EP1036256B1 - Valve operating lever - Google Patents

Valve operating lever Download PDF

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Publication number
EP1036256B1
EP1036256B1 EP98965707A EP98965707A EP1036256B1 EP 1036256 B1 EP1036256 B1 EP 1036256B1 EP 98965707 A EP98965707 A EP 98965707A EP 98965707 A EP98965707 A EP 98965707A EP 1036256 B1 EP1036256 B1 EP 1036256B1
Authority
EP
European Patent Office
Prior art keywords
tabs
symmetry plane
longitudinal symmetry
actuating lever
valve actuating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP98965707A
Other languages
German (de)
French (fr)
Other versions
EP1036256A1 (en
Inventor
Helmut Engelhardt
Wolfgang Mayer
Johannnes Mayer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bayerische Motoren Werke AG
IHO Holding GmbH and Co KG
Original Assignee
Bayerische Motoren Werke AG
INA Waelzlager Schaeffler OHG
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Filing date
Publication date
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Publication of EP1036256A1 publication Critical patent/EP1036256A1/en
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Publication of EP1036256B1 publication Critical patent/EP1036256B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/12Transmitting gear between valve drive and valve
    • F01L1/18Rocking arms or levers
    • F01L1/185Overhead end-pivot rocking arms
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L2303/00Manufacturing of components used in valve arrangements
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49295Push rod or rocker arm making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20576Elements
    • Y10T74/20882Rocker arms

Definitions

  • the present invention relates to a valve operating lever for transmitting the Movement of a cam arranged on a camshaft onto a gas exchange valve an internal combustion engine.
  • a roller rocker arm of the type in question is by DE 195 43 657 A1 became known.
  • the known valve actuation lever has a U-shaped base body on, at one end a pan-like depression is provided with which the lever supports in the installed state via a support element on the cylinder head. At the other end there is the valve contact area through which the gas exchange valve the internal combustion engine depending on the position of the cam of the camshaft is operated.
  • the cam is in a cam contact area with the valve actuation lever Contact, one in this cam contact area with a roller rocker arm roller is rotatably mounted by rolling elements.
  • the base body of the valve actuation lever is formed without cutting and points to the End at which the valve contact area is provided, inwardly bent tabs which form lateral boundary surfaces.
  • the present invention is therefore based on the object of a valve actuation lever and in particular a roller rocker arm and a method for the same To provide production at which the moment of inertia the lever around the axis of rotation is reduced. Another aspect of this task is it to design the valve actuation lever so that the rigidity against the State of the art increased and low manufacturing costs can be achieved.
  • the valve actuation lever according to the invention has a substantially non-cutting shaped elongated body, preferably with a U-shaped profile.
  • the basic body is essentially symmetrical to itself in its longitudinal direction extending longitudinal plane of symmetry.
  • tabs are arranged in the valve contact area, each one have the side surface facing the longitudinal plane of symmetry.
  • the tabs are on molded onto an end edge of this base body and towards the valve contact area bent.
  • At least one of these tabs points away from this plane of longitudinal symmetry away extending transition area, in which the distance between them Side surfaces enlarged and at least one parallel area in which this Side surfaces run essentially parallel to this longitudinal plane of symmetry.
  • the two tabs are at a clear distance at the end edge of the body arranged, which is less than the clear distance of the side surfaces in the parallel area, this distance in each case in a direction perpendicular to the longitudinal plane of symmetry is determined.
  • the design according to the invention has a number of essential advantages.
  • the distance between the tabs on the end edge of the elongated body is constructive Size, which is the width of the elongated body in the valve contact area certainly. By reducing this distance, the width of the elongated one becomes simultaneously Base body at least in the valve contact area and thereby also its Weight decreased. Because the valve contact area is radial from the axis of rotation of the valve operating lever is spaced, this results in a significant reduction the moment of inertia around the axis of rotation of the lever. With that, the forces required to operate the lever are reduced at the same speed, and it becomes the permissible for the valve train with regard to the actuation forces Speed limit raised.
  • the bending lengths of the lever are also transverse to its longitudinal direction reduced, which can increase the rigidity.
  • the tabs are on the base body the bending process molded in such a way that they are parallel to the plane of longitudinal symmetry extend, d. H. run straight. The bending then takes place in such a way that one or both tabs to form the transition area from the longitudinal plane of symmetry be bent away. At the end of the transition area are the tabs then bent in such a way that the inner plane facing the plane of symmetry Side surface of the tab runs parallel to this.
  • this parallel area can then be used connect yet another constriction area in which one or both tabs are facing the longitudinal plane of symmetry again.
  • the tabs are such punched that the transition area and the parallel area already with the deformed tabs are present.
  • the tabs then only have to be bent through 180 ° and then in the bent state, without further bending, the desired contour in the valve contact area.
  • the first and the second embodiment can also be combined with one another.
  • the flaps are stamped into an initial shape followed by a 180 ° bend and an additional bend brought to the longitudinal symmetry plane or away from it into the final shape.
  • Tabs it is also possible to treat the tabs differently, so that e.g. a Tab is only subjected to a bend of approximately 180 °, while the other tab both this bend and a further bend, in particular to the plane of longitudinal symmetry there or away from it.
  • the initial form of Tabs be the same, e.g. the shape of an elongated cuboid parallel to the plane of longitudinal symmetry corresponding longitudinal edges or different from each other his.
  • Fig. 1 shows a first embodiment of the roller finger follower according to the invention.
  • the roller rocker arm has a base body designated 1 overall, which extends essentially symmetrically along a longitudinal plane of symmetry 2.
  • the term plane of symmetry is not to be understood here in a purely geometrical sense, it simply means that essential areas of the valve actuation lever are designed symmetrically to this plane of symmetry.
  • the plane of symmetry 2 1 runs perpendicular to the plane of the drawing and forms in the 2 the sectional plane.
  • the elongated body is, as can be seen from the illustration in FIG. 3, in designed essentially U-shaped and has a symmetrical to the plane of symmetry 2 extending recess 4 in which a roller 7 mounted on rolling elements 6th is arranged. When installed, the roller 7 stands with the cam of a camshaft in contact.
  • this recess 10 for receiving a Support element (not shown) is provided. When installed this element in turn is supported within the cylinder head (not shown) from.
  • This recess 10 is known in the prior art and therefore need not be discussed further here.
  • valve contact area 20 On the left side of the base body in the illustration according to FIG. 1 there is a valve contact area 20 provided.
  • the valve contact area has a surface 21, which is designed to be slightly convex in the exemplary embodiment, but can also do other things Have curvature shapes or just be designed.
  • the valve contact area is through two, the longitudinal symmetry plane 2 facing limited lateral surfaces 23, 24, which are part of the tabs 25, 26.
  • the tabs 25, 26 are formed on an end edge 30 of the elongate base body 1, the end edge 30 being substantially perpendicular to the plane of symmetry 2.
  • the distance between the tabs 25 and 26 corresponds to this end edge of the base body the length a in Fig. 5 between the arrows 31 and 32 or, in other words, the Tabs 25 and 26 are on the end edge 30 of a web 30a, which has the width c (see Fig. 5) between the arrows 33 and 34, integrally formed.
  • both tabs 25, 26 have a transition region 35, 36 on, in which the tabs away from the plane of symmetry 2 extend.
  • a parallel area 37 adjoins this transition area 35, 36 38 in which both tabs run parallel to the plane of symmetry 2.
  • At the tab 26 is followed by a constriction area 40, in which the tab rests on the Plane of symmetry 2 runs.
  • transition area is therefore defined by the fact that here the angular Alignment of the tab or the side surfaces with respect to the longitudinal plane of symmetry changes.
  • the distance between the two tabs corresponds to the distance b, as shown between arrows 42, 43.
  • This distance b is larger than the distance a.
  • the difference between the two routes essentially corresponds to the width savings of the base body compared to the prior art discussed above.
  • the two tabs 25, 26 are located, in particular the representation according to Figure 2 shows, flush, d. H. without space on which curved surface of the valve contact area 20.
  • the tabs can also in this embodiment be designed in the next embodiment so that between the tabs and a gap is provided on the surface of the valve contact area, the tabs are then shaped so that their end area rests on the valve contact area.
  • the end region in the illustration according to FIG. B. at the tab 26 of the Constriction area 40, with respect to the valve contact area, can be fixed in the first alternative, d. H. with flush-fitting tabs, as well as with the second alternative, d. H. in the case of tabs that are partially at a distance from the valve contact area have at the end of an additional connection, preferably by a spot weld is made.
  • the roller rocker arm shown in the embodiment is a total of one Metal sheet punched out and then preferably cold-formed to the in Fig. 1 to 4 to achieve the final design shown.
  • the tabs 25 and 26 are at Punching as an essentially straight extension of the base body 1 educated. Then, as shown in Fig. 6, they are down (in the illustration seen the drawing) reshaped, the distance between the tabs continues corresponds to the distance a. Then the tabs from the plane of symmetry 2 bent away to form the transition region 35, 36.
  • This bending process is carried out so that the tabs are initially at a first bending angle are bent outwards so that the outwards from the plane of symmetry 2nd forms the first part of the transition region 35, 36 and that adjoins it the tabs bent back in the direction of the plane of symmetry 2 be that the further part of the tabs runs parallel to the line of symmetry 2. Only one or both ends of the tabs, as indicated by 40 in Fig. 1, is again with an inward bending angle, formed on the plane of symmetry 2.
  • this design makes it possible run the valve operating lever with a small width. This becomes significant of material saved, thereby reducing the moment of inertia around the axis of rotation reduced and, with otherwise the same dimensions, the rigidity is increased.
  • this essentially corresponds to that shown in FIG. 8 End product, namely the roller finger follower, essentially as shown Fig. 1. Corresponding reference numerals are therefore also used there.
  • the tabs are here during a punching process immediately formed so that the desired transition area is already during the punching process and not, as in the exemplary embodiment according to FIGS. 1 to 6, results in bending.
  • the tab 51 is on the substantially perpendicular to the plane of symmetry 2 End edge 30 of the base body 1 is formed.
  • the tab 51 has a first Area in which the tab is designated 53 even in the undeformed state forms an acute angle to this end edge 30, whereby one of the longitudinal symmetry plane 2 pointing transition area 54 forms.
  • the transition area 54 is followed by a parallel region 55, which is designed parallel to the plane of longitudinal symmetry and there is an area 56 in which the side surface is at an acute angle to the longitudinal plane of symmetry is directed towards.
  • a parallel region 57 is initially provided, which is parallel to the Longitudinal plane of symmetry 2 runs, to which the transition region 58 then adjoins, in which the tab extends outward from the longitudinal plane of symmetry 2.
  • a further parallel area 59 which is parallel to the longitudinal plane of symmetry 2 extends and which forms the side surface 60.

