The present disclosure relates to engine positive crankcase ventilation 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. A portion of the combustion gases (blowby) may escape the combustion chamber past the piston and enter the engine crankcase. Crankcase ventilation systems may be incorporated into engines in order to mitigate the effects of blowby gases in the crankcase.
An engine assembly may include an engine structure, an air intake assembly and a positive crankcase ventilation system. The engine structure may define an intake port and a crankcase. Furthermore, the air intake assembly may be in communication with the intake port. The positive crankcase ventilation system may include a fresh air line, a housing and a foul air line. The fresh air line may be in communication with the air intake assembly and the crankcase. The housing may define an air inlet and an air outlet with the air inlet being in communication with the crankcase and partially defined by a wall extending into an inner volume of the housing. An oil separation mechanism may be located in the housing between the air inlet and the air outlet. The foul air line may be in communication with the air intake assembly and the air outlet.
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.
With reference to
The valvetrain assembly 22 may include a camshaft 32, intake and exhaust valves 34, 36, and a valve actuation assembly 38. The camshaft 32 may include intake and exhaust lobes 40, 42. The valve actuation assembly 38 may be engaged with the intake and exhaust lobes 40, 42 and the intake and exhaust valves 34, 36 to selectively open the intake and exhaust valves 34, 36. The valve actuation assembly 38 may include valve lift mechanisms 44 and rocker arms 46. The valve lift mechanisms 44 may each include a pushrod 48 engaged with the rocker arm 46 and a lifter 50 engaged with the camshaft 32.
The engine assembly 10 may additionally include an air intake assembly 52 and a positive crankcase ventilation (PCV) system 54. The air intake assembly 52 may include an air induction system 56 in communication with a fresh air supply (A) and an intake manifold 58 in communication with the air induction system 56 via a throttle body 60. The PCV system 54 may include a PCV air-oil separator 62, a fresh air line 64 and a foul air line 68. The fresh air line 64 may be in communication with the engine crankcase 70 and the air intake assembly 52. In the present non-limiting example, the PCV air-oil separator 62 is located in a valley of the engine block 24 between the first and second banks 28, 30 and the fresh air line 64 extends from the cylinder head cover 72 to the air induction system 56. The fresh air line 64 may be in communication with the crankcase 70 through passages (not shown) in the cylinder heads 26 and may provide fresh air flow into the crankcase 70.
The foul air line 68 may be in communication with the PCV air-oil separator 62 and the air intake assembly 52. In the present non-limiting example, the foul air line 68 extends from the PCV air-oil separator 62 to the intake manifold 58. With additional reference to
The passages 84 may be similar to one another. Therefore, a single passage 84 will be described with the understanding that the description applies equally to each of the passage 84. The passage 84 may provide blowby gas flow from the crankcase 70 to the foul air line 68 while allowing oil separated from the blowby flow to drain back to the crankcase 70. Therefore, the passage 84 may form an air inlet to the housing 74 and an oil drain passage.
The lower portion 86 may be located above the crankcase 70 and the passage 84 may face the crankcase 70. The passage 84 may be defined by a wall 88 extending into an inner volume of the housing 74. More specifically, the wall 88 may extend into the second region 80 above a lower interior surface 90 of the lower portion 86, defining an end 92 of the wall 88 within the second region 80. The wall 88 may extend into the second region 80 at an angle (θ) of between thirty and forty degrees relative to the lower portion 86 of the housing 74 and may form upper surface of the passage 84. In the present non-limiting example, the angle (θ) is approximately thirty-three degrees. The wall 88 may extend at a first perimeter region 94 of the passage 84 and a second perimeter region 96 of the passage 84 may terminate at the lower interior surface 90 of the lower portion 86.
During engine operation, blowby gas may flow from the crankcase 70 through the passage 84 at the first perimeter region 94 adjacent to the wall 88. Oil may be separated from the blowby gas flow by the air-oil separation mechanism 76 and may accumulate in the lower portion 86 of the PCV air-oil separator 62. The oil may drain back to the crankcase 70 via a return flow path defined at the second perimeter region 96 of the passage 84. The orientation of the wall 88 may result in a maximum air flow velocity being defined adjacent to the wall 88. With the maximum air flow velocity located adjacent to the wall 88, oil may drain to the crankcase 70 via the passage 84 at a location opposite the wall 88 without encountering the high air flow velocity that may otherwise inhibit oil flow through the passage 84.
This application claims the benefit of U.S. Provisional Application No. 61/492,848, filed on Jun. 3, 2011. The entire disclosure of the above application is incorporated herein by reference.
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Number | Date | Country | |
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20120304971 A1 | Dec 2012 | US |
Number | Date | Country | |
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61492848 | Jun 2011 | US |