WO1983002406A1 - Centrifugal separator - Google Patents

Centrifugal separator Download PDF

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Publication number
WO1983002406A1
WO1983002406A1 PCT/GB1983/000009 GB8300009W WO8302406A1 WO 1983002406 A1 WO1983002406 A1 WO 1983002406A1 GB 8300009 W GB8300009 W GB 8300009W WO 8302406 A1 WO8302406 A1 WO 8302406A1
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WO
WIPO (PCT)
Prior art keywords
oil
chamber
rotor
air
float
Prior art date
Application number
PCT/GB1983/000009
Other languages
English (en)
French (fr)
Inventor
Plc Ae
Henry Woods Martin
Original Assignee
Plc Ae
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 Plc Ae filed Critical Plc Ae
Priority to DE19838322870U priority Critical patent/DE8322870U1/de
Priority to DE8383900493T priority patent/DE3363978D1/de
Priority to AT83900493T priority patent/ATE20315T1/de
Priority to BR8305198A priority patent/BR8305198A/pt
Publication of WO1983002406A1 publication Critical patent/WO1983002406A1/en

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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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01MLUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M1/00Pressure lubrication
    • F01M1/10Lubricating systems characterised by the provision therein of lubricant venting or purifying means, e.g. of filters
    • F01M2001/1028Lubricating systems characterised by the provision therein of lubricant venting or purifying means, e.g. of filters characterised by the type of purification
    • F01M2001/1035Lubricating systems characterised by the provision therein of lubricant venting or purifying means, e.g. of filters characterised by the type of purification comprising centrifugal filters