Description

Die vorliegende Erfindung betrifft einen Ventilbetätigungshebel zur Übertragung der Bewegung eines auf einer Nockenwelle angeordneten Nockens auf ein Gaswechsel-Ventil einer Brennkraftmaschine.The present invention relates to a valve operating lever for transmitting the Movement of a cam arranged on a camshaft onto a gas exchange valve an internal combustion engine.

Die Aufgabe der Erfindung und ihre Lösung werden nachfolgend am Beispiel eines Rollenschlepphebels beschrieben. Es wird darauf hingewiesen, daß diese Beschreibung nicht als Einschränkung der Anwendung der Erfindung zu verstehen ist, es ist vielmehr möglich, die Erfindung auch mit andersartig gestalteten Ventilbetätigungshebeln, wie z. B. mit Kipphebeln oder mit nicht-rollenbetätigten Ventilbetätigungshebeln auszuführen.The object of the invention and its solution are described below using the example of a Roller rocker arm described. It should be noted that this description is not to be construed as limiting the application of the invention, it is rather, the invention is also possible with valve actuation levers of a different design, such as B. with rocker arms or with non-roller-operated valve actuation levers perform.

Ein Rollenschlepphebel der hier in Rede stehenden Art ist durch die DE 195 43 657 A1 bekannt geworden.A roller rocker arm of the type in question is by DE 195 43 657 A1 became known.

Der bekannte Ventil-Betätigungshebel weist einen U-förmig gestalteten Grundkörper auf, an dessen einem Ende eine pfannenartige Vertiefung vorgesehen ist, mit der sich der Hebel im eingebauten Zustand über ein Stützelement am Zylinderkopf abstützt. Am anderen Ende ist der Ventil-Kontaktbereich vorgesehen, durch den das Gaswechsel-Ventil der Brennkraftmaschine in Abhängigkeit der Stellung des Nockens der Nokkenwelle betätigt wird.The known valve actuation lever has a U-shaped base body on, at one end a pan-like depression is provided with which the lever supports in the installed state via a support element on the cylinder head. At the other end there is the valve contact area through which the gas exchange valve the internal combustion engine depending on the position of the cam of the camshaft is operated.

