This application provides an overhead solenoid arrangement, an actuation lever arrangement, a switching rocker arm arrangement, and methods for their use including methods for minimizing the mechanical resistance at the solenoid, methods for commanding switching of the solenoid while the rocker arm is on lift, and methods for varying the triggering timing for the valvetrain.
A switching roller finger follower or rocker arm allows for control of valve actuation by alternating between two or more states. In some examples, the rocker arm can include multiple arms, such as an inner arm and an outer arm. In some circumstances, these arms can engage different cam lobes, such as low-lift lobes, high-lift lobes, and no-lift lobes. Mechanisms are required for switching rocker arm modes in a manner suited for operation of internal combustion engines.
The switching mechanisms must fit into a tight compartment and it is challenging to arrange the switching mechanisms according to all customer constraints. Particularly, it has been difficult to fit electrification equipment into the engine compartment.
The background description provided herein is for the purpose of generally presenting the context of the disclosure. Work of the presently named inventors, to the extent it is described in this background section, as well as aspects of the description that may not otherwise qualify as prior art at the time of filing, are neither expressly nor impliedly admitted as prior art against the present disclosure.
In the context of cylinder deactivation actuation, the time “window” allowed for switching between activated and deactivate modes is dependent on engine speed. However, solenoid response time is independent of engine speed. If the solenoid were to be triggered at a constant point in the engine cycle, it would complete its motion at a different point in the engine cycle depending on speed. So, it is desired to vary the timing for the solenoid triggering so that the actual motion of the solenoid comports with the desired valve actuation.
The inventors have also discovered a timing for triggering the solenoid that ultimately permits reduction in the mass of the solenoid. Alternative compliance spring arrangements, alternative actuator assemblies, and various latches and rocker arms are compatible with the timing technique. The smaller solenoid is better suited to install directly over the rocker arm or arms on which it is acting. This fits the engine compartment footprint efficiently. And, the solenoid is direct-acting. Additional benefits can accumulate because the relationship among the solenoid, actuator assembly and rocker arm is calibratable. Gap settings and variances are tighter through alignment techniques.
Systems, methods, and control systems for a switching rocker arm assembly are disclosed. A switching rocker arm engages a valve, the switching rocker arm is movable by contact with a cam having a lift portion and a base circle. The switching rocker arm comprises an inner arm, an outer arm pivotably secured to the inner arm and having a latch bore, and a latch pin selectively movable between a first position where the latch pin does not contact the inner arm, and a second position wherein the latch pin contacts the inner arm. A solenoid assembly is energized while the rocker arm is in contact with the lift portion of the cam. The solenoid assembly is direct-acting and overhead and is calibratable with respect to the rocker arm. Actuating the solenoid as disclosed leads to the switching of the switchable rocker arm occurring on base circle such that the latch pin moves to the first position where the latch pin does not contact the inner arm
The switching rocker arm can comprise a latch pin and a latch lever extending from the latch pin. With the solenoid assembly overhead, new actuation levers have been developed. So, a switching rocker arm assembly can comprise an actuation lever that is selectively movable into contact with the latch lever, the latch lever configured to urge the latch pin into the second position when the actuation lever contacts the latch lever. The actuation lever can comprise a spring-loaded hinge, and energizing the solenoid while the rocker arm is in contact with the lift portion of the cam can result in the spring-loaded hinge being pre-loaded so that the actuation lever acts on the latch lever to urge the latch pin into the second position as the cam rotates from the lift portion to base circle.
The solenoid assembly can be an electromechanical solenoid and can comprise an armature biased by at least one compliance spring out of the solenoid assembly. The actuation lever extending between the solenoid assembly and the switching rocker arm can alternatively or additionally comprise a linkage between the armature and the actuation lever comprising a pin in a slot. The slot can be tailored to control actuation forces for moving the actuation lever and the latch pin. The slot can vary between an oblong “pill” shape and a curved shape such as a crescent.
When applying methods for switching the switchable rocker arm assembly, several alternatives are available. The methods can comprise processing engine speed data to select a timing of triggering for the solenoid assembly to energize, and adjusting the timing of triggering of the solenoid assembly as the engine speed data indicates a change in engine speed. The methods can comprise determining an operating temperature of the system; determining a voltage available to the solenoid in the system; determining a timing of triggering of the solenoid based on the determined temperature and voltage; and commanding the solenoid to trigger based on the determined timing. Control hardware and stored programming can enable the methods, and a storage device of the control hardware can further comprise a look-up table (“LUT”) that corresponds to a given engine speed. Additional data such as temperature data can be collected and correlated to the LUT. The methods can vary the valve actuation timing for variable valve actuation techniques such as cylinder deactivation (CDA), internal exhaust gas recirculation (iEGR, reverse breathing, rebreathing), Negative Valve Overlap (NVO), early or late valve opening or closing techniques (EEVO, EIVO, EIVC, EEVC, LIVO, LEVO, LIVC, LEVC), engine braking (EB, CRB), among the many alternative variable lift events. So, the timing of triggering determined relative to a sequence of a first, a second and a third lift event, and wherein determining the timing comprises determining a preferred timing such that switching of a rocker arm associated with the solenoid concludes subsequent to the second lift event.
