EP2396522B1 - Valve train of an internal combustion engine - Google Patents
Valve train of an internal combustion engine Download PDFInfo
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- EP2396522B1 EP2396522B1 EP10704501.5A EP10704501A EP2396522B1 EP 2396522 B1 EP2396522 B1 EP 2396522B1 EP 10704501 A EP10704501 A EP 10704501A EP 2396522 B1 EP2396522 B1 EP 2396522B1
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- cam
- section
- axial
- excursion
- groove
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- 238000002485 combustion reaction Methods 0.000 title claims description 7
- 230000001133 acceleration Effects 0.000 claims description 5
- 230000007704 transition Effects 0.000 claims description 3
- 238000006073 displacement reaction Methods 0.000 description 9
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000000630 rising effect Effects 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L13/00—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
- F01L13/0015—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
- F01L13/0036—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque the valves being driven by two or more cams with different shape, size or timing or a single cam profiled in axial and radial direction
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
- F01L1/02—Valve drive
- F01L1/04—Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
- F01L1/047—Camshafts
- F01L2001/0471—Assembled camshafts
- F01L2001/0473—Composite camshafts, e.g. with cams or cam sleeve being able to move relative to the inner camshaft or a cam adjusting rod
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L13/00—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
- F01L13/0015—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
- F01L13/0036—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque the valves being driven by two or more cams with different shape, size or timing or a single cam profiled in axial and radial direction
- F01L2013/0052—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque the valves being driven by two or more cams with different shape, size or timing or a single cam profiled in axial and radial direction with cams provided on an axially slidable sleeve
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L2301/00—Using particular materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L2800/00—Methods of operation using a variable valve timing mechanism
- F01L2800/12—Fail safe operation
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49293—Camshaft making
Definitions
- the invention relates to a valve train of an internal combustion engine, comprising a carrier shaft and a rotatably mounted thereon and slidably disposed between two axial cam piece comprising at least one cam group immediately adjacent cams with different cam lobes and a Axialkulisse with two axially peripherally
- Axialkulisse actuator for moving the cam piece in the direction of both cam tracks.
- Such a valve train which is used for variable actuation of gas exchange valves by means of sliding cam and in which a single actuator per cam piece is sufficient to move the cam piece in the direction of both cam tracks of Axialkulisse is considered from the considered generic DE 101 48 177 A1 previously known.
- There two cam pieces are disclosed with alternatively designed Axialkulissen, wherein the first Axialkulisse has a central guide bar to form inner guide walls for the actuator in the form of a dipping into the Axialkulisse cylindrical pin and the second Axialkulisse consists only of outer guide walls.
- the latter embodiment has the advantage that the production cost for the axial slide is significantly smaller due to the omission of the guide bar.
- a considerable risk in terms of the reliability of the valve train in this embodiment is that the displacement of the cam piece is completed completely, ie without a fault, if the mass inertia of the cam piece is sufficient to pass it through the crossing region of the curved paths without force of the cylinder pin to a certain extent in free flight to move to its other end position.
- a prerequisite for the sufficient inertia of the cam piece is of course a minimum speed of the camshaft, which directly from the friction between the cam piece and the Carrier shaft is dependent.
- a displacement of the cam piece rotating below this minimum rotational speed can cause the cam piece to stop "halfway" and a cam follower acting on the gas exchange valve to be acted upon by several cams of the cam group uncontrolled and under high mechanical loads simultaneously.
- a valve train having the features of the preamble of claim 1 is also known from DE 101 48 178 A1 and the DE 10 2007 037 232 A1 out.
- the present invention is therefore the object of a valvetrain of the type mentioned in such a way that the said functional limitations and risks are at least partially eliminated.
- the object is therefore, when using a single actuator for both Verschieberungen even at low speeds of the camshaft, for example during the starting process of the internal combustion engine, a successful, i. ensure complete switching of the cam piece.
- the curved paths should be arranged one behind the other in the circumferential direction of the axial slide.
- a significant difference of the invention over the prior art thus relates to the mutual arrangement of the curved paths on the Axialkulisse, which now consecutively, ie in series, and no longer next to each other, ie in parallel, run and therefore no longer intersect. Due to the omission of the crossing region, the displacement of the cam piece takes place under permanent forced guidance of the axial slide against the actuating element coupled thereto, so that a complete switching operation of the cam piece is ensured even at the lowest rotational speeds of the camshaft.
