Variable valve actuation assembly for an internal combustion engine

Information

  • Patent Grant
  • 6591798
  • Patent Number
    6,591,798
  • Date Filed
    Monday, December 17, 2001
    24 years ago
  • Date Issued
    Tuesday, July 15, 2003
    23 years ago
Abstract
A variable valve actuation assembly for actuation of an engine intake valve between low-lift and high-lift modes. The VVA assembly includes a special rocker assembly having a pivotable central high-lift cam follower and two peripheral low-lift cam followers; a camshaft having low-lift and high-lift lobes engageable with the respective cam followers; a primary latching assembly including a slidable primary latching pin in the rocker assembly for engaging and disengaging the high-lift follower; a solenoid for causing the primary latching pin to be engaged and disengaged; and a secondary latching mechanism between the solenoid and the primary latching pin to automatically limit engagement and disengagement of the primary latching pin to times in the duty cycle of the camshaft (during lift events) when ejections of the primary latching pin are not possible.
Description




TECHNICAL FIELD




The present invention relates to internal combustion engines; more particularly, to devices for controlling the variable actuation of intake valves in an internal combustion engine; and most particularly, to a variable valve actuation assembly for controllably actuating and deactuating a rocker assembly responsive to a triple-lobed cam in an internal combustion engine between high valve lift and low valve lift modes.




BACKGROUND OF THE INVENTION




Internal combustion engines are well known. 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 which may include valve lifters, pushrods, and rocker arms.




It is known that for a portion of the duty cycle of a typical multiple-cylinder engine, especially at times of low torque demand, valves may be opened to only a low lift position to conserve fuel; and that at times of high torque demand, the valves may be opened wider to a higher lift position to admit more fuel. It is known in the art to accomplish this by providing a special rocker assembly having a switching or latching pin which may be actuated and/or deactuated electromechanically. The rocker assembly includes both fixed peripheral low-lift cam followers that cause low lift of the valve when the pin is disengaged, and a pivotable central high lift cam follower that causes high lift of the valve when the latching pin is engaged into the high lift follower.




Various methods for actuating this type of latching pin are known. For example, see the disclosures of U.S. Pat. Nos. 5,619,958; 5,623,848; and 5,697,333. All of these methods employ individual solenoids, acting through bellcranks or similar structures, as part of an actuation system.




A significant problem for these devices is how to balance the physical size of the solenoid against the force required to actuate the mechanism. The solenoid desirably has rapid response, small size, sufficient stroke and pull-in force, low power requirement, and low sensitivity to voltage and temperature variations; whereas, large size, high pull-in force, and high power are typically required to energize prior art mechanisms.




One approach, disclosed in the above-referenced patents, is to reduce the solenoid force required by using the rotational motion of the rocker assembly inherent in its duty cycle to supply a portion of the actuating force. Typically, the motion of the rocker assembly permits the solenoid to “pull in” to a low air gap wherein high actuating forces can be generated. The solenoid essentially locks itself in the engaged position during a valve lift event (lift portion of the duty cycle), and some other compliant element in the device, such as a bellcrank, resiliently deflects as the rocker returns to the base circle portion of the cam at the conclusion of the lift event. Once the rocker reaches the base circle, the energy stored in the compliant element causes the locking pin to become engaged with the high-lift follower, shifting the rocker assembly to high-lift mode. This configuration requires the holding force of the solenoid in the actuated position to be greater than the force exerted against it by the compliant element; otherwise, the motion of the rocker assembly will overcome the solenoid and increase the magnetic air gap within the solenoid to a point at which the solenoid force becomes too small to actuate the pin, and the rocker then does not shift to high-lift mode.




Another prior art approach, disclosed in U.S. Pat. No. 5,623,897, decouples the force generated by the compliant element from the locking force of the solenoid. One end of the compliant element is “grounded” to the cylinder head, and the solenoid moves the opposite end of the compliant element into a position wherein it may engage the rotational displacement of the rocker assembly. The solenoid simply has to hold the compliant element in that position; it is not required to resist the internal force carried by the compressed compliant element.