Der Nocken steht mit dem Ventilbetätigungshebel in einem Nocken-Kontaktbereich in Kontakt, wobei in diesem Nocken-Kontaktbereich bei einem Rollenschlepphebel eine durch Wälzelemente drehbar gelagerte Rolle angeordnet ist. The cam is in a cam contact area with the valve actuation lever Contact, one in this cam contact area with a roller rocker arm roller is rotatably mounted by rolling elements.

Der Grundkörper des Ventilbetätigungshebels ist spanlos geformt und weist an dem Ende, an dem der Ventil-Kontaktbereich vorgesehen ist, nach innen gebogene Laschen auf, die seitliche Begrenzungsflächen bilden.The base body of the valve actuation lever is formed without cutting and points to the End at which the valve contact area is provided, inwardly bent tabs which form lateral boundary surfaces.

Obwohl dieser bekannte Ventilbetätigungshebel seine Funktion sehr zufriedenstellend erfüllt, besteht dennoch das Bedürfnis, die technische Funktionalität weiter zu steigern, indem das Gewicht und damit das Massenträgheitsmoment des Hebels um seine Drehachse vermindert wird, ohne daß die Steifigkeit beeinträchtigt wird. Ferner besteht der Wunsch, die Herstellungskosten weiter zu senken.Although this known valve actuation lever works very satisfactorily fulfilled, there is still a need to further increase the technical functionality, by the weight and therefore the moment of inertia of the lever around its Axis of rotation is reduced without affecting the rigidity. There is also the desire to further reduce manufacturing costs.

Der vorliegenden Erfindung liegt deshalb die Aufgabe zugrunde, einen Ventilbetätigungshebel und insbesondere einen Rollenschlepphebel sowie ein Verfahren zu dessen Herstellung zur Verfügung zu stellen, bei welchem das Massenträgheitsmoment des Hebels um die Drehachse vermindert ist. Ein weiterer Aspekt dieser Aufgabe ist es, den Ventilbetätigungshebel so zu gestalten, daß die Steifigkeit gegenüber dem Stand der Technik erhöht und günstige Herstellungskosten erreichbar sind.The present invention is therefore based on the object of a valve actuation lever and in particular a roller rocker arm and a method for the same To provide production at which the moment of inertia the lever around the axis of rotation is reduced. Another aspect of this task is it to design the valve actuation lever so that the rigidity against the State of the art increased and low manufacturing costs can be achieved.

Diese Aufgabe wird erfindungsgemäß durch den Gegenstand des Anspruchs 1 gelöst.This object is achieved by the subject matter of claim 1.

Das erfindungsgemäße Verfahren ist Gegenstand der Ansprüche 13 und 14.The method according to the invention is the subject of claims 13 and 14.

Zu bevorzugende Weiterbildungen der Erfindung sind Gegenstand der Unteransprüche.Preferred developments of the invention are the subject of the dependent claims.

Der erfindungsgemäße Ventilbetätigungshebel weist einen im wesentlichen spanlos geformten länglichen Grundkörper, vorzugsweise mit U-förmigem Profil auf. Der Grundkörper ist im wesentlichen symmetrisch zu einer sich in seine Längsrichtung erstreckenden Längssymmetrieebene gestaltet. Zu beiden Seiten dieser Längssymmetrieebene sind im Ventil-Kontaktbereich Laschen angeordnet, welche jeweils eine der Längssymmetrieebene zugewandte Seitenfläche aufweisen. Die Laschen sind an einer Endkante dieses Grundkörpers angeformt und zum Ventil-Kontaktbereich hin umgebogen.The valve actuation lever according to the invention has a substantially non-cutting shaped elongated body, preferably with a U-shaped profile. The The basic body is essentially symmetrical to itself in its longitudinal direction extending longitudinal plane of symmetry. On both sides of this plane of longitudinal symmetry tabs are arranged in the valve contact area, each one have the side surface facing the longitudinal plane of symmetry. The tabs are on molded onto an end edge of this base body and towards the valve contact area bent.

Zumindest eine dieser Laschen weist einen sich von dieser Längssymmetrieebene weg erstreckenden Übergangsbereich auf, in welchem sich der Abstand zwischen diesen Seitenflächen vergrößert sowie wenigstens einen Parallelbereich, in dem diese Seitenflächen im wesentlichen parallel zu dieser Längssymmetrieebene verlaufen.At least one of these tabs points away from this plane of longitudinal symmetry away extending transition area, in which the distance between them Side surfaces enlarged and at least one parallel area in which this Side surfaces run essentially parallel to this longitudinal plane of symmetry.

Die beiden Laschen sind mit einem lichten Abstand an der Endkante des Grundkörpers angeordnet, der geringer ist, als der lichte Abstand der Seitenflächen im Parallelbereich, wobei dieser Abstand jeweils in einer Richtung senkrecht zur Längssymmetrieebene bestimmt wird.The two tabs are at a clear distance at the end edge of the body arranged, which is less than the clear distance of the side surfaces in the parallel area, this distance in each case in a direction perpendicular to the longitudinal plane of symmetry is determined.

Die erfindungsgemäße Gestaltung hat eine Reihe von wesentlichen Vorteilen.The design according to the invention has a number of essential advantages.

Der Abstand der Laschen an der Endkante des länglichen Grundkörpers ist eine konstruktive Größe, die die Breite des länglichen Grundkörpers im Ventil-Kontaktbereich bestimmt. Indem dieser Abstand vermindert wird, wird gleichzeitig die Breite des länglichen Grundkörpers zumindest im Ventil-Kontaktbereich und dadurch auch dessen Gewicht vermindert. Da der Ventil-Kontaktbereich radial von der Drehachse des Ventilbetätigungshebels beabstandet ist, ergibt sich dadurch eine wesentliche Verringerung des Massenträgheitsmoments um die Drehachse des Hebels. Damit werden die für die Betätigung des Hebels erforderlichen Kräfte bei gleicher Drehzahl vermindert, und es wird die für den Ventiltrieb im Hinblick auf die Betätigungskräfte zulässige Drehzahlgrenze heraufgesetzt.The distance between the tabs on the end edge of the elongated body is constructive Size, which is the width of the elongated body in the valve contact area certainly. By reducing this distance, the width of the elongated one becomes simultaneously Base body at least in the valve contact area and thereby also its Weight decreased. Because the valve contact area is radial from the axis of rotation of the valve operating lever is spaced, this results in a significant reduction the moment of inertia around the axis of rotation of the lever. With that, the forces required to operate the lever are reduced at the same speed, and it becomes the permissible for the valve train with regard to the actuation forces Speed limit raised.