- the cam tracks are each formed as a groove and the actuating element as engaging in the grooves cylindrical pin.
- the curved paths are each of successive track sections composed with different axial strokes of the groove bounding groove walls, namely an entry section without Axialhub, a ramp section and a lifting section, wherein the lifting section has a significantly greater axial acceleration than the ramp section.
- the cams should have a common base circle area, which begins at the latest with the ramp portion of the first curved path and ends at the earliest with the lifting portion of the second curved path. Since the common base circle region is to be understood as the angular range of the cam piece in which all the cams of the cam group are free of elevation, the displacement of the cam piece takes place only when the gas exchange valve associated with the cam group is closed and the cam to be engaged during the entire displacement operation also located in its base circle position. Thus, during the displacement process, no valve spring forces increasing the friction between the cam piece and the carrier shaft act on the cam piece. In order to keep the axial acceleration of the cam piece as small as possible, the beginning and the end of the base circle area and of the shifting process are ideally identical.
- the lifting sections may each be composed of successive Operahubabitesen with different radial strokes of the groove delimiting groove base, namely a first Operahubabites without radial stroke and a second Operahubabites with radially outwardly uplifting groove bottom.
- the actuating pin is "ejected" only in axialkraft laminate state from the radially rising groove in its non-engaging rest position
- the cam angle of the lifting sections can be maximized for a given length of the intermediate section.
- FIG. 1 a section of a variable valve train of an internal combustion engine essential for the understanding of the invention is disclosed.
- the valve train points a camshaft 1, which a carrier shaft 2 and - the number of cylinders of the internal combustion engine accordingly - rotatably thereto and slidably disposed between two axial positions cam pieces 3 comprises.
- the carrier shaft 2 are provided with an outer longitudinal toothing and the cam piece 3 with a corresponding inner longitudinal toothing.
- the teeth are known per se and not shown here.
- the cam piece 3 has on both sides of a bearing 4 arranged cam groups, each with two immediately adjacent cams 5 and 6, which have different cam elevations at the same base circle radius.
- the displacement of the cam piece takes place outside the cam elevations during the common base circle region of the cams 5, 6.
- the cam elevations are each in a known manner by a cam follower symbolized here only by a cam roller 7, e.g. a drag lever, selectively transmitted in dependence on the instantaneous axial position of the cam piece 3 to a gas exchange valve, not shown.
- the different cam elevations are to be understood as meaning different amounts of the respective cam lift and / or different valve control times of the cams 5, 6.
- the cam piece 3 is provided with a manufactured as a single part and joined by means of interference fit Axialkulisse 8.
- Axialkulisse 8 On the circumference of the Axialkulisse 8 are two axially oppositely extending and circumferentially of the Axialkulisse 8 successively arranged cam tracks 9, 10 are formed in the form of grooves, in which an actuating element 11 can be coupled.
- the actuating element 11 is a cylindrical pin, which is part of a likewise known actuator, which is not explained here, for such valve trains.
- the cylinder pin 11 is axially fixed relative to the camshaft 1, but arranged radially displaceable in the internal combustion engine and serves to move the cam piece 3 in the direction of both cam tracks 9, 10th
- FIGS. 1 to 6 The design of the curved paths 9, 10 results from a synopsis of FIGS. 2 to 6 .
- the in the FIGS. 2 to 4 shown views on the axial slide 8 correspond to the view arrows x, y and z in FIG. 5 in which the axial slide 8 shown in side view is additionally provided with a radial control diagram of the cam tracks 9, 10 according to the dashed line.
- the in the FIGS. 1, 2 and 5 Arrows indicated represent the direction of rotation of the camshaft 1.
- a complete lift diagram with radial and axial stroke of the cam tracks 9, 10 as a function of the camshaft angle goes out FIG. 6 out.
- the two cam tracks 9, 10 each consist of successive track sections with different axial strokes (solid line in FIG FIG. 6 ) of the groove bounding groove walls 12 together.
- These track sections are an entry section F or C without axial stroke, a ramp section A or D for compensating axial position tolerances of the cylindrical pin 11 relative to the groove walls 12 and a lift section B or E, wherein the axial acceleration of the lift sections B, E is significantly greater than that of the ramp sections A, D.
- the common base circle area of the cams 5, 6 is identical to the track sections A to E, ie the common base circle area begins with the ramp section A of the first cam track 9 and ends with the Lifting section E of the second curved path 10.
- the cam elevations of the cams 5, 6 are in the region of the entry section F.
