EP1009537A1 - Zentrifugale trennvorrichtung - Google Patents

Zentrifugale trennvorrichtung

Info

Publication number
EP1009537A1
EP1009537A1 EP98940398A EP98940398A EP1009537A1 EP 1009537 A1 EP1009537 A1 EP 1009537A1 EP 98940398 A EP98940398 A EP 98940398A EP 98940398 A EP98940398 A EP 98940398A EP 1009537 A1 EP1009537 A1 EP 1009537A1
Authority
EP
European Patent Office
Prior art keywords
rotor
canister
liquid
end wall
centrifugal separator
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP98940398A
Other languages
English (en)
French (fr)
Other versions
EP1009537B1 (de
Inventor
Andrew Leonard Samways
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mann and Hummel GmbH
Original Assignee
Glacier Metal Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Glacier Metal Co Ltd filed Critical Glacier Metal Co Ltd
Publication of EP1009537A1 publication Critical patent/EP1009537A1/de
Application granted granted Critical
Publication of EP1009537B1 publication Critical patent/EP1009537B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B04CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
    • B04BCENTRIFUGES
    • B04B5/00Other centrifuges
    • B04B5/005Centrifugal separators or filters for fluid circulation systems, e.g. for lubricant oil circulation systems

Definitions

  • This invention relates to centrifugal separation apparatus for separating particulate contaminants from liquids, such as engine lubricants, passed therethrough and in particular relates to rotor containers used within such apparatus to perform the actual separation and retention of such contaminants.
  • Centrifugal separators are well known for use within the lubrication systems of vehicle internal combustion engines as efficient means for removing very small particulate contaminants from the constantly recirculated liquid lubricant over a long period of operation.
  • Such centrifugal separators are usually of the self-powered type, in which a separation rotor comprising a canister is supported for rotation about a rotor axis within a housing, the canister being supplied with liquid lubricant at elevated pressure along the axis and said liquid-being forced from the base of the canister (or other peripheral wall) by way of jet reaction nozzles, the reaction to said ejection causing the rotor canister and liquid within it to spin at high speed about the axis and thereby cause solid particles to migrate from the liquid passing through the canister and agglomerate on the peripheral walls thereof.
  • reaction nozzles are directed substantially tangentiaily with respect to the rotation axis, at least in a plane orthogonal to the axis, so that jets of liquid which leave the rotor canister are instantaneously tangential to the fastly spinning rotor.
  • the efficiency of separation is inter alia dependant upon the quantity of liquid lubricant passed therethrough in a given time and the time for which the liquid remains therein in passing through, and also upon the rotation speed of the rotor canister and contained liquid, which is in turn dependant upon the pressure drop between supply and housing and the dimensions of the nozzles, within the constraints of such nozzle dimensions/pressure drops providing sufficient torque to overcome resistance to commencement of, and continuation of, rotation.
  • the rotor canister divided internally by way of a radially inwardly extending partition wall which defines an outflow chamber in the vicinity of the reaction nozzles that is distinct from a separation chamber in which said particulate contaminants are separated from the input liquid and retained; the outflow chamber and reaction nozzles are protected from said separated contaminants by a transfer aperture between the chambers at radially inwardly of the partition wall, that is, surrounding the rotation axis.
  • liquid flow arrangement thereof and the internal structure it entails is unnecessarily and inappropriately complex, particularly with a view to manufacture of an inexpensive and discardable rotor canister, or, if it is employed, not used to best effect; and it is an object of the present invention to provide for a self- powered centrifugal separator a rotor canister construction that achieves improved efficiency over traditional designs whilst being simple and inexpensive to implement. It is also an object of the present invention to provide a self-powered centrifugal separator including such a rotor canister.
  • a centrifugal separator comprising a housing enclosure, an axis extending through the housing enclosure in an operationally substantially vertical orientation and a rotor arranged to receive a liquid at elevated pressure and, in reaction to ejection of the liquid therefrom substantially tangentially, spin about the axis at at least a predetermined minimum speed to effect separation of said contaminant particles from contaminated liquid therein