Da es möglich ist, bei sonst gleichen Abmessungen die Breite des Hebels zu verringern, werden dadurch auch die Biegelängen des Hebels quer zu seiner Längsrichtung vermindert, wodurch die Steifigkeit erhöht werden kann.Since it is possible to reduce the width of the lever with the same dimensions, the bending lengths of the lever are also transverse to its longitudinal direction reduced, which can increase the rigidity.

Weiterhin wird durch die Verringerung der Hebelbreite der Materialaufwand verringert, wodurch die Herstellungskosten gesenkt werden. Gegenüber anderen Herstellungsverfahren hat die spanlose Formgebung, bei welcher auch die Laschen durch einen einfachen Stanz- und Biegevorgang hergestellt werden, ohnehin erhebliche Kostenvorteile.Furthermore, the material costs are reduced by reducing the lever width, thereby reducing manufacturing costs. Compared to other manufacturing processes has the non-cutting shape, in which the tabs are also through one simple punching and bending process can be produced, significant cost advantages anyway.

Die Verringerung der Breite des Hebels hat weiterhin den Vorteil, daß der Ventiltrieb insgesamt schmaler bauen kann. Da die Motorkonstrukteure aufgrund der Anforderungen an die Raumökonomie und die Gewichtsoptimierung gezwungen sind, Motoren mit möglichst kurzer Baulänge zu entwickeln, ist dies insbesondere aber nicht nur dann von Bedeutung, wenn aufgrund der Vorgaben für Leistungs- Verbrauchs- und Abgaswerte drei oder mehr Ventile pro Zylinder verwendet werden sollen.Reducing the width of the lever also has the advantage that the valve train overall can build narrower. Because the engine designers due to the requirements are forced to space economy and weight optimization, engines Developing with the shortest possible overall length is not only particularly then of importance if due to the specifications for power, consumption and Exhaust levels three or more valves per cylinder are to be used.

Bei einer ersten, bevorzugten Ausführungsform sind die Laschen am Grundkörper vor dem Biegevorgang derart angeformt, daß sie sich parallel zur Längssymmetrieebene erstrecken, d. h. geradlinig verlaufen. Das Umbiegen erfolgt dann in der Weise, daß eine oder beide Laschen zur Bildung des Übergangbereichs von der Längssymmetrieebene weggebogen werden. Am Ende des Übergangsbereichs werden die Laschen dann in der Weise gebogen, daß die innere, der Symmetrieebene zugewandte Seitenfläche der Lasche parallel zu dieser verläuft.In a first, preferred embodiment, the tabs are on the base body the bending process molded in such a way that they are parallel to the plane of longitudinal symmetry extend, d. H. run straight. The bending then takes place in such a way that one or both tabs to form the transition area from the longitudinal plane of symmetry be bent away. At the end of the transition area are the tabs then bent in such a way that the inner plane facing the plane of symmetry Side surface of the tab runs parallel to this.

Je nach den konstruktiven Anforderungen kann sich an diesen parallelen Bereich dann noch ein weiterer Verengungsbereich anschließen, in dem eine oder beide Laschen der Längssymmetrieebene wieder zugewandt sind.Depending on the design requirements, this parallel area can then be used connect yet another constriction area in which one or both tabs are facing the longitudinal plane of symmetry again.

Bei einer zweiten, bevorzugten Ausführungsform der Erfindung sind die Laschen derart gestanzt, daß der Übergangsbereich und der Parallelbereich bereits bei den nicht verformten Laschen vorhanden sind. Die Laschen müssen dann nur um 180° umgebogen werden und weisen im umgebogenen Zustand dann, ohne weiteren Biegevorgang, die gewünschte Kontur im Ventil-Kontaktbereich auf.In a second, preferred embodiment of the invention, the tabs are such punched that the transition area and the parallel area already with the deformed tabs are present. The tabs then only have to be bent through 180 ° and then in the bent state, without further bending, the desired contour in the valve contact area.

Die erste und die zweite Ausführungsform können auch miteinander kombiniert werden. In diesem Fall werden die Laschen durch einen Stanzvorgang in eine Ausgangsform und daran anschließend durch eine Biegung um 180° und eine zusätzliche Biegung zur Längssymmetrieebene hin oder von dieser weg in die Endform gebracht.The first and the second embodiment can also be combined with one another. In this case, the flaps are stamped into an initial shape followed by a 180 ° bend and an additional bend brought to the longitudinal symmetry plane or away from it into the final shape.

Es ist ferner möglich, die Laschen unterschiedlich zu behandeln, so daß also z.B. eine Lasche lediglich einer Biegung um ca. 180° unterworfen wird, während die andere Lasche sowohl diese Biegung als auch eine weitere Biegung insbesondere zur Längssymmetrieebene hin oder von dieser weg erfährt. Dabei kann die Ausgangsform der Laschen gleich sein, z.B. der Form eines länglichen Quaders mit parallel zur Längssymmetrieebene verlaufenden Längskanten entsprechen oder voneinander unterschiedlich sein. It is also possible to treat the tabs differently, so that e.g. a Tab is only subjected to a bend of approximately 180 °, while the other tab both this bend and a further bend, in particular to the plane of longitudinal symmetry there or away from it. The initial form of Tabs be the same, e.g. the shape of an elongated cuboid parallel to the plane of longitudinal symmetry corresponding longitudinal edges or different from each other his.

Weitere Vorteile, Merkmale und Anwendungsmöglichkeiten der vorliegenden Erfindung ergeben sich aus der nachfolgenden Beschreibung von Ausführungsbeispielen in Zusammenhang mit den Figuren. Darin zeigen:

Figur 1
eine Untersicht eines ersten Ausführungsbeispiels der Erfindung, welches als Rollenschlepphebel ausgebildet ist;
Figur 2
einen Längsschnitt des Ausführungsbeispiels gemäß Fig. 1;
Figur 3
einen Schnitt durch die Darstellung gemäß Fig. 2 entlang der Linien III-III gesehen;
Figur 4
eine Aufsicht auf das Ausführungsbeispiel gemäß Fig. 1;
Figur 5
eine Ansicht des Rollenschlepphebels des Ausführungsbeispiels gemäß Fig. 1 während der Fertigung, von unten gesehen;
Figur 6
eine Darstellung entsprechend der Fig. 5 in einem weiteren Stadium der Fertigung;
Figur 7
ein zweites Ausführungsbeispiel des erfindungsgemäßen Rollenschlepphebels in einem vorhergehenden Stadium der Fertigung, von unten gesehen;
Figur 8
den Rollenschlepphebel gemäß Fig. 7 in einer Ansicht von unten gesehen;
Further advantages, features and possible uses of the present invention result from the following description of exemplary embodiments in connection with the figures. In it show:
Figure 1
a bottom view of a first embodiment of the invention, which is designed as a roller rocker arm;
Figure 2
a longitudinal section of the embodiment of FIG. 1;
Figure 3
seen a section through the representation of Figure 2 along the lines III-III.
Figure 4
a plan of the embodiment of FIG. 1;
Figure 5
a view of the roller rocker arm of the embodiment of Figure 1 during manufacture, seen from below.
Figure 6
a representation corresponding to Figure 5 in a further stage of manufacture.
Figure 7
a second embodiment of the roller finger follower according to the invention in a previous stage of manufacture, seen from below;
Figure 8
seen in a view from below.