The prior art configurations as disclosed have several shortcomings.




First, several of the linkages are fixed with respect to the pivot point of the rocker assembly, which typically is the ball-head of a hydraulic lash adjuster (HLA) supporting the assembly. The vertical length of the HLA may vary in the normal course of operating, and thus the pivot point may also vary in the z (vertical) direction. Further, the vertical and horizontal (x,y) locations of the pivot point must vary inherently from engine to engine as a result of stack-up of manufacturing tolerances. The prior art disclosures do not address practical or self-compensating means for accommodating tolerances in the cylinder head and cam cover.




Second, mechanisms disclosed in the prior art typically employ rotating linkages which may add friction to the force required for actuation and thus increase the force requirements of the solenoid.




Third, none of the disclosed mechanisms, except that shown in U.S. Pat. No. 5,623,897, fully decouples the solenoid force from the compliant element and, therefore, from the pin actuating force. In the disclosure of U.S. Pat. No. 5,623,897, a rotating rocker assembly with a large rocker ratio and large rotational inertia pivots through a relatively large angle in actuating the engine valve. These characteristics add to the force requirements of the solenoid. Further, the solenoid plunger does not act orthogonally to the rocker assembly, resulting in side-loading and friction in the solenoid bearings.




Fourth, in some prior art mechanisms, the point in the rotational cycle of the cam at which the solenoid is energized must be very carefully timed to avoid a phenomenon known in the art as “ejection” wherein the mechanism attempts to engage or disengage the locking pin into or out of the high-lift follower. When the pin is only slightly engaged, it is violently ejected, which can damage the pin or the high-lift follower and which causes a very loud and objectionable noise. Accurate timing of the solenoid energizing can be complex, as the response time of the mechanism may be affected by various operating parameters, such as oil temperature and thus viscosity.




It is a principal object of the present invention to provide an improved variable valve actuation (VVA) assembly wherein a secondary latching mechanism between the solenoid and the primary latching pin in the rocker assembly automatically self-times the engagement of the secondary latching mechanism such that the timing of solenoid energizing and de-energizing is not critical and ejections are prevented.




It is a further object of the invention to provide an improved VVA requiring a low solenoid actuating force and short stroke.




It is a still further object of the invention to provide an improved VVA wherein variation in assembly performance from the stack-up of manufacturing and operating tolerances among the components of the assembly is minimized.




SUMMARY OF THE INVENTION




Briefly described, a variable valve actuation assembly for variably opening of an engine intake valve in either a low-lift or high-lift mode includes a special rocker assembly pivotably disposed in the engine for opening and closing the valve and having a central high-lift cam follower and two peripheral low-lift cam followers, responsive to rotation of a camshaft having low-lift and high-lift lobes engageable with the respective cam followers; a primary latching mechanism including a slidable primary latching pin in the rocker assembly for engaging and disengaging the high-lift follower; a solenoid for causing the primary latching pin to be engaged and disengaged; and a secondary latching mechanism between the solenoid and the primary latching pin to automatically limit engagement and disengagement of the primary latching pin to times in the duty cycle of the camshaft when ejections are not possible.











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 an isometric view from above, taken from the camshaft side (camshaft omitted for clarity) showing two variable valve actuation assemblies in accordance with the invention configured for operation of adjacent intake valves of adjacent engine cylinders;





FIG. 2

is an isometric view from above of the VVA assemblies shown in

FIG. 1

, taken from opposite the camshaft side (camshaft omitted for clarity);





FIG. 3

is an isometric view similar to that shown in

FIG. 1

, showing the VVA assemblies installed in the head of an engine;





FIG. 4

is a view similar to that shown in

FIG. 1

, but including a camshaft with high-lift and low-lift cams for one of the VVA assemblies;





FIG. 5

is an isometric view, partially exploded, taken from the VVA side opposite the camshaft side, of secondary latching mechanisms in the VVA assemblies shown in

FIGS. 1-4

;