  • the rotor comprises a canister having (i) an outer, peripheral wail including a peripheral side wall displaced from the axis, (ii) An internal partition wall extending radially inwardly from the peripheral wall dividing the canister into a separation chamber and an outflow chamber and defining at its radially inner periphery a transfer aperture between the separation and outflow chambers, said separation chamber including an inlet aperture to admit contaminated liquid thereto from the rotation axis and the outflow chamber having at least one nozzle spaced radially from said rotation axis to eject liquid from the can
  • a centrifugal separator for separating particulate contaminants from a liquid supplied thereto comprising a housing enclosure, an axis extending through the housing enclosure in an operationally substantially vertical orientation, and a rotor arranged to receive a liquid at elevated pressure and, in reaction to ejection of the liquid therefrom substantially tangentially, spin about the axis at at least a predetermined minimum speed to effect separation of said contaminant particles from contaminated liquid therein, has said rotor as defined in the preceding paragraph
  • the said outer regions of the axial discontinuities of the rotor canister are displaced circumferentially in a in a direction that is trailing with respect to the rotation direction of the rotor that results from ejection of liquid from the canister.
  • outer regions of the axial discontinuities may, however, in the alternative be displaced circumferentially in a direction that is leading with respect to the rotation direction of the rotor that results from ejection of liquid.
  • Figure 1 (a) is a sectional elevation through centrifugal separator in accordance with a first embodiment of the present invention, showing particularly within a housing, and mounted for rotation in a clockwise direction about a vertical axis therethrough, a first embodiment of rotor canister, also in accordance with the present invention, that is defined radially between an outer peripheral side wall and an inner bearing tube and axially between upper and lower end walls and divided by a partition wall into a lower outflow chamber having tangentially directed reaction nozzles in the end wall thereof and an upper inlet and separation chamber that has inlet apertures in the bearing tube and in the upper end wall axial discontinuities in the form of embossed ribs extending radially and also circumferentially in a direction which is trailing with respect to the rotation direction of the rotor that results from liquid ejection form the reaction nozzles,
  • Figure 1(b) is a perspective view of the rotor canister of Figure 1(a), illustrating the trailing directional nature of the axial discontinuity ribs in the rotor canister end wall,
  • Figure 1(c) is a cross section through the rotor canister of Figures 1(a) along the line (b)-(b) viewed in the direction towards the upper end wall, the sectional elevation of Figure 1(a) being along the line (a) - (a) of the Figure,
  • Figure 2 is a cross section view, similar to that of Figure 1 (c), of a second embodiment of centrifugal separator canister in which the axial discontinuities comprise an array of full length ribs which each extend between the bearing tube at the radially inner end of the end wall and the radially outer end of said end wall and an array of radially shorter ribs, each disposed between a pair of full length ribs, which extend from the radially outer end of the canister end wall to a termination well short of the axle tube,
  • Figures 3 and 4 each show in part cross-section views, similar to those of Figures 1 (c) and 2, of third and fourth embodiments respectively but wherein the radially inner ends of the axial discontinuity ribs terminate adjacent the bearing tube in a circumferentially trailing direction,
  • Figure 5 is a cross-section view, similar to Figure 1 (c), of a fifth embodiment of rotor canister in which all of the axial discontinuities only extend part way between the radially outer edge of the end wall and the axle tube,
  • Figure 6 is cross-section view, similar to Figure 5, of a sixth embodiment of rotor canister, in which the axial discontinuities comprise radially inner and outer arrays of short discontinuities, those of the inner array extending substantially straight and radial,
  • Figure 7 is a cross-section view, similar to Figure 1 (c), of a seventh embodiment of rotor canister in which the axial discontinuities comprise alternate depressed and raised
  • Figures 8(a) and 8(b) are sectional elevation and cross section views respectively, similar to Figure 1(a) and 1(c), of an eighth embodiment of rotor canister in which the axial discontinuities are defined on a discrete carrier member overlying the end wall as circumferentially thin vanes,
  • Figure 9(a) is a sectional elevation through a further embodiment of centrifugal separator in accordance with the present invention including a ninth embodiment of rotor canister, also mounted for clockwise rotation, in which the axial discontinuities are formed of embossed ribs that extend radially and also circumferentially in a direction which is leading with respect to the rotation direction of the rotor, and