Definitions

  • This invention relates generally to centrifugal separators, and more particularly to centrifugal separators of the self-powered type that can be used for removing contaminants from a liquid system such as the lubricating oil system .of internal combustion engines.
  • these filters can be classified as one of two types, either full flow or bypass filters.
  • a porous type filtering element is used, and it is placed directly between the oil pump and the remainder of the lubricating system so that all of the oil passes through the filter.
  • Such filters generally tend to have filtering elements of relatively large porosity, not only because they must pass a relatively high volume of oil with a minimum of pressure drop across the filter, but also because as the contaminants are filtered out of the oil and remain on the filter element, they tend to reduce the size of the pores, which further limits the filtering action and increases the problems of' rate of oil flow through the filter. With such full flow filters, it may be necessary to provide a bypass passage so that when the filter prcduces an excessive amount of restriction, oil flow is allowed to pass directly around the filter and such oil receives no filtering action whatever. Furthermore, because of the relatively large porosity of the filter elements, there are a number of fine-grained particulate materials which are not filtered out of the oil because they are too small to be retained on the filter element.
  • the other type of oil filter is the bypass type in which a certain amount of oil as it leaves the oil pump is diverted into a filter from which it returns to the oil sump to be recirculated through the oil pump without passing through the remainder of the lubricating system. While such bypass filters filter only a portion of the oil being pumped, they can be very efficient in terms of removing very small particulates because they operate under a high pressure drop between the supply pressure and the oil sump.
  • bypass filters may be of the mechanical type .having a porous filter element
  • centrifugal type filters are quite advantageously used in such applications.
  • a typical such centrifugal filter is the one shown in Beazley patent No. 3,432,091, which includes a hollow casing within which is rotatably mounted a rotor element having an internal chamber and an outer wall. The casing is connected directly to the sump or drain, while high pressure oil is directed into the interior of the rotor. As the rotor fills with pressurized oil, the oil passes downwardly to a pair of diametrically located discharge orifices or jets having a restricted diameter.
  • centrifugal filters of this type function normally, they will remove a very high proportion of the contaminants and keep the lubricating oil from deteriorating.
  • fil ter cleaning or replacement should be done at certain regular intervals, and if the filter has been functioning in its intended manner, there should be a predictable amount of accumulated sludge in the filter rotor.
  • the filter has not been functioning in the intended manner. This presumably results either from the rotor not reaching the intended operating speed of rotation or by the fact that perhaps at certain times the rotor was not even spinning at all.
  • the present invention provides an improved arrangement for preventing possible build-up of return oil in the filter housing by introducing a controlled amount of air at a pressure above atmospheric into a chamber below the filter to prevent the possibility of the oil level rising upward until it may contact the rotor.
  • a regulator housing mounted directly below the filter housing, and which includes an air valve which is connected to a suitable source of air pressure such as an air brake compressor or other pump.
  • a float is mounted within this regulator chamber and is actuated by the oil level within the chamber. As long as this oil level remains low, the air valve is closed and no additional air is admitted to the chamber. However, if the oil level begins to rise, as will occur when the entrainment of air from the jets within the return oil removes air from the filter housing, the oil level will begin to build up and raise the float.
  • the float When the float reaches a predetermined position, it will open the air valve so that air from the pressure source enters the regulator chamber, and hence, by its direct connection, the interior of the filter housing. Because of this positive action, the air pressure within the filter housing will rise above atmospheric and increase the force on the oil within the return line, to increase the rate of return flow and lower the oil level within the regulator chamber. It has been found that, regardless of the pressure of the air source, it is never necessary to increase the pressure within the filter housing by more than a few psi, so that the pres sure drop of oil across the rotor orifices or jets remains substantially the same, to allow the filter to function in the normal manner.
  • the amount of air that is added through the regulator is relatively small in volume, and corresponds only to the amount of entrained air removed through the oil flowing back, to the sump.
  • Another feature of this invention is that it has been found possible to greatly reduce the diameter of the return line from the air regulator back to the sump.
  • the return lines formerly were sized to allow a free drain without any pressure assist other than normal forces of gravity, since it was always a procedure to mount the filter substantially above the oil level in the sump.
  • Using the regulator of this invention it is now possible to use a return line that is not much larger than, and may even be equal in size to, the oil supply line from the engine oil pump.
  • the mounting arrangement possibilities are greatly increased, since the use of a smaller drain hose provides greater flexibility for the hose, and therefore more convc luted paths of the hose, without creating undesirable restrictions against return or drain flow of the oil. Additionally, it is even possible to mount the filter below the level of. oil in the sump, since there is now a small positive pressure which can overcome the forces of gravity and possibly force the oil to the return line into the sump.
  • centrifugal filters of the disposable type such as those shown in U.S. patents Nos. 4,106,689 and 4,165,032.