- the lifting sections B and E are each composed of successive Operahubabrisken B1 and B2 or E1 and E2, which in the radial stroke of the groove bottom 13 (dashed line in FIGS. 5 and 6 ).
- the first Operahubabriske B1 and E1 a groove bottom 13 with constant and identical to the sections F and A and C and D depth, while the groove base 13 rises radially outwardly over the second Operahubabriske B2 and E2 to the cylinder pin 11 already eject during the sliding operation of the cam piece 3 from the respective groove in its non-engaging rest position.
- the switching of the cam piece 3 along the first cam track 9, ie from the currently active cam 5 on the cam 6 see FIG.
- the locking device comprises two in a formed as a through hole radial bore 14 of the support shaft 2 diametrically opposed, slidably mounted locking body 15 and the inner circumference of the cam piece 3 extending, as circumferential grooves formed locking grooves 16 and 17, in which the force-loaded by a spring means 18 in radially outward direction locking body 15 are engaged in the respective associated axial positions.
- the locking bodies 15 are unilaterally open, thin-walled Blechumformmaschine.
- the open side is each as mounted in the radial bore 14 and formed as a helical compression spring spring means 18 enclosing hollow cylinder, while it is in the subsequent closed side each in the direction of the locking grooves 16, 17 tapered hollow body, the first conical and the front side is spherical.
- the locking body 15 are provided in the conical portion of the hollow body with a pressure relief opening 19.
- the function of the locking device is not limited to the fixation of the cam piece 3 in the two axial positions, but also includes a braking of the cam piece 3 in its axial movement towards the end of Operahubabitese B2 and E2.
- This braking is generated by contact friction of the spring-loaded locking body 15 on the both sides of the apex point 20 axially adjacent groove walls of the locking grooves 16, 17.
- the locking grooves 16, 17 are geometrically identical and the vertex 20 - based on the distance of the locking grooves 16, 17 associated axial positions of the cam piece 3 - runs centrally.
Description
Die Erfindung betrifft einen Ventiltrieb einer Brennkraftmaschine, mit einer Nockenwelle, die eine Trägerwelle sowie ein darauf drehfest und zwischen zwei Axialpositionen verschiebbar angeordnetes Nockenstück umfasst, das zumindest eine Nokkengruppe unmittelbar benachbarter Nocken mit unterschiedlichen Nockenerhebungen und eine Axialkulisse mit zwei sich an deren Umfang axial gegenläufig erstrekkenden Kurvenbahnen aufweist, und mit einem mit der Axialkulisse koppelbaren Betätigungselement zum Verschieben des Nockenstücks in Richtung beider Kurvenbahnen.The invention relates to a valve train of an internal combustion engine, comprising a carrier shaft and a rotatably mounted thereon and slidably disposed between two axial cam piece comprising at least one cam group immediately adjacent cams with different cam lobes and a Axialkulisse with two axially peripherally entgegenrekkenden on the circumference Has cam tracks, and with a coupled with the Axialkulisse actuator for moving the cam piece in the direction of both cam tracks.
Ein derartiger Ventiltrieb, der zur variablen Betätigung von Gaswechselventilen mittels verschiebbarer Nocken dient und bei dem ein einziges Betätigungselement je Nockenstück ausreichend ist, um das Nockenstück in Richtung beider Kurvenbahnen der Axialkulisse zu verschieben, ist aus der als gattungsbildend betrachteten
