Separator and method for separating liquid droplets from an aerosol

Patent metadata

Field	Value
Publication number	US-9670808-B2
Application number	US-201414549864-A
Country	US
Kind code	B2
Filing date	Nov 21, 2014
Priority date	May 29, 2012
Publication date	Jun 6, 2017
Grant date	Jun 6, 2017

Abstract

A separator for separating liquid droplets from an aerosol is provided, including a rotor arranged in a housing and including a plurality of parallel disks, a dirty gas inlet, a clean gas outlet, and an annular space between the rotor's circumference and the housing, wherein adjacent disks form an interspace therebetween, the radially outer area of the interspace opening into the annular space, and wherein one of the dirty gas inlet and the clean gas outlet communicates with the annular space and the other communicates with radially inner areas of the interspaces. The disks have flat disk bodies perpendicular to the rotor axis, and between adjacent disk bodies, there are a plurality of adjacent channels allowing passage of the gas to be cleaned. Each channel is curved and the radially outer channel wall forms an impaction and separation surface for the liquid droplets.

First claim

The invention claimed is:

1. A separator for separating liquid droplets from an aerosol, in particular an oil separator for the crankcase ventilation gases of a reciprocating internal combustion engine, comprising a rotor arranged in a stationary housing and capable of being driven in rotation about a rotor axis, said rotor comprising a plurality of disks which are concentric with the rotor axis and are arranged parallel to one another, said disks together forming a stack of disks capable of being driven in rotation about the rotor axis and being arranged at in particular equal distances relative to one another in a direction of the rotor axis, a gas flow path between a dirty gas inlet of the separator for a gas entraining liquid droplets to be separated and a clean gas outlet of the separator for the gas cleaned, at least to a large extent, of the liquid droplets, a liquid outlet for discharging separated liquid from the housing, and an annular space between the circumference of the rotor and a circumferential wall of the housing enclosing the rotor, wherein the liquid outlet is in communication with the annular space and disks adjacent to each other in each case form therebetween an interspace that is concentric with the rotor axis and through which the gas is to flow, the radially outer area of said interspace opening into the annular space, and wherein one of the dirty gas inlet and the clean gas outlet is in communication with the annular space and the other one of the dirty gas inlet and the clean gas outlet is in communication with radially inner areas of the interspaces, wherein the disks have flat disk bodies which extend in planes perpendicular to the rotor axis, wherein in each of at least a plurality of said interspaces there are provided a plurality of channels adjacent to one another and allowing passage therethrough of the gas to be cleaned, wherein each channel extends at least substantially from a first radial area to a second radial area of the interspace, with the two areas being arranged at a radial distance from each other, wherein each channel is curved when viewed in a direction of the rotor axis, and wherein between channel wall surfaces bounding the channel width on either side are provided, the radially outer one of said channel wall surfaces forming an impaction an separation surface for the liquid droplets entrained by the gas to be cleaned.

2. The separator in accordance with claim 1 , wherein all of the channels extend at least substantially from a radially inner area to a radially outer area of the interspace.

3. The separator in accordance with claim 1 , wherein each of the channels is continuously curved.

4. The separator in accordance with claim 1 , wherein each channel, starting from its radially inner end, bends in a circumferential direction of the rotor and is curved such that with increasing radial distance from the rotor axis, the direction of the channel forms an increasingly smaller angle with this circumferential direction of the rotor.

5. The separator in accordance with claim 4 , wherein this circumferential direction of the rotor is the direction of rotation thereof.

6. The separator in accordance with claim 1 , wherein when viewed in a direction of the rotor axis, each channel is bounded by two channel walls and a center line of the channel extending between the channel walls forms at least approximately at least a portion of one of a spiral and a circular arc.

7. The separator in accordance with claim 6 , wherein the spiral is an involute or an Archimedean spiral.

8. The separator in accordance with claim 1 , wherein when viewed in a direction of the rotor axis, each channel has a width that is at least nearly constant along the channel.

9. The separator in accordance with claim 8 , wherein along the length of a channel, the width thereof does not vary by more than ¼ of the mean channel width.

10. The separator in accordance with claim 1 , wherein when viewed in a direction of the rotor axis, the channel width is no greater than 15 mm.

11. The separator in accordance with claim 1 , wherein when viewed in a direction of the rotor axis, the channel width is at least 0.1 mm.

12. The separator in accordance with claim 1 , wherein in an interspace, the height of the channels as measured in a direction of the rotor axis is constant.

13. The separator in accordance with claim 12 , wherein the height of all of the channels provided in all of the interspaces is the same size.

14. The separator in accordance with claim 1 , wherein each channel is bounded by two channel walls that are at least substantially parallel to each other.

15. The separator in accordance with claim 14 , wherein the channel walls extend along a course transverse to a plane defined by a disk body.

16. The separator in accordance with claim 1 , wherein the channel height is substantially larger than the channel width and is in particular approximately a multiple of the channel width.

17. The separator in accordance with claim 1 , wherein the height, as measured in a direction of the rotor axis, of the channel wall surfaces provided between two disk bodies adjacent to one another is at least nearly equal to the axial distance of these disk bodies from each other.

18. The separator in accordance with claim 1 , wherein channels adjacent to one another have in each case a wall of at least substantially constant wall thickness extending therebetween.

19. The separator in accordance with claim 1 , wherein at least two disk bodies adjacent to each other are provided, on the sides thereof facing each other, with web-shaped walls which form said channel wall surfaces and, when viewed in a direction of the rotor axis, extend along a course corresponding to the shape of the channels, wherein the height of these walls, measured in a direction of the rotor axis, is at least nearly equal to the axial distance of these disk bodies from each other, and wherein when seen in a direction of the rotor axis, in at least a plurality of channels the walls of the one disk body are at least substantially centrally arranged between the walls of the other disk body.

20. The separator in accordance with claim 1 , wherein the disks are injection-molded plastic parts.

21. The separator in accordance with claim 16 , wherein the ratio of channel height to channel width is no greater than 5.

22. A method for separating liquid droplets from an aerosol, in particular for separating oil droplets from crankcase ventilation gases of a reciprocating internal combustion engine, by way of a separator comprising a rotor arranged in a stationary housing and capable of being driven in rotation about a rotor axis, said rotor comprising a plurality of disks each of which having a flat disk body extending perpendicularly to the rotor axis and being concentric with the rotor axis, said disk bodies being arranged parallel to one another and axially spaced apart from one another in a direction of the rotor axis, said disks forming between each pair of adjacent disks an interspace concentric with the rotor axis, wherein a plurality of partial gas streams formed by the gas to be cleaned are directed along flow paths extending at least substantially from a radially inner to a radially outer area of each of said interspaces and are flowed simultaneously between said flat disk bodies through the interspaces, wherein in a view of a disk in a direction of the rotor axis said flow paths are adjacent to one another and are curved in the same sense such

Assignees

• Elringklinger Ag

Inventors

• Gorbach Gabriele
• Coolens Holger
• Piesche Manfred
• Junker Malte

Classifications

• C04B38/0006

  Honeycomb structures (from one or more corrugated sheets by winding or stacking C04B38/0083) · CPC title

• B04B5/12 Primary

  Centrifuges in which rotors other than bowls generate centrifugal effects in stationary containers · CPC title

• C04B41/009

  characterised by the material treated · CPC title

• F01M13/04 Primary

  having means for purifying air before leaving crankcase, e.g. removing oil · CPC title

• F01M2013/0422

  Separating oil and gas with a centrifuge device · CPC title