  • the float may be mounted within the dispcsable container and so arranged that it controls the actuation of an air valve in an air supply line connected directly to the casing of the disposable filter. Since the air valve can be mounted directly in the casing, this means that when the filter is full it can be removed and replaced very quickly, and therefore requires only the removal of the casing in its connection lines as well as the disconnection and reconnection of the air supply line, so that the down-time of the machinery with which the filter is used is held to a minimum.
  • centrifugal filter is used in this specification, it will be appreciated that true filtration need not take place and that separation of contaminants is effected by centrifugal force.
  • FIG. 1 is an elevational, cross-sectional view through a centrifugal filter and its mounting in accordance with a first embodiment of this invention
  • Fig. 2 is an elevational, cross-sectional view through a second embodiment of this invention utilizing a filter of the disposable type;
  • Fig. 3 is a. cross-sectional view taken on line 3-3 of Fig. 2;
  • Fig. k is an elevational view partially in cross section of a third embodiment of this invention.
  • Fig. 5 is an elevation, cross-sectional view through a fourth embodiment of the invention.
  • the centrifugal separator or filter 10 includes a lower housing member 11 and an upper housing member 12 which have flanges 13 and 14, respectively, which fit together in interlocking, telescoping relationship.
  • a clamp 16 firmly holds the two members together and an O-ring seal 15 prevents any fluid leakage out of this joint.
  • the upper and lower housings 12 and 11 define a housing chamber 18, which terminates at its lower end in a drain passage 19 extending downwardly and out through the bottom of the lower housing member 11.
  • a rotor 20 which includes a rotor base member 21 having an upwardly extending, peripheral wall 22.
  • the rotor also includes a cover 24 having a top wall 25 and a downwardly extending, peripheral sidewall 27 which terminates in an enlarged flange 28 adapted to fit over the upper end of the peripheral wall 22, and a suitable O-ring seal 31 is provided at this joint to prevent leakage of the oil within the rotor 20 outwardly into the housing chamber 18.
  • the rotor in order to mount the rotor 20 for rotation within the housing chamber 18, the rotor is provided with a spindle 34 which at its lower end extends through an aperture 35 in the rotor base 21.
  • a thrust washer 37 which fits against a flange 38 on the lower end of the spindle.
  • the spindle 34 extends upwardly through an aperture 41 in the rotor cover top wall 25, and above the aperture 41 a nut 43 is threadedly engaged with a threaded portion on the spindle 34 so that, by tightening the nut 43, the rotor cover 24 is forced downwardly to firmly engage the base member at the seal 31, and force the base member against the thrust washer 37 and flange 38, so that the spindle 34 becomes an intergral part of the rotor 20, to rotate therewith.
  • the rotor 20 is mounted on a pair of bearings supported in the upper and lower housing members 12 and 11, respectively , and , accordingly , at its lower end , the spindle 34 has a journal porti on 45 which fits within a bearing member 47 mounted in a recess 48 f ormed in projecting boss 49 on the lower housing member 11.
  • the bearing 47 has an outwardly extending flange 50 above the recess 48 arranged to abut against the thrust washer 37 and support the weight of the rotor .
  • the top wall 52 of upper housing member 12 is provided with a f ormed recess 53 which receives a radial bearing 54 and thrust bearing 55 to journal the upper end 57 of spindle 34.
  • the spindle 34 has a bore 59 of unif orm diameter therethrough , so that the hydraulic f orces at e2ch end of the spindle 34 at the bearing recesses 48 and 53 are balanced , and the thrust washer 37 needs support only the weight of the rotor 20 i ndependent of any pressure f orces .
  • Oil is supplied under pressure to the separator 10 by a line from the oil pump of an internal combustion engine or other machine (not shown) and this line is connected to an inlet bore 62 formed in the lower housing member 11.
  • the oil then- passes through an isolating valve 63 and passage 64 to the bearing recess 48 , f rom which it can enter the bore 59 and spindle 34.
  • the isolating valve 63 is spring-biased to a closed posi tion under low oil pressure conditi ons , such as at engine idle , so as not to rob oil from the engine bearings.
  • This valve is optional and is not used in many applicati ons . Therefore , it does not f orm any part of the present invention.
  • a cylindrical screen 71 extends coaxi ally with the spindle 34 and spaced away therefr ⁇ n between the deflector cup 67 at the upper end in a conical baffle 73 at the lower end.
  • Conical baffle 73 extends downwardly and outwardly to fit within an annular groove 74 formed in the rotor base member 21.
  • the separator 10 must be mounted in a generally vertical position for optimum performance, so that there is a minimum of unbalanced forces acting on the rotor 20. Accordingly, the lower housing member is secured to the mounting bracket 90, which in turn is secured to a frame rail indicated at 92 of a motor vehicle or other support by means of suitable bolts 93.
  • the return flow of oil from the housing chamber 18 to the sump of the internal combustion engine was performed by providing a suitable fitting connected to the drain passage 19 so that the oil could then pass by a suitable flexible hose or pipe to the oil pump, under normal conditions, this return line had to be of relatively large diameter because, for optimum speed of the rotor, no oil could be allowed to accumulate within the housing chamber 18 , which is normally filled with air which may enter through the drain line by counterflow from the sump or by means of an air bleed valve , which is no longer required with the present invention .
  • the return line Since there is substantially no pressure drop between the housing chamber 18 and the oil sump , the return line must be of relatively large diameter to prevent fluid from building up within the housing chamber 18 , because if the level does build up where the oil can reach the level of the rotor base member 21 , the fricti onal drag will cause the rotor to rotate at a much lower speed , thereby greatly decreasing the centrifugal forces required to produce the effective filtering action of these separators , and consequently little or no particulate matter will be removed from the lubricating oil .
