The present invention relates to a valve control system for an internal combustion engine, and more particularly, to such a system which can vary the operational characteristics of an engine poppet valve, in accordance with various operational modes of the engine.
Variable valve control systems for engine poppet valves are already generally well known in the art. Although such variable valve control systems can be applied to either the intake poppet valve, or the exhaust poppet valve, or both, it is most common to utilize such a variable valve control system to vary the “lift” (the amount of opening of the engine poppet valve) of only the intake poppet valves, and the invention will be described in connection with such an arrangement.
A “dual lift” valve control system is known from U.S. Pat. Nos. 4,762,096 and 5,660,153, both of which are assigned to the assignee of the present invention and incorporated herein by reference. In a typical dual lift valve control system, there is a low lift condition in which the poppet valve opens a relatively small amount while the engine is operating at relatively lower speeds, and a high lift condition in which the poppet valve opens a relatively large amount while the engine is operating at relatively higher speeds. Normally, such dual lift valve control systems require some sort of actuator (typically an electromagnetic or electro-hydraulic actuator) to move a latch member between unlatched (low lift) and latched (high lift) conditions. Although such dual lift valve control systems have shown the ability to perform in a generally satisfactory manner, there are many vehicle applications in which it is desirable to be able to select from among a greater range of lift options than merely “high” lift and “low” lift.
Also now well know to those skilled in the art are valve control systems of the type including “valve deactivation” capability. One embodiment of a valve deactivation control system is illustrated and described in U.S. Pat. No. 6,321,704, also assigned to the assignee of the present invention and incorporated herein by reference. In the valve deactivation system of the cited patent, there is an hydraulic lash adjuster (HLA) which may be operated in either: (i) a latched condition, in which case the rotation of the camshaft will result in normal valve lift, or (ii) an unlatched condition, introducing lost motion into the valve gear train, whereby rotation of the camshaft will result in very little lift, or more commonly, no lift at all of the engine poppet valve. Such valve deactivation systems have now started to enjoy a certain amount of commercial success, although the required latching mechanism, and the associated controls, add substantially to the cost of the engine valve train, especially considering that the result is merely a choice between normal lift and valve deactivation.
As is well know to those skilled in the art, in a typical dual lift valve control system, the dual lift capability would be provided for each and every cylinder. For example, on a V-8 engine, all eight of the intake poppet valves (assuming one intake valve per cylinder) would be provided with a dual lift valve control system, and normally, all of the intake poppet valves would operate “together”, i.e., all would be in the low lift mode or all would be in the high lift mode, at any given point in time.
On the other hand, on engines having valve deactivation capability (also referred to as “cylinder deactivation”), only a portion of the cylinders are deactivated. For example, on a V-8 engine, it would be typical to provide the intake poppet valves, and the exhaust poppet valves, for two of the cylinders on each bank with valve deactivation capability so that, as the engine speed and load reach predetermined values, all of the valves for those two cylinders of each bank would be deactivated, such that the engine then operates on four cylinders (i.e., as a “V-4” engine) at highway speeds and low throttle loads.
On certain vehicle engines, it would be desirable to provide both dual lift and valve deactivation capability. Unfortunately, based upon the known prior art, to provide even half of the engine poppet valves with both dual lift and valve deactivation capability would result in a valve control system which would be prohibitively expensive, and in many engine applications, would provide substantial packaging problems. The above disadvantage of the prior art is even more of a problem if, instead of “cylinder deactivation”, it is desired to provide true “valve deactivation”, and it will be understood that references hereinafter to “deactivation” will mean and include both cylinder-type and valve-type deactivation. In a true valve deactivation system, there would be two intake poppet valves per cylinder, and deactivation would be provided for one (typically, the “tumble” intake valve) of the two intake valves on each cylinder. Thus, the problems noted above regarding cost and packaging would be exacerbated by requiring deactivation capability on all eight cylinders.
Accordingly, it is an object of the present invention to provide an improved valve control system for an internal combustion engine having both dual lift capability and valve (or cylinder) deactivation capability.
It is a more specific object of the present invention to provide such an improved valve control system which achieves the above-stated object in a manner which is economically feasible and at the same time is feasible in terms of the overall packaging of the valve control system.
It is a further object of the present invention to provide such a valve control system which achieves the above-stated objects, but which does not require a separate actuator for each cylinder, or for each poppet valve being controlled, and which is able to use the same structure to achieve both the dual lift and the deactivation.
The above and other objects of the invention are accomplished by the provision of an improved valve control system for an internal combustion engine including a cylinder head and a poppet valve moveable relative to the cylinder head between open and closed positions. A camshaft has a first cam lobe profile and a second cam lobe profile formed thereon. The valve control system comprises a rocker arm assembly including a first cam follower engageable with the first cam lobe profile and a second cam follower engageable with the second cam lobe profile. The rocker arm assembly defines a valve pad in engagement with a stem tip portion of the poppet valve, and disposed toward a first axial end of the rocker arm assembly, and further defines a first fulcrum surface toward a second axial end of the rocker arm assembly, the first and second axial ends being oppositely disposed about the first and second cam followers. A first lash compensation device is operably associated with the cylinder head and includes a first plunger in engagement with the first fulcrum surface of the rocker arm assembly.
The improved valve control system is characterized by the rocker arm assembly defining a second fulcrum surface disposed axially between the first fulcrum surface and the cam followers. A second lash compensation device is operably associated with the cylinder head and includes a second plunger in engagement with the second fulcrum surface of the rocker arm assembly. Each of the first and second lash compensation devices is selectively switchable between a latched condition and an unlatched condition.
Referring now to the drawings, which are not intended to limit the invention,
The valve control system 13 operates in conjunction with a camshaft, generally designated 21, to provide cyclical opening motion to the engine poppet valve 15, in opposition to the biasing force of the valve return spring 20. The camshaft 21 includes a base circle portion 23, a first, low lift cam profile 25 and a second, high lift cam profile 27. As will be understood from the subsequent description of the invention, typically there would be one of the high lift cam profiles 27 and a pair of low lift cam profiles 25, disposed on axially opposite sides of the high lift cam profile 27. For purposes of the subsequent description, it will be assumed that the camshaft 21 is rotating counter-clockwise, as is shown by the arrow in FIG. 1.
The valve control system 13 of the present invention comprises two primary “subsystems”, a rocker arm assembly, generally designated 29, and a hydraulic lash adjuster assembly, generally designated 31. Each of the assemblies 29 and 31 will now be described in greater detail. It should be understood by those skilled in the art that the particular construction, shown and described hereinafter, of the rocker arm assembly 29, and of the HLA assembly 31 is by way of example only, and is not essential to the present invention, except as is specifically recited in the appended claims.
Referring now primarily to
The outer body member 37 includes a pair of pocket portions 47 which are deformed laterally outward, out of the plane of the rest of the outer body member 37, and therefore, cooperate with the adjacent outer surface of the inner body member 35 to define openings or “pockets”. In each of the pockets formed by the portions 47, there is disposed a generally cylindrical cam follower 49, each of the cam followers 49 being disposed for engagement with one of the low lift cam profiles 25. Although not shown herein, for simplicity of illustration, those skilled in the art will understand that, preferably, each of the cam followers 49 would rotate about a shaft, with the opposite ends of each of the shafts being received within mating openings in the adjacent wall portions of the inner body member 35 and the pocket portion 47. Such an arrangement is already well known in the art.
The inner and outer body members 35 and 37 also cooperate to define a pair of aligned circular openings 51 (see
Referring now primarily to
Referring now primarily to
The housing member 71 is, in the subject embodiment, an investment cast part which is then subsequently machined to the configuration shown. The housing member 71 defines a first vertical bore 79 and a second vertical bore 81, the bores 79 and 81 preferably being parallel and having their center lines defining a plane (the plane of
Disposed within the first bore 79 is a first lash compensation device 83 (see FIG. 8), and disposed within the second bore 81 is a second lash compensation device 85 (see FIG. 9). The lash compensation devices 83 and 85 (each of which is also referred to as a “hydraulic lash adjuster” or an “HLA”) may be of the type which are generally well know to those skilled in the art, are nearly identical to each other, and therefore will be described only briefly hereinafter. It should be understood by those skilled in the art that the lash compensation devices 83 and 85 are functionally important elements of the overall valve control system 13, although the particular construction details shown herein are not essential, except as may be noted subsequently.
Each of the lash compensation devices 83 and 85, in the subject embodiment, and by way of example only, includes a body member 87 defining an annular groove 89. Disposed within the body member 87 is a lower plunger member 91 which cooperates with the body member 87 to define a high pressure chamber 93. The lower plunger member 91 also defines a seat surface for a ball check valve 95.
Referring now to
In accordance with one important aspect of the present invention, each of the first and second lash compensation devices 83 and 85 is selectively switchable between a latched condition, as shown in
In the subject embodiment, and by way of example only, there is provided within the cylinder head 11 at least a pair of latch members 103 for each of the lash compensation devices 83 and 85, although for simplicity of illustration, only one of the latch members 103 is shown (in
In the unlatched condition, the latch members 103 are retracted far enough radially such that they are out of engagement with the annular groove 89, thus permitting the lash compensation device (83 or 85) to move within its respective vertical bore (79 or 81). As is shown only in
On the other hand, when there is pressure present in one of the grooves 89, the respective HLA (83 or 85) will be in the unlatched condition, such that rotation of the camshaft 21 will cause the particular HLA to move downward in its bore (79 or 81), in opposition to the force of its lost motion spring 107. As is well known to those skilled in the art of engine valve controls, the lost motion spring 107 is selected to provide less biasing force than the valve return spring 20 so that, when the HLA is unlatched, the respective rocker arm will pivot about the tip portion 17 of the poppet valve 15, and the end of the respective rocker arm engaging the HLA will move vertically up and down with the unlatched HLA (83 or 85).
Based upon the above explanation and understanding of how each individual HLA and rocker arm operate, depending upon whether the HLA is latched or unlatched, the operation of the entire valve control system of the present invention will now be described. The subsequent description of the operation of the valve control system will, for simplicity, be based upon the assumption of only a single intake poppet valve 15 per cylinder, and that what is shown in
When the engine is operating at a relatively higher speed and/or at a relatively higher engine load, as those terms are generally understood in the art, the engine microprocessor (not shown herein) will provide a suitable command signal, resulting in the discontinuance of control pressure to the annular grooves 89. As a result, both the HLA 83 and the HLA 85 will be in the latched condition, as was described previously, and the high lift cam profile 27 will engage the second cam follower 61, causing the entire rocker arm assembly 29 to pivot about the point of engagement of the undersurface of the bottom portion 59 and the upper surface 101 of the HLA 85. With the rocker arm assembly 29 now pivoting about the HLA 85, which defines a shorter “lever arm”, the high lift cam profile 27 causes a relatively larger valve lift to occur, as shown by the lift height designated “H” in FIG. 1. It should be noted that the entire valve control system 13 is shown in
When the engine operates at a relatively lower engine speed and/or at a relatively lower engine load, the engine microprocessor will provide a suitable command signal, resulting in the presence of control pressure in the annular groove 89 of only the HLA 85, such that the HLA 85 will now be in the unlatched condition, whereas the HLA 83 will continue in the latched condition. With the HLA 83 and the HLA 85 in the particular combination of conditions described above, engagement of the high lift cam profile 27 with the cam follower 61 merely results in the inner rocker arm subassembly 55 pivoting (counterclockwise in
At the same time that the HLA 85 is engaging in “lost motion”, as described previously, the HLA 83 remains in the latched condition, such that the entire rocker arm assembly 29 (and specifically, the outer rocker arm subassembly 33) will now pivot about the engagement of the plunger 97 and the hemispherical surface 98. This pivotal movement of the rocker arm assembly will occur in response to the low lift cam profiles 25 engaging the first cam followers 49, and because of the longer “lever arm” between the plunger 97 and the cam follower 49, and the lower “lift” provided by the cam profiles 25, the result is a relatively smaller valve lift height than the lift height “H” shown in FIG. 1.
When the engine is operating at very low load but is cruising at highway speeds, the poppet valve 15 may be operated in the valve deactivation (“cylinder deactivation”) condition by providing a suitable command to communicate control pressure to the annular grooves 89 of both HLA 83 and HLA 85. In this condition, rotation of the camshaft 21 results in the outer rocker arm subassembly 33 pivoting about the elephant's foot member 45, while the inner rocker arm subassembly 55 pivots about the axle shaft 53, but with no motion being transmitted to the poppet valve 15. Instead, the poppet valve 15 remains in its closed position, under the influence of the return spring 20, while both the HLA 83 and the HLA 85 reciprocate in their respective bores 79 and 81, overcoming the biasing force of their respective lost motion springs 107, once per rotation of the camshaft 21.
The invention has been described in great detail in the foregoing specification, and it is believed that various alterations and modifications of the invention will become apparent to those skilled in the art from a reading and understanding of the specification. It is intended that all such alterations and modifications are included in the invention, insofar as they come within the scope of the appended claims.
Number | Name | Date | Kind |
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4762096 | Kamm et al. | Aug 1988 | A |
5189997 | Schneider | Mar 1993 | A |
5386806 | Hurr et al. | Feb 1995 | A |
5501186 | Hara et al. | Mar 1996 | A |
5660153 | Hampton et al. | Aug 1997 | A |
5960756 | Miyachi et al. | Oct 1999 | A |
6321704 | Church et al. | Nov 2001 | B1 |
Number | Date | Country |
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361118513 | Jun 1986 | JP |
Number | Date | Country | |
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20040182340 A1 | Sep 2004 | US |