Ein erstes Ausführungsbeispiel der Erfindung wird nun in bezug auf die Figuren 1 bis 6 beschrieben.A first embodiment of the invention will now be described with reference to FIGS. 1 to 6 described.

Fig. 1 zeigt ein erstes Ausführungsbeispiel des erfindungsgemäßen Rollenschlepphebels.Fig. 1 shows a first embodiment of the roller finger follower according to the invention.

Der Rollenschlepphebel weist einen insgesamt mit 1 bezeichneten Grundkörper auf, der sich im wesentlichen symmetrisch entlang einer Längssymmetrieebene 2 erstreckt. Der Begriff Symmetrieebene ist hier nicht im rein geometrischen Sinn zu verstehen, sondern bedeutet lediglich, daß wesentliche Bereiche des Ventilbetätigungshebels symmetrisch zu dieser Symmetrieebene gestaltet sind. Die Symmetrieebene 2 verläuft in der Darstellung gemäß Fig. 1 senkrecht zur Zeichenebene und bildet in der Darstellung gemäß Fig. 2 die Schnittebene.The roller rocker arm has a base body designated 1 overall, which extends essentially symmetrically along a longitudinal plane of symmetry 2. The term plane of symmetry is not to be understood here in a purely geometrical sense, it simply means that essential areas of the valve actuation lever are designed symmetrically to this plane of symmetry. The plane of symmetry 2 1 runs perpendicular to the plane of the drawing and forms in the 2 the sectional plane.

Der längliche Grundkörper ist, wie aus der Darstellung gemäß Fig. 3 ersichtlich, im wesentlichen U-förmig gestaltet und weist eine sich symmetrisch zur Symmetrieebene 2 erstreckende Aussparung 4 auf, in der eine über Wälzelemente 6 gelagerte Rolle 7 angeordnet ist. Im eingebauten Zustand steht die Rolle 7 mit dem Nocken einer Nokkenwelle in Kontakt.The elongated body is, as can be seen from the illustration in FIG. 3, in designed essentially U-shaped and has a symmetrical to the plane of symmetry 2 extending recess 4 in which a roller 7 mounted on rolling elements 6th is arranged. When installed, the roller 7 stands with the cam of a camshaft in contact.

Im rechten Teil der Darstellung gemäß Fig. 1 ist eine Vertiefung 10 zur Aufnahme eines (nicht dargestellten) Abstützelementes vorgesehen. Im eingebauten Zustand stützt sich dieses Element seinerseits innerhalb des (nicht dargestellten) Zylinderkopfes ab. Die Gestaltung dieser Vertiefung 10 ist im Stand der Technik bekannt und braucht deshalb hier nicht weiter erörtert zu werden.In the right part of the illustration according to FIG. 1 there is a depression 10 for receiving a Support element (not shown) is provided. When installed this element in turn is supported within the cylinder head (not shown) from. The design of this recess 10 is known in the prior art and therefore need not be discussed further here.

Auf der in der Darstellung gemäß Fig. 1 linken Seite des Grundkörpers ist ein Ventil-Kontaktbereich 20 vorgesehen. Der Ventil-Kontaktbereich weist eine Fläche 21 auf, die beim Ausführungsbeispiel leicht konvex gestaltet ist, kann aber auch andere Krümmungsformen aufweisen oder eben gestaltet sein.On the left side of the base body in the illustration according to FIG. 1 there is a valve contact area 20 provided. The valve contact area has a surface 21, which is designed to be slightly convex in the exemplary embodiment, but can also do other things Have curvature shapes or just be designed.

Der Ventil-Kontaktbereich ist durch zwei, der Längssymmetrieebene 2 zugewandte seitliche Flächen 23, 24 begrenzt, die Teil der Laschen 25, 26 sind.The valve contact area is through two, the longitudinal symmetry plane 2 facing limited lateral surfaces 23, 24, which are part of the tabs 25, 26.

Die Laschen 25, 26 sind an einer Endkante 30 des länglichen Grundkörpers 1 angeformt, wobei die Endkante 30 im wesentlichen senkrecht zur Symmetrieebene 2 ist. Der Abstand der Laschen 25 und 26 an dieser Endkante des Grundkörpers entspricht der Länge a in Fig. 5 zwischen den Pfeilen 31 und 32 oder, anders ausgedrückt, die Laschen 25 und 26 sind an der Endkante 30 eines Steges 30a, welcher die Breite c (siehe Fig. 5) zwischen den Pfeilen 33 und 34 aufweist, angeformt.The tabs 25, 26 are formed on an end edge 30 of the elongate base body 1, the end edge 30 being substantially perpendicular to the plane of symmetry 2. The distance between the tabs 25 and 26 corresponds to this end edge of the base body the length a in Fig. 5 between the arrows 31 and 32 or, in other words, the Tabs 25 and 26 are on the end edge 30 of a web 30a, which has the width c (see Fig. 5) between the arrows 33 and 34, integrally formed.

Beim Ausführungsbeispiel gemäß Fig. 1 weisen beide Laschen 25, 26 einen Übergangsbereich 35, 36 auf, in dem die Laschen sich von der Symmetrieebene 2 weg erstrecken. An diesen Übergangsbereich 35, 36 schließt sich ein Parallelbereich 37, 38 an, in dem beide Laschen parallel zur Symmetrieebene 2 verlaufen. Bei der Lasche 26 schließt sich daran ein Verengungsbereich 40 an, in dem die Lasche wieder auf die Symmetrieebene 2 zu verläuft.1, both tabs 25, 26 have a transition region 35, 36 on, in which the tabs away from the plane of symmetry 2 extend. A parallel area 37 adjoins this transition area 35, 36 38 in which both tabs run parallel to the plane of symmetry 2. At the tab 26 is followed by a constriction area 40, in which the tab rests on the Plane of symmetry 2 runs.

Der Begriff Übergangsbereich ist folglich dadurch definiert, daß sich hier die winkelmäßige Ausrichtung der Lasche bzw. der Seitenflächen in bezug auf die Längssymmetrieebene ändert.The term transition area is therefore defined by the fact that here the angular Alignment of the tab or the side surfaces with respect to the longitudinal plane of symmetry changes.