  • Figures 9(b) and 9(c) are perspective views and cross-section views respectively, similar to Figures 1(b) and 1(c), of the rotor canister of Figure 9(a).
  • a centrifugal separator 10 of the type used with an automobile internal combustion engine comprises a housing enclosure 11 formed by a base 12 and removable cover 13 and between which base and cover extends, along an operationally substantially vertical axis 14, a fixed axle 15 that serves to retain the cover with respect to the base in a fluid-tight manner.
  • the axle includes a supply duct 16 along a part of its length and provides passage for engine lubricant, delivered thereto at elevated pressure by the engine lubricant pump (not shown), to ports 17 which open into the housing enclosure.
  • the base 12 is shaped such that it provides a gravity drain into the engine sump (not shown) for liquid in the enclosure.
  • the axle 15 supports for rotation thereabouts a rotor 20 which comprises a canister for containing the liquid lubricant and, in known manner, is arranged to receive said lubricant from the axle ports at said elevated pressure and eject it from substantially tangentially directed reaction nozzles such that the rotor canister spins at such speed as to effect centrifugal separation of particulate contaminants from the liquid passing therethrough.
  • the rotor canister 20 comprises an outer peripheral wall 21 , including axially extending peripheral side wall 22 displaced from the axis 14 and radially extending upper and lower end walls 23 and 24 respectively, and an inner peripheral wall 25 comprising a tubular member fixed to and extending between said end walls.
  • the tubular member 25 is deformed to locate it with respect to through-apertures in the end walls and is arranged to carry bearing bushes 26, 27 at its ends to support the rotor with respect to the axle for rotation thereabout, and is consequently referred to also as a bearing tube.
  • the bearing tube has therein apertures 28 n , 28 2 ... which direct lubricant delivered by the axle supply duct 16 into the container near to the upper end wall 23 rather than any other part of the housing enclosure.
  • the upper end wall 23 and peripheral side wall of the canister are formed integrally from a single sheet of metal drawn into the canister shape and secured to the lower end wall 24 by peripheral folded seam 29.
  • the rotor canister 20 furthermore includes an internal partition wall 30 extending radially inwardly from the seam 29, of which it is conveniently a part, in a upwardly converging conical manner.
  • the partition wall 30 serves to divide the canister 20 into an upper inlet and separation chamber 33 in communication with apertures 28 ⁇ , 28 2 , ... and an outflow chamber 34 in communication with reaction nozzles 35 in the end wall 24, and furthermore defines at its radially inner periphery 37, a transfer aperture 38 between the separation and outflow chambers.
  • centrifugal separator and rotor canister are conventional.
  • the upper end wall 23, that is the end wall opposite to the outflow chamber, has at its internal surface 23 s an array of axial discontinuities 40 ⁇ , 40 2 ... formed as embossments pressed at the time of drawing the contained wall to shape, and in particular comprise ribs, raised with respect to the internal surface 23 s of the wall, of relatively narrow cross-section and smooth contour side-to-side, within the constraints of being pressed unidirectionally with drawing of the container wall.
  • the ribs extend between the radially inner and outer edges of the end wall, as defined by the junction with the peripheral side wall 22 and bearing tube 25, the ribs having not only a radial component of direction but also a circumferential component as a smooth and consistent curvature along their entire lengths such that at their radially outer regions they are displaced circumferentially with respect to regions inwardly thereof in a direction that is trailing with respect to the rotation direction of the rotor canister that results from ejection of liquid lubricant from the container.
  • the radially outer regions are displaced with respect to the radially inner regions in the same circumferential direction as liquid is ejected from the outflow chamber by way of the reaction nozzles.
  • Liquid is supplied to the rotor canister at elevated pressure and enters the separation chamber 33 in the vicinity of the end wall 23 in a substantially radial direction relative to the rotating canister and at least some of it enters the shallow channels 41 1 , 42 2 , ... formed between adjacent ribs 40-i , 40 2 , ... where it is acted upon by the ribs to the extent that it is given components of motion both circumferentially about the rotation axis and radially towards the outer peripheral side wall.