  • the jet of oil is broken up into a fine spray of droplets , which tend to entrain or dissolve the air therein , either by actual solution or by f orming a f oam , and as the oil with the entrained air passes back to the sump , it necessarily tends to cause the pressure within the housing chamber 18 to drop so that the oil level will rise upwardly within the drain passage 19 . Accordingly , the present inventi on solves this problem by admitting additional air into the housing chamber 18 to replace the air removed by the entraining acti on of the oil , to positively prevent the oil level f rom rising to contact the rotor base member 21.
  • a regulator housing 95 having a bottom wall 96 and sidewalls 97 defining a chamber 99.
  • the regulator housing 95 is positioned below the mounting bracket 90 , and has a top surface 101 which is clamped against a gasket 104 to the lower side of the mounting bracket 90.
  • the separator 10 can be mounted on the upper side of the mounting bracket 90 using a gasket 103 and , by extending bolts 106 through the l ower housi ng member 11 , the mounting bracket 90 , and the regulator housing 95 , the entire assembly can be clamped together in a unitary relati onship.
  • a drain opening 108 is provided in the regulator housing bottom wall 96 , and to this is connected a return line to the engine sump.
  • the regulator housing 95 also includes an air inlet fitti ng 111 to which is connected an air supply line from a suitable source , such as an air brake compressor, or the like .
  • a suitable source such as an air brake compressor, or the like .
  • Di rectly above the inlet 11 is a reduced diameter threaded bore 112 within which is mounted a valve 113 having an upwardly projecting valve stem 114.
  • This valve may be constructed in the manner of an ordinary tire valve , which is normally closed so that the ai r at the inlet 111 cannot oass the valve . However , whenever the stem 114 is depressed , the valve is opened to allow the passage of air .
  • valve stem 14 Directly above the valve stem 14 is a bore 116 within which is mounted a valve rod 118 having a smaller diameter than that of bore 116 , to allow the passage of air between the valve rod and bore upwardly into the regulator chamber 99 .
  • a float arm 121 carried by a pivot pin 122 secured in the regulator housing adjacent the upper end of valve rod 118.
  • the float arm 121 is connected to a hollow float 124 , which is free to move within the chamber 99 as the arm 121 pivots about the pivot pin 122.
  • the float arm also has an actuating end 126 which extends in the opposite directi on from the- pivot pin 122 to a point above the valve rod 118.
  • the float 124 when there is no oil within the regulator chamber 99 , the float 124 normally is in a lowered positi on so that the actuating end 126 of float arm 121 is spaced above the valve rod 118. Since the valve stem 114 is in a closed positi on , no air enters the chamber through the inlet 111.
  • the filter When the filter is operating so. that oil is discharged into the housing chamber 18 to flow downwardly through the drain passage 19 , oil may build up within the regulator chamber 99 , and if the oil level begins to rise because of insufficient flow rate through the drain opening 108 , the float may rise to the positi on shown in phantom lines at 128.
  • the return line connected to the drain opening 108 is of quite large diameter, the pressure within the regulator chamber 99 and housing chamber 118 will still be at substantially atmospheric pressure.
  • the separator 10 may be located below the oil level in the engine sump, so that there may be a tendency for reverse flow of the oil drain line.
  • the regulator of this invention will then admit air into the housing chamber 18 and the pressure may tend to build up above atmospheric pressure to pre prise the necessary pressure forces to cause a sufficient rate of flow to the sump through the return line to keep the oil level in the regulator housing so that the float is positioned belcw the phantom line position shown at 128. It should be pointed out. that this arrangement now allows the filter to be mounted below the sump level and when the engine is not running, the balance of forces may actually cause the entire housing chamber 18 to be filled with oil by return flow through the drain line. This causes no undesirable condition, but merely a slight delay in the operation of the filter when the engine is started.
  • the housing chamber 18 may be full of oil when the engine starts, the float will be in the upper position and air will immediately enter through the inlet 111, and hence into the housing chamber 18. This then drives the oil level down and when it drops belcw the level of the rotor base member 21, the rotor may then begin to rotate in the customary manner and the oil level will continue downward until stabilized by the position of float 124 in the manner previously described. It should be pointed out that the source of air connected to the air inlet 111 need have a pressure only a small differential above that required within the housing chamber 18.
  • the maximum pressure expected within the hous ing 18, either because of a low position of the filter or a relatively small drain line, may be in the range of 3 to 10 psi
  • a pressure source in the range of 15 to 20 psi may be sufficient, although higher pressures, such as those of air brake compressors, may also be used so long as such pressures are within the capacity of the valve 113.
  • the volume of air required is relatively small because the volume of air required is only that needed to make up for the air removed by entrainment in the oil. That is, the volume of air that may flow through the filter is relatively small compared to the volume of oil flowing through the separator between the inlet bore 62 and the drain opening 108.
  • the volume of air does not assist in the return flow except to make up for the entrained air and, for that reason, it is necessary to allow the float 124 to position itself where the valve 113 can close, since the failure of this valve to close at a stable point would result in an excess flow of air into the system, which would tend not only to pressurize the chamber 118, which would reduce the filter's efficiency because the oil pressure drop across the orifice 78 would be reduced and thereby reduce the reaction forces causing the rotors to spin, but also because such excess air might cause foaming or frothing of the oil in the sump, which could adversely affect the lubrication of the internal combustion engine. As shown in FIGS.
