This disclosure generally relates to a system for controlling cylinder deactivation (CDA), and more particularly to a CDA lifter having hydraulic control feed from outside of an engine block.
Various lifter designs have been produced in the past for use in valvetrain systems of an internal combustion engine. Generally, such lifter is coupled to a camshaft on one side and to an engine cylinder on the other side in a way for delivering actuation motion from the camshaft to downstream valves located in the cylinder. Independent cylinder control for cylinder deactivation—that is, selected cylinder combination may be disabled by deactivating the valves in those cylinders—is highly desirable especially for multi-cylinder engine, for example, in order to better adjust engine and/or fuel efficiency on demand. Typically, in a lifter constructed to achieve such CDA function, hydraulic switching components (e.g., latching mechanism) are usually employed, which, in operation, may rapidly shift the system from activation mode (i.e., valve actuation motion provided by the camshaft is allowed to be delivered to the cylinder) to deactivation mode (e.g., motion originated from the camshaft is absorbed by the hydraulic switching components, thus the respective valve is unactuated,) or vice versa as needed. However, this usually requires additional fluid passages that run inside the engine block to feed control pressure to the selected lifter, thus significantly increasing overall system complexity. It also requires extensive machining to recast the engine block to accommodate the complex passage designs, making the construction process costly and time-consuming.
Accordingly, there exists a need to design a simplified system that permits hydraulic control of CDA operation without introducing substantial engine complexity.
The disclosure presents a simplified lifter assembly for controlling CDA operation. In particular, the lifter assembly according to this disclosure utilizes a pin-and-slot combination to both prevent undesired rotational movement of a roller lifter and at the same time enable hydraulic pressure control for CDA operation. The disclosure moreover presents an engine block assembly that houses a lifter of such configurations and is suitable to receive hydraulic control feed from outside.
By feeding control fluid through fluid passages of the anti-rotation slot and pin, the need for additional fluid circuit inside the engine block may be eliminated. Furthermore, since the pin may be mounted from outside the engine block, a hydraulic feed source may be routed externally to the pin for controlling CDA switching. In this way, it may allow simple modification to existing engine condition to fit to CDA requirements, thereby reducing construction cost and program timing.
An embodiment of a lifter assembly according to this disclosure comprises a lifter having a latching mechanism, a slot arranged on an outer wall of the lifter and comprising an inlet that provides access to the latching mechanism, and a pin comprising a fluid channel. In particular, the latching mechanism may be switchable between a latched position and an unlatched position. In the same embodiment, the pin is configured to interface with the slot such that the lifter is prevented from rotation about a lifter axis. Furthermore, the fluid channel is configured to be fluidly coupled to the inlet of the slot.
In particular embodiments, the slot is elongated in shape. In particular embodiments, the slot has a length that is configured to maintain engagement with the pin as the lifter travels in a vertical direction. In particular embodiments, the slot is configured to receive an end of the pin. In particular embodiments, the slot has a width that is slightly larger than an outer diameter of the end of the pin.
In particular embodiments, when the pin interfaces with the slot, a clearance is formed between an end of the pin and a bottom surface of the slot in order to allow fluid communication. In particular embodiments, the inlet is arranged at a bottom surface of the slot. In particular embodiments, the fluid channel is in proximity to the inlet when the lifter is on a base circle position. In particular embodiments, the latching mechanism is configured to switch to the unlatched position by means of fluid pressure supplied via the fluid channel of the pin.
In particular embodiments, the lifter assembly is configured to be housed inside an engine block. In particular embodiments, the pin is configured to be mounted into the engine block from the outside. In particular embodiments, the fluid channel is configured to be fluidly coupled to a fluid supply external to the engine block.
An embodiment of an engine block assembly according to this disclosure comprises an engine block, a lifter assembly housed inside the engine block, and a pin mounted from outside of the engine block and comprising a fluid channel. In particular, the lifter assembly may comprise a lifter having a latching mechanism. The latching mechanism is switchable between a latched position and an unlatched position. Furthermore, the pin is configured to interface with the slot such that the lifter is prevented from rotation about a lifter axis. The fluid channel is configured to be fluidly coupled to the inlet of the slot.
In particular embodiments, the fluid channel is configured to be fluidly coupled to a fluid supply external to the engine block. In particular embodiments, the pin comprises a head that is configured to be mounted against an outer wall of the engine block. In particular embodiments, the pin comprises a body portion that is configured to extend through an outer wall of the engine block. In particular embodiments, the pin comprises an end that is configured to fit into the slot. In particular embodiments, the slot is elongated in shape. In particular embodiments, the slot has a length that is configured to maintain engagement with the pin as the lifter travels in a vertical direction. In particular embodiments, when the pin interfaces with the slot, a clearance is formed between an end of the pin and a bottom surface of the slot in order to allow fluid communication.
Embodiments in accordance with this disclosure will now be described by reference to the accompanying drawings, in which:
Reference will now be made in detail to the examples which are illustrated in the accompanying drawings. Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts. Directional references such as “up”, “down”, “right”, and “left” are for ease of reference to the figures and not intended to limit the scope of this disclosure.
In the illustrated embodiment, the lifter assembly 100 comprises a roller lifter 110 that may ride, at a roller bearing 116 thereof, on a camshaft 114 and is configured to reciprocate in a vertical direction along a lifter axis 118 in a controllable manner upon actuation by camshaft rotation. As depicted, upper portion of the roller lifter 110 may be coupled to a lower end of a push rod 112, while an upper end of the push rod 112 may in turn engage with a rocker arm (not shown). Configured as such, vertical displacement of the roller lifter 110—i.e., by rotation of the camshaft 114—may be conveyed through the push rod 112 to the rocker arm, thereby causing the rocker arm to rotate to activate the associated cylinder as needed.
In particular embodiments, the lifter assembly 100 may be configured for providing so-called CDA functionalities, i.e., a chosen combination of cylinders is systematically disabled, for example, for better fuel economy or overall engine efficiency such that the system may operate on fewer cylinders when less power output is demanded. To this end, the roller lifter 110 may be provided with various switching components to selectively enable and/or disable motion transfer from the camshaft 114 to the rocker arm. For example, the switching components may mechanically switch the roller lifter 110 between a latched mode for cylinder activation and an unlatched mode for cylinder deactivation. Details of the switching components will be described below with reference to
It will be appreciated that the switching components described herein is merely exemplary and not intended to limit the scope of this disclosure. Although the above explains switching of the roller lifter by referencing to particular components, these components are provided for illustration purposes only and are not necessarily a requirement. In some embodiments, one or more components may be omitted from or added to the roller lifter. Other suitable configurations of the roller lifter may be apparent to those skilled in the art and are not explained in exhaustive details by this disclosure.
With continued reference to
In configurations where the lifter assembly 100 is housed by the engine block, the pin 122 may be mounted from outside the engine block. For example, an external wall of the engine block may be modified with a through hole, for example, by drilling, boring or other suitable methods as familiar to those in the art. The pin 122 may be fitted into the through hole and further extend inwards so as to interface with the roller lifter 110. In particular embodiments, the fluid supply such as an oil control valve or other suitable fluid source as familiar to those skilled in the art may be connected to the pin 122 for feeding fluid to the roller lifter 110. As a non-limiting example, the fluid supply may be constructed external to the engine block and optionally comprises a mounting structure that may sit over and fluidly connects to the pin 122. Of course, it will be appreciated that while illustrated as such, the disclosure is not so limited. Other suitable configurations of the fluid supply are also envisioned by this disclosure. For example, a tube or a manifold may be directed to the pin 122 for providing hydraulic feed.
For a conventional system to control cylinder deactivation, an individual fluid circuit is typically required, which is routed inside the engine block to the roller lifter so as to hydraulicly control switching. However, this leads to complex passage designs in the engine architecture and requires recasting and/or redesigning of the engine block, which significantly increases cost and program timing. The design of the lifter assembly 100 according to this disclosure contrasts those of prior art since it incorporates the fluid feed and anti-rotation capabilities into a single pin-and-slot configuration, thereby significantly reducing design complexity of the overall system and making the machining process simpler and more cost effective. Furthermore, by routing the hydraulic control feed external to the engine block, the system disclosed herein eliminates the need of engine recast and enables simple modification to the existing engine condition, thus allowing the engine block to be easily adapted to fit specific customer requirements.
In particular embodiments, the slot 120 may comprise the inlet 230. For example, the inlet 230 may be arranged at the bottom surface of the slot 120 and provide access to interior structures of the roller lifter 110. In one embodiment, the inlet 230 may be positioned in a vertical location that is generally in alignment with the latching mechanism 216 in the latched configuration. In this way, fluid may be communicated through the inlet 230 into the roller lifter 110 to act upon the latching mechanism 216, thereby controlling the switching event.
Herein, “or” is inclusive and not exclusive, unless expressly indicated otherwise or indicated otherwise by context. Therefore, herein, “A or B” means “A, B, or both,” unless expressly indicated otherwise or indicated otherwise by context. Moreover, “and” is both joint and several, unless expressly indicated otherwise or indicated otherwise by context. Therefore, herein, “A and B” means “A and B, jointly or severally,” unless expressly indicated otherwise or indicated otherwise by context.
The scope of this disclosure encompasses all changes, substitutions, variations, alterations, and modifications to the example embodiments described or illustrated herein that a person having ordinary skill in the art would comprehend. The scope of this disclosure is not limited to the example embodiments described or illustrated herein. Moreover, although this disclosure describes and illustrates respective embodiments herein as including particular components, elements, feature, functions, operations, or steps, any of these embodiments may include any combination or permutation of any of the components, elements, features, functions, operations, or steps described or illustrated anywhere herein that a person having ordinary skill in the art would comprehend. Furthermore, reference in the appended claims to an apparatus or system or a component of an apparatus or system being adapted to, arranged to, capable of, configured to, enabled to, operable to, or operative to perform a particular function encompasses that apparatus, system, component, whether or not it or that particular function is activated, turned on, or unlocked, as long as that apparatus, system, or component is so adapted, arranged, capable, configured, enabled, operable, or operative. Additionally, although this disclosure describes or illustrates particular embodiments as providing particular advantages, particular embodiments may provide none, some, or all of these advantages.
This application claims the benefit under 35 U.S.C. § 365 (c) of International Patent Application No. PCT/EP2023/025264, filed 2 Jun. 2023, which claims the benefit of U.S. Provisional Patent Application No. 63/348,632, filed 3 Jun. 2022, each of which is incorporated herein by reference.
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International search report and Written Opinion received for PCT Application No. PCT/EP2023/025264, 8 pages, Sep. 15, 2023. |
Number | Date | Country | |
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20250092804 A1 | Mar 2025 | US |
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63348632 | Jun 2022 | US |
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Parent | PCT/EP2023/025264 | Jun 2023 | WO |
Child | 18962882 | US |