  • the circumferentially trailing sweep of the axial displacement ribs elongates the effective length of each channel or radial distance to the vicinity of the outer peripheral side wall and subject the liquid to corresponding lower acceleration forces than are seen with straight radial axial displacement ribs.
  • the liquid encounters circumferentially moving, but trailing, ribs which apply forces to the liquid to change its velocity from principally radial to principally circumferential over a longer flow path.
  • the liquid is subjected to a lower level of acceleration force thereon, which force has to be obtained from the energy of the rotating canister. To this end it would appear that less rotation energy is absorbed from the rotating canister in providing radial movement of the liquid relative to the end wall 23.
  • the pressure gradient in the liquid in the direction along the curved path it takes in the channels, that is, following the line of the ribs, is found to be less that with straight radially-extending ribs and thus notwithstanding the lower radial forces applied to the introduced liquid that flows between the ribs, there is less opposition to the flow, and the structure departs from the perceived wisdom that the introduced liquid has to be accelerated forcefully to overcome considerably higher pressure at the radially outer regions if flow is to occur by way of the radially outer regions of the canister chamber rather than along a short-circuit path as discussed above.
  • the curvature of the ribs is chosen having regard to the anticipated conditions of operation, namely lubricant supply pressure (which is substantially constant at engine operating speeds), rotor rotation rate and rate of flow through the canister, such that the lubricant input to the separation chamber at apertures 28, , 28 2 ... maintains a substantially constant velocity vector as it passes towards the peripheral side wall and changes flow direction from one that substantially radial into the chamber to being substantially circumferential at the peripheral side wall.
  • the outer extremities of the ribs are substantially tangential to the edge of the end wall as defined by the peripheral side wall, and the inner extremities may reach the bearing tube substantially perpendicular to the tube, that is radially and in the same direction as new liquid enters the chamber or in a said trailing circumferential direction.
  • Figure 2 is a cross section view similar to Figure 1 (c) of a second embodiment of a rotor canister 50 differing in that in this second embodiment the canister end wall 51 has at its internally facing surface 51 s axial discontinuities comprising an array of full-length ribs 52 ⁇ , 52 2 ... , extending between the radially outer and inner edges of the end wall as described above, and between pairs of adjacent ribs, an array of short ribs 53- t , 53 2 ... which at the outer edge of the end wall conform to the curvature of the full- length ribs but which have their radially inner ends spaced from the radially inner edge of the wall and bearing tube.
  • axial discontinuities comprising an array of full-length ribs 52 ⁇ , 52 2 ... , extending between the radially outer and inner edges of the end wall as described above, and between pairs of adjacent ribs, an array of short ribs 53- t , 53 2 ... which at the outer edge of the end wall conform to the
  • the internal surface 61 s of end wall 61 carries full-length ribs 62, , 62 2 ... whose curvature is such that at their radially inner extremities they are substantially tangential with respect to the inner edge of the end wall and the bearing tube thereat.
  • the end wall 71 has at its internal surface 71 s full length ribs 72, , 72 2 ... which are interspersed with short ribs 73, , 73 2 ... , but wherein the full-length ribs terminate substantially tangentially with respect to the bearing tube.
  • rotor canister 80 shown in Figure 5
  • all of the axial discontinuities at surface 81 s of end wall 81 are formed by radially short ribs, there being a radially inner array 82 ⁇ , 82 2 , 82 3 ... being surrounded by a circumferentially offset radially outer array of ribs 83,, 83 2l 83 3 ....
  • the extremities of the ribs are shown in radially overlapping relationship but this may be considered optional.
  • the axial displacements formed at the end wall 91 and in the internal (to the canister) surface 91 s thereof comprise an outer array of short ribs 93,, 93 2 ... corresponding to ribs 83, ... and an inner array of short ribs 92,, 92 2 ... which extend for a short distance in a radial direction with little or no trailing curvature.
  • the radially-inner, straight ribs guide the liquid that enters the canister in a substantially radial direction to the mainly curved channels 94,, 94 2 , 94 3 ... between adjacent ribs of the outer array.
  • the array of axial discontinuities take the form of alternate depressed and raised regions 103, , 103 2 ... and 104,, 104 2 ... respectively that are circumferentially extensive compared to the ribs described hitherto.
  • the depressed regions 103, ... that correspond to the depressed, embossed ribs being substantially equally dimensioned to the non-depressed regions 104, ... that correspond to the channels between such ribs.