Im Parallelbereich 37, 38 entspricht der Abstand der beiden Laschen der Strecke b, wie zwischen den Pfeilen 42, 43 dargestellt. Dieser Abstand b ist größer als der Abstand a. Die Differenz der beiden Strecken entspricht im wesentlichen der Breiteneinsparung des Grundkörpers gegenüber dem eingangs erörterten Stand der Technik.In the parallel area 37, 38, the distance between the two tabs corresponds to the distance b, as shown between arrows 42, 43. This distance b is larger than the distance a. The difference between the two routes essentially corresponds to the width savings of the base body compared to the prior art discussed above.

Beim gezeigten Ausführungsbeispiel liegen die beiden Laschen 25, 26, wie insbesondere die Darstellung gemäß Figur 2 zeigt, bündig, d. h. ohne Zwischenraum, auf der gekürmmten Fläche des Ventil-Kontaktbereichs 20 auf.In the embodiment shown, the two tabs 25, 26 are located, in particular the representation according to Figure 2 shows, flush, d. H. without space on which curved surface of the valve contact area 20.

Davon abweichend können die Laschen bei diesem Ausführungsbeispiel und auch beim nächsten Ausführungsbeispiel so gestaltet sein, daß zwischen den Laschen und der Fläche des Ventilkontaktbereichs ein Spalt vorgesehen ist, wobei die Laschen dann so geformt sind, daß ihr Endbereich auf dem Ventil-Kontaktbereich aufliegt. Um den Endbereich, in der Darstellung gemäß Figur 1 ist dies z. B. bei der Lasche 26 der Verengungsbereich 40, in bezug auf den Ventilkontaktbereich zu fixieren, kann sowohl bei der ersten Alternative, d. h. bei bündig aufliegenden Laschen, als auch bei der zweiten Alternative, d. h. bei Laschen, die teilweise einen Abstand zum Ventil-Kontaktbereich aufweisen, am Ende eine zusätzliche Verbindung, vorzugsweise durch einen Schweißpunkt hergestellt werden.Deviating from this, the tabs can also in this embodiment be designed in the next embodiment so that between the tabs and a gap is provided on the surface of the valve contact area, the tabs are then shaped so that their end area rests on the valve contact area. Around the end region, in the illustration according to FIG. B. at the tab 26 of the Constriction area 40, with respect to the valve contact area, can be fixed in the first alternative, d. H. with flush-fitting tabs, as well as with the second alternative, d. H. in the case of tabs that are partially at a distance from the valve contact area have at the end of an additional connection, preferably by a spot weld is made.

Ein Verfahren zur Herstellung dieses Ausführungsbeispiels der Erfindung wird nun in bezug auf die Fig. 5 und 6 erläutert.A method of making this embodiment of the invention is now described in with reference to FIGS. 5 and 6 explained.

Der im Ausführungsbeispiel gezeigte Rollenschlepphebel wird insgesamt aus einem Metallblech ausgestanzt und dann vorzugsweise kalt verformt, um die in den Fig. 1 bis 4 gezeigte endgültige Gestaltung zu erlangen. Die Laschen 25 und 26 werden beim Stanzen als im wesentlichen geradlinig verlaufende Verlängerung des Grundkörpers 1 ausgebildet. Anschließend werden sie, wie in Fig. 6 gezeigt, nach unten (in der Darstellung der Zeichnung gesehen) umgeformt, wobei der Abstand der Laschen weiterhin dem Abstand a entspricht. Anschließend werden die Laschen von der Symmetrieebene 2 weg gebogen, um den Übergangsbereich 35, 36 zu bilden. Dieser Biegevorgang wird so ausgeführt, daß die Laschen zunächst in einem ersten Biegewinkel nach außen gebogen sind, so daß sich der nach außen von der Symmetrieebene 2 wegverlaufende erste Teil des Übergangsbereichs 35, 36 bildet und daß daran anschließend die Laschen derart in Richtung auf die Symmetrieebene 2 zurückgebogen werden, daß der weitere Teil der Laschen parallel zur Symmetrielinie 2 verläuft. Lediglich ein oder beide Enden der Laschen, wie durch 40 in Fig. 1 angedeutet, ist wieder mit einem Biegewinkel nach innen, auf die Symmetrieebene 2 hin geformt.The roller rocker arm shown in the embodiment is a total of one Metal sheet punched out and then preferably cold-formed to the in Fig. 1 to 4 to achieve the final design shown. The tabs 25 and 26 are at Punching as an essentially straight extension of the base body 1 educated. Then, as shown in Fig. 6, they are down (in the illustration seen the drawing) reshaped, the distance between the tabs continues corresponds to the distance a. Then the tabs from the plane of symmetry 2 bent away to form the transition region 35, 36. This bending process is carried out so that the tabs are initially at a first bending angle are bent outwards so that the outwards from the plane of symmetry 2nd forms the first part of the transition region 35, 36 and that adjoins it the tabs bent back in the direction of the plane of symmetry 2 be that the further part of the tabs runs parallel to the line of symmetry 2. Only one or both ends of the tabs, as indicated by 40 in Fig. 1, is again with an inward bending angle, formed on the plane of symmetry 2.

Wie die Darstellung gemäß Fig. 1 bis 6 zeigt, ist es durch diese Gestaltung möglich, den Ventilbetätigungshebel mit einer geringen Breite auszuführen. Dadurch wird erheblich an Material eingespart, wodurch das Massenträgheitsmoment um die Drehachse vermindert und, bei sonst gleichen Abmessungen, die Steifigkeit erhöht wird.As the representation according to FIGS. 1 to 6 shows, this design makes it possible run the valve operating lever with a small width. This becomes significant of material saved, thereby reducing the moment of inertia around the axis of rotation reduced and, with otherwise the same dimensions, the rigidity is increased.

Ein weiteres Ausführungsbeispiel der Erfindung wird nun in bezug auf die Fig. 7 und 8 erläutert.Another embodiment of the invention will now be described with reference to FIGS. 7 and 8 explained.

Bei diesem Ausführungsbeispiel entspricht das in Fig. 8 im wesentlichen dargestellte Endprodukt, nämlich der Rollenschlepphebel, im wesentlichen der Darstellung gemäß Fig. 1. Es werden deshalb dort auch entsprechende Bezugszeichen verwendet.In this exemplary embodiment, this essentially corresponds to that shown in FIG. 8 End product, namely the roller finger follower, essentially as shown Fig. 1. Corresponding reference numerals are therefore also used there.

