Control system for deactivation of valves in an internal combustion engine

Information

  • Patent Grant
  • 6439176
  • Patent Number
    6,439,176
  • Date Filed
    Monday, March 5, 2001
    23 years ago
  • Date Issued
    Tuesday, August 27, 2002
    22 years ago
Abstract
A hydraulic control system for controllably directing pressurized engine oil to deactivation valve lifters to activate or deactivate the associated engine intake and exhaust valves. Passages to the lifters are controllably opened or closed by a solenoid control valve responsive to signals from a computerized engine control system. Preferably, the hydraulic control system includes a top plate having a first pattern of channels and bores formed in its underside, and a bottom plate having a second such pattern formed in its upper surface. The top and bottom plates are joined to form a hydraulic distribution manifold mounted on the engine. In a presently preferred embodiment, a gasket plate having bores and patterns of resilient gasketing material is provided between the top and bottom plates to simplify fabrication of the top and bottom plates. Solenoid control valves disposed on the bottom plate extend into the manifold to open and close respective control passages to the deactivation valve lifters upon command. A dual-purpose lead frame retainer/connector retains the control valves in the bottom plate and provides electrical connection to each control valve.
Description




TECHNICAL FIELD




The present invention relates to internal combustion engines; more particularly, to devices for controlling systems in an internal combustion engine; and most particularly, to a hydraulic control means for controlling the activation and deactivation of valve lifters in an internal combustion engine to engage and disengage selected cylinders from participating in the combustion of such an engine.




BACKGROUND OF THE INVENTION




Internal combustion engines are well known. Such an engine may include a plurality of combustion cylinders, each containing a reciprocable piston connected to a common crankshaft by a connecting rod. In so-called four-stroke or four-cycle engines, each cylinder is provided with one or more intake valves for admitting fuel/air mixture to the cylinder and one or more exhaust valves for exhausting burned mixture from the cylinder. A sparking plug extending into each cylinder ignites the compressed fuel/air mixture at a predetermined time relative to the rotary position of the crankshaft. Typically, the intake valves are actuated by an intake camshaft operatively connected to the crankshaft and having a plurality of cam lobes radially disposed at varying predetermined angles to cause the intake valves to open and close at the proper preselected times during rotation of the crankshaft. The exhaust valves are similarly controlled by an exhaust camshaft. In some engines, the intake and exhaust cam lobes are provided on a single, common camshaft. In an overhead valve engine, the valves may be actuated directly by camshafts disposed on the head itself, or the camshaft(s) may be disposed within the engine block and may actuate the valves via a valve train including valve lifters, pushrods, and rocker arms. In V-style engines, alternate cylinders are disposed at an included central angle from the crankshaft bearing axis such that even-number cylinders are grouped into a first cylinder bank and odd-number cylinders are grouped into a second cylinder bank. A single camshaft disposed within the engine block may actuate all the valves in both cylinder banks. The longitudinal depression between the banks of a V-style engine, and below the intake manifold, is known in the art as the engine “valley.”




In most prior art four-stroke internal combustion engines, the mutual relationships of the crankshaft, camshaft, and valves are mechanically fixed; that is, the valves are opened and closed fully and identically with every two revolutions of the crankshaft, fuel/air mixture is drawn into each cylinder in a predetermined sequence, ignited by the sparking plug, and the burned residue discharged. This sequence occurs irrespective of the rotational speed of the engine or the load being placed on the engine at any given time.




It is known that for much of the operating life of a multiple-cylinder engine, the load might be met by a functionally smaller engine having fewer firing cylinders, and that at low-demand times fuel efficiency could be improved if one or more cylinders of a larger engine could be withdrawn from firing service. It is known in the art to accomplish this by de-activating the valve train leading to preselected cylinders in any of various ways, such as by providing special valve lifters having internal locks which may be switched on and off either electrically or hydraulically.




It is a principal object of the present invention to provide an improved electric/hydraulic system for controlling the hydraulic locking and unlocking of deactivatable valve lifters in an internal combustion engine.




It is a further object of the invention to provide such a system wherein trapped air is automatically purged immediately upon engine startup and is prevented from re-entry during engine operation.




It is a still further object of the invention to provide such a system comprising a minimum number of components which then may be easilyfabricated.




It is a still further object of the invention to provide such a system which can reliably activate or deactivate selected valves within the time required for one revolution of an engine's camshaft.




