This application is the U.S. National Phase of PCT Application No. PCT/DE2019/100005 filed on Jan. 7, 2019 which claims priority to DE 10 2018 101 868.1 filed on Jan. 29, 2018, the entire disclosures of which are incorporated by reference herein.
This disclosure relates to a switchable rocker lever for a valve drive of an internal combustion engine.
A generic rocker lever is known from FIGS. 1 to 6 of US2013/0146008 A1. The rocker lever is constructed in the form of a case and has at one end a pivot axle, on which the inner and outer lever rest. At a lower side at one end, the outer lever has two gas exchange valve abutments. At the other end, the outer lever has two support faces for support elements at the lower side thereof. As shown in FIG. 5 in this instance, there are located, when viewed in the lever longitudinal direction from one end to the other, behind the support faces transversely extending coupling sliding means and in front of the support faces (see also FIGS. 2, 3) a vertically installed helical pressure spring as a cam return resilient means. The helical pressure spring rests in a pocket-like protrusion above the upper side of the inner lever and acts with the lower end thereof on a collar-like shoulder of the outer lever below the lower side.
Another rocker lever, in this instance in the form of a cam profile switching rocker lever is disclosed in DE 10 2005 048 984 A1. The cam return resilient means thereof which is constructed in an upright manner (helical pressure spring), also called the lost motion spring, is located in this instance at one end on the valve shaft abutment. The helical pressure spring is clamped between a cantilever arm of the inner lever protruding from the upper side and a crossbeam of the outer lever. In order to displace the coupling sliding means in one direction, a hydraulic medium pressure is used.
It is disadvantageous with the last rocker lever mentioned above that the helical pressure spring abuts the free pivot end of the rocker lever. Consequently, the mass inertia is unnecessarily increased. On the other hand, the helical pressure spring does not have sufficient guiding and fixing or complex measures have to be taken for this purpose. At the same time, the rocker lever is unnecessarily high at the valve side so that, with current compact internal combustion engines, there may inter alia be collision problems with surrounding components. In addition, it is determined that, as a result of the comparatively short lever arm, an unnecessarily strong helical pressure spring has to be constructed.
In addition, reference may be made to DE 102 20 904 A1. Between the lever components visible, for example, in FIG. 3, two upright helical pressure springs act on the other end at the support face of the inner lever. The helical pressure springs are constructed at the side of the support face.
Other switchable rocker levers with upright helical pressure springs can be seen in documents DE 10 2010 011 421 A1, DE 101 37 490 A1 and EP 2 050 933 A1.
An object is to produce a compact and simply constructed and easy-to-assemble switchable rocker lever.
According to the disclosure, this object is achieved in that the coupling extends directly above the support face. The helical pressure spring, when viewed in the lever longitudinal direction from one end to the other, is guided in a receptacle in the inner lever which is located directly and completely in front of the support face. The receptacle is constructed as a bore and one end of the helical pressure spring abuts a base or annular collar of the bore facing the lower side. Another end of the helical pressure spring acts against a curved crossbar which connects the arms of the outer lever at the upper side. The crossbar is guided in two diametrically opposed longitudinal slots of the inner lever which intersect with the receptacle. When the curved crossbar abuts the base of the longitudinal slots, the outer lever is subjected to an outward rotational limitation with respect to the inner lever in the uncoupling mode.
Consequently, a rocker lever is provided without the above-mentioned disadvantages. The vertical helical pressure spring extends directly at the pivot center of the rocker lever in a bore or similar type of opening. At the same time, the spring is subjected to a simple guiding and support. The lever additionally takes up little structural height and, as a result of the transversely extending coupling which is accommodated above the support face, less structural length.
Consideration is given particularly but not exclusively as the support face to a dome-shaped formation in the lower side of the inner lever, via which the rocker lever can be supported on a head of a support element. However, a rotary articulation or the like is also conceivable in this instance.