Ein Unterschied ergibt sich aber in der Gestaltung der Laschen 51 und 52.However, there is a difference in the design of the tabs 51 and 52.

Wie die Darstellung gemäß Fig. 7 zeigt, werden hier die Laschen bei einem Stanzvorgang unmittelbar so gebildet, daß sich der gewünschte Übergangsbereich bereits während des Stanzvorganges und nicht, wie beim Ausführungsbeispiel gemäß Fig. 1 bis 6, beim Biegen ergibt.As the illustration in FIG. 7 shows, the tabs are here during a punching process immediately formed so that the desired transition area is already during the punching process and not, as in the exemplary embodiment according to FIGS. 1 to 6, results in bending.

Die Lasche 51 ist an der im wesentlichen senkrecht zur Symmetrieebene 2 verlaufenden Endkante 30 des Grundkörpers 1 angeformt. Die Lasche 51 weist einen ersten Bereich auf, bei dem die Lasche auch in unverformtem Zustand einen mit 53 bezeichneten spitzen Winkel zu dieser Endkante 30 bildet, wodurch sich ein von der Längssymmetrieebene 2 weg weisender Übergangsbereich 54 bildet. Dem Übergangsbereich 54 folgt ein Parallelbereich 55, der parallel zur Längssymmetrieebene gestaltet ist und daran ein Bereich 56, bei dem die Seitenfläche im spitzen Winkel zur Längssymmetrieebene hin gerichtet ist.The tab 51 is on the substantially perpendicular to the plane of symmetry 2 End edge 30 of the base body 1 is formed. The tab 51 has a first Area in which the tab is designated 53 even in the undeformed state forms an acute angle to this end edge 30, whereby one of the longitudinal symmetry plane 2 pointing transition area 54 forms. The transition area 54 is followed by a parallel region 55, which is designed parallel to the plane of longitudinal symmetry and there is an area 56 in which the side surface is at an acute angle to the longitudinal plane of symmetry is directed towards.

Bei der Lasche 52 ist zunächst ein Parallelbereich 57 vorgesehen, der parallel zur Längssymmetrieebene 2 verläuft, an den sich dann der Übergangsbereich 58 anschließt, bei dem die Lasche von der Längssymmetrieebene 2 weg nach außen verläuft. Daran schließt sich ein weiterer Parallelbereich 59 an, der parallel zur Längssymmetrieebene 2 verläuft und der die Seitenfläche 60 bildet.In the case of the tab 52, a parallel region 57 is initially provided, which is parallel to the Longitudinal plane of symmetry 2 runs, to which the transition region 58 then adjoins, in which the tab extends outward from the longitudinal plane of symmetry 2. This is followed by a further parallel area 59, which is parallel to the longitudinal plane of symmetry 2 extends and which forms the side surface 60.

Das Verfahren zur Herstellung dieses Ventilbetätigungshebels ist ähnlich gestaltet wie beim vorbeschriebenen Ausführungsbeispiel. Die Laschen werden auch hier um ca. 180° gebogen, wodurch sich eine Gestaltung des Schlepphebels entsprechend der Fig. 8 ergibt. Die auf die Längssymmetrieebene zu oder von dieser weg gerichtete Biegung entfällt hier allerdings. Das Stanzwerkzeug ist insgesamt etwas aufwendiger gestaltet als beim Ausführungsbeispiel gemäß Fig. 1 bis 6. Dem steht aber der Vorteil gegenüber, daß der Biegevorgang leichter vonstatten geht. The process for producing this valve actuation lever is similar to that in the above-described embodiment. The tabs are also approx. Bent 180 °, which is a design of the rocker arm according to the Fig. 8 results. The directed towards or away from the longitudinal plane of symmetry Bending is omitted here. The punching tool is somewhat more complex overall designed as in the embodiment of FIGS. 1 to 6. But there is the advantage compared to that the bending process is easier.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Grundkörperbody
22
LängssymmetrieebeneLongitudinal plane of symmetry
44
Aussparungrecess
66
Wälzelementrolling
77
Rollerole
1010
Vertiefungdeepening
2020
Ventil-KontaktbereichValve contact area
2121
Fläche von 20Area of 20
23, 2423, 24
Seitliche FlächeLateral surface
25, 2625, 26
Lascheflap
3030
Endkanteend edge
30a30a
Stegweb
31, 3231, 32
Pfeilarrow
33, 3433, 34
Pfeilarrow
35, 3635, 36
ÜbergangsbereichTransition area
37, 3837, 38
Parallelbereichparallel area
4040
Verengungsbereichthroat area
42, 4342, 43
Pfeilarrow
51, 5251, 52
Lascheflap
5353
spitzer Winkelacute angle
5454
ÜbergangsbereichTransition area
5555
Parallelbereichparallel area
5656
Verengungsbereichthroat area
5858
ÜbergangsbereichTransition area
5959
Parallelbereichparallel area
6060
seitliche Flächeside surface
aa
Abstand senkrecht zur LängssymmetrieebeneDistance perpendicular to the plane of longitudinal symmetry
bb
Abstand senkrecht zur LängssymmetrieebeneDistance perpendicular to the plane of longitudinal symmetry
cc
Breite zwischen den Pfeilen 33 und 34Width between arrows 33 and 34

Claims (15)