SUMMARY OF THE INVENTION




Briefly described, a hydraulic control system in accordance with the invention includes a hydraulic manifold assembly for controllably directing or withholding engine oil, provided under pressure by the engine oil pump, to an engine's deactivation valve lifters to activate or deactivate the associated engine intake and exhaust valves. The assembly may be conveniently disposed, for example, in the valley of a V-style engine beneath the intake manifold. Passages to the valve lifters are controllably opened or closed by an electric solenoid activation control valve, such control valves being responsive to signals from a computerized engine control system. Preferably, the hydraulic manifold assembly comprises a top plate having a first pattern of channels formed in the underside thereof, and a bottom plate having a second such pattern formed in the upper surface thereof, such that when the top and bottom plates are matably joined the appropriate manifold is formed. In a presently preferred embodiment, a gasket plate having a pattern of bores therethrough and different patterns of resilient gasketing material around the bores applied to the upper and lower surfaces of the plate, is provided between the top and bottom plates to simplify fabrication of the top and bottom plates. Alternatively, the resilient gasketing material may be applied in appropriate patterns directly to the top and bottom plates. Solenoid control valves are disposed on the underside of the bottom plate and extend therethrough into the manifold to open and close their respective control passages in the manifold upon command. A dual-purpose lead frame retainer/connector both retains the control valves in the bottom plate and provides electrical connection to each control valve.











BRIEF DESCRIPTION OF THE DRAWINGS




These and other features and advantages of the invention will be more fully understood and appreciated from the following description of certain exemplary embodiments of the invention taken together with the accompanying drawings, in which:





FIG. 1

is a schematic drawing of an oil system for an internal combustion engine showing the relationship of a valve deactivation control system in accordance with the invention to a prior art pressurized oil system;





FIG. 2

is an exploded isometric view from above of a first embodiment of a hydraulic manifold assembly in accordance with the invention;





FIG. 2



a


is an assembled isometric view of the exploded components shown in

FIG. 2

;





FIG. 3

is an isometric view from below of the assembly shown in

FIG. 2



a;







FIG. 4

is an isometric view from above of a gasket plate for use in the hydraulic manifold assembly shown in

FIGS. 2



a


and


3


;





FIG. 5

is an isometric view from below of the gasket plate shown in

FIG. 4

;





FIG. 6

is a plan view from above of the assembly shown in

FIGS. 2



a


and


3


;





FIG. 7

is a plan view from below of the assembly shown in

FIG. 6

;





FIG. 8

is a cross-sectional view of the assembly shown in

FIG. 6

, taken along line


8





8


, the control valves and connector/retainer being omitted for clarity;





FIG. 9

is a cross-sectional view of the assembly shown in

FIG. 6

taken along line


9





9


;





FIG. 10

is an exploded isometric view from above of the electrical connector portion of the lead frame connector/retainer shown in

FIG. 3

;





FIG. 11

is an assembled isometric view of the connector/retainer shown in

FIG. 10

;





FIG. 12

is a plan view of the connector/retainer shown in

FIG. 3

, showing the location of electrical leads embedded therein;





FIG. 13

is a side elevational view of the connector/retainer shown in

FIGS. 3 and 12

; and





FIG. 14

is an isometric view from above of the connector/retainer shown in FIGS.


12


and


13


.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




Referring to

FIG. 1

, the engine oil circuits for an internal combustion engine are provided with a valve deactivation control circuit in accordance with the invention. While only a single control valve and lifter are shown in the schematic drawing, it should be understood that valve deactivation is useful only in multiple-cylinder engines for selectively reducing the number of combusting cylinders. Multiple-cylinder embodiments are discussed below. In

FIG. 1

, an oil pump


10


feeds oil from sump


12


to a juncture


14


where the flow is split three ways. A first portion


16


provides conventional general lubrication to the engine. A second portion


18


provides oil conventionally to the hydraulic valve lifters


20


, which are also valve deactivation lifters. A third portion


22


provides oil to a valve deactivation control system


24


. An optional pressure relief valve


26


is openable to the sump to maintain pressure in system


24


at a predetermined maximum level. Oil is filtered by strainer


28


and then is supplied to a solenoid control valve


30


wherein it is either diverted to the sump


12


if the control valve


30


is not energized, or is diverted to deactivation lifter


20


if the control valve


30


is energized, to cause the associated engine intake and exhaust valves to be deactivated. An engine control module (ECM)


32


, preferably mounted on other than the engine, receives input signals


33


from a pressure transducer


34


in the control system


24


and integrates via an algorithm such signals with other input operating data such as oil temperature and engine speed to provide output signals


36


to energize or deenergize solenoid control valve


30


.




