WO2014120257A1

WO2014120257A1 - Crankcase ventilation self-cleaning coalescer with intermittent rotation

Info

Publication number: WO2014120257A1
Application number: PCT/US2013/036278
Authority: WO
Inventors: Saru Dawar; Scott W. Schwartz; Brian W. Schwandt; Barry Mark Verdegan
Original assignee: Cummins Filtration Ip, Inc.
Priority date: 2013-01-29
Filing date: 2013-04-12
Publication date: 2014-08-07
Also published as: CN104937223A; CN104937223B; DE112013006531B4; DE112013006531T5

Abstract

A method and system is provided for regenerating and cleaning an air-oil coalescer of a crankcase ventilation system of an internal combustion engine generating blowby gas in a crankcase. The coalescer coalesces oil from the blowby gas. The method and system includes regenerating and cleaning the coalescer by intermittent rotation thereof.

Description

CRANKCASE VENTILATION SELF-CLEANING COALESCES*

WITH INTERMITTENT ROTATION

CROSS-REFERENCE TO RELATED APPLICATIONS jOOOIJ The present application is a continuation-in-part of U.S. Patent Application. No. 12/969,742, filed December 16, 2010, and a continuation-in-part of U.S. Patent Application No. ! 2/969,755, filed December .16, 2010. The '742 and '755 applications claim the benefit of and priority from Provisional U.S. Patent Application No. 61/298,630, filed January 27, 2010, Provisional U.S. Patent Application No. 61/298,635, filed January 27, 2010, Provisional U.S. Patent Application No. 61/359,192, filed June 28, 2010, Provisional U.S. Patent Application No. 61/383,787, filed September 17, 2010, U.S. Patent Provisional Patent Application No. 61/383,790, filed September 17, 2010, and Provisional U.S. Patent Application No. 61/383,793, filed September 17, 2010, all incorporated herein by reference.

BACKGROUND AND SUMMARY

[0002] The invention relates to internal combustion engine crankcase ventilation separators, particularly coalescers.

10003) internal combustion engine crankcase ventilation separators are known in the prior art. One type of separator uses inertial impaction air-oil separation for removing oil particles from the crankcase blowby gas or aerosol by accelerating the blowby gas stream to high velocities through nozzles or orifices and directing same against an irnpactor, causing a sharp directional change effecting the oil separation. Another type of separator uses coalescence in a coalescing filter for removing oil droplets.

[0004] The present invention arose during continuing development efforts in the latter noted air-oil separation technology, namely removal of oil from the crankcase blowby gas stream by coalescence using a coalescing filter.

BRIEF DESCRIPTION OF THE DRAWINGS

[0005] Fig. 1 is a sectional view of a coalescing filter assembly. [0006] Fia 2 is a sectional view of another coalescing filter assembly.

1»007| Fig. 3 is like Fig, 2 and shows another embodiment.

i0008j Fig. 4 is a sectional view of another coalescing filter assembly.

10009} Fig, 5 is a schematic view illustrating operation of the assembly of Fig. 4.

[0010] Fig. 6 is a schematic system diagram illustrating ait engine intake system.

[0011 J Fia. 7 is a schematic diagram illustrating a control option for the system of

Fig. 6.

[0012) Fig. 8 is a flow diagram illustrating an operational control for the system of

[0013) Fig, 9 is like Fig. 8 and shows another embodiment.

[0014) Fi«. 10 is a schematic sectional view show a coalescing filter assembly.

[0015) Fig. 1 1 is an enlarged view of a portion of Fig, if⁾.

[0016) Fig, 12 is a schematic sectional view of a coalescing filter assembly.

[0017) Fig. 13 is a schematic secti onal view of a coalescing filter assembly.

[0018] Fig. 14 is a schematic sectional view of a coalescing filter assembly.

[0019) Fig. 15 is a schematic sectional view of a coalescing filter assembly.

[0020) Fig. 1 is a schematic sectional view of a coalescing filter assembly.

[0021] Fig, 1.7 is a schematic view of a coalescing filter assembly.

[0022| Fig, 18 is a schematic sectional view of a coalescing filter assembl .

[00231 Fig. 1 is a schematic diagram illustrating a control system.

[0024) Fig. 20 is a schematic diagram illustrating a control system.

[0025) Fig. 21. is a schematic diagram illustrating a control system.

[0026] ϊ¾- 22 is a graph showing efficiency vs. particle size.

[0027) Fie. 23 shows a control system for intermittent operation.

[0028! Fig. 24 shows one form of intermittent operati on.

