WO1998011994A1 - Centrifugal separation apparatus - Google Patents
Centrifugal separation apparatus Download PDFInfo
- Publication number
- WO1998011994A1 WO1998011994A1 PCT/GB1997/002248 GB9702248W WO9811994A1 WO 1998011994 A1 WO1998011994 A1 WO 1998011994A1 GB 9702248 W GB9702248 W GB 9702248W WO 9811994 A1 WO9811994 A1 WO 9811994A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- housing
- centrifugal separator
- rotor
- charaderised
- daimed
- Prior art date
Links
- 238000000926 separation method Methods 0.000 title claims abstract description 18
- 239000012530 fluid Substances 0.000 claims description 7
- 239000002184 metal Substances 0.000 claims description 5
- 238000009825 accumulation Methods 0.000 claims description 3
- SGPGESCZOCHFCL-UHFFFAOYSA-N Tilisolol hydrochloride Chemical compound [Cl-].C1=CC=C2C(=O)N(C)C=C(OCC(O)C[NH2+]C(C)(C)C)C2=C1 SGPGESCZOCHFCL-UHFFFAOYSA-N 0.000 claims 9
- 239000007788 liquid Substances 0.000 abstract description 48
- 241000239290 Araneae Species 0.000 abstract description 3
- 239000000356 contaminant Substances 0.000 abstract description 3
- 239000010705 motor oil Substances 0.000 abstract description 2
- 239000003921 oil Substances 0.000 abstract 2
- 230000009194 climbing Effects 0.000 abstract 1
- 238000006243 chemical reaction Methods 0.000 description 11
- 230000000694 effects Effects 0.000 description 6
- 239000000314 lubricant Substances 0.000 description 4
- 238000009987 spinning Methods 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B04—CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
- B04B—CENTRIFUGES
- B04B5/00—Other centrifuges
- B04B5/005—Centrifugal separators or filters for fluid circulation systems, e.g. for lubricant oil circulation systems
Definitions
- This invention relates to centrifugal separation apparatus for separating particutate contaminants from liquids, such as engine lubricants, passed therethrough, and in particular relates to the efficient drainage of low viscosity liquids from such apparatus.
- Centrifugal separators are well known for use within the lubrication systems of vehicle internal combustion engines as efficient means for removing very small paniculate 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 substantially tangentially- dire ed jet reaction nozzles, the reaction to said ejection causing the rotor canister 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.
- the jet or reaction nozzles are directed substantially tangentially 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 rotor canister may also be impeded in rotation by droplets of lubricant emitted by the nozzles which splashes from the surfaces within the housing.
- the lubricant Whilst this reduces the tendency to splash and impede rotation to some extent, but not completely (and for which reason the axes of the reaction nozzles may be declined towards the floor of the housing), the lubricant is incident on the wall and or floor at such angle as to cause this liquid to circulate around the housing as it falls towards the floor thereof and the drain.
- Patent specifications GB 2049494 and 2120134 describe a centrifugal separator in which the floor of a drculariy cylindrical housing is in the form of a substantially conical funnel leading to a central, or axial, drainage duct.
- the centrifugal separation rotor composes a canister mounted for rotation within the housing (from the side wall of which it is separated by only a small radial dearance) on an axle which is supported, with respect to the housing, raised above the floor by a cage or spider comprising an array of divergent legs separated drcumferentially by drainage apertures for the liquid ejected from the rotor.
- a vortex of liquid with a higher viscosity tends to have a more uniform structure and surface on which the newly ejected liquid impinges and merges with uniform results
- a vortex of liquid with a low viscosity is found to have local turbulence within the body of the vortex and out of its surface and a tendency for both the liquid of the vortex and liquid ejeded from the rotor that is inddent on the vortex to splash and froth in the proximity of the rotor to the extent that the presence per se of such vortex separately from its dimbing to fill the gap between rotor canister and housing, is a source of impedance to canister rotation detracting from the separation effidency.
- a self-powered centrifugal separator comprises a housing defined by a cylindrical side wall and by a floor shaped to effect drainage of fluid from the housing into a drainage dud, a centrifugal separation rotor, supported with respect to the housing for rotation therein about a rotation axis, arranged to receive fluid at elevated pressure and ejed it by way of substantially tangentially direded readion nozzles into the housing, said rotor being supported spaced with resped to the floor of the housing by means of a cage having a central mounting region coupled to the rotor and a surrounding apertured drainage region extending to the housing, and vortex disruption means, operable to inhibit accumulation of ejeded fluid within the housing, comprising at least one defledion vane extending overlying a part of the cage drainage region in the same direction as rotation of the rotor, said vane having a first edge extending substantially parallel to the housing side wall closer than the spa ng between said side wall and separation rotor and
- Figure 1 is a sedional elevation through a centrifugal separator in accordance with the present invention.