FIG. 6

is an isometric view, partially in cross-section, similar to that shown in

FIG. 5

, showing the relationship of the solenoid mounted on an arbor on the engine and a secondary latching pin in the secondary latching mechanisms shown in

FIG. 5

;





FIGS. 7 through 10

are cross-sectional elevational views through a VVA taken along plane


7


-


10


in

FIG. 4

, showing successive stages in one operating cycle of a VVA in accordance with the invention; and





FIG. 11

is another view of

FIG. 1

showing cam follower rollers as an alternate embodiment.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




Referring to

FIGS. 1 and 2

, an improved dual variable valve actuation (VVA) assembly


10


in accordance with the invention is shown for variable actuation of two separate valves


12


of internal combustion engine


13


. Assembly


10


includes two separate, substantially identical VVA mechanisms


10


′ sharing a common arbor


14


mountable onto an engine head


94


(as shown in FIG.


3


). As the two VVA assemblies are substantially mirror images of each other, the following discussion is directed to only one VVA but should be understood as being applicable to both except as noted. Each mechanism


10


′ includes a rocker assembly


16


and a secondary latching assembly


18


. Rocker assembly


16


is pivotably mounted, preferably by a ball-and-socket joint, on a conventional hydraulic lash adjuster (HLA)


20


and is pivotably connected near a distal end


22


, to the stem of a valve


12


.




Referring to

FIGS. 1 and 2

and any of

FIGS. 7 through 10

, rocker assembly


16


is similar to two-stage rocker assemblies known in the art, as described above. A frame


24


has a spherical socket


26


for pivotably mating with the ball head


28


of HLA


20


. Frame


24


provides a rigid but pivotable bridge between HLA


20


and valve


12


, and is formed having a generally rectangular longitudinal aperture


30


for receiving a high-lift cam follower


32


having a surface for following a high-lift cam lobe as described below. Follower


32


is pivotably pinned at one end by pin


34


in slot


36


formed in frame


24


in communication with aperture


30


. Preferably, a first torsion spring (not shown) is disposed on pin


34


in slot


36


to bias follower


32


upwards into continual contact with its respective cam lobe. Frame


24


further is provided with two rigidly-mounted low-lift cam followers


38


, each having a surface for following a low-lift cam lobe as described below.




At the proximal end


40


of rocker assembly


16


, a primary latching assembly


17


in frame


24


includes a stepped bore


42


slidably receivable of a primary latching pin


44


comprising a latching portion


46


and a trigger portion


48


. Pin


44


is urged away from high-lift follower


32


by a compression spring


50


disposed in bore


42


between frame


24


and trigger portion


48


. When follower


32


is suitably positioned (as shown in FIG.


10


), portion


46


may be moved axially of bore


42


to engage portion


46


under latching nose


52


of follower


32


, thereby preventing follower


32


from rotating about pin


34


, and transforming rocker assembly


16


into high-lift mode, as described below.




Referring to

FIGS. 5 through 10

, secondary latching assembly


18


includes a backer frame


54


having a central aperture


56


for receiving a blocker plate


58


therein. Backer frame


54


is provided with bores


60


for receiving pivot screw


62


which is threadedly received in a bore in arbor


14


to pivotably attach frame


54


to arbor


14


. A shim


64


on screw


62


spaces frame


54


a predetermined distance from arbor


14


and supports a second torsion spring


66


engaged by a first tang


68


into arbor


14


and by a second tang


70


onto frame


54


for urging frame


54


pivotably toward rocker assembly


16


. As shown in

FIGS. 5 and 6

, each siderail


72


of frame


54


is further provided with a stepped bore


74


for receiving a stepped secondary latching pin


76


having a flat boss


78


at one end thereof. A compression spring


80


is disposed in bore


74


around pin


76


for urging pin


76


outwards of bore


74


. Only one bore


74


is used for each frame


54


, but preferably the two bores


74


provided in each frame are mirror images of each other so that a single configuration of frame


54


may be used for either of the assemblies


18


shown in these figures.