  • the invention is also applicable not only to the centrifugal separators of the permanent type, which are intended to be disassembled, cleaned, and thereafter reassembled, but also to centrifugal separators of the disposable type, such as those shown in U.S. patents Nos. 4,106,689 and 4,165,032, both of which patents are incorporated by reference herein in their entirety.
  • the centrifugal filter shown in FIGS. 2 and 3 generally conforms to that shown in the above patents except for the additional structure for admitting air into the housing and for the elimination of the air bleed valve shown in those patents, which is not required with the present invention.
  • the separator 140 includes a thin sheet metal.
  • housing shell 141 defining a shell chamber 142 and closed at the one end by a cover 143 joined to the shell 141 along a suitable seam 144.
  • a cover 143 Within the cover 143 is a rigid support disc 145, while the cover 143 also carries an annular sealing gasket 147.
  • An inlet fitting 148 is centrally mounted on the support disc 145 to engage a suitable fit ting 149 formed on the engine block 150 against which the gasket 147 seals when the separator 140 is installed in place.
  • the inlet fitting 148 also serves to support a spindle 152, the lower end of which is resiliently supported by a helical compression spring 154 abutting at the one end against the lower end of spindle 152 and at the other end against an outlet fitting 156 secured in the closed bottom end of the housing shell 141. It will be understood that the outlet fitting 156 is connected back to the sump of the engine in the usual manner.
  • a rotor 158 mounted within the shell chamber 142 is a rotor 158 having a central tube 159 rotatably journaled on bearings 160 and 161 at the upper and lower ends, respectively, of the spindle 152.
  • the rotor 158 has a shell 164 which, in combination with the rotor tube 159, forms a sealed enclosed rotor chamber 165 which, in operation, will be pressurized with respect to the shell chamber 142.
  • the rotor 158 includes a lower wall 166 adjacent the lower bearing 161 which is provided with a pair of downwardly extending, hollow projections 167 which carry the j et openings 168 to r otatably dr ive the rotor 158 within the separator as a result of the pressure admitted through the inlet fitting 148.
  • centrifugal separator described above is substanti ally the same as that disclosed in D .S. patent No. 4 ,106 , 689 , except that , as shown in FIG . 2, the housing shell 141 has a greater vertical extent and the support spring 154 is likewise l onger , to increase the space available within the housing shell 141 below the r otor 158.
  • a float arm 170 which may be made of a thin, flexible sheet material and has an end 171 secured to the inside of the housing shell 141.
  • the float arm 170 has a pair of fork arms 173 passing on each side of the spring 154 and to which is secured a hollow float 175.
  • Another inlet fitting 177 is secured in the lower wall of the housing shell 141 adjacent the float arm 171 and is provided with a valve seat end 178 within the shell chamber 142.
  • a sui table valve member 180 such as a molded piece of rubber , is secured to the float arm 170 adjacent the valve seat 178.
  • Another inlet tube 182 is connected to the fitting 177 and through a suitable check valve 183 to a source of air under pressure.
  • the valve member 180 moves off the valve seat 178 so that air is admitted into the shell chamber 172 through the fitting 177, to make up for the air which is entrained in the oil passing back to the sump.
  • the disposable type of centrifugal separator shown in the embodiment of FIGS. 2 and 3 functions in the same manner as the embodiment of FIG. 1.
  • the centrifugal filter becomes full of sediment within the rotor 158, it is simply removed and replaced with a new one by unscrewing it from the fitting 149 after disconnecting tubes from the outlet fitting 156 and the air inlet fitting 177, and after a new separator is attached to the fitting 149, these tubes are reattached in the usual manner.
  • FIG. 4 Another embodiment of a disposable centrifugal fil ter is shown in FIG. 4, which eliminates the separate connection for the outlet fitting 156 of the embodiment of FIGS. 2 and 3.
  • the separator 201 includes a housing or shell 203 which is generally cylindrical in shape and is closed by a cover 205 at the one end, secured to the shell 203 along a seam 206.
  • An outer support disc 208 is secured inside the shell 203 adjacent the cover 205, while the latter also mounts an annular gasket 209.
  • An inlet fitting 210 is mounted in the support disc 208 at the center thereof f or engagement with a fitting 212 carried on an engine block 213.
  • the block 213 also has an annular boss 214 aga inst which the gasket 209 makes sealing engagement .
  • An inlet fitting 210 is fully threaded in the fitting 212. Also provided i n the engine bl ock 213 are drain passages 216 leading to the sump of the engi ne and communicating wi th the annular space between the fitting 212 and the annular boss 214. Likewise , apertures 217 are f ormed in the outer support disc 208 , as will be explained in greater detail hereinaf ter . An inner support disc 219 is also mounted within the shell 203 a spaced distance inwardly from the outer support disc 208 and extending generally parallel thereto.
  • the inner support disc 219 makes sealing engagement with the shell 203, and also with the inlet fitting 210, to thereby define a drain chamber 220 between the two support discs, as well as the shell chamber 222 below the inner support disc 219.
  • a rotor 223 is mounted in the chamber 222 in the same manner as in the embodiment shown in FIG. 2, and since the structure is essentially the same, it has not been shown in detail in FIG. 4.
  • a support spring 225 similar to support spring 154 is mounted in the lower end of the shell 203 to abut against the rotor 223 on the upper end and against an outlet fitting 226 formed in the bottom wall 227 of the shell 203.
  • a drain tube 228 makes sealing engagement with the outlet fitting 226 on the lower side of bottom wall 227, and extends along the surface of the shell 203 upwardly toward the engine block 213, where at its upper end 229 it opens into the drain chamber 220.