- Figure 2 is a top view of the separator of Figure 1 with the rotor removed.
- a centrifugal separator 10 for use in the lubrication system of a vehicle internal combustion engine comprises a housing 11 in the form of a right circular cylinder centred on longitudinal axis 12 and open at one end 13.
- the housing is surrounded thereat by a sealing element 14 for mounting against a surface of the vehide engine (not shown) which serves to close off the end of the housing and from which the housing operably depends.
- the other end of the housing is formed as a floor 15 which tapers as a funnel to a coaxial drainage dud 16.
- An axle 17 extends along the longitudinal axis 12 within the housing from a first axle end region 17', at which it is secured to a mount 20, to a second end region 17" having a threaded periphery by way of which the axle, and the separator as a whole, is removably secured to the vehide engine.
- the mount 20 comprises a cage or spider 21 having a central mounting region 22, to which the axle end region 17' is secured spaced with resped to the floor 15, and a surrounding apertured drainage region, indicated at 23, extending radially and axially to the housing.
- the drainage region of the cage comprises an array of legs 25 1f 25 2 , 25 3 diverging with resped to each other radially outwardly from the central mounting region and separated in a drcumferential direction by drainage apertures 26 ⁇ , 26 2 , 26 3 , said legs at the ends thereof adjacent the housing being jointed by an annular rim 27 in contad with the housing wall continuously about the periphery.
- the annular rim is curled to conform to the comer of the housing between the side wall and floor to align the axes of the axle and housing, and is secured to the housing by welding or the like, whereby the housing is secured with resped to the vehide by way of the axle 17. That is, the axle depends from the vehide and the housing depends from the axle.
- the cage is formed from a flat metal sheet by stamping out the drainage apertures 26, etc and then deforming it axially to provide said central mounting region, legs and annular rim integrally,
- the cage appears in elevation with the aperture drainage region as a truncated cone and the legs and drainage apertures defining a frusto conical plane within the housing.
- the legs 25 ⁇ etc of the cage are provided with strength to take axial mounting loads by means of pressed ribs or embossment 28 1t 28 2 283.
- a correspondingly legged bra ⁇ ng member 30, having a central region 31 and integral legs 32 ⁇ etc, is disposed adjacent to the cage sheet with the legs overlying and joined to each other and the central mounting regions 22 and 31 spaced axially as a 'box section' into which the end region 17' of the axle is mounted.
- the axle 17 contains a passage extending from the end 17' and opening by way of transverse aperture 35.
- a centrifugal separation rotor 40 in the form of an annular canister having an integral sidewall and top portion 41 and base portion 42 containing an array of jet reaction nozzles, only one of which is shown at 43.
- the portions 41 and 42 surround a tubular member 44 which extends for the length of the rotor and defines an annular endosure 45 within the rotor, the tubular member 44 being apertured at 46 to receive liquid from the axle aperture 35 and further ca ⁇ rying at opposite ends thereof bearing bushes 47 and 48 by way of which the rotor is able to undertake high speed rotation about the axle.
- the jet reaction nozzles 43 et al in the base of the rotor are direded substantially tangentially with resped to the longitudinal axis 12 and possibly slightly dedined towards the floor of the housing, such arrangement being conventional to avoid, as far as is feasible, the liquid from the reaction jets which impinges against the wall of the housing from splashing against the rotor and disrupting its smooth rotation.
- the drcular cross section of the housing encourages the discharged liquid to drculate around the housing, low viscosity liquid tending on the one had to swirl more readily and rapidly but on the other hand more turbulentiy and presenting a rough surface, so that frothing and splashing of the vortex liquid itself and subsequently ejeded liquid which is inddent upon the liquid of the vortex is more likely to forth and splash and impinge detrimentally on the rotor canister.
- low liquid viscosities it is perceived as being the presence per se of a vortex of undrained liquid that is detrimental to rotation effidency, irrespective of the effeds of such vortex dimbing the housing wall towards the rotor.