Blocker plate


58


is provided with a first bore


82


at an end thereof for receiving screw


62


to pivotably mount plate


58


between bores


60


in frame


54


such that plate


58


can swing through aperture


56


. A third torsion spring


75


is disposed on screw


62


coaxially with plate


58


and is configured conventionally to urge plate


58


rotationally of screw


62


against trigger portion


48


. Plate


58


is further provided with a medial bore


84


for receiving secondary latching pin


76


to rotationally lock plate


58


to frame


54


when so desired.




Frame


54


is further provided with an actuating extension


77


for engaging with the bearing surface


79


of rocker proximal end


40


. Preferably, the bearing surface


81


of extension


77


is included in a plane including the pivot axis


83


of backer frame


54


and bearing surface


79


is a cylindrical arc centered on the center of arcuate pad


85


which interfaces with the stem of valve


12


. As rocker assembly


16


oscillates about HLA head


28


during actuation thereof, surface


79


rotates and slides along surface


81


at a constant radius, and therefore the position of backer frame


54


is unaffected by such action. Further, these geometric relationships make the VVA mechanism virtually insensitive to normal manufacturing, assembly, and operating variations in the size and position of these components.




Arbor


14


is provided with a well


87


for receiving a solenoid


86


having an armature plunger


88


extending toward boss


78


on pin


76


in a direction orthogonal to plane


7


-


10


(FIG.


4


), which is the actuation plane of assembly


10


′, and parallel to the axis of rotation of the camshaft. When solenoid


86


is energized, pin


76


is urged toward blocker plate


58


in attempt to enter into bore


84


to lock plate


58


to frame


54


. Such entry is permitted under conditions as described below, wherein bore


74


becomes axially aligned with bore


84


. Where entry is not permitted immediately upon energizing of the solenoid, the energized solenoid acts as a cocked electromechanical spring and will insert pin


76


into bore


84


at the earliest opportunity during the camshaft duty cycle, as described below.




Referring to

FIGS. 3 and 4

, a camshaft


90


is carried in bearing mounts


92


formed in engine head


94


which positions cam lobes for actuation of valves


12


via rocker assembly


16


. In

FIG. 4

, the camshaft and cam lobes are shown for only one valve, but it should be understood that identical lobes are provided for each valve having an associated VVA mechanism. Camshaft


90


is provided with a central high-lift lobe


96


, which is followed by central high-lift follower


32


, and a pair of identical peripheral low-lift lobes


98


flanking lobe


96


, which are followed by peripheral low-lift followers


38


.




The conversion of a VVA assembly


10


′ from low-lift mode (default mode) to high-lift mode is shown sequentially in

FIGS. 7 through 10

. Beginning with

FIG. 7

, in default low-lift mode, primary latching pin


44


is disengaged from high-lift follower


32


. Valve


12


is closed. Low-lift cam lobe


98


is engaged on its base circle portion


100


with low-lift follower


38


, and high-lift cam lobe


96


is engaged on its base circle portion


102


with high-lift follower


32


. Solenoid


86


is de-energized and therefore secondary latching pin


76


is disengaged from blocker plate


58


which is pivoted out of alignment by contact with trigger portion


48


at contact point


112


. Thus compression spring


50


which urges primary latching pin


44


out of engagement must be stronger than, and overcome, third torsion spring


75


. To begin the change from low-lift mode to high lift mode, solenoid


86


may be energized at any time during the camshaft duty cycle. Plunger


88


of the solenoid forcibly engages boss


78


(not visible in

FIGS. 7-10

) but secondary latching pin


76


cannot yet enter bore


84


because of axial misalignment. Secondary latching pin


76


is thus cocked by the energized solenoid to enter bore


84


in the blocker plate to lock the blocker plate to the backer frame


54


as soon as bore


84


becomes coaxially aligned with the pin.




