of the invention taken in conjunction with the accompanying drawings, wherein:

(2) FIG. 1 is a schematic cross-section view of a pressure screen of the present invention, parallel to the rotational axis; and

(3) FIG. 2 is a cross-section view of the through rotor as shown in FIG. 1, perpendicular to the rotational axis.

(4) Corresponding reference characters indicate corresponding parts throughout the several views. The exemplification set out herein illustrates one embodiment of the invention, in one form, and such exemplification is not to be construed as limiting the scope of the invention in any manner.

DETAILED DESCRIPTION OF THE INVENTION

(5) Referring now to the drawings, and more particularly to FIG. 1, there is shown a pressure screen which includes a screen element 2here in the embodiment of a cylindrical screen basket with vertical screen axis 1which divides the interior space of the pressure screen into an inlet chamber 3 and an accepted stock chamber 4.

(6) Via a suspension inlet 5 the fibrous stock suspension is fed at the lower end of the screen basket into inlet chamber 3.

(7) With the herein utilized pressure screen the fibrous stock suspension receives an angular momentum that moves it into a circumferential motion. In addition hereto and as a result of the prevailing pressure gradient between lower suspension inlet 5 and reject outlet 6 of inlet chamber 3 that is located at the upper end of the screen basket a transport flow is produced.

(8) Over the path of this transport flow a large portion of the fibrous stock suspension is diverted as intended through screen element 2 as accepted stock into accepted stock chamber 4 and from there is discharged via upper accepted stock outlet 7. During this process a large portion of fibers that are contained in the fibrous stock suspension also pass into accepted stock chamber 4.

(9) The portion of fibrous stock suspension that is rejected by screen element 2 is removed as reject from inlet chamber 3 via reject outlet 6.

(10) In order to avoid that the apertures of screen element 2 become clogged, a screen scraper that moves relative to screen element 2 can be used.

(11) According to the invention this screen scraper can also include a rotor 8 that is rotating in screen element 2 and has rotor blades 9 attached to it. Rotor 8 herein has the shape of a cylindrical drum, whereby rotational axis 10 corresponds to screen axis 1.

(12) All rotor blades 9 herein have the same shape, resulting in a uniform effect on the fibrous stock suspension and screen element 2.

(13) Rotor blades 9 can furthermore be arranged distributed over severalin this case threecircumferential planes 11 of rotor 8 that extend perpendicular to rotational axis 10, whereby each circumferential plane 11 comprises severalin this case tworotor blades 9.

(14) The width of annular gap 12 between rotor 8 and screen element 2 from suspension inlet 5 to reject outlet 6 can decrease in steps. The stepped transitions can be located between two adjacent circumferential planes 11. Since screen element 2 has a cylindrical shape this means that the diameter of rotor 8 enlarges intermittently from the bottom to the top. This has a very positive effect on the energy requirement of the pressure screen.

(15) In order to further support this, the radial extension of rotor blades 9 also decreases from suspension inlet 5 to reject outlet 6.

(16) The invention may also include other shapes of rotor blades 9. However, manufacture is especially simple, if rotor blade 9 is formed by elevations on rotor 8.

(17) For the same reason, the radial extension of rotor blades 9 can decrease in steps, in other words, the height of the elevations on rotor 8 can decrease in steps from suspension inlet 5 to reject outlet 6, whereby also in this case the steps are positioned between circumferential planes 11.

(18) The cross sectional area of rotor blades 9 extending in rotational direction of rotor 8 is rectangular.

(19) Rotor blades 9 herein not only have the same shape, but also the same dimensions, resulting in a reduction of manufacturing costs. Moreover, rotor blades 9 completely overlap each other in rotational direction in one circumferential plane 11.

(20) In order to reduce clogging danger even further, rotor 8 can include in each circumferential plane 11 at least one recess 13 between rotor blades 9, which can however extend only over a part of the axial extension of respective circumferential plane 11.

(21) Rotor blades 9 of adjacent circumferential planes 11 are moreover arranged offset to one another in the circumferential direction.

(22) While this invention has been described with respect to at least one embodiment, the present invention can be further modified within the spirit and scope of this disclosure. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains and which fall within the limits of the appended claims.