- vortex disruption means is provided, indicated generally at 50 comprising assodated with each radially and axially extending leg of the cage a deflection vane 51 51 2 , 51 3 respectively which extends from the leg in the same direction as the rotation of the rotor and overlying a part of the cage drainage region 26 1( 26 2 , 23a respectively.
- Each vane such as 51 1 , is formed as an integral extension of a layer of the laminated leg, that is, formed by a sheet of metal, conveniently that of the leg member 25 ⁇ .
- the vane extends in the same direction as rotation of the rotor, overlying the cage drainage region aperature 26 that is, in a generally tangential direction in which it would intersed the side wall of the housing, but also is bent with resped to the edge of the leg in a direction towards the wall so that it intrudes into the region above the drainage region through which the reaction jets are ejeded such that its lower surface serves to intercept such jets at appropriate rotational positions of the rotor.
- a readion jet impinge directiy upon the deflection vane, it impinges upon the housing side wall which defleds it drcumferentially and by gravitational forces, impinge upon any liquid attempting to drculate as a vortex above rim 27.
- the deflection vane extends also to the vidnity of the side wall of the housing and any part of it effeded by the annular rim 27.
- the vane 51 has a first edge 52 ⁇ which extends substantially parallel to, the side wall being indined to the longitudinal axis 12 in accordance with the deflection of the vane; it has a second edge 53 ⁇ which extends from the end of the first edge to the vidnity of the rotor mounting region.
- the deflection vane extends from the leg to the extent that the second edge extends (in plan view) in a substantially radial direction towards the housing wail.
- the intersection between side wall and rim 27 is both cranked, in resped of the side wall locating the rim and the additional thickness of the rim, and curved by the curled form of the rim. Therefore it is convenient to cut the edge of the more blank before bending so that it conforms dosely to the shape locally.
- the first edge 521 is conveniently straight, notwithstanding that it is intended to lie against a side wall curved in the drcumferential direction, providing that any part of the edge is doser to the side wall than the separation between rotor canister and side wall.
- the first edge is arranged to contad the wall at one or both edges, but contad is not essential if the maximum spadng is not exceeded, permitting the vane to be set with assembly of the cage prior to disposal within the housing.
- vane 25 1t is of course applicable to the other vanes 25 2 and 25a.
- Each vane is conveniently a flat plane so that liquid ejeded from the rotor canister in a tangential direction is defleded inwardly perpendicularly to the legs/drainage apertures whilst being a simple structure to manufacture, but if desired the vane may have a curvature along and/or across all or part of it to modify the redirection of the liquid or disruption of any vortex tending to form.
- each vane overlies the respective drainage aperture, to an extent which does not interfere with the effective area as seen liquid above it, by bending the vane upwardly towards the rotor and housing. It will be appredated that if desired the vane may be less indined, if at all, and extend further in a drcumferential direction until intersection with the side wall, that is, tangentially.
- each deflection vane may be formed integrally with either layer of such laminated leg strudure or even formed non-integrally, being either secured to any such leg structure or, in the case of such laminated leg strudure, being sandwiched between laminations.
- Any deflection vane may be formed of other than the above-mentioned sheet metal, provided it is compatible with the operating conditions encountered within the housing.
- axle mount cage may be formed substantially as described but omitting the bra ng member, which structural form limits only the options available for mounting the deflection vanes.
- axle mount cage may be formed with other than discrete identifiable legs separated by arcuate drainage apertures, for example, as a mesh or perforated sheet structure, but by appropriate construction one or more such deflection vanes may be employed attached to such mount or separately mounted within the housing between the mount and rotor.
- centrifugal separator strudure described above has a fixed axle which supports and defines a rotation axis for the separation rotor canister. It will be appredated that the present invention is applicable without change where the separation rotor is of the type that has an integral rotatable spindle which is mounted in place of the axle.
- the floor of the housing need not be of the funnel shape of the above-described embodiment as such effects occur with substantially 'flaf floors where such rotational motion is permitted to build up in the ejeded fluid.