The rocker arm can include design features for variable lift as can the cam lobe associated with rocker arm. While a type II end pivot rocker arm is shown in the drawings, the assembly is not limited thereto. Other latched rocker arms can benefit from the overhead solenoid and actuation levers disclosed herein.
A control system can be implemented for operating an electro-mechanical valvetrain cylinder deactivation system. The control system can comprise a switching rocker arm having an inner arm, an outer arm and a latch pin selectively movable between a first position where the latch pin does not contact the inner arm, and a second position wherein the latch pin contacts the inner arm. A solenoid assembly connected to the control system can be triggered by the control system, resulting in selective actuation of the latch pin. A controller determines a timing of the triggering of the solenoid assembly based on a temperature and a voltage of the electro-mechanical valvetrain cylinder deactivation system.
Additional objects and advantages will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the disclosure. The objects and advantages will also be realized and attained by means of the elements and combinations particularly pointed out in the appended claims.
Reference will now be made in detail to the examples which are illustrated in the accompanying drawings. Directional references such as “left” and “right” are for ease of reference to the figures and are not limiting of the invention in its practical installation. Overhead, however, can be construed as being atop the rocker arm assembly and as pertains the solenoid assembly, overhead can be construed as the armature arranged to actuate substantially transverse to the latch pin.
The plate 700 can be aligned relative to the rocker arms 10 as by a calibratable alignment of mounting pins 701, which improves the accuracy of the actuation of the valves 29. For example, the mounting pins 701 can be aligned with the engine block or a carrier 704 comprising cam rail mount or both. A first alignment nut or bushing 702 can be welded or tightened to secure the tower with respect to the engine block and cam rail mount 704. But, the mounting plate 700 can comprise holes surrounding top ends of mounting pins 701. The holes can comprise an amount of “play” or variance such that the solenoid assembly 500 can be moved relative to the cam shaft 61 and switching rocker arms 10. A gage or other calibration device can be used to set the location of the solenoid assembly 500 relative to the rocker arms 10. Or, the actuation lever 400 can be the aligned relative to the rocker arms 10, particularly relative to the latch pin 28 and latch lever 30. Mounting pins 701 can be locked in place once the alignment technique is completed.
In an alternative, bushing 702 can be aligned via a gage or other alignment tool in an alignment slot of plate 700. The bushing can be secured as by welding, tightening or the like to the carrier 704, which carrier also serves as a base for the solenoid assembly when the carrier 704 is aligned with the cylinder head, which has the rocker arms 10 aligned thereto, the solenoid assembly 500 is aligned, the actuation arm is aligned, and the contact gap 92, 94 is constrained. An alignment pin of the cylinder head can protrude through the bushing 702. The carrier can comprise one or more alignment slots with corresponding aligned bushing 702.
In
The solenoid assembly 500 is direct-acting and overhead and is calibratable and alignable with respect to the switching rocker arm 10. In
In
The solenoid assembly 500 can be energized while the rocker arm 10 is in contact with the lift portion 56 of the cam 60. Actuating the solenoid as disclosed leads to the switching of the switchable rocker arm 10 occurring on base circle 58 such that the latch pin 28 moves to the first position where the latch pin does not contact the inner arm 20. Preloading the actuation lever 400 while the valve 29 is on lift and the lift portion 56 is in contact with the roller 23 yields benefits in downsizing the solenoid. The spring 68 in the spring-hinge provides actuation force to move the latch pin 28 in a complementary manner to the forces from the solenoid assembly 500. With the additive force from the compliance spring 68, the coil 51 of the solenoid can be smaller and less powerful. This leads to energy, heat, and space savings. With the valve on lift, the force on the latch pin 28 is initially too great to disengage the latch end 280 from the inner arm ledge 24, but as the cam 60 rotates to base circle 56 from the lift portion 58, the force on the roller 23 and inner arm 20 reduces and the latch pin 28 can slide in the latch bore 281 as the paddle 455 of actuation lever 400 acts on latch lever 30 to pivot the latch lever 30. A pivot pin 102 or stake can be used to mount latch lever 30 to the rocker arm 10 in a pivoting relationship.