[0029) Fig. 25 is a graph showing restriction vs. flow. DETAILED DESCRIPTION

|0d30l Fig. 1 shows an internal combustion engine crankcase ventilation rotating coalesces' 20 separating air from oil in blowby gas 22 frorn engine crankcase 24. A coalescing filter assembly 26 includes an annular rotating coalescing filter element 28 having an inner periphery 30 defining a .hollow interior 32, and an outer periphery 34 defining an exterior 36. And inlet port 38 supplies blowby gas 22 from crankcase 24 to hollow interior 32 as shown at arrows 40. An outlet port 42 delivers cleaned separated air from the noted exterior zone 36 as shown at arrows 44. The direction of blowby gas flow is inside-out, namely radially outwardly from hollow interior 32 to exterior 36 as shown at arrows 46. Oil in the blowby gas is forced radially outwardly from inner periphery 30 by centrifugal force, to reduce clogging of the coalescing filter element 28 otherwise caused by oil sitting on inner periphery 30. This also opens more area of the coalescing filter element to flow-through, whereby to reduce restrictio and pressure drop. Centrifugal force drives oil radially outwardly from inner periphery 30 to outer periphery 34 to clear a greater volume of coalescing fil ter element 28 open to flow-through, to increase coalescing capacity. Separated oil drains from outer periphery 34. Drain port 48 communicates with exterior 36 and drains separated oil from outer periphery 34 as shown at arrow 50, which oil may then be returned to the engine crankcase as showo at arrow 52 from drain 54.

[00311 Centrifugal force pumps blowby gas from the crankcase to hollow interior 32, The pumping of blowby gas from the crankcase to hollow interior 32 increases with increasing speed of rotation of coalescing filter element 28. The increased pumping of blowby gas 22 from crankcase 24 to hollow interior 32 reduces restriction across coalescing filter element 28. In one embodiment, a set of vanes may be provided in hollow interior 32 as shown in dashed line at 56. enhancing the noted p inping. t he noted centrifugal force creates a reduced pressure zone in hollow interior 32, which reduced pressure zone sucks blowby gas 22 from crankcase 24,

£ 032| Ϊ» one embodiment, coalescing filter element 28 is driven to rotate by a mechanical coupl ing to a component of the engine, e.g. axially extending shaft 58 connected to a gear or drive pulley of the engine. In another embodiment, coaiescmg filter element 28 is driven to rotate by a fluid motor, e.g. a pelio or turbine drive wheel 60, Fig. 2, driven by pumped pressurized oi! from the engine oil pump 62 and returning same to engine crankcase sump 64. Fig, 2 uses like reference numerals from Fig. 1 where appropriate to facilitate understanding. Separated cleaned air is supplied through pressure responsive valve 66 to outlet 68 which is an alternate outlet io thai shown at 42 in Fig. I . In another embodiment, coalescing filter element 28 is driven to rotate by an electric motor 70, Fig. 3, having a drive output rotary shaft 72 coupled to shaft 58. In another embodiment coalescing filter element 28 is driven to rotate by magnetic coupling to a component of tlie engine, Figs. 4, 5. An engine driven rotating gear 74 has a plurality of magnets such as 76 spaced around the periphery thereof and magnetically coupling to a plurality of magnets 78 spaced around inner periphery 30 of the coalescing filter element such that as gear or driving wheel 74 rotates, magnets 76 move past. Fig. 5, and magnetically couple with magnets 78, to in turn rotate the coalescing filter element as a driven member, in Fig. 4, separated cleaned air flows from exterior zone 36 through channel 80 to outlet 82, which is an alternate cleaned air outlet to that shown at 42 in Fig. 1. The arrangement in Fig. 5 provides a geaiing-up effect to rotate the coalescing filter assembly at a greater rotational speed (higher angular velocity) than driving gear or wheel 74, e.g. where it is desired to provide a higher rotational speed of the coalescing filter element.

O033j Pressure drop across coalescing filter element 28 decreases with increasing rotational speed of the coalescing filter element. Oil saturation of coalescing filter element 28 decreases with increasing rotational speed of the coalescing fil ter element. Oil drains from outer periphery 34. and the amount of oil drained increases with increasing rotational speed of coalescing filter element 28. Oil particle settling velocity in coalescing filter element 28 acts in the same direction as the direction of air flow tlirough the coalescing filter element. Tlie noted same direction enhances capture and coalescence of oil particles by the coalescing filter element.

{ΌΘ34| The system provides method for separating air from oil in internal combustion engine crankcase ventilation biowby gas by introducing a G force in coalescing filter element 28 to cause increased gravitational settling in the coalescing filter element, to improve particle capture and coalescence of submicron oil particles by the coalescing filter element. The method includes providing an annular- coaiescing filter element 28, rotating the coalescing filter element, and providing inside-out flow through the rotating coaiescing filter element.