Landscapes
- Centrifugal Separators (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Cyclones (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP97937692A EP0927079B1 (en) | 1996-09-17 | 1997-08-21 | Centrifugal separation apparatus |
AT97937692T ATE217211T1 (en) | 1996-09-17 | 1997-08-21 | SEPARATION CENTRIFUGE |
US09/254,317 US6196962B1 (en) | 1996-09-17 | 1997-08-21 | Centrifugal separator with vortex disruption vanes |
DE69712497T DE69712497T2 (en) | 1996-09-17 | 1997-08-21 | SEPARATION CENTRIFUGE |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9619366.9 | 1996-09-17 | ||
GB9619366A GB2317128B (en) | 1996-09-17 | 1996-09-17 | Centrifugal separation apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1998011994A1 true WO1998011994A1 (en) | 1998-03-26 |
Family
ID=10800037
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB1997/002248 WO1998011994A1 (en) | 1996-09-17 | 1997-08-21 | Centrifugal separation apparatus |
Country Status (7)
Country | Link |
---|---|
US (1) | US6196962B1 (en) |
EP (1) | EP0927079B1 (en) |
AT (1) | ATE217211T1 (en) |
DE (1) | DE69712497T2 (en) |
GB (1) | GB2317128B (en) |
WO (1) | WO1998011994A1 (en) |
ZA (1) | ZA978290B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6364822B1 (en) | 2000-12-07 | 2002-04-02 | Fleetguard, Inc. | Hero-turbine centrifuge with drainage enhancing baffle devices |
Families Citing this family (42)
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---|---|---|---|---|
GB2322314B (en) * | 1997-02-21 | 2000-08-23 | Glacier Metal Co Ltd | Centrifugal separator |
US6579220B2 (en) | 1999-07-07 | 2003-06-17 | Fleetguard, Inc. | Disposable, self-driven centrifuge |
US6602180B2 (en) | 2000-04-04 | 2003-08-05 | Fleetguard, Inc. | Self-driven centrifuge with vane module |
US6652439B2 (en) | 2000-04-04 | 2003-11-25 | Fleetguard, Inc. | Disposable rotor shell with integral molded spiral vanes |
US6540653B2 (en) | 2000-04-04 | 2003-04-01 | Fleetguard, Inc. | Unitary spiral vane centrifuge module |
US6551230B2 (en) | 2000-04-04 | 2003-04-22 | Fleetguard, Inc. | Molded spiral vane and linear component for a centrifuge |
US6533712B1 (en) * | 2000-10-17 | 2003-03-18 | Fleetguard, Inc. | Centrifuge housing with oil fill port |
US6793615B2 (en) * | 2002-02-27 | 2004-09-21 | Fleetguard, Inc. | Internal seal for a disposable centrifuge |
US7210195B2 (en) * | 2002-10-11 | 2007-05-01 | Rexair, Inc. | Integrated spider separator |
US8075668B2 (en) | 2005-03-29 | 2011-12-13 | Dresser-Rand Company | Drainage system for compressor separators |
GB2425077B (en) * | 2005-04-15 | 2009-11-18 | Mann & Hummel Gmbh | Centifrugal separator and rotor therefor |
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CA2663880C (en) | 2006-09-25 | 2015-02-10 | William C. Maier | Compressor mounting system |
BRPI0718451A2 (en) | 2006-09-25 | 2013-11-26 | Dresser Rand Co | FLUID DEFLECTOR FOR FLUID SEPARATOR DEVICES |
BRPI0717253B1 (en) | 2006-09-26 | 2018-05-08 | Dresser Rand Co | fluid separator |
US8021290B2 (en) * | 2007-11-26 | 2011-09-20 | Honeywell International Inc. | Oil centrifuge for extracting particulates from a fluid using centrifugal force |
BRPI0908051A2 (en) | 2008-03-05 | 2015-08-11 | Dresser Rand Co | Compressor set including separator and ejector pump |
US8062400B2 (en) | 2008-06-25 | 2011-11-22 | Dresser-Rand Company | Dual body drum for rotary separators |
US7922218B2 (en) | 2008-06-25 | 2011-04-12 | Dresser-Rand Company | Shear ring casing coupler device |
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US8210804B2 (en) | 2009-03-20 | 2012-07-03 | Dresser-Rand Company | Slidable cover for casing access port |
US8061972B2 (en) | 2009-03-24 | 2011-11-22 | Dresser-Rand Company | High pressure casing access cover |
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US20110097216A1 (en) * | 2009-10-22 | 2011-04-28 | Dresser-Rand Company | Lubrication system for subsea compressor |