The solenoid assembly can be an electromechanical solenoid and can comprise an armature 54 biased by at least one compliance spring 67, 65, 68, 69 out of the solenoid assembly 500. The actuation lever 40, 400 extending between the solenoid assembly 500 and the switching rocker arm 10 can alternatively or additionally comprise a linkage between the armature 53, 54 and the actuation lever 40, 400 comprising a pin 101, 103 in a slot 45, 87, 403, 403. The slot can be tailored to control actuation forces for moving the actuation lever 40, 400 and the latch pin 28. The slot can vary between an oblong “pill” shape and a curved shape such as a crescent, as shown in
The compliance springs 65, 67, 68, 69 can perform several functions, including biasing the armature out of the solenoid to ensure normal operation is always available as a default mode; reduction of assembly stack up as by creating a nominal contact gap between the actuation lever 40, 400 and the latch pin assembly; assisting with setting a precise contact gap as by a feeler gauge; setting the triggering timing as by providing a consistent gap for the extent that the armature extends from the solenoid assembly; storing energy used for pulling the latch pin 28 out of the rocker arm 10.
Actuation lever 400 can comprise a first actuation arm 401 and a second actuation arm 450. First actuation arm 401 can comprise the slot 403, 87 for interfacing the linkage end 55 of the armature and linkage pin 103. The second actuation arm 450 is designed to move as a spring-loaded hinge. So, a second linkage pin 104 can join a pivot point 402 of the first actuation arm 401 with a pivot point 453 of the second actuation arm 450 with the compliance spring 68 coiled or otherwise seated in cup 405. When the compliance spring 68 is a torsion spring, it can be coiled around the second linkage pin 104. Other springs like leaf springs can be appropriately mounted. Compliance spring 68 has a spring end 682 pressing against first actuation arm 401 and a spring end 681 pressing against second actuation arm 450; compliance spring 68 can maintain minimum contacts therebetween. Spring end 681 can pass through a window 452 in second actuation arm 450. A torsional spring or leaf spring or the like can be used and arranged to bias the second actuation arm 450. A pressure point formed at stake 451 and seat 406 yields a hinge location. Linkage end 454 of second actuation arm 450 is positioned relative to pivot point 453 and stake 451 in seat 406. Paddle end 455 of second actuation arm 450 swings as the solenoid assembly 500 draws the armature 54 or releases the armature. When there is a gap 92 or 94, the paddle end 455 receives no pressure other than the spring pressure from spring end 682. But when the paddle end 455 contacts the latch lever 30, the second actuation arm 450 can hinge and put pressure on the compliance spring 68, which stores energy in the compliance spring 68 for moving the latch pin 28. As disclosed, one technique for moving the latch pin is to trigger the solenoid when the valve is on lift, which yields a situation where the latch pin 28 is receiving too much force to move. So if the paddle pushes against the latch lever 30, it causes a hinging force and loading of the compliance spring 68. The force stored in the spring can be released to act on the latch pin 28 when the valve comes off lift as detailed herein.
While the actuation lever 400 comprises two actuation arms and two pivot points (linkage and hinge), the actuation lever 40 is a contiguous piece that comprises two pivot points. The actuation lever 40 comprises a controlled slot 45 that can be shaped as oblong 87 or crescent 403 as in
With reference to
A latch pin lever 30 extends from the latch 28 and is arranged to be engaged by an actuation lever 40. A solenoid coil 50 energizes causing an armature 52 to move to close a gap 90. That is, the armature 52 is drawn into the solenoid assembly 500 when the coil 50 is energized, which lifts the actuation lever 40 and cants the actuation lever to press the paddle 42 into contact with the latch lever 30. As will become appreciated from the following discussion, the solenoid coil 50 is energized while the valve 29 is on lift (corresponding to cam lobe or lift portion 56 on cam 60). By switching on valve lift (rather than on the base circle 58 of the cam 60), mechanical resistance on the solenoid assembly is minimized. The compliance springs 67, 66 and latch spring 26 are reducing the available force provided by the solenoid assembly, but the actuation lever 40 is designed to increase the available force. The solenoid coil 50 has the highest force when the motion of the armature 52 is complete (such as 50N for example) as compared to 15N when the solenoid coil 50 is first energized.
Turning now to
Returning now to
The latch 28 is moved to the retracted position such as to transition from lift to cylinder deactivation. Turning to
The instant disclosure further provides a method for triggering the solenoid coil 50, 51 in an electro-mechanical cylinder deactivation valvetrain system or other variable valve actuation valvetrain at a variable time within the engine cycle as a function of temperature, voltage, and engine speed. The method maximizes the available force in the solenoid assembly 500 and allows for switching in a consistent manner regardless of solenoid response time. In general, the force available in an electro-mechanical solenoid depends on temperature and voltage. This has a significant effect on both the solenoid's ability to successfully perform the intended function as well as the response time it takes to complete that function.