  • the oil enters the filter assembly through the inlet fitting 210. passes into the rotor 223, and, on discharge through the jets, enters the shell chamber 222. The oil then flows from the outlet fitting 226 through the drain tube 228, upwardly into the drain chamber 220, where it passes through' the apertures 217 and outer support disc 208, to return to the engine through the drain passages 216.
  • a float arm 231 is mounted in the lower portion of the shell chamber 222 and carries a float 232 at the free end. At the other end of float arm 231 is mounted a valve member 234 adapted to make sealing contact against the valve seat 235 carried on air inlet fitting 237. Air is supplied by an inlet tube 239 through a check valve 240, which prevents any possible flow of oil out through the air inlet tube 239.
  • the check valve 240 positively prevents any reverse flew of oil through the air inlet line 239, and when the engine is restarted and the air supply turned on, the air will immediately enter through the inlet fitting 237 until conditions are stabilized in the- manner discussed previously.
  • Fig. 5 shows a centrifugal separator which is similar in many respects to that shown in Fig. 1
  • the centrifugal separator 310 has a lower housing member 311 and an upper housing member 312, the latter fitting into the former as shown at 313 and an O-ring seal 315 being provided to prevent escape of oil.
  • the housing members 311, 312 define a housing chamber 318 having a drain passage 319 which extends through .member 311.
  • a rotor 320 which includes a rotor cover 324 and a member 321 providing a base 322 and hollow shaft 323.
  • the rotor cover 324 has a top wall 325 and a downwardly extending peripheral sidewall 327 which fits over the base 322 with O-ring seal 331 being provided to prevent leakage of oil from the rotor.
  • the rotor top wall 325 has eight equispaced radially extending depressions, two of which are shown at 329.
  • the rotor 324 is secured in position by a nut 328 on a screw threaded upper portion of the shaft 323.
  • the rotor 320 is rotatably mounted on a fixed spindle 334 which at its lower end is screwed into a bore 335 in a cylindrical member 336 integral with and upstanding from a bridge extending across the base of the lower housing member 311. At its upper end the spindle 334 is screwthreaded and passes through an opening 337 in the upper housing member 312.
  • a cap nut 338 which is held captive by a circl ⁇ p 339 in an annular groove at its lower end with a washer 340 interposed.
  • the nut 338 holds the housing members 311, 312 together and the housing member 312 may be removed by simply unscrewing the nut 338 from the spindle 334.
  • a rod 341 may be included in the nut 338.
  • the spindle 334 has a lower journal portion 345 on which is rotatably mounted a bearing bush 347 fitted in a counter bore 348 in the shaft 323.
  • the bush 347 extends from the counterbore 348 to provide a thrust bearing.
  • the spindle also has an upper journal portion 352 on which is rotatably mounted a flanged bearing bush 354 fitted in the shaft 323.
  • a flanged bearing bush 354 fitted in the shaft 323.
  • the diameter of lower journal portion 345 is slightly greater than the diameter of upper journal portion 352 so that when the rotor 320 is fed with oil under pressure, there is a tendency for the rotor 320 to be lifted so as to reduce friction at the thrust bearing 349.
  • the flange on bush 354 serves to reduce friction if the rotor 320 rises sufficiently to abut the nut 338.
  • the spindle 334 has a bore 359 of uniform diameter therethrough which is in communication with the bore 335 in cylindrical member 336. Oil is supplied under pressure to bore 335 from a radial bore 362 in the bridge member in lower bousing member 31 1.
  • the spindle 334 has a pair of radially opposite ports 363 near its upper end through which oil flows into the circular space 364 between the spindle 334 and the shaft 323. The oil then flows from the space 364 into the rotor 320 via a pair of radially opposite ports 365 in the shaft 323.
  • a deflector cup 367 in the rotor cover 324 directs the oil towards the upper part of the rotor 320 through the spaces (not shown) between depressions 329.
  • a cylindrical perforated metal screen 371 extends coaxially with the shaft 323 and is welded at its upper end to the cup 367 and at its lower end to a conical baffle 373 such that cup 367, screen 371 and baffle 373 form a unit which can be dropped into position on rotor member 321.
  • the baffle 373 extends downwardly and outwardly to fit in an annular groove 374 In the rotor base 322.
  • the pressure of inwardly flowing oil causes oil to pass radially inward through the screen 371, below the baffle 373 and into a pair of vertical passages 376 formed within rotor base 322. At their lower ends these passages 376 terminate in tangentially extending jet orifices 378 which operate to rotate the rotor 320 as in the Fig. 1 embodiment.
  • a regulator housing 395 having a bottom wall 396 and sidewalls 397 defining a chamber 399.
  • the regulator housing 395 constitutes a mounting bracket for the separator 310 which is bolted thereto by bolts (not shown) with a gasket 403 interposed.
  • a drain opening 408 is provided in the regulator housing bottom wall 396 and to this is connected a return line to the engine sump.
  • the housing 395 also includes an air inlet 411 to which is connected an air line. Above the inlet 411 is a reduced diameter threaded bore 412 in which is mounted a tire valve 413 with a projecting stem 414.
  • a similar but inverted valve 415 is mounted in the bore 412 between the inlet 411 and the valve 413 to act as a check valve to ensure that oil does not get into the air line.
  • a float arm 421 carried by a pivot pin 422 secured in the regulator housing adjacent the valve stem 414.
  • the float arm 421 carries a hollow float 424 and at the other end 426 is arranged to depress the valve stem 414 when the oil in chamber 399 rises above a predetermined level.
  • the pin 422 is carried by a pair of angle brackets 427 screwed to the housing.
  • centrifugal separator and its associated regulator shown in Fig. 5 is substantially similar to the operation of the Fig. 1 embodiment.
  • the centrifugal separator shown in Fig. 5 will normally be mounted vertically but a slight inclination is permissible.
  • the use of a fixed spindle has been found to facilitate bearing alignment and thus permit a reliably high rotor speed.