[0035] The system provides a method for reducing crankcase pressure in an interna! combustion engine crankcase generating b!owby gas. The method includes providing a crankcase ventilation system including a coalescing filter element 28 separating air from oil in the blowby gas, providing the coalescing filter element as an annular element having a hollow interior 32, supplying the blowby gas to the hollow interior, and rotating the coalescing filter element to pump blowby gas out of crankcase 24 and into hollow interior 32 due to centrifugal force forcing the blowby gas to flow radially outwardly as shown at arrows 46 through coaiescing filter element 28, which pumping effects reduced pressure in crankcase 24.

[0036] One type of internal combustion engine crankcase ventilation system provides open crankcase ventilation (QCV), wherein the cleaned air separated from the blowby gas is discharged to the atmosphere. Another type of internal combustion crankcase ventilation system involves closed crankcase ventilation (CCV), wherein the cleaned air separated from the blowby gas is returned to the engine, e.g. is returned to the combustion air intake system to be mixed with the incoming combustion air supplied to the engine.

[0037] Fig. 6 shows a closed crankcase ventilation (CCV) system 100 tor an internal combustion engine 102 generating blowby gas 104 in a crankcase 106. The system includes an air intake duct 108 supplying combustion air to the engine, and a reiura duct 1 10 having a first segment 112 supplying the blowby gas from the crankcase to air-oil coalescer 114 to clean the blowby gas by coaiescing oil therefrom and outputtmg cleaned air at output 1.16, which may be outlet 42 of Fig. 1, 68 of Fig. 2, 82 of Fig. 4. Return duct 1 10 includes a second segment 118 supplying the cleaned air from coalescer 1.14 to air intake duct iOS to join the combustion air being supplied to the engine, Coalescer 1 14 is variably controlled according to a given condition of the engine, to be described,

[0038] Coalescer 1 14 has a variable efficiency variably controlled according to a given condition of the engine. I one embodiment, coalescer 1 14 is a. rotating coalescer, as above, and the speed of rotation of the coaiescer is varied according to the given condition of the engine. In one embodiment, the give condition is engine speed. In one embodiment, the coaiescer is driven to rotate by an electric motor, e.g. 70, Fig. 3. In one embodiment, the electric motor is a variable speed electric motor to vary the speed of rotation of the coaiescer. in another embodiment, the coaiescer is hydraulicaiiy driven to rotate, e.g. Fig. 2. in one embodiment, the speed of rotation of the coalescer is hydraulic-ally varied. In this embodiment, the engine oil pump 62, Figs. 2, 7, supplies pressurized oil through a plurality of parallel shut-off valves such as 120, 122, 124 which are controlled betwee closed and open or partially open states by the electronic control module (ECM) 126 of the engine, tor flow through respective parallel orifices or nozzles 128, 130, 132 to controilably increase or decrease the amount of pressurized oil supplied against peitors or turbine wheel 60. to in turn controilably vary the speed of rotation of shaft 58 and coalescing filter element 28.

(0039] In one embodiment, a turboeharger system 140, Fig. 6. is provided for the internal combustion 102 generating blowby gas 104 in craakcase 106. The system includes the noted air intake duct 108 having a first segment 142 supplying combustion air to a turboeharger 144, and a second segment 146 supplying mrbocharged combustion air from turboeharger 144 to engine 1 2. Return duct 1 10 has the noted first segment 1.1.2 supplying the blowby gas 104 from, crahkease 106 to air-oil coalescer 1 14 to clean the blowby gas by coalescing oil therefrom and outputting cleaned air at 116. The return duct has the noted second segment 1 18 supplying cleaned air from coalescer 1 .14 to first segment 142 of air intake duct 108 to join combustion air supplied to turboeharger 144. Coalescer 1 14 is variably controlled according to a given condition of at least one of turboeharger 144 and engine 102. In. one embodiment, the gi ven condition is a condition of the turboeharger. In a further embodiment, the coalescer is a rotating coaiescer, as above, and the speed of rotation of the coalescer is varied according to turboeharger efficiency. I a further embodiment, the speed of rotation of the coalescer is varied according to turboeharger boost pressure. In a further embodiment, the speed of rotation of the coalescer is varied according to turboeharger boost ratio, which is the ratio of pressure at the turboeharger outlet, versus pressure at the turboeharger inlet, fa a furthe embodiment, the coalescer is driven to rotate by an electric motor, e.g. 70, Fig. 3. hi a further embodiment, the electric motor is a variable speed electric motor to vary the speed of rotation of the coalescer. in another embodiment, the coalescer is hydraultcally driven to rotate, Fig. 2. In a further embodiment, the speed of rotation of the coalescer is Irydraulieally varied. Fig. 7.