Referring to

FIG. 8

, a low-lift event is shown in progress. The camshaft has rotated the cam lobes counterclockwise such that eccentric portion


104


of low-lift lobe


98


is engaged with low-lift follower


38


, thereby rotating rocker assembly


16


clockwise about HLA head


28


and opening valve


12


with low lift. Eccentric portion


106


of high-lift lobe


96


is similarly engaged with high-lift follower


32


, but because follower


32


is disengaged from primary latching pin


44


the follower simply pivots on pin


34


without lift effect on valve


12


. Note that bearing surface


108


on trigger


48


is preferably cylindrically arcuate and bearing surface


110


on blocker plate


58


is preferably flat. Comparing the contact point


112


between these two surfaces in FIG.


7


and

FIG. 8

, it is seen that the surface


108


moves along surface


110


in a combination sliding and rolling motion in response to the clockwise rotation of rocker assembly


16


. The angle of surface


110


with respect to pivot point


83


is such that the relationship of blocker plate


58


to backer frame


54


does not vary with tolerance variations in the cylinder head, an importance advance in the art conferred by an assembly in accordance with the invention. Further, because the change in contact point between the bearing surfaces is eccentric with respect to the pivot point of the rocker assembly, blocker plate


58


is permitted to pivot counterclockwise slightly about pivot axis


83


, bring bore


84


into alignment with pin


76


, which then enters bore


84


at the urging of the previously energized solenoid. Because the pin is small and of low mass, and because bore


84


is aligned with pin


76


by the natural motion of rocker assembly


16


imparted by the engine, solenoid


86


may be very small and relatively weak, thus overcoming the disadvantages of prior art VVA mechanisms as described above. This is an important advantage of a VVA assembly in accordance with the invention.




Referring to

FIG. 9

, as the low-lift event progresses, the cam lobes have rotated further counterclockwise such that the followers are in contact with the lobes at the point of merger between the eccentric portions


104


,


106


and the base circle portions


100


,


102


of the lobes


98


,


96


. Valve


12


has been closed by the action of a conventional valve spring (not shown), causing rocker assembly


16


to rotate counterclockwise back to its rest position, as shown previously in FIG.


7


. However, blocker plate


58


is not free to also return to its former position because it is now locked to backer frame


54


, as was seen in FIG.


8


. Further, latching portion


46


of primary latching pin


44


is still in slight interference with latching nose


52


. Therefore, the locked unit of backer frame and blocker plate is pivoted clockwise about axis


83


against second torsion spring


66


, cocking the primary and secondary latching mechanisms for engagement of primary latching pin


44


with latching nose


52


at the earliest opportunity.




Referring to

FIG. 10

, the low-lift event is completed and rocker assembly


16


is locked in high-lift mode by primary locking pin


44


. The cam lobes have rotated slightly farther than as shown in

FIG. 9

, onto their respective base circle portions, and high-lift follower


32


has pivoted farther clockwise about pivot pin


34


, bringing latching nose


52


into latching alignment with latching portion


46


. Second torsion spring


66


is stronger than compression spring


50


and immediately urges primary latching pin


44


into engagement with latching nose


52


, compressing spring


50


and completing the conversion of the rocker assembly from low-lift mode to high-lift mode. During the next revolution of the camshaft, the high-lift eccentric of lobe


96


will cause rocker assembly


16


to rotate through a greater angle than in the previous duty cycle, thereby opening valve


12


wider (higher lift) than in its previous opening.




Both primary latching pin


44


and secondary latching pin


76


will remain engaged as long as solenoid


86


is energized; the assembly will thus remain in high-lift mode. To shift back to low-lift (default) mode, the solenoid may be de-energized at any point. It will be seen that there is no shear force on secondary pin


76


while either a low-lift or high-lift event is in progress (eccentric lobe portions are engaged). Thus pin


76


is free to engage or disengage with bore


84


at any such time. De-energizing the solenoid during the high-lift event permits compression spring


80


to eject pin


76


from bore


84


; however, primary latching pin


44


remains engaged with latching nose


52


because of shear force therebetween. When the lobes return to their base circles and such shear force is removed, compressed spring


50


immediately urges primary latching pin out of engagement with nose


52


. Blocker plate


85


is free to pivot away, and the assembly is returned to the default low-lift mode shown in FIG.