Referring to

FIGS. 2 through 9

, a first and currently preferred embodiment


38


of a valve deactivation hydraulic control circuit in accordance with the invention includes a top plate


40


, a bottom plate


42


, and a gasket plate


44


sandwiched between the top and bottom plates. The three plates are held together by bolts


46


to form a complex oil distribution manifold as described below. When assembled, circuit


38


may be conveniently installed into an internal combustion engine, for example, via bolts


48


extending through bores in top plate


40


and gasket plate


44


and being secured, for example, onto engine block towers provided along opposite sides of the valley of a V-style engine (not shown) for operative control of the deactivation lifters of the engine.




A first pattern of passages


50


is formed in the underside


51


of top plate


40


, which may be expressed as a corresponding pattern of ridges


52


on the upper surface thereof. Similarly, a second pattern of passages


54


is formed in the upper surface


55


of bottom plate


42


. Gasket plate


44


is provided with a plurality of bores


56


extending completely through the plate at selected locations for connecting passages


50


in top plate


40


with passages


54


in bottom plate


42


. The upper surface


58


and the lower surface


60


of gasket plate


44


are further provided with respective patterns


62


,


64


of resilient gasketing material generally in the shape of the patterns of passages and bores in the top and bottom plates. Preferably, the gasketing patterns are disposed in shallow grooves


66


in surfaces


58


,


60


into which the gasketing material may be fully compressed when embodiment


38


is assembled.




The oil passages and gasketing patterns in plates


40


,


42


,


44


cooperate to define and form the oil galleries of a complex three dimensional hydraulic manifold


68


for selectively distributing pressurized oil from an oil riser


70


to each of four solenoid control valves


30


received in sockets


72


formed in bottom plate


42


, as shown clearly in FIG.


9


. Valves


30


extend through bottom plate


42


and the valve heads thereof seal against seats


74


on the underside of gasket plate


44


. Each of the control valves


30


controls the activation and deactivation of all valve lifters for a given cylinder of an eight-cylinder engine via outlet ports


69


in manifold


68


; thus, four control valves are required, for example, to deactivate valves for four cylinders of an eight-cylinder engine.




Oil is distributed along the manifold from riser


70


via a global supply gallery


76


which connects via bores


78


in gasket plate


44


to control valves


30


below seats


74


. Riser


70


may be provided with an inline strainer housing


71


for ready replacement of strainer


28


. When a valve


30


is energized to open, oil is admitted through seat


74


and upwards through plate


44


via bore


75


into an individual supply gallery


80


for supplying two deactivation valve lifters via bores


79


and associated outlet ports


69


. It is highly important for proper and reliable engine response that galleries


80


be entirely free of air when valves


30


are called upon to provide pressure to their respective deactivation lifters. During periods of engine shutdown, the galleries in manifold


68


tend to drain by gravity to sump


12


via bore


75


which is then connected to a drain port through valve


30


, the oil being replaced by air. It is highly undesirable to purge such air through the lifters upon startup; therefore, a fill path is provided for each of galleries


80


. Bypass ports


82


are provided through gasket plate


44


in global supply gallery


76


leading via bypass orifices


77


into each of the individual galleries


80


to fill galleries


80


and the lines leading to the deactivation lifters (not shown). Oil is continually flowed, when control valve


30


is de-energized, via bore


75


, through a passage in valve


30


, and up through bore


85


into return gallery


81


. The entry to each of galleries


81


includes a cylindrical weir


87


extending above gasket plate surface


58


and having an upper lip higher than the inside height of gallery


80


, the return oil overflowing weir


87


and returning to sump


12


via outlet bore


89


in galleries


81


. This arrangement keeps gallery


80


filled with oil and thus prevents entry of air into the supply lines leading from the control valves to the deactivation lifters.




Orifices


77


must be small enough in diameter that the bypass circuits do not deprive the other engine oil circuits of oil, yet large enough that they permit rapid purging of galleries


80


and are not readily fouled by particles of contamination within the oil stream. A diameter of about


0


.


4


mm has been found to meet both requirements. Further, the exit aperture of each orifice


77


is preferably flared outwards, as shown in

FIG. 8

, to assist in scavenging air from galleries


80


.




Preferably, provision is made in manifold


68


for a breather pipe


65


connected to a conventional positive crankcase ventilation (PCV) valve (not shown).