  • the numbers and circumferential widths of the individual axial displacements may vary as desired to achieve different degrees of flow path elongation and dwell time as appropriate for the operating conditions to be met by the rotor canister and centrifugal separator containing it.
  • the upper end wall 111 has a surface 111 s facing into the separation chamber and overlying that surface a carrier member 113 on which are carried axial discontinuities 15,, 115 2 ... extending thereon in said axial, radial and circumferential directions.
  • the axial discontinuities are formed by vanes each having thickness in a circumferential direction that is much less than the vane length, and indeed less than the ribs formed by embossment and described above.
  • the vanes may be formed integrally with the carrier member as moulding or casting of, for example, plastics material or metal, or may be stamped and bent out of a sheet of suitable material.
  • vanes may take any of the variety of forms described above, varying in circumferential thickness as well as length and curvature. Also, although it is convenient for such vanes to extend in an axial direction, they may be inclined thereto.
  • axial displacements particularly in the form vanes which are thin in a circumferential direction, may be formed by discrete shaped bodies of any material secured directly to the internal surface of the end wail rather than a carrier member such as 113.
  • centrifugal separator rotor canister in which an inner peripheral wall is defined by an apertured bearing tube 25 that rotates as part of the canister about the axle 15, and which bearing tube conveniently defines the radially inner edge of the end wall 23 from the point of having axial surface projection
  • the rotor canister man be formed without such tube and with the bearing bushes 26, 27 mounted directly in the canister end walls so that the axle 15 defines a stationery inner wall of the canister and the supply ports 17 open directly into the separation chamber of the canister.
  • the above described embodiments have concentrated upon a form of rotor canister in which the axial discontinuities at the end wall adjacent the liquid inlet region exhibit at their radially outer regions a circumferential displacement in a trailing direction.
  • FIGS 9(a) to 9(c) these are generally similar to the views of Figures 1(a) to 1 (c) but of a further embodiment of centrifugal separator 200 including a ninth embodiment of rotor canister 220.
  • Those parts of the separator housing which correspond to those described above with reference to Figure 1 (a) are given like references and not described further.
  • the rotor canister 220 likewise has many parts identical with rotor canister 20 and like references are again used and detailed description omitted. Where the rotor canister does differ is that the axial displacements, in the form of embossed ribs 240,, 240 2 , 240 3 ... have their radially outer regions circumferentially displaced in a direction that is leading, or forward, with respect to the clockwise rotation direction of the canister that results from ejection of the liquid from the outflow chamber.
  • the additional degree of acceleration from axial discontinuities with circumferentially leading regions may be achieved at little overall cost of energy absorption from the rotating canister system.
  • the axial displacements have been at the upper end wall of the rotor canister separation chamber, and opposite to the outflow chamber at the lower end of the canister, it will be appreciated that if the rotor is designed such that liquid is ejected from an outflow chamber at the operationally upper end of the rotor then the separation chamber inlet apertures will be moved to the lower end wall of the canister and the axial displacements formed at such lower end wall.
  • any component part of length may be very shallow or non-existent, is straight, and/or any axial displacement may, along its radial length, comprise a series of straight or nearly-straight segments inclined with respect to each other so as to give, along the whole length, an effective curvature in said circumferentially trailing direction.
  • the centrifugal separator has been shown with the rotor committed to rotation about the axle in a clockwise direction and the axial discontinuities circumferentially displaced to suit, it will be appreciated that the rotor canister may be arranged to have the reaction jet nozzles oppositely directed whereby it undergoes rotation in an anti-clockwise direction about the axis, and with the circumferential displacement of the radially outer regions of the axial displacements also oppositely directed from that illustrated.
  • non-radial axial displacement is not limited to rotor canisters of the sealed or discardable type and may be employed with different types of canister construction that are known in the art and permit dis-assembly for cleaning and the like.