Letztere Ausgestaltung hat den Vorteil, dass der Fertigungsaufwand für die Axialkulisse durch den Entfall des Führungsstegs deutlich kleiner ist. Ein im Hinblick auf die Funktionssicherheit des Ventiltriebs beträchtliches Risiko besteht bei dieser Ausgestaltung jedoch darin, dass der Verschiebevorgang des Nockenstücks nur dann vollständig, d.h. fehlschaltungsfrei abgeschlossen wird, wenn die Massenträgheit des Nockenstücks ausreichend ist, um es nach Durchfahren des Kreuzungsbereichs der Kurvenbahnen auch ohne Zwangseinwirkung des Zylinderstifts gewissermaßen im Freiflug in seine andere Endposition zu bewegen. Voraussetzung für die ausreichende Massenträgheit des Nockenstücks ist selbstverständlich eine Mindestdrehzahl der Nockenwelle, welche direkt von der Reibung zwischen dem Nockenstück und der Trägerwelle abhängig ist. Ein Verschieben des unterhalb dieser Mindestdrehzahl rotierenden Nockenstücks kann dazu führen, dass das Nockenstück "auf halbem Wege" stehen bleibt und ein das Gaswechselventil beaufschlagender Nockenfolger von mehreren Nocken der Nockengruppe unkontrolliert und unter hohen mechanischen Belastungen gleichzeitig beaufschlagt wird. Zudem besteht in diesem Fall keine Möglichkeit mehr, das Nockenstück mittels des Zylinderstifts nachträglich in eine der Endpositionen zu verlagern, da dann die axiale Zuordnung zwischen dem Zylinderstift und den äußeren Führungswänden nicht mehr gegeben ist.The latter embodiment has the advantage that the production cost for the axial slide is significantly smaller due to the omission of the guide bar. A considerable risk in terms of the reliability of the valve train in this embodiment, however, is that the displacement of the cam piece is completed completely, ie without a fault, if the mass inertia of the cam piece is sufficient to pass it through the crossing region of the curved paths without force of the cylinder pin to a certain extent in free flight to move to its other end position. A prerequisite for the sufficient inertia of the cam piece is of course a minimum speed of the camshaft, which directly from the friction between the cam piece and the Carrier shaft is dependent. A displacement of the cam piece rotating below this minimum rotational speed can cause the cam piece to stop "halfway" and a cam follower acting on the gas exchange valve to be acted upon by several cams of the cam group uncontrolled and under high mechanical loads simultaneously. In addition, there is no longer a way in this case to shift the cam piece by means of the cylindrical pin later in one of the end positions, since then the axial assignment between the cylinder pin and the outer guide walls is no longer given.
Dieses Funktionsrisiko ist zwar bei der ersteren Ausgestaltung der Axialkulisse mit mittigem Führungssteg, dessen innere Führungswände bei niedrigen Drehzahlen des Nockenstücks als den Zylinderstift weiter beschleunigende Zwangsführung wirken, deutlich geringer. Dennoch besteht auch hierbei die Gefahr, dass der Zylinderstift nach Durchfahren des Kreuzungsbereichs nicht in die vorgegebene Kurvenbahn einspurt, sondern mit der Stirnseite des Führungsstegs ebenfalls unter hoher mechanischer Belastung kollidiert.Although this function risk is significantly lower in the former embodiment of the Axialkulisse with central guide bar, the inner guide walls act at low speeds of the cam piece as the cylinder pin further accelerating forced operation. Nevertheless, there is also the risk here that the cylindrical pin does not engage in the predetermined curved path after passing through the crossing region, but also collides with the end face of the guide web under high mechanical load.
Ein Ventiltrieb mit den Merkmalen des Oberbegriffs von Anspruch 1 geht ebenfalls aus der
Der vorliegenden Erfindung liegt daher die Aufgabe zugrunde, einen Ventiltrieb der eingangs genannten Art so fortzubilden, dass die genannten Funktionseinschränkungen und -risiken zumindest teilweise beseitigt sind. Konkret ausgedrückt besteht die Aufgabe also darin, bei Verwendung eines einzigen Betätigungselements für beide Verschieberichtungen auch bei niedrigen Drehzahlen der Nockenwelle, beispielsweise während des Startvorgangs der Brennkraftmaschine, einen erfolgreichen, d.h. vollständigen Umschaltvorgang des Nockenstücks zu gewährleisten.The present invention is therefore the object of a valvetrain of the type mentioned in such a way that the said functional limitations and risks are at least partially eliminated. In concrete terms, the object is therefore, when using a single actuator for both Verschieberungen even at low speeds of the camshaft, for example during the starting process of the internal combustion engine, a successful, i. ensure complete switching of the cam piece.