[0040] The system provides a method for improving turbocharger efficiency in a turbocharger system 140 for an internal combustion engine 102 generating blowby gas 104 in a crankcase 106, the system having an air intake duct 108 having a first segment 142 supplying combustion air to a turbocharger 144, and a second segment 146 supplying tnrbocharged combustion air from the turbocharger 144 to the engrae 102, and having a return duct 110 having a first segment 1 12 supplying the blowby gas 104 to air-oil coalescer 1 1.4 to clean the blowby uas by coalescins oil theref om and outputtmu cleaned air at 1 16. the return duct bavins a second segment 1.1.8 supplying the cleaned air f om the coalescer 1.14 to the first segment 1.42 of the air intake duct to join combustion air supplied to turbocharger 1 4, The method includes variably controlling coalescer 114 according to a given condition of at least one of turbocharger 1 4 and engine 102. One embodiment variably controls coalescer 1 14 according to a gi ven condition of turbocharger 144. A further embodiment provides the coalescer as a rotating coalescer, as above, and varies the speed of rotation of the coalescer according to turbocharger efficiency. A further method varies the speed of rotation of coalescer 1 14 according to turbocharger boost pressure. A further embodiment varies the speed of rotation of coalescer 114 according to turbocharger boost ratio, which is the ratio of pressure at the turbocharger outlet versus pressure at. the turbocharger inlet.

{00411 Fig. 8 shows a control scheme for CCV implementation. At step 160, turbocharger efficiency is monitored, and if the turbo efficiency is ok as determined at step 1 2, then rotor speed of the coalescing filter element is reduced at step 164. If the turbocharger efficiency is not ok, then engine duty cycle is checked at step 166, and if the engine duty cycle is severe then rotor speed is increased at step 168, and if engine duty cycle is not severe then no action is taken at step 1 0.

[00421 Fi . 9 shows a control scheme for OCV implementation. Crankcase pressure is monitored at step 172, and if it is ok as determined at step 174 then rotor speed is reduced at step 1 76_; and if not ok then ambient temperature is checked at step 78 and if less than 0° C, then at step 180 rotor speed is increased to a maximum to increase warm gas pumping and increase otl-water slinging. If ambient temperature is not less than 0° C, then engine idling is checked at step 182, and if the engine is idling then at step 184 rotor speed is increased and maintained, and if the engine is not idling, then at step 186 rotor speed is increased to a maximum for five minutes.

{0043J The flow path through the coalescing filter assembly is from upstream to downstream, e.g. in Fig. 1 from inlet port 38 to outlet port 42, e.g. in Fig. 2 from inlet port 38 to outlet port 68, e.g. in Fig. 10 from inlet port 1 0 to outlet port 1 2. There is further provided in Fig. 10 in combination a rotary cone stack separator 1 4 located in the flow path and separating air from oil in the blowby gas. Cone stack separators are known in the prior art. The direction of blowby gas flow through the rotating cone stack separator is inside-out, as shown at arrows 196, Figs. 1 - 12. Rotating cone stack separator 194 is upstream of rotating coalescer filter element 198. Rotating cone stack separator 194 is in hollow interior 200 of rotating coalescer filter element 1 8. In Fig. 12, an annular shroud 202 is provided in hollow interior 200 and is located radially between rotating cone stack separator 1 4 and rotating coalescer filter element 198 such that shroud 202 is downstream of rotating cone stack separator 1 4 and upstream of rotating coalescer filter element 198 and such that shroud 202 provides a collection and drain surface 204 along which separated oi l drains after separation by the rotating cone stack separator, which oil drains as shown at droplet 206 through drain hole 208, which oil then joins the oil separated by coalescer 198 as shown at 210 and drains through, main drain 212.

[0044] Fig. 13 shows a further embodiment and uses like reference numerals from above where appropriate to facilitate understanding. Rotating cone stack separator 214 is downstream of rotating coalescer filter element 1 8. T he directi on of flow through rotating cone stack separator 214 is inside-out. Rotating cone stack separator 214 is located radially outwardly of and circumscribes rotating coalescer filter element 1 8.

[0045J Fig, 14 shows another embodiment and uses like reference numerals from above where appropriate to facilitate undemanding. Rotating cone stack separator 216 is downstream of rotating coalescer filter element 1 8, The direction of flow through rotating cone stack separator 216 is outside-in, a shown at arrows 218. Rotating coalescer filter element 1.98 and rotating cone stack separator 216 rotate about a common axis 220 and are axialiy adjacent each other. Blowby gas flows radially outwardly through rotating coalescer filter element 1 8 as shown at arrows 222 then axialiy as shown at arrows 224 to rotating cone stack separator 2 6 then radially inwardly as shown at arrows 218 through rotating cone stack separator 216.

100 6] Fig. 15 shows another embodiment and uses like reference numerals from above where appropriate to facilitate understanding. A second annular rotating coaiescer filter element 230 is provided in the noted flow path from inlet 190 to outlet 1 2 and separates air from oil in the blowby gas. The direction of flow through second rotating coalescer filter element 230 is outside-in as shown at arrow 232. Second rotating coalescer filter element 230 is downstream of first rotating coalescer element 198. First and second rotating coaiescer filter elements 198 and 230 rotate about a common axis 234 and are axialiy adjacent each other. Blowb gas flows radially outwardly as shown at arrow 222 through first rotating coaiescer filter element 198 then axialiy as shown at arrow 236 to second rotating coaiescer filter element 230 then radially inwardly as shown at arrow 232 through second rotating coalescer filter element 230.

[0047] In various embodiments, the rotating cone stack separator may be perforated with a plurality of drain holes, e.g. 238, Fig. 13, allowing drainage therethrough of separated oil.

(00481 Fig. 16 shows another embodiment and uses like reference numerals from above where appropriate to facilitate understanding. An annular shroud 240 is provided along the exterior 242 of rotating coalescer filter element 198 and radially outwardly thereof and downstream thereof such thai shroud 240 provides a collection and drain surface 244 along which separated oil drains as shown at droplets 246 after coalescence by rotating coaiescer filter element 1 8. Shroud 240 is a rotating shroud and may be part of the filter frame or end cap 248. Shroud 240 circumscribes rotating coalescer filter element 1 8 and rotates about a common axis 250 therewith. Shroud 240 is conical and tapers along a conical tape relative to the noted axis. Shroud 240 has an inner surface at 244 radially facing rotating coaiescer filter element 1 8 and spaced therefrom by a radial gap 252 which increases as the shroud extends axially downwardly and along the noted conical taper. Inner surface 244 may have ribs such as 254, Fig, 17, circumferentiaHy spaced therearound and extending axiaJly and along the noted conical taper and facing rotating coaiescer filter element 1 8 and providing channeled drain paths such as 256 therealong guiding and draining separated oil flow therealong. Inner surface 244 extends axially downwardly along the noted conical taper from a first upper axial end 258 to a second lower axial end 260. Second axial end 260 is radially spaced from rotating coalesce!" filter element 198 by a radial gap greater than the radial spacing of first axial end 258 from rotating coaiescer filter element 198. In a further embodiment, second axial end 260 has a scalloped lower edge 262, also focusing and euidins; oil drainage.

{0049] Fig. 18 shows a further embodiment and uses like reference numerals from above where appropriate to facilitate understanding. In lieu of lower inlet 190. Figs. 13-15, an. upper inlet port 270 is provided, and a pair of possible or alternate outlet ports are shown at 272 and 274. Oil drainage throug drain 212 may be provided through a one-way check valve such as 276 to drain hose 278, for return to the engine crankcase, as above.

{OOSOJ As above noted, the coaiescer can be variably controlled according to a given condition., which may be a given condition of at least one of the engine, the turbocharger, and the coaiescer. In one embodiment, the noted given conditio is a give condition of the engine, as above noted. In another embodiment, d e given condition is a given condition of the turbocharger, as above noted. In another embodiment, the given condition is a given condition of the coaiescer. in a version of this embodiment, the noted given condition is pressure drop across the coaiescer. In a version of this embodiment, the coaiescer is a rotating coaiescer, as above, and is driven at higher rotational speed when pressure drop across the coaiescer is above a predetermined threshold, to prevent a cumulati n of oil on die coaiescer, e.g. along the inner periphery thereof in the noted hollow interior, and to lower the noted pressure drop. Fig, 19 shows a control scheme wherein the pressure drop, dP, across the rotating coaiescer is sensed, and monitored by the EC (engine control module), at step 290, and then it is determined at step 292 whether dP is above a certain value at lo engine RPM, and if not, then rotational speed of the coalescer is kept the same at step 294, and if dP is above a certain value then the coalescer is rotated at a higher speed at step 296 until dP drops down to a certain point. The noted given condition is pressure drop across the coalescer, and the noted predetermined threshold is a predetermined pressure drop threshold.