It will be appreciated that other similar embodiments are possible within the scope of the invention. For example, the grooves


66


and gasketing patterns


62


,


64


may be applied directly to top plate surfaces


51


, in which case gasket plate


44


may be omitted entirely, and a suitable manifold formed by bolting top and bottom plates


40


,


42


directly together. However, such embodiment is not presently preferred because it cannot provide for bypass orifices


82


, although a similar channel may be incised laterally into plate


40


. Similarly, oil passage patterns


50


,


54


, presently provided in the top and bottom plates, respectively, may instead be provided along with the gasketing patterns in surfaces


58


,


60


, respectively, of gasket plate


44


, and surfaces


51


,


55


of the top and bottom plates may be substantially unfeatured. Such an embodiment is not presently preferred because the ridges


52


formed in top plate


40


also function as rib supports to increase desirably the stiffness of the overall assembly.




Referring to

FIGS. 2

,


3


,


7


, and


9


-


14


, a connector/retainer


84


holds the solenoid control valves


30


in their respective sockets


72


and provides electrical connection of the solenoids to the ECM


32


. Connector/retainer


84


is preferably insert molded or cast of a high-temperature dielectric plastic. Two different styles of connector/retainer are shown which are functionally equivalent. The connector/retainer


84


shown in

FIGS. 2

,


3


,


7


and


10


-


14


supports control valves


30


at their bases via cups


86


; or, as shown in

FIG. 9

, at a shoulder flange


88


on the valves via deep cups


90


. Connector/retainer


84


is provided with integral standoffs


92


through which it is bolted into manifold


68


. As shown in

FIG. 12

, electrical leads


83


are cast into connector/retainer


84


, terminating distally at conductive slotted tabs


94


into which connector tabs


96


on the control valves


30


(

FIG. 2

) are connectively inserted to provide power to the solenoids. Leads


83


terminate proximally at a female socket


98


(

FIG. 10

) into which a spaded connector


100


may be inserted (

FIG. 11

) for conventional connection of the control valves to ECM


32


.




In operation, at engine start-up, typically all valve lifters are activated, all engine valves are functional, and all control valves are de-energized. Oil pump


10


via riser


70


fills global oil gallery


76


and individual oil galleries


80


via bypass orifices


77


, purging entrained air through bore


75


. Upon a signal sent from engine control module


32


to any one or more of control valves


30


via connector


100


and electrical leads


83


, the control valve(s) is actuated, permitting pressurized oil to flow from gallery


76


past valve


30


to outlet ports


69


for passage via engine block towers (not shown) to intake and exhaust valve deactivation lifters


20


(FIG.


1


). Oil continues to flow through bypass orifice


77


, over cylindrical weir


87


, and via return gallery


81


to sump


12


. Pressure is applied continuously to the lifters while control valve


30


is actuated. Upon a deactivation signal from ECM


32


, control valve


30


is closed, as by an internal spring or other conventional means (not shown), shutting off further pressure to lifters


20


. Excess oil in lifters


20


is expelled to sump


12


, and lifters


20


resume activation of the intake and exhaust valves.




While the invention has been described by reference to various specific embodiments, it should be understood that numerous changes may be made within the spirit and scope of the inventive concepts described. Accordingly, it is intended that the invention not be limited to the described embodiments, but will have full scope defined by the language of the following claims.