Die Lösung dieser Aufgabe ergibt sich aus den kennzeichnenden Merkmalen des Anspruchs 1, während vorteilhafte Weiterbildungen und Ausgestaltungen der Erfindung den Unteransprüchen entnehmbar sind. Demnach sollen die Kurvenbahnen in Umfangsrichtung der Axialkulisse hintereinander angeordnet sein. Ein wesentlicher Unterschied der Erfindung gegenüber dem bekannten Stand der Technik betrifft also die gegenseitige Anordnung der Kurvenbahnen auf der Axialkulisse, welche nun hintereinander, d.h. in Reihenschaltung, und nicht mehr nebeneinander, d.h. in Parallelschaltung, verlaufen und sich folglich auch nicht mehr kreuzen. Durch den Entfall des Kreuzungsbereichs erfolgt die Verschiebung des Nockenstücks unter permanenter Zwangsführung der Axialkulisse gegenüber dem damit gekoppeltem Betätigungselement, so dass ein vollständiger Umschaltvorgang des Nockenstücks auch bei niedrigsten Drehzahlen der Nockenwelle gewährleistet ist.The solution to this problem arises from the characterizing features of Claim 1, while advantageous developments and refinements of the invention are the dependent claims. Accordingly, the curved paths should be arranged one behind the other in the circumferential direction of the axial slide. A significant difference of the invention over the prior art thus relates to the mutual arrangement of the curved paths on the Axialkulisse, which now consecutively, ie in series, and no longer next to each other, ie in parallel, run and therefore no longer intersect. Due to the omission of the crossing region, the displacement of the cam piece takes place under permanent forced guidance of the axial slide against the actuating element coupled thereto, so that a complete switching operation of the cam piece is ensured even at the lowest rotational speeds of the camshaft.
Hinsichtlich der Kopplung des Betätigungselements mit der Axialkulisse sind die Kurvenbahnen jeweils als Nut und das Betätigungselement als in die Nuten eingreifender Zylinderstift ausgebildet. Vorzugsweise sind dabei die Kurvenbahnen jeweils aus aufeinander folgenden Bahnabschnitten mit unterschiedlichen Axialhüben der die Nut begrenzenden Nutwände zusammengesetzt, nämlich einem Einfahrabschnitt ohne Axialhub, einem Rampenabschnitt und einem Hubabschnitt, wobei der Hubabschnitt eine deutlich größere Axialbeschleunigung als der Rampenabschnitt aufweist.With regard to the coupling of the actuating element with the Axialkulisse the cam tracks are each formed as a groove and the actuating element as engaging in the grooves cylindrical pin. Preferably, the curved paths are each of successive track sections composed with different axial strokes of the groove bounding groove walls, namely an entry section without Axialhub, a ramp section and a lifting section, wherein the lifting section has a significantly greater axial acceleration than the ramp section.
Außerdem sollen die Nocken einen gemeinsamen Grundkreisbereich haben, der spätestens mit dem Rampenabschnitt der ersten Kurvenbahn beginnt und frühestens mit dem Hubabschnitt der zweiten Kurvenbahn endet. Da unter dem gemeinsamen Grundkreisbereich der Winkelbereich des Nockenstücks zu verstehen ist, in welchem sämtliche Nocken der Nockengruppe erhebungsfrei sind, erfolgt die Verschiebung des Nockenstücks lediglich dann, wenn das der Nockengruppe zugeordnete Gaswechselventil geschlossen ist und sich der in Eingriff zu bringende Nocken während des gesamten Verschiebevorgangs ebenfalls in dessen Grundkreisstellung befindet. Somit wirken während des Verschiebevorgangs keine die Reibung zwischen Nockenstück und Trägerwelle erhöhenden Ventilfederkräfte auf das Nockenstück. Um die Axialbeschleunigung des Nockenstücks so gering wie möglich zu halten, sind der Beginn und das Ende vom Grundkreisbereich und vom Verschiebevorgang idealerweise identisch.In addition, the cams should have a common base circle area, which begins at the latest with the ramp portion of the first curved path and ends at the earliest with the lifting portion of the second curved path. Since the common base circle region is to be understood as the angular range of the cam piece in which all the cams of the cam group are free of elevation, the displacement of the cam piece takes place only when the gas exchange valve associated with the cam group is closed and the cam to be engaged during the entire displacement operation also located in its base circle position. Thus, during the displacement process, no valve spring forces increasing the friction between the cam piece and the carrier shaft act on the cam piece. In order to keep the axial acceleration of the cam piece as small as possible, the beginning and the end of the base circle area and of the shifting process are ideally identical.
Ferner können die Hubabschnitte jeweils aus aufeinander folgenden Teilhubabschnitten mit unterschiedlichen Radialhüben des die Nut begrenzenden Nutgrunds zusammengesetzt sein, nämlich einem ersten Teilhubabschnitt ohne Radialhub und einem zweiten Teilhubabschnitt mit sich radial auswärts erhebendem Nutgrund. Im Gegensatz zu den im Stand der Technik bekannten Nutgeometrien, bei denen der Betätigungsstift erst im axialkraftfreien Zustand aus der radial ansteigenden Nut in seine eingriffslose Ruheposition "ausgeworfen" wird, ist es vorliegend zweckmäßig, den Axialhub und den Radialhub der Nut zu überlagern, um den jeweils zur Verfügung stehenden Nockenwinkel der Hubabschnitte zu maximieren und folglich die vergleichsweise hohen Axialbeschleunigungen in den Hubabschnitten auf ein mechanisch beherrschbares Niveau zu beschränken.Further, the lifting sections may each be composed of successive Teilhubabschnitten with different radial strokes of the groove delimiting groove base, namely a first Teilhubabschnitt without radial stroke and a second Teilhubabschnitt with radially outwardly uplifting groove bottom. In contrast to the known in the prior art groove geometries in which the actuating pin is "ejected" only in axialkraftfreien state from the radially rising groove in its non-engaging rest position, it is expedient here to superimpose the Axialhub and the radial stroke of the groove to the each available cam angle of the lift sections to maximize and consequently to limit the comparatively high axial accelerations in the Hubabschnitten to a mechanically manageable level.
Vor demselben Hintergrund ist es schließlich vorgesehen, dass jeweils der zweite Teilhubabschnitt und der Einfahrabschnitt unmittelbar aneinander grenzen, wobei der Nutgrund am Übergang vom zweiten Teilhubabschnitt zum Einfahrabschnitt radial steil abfallend verläuft. Insbesondere bei einem bezüglich des Umfangs der Axialkulisse senkrecht abfallenden Nutgrund, d.h. bei einem Summenwinkel der Kurvenbahnen von 360°, können somit die Nockenwinkel der Hubabschnitte bei gegebener Länge des dazwischen liegenden Einfahrabschnitts maximiert werden.Finally, in the same background, it is provided that each of the second Teilhubabschnitt and the entrance section immediately adjacent to each other, wherein the groove bottom at the transition from the second Teilhubabschnitt to the entry section extends radially steeply sloping. In particular, with respect to the circumference of the Axialkulisse perpendicular sloping groove bottom, ie at a sum angle of the cam tracks of 360 °, thus, the cam angle of the lifting sections can be maximized for a given length of the intermediate section.
Weitere Merkmale der Erfindung ergeben sich auf der nachfolgenden Beschreibung und aus den Zeichnungen, in denen ein Ausführungsbeispiel der Erfindung dargestellt ist. Es zeigen:
- Figur 1
- einen Ausschnitt eines erfindungsgemäßen Ventiltriebs im Längsschnitt;
Figur 2- die Axialkulisse in einer ersten perspektivischen Ansicht X gemäß
;Figur 5 Figur 3- die Axialkulisse in einer zweiten perspektivischen Ansicht Y gemäß
;Figur 5 Figur 4- die Axialkulisse in einer dritten perspektivischen Ansicht Z gemäß
;Figur 5 Figur 5- eine Seitenansicht der Axialkulisse gemäß
Figur 1 mit radialem Steuerdiagramm und Figur 6- ein vollständiges Hubdiagramm der Axialkulisse.
- FIG. 1
- a section of a valve gear according to the invention in longitudinal section;
- FIG. 2
- the axial backdrop in a first perspective view X according to
FIG. 5 ; - FIG. 3
- the axial backdrop in a second perspective view Y according to
FIG. 5 ; - FIG. 4
- the axial backdrop in a third perspective view Z according to
FIG. 5 ; - FIG. 5
- a side view of the axial slide according to
FIG. 1 with radial control diagram and - FIG. 6
- a complete lift diagram of the Axialkulisse.
In
Das Nockenstück 3 weist beidseits einer Lagerstelle 4 angeordnete Nockengruppen mit jeweils zwei unmittelbar benachbarten Nocken 5 und 6 auf, die bei gleichem Grundkreisradius unterschiedliche Nockenerhebungen haben. Das Verschieben des Nockenstücks erfolgt außerhalb der Nockenerhebungen während des gemeinsamen Grundkreisbereichs der Nocken 5, 6. Die Nockenerhebungen werden jeweils in bekannter Weise von einem hier lediglich durch eine Nockenrolle 7 symbolisierten Nockenfolger, wie z.B. einem Schlepphebel, in Abhängigkeit der momentanen Axialposition des Nockenstücks 3 auf ein nicht dargestelltes Gaswechselventil selektiv übertragen. Unter den unterschiedlichen Nockenerhebungen sind unterschiedliche Beträge des jeweiligen Nockenhubs und/oder unterschiedliche Ventilsteuerzeