The present disclosure relates to engine oil systems, and more specifically to valvetrain lubrication systems.
This section provides background information related to the present disclosure which is not necessarily prior art.
Internal combustion engines may combust a mixture of air and fuel in cylinders and thereby produce drive torque. Intake and exhaust valves control air flow to and from the engine cylinders. Oil may be provided to the cylinder head from the engine block to lubricate the valvetrain components.
An engine assembly may include an engine block, a cylinder head coupled to the engine block and first and second lubrication systems. The first lubrication system may include a first pump in communication with the engine block and providing a first fluid to the engine block. The second lubrication system may be isolated from the first lubrication system and may include a second pump in communication with the cylinder head and providing a second fluid to the cylinder head.
In another arrangement, an engine assembly may include an engine structure defining a cylinder bore, a first valve supported by the engine structure and in communication with the cylinder bore, a second valve supported by the engine structure and in communication with the cylinder bore, a hydraulic valve actuation mechanism and a mechanical valvetrain assembly. The hydraulic valve actuation mechanism may include an inlet in communication with a pressurized fluid and engaged with the first valve to control displacement of the first valve between an open position and a closed position. The mechanical valvetrain assembly may be engaged with the second valve and in communication with the pressurized fluid from an outlet of the hydraulic valve actuation mechanism.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only and are not intended to limit the scope of the present disclosure in any way.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Examples of the present disclosure will now be described more fully with reference to the accompanying drawings. The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses.
Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.
When an element or layer is referred to as being “on,” “engaged to,” “connected to” or “coupled to” another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being “directly on,” “directly engaged to,” “directly connected to” or “directly coupled to” another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., “between” versus “directly between,” “adjacent” versus “directly adjacent,” etc.). As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.
Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
An engine assembly 10 is illustrated in
The valvetrain assembly 18 will be described relative to a single cylinder bore 26 of the engine assembly 10 for simplicity. The valvetrain assembly 18 may include a hydraulic valve actuation mechanism 30 supported on the cylinder head 28 and engaged with a first valve 32 and a mechanical valve lift mechanism 34 supported on the cylinder head 28 and engaged with a second valve 36. The valvetrain assembly 18 may additionally include a camshaft 35 supported for rotation on a cam bearing region 37 of the cylinder head 28 and engaged with the mechanical valve lift mechanism 34 and a cam phaser 39 coupled to the camshaft 35 and rotationally driven by the crankshaft 16. In the non-limiting example illustrated in
In the present non-limiting example, the first valve 32 is an intake valve, the second valve 36 is an exhaust valve, and the mechanical valve lift mechanism 34 is a rocker arm 38 supported for pivotal displacement on a hydraulic lash adjuster 40. The camshaft 35, rocker arm 38 and hydraulic lash adjuster 40 form a mechanical valvetrain assembly. A simplified hydraulic valve actuation mechanism 30 is schematically illustrated for simplicity and includes a housing defining a fluid chamber 42 housing a piston 44 engaged with the first valve 32, a fluid inlet 46 selectively in communication with the fluid chamber 42 via a first control valve 48 and a fluid outlet 50 selectively in communication with the fluid chamber 42 via a second control valve 52.
The first lubrication system 20 may include a first pump 54 in communication with a fluid reservoir 56 containing a first fluid and passages defined by the engine block 24. More specifically, the fluid reservoir 56 may include an engine oil pan 58 and the first fluid may include engine oil. The first pump 54 may provide the engine oil to main bearings 60 rotationally supporting the crankshaft 16. The second lubrication system 22 may provide a second fluid to the valvetrain assembly 18. The second lubrication system 22 may be isolated from the first lubrication system 20 and the second fluid may be different from the first fluid. By way of non-limiting example, the second fluid may include engine oil having a greater density than the first fluid.
As seen in
The second lubrication system 22 may from a closed loop system with a pump outlet of the second pump 62 providing pressurized fluid (second fluid) to the supply rail 66 via the supply line 64 and the fluid manifold 76. A pump inlet of the second pump 62 may receive the second fluid after the second fluid passes through the valvetrain assembly 18.
During engine operation, the first control valve 48 may allow communication between the pressurized second fluid from the supply rail 66 via the fluid inlet 46 and the fluid chamber 42 to selectively displace the first valve 32 to an open position. The first valve 32 may be displaced to a closed position by closing the first control valve 48 and opening the second control valve 52.
The fluid outlet 50 may be in communication with a pressurized fluid reservoir 86 defined in the cylinder head. When the second control valve 52 is in the open position, the fluid chamber 42 may be in communication with the pressurized fluid reservoir 86 via the fluid outlet 50 and the valve spring 88 may displace the first valve 32 to a closed position, exhausting the second fluid within the fluid chamber 42 to the pressurized fluid reservoir 86 via a first passage 90 defined in the cylinder head 28. The second fluid within the supply rail 66 may be at a first operating pressure and the second fluid within the pressurized fluid reservoir 86 may be at a second operating pressure less than the first operating pressure. The first operating pressure may be at least ten times the second operating pressure. By way of non-limiting example, the second operating pressure may remain at least five hundred kilopascal (500 kPa) within the pressurized fluid reservoir 86 and the first operating pressure may be greater than five thousand kilopascal (5,000 kPa).
The cylinder head 28 may define a second passage 92 from the pressurized fluid reservoir 86 to a hydraulic lash adjuster bore 94 housing the hydraulic lash adjuster 40 and a third passage 96 in communication with the pressurized fluid reservoir 86 (via the second passage 92) and the cam bearing region 37. The second fluid exiting the second and third passages 92, 96 may ultimately be collected in the fluid reservoir 80. The fluid reservoir 80 may contain the second fluid at approximately atmospheric pressure.
As seen in
The lift pump 78 may draw the second fluid from the fluid reservoir 80 and pump the second fluid to the fluid manifold 76 and ultimately return the second fluid to the second pump 62. The return flow path from the fluid manifold 76 to the second pump 62 may include the second fluid travelling from the fluid manifold 76 to the oil cooler 72 and oil filter 74 via the first return line 68 and then to the second pump 62 via the second return line 70.
As indicated above and seen in
As schematically illustrated in
The third seal 110 may form an annular lip seal located in an annular recess defined by the cylinder head 28 and a cam bearing cap 112. An L-shaped bracket 114 may be fixed within the annular recess defined by the cylinder head 28 and the cam bearing cap 112 and the third seal 110 may be engaged with the bracket 114 and an outer circumference of the camshaft 35 to further isolate the first and second lubrication systems 20, 22 from one another. A passage 116 may be located in the cylinder head 28 and may extend from the annular recess defined by the cylinder head 28 and the cam bearing cap 112 to a region of the second lubrication system 22 to allow trapped oil to drain back to the second lubrication system 22.
Number | Name | Date | Kind |
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5195474 | Urata et al. | Mar 1993 | A |
5709186 | Taue | Jan 1998 | A |
6899070 | Neal | May 2005 | B2 |
7162996 | Yang | Jan 2007 | B2 |
Entry |
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Vasilash, Gary S., Automotive Design Production—Powertrain: Designing, Engineering and Producing, Field Guide for Automotive Management, Mar./Apr. 2011, 2 pages. |
Number | Date | Country | |
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20130042826 A1 | Feb 2013 | US |