Claims
  • 1. A control system for deactivation of valves in a multiple-cylinder internal combustion engine having a pressurized oil source and hydraulically-operable deactivation valve lifters, comprising:a) a hydraulic manifold having a plurality of oil galleries connected between said oil source and said lifters; b) a plurality of independently-controllable solenoid control valves disposed on said manifold and extending into said galleries, said control valves being operable for activation and deaactivation of lifters associated with one or more of said cylinders by controlling the flow of pressurized oil to said associated lifters; and c) a lead frame connector/retainer mounted on said manifold for retaining said control valves in said disposition on said manifold and for carrying electrical signals to said control valves for activation and deactivation of said lifters.
  • 2. A control system in accordance with claim 1, wherein said hydraulic manifold is an assembly comprising:a) a top plate having a first pattern of oil passages formed in a lower surface thereof and a first pattern of resilient gasketing material disposed on said lower surface; and b) a bottom plate having a second pattern of oil passages formed in an upper surface thereof and a second pattern of reslient gasketing material disposed on said upper surface; wherein said lower and upper surfaces are matably joined to form said oil galleries.
  • 3. A control system in accordance with claim 2 wherein said lower and upper surfaces each further comprises a pattern of grooves for receiving said first and second patterns of resilient gasketing material, respectively.
  • 4. A control system in accordance with claim 2, wherein said hydraulic manifold is an assembly comprising:a) a top plate having a first pattern of oil passages formed in a lower surface thereof; b) a bottom plate having a second pattern of oil passages formed in an upper surface thereof; and c) a gasket plate having a first pattern of resilient gasketing material corresponding to said first pattern of oil passages disposed on a first surface thereof, and having a second pattern of resilient gasketing material corresponding to said second pattern of oil passages disposed on a second and opposite surface thereof, and having a plurality of bores extending between said first and second surfaces; wherein said gasket plate is matably retained between said top plate and said bottom plate to form said oil galleries.
  • 5. A control system in accordance with claim 4 wherein said first and second surfaces of said gasket plate each further comprises a pattern of grooves for receiving said first and second patterns of resilient gasketing material, respectively.
  • 6. A control system in accordance with claim 5 wherein said first and second patterns of gasketing material are non-identical.
  • 7. A control system in accordance with claim 4 wherein at least one of said bores through said gasket plate is an oil bypass orifice for purging air from at least one of said galleries.
  • 8. A control system in accordance with claim 7 wherein said bypass is orifice is flared at one of said plate surfaces to improve flushing of air from said gallery.
  • 9. A control system in accordance with claim 4 wherein at least one of said bores through said gasket plate at its exit from said first surface is provided with a length of conduit extending beyond said first surface.
  • 10. A control system in accordance with claim 1 wherein said lead frame connector/retainer includes electrical leads embedded in a plastic matrix.
  • 11. A control system in accordance with claim 1, wherein said control system is configured for mounting in the engine valley of a V-style engine.
  • 12. A control system in accordance with claim 1, wherein said hydraulic manifold is an assembly comprising:a) a top plate; b) a bottom plate; and c) a gasket plate having a first pattern of oil passages formed in a first surface thereof and having a first pattern of resilient gasketing material corresponding to said first pattern of oil passages disposed on said first surface, and having a second pattern of oil passages formed in a second and opposite surface thereof and having a second pattern of resilient gasketing material corresponding to said second pattern of oil passages disposed on said second and opposite surface thereof, and having a plurality of bores extending between said first and second surfaces, said second pattern of oil passages differing from said first pattern of oil passages; wherein said gasket plate is matably retained between said top plate and said bottom plate to form said oil galleries.
  • 13. A control system in accordance with claim 4 wherein at least one of said top plate, said bottom plate, and said gasketing plate is formed from a material selected from the group consisting of metals and plastics.
  • 14. A multiple-cylinder internal combustion engine having a system for deactivation of engine valves, the engine comprising:a) a deactivation valve lifter for each valve to be deactivatable; b) an engine control module for controlling the activation and deactivation of said valve lifters; c) a source of pressurized oil; and d) a valve deactivation control system disposed in said engine between said valve lifters and said engine control module, said system including i) a hydraulic manifold having a plurality of oil galleries connected between said oil source and said lifters; ii) a plurality of independently-controllable solenoid control valves disposed on said manifold and extending into said galleries, a one of said control valves being operable for activation and deactivation of lifters associated with each one of said cylinders by controlling the flow of pressurized oil to said associated lifters; and iii) a lead frame connector/retainer mounted on said manifold for retaining said control valves in said disposition on said manifold and for providing electrical signals to said control valves for activation and deactivation of said lifters.
  • 15. A control system for use with hydraulically-actuated deactivation valve lifters, comprising:a hydraulic manifold including a top plate, said top plate having a lower surface, said lower surface defining an upper portion of a first pattern of oil passages, a bottom plate having an upper surface, said upper surface defining a lower portion of a second pattern of oil passages, said top and bottom plate being connected together, oil galleries defined at least in part by said first and second pattern of oil passages; a gasket plate having a first surface and a second surface, a first pattern of resilient gasketing material disposed on said first surface and corresponding to said first pattern of oil passages, a second pattern of resilient gasketing material disposed on said second surface and corresponding to said second pattern of oil passages, said gasket plate defining a plurality of bores extending from said first surface to said second surface, said gasket plate being disposed between said top and bottom plates, said gasket plate defining at least in part said oil galleries in conjunction with said first and second pattern of oil passages; and a lead frame connector/retainer affixed to said manifold, said lead frame including a plurality of retaining means and electrical signal carrying means.
  • 16. The control system of claim 5, further comprising a plurality of independently-controllable solenoid control valves, each of said control valves disposed within a corresponding one of said plurality of retaining means and extending into a corresponding one of said oil galleries, each said control valve controlling the flow of fluid to a corresponding one of the deactivation valve lifters, said control valves receiving and being responsive to electrical signals from said electrical signal carrying means.
US Referenced Citations (3)
Number Name Date Kind
1872141 Hallett Aug 1932 A
5086803 Nakajima Feb 1992 A
5970956 Sturman Oct 1999 A
Foreign Referenced Citations (2)
Number Date Country
3300763 Jul 1984 DE
59122714 Jul 1984 JP