|0051J In a further embodiment, the coalescer is an intermittently rotating coalescer having two modes of operation, and is in a first stationary mode when a given condition is below a predetermined threshold, and is in a second rotating mode when the given condition is above the predetermined threshold, with hysteresis if desired. The first stationary mode provides energy efficiency and reductio of parasitic energy loss. The second rotating mode provides enhanced separation efficiency removing oil from the air in the hlowby gas. In one embodiment, the given condition is engine speed, and the predetermined threshold is a predetermined engine speed threshold. ^'In another embodiment, the given condition is pressure drop across the coalescer, and the predetermined threshold is a predetennined pressure drop threshold, in another embodiment, the given condition is turbocharger efficiency, and the predetermined threshold is a predetermined turbocharger efficiency threshold. In a further version, the given condition is turbocharger boost pressure, and the predetermined threshold is a predetermined turbocharger boost pressure threshold, in a further version, the given condition is turbocharger boost ratio, and the predetermined threshold is a predetermined turbocharger boost ratio threshold, where, as above noted, turbocharger boost ratio is the ratio of pressure at the turbocharger outlet vs. pressure at the turbocharger inlet. Fig. 20 shows a control scheme for an electrical version wherein engine RPM or coalescer pressure drop is sensed at step 298 and monitored by the ECM at step 300 and then at step 302 if the RPM or pressure is above a threshold then rotation of the coalescer is initiated at step 304, and if the RPM or pressure is not above the threshold then the coalescer is left in the stationary mode at step 306. Fig. 21 shows a mechanical version and uses like reference numerals from above where appropriate to facilitate understanding. A check val ve, spring or other mechanical component at step 308 senses RPM or pressure and the decision process is carried out. at steps 302, 304, 306 as above. [00S2| The noted method for improving turbocharger efficiency includes variably controlling the coalescer according to a given condition of at least one of the turbocharger, the engine, and the coalescer. One embodiment variably controls the coalescer according to a given condition of the turbocharger, h one version, the coalescer is provided as a .rotating coalescer, and the method includes varying the speed of rotation of the coalescer according to turbocharger efficiency, and in another embodiment according to turbocharger boost pressure, and in another embodiment according to turbocharger boost ratio, as above noted. A further embodiment variably controls the coalescer according to a given condition of the engine, and in a further embodiment according to engine speed. In a further version, the coalescer is provided as a rotating coalescer, and the method involves varying the speed of rotation of the coalescer according to engine speed. A further embodiment: variably controls die coalescer according to a given condiiion of the coalescer, and in a. further version according to pressure drop across the coalescer. in a further version, the coalescer is provided as a rotating coalescer, and the method involves varying the speed of rotation of the coalescer according to pressure drop across the coalescer. A further embodiment involves intermittently rotating the coalescer to have two modes of operation including a first stationary mode and a second rotating mode, as above.

{0053] A method is provided for regenerating and. cleaning the air-oil coalescer 28, 1 14, 198 of a crankcase ventilation system of an internal combustion engine 102 generating b! wby gas 22, 104 in a crankcase 24, 106. The coalescer coalesces oil from the bio why gas. The method includes regenerating and cleaning the coalescer by intermittent rotation thereof. f 0O54| Fig. 22 shows fractional efficiency vs. particle size. At particle size greater than about 1.5μ, efficiency is roughly the same, e.g. 100%, whether the coalescer filter is rotated or not. As particle size decreases, efficiency drops, particularly for lower RPM (revolutions per minute).

1 0551 Fig. 23 shows a control system including a pressure drop (dP) sensor or regulator 320 sensing pressure drop across the coalescer and sending a signal to the ECM 322 (engine control module) which in turn outputs a signal to a frequency generator or rotating unit 324 to rotate the coalescer when pressure drop across the latter rises above a given threshold. Fig. 24 illustrates intermittent operation wherein the coalescer is stationary at 326 and the pressure drop thereacross increases. When the pressure drop reaches a given threshold such as 328, the coalescer is rotated, and the pressure drop thereacross decreases as shown at 330, When the pressure dro reaches a lower threshold such as 332, the rotation is stopped. The pressure drop then begins increasing again at 334, and the cycle repeats. The coalescer is stationary during intervals such as 326, 334. during which pressure drop thereacross increases. The coalescer spins during intervals such as 330, during which the pressure drop thereacross decreases due to the cleaning and regenerating thereof, as the coalescer becomes unsaturated. Fig, 25 shows restriction levels of the same coalescer element after a series of static and rotating modes. The first bar indicates the restrictio after 2000 hours of operation in a static mode. otaiitm the coalescer reduces the restriction from bar 1 to bar 2, whereafter the rotation is stopped and the restriction increases from bar 2 to bar 3, whereafter the coalescer element is again rotated and the restriction decreases from bar 3 to bar 4. Various other intermittent operational patterns may be followed.

[0056] Regeneration of the coalescer by intermittent rotation retains high efficienc and clean coalescing filter media and low pressure dro for die life of the coalescer. The high efficiency is produced by efficiently draining the liquid from the filter media with intermittent rotation. Static coalescers have a finite life and must be serviced and replaced. Rotating coalescers, on the other hand, provide higher efficiency at a Sower pressure drop than static coalescers and can potentially last the life of the engine, but require energy input to cause or drive the rotation, and may be more complex and costly from a first fit point of view. Customers are increasingly demanding a crankcase ventilation separa tor system thai will last the life of the engine, provide high oil mist removal efficiency with low restriction, and with minimal to no parasitic energy loss from the engine. The coalescer fibrous media saturates with contaminants such as soot and oil in the engine crankcase ventilation blowby gas, reducing the lite of the coalescer filter element. Fibrous polymer media traps the oil within the fiber matrix, and the butld-up of trapped oil ultimately results in a saturated coalescer element condition which raises the crankcase pressure to the point where the coalescer element needs to be changed. Intermittent rotation extends coaleseer filter life and reduces parasitic energy loss otherwise needed to accomplish continuous rotation.

)0057| The present method regenerates and cleans the coaleseer by applying centrifugal force thereto by intermittent rotation thereof, In one embodiment, the intermittent rotation is controlled according to a given parameter, In one embodiment, the given parameter is a condition of the coaleseer. In one embodiment, the given parameter is a condition, of the engine, hi one embodiment, the given parameter is crankcase pressure of the engine. In one embodiment, the given parameter is operational service time of the engine. In one embodiment the give parameter is mileage of a vehicle driven by the engine.

(0058) In one embodiment, the method includes regenerating and cleaning the coaleseer by intemiirtent operatio diiven by a rotary shaft In one embodiment, the rotary shah is driven by the engine. In one embodiment, the method includes regenerating and cleaning the coaleseer by intermittent rotation driven by an electric motor. In one embodiment, the method includes regenerating and cleaning the coaleseer by intermittent rotation driven by a hydraulic motor, hi one embodiment, the method includes regenerating and cleaning the coaleseer by intermittent rotation driven by pressurized engine oil. In one embodiment, the method includes regenerating and cleaning the coaleseer by intermittent rotation driven by pressurized engine oil driving a peiton iurbine. In one embodiment, the engine has an oil pump pumping lubricating oil to components of the engine, and the method includes regenerating and clean ing the coaleseer by intermittent rotation driven by pumped oil from the oii pump. In one embodiment, the oii pump has a relief valve returning excess oil to a sump to protec t against overpressure, and the method Includes regenerating and cleaning the coaleseer by intermittent rotation driven by excess oil from the relief valve,

(0059) In one embodiment, the method includes regenerating and cleaning the coaleseer by intermittent rotation commanded when to spin and when not to spin, i one embodiment, the method includes regenerating and cleaning the coaleseer by intermittent rotation at a commanded frequency having a plurality of cycles, each cycle havi ng an off interval during which the coaleseer is stationary and nonrotatecl, and an on interval during which the coalescer is rotated. In one embodiment, at least one of a) the commanded frequency, b) the duty cycle of the commanded frequency between the off and on intervals, and c) the speed of rotation during the on interval, is controlled according to a given parameter. In one embodiment, during the on interval the method includes pulsing the rotation of the coalescer to provide pulsed rotation thereof, including a plurality of centrifugal force impulses thereto during rotation during the on interval, in one embodiment, during the on interval, the method includes pulsing the rotation of the coalescer to provide a plurality of accelerational bursts during rotation thereof, in one embodiment, the method includes regenerating and cleaning the coalescer by intermittent rotation while the coalescer is mounted to the engine.

O06O| In one embodiment, the noted given parameter or trigger for rotation is excess oil flow from the noted relief valve of the oil pump. In this embodiment, rotation, of the coalescer takes place only when the system oil pressure reaches a higher or excess level above that needed to lubricate engine components, and thus the coalescer rotational system would not "steal" oil fr m the lube system otherwise needed at lower engine RPMs or system pressures. In another embodiment, the parameter or trigger for coalescer rotation is crankcase pressure, hi one embodiment, the coalescer element is integrated with a pressure sensor on a rotating drive-shaft, with the sensor sensing pressure drop across the coalescer media.

10061! In the foregoing description, certain terms have been used for brevity, clarity, and understanding. No unnecessary limitations are to be inferred therefrom beyond the requirement of the prior art because such terras are used for descriptive purposes and are intended to be broadly construed. The different configurations, systems, and method steps described herein may be used alone or in combination with other configurations, systems and method steps. It is to be expected that various equivalents, alternatives and modifications are possible within the scope of the appended claims. Each limitation in the appended claims is intended to invoke interpretation under 35 II.S.C. §1 12, sixth paragraph, only if the terms "means for" or "step tor" are explicitly recited in the respective limitation.

Claims

What is claimed is:

1. A method for regenerating and cleaning an air-oil coalescer of a crankcase ventilation system of an internal combustion engine generating blowby gas in a crankcase, said coalescer coalescing oil from said blowby gas, said method comprising regenerating and cleaning said coalescer by intermittent rotation thereof

2. The method according to claim 1 comprising regenerati g and cleaning said coalescer by applying centri ugal force thereto by said intermittent rotation thereof

3. The method accordmg to claim 2 comprising controlling said intermittent rotation according to a given parameter.

4. The method according to claim 3 comprising providing said given parameter as a condition of said coalescer.

5. The method according to claim 3 comprising providing said given parameter as a condition of said engine.

6. The method according to claim 3 wherein said given parameter is pressure dro across said coalescer.

7. The method according to claim 3 wherein said given parameter is crankcase pressure of said engine.

8. The method according to claim 3 wherein said given, parameter is operational service time of said engine,

9. The method accordmg to claim 3 wherein said given parameter is mileage of vehicle driven by said engine.

10. The method according to claim 2 comprising regenerating and cleaning said coalescer by intermittent rotation driven by a rotary shaft,

11. T he method according to claim 10 wherein said rotary shaft is driven by said engine,

12. The method according to claim 2 composing regenerating and cleaning said coalescer by intermittent rotation driven by an electric motor.

13. The method according to claim 2 comprising regenerating and cleaning said coalescer by intermittent rotation driven by a hydraulic motor.

14. The method according to claim 2 comprising regenerating and cleaning said coalescer by intermittent rotation driven by pressurized engine oil

15. The method according to claim 2 comprising regenerating and cleaning said coalescer by intermittent rotation driven by pressurized engine oil driving a pelto turbine,

16 The method according to claim 14 wherein said engine has an oil pump pumping lubricating oil to components of said engine, and comprising regenerating and cleaning said coalescer by intermittent rotation driven by pumped oil from said oi! pump.

17 The method according to claim 2 wherein said engine has an oil pump pumping lubricating oil to components of said engine and having a relief valve returning excess oil to a sump to protect against overpressure, and comprising regenerating and cleaning said coalescer by intermittent rotation driven b excess oil flow from said relief valve,

18. The method according to claim 2 comprising regenerating and cleaning said coalescer by iniermitteni rotation commanded when to spin and when not to spin. 1 The method according to claim 2 comprising regenerating and cleaning said coaiescer by intermittent rotation at a commanded frequency having a plurality of cycles, each cycle having an off interval during which said coaiescer is stationary and nonrotated, and an on interval during which said coaiescer is rotated,

20. The method according to claim 19 wherein at least one of a) said commanded frequency, b ) the duty cycle of said commanded frequency between said off and on intervals, and c) the speed of rotation during said on interval , is controlled according to a given parameter,

21. The method according to claim 19 comprising during said on interval, pulsing the rotation of said coaiescer to provide pulsed rotation thereof including a plurality of centrifugal force impulses thereto during rotation during said on interval.

22. The method according to claim 19 comprising during said on interval, pulsing the rotation of said coaiescer to provide a plurality of accelerational bursts during pulsed rotaijon thereof.

23. The method according to claim 2 comprising regenerating and cleaning said coaiescer by intermittent rotation while said coaiescer is mounted to said engine.

24. A system for regenerating and cleaning an air-oil coaiescer of a craiikcase ventilation system of an. internal combustion engine generating blowby gas in a c ankcase, said coaiescer coalescing oil from said blowby gas, said system regenerating and cleaning said coaiescer by intermittent rotation thereof

25. The system according to claim. 24 wherein said intermittent rotation is controlled according to a given parameter selected from the group consisting of; a condition of said coaiescer; a condition of said engine; pressure drop across said coaiescer; crankcase pressure of said engine; operational sen-ice time of said engine; mileage of a vehicle driven by said engine.

26. The system according to claim 24 wherein said intermittent rotatio is driven by a source selected from the group consisting of: a rotary shaft; a rotary shaft dri ven b said engine; an electric motor; a hydraulic motor; pressurized engine oil.

27. The system according to claim 24 wherein said engine has an oil pump pumping lubricating oil to components of said engine and having a relief valve returning excess oil to a sump to protect against overpressure, and wherein said system regenerates and cleans said coaiescer by .intermittent rotation drive by excess oil flow from said relief valve.

28. The system according to claim 24 wherein said coaiescer is regenerated and cleaned by intermittent rotation commanded when to spin and when not to spin.

29. The system according to claim 24 wherein said coaiescer is regenerated and cleaned by intermittent rotation at a commanded frequency having a plurality of cycles, each cycle having an off interval during which said coaiescer is stationary and non-rotated, and an on interval during which said coaiescer is rotated.

30. The system according to claim 29 wherein at least one of a) said commanded frequency; b) the duty cycle of said commanded frequency between said off and on intervals, and c) the speed of rotation during said on interval, is controlled according to a given parameter. ! . The system according to claim 2 wherein during said on interval, said- system pulses the rotation of said coaiescer to provide pulsed rotation thereof, including a plurality of centrifugal force impulses during rotation during said on interval.

32. The system according to claim 29 wherein during said on interval, said system pulses the rotation of said coaiescer to provide a pl urality of acceleraiional bursts during rotation thereof

33. The system according to claim 24 wherein said coalescer is regenerated and cleaned by Intermittent rotation while said coalescer is mounted to said engine.