Landscapes

  • Centrifugal Separators (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
  • Cyclones (AREA)
EP98940398A 1997-09-03 1998-08-26 Zentrifugale trennvorrichtung Expired - Lifetime EP1009537B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB9718564A GB2328890B (en) 1997-09-03 1997-09-03 Centrifugal separation apparatus
GB9718564 1997-09-03
PCT/GB1998/002572 WO1999011381A1 (en) 1997-09-03 1998-08-26 Centrifugal separation apparatus

Publications (2)

Publication Number Publication Date
EP1009537A1 true EP1009537A1 (de) 2000-06-21
EP1009537B1 EP1009537B1 (de) 2002-06-12

Family

ID=10818385

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98940398A Expired - Lifetime EP1009537B1 (de) 1997-09-03 1998-08-26 Zentrifugale trennvorrichtung

Country Status (7)

Country Link
EP (1) EP1009537B1 (de)
JP (1) JP2001518374A (de)
AT (1) ATE218924T1 (de)
DE (2) DE69806021T2 (de)
GB (1) GB2328890B (de)
WO (1) WO1999011381A1 (de)
ZA (1) ZA987954B (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9718563D0 (en) * 1997-09-03 1997-11-05 Glacier Metal Co Ltd Centrifugal Separation Apparatus
US8220177B2 (en) * 2007-05-23 2012-07-17 Gala Industries, Inc. Centrifugal pellet dryer screen with integral embossed deflector strips
KR101151975B1 (ko) 2010-11-03 2012-06-01 울산대학교 산학협력단 복합 구동형 원심 분리기
CN111663980B (zh) * 2020-06-09 2020-12-29 深圳市创裕达电子有限公司 一种智能滤芯

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB732132A (en) * 1952-08-01 1955-06-22 Glacier Co Ltd Improvements in or relating to centrifugal separators
GB1036661A (en) * 1964-02-26 1966-07-20 Veb Zek Improvements in or relating to centrifugal oil separators
JPS5620661U (de) * 1979-07-25 1981-02-24
US4430071A (en) * 1982-05-27 1984-02-07 Dorr-Oliver Incorporated Feed seal for bottom feed centrifuge
GB8504880D0 (en) * 1985-02-26 1985-03-27 Ae Plc Disposable cartridges
AU6891191A (en) * 1989-12-08 1991-07-18 Reginald Norman Harris Centrifugal separator
GB2274413B (en) * 1993-01-23 1996-07-10 Glacier Metal Co Ltd Oil cleaning assemblies for engines
US5637217A (en) * 1995-01-25 1997-06-10 Fleetguard, Inc. Self-driven, cone-stack type centrifuge
US5575912A (en) * 1995-01-25 1996-11-19 Fleetguard, Inc. Self-driven, cone-stack type centrifuge

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9911381A1 *

Also Published As

Publication number Publication date
ATE218924T1 (de) 2002-06-15
WO1999011381A1 (en) 1999-03-11
GB2328890A (en) 1999-03-10
JP2001518374A (ja) 2001-10-16
ZA987954B (en) 1999-03-03
DE69806021D1 (de) 2002-07-18
DE29815879U1 (de) 1998-11-26
GB2328890B (en) 2001-08-22
GB9718564D0 (en) 1997-11-05
EP1009537B1 (de) 2002-06-12
DE69806021T2 (de) 2003-02-06

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