Since the force available in the solenoid assembly 500 varies, there are certain combinations of temperature and voltage that require the solenoid motion to occur while the valve 29 is “on lift” because the rocker arm 10 moves out of the way at this point in the cycle, allowing the actuation mechanism 40, 400 to move with very little mechanical resistance. Such cases also require early pre-triggering of the solenoid 50 to begin building force before the valve 29 goes on lift in order to successfully complete its motion. However, for other combinations of temperature and voltage where the available force is significantly higher, triggering this early may result in unintended movement or partial disengagement of the rocker arm latch 24, which could result in mis-shifting or critical shifting between cylinder activated and deactivated modes. In this regard, the resistance in the solenoid assembly 500 changes as a function of temperature, and as a function of changes of voltage (e.g., battery in the vehicle). As the resistance varies, the amount of force the solenoid assembly is able to generate also varies. As a result, the timing of solenoid triggering is a function of temperature and voltage. Furthermore, engine speed will impact proper timing of the solenoid triggering.
As will become appreciated herein, the present teachings provide methods for triggering the solenoid coil 50, 51 at a variable point in the engine cycle such that it completes its motion at the appropriate time. The triggering timing is determined by way of analytical simulations (and physical testing) of the actuation system. The response time of the solenoid assembly 500 at various operating points is predicted. Further, the methods determine whether switching “on lift” would be required to successfully complete actuation. A series of maps of triggering timings are generated. The maps can be further adjusted as a function of engine speed to match up time with crank angle position.
Plots can be created and correlated to lookup tables to algorithmically correlate solenoid force versus temperature and voltage. Such can be correlated to the size of the solenoid air gap. And discrepancy between minimum and maximum force and air gap sized can be accounted for in the control system. Force changes to close various sized gaps can be programmed in the control system with corresponding methods for implementations so that as temperature and voltage change, the air gap can be closed while the valve is on lift.
Trigger timings can be established.
However, as discussed above, it is possible to have variability in the WA techniques. By triggering the solenoid assembly 500 at different timings, different valve lift techniques can be achieved. For example, at first engine speed, an early exhaust valve opening can be implemented and at a second engine speed, an earlier or later exhaust valve opening can be implemented relative to the first early exhaust valve opening. So, the triggering timing can be thought of as a range 140, as shown in
By mapping latch pin motion versus time at various voltage/temperature combinations, the triggering timing can be established. Switching the rocker arm 10 ideally occurs before the second lift event 134 of
Mapping valve displacement lift versus time can also be mapped to establish triggering timing. A trigger window 140 (range) for triggering the solenoid assembly 50, 500 can be established. The trigger window 140 can yield latch pin motion at a time “x” before a third lift 150. According to the present teachings, a plurality of variable trigger timing maps are determined and stored in an engine control unit for a plurality of engine speeds.
Variable trigger timing can result in instances where switching occurs during the second lift event 134, or instances where the switching occurs subsequent to the second lift event 134. No “in between” cases of significant partial un-latching events occur when the solenoid assembly is triggered on lift just prior to a cam cycle requiring the latch pin in the first position. As a result, the risk of mis-shifts and critical shifts are minimized.
The methods disclosed herein select the timing of the triggering of the solenoid assembly as a function of system response time such that triggering consistently occurs at an optimal time regardless of operating conditions.
A control system can be implemented for operating an electro-mechanical valvetrain system in a variable valve actuation technique such as cylinder deactivation, among others. The control system can comprise a switching rocker arm such as a triple roller rocker arm, a slider type rocker arm, a roller finger follower, among other rocker arms. As illustrated the rocker arm has at least an inner arm, an outer arm and a latch pin selectively movable between a first position where the latch pin does not contact the inner arm, and a second position wherein the latch pin contacts the inner arm. A solenoid assembly connected to the control system can be triggered by the control system, resulting in selective actuation of the latch pin. A controller such as ECU 220 determines a timing of the triggering of the solenoid assembly 500 based on a temperature T on line 222 and a voltage V on line 224 of the electro-mechanical WA valvetrain system. The Temperature T, Voltage V, Engine Speed ES can be measured by sensors or solved for. But, ECU 220 collects necessary inputs on lines 222, 224, 226. A processor in ECU 220 can process collected data algorithmically using stored programming.
The control system of
Other implementations will be apparent to those skilled in the art from consideration of the specification and practice of the examples disclosed herein.
This is a § 371 National Stage Entry of Patent Cooperation Treaty Application No. PCT/EP2019/025293, filed Sep. 3, 2019 which claims the benefit of U.S. provisional application No. 62/744,674, filed Oct. 12, 2018, and which claims the benefit of U.S. provisional application 62/726,954 filed Sep. 4, 2018 all of which are incorporated herein by reference.
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PCT/EP2019/025293 | 9/3/2019 | WO |
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WO2020/048639 | 3/12/2020 | WO | A |
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Number | Date | Country | |
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