  1. Valve actuating lever for transmitting movement of a cam arranged on a camshaft to a gas changing valve of an internal combustion engine comprising:
    an essentially non-cut formed oblong base body (1) configured essentially symmetrical to its longitudinal symmetry plane (2) extending longitudinally therefrom,
    a valve contact area (20) arranged at a first end of said base body,
    two tabs (25, 26; 51, 52) arranged at both sides of said longitudinal symmetry plane in said valve contact area, each respectively having a lateral surface (23, 24; 60, 61) aligned facing said longitudinal symmetry plane, whereby said tabs are formed on said base body and are bent over toward said valve contact area,
    characterized in that
    said tabs are arranged spaced at a clearance (a) at an end edge (30) of said base body, said clearance (a) being less than the clearance (b) of said lateral surfaces in said valve contact area, whereby said clearance is respectively measured perpendicular to said longitudinal symmetry plane (2), and
    at least one of said tabs has at least one connecting portion (35, 36; 54, 58) extending from said longitudinal symmetry plane in which the clearance between said lateral surfaces enlarges as well as at least one parallel portion (37, 38; 55, 59) in which said lateral surfaces extend essentially parallel to said longitudinal symmetry plane (2).
  2. Valve actuating lever according to claim 1, characterized in that
    said connecting portion (35, 36) is created through means of plastic deformation.
  3. Valve actuating lever according to claim 1, characterized in that
    said connecting portion (54, 58) is created through means of a material removal process.
  4. Valve actuating lever according to at least one of the preceding claims, characterized in that
    at least one of said tabs comprises a narrowed portion (40, 56) adjoining said parallel portion in which said tab is formed toward said longitudinal symmetry plane (2).
  5. Valve actuating lever according to at least one of the preceding claims, characterized in that
    said base body is configured of essentially U-shape in a section plane which lies perpendicular to said longitudinal symmetry plane.
  6. Valve actuating lever according to at least one of the preceding claims, characterized in that
    said tabs are of rectangular configuration in cross-section and preferably of square configuration in cross-section.
  7. Valve actuating lever according to at least one of the preceding claims, characterized in that
    said surface (21) formed by said valve contact area (20) extends in curved configuration and that said tabs are bent in such a manner so as to abut up against said surface to follow said curvature.
  8. Valve actuating lever according to at least one of claims 1 - 6, characterized in that
    said surface (21) formed by said valve contact area (20) extends in curved configuration and that said tabs are bent in such a manner that they have a clearance from said surface in a partial section and only abut up against said surface at their end sections.
  9. Valve actuating lever according to claim 7 or 8, characterized in that
    said curvature is at least partially a convex curvature.
  10. Valve actuating lever according to at least one of the preceding claims, characterized in that
    said valve lever is configured as a drag lever.
  11. Valve actuating lever according to claim 10, characterized in that
    said valve actuating lever is configured as a roller drag lever.
  12. Valve actuating lever according to claim 11, characterized in that
    said roller drag lever comprises a roller (7) rotatably mounted via roller elements (6).
  13. Valve actuating lever according to claim 1, characterized in that
    said base body (1) is of U-shaped form in cross-section and that said tabs are formed on one end edge (30) of said base body, in particular on a trestle (30a) of narrower width (c) of said U-shaped base body (1).
  14. Method for manufacturing a valve actuating lever and especially a valve actuating lever in accordance with one of claims 1 - 13 including the following procedural steps:
    stamping out of an oblong base body (1) configured essentially symmetrical to a longitudinal symmetry plane (2) extending longitudinally therefrom having two tabs (25, 26) arranged at both sides of said longitudinal symmetry plane (2) on an end edge, each respectively having a lateral surface (23, 24) aligned facing said longitudinal symmetry plane (2), whereby said tabs (25, 26) are formed on said base body (1) and extend parallel to said longitudinal symmetry plane (2),
    bending of said tabs (25, 26) at an angle of approximately 180°,
    bending of at least one of said tabs (25, 26) to form a connecting portion (35, 36) extending from said longitudinal symmetry plane (2) in which the clearance between said lateral surfaces (23, 24) enlarges, as well as at least one parallel portion (37, 38) in which said lateral surfaces (23, 24) extend essentially parallel to said longitudinal symmetry plane (2).
  15. Method for manufacturing a valve actuating lever and especially a valve actuating lever in accordance with one of claims 3 - 13, including the following procedural steps:
    stamping out of an oblong base body (1) configured essentially symmetrical to a longitudinal symmetry plane (2) extending longitudinally therefrom having two tabs (51, 52) arranged at both sides of said longitudinal symmetry plane, each respectively having a lateral surface (60, 61) aligned facing said longitudinal symmetry plane, whereby said tabs (51, 52) are formed on said base body and whereby at least one of said tabs (51, 52) comprises at least one connecting portion (54, 58) extending from said longitudinal symmetry plane (2) in which the clearance between said lateral surfaces enlarges as well as at least one parallel portion (55, 59) in which said lateral surfaces extend essentially parallel to said longitudinal symmetry plane (2),
    bending of said tabs at an angle of approximately 180°.
EP98965707A 1997-12-02 1998-11-27 Valve operating lever Expired - Lifetime EP1036256B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19753424A DE19753424A1 (en) 1997-12-02 1997-12-02 Valve actuation lever
DE19753424 1997-12-02
PCT/EP1998/007674 WO1999028600A1 (en) 1997-12-02 1998-11-27 Valve operating lever

Publications (2)

Publication Number Publication Date
EP1036256A1 EP1036256A1 (en) 2000-09-20
EP1036256B1 true EP1036256B1 (en) 2002-04-03

Family

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EP98965707A Expired - Lifetime EP1036256B1 (en) 1997-12-02 1998-11-27 Valve operating lever

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US (1) US6273044B1 (en)
EP (1) EP1036256B1 (en)
DE (2) DE19753424A1 (en)
ES (1) ES2174539T3 (en)
WO (1) WO1999028600A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6470842B2 (en) * 2000-10-12 2002-10-29 Ina Walzlager Schaeffler Ohg Lever-type cam follower
ES2228241B1 (en) * 2003-02-20 2006-06-01 Tratasa 2000, S.L. PROCEDURE FOR MANUFACTURING A FILTER FOR WATER AND OTHER FLUIDS.
US20100018276A1 (en) * 2008-07-28 2010-01-28 Edelmayer Thomas C Sheet metal rocker arm with integrally formed cross member
DE102011006694A1 (en) * 2010-04-15 2011-10-20 Schaeffler Technologies Gmbh & Co. Kg Assembly for a gas exchange valve drive of an internal combustion engine
DE102011076727A1 (en) 2011-05-30 2012-12-06 Schaeffler Technologies AG & Co. KG Rocker arm i.e. roller rocker arm, for variable valve train of combustion piston engine, has bars designed in stepped manner at inner walls, where distance between walls in inner region is less than that between walls in outer region
JP6769691B2 (en) * 2014-12-26 2020-10-14 株式会社オティックス Rocker arm manufacturing method

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5016582A (en) * 1990-10-12 1991-05-21 Henley Manufacturing Holding Company, Inc. Rocker arm
WO1993014301A1 (en) * 1992-01-07 1993-07-22 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Roller rocker arm and process for manufacturing the same
DE19617668C2 (en) * 1995-11-23 2003-11-20 Ina Schaeffler Kg Chipless rocker arm or rocker arm
DE19543657C2 (en) 1995-11-23 1998-07-02 Schaeffler Waelzlager Ohg Chipless rocker arm or rocker arm
DE19617523C2 (en) * 1996-05-02 2001-11-08 Schaeffler Waelzlager Ohg Securing for operating lever of valve controls for internal combustion engines

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US6273044B1 (en) 2001-08-14
EP1036256A1 (en) 2000-09-20
WO1999028600A1 (en) 1999-06-10
ES2174539T3 (en) 2002-11-01
DE19753424A1 (en) 1999-06-10
DE59803669D1 (en) 2002-05-08

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