Landscapes

  • Centrifugal Separators (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
  • Filtration Of Liquid (AREA)
  • Cyclones (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
PCT/GB1983/000009 1982-01-19 1983-01-18 Centrifugal separator WO1983002406A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE19838322870U DE8322870U1 (de) 1982-01-19 1983-01-18 Vorrichtung zum entfernen von verunreinigungen aus einer fluessigkeit durch zentrifugieren
DE8383900493T DE3363978D1 (en) 1982-01-19 1983-01-18 Centrifugal separator
AT83900493T ATE20315T1 (de) 1982-01-19 1983-01-18 Zentrifugalseparator.
BR8305198A BR8305198A (pt) 1982-01-19 1983-01-18 Metodo para ekiminar contaminantes por meio de centrifugacao;conjunto de limpador de oleo centrifugo;sistema de filtro de oleo centrifugo

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US34088482A 1982-01-19 1982-01-19
US340,884820119 1982-01-19

Publications (1)

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WO1983002406A1 true WO1983002406A1 (en) 1983-07-21

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PCT/GB1983/000009 WO1983002406A1 (en) 1982-01-19 1983-01-18 Centrifugal separator

Country Status (15)

Country Link
EP (1) EP0098866B1 (de)
JP (1) JPS58502188A (de)
AT (1) ATE20315T1 (de)
AU (1) AU555683B2 (de)
BR (1) BR8305198A (de)
CA (1) CA1188662A (de)
DD (1) DD228183A5 (de)
DE (2) DE8322870U1 (de)
ES (1) ES8501052A1 (de)
GB (1) GB2113122B (de)
HK (1) HK54786A (de)
IT (1) IT1161851B (de)
PT (1) PT76116A (de)
WO (1) WO1983002406A1 (de)
ZA (1) ZA83314B (de)

Cited By (10)

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Publication number Priority date Publication date Assignee Title
EP0254356A2 (de) * 1986-07-23 1988-01-27 Ae Plc Zentrifugalölfilter
WO1996021511A1 (en) * 1995-01-12 1996-07-18 The Glacier Metal Company Limited Fluid circulation centrifugal cleaner
WO1996023589A1 (en) * 1995-02-02 1996-08-08 The Glacier Metal Company Limited Centrifugal liquid cleaning arrangement
US6210311B1 (en) * 1998-09-25 2001-04-03 Analytical Engineering, Inc. Turbine driven centrifugal filter
US6261455B1 (en) 1998-10-21 2001-07-17 Baldwin Filters, Inc. Centrifuge cartridge for removing soot from oil in vehicle engine applications
US6428700B1 (en) 2000-09-06 2002-08-06 Baldwin Filters, Inc. Disposable centrifuge cartridge backed up by reusable cartridge casing in a centrifugal filter for removing soot from engine oil
US6517475B1 (en) 1998-09-25 2003-02-11 Baldwin Filters, Inc. Centrifugal filter for removing soot from engine oil
US6520902B1 (en) 1998-10-21 2003-02-18 Baldwin Filters, Inc. Centrifuge cartridge for removing soot from engine oil
US6579218B1 (en) 1998-09-25 2003-06-17 Analytical Engineering, Inc. Centrifugal filter utilizing a partial vacuum condition to effect reduced air drag on the centrifuge rotor
RU2511796C1 (ru) * 2012-12-26 2014-04-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Иркутская государственная сельскохозяйственная академия" Центробежный масляный фильтр двигателя внутреннего сгорания

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2160796B (en) * 1984-05-04 1987-09-16 Ae Plc Oil cleaning assemblies for engines
FR2725917B1 (fr) * 1994-10-19 1997-11-21 Moatti Filtration Ensemble de traitement d'un fluide par filtration et centrifugation
GB2314036B (en) * 1996-06-10 2000-02-02 Fram Europ Centrifugal filter
US7393317B2 (en) * 2005-04-11 2008-07-01 Cummins Filtration Ip, Inc. Centrifuge rotor-detection oil-shutoff device
DE102008013465A1 (de) * 2008-03-10 2009-09-17 Hengst Gmbh & Co.Kg Schmierölzentrifuge einer Brennkraftmaschine
US20110011795A1 (en) * 2009-07-15 2011-01-20 Hoff William D Fluid pressure driven centrifuge apparatus
CN102029086A (zh) * 2009-09-30 2011-04-27 奥凯嘉集团有限公司 一种离心式滤清器转子
KR101470837B1 (ko) * 2014-04-08 2014-12-10 신흥정공(주) 수분배출구조를 갖는 원심분리기 및 이를 이용한 퓨리파이어 시스템
GB2569167B (en) * 2017-12-08 2020-10-14 Mann & Hummel Gmbh Filter assembly having a valve movable between closed and open configurations

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FR1097316A (fr) * 1953-03-03 1955-07-04 Glacier Co Ltd Filtre centrifuge pour débarrasser les huiles lubrifiantes et les huiles combustibles de leurs impuretés dans les moteurs à combustion interne
US2983384A (en) * 1958-05-07 1961-05-09 Charles A Winslow Centrifuging and lubricant-purifying device
US3432091A (en) * 1965-09-22 1969-03-11 Glacier Metal Co Ltd Centrifugal fluid cleaners
US4046315A (en) * 1975-10-23 1977-09-06 The Weatherhead Company Centrifugal separator with discharge pump
US4106689A (en) * 1977-04-06 1978-08-15 The Weatherhead Company Disposable centrifugal separator

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS479392U (de) * 1971-02-24 1972-10-04

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1097316A (fr) * 1953-03-03 1955-07-04 Glacier Co Ltd Filtre centrifuge pour débarrasser les huiles lubrifiantes et les huiles combustibles de leurs impuretés dans les moteurs à combustion interne
US2983384A (en) * 1958-05-07 1961-05-09 Charles A Winslow Centrifuging and lubricant-purifying device
US3432091A (en) * 1965-09-22 1969-03-11 Glacier Metal Co Ltd Centrifugal fluid cleaners
US4046315A (en) * 1975-10-23 1977-09-06 The Weatherhead Company Centrifugal separator with discharge pump
US4106689A (en) * 1977-04-06 1978-08-15 The Weatherhead Company Disposable centrifugal separator

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0254356A3 (de) * 1986-07-23 1989-07-12 Ae Plc Zentrifugalölfilter
EP0254356A2 (de) * 1986-07-23 1988-01-27 Ae Plc Zentrifugalölfilter
US5904841A (en) * 1995-01-12 1999-05-18 The Glacier Metal Company Limited Fluid circulation centrifugal cleaner with pressure regulator
WO1996021511A1 (en) * 1995-01-12 1996-07-18 The Glacier Metal Company Limited Fluid circulation centrifugal cleaner
US5906733A (en) * 1995-02-02 1999-05-25 The Glacier Metal Company Limited Liquid cleaning system including back-flushing filter and centrifugal cleaner therefor
WO1996023590A1 (en) * 1995-02-02 1996-08-08 The Glacier Metal Company Limited Liquid cleaning system including back-flushing filter and centrifugal cleaner therefor
WO1996023589A1 (en) * 1995-02-02 1996-08-08 The Glacier Metal Company Limited Centrifugal liquid cleaning arrangement
US6210311B1 (en) * 1998-09-25 2001-04-03 Analytical Engineering, Inc. Turbine driven centrifugal filter
US6517475B1 (en) 1998-09-25 2003-02-11 Baldwin Filters, Inc. Centrifugal filter for removing soot from engine oil
US6579218B1 (en) 1998-09-25 2003-06-17 Analytical Engineering, Inc. Centrifugal filter utilizing a partial vacuum condition to effect reduced air drag on the centrifuge rotor
US6261455B1 (en) 1998-10-21 2001-07-17 Baldwin Filters, Inc. Centrifuge cartridge for removing soot from oil in vehicle engine applications
US6296765B1 (en) 1998-10-21 2001-10-02 Baldwin Filters, Inc. Centrifuge housing for receiving centrifuge cartridge and method for removing soot from engine oil
US6520902B1 (en) 1998-10-21 2003-02-18 Baldwin Filters, Inc. Centrifuge cartridge for removing soot from engine oil
US6428700B1 (en) 2000-09-06 2002-08-06 Baldwin Filters, Inc. Disposable centrifuge cartridge backed up by reusable cartridge casing in a centrifugal filter for removing soot from engine oil
RU2511796C1 (ru) * 2012-12-26 2014-04-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Иркутская государственная сельскохозяйственная академия" Центробежный масляный фильтр двигателя внутреннего сгорания

Also Published As

Publication number Publication date
EP0098866A1 (de) 1984-01-25
GB2113122A (en) 1983-08-03
DE8322870U1 (de) 1984-04-05
PT76116A (en) 1983-02-01
GB8301240D0 (en) 1983-02-16
JPS58502188A (ja) 1983-12-22
GB2113122B (en) 1985-07-17
DD228183A5 (de) 1985-10-09
ES519063A0 (es) 1984-11-01
IT8319179A0 (it) 1983-01-19
ES8501052A1 (es) 1984-11-01
ATE20315T1 (de) 1986-06-15
HK54786A (en) 1986-08-01
AU555683B2 (en) 1986-10-02
EP0098866B1 (de) 1986-06-11
AU1157383A (en) 1983-07-28
ZA83314B (en) 1984-05-30
CA1188662A (en) 1985-06-11
BR8305198A (pt) 1983-12-27
DE3363978D1 (en) 1986-07-17
IT1161851B (it) 1987-03-18

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