US9095856B2 (en) | 2010-02-10 | 2015-08-04 | Dresser-Rand Company | Separator fluid collector and method |
WO2012009159A2 (en) | 2010-07-15 | 2012-01-19 | Dresser-Rand Company | Radial vane pack for rotary separators |
US8673159B2 (en) | 2010-07-15 | 2014-03-18 | Dresser-Rand Company | Enhanced in-line rotary separator |
WO2012012018A2 (en) | 2010-07-20 | 2012-01-26 | Dresser-Rand Company | Combination of expansion and cooling to enhance separation |
US8821362B2 (en) | 2010-07-21 | 2014-09-02 | Dresser-Rand Company | Multiple modular in-line rotary separator bundle |
EP2614216B1 (en) | 2010-09-09 | 2017-11-15 | Dresser-Rand Company | Flush-enabled controlled flow drain |
US9024493B2 (en) | 2010-12-30 | 2015-05-05 | Dresser-Rand Company | Method for on-line detection of resistance-to-ground faults in active magnetic bearing systems |
US8994237B2 (en) | 2010-12-30 | 2015-03-31 | Dresser-Rand Company | Method for on-line detection of liquid and potential for the occurrence of resistance to ground faults in active magnetic bearing systems |
US9551349B2 (en) | 2011-04-08 | 2017-01-24 | Dresser-Rand Company | Circulating dielectric oil cooling system for canned bearings and canned electronics |
WO2012166236A1 (en) | 2011-05-27 | 2012-12-06 | Dresser-Rand Company | Segmented coast-down bearing for magnetic bearing systems |
US8851756B2 (en) | 2011-06-29 | 2014-10-07 | Dresser-Rand Company | Whirl inhibiting coast-down bearing for magnetic bearing systems |
JP6167381B2 (en) * | 2013-04-09 | 2017-07-26 | サクラ精機株式会社 | Centrifugal smearing device and sealed rotating container |
CN112648044B (en) * | 2019-10-11 | 2022-02-25 | 东京滤器株式会社 | Oil separator |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1980001764A1 (en) * | 1977-06-17 | 1980-09-04 | Glacier Metal Co Ltd | Centrifugal separator |
US4284504A (en) * | 1979-10-09 | 1981-08-18 | Hastings Manufacturing Company | Centrifugal spin-on filter or separator and method of making and assembling the same |
GB2120134A (en) * | 1982-04-16 | 1983-11-30 | Ae Plc | Centrifugal separator |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2049494B (en) * | 1979-04-12 | 1982-12-15 | Glacier Metal Co Ltd | Centrifugal separator |
US4400167A (en) * | 1980-04-11 | 1983-08-23 | The Glacier Metal Company Limited | Centrifugal separator |
CA2130243A1 (en) * | 1993-09-09 | 1995-03-10 | Lonny R. Kelley | Oil spill recovery centrifuge |
-
1996
- 1996-09-17 GB GB9619366A patent/GB2317128B/en not_active Expired - Fee Related
-
1997
- 1997-08-21 WO PCT/GB1997/002248 patent/WO1998011994A1/en active IP Right Grant
- 1997-08-21 EP EP97937692A patent/EP0927079B1/en not_active Expired - Lifetime
- 1997-08-21 AT AT97937692T patent/ATE217211T1/en not_active IP Right Cessation
- 1997-08-21 DE DE69712497T patent/DE69712497T2/en not_active Expired - Lifetime
- 1997-08-21 US US09/254,317 patent/US6196962B1/en not_active Expired - Lifetime
- 1997-09-15 ZA ZA9708290A patent/ZA978290B/en unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1980001764A1 (en) * | 1977-06-17 | 1980-09-04 | Glacier Metal Co Ltd | Centrifugal separator |
US4284504A (en) * | 1979-10-09 | 1981-08-18 | Hastings Manufacturing Company | Centrifugal spin-on filter or separator and method of making and assembling the same |
GB2120134A (en) * | 1982-04-16 | 1983-11-30 | Ae Plc | Centrifugal separator |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6364822B1 (en) | 2000-12-07 | 2002-04-02 | Fleetguard, Inc. | Hero-turbine centrifuge with drainage enhancing baffle devices |
Also Published As
Publication number | Publication date |
---|---|
ZA978290B (en) | 1998-03-17 |
ATE217211T1 (en) | 2002-05-15 |
GB2317128A (en) | 1998-03-18 |
EP0927079B1 (en) | 2002-05-08 |
GB2317128B (en) | 2000-07-12 |
US6196962B1 (en) | 2001-03-06 |
DE69712497D1 (en) | 2002-06-13 |
EP0927079A1 (en) | 1999-07-07 |
GB9619366D0 (en) | 1996-10-30 |
DE69712497T2 (en) | 2003-01-02 |
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