7


.




It is an important advantage of a VVA assembly in accordance with the invention that the engagement of the primary latching pin with the high-lift follower necessarily occurs at the beginning of the base circle lobe engagement, at a point of no shear force between the pin and the follower. Thus, ejections of the primary latching pin, as are well known in the prior art, are rendered impossible. Further, because the secondary latching pin engages the blocker arm only when they are axially aligned, which occurs only during the lift portion of a low-lift duty cycle, the solenoid need be only strong enough to displace the secondary pin axially a short distance.




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. For example, high-lift and low-lift cam followers


32


,


38


are shown as sliders herein but some or all of the followers may instead be provided as rollers rotatably mounted to frame


24


within the scope of the invention. For example, in

FIG. 11

, roller


38


′ is shown instead of slider


38


. 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 variable valve actuation (VVA) assembly for actuation and deactuation of valves in an internal combustion engine having a camshaft with high-lift and low-lift lobes for at least one of said valves, each of said lobes having a lift portion and a base circle portion, the camshaft having an axis of rotation, comprising:a) a rocker assembly pivotably disposed on pivot means in said engine for variably responding to rotary motion of said lobes to open and close a valve of said engine, said rocker assembly including a frame fixedly supportive of at least one low-lift cam follower and pivotably supportive of a variably pivotable high-lift cam follower, said follower being pivotable about a first pivot axis; b) a primary latching assembly and a secondary latching assembly, said primary latching assembly disposed on said rocker assembly for variably latching said high-lift cam follower to said frame, said primary latching assembly including a primary latching pin slidingly disposed in a bore in said frame and variably engageable with said high-lift cam follower, said primary latching pin having a trigger portion for engaging with said secondary latching assembly, a first spring operatively connected to said primary latching pin for urging said pin out of engagement with said high-lift follower, said secondary latching assembly adjacent said primary latching assembly for variably actuating said primary latching assembly; and c) a solenoid adjacent said secondary latching assembly for variably actuating said secondary latching assembly.
  • 2. A VVA assembly in accordance with claim 1 further comprising an arbor mountable to said engine, wherein said secondary latching assembly comprises:a) a backer frame pivotably mounted to said arbor for pivoting about a second pivot axis for variable contact with said rocker assembly; b) secondary latching means disposed on said backer frame; and c) a blocker plate pivotably mounted to said arbor for pivoting about said second pivot axis and having a bore variably receivable of said secondary latching means for locking said backer frame and said blocker plate together for unified pivoting.
  • 3. A VVA assembly in accordance with claim 2 wherein said solenoid is disposed on said arbor for variably actuating said secondary latching means.
  • 4. A VVA assembly in accordance with claim 3 wherein said solenoid has an axis of linear actuation, and wherein said axis is parallel to said axis of rotation of said camshaft.
  • 5. A VVA assembly in accordance with claim 2, said trigger portion having a first bearing surface for engaging said blocker plate and said blocker plate having a second bearing surface for engaging said trigger portion, wherein said first bearing surface is arcuate and said second bearing surface is planar.
  • 6. A VVA assembly in accordance with claim 2 wherein said backer frame further comprises an actuating extension for variably engaging said rocker assembly.
  • 7. A VVA assembly in accordance with claim 6 wherein said actuating extension has a first surface for engaging said rocker assembly, and wherein said first surface is planar and is included in a plane including said second pivot axis.
  • 8. A VVA assembly in accordance with claim 6 wherein said rocker assembly has a bearing surface for engaging said first surface of said actuation extension, and wherein said assembly bearing surface is arcuate.
  • 9. A VVA assembly in accordance with claim 2 wherein said pivoting of said rocker assembly in response to motion of said eccentric portion of said low-lift cam lobe causes said primary latching assembly to pivot said blocker plate about said second pivot axis such that said secondary latching means can enter said bore in said blocker plate to lock said blocker plate to said backer frame.