The helical pressure spring is additionally clamped in a very simple manner and rests with the lower end thereof on a base or an annular collar of the bore thereof in the internal element. Where applicable, the bore may also be continuous and a subsequently applied securing ring or the like is provided as a lower abutment. The upper clamping of the cam return spring (lost motion spring) is advantageously carried out at a lower side of a curved crossbar of the outer lever, which curved crossbar extends from the arms thereof and spans the upper side of the inner lever. In this instance, the curved crossbar is guided in longitudinal slots of the inner lever in the bore and is subjected to an abutment against base faces of the longitudinal slots. Consequently, structural height is saved. At the same time, there is an additional lateral guiding of the two lever portions and a simple outward rotational limitation of the outer lever with respect to the inner lever in the uncoupling mode is provided.
In order to act on the coupling which extends transversely above the support face, an external means, such as, for example, an electromagnetic servo means, in at least one displacement direction of the total of at least two pins may advantageously be considered as the coupling. To this end, a direct action of an actuator on an outer end face of the second pin which rests in the bore of the outer lever is conceivable and provided. Alternatively, the second pin may also be contacted, for example, by a transmission member such as a resilient tongue which is connected to a centrally electromagnetically operated sliding rail in the cylinder head.
A restoration of the pin bundle in the inner and outer lever can be carried out by means of pressure spring force when the cam passes through the base circle, the pressure spring being arranged in front of the first pin or surrounding it. Alternatively, both displacement movements of the pin bundle can also be carried out by means of an electromagnetic servo means.
In the drawings:
The rocker lever 1 has a box-like outer lever 2, between the arms 3 of which there is located an inner lever 4 in a pivotably movable manner relative thereto. In this instance, the outer lever 2 has at an upper side 11 two cam contact surfaces 12 which are provided as sliding interfaces for high-lift cams. The inner lever 4 in contrast has a roller as a cam contact surface 27 for a low-lift cam.
The outer and inner levers 2, 4 rest on a pivot axle 5 at one end 8 thereof. At a lower side 7 of the inner lever 4 (see
Furthermore, in
For selective coupling/uncoupling of the two levers 2, 4 from each other, there is provided a transversely extending coupling 6, which is located directly above the support face 10. In this instance, the inner lever 4 has a continuous main bore 15 with a first pin 17 which extends continuously from bore end to bore end. The first pin 17, as can be seen more clearly in
The above-mentioned main bore 15, which is stepped in order to provide a single-ended abutment for the return guiding means 29, is in alignment in a non-pivoted basic position from the inner to the outer lever 4, 2 (cam base circle passage) with a continuous auxiliary bore 16 in the arms 3 of the outer lever 2. In the auxiliary bore 16 depicted on the right in
As can be seen in
A coupling of the two lever portions 2, 4 is carried out in a well-known manner at the cam base circle passage, at which the lever portions 2, 4 are “unclamped” and the main and auxiliary bores 15, 16 thereof are in alignment with each other so that, when the additional pin 18 is acted on externally, it engages partially in the main bore 15 and in this instance displaces the first pin 17 partially into the auxiliary bore 16 of the left arm 3 which is depicted on the left in
Number | Date | Country | Kind |
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10 2018 101 868.1 | Jan 2018 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/DE2019/100005 | 1/7/2019 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2019/144985 | 8/1/2019 | WO | A |
Number | Name | Date | Kind |
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7201126 | Seitz | Apr 2007 | B1 |
20010023675 | Lee et al. | Sep 2001 | A1 |
20030209216 | Kreuter | Nov 2003 | A1 |
20040206324 | Artmann | Oct 2004 | A1 |
20100236508 | Kang | Sep 2010 | A1 |
20130146008 | Stoody | Jun 2013 | A1 |
Number | Date | Country |
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10137490 | Feb 2003 | DE |
10220904 | Nov 2003 | DE |
102004029555 | Jan 2006 | DE |
102005048984 | Apr 2007 | DE |
102010011421 | Sep 2010 | DE |
102014108598 | Dec 2015 | DE |
2050933 | Apr 2009 | EP |
2013067506 | May 2013 | WO |
Number | Date | Country | |
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20210115818 A1 | Apr 2021 | US |