  • 10. A VVA assembly in accordance with claim 2 wherein said primary latching pin is engageable of said high-lift follower only while said at least one low-lift follower is being engaged by said base circle portion of said low-lift cam lobe.
  • 11. A VVA assembly in accordance with claim 2 further comprising:a) a second spring disposed between said backer frame and said arbor for urging said backer frame toward said rocker assembly; and b) a third spring disposed between said blocker plate and said backer frame for urging said blocker plate toward said trigger portion.
  • 12. A VVA assembly in accordance with claim 11 wherein said first spring is stronger than said third spring, and wherein said second spring is stronger than either of said first and third springs.
  • 13. A VVA assembly in accordance with claim 1 wherein at least one of said high-lift and low-lift followers includes a roller rotatably disposed on said frame.
  • 14. A variable valve actuation (VVA) assembly for actuation and deactuation of first and second valves in an internal combustion engine having a camshaft with high-lift and low-lift lobes for each one of said valves, each of said lobes having a lift portion and a base circle portion, the camshaft having an axis of rotation, comprising:a) an arbor mounted on said engine; b) first and second rocker assemblies pivotably disposed on first and second pivot means in said engine for variably responding to rotary motion of said lobes to open and close said first and second valves, respectively, each of said rocker assemblies including a frame fixedly supportive of at least one low-lift cam follower and pivotably supportive of a variably pivotable high-lift cam follower, said follower being pivotable about a first pivot axis; c) first and second primary latching assemblies disposed on said first and second rocker assemblies, respectively, for variably latching said high-lift cam followers to said frames; d) first and second secondary latching assemblies for variably actuating said first and second primary latching assemblies, respectively; and e) first and second solenoids disposed on said arbor for variably actuating said first and second secondary latching assemblies, respectively.
  • 15. A secondary latching assembly mountable to an internal combustion engine for actuating a primary latching means in a rocker assembly for variably actuating a valve in the engine, comprising:a) a backer frame pivotably mounted to said engine for pivoting about a second pivot axis for variable contact with said rocker assembly; b) secondary latching means disposed on said backer frame; and d) a blocker plate pivotably mounted to said engine for pivoting about said second pivot axis and having a bore variably receivable of said secondary latching means for locking said backer frame and said blocker plate together for unified pivoting.
  • 16. A secondary latching assembly in accordance with claim 15 further comprising a solenoid disposed on said arbor for variably actuating said secondary latching means.
  • 17. A secondary latching assembly in accordance with claim 16 further comprising an actuating extension for engaging said rocker assembly, said actuating extension having a first surface for engaging said rocker assembly, wherein said first surface is planar and is included in a plane including said second pivot axis.
  • 18. An internal combustion engine having a variable valve actuation assembly for variable actuation of an engine valve, comprising:a) a rocker assembly pivotably disposed on pivot means in said engine for variably responding to rotary motion of camshaft lobes to open and close on at least one valve of said engine, said rocker assembly including a frame fixedly supportive of at least one low-lift cam follower and pivotably supportive of a variably pivotable high-lift cam follower, said follower being pivotable about a first pivot axis; b) a primary latching assembly and a secondary latching assembly, said primary latching assembly disposed on said rocker assembly for variably latching said high-lift cam follower to said frame, said primary latching assembly including a primary latching pin slidingly disposed in a bore in said frame and variably engageable with said high-lift cam follower, said primary latching pin having a trigger portion for engaging with said secondary latching assembly, a first spring operatively connected to said primary latching pin for urging said pin out of engagement with said high-lift follower, said secondary latching assembly adjacent said primary latching assembly for variably actuating said primary latching assembly; and c) a solenoid adjacent said secondary latching assembly for variably actuating said secondary latching assembly.
US Referenced Citations (5)
Number Name Date Kind
4151817 Mueller May 1979 A
5445116 Hara Aug 1995 A
5529033 Hampton Jun 1996 A
5623897 Hampton et al. Apr 1997 A
5653198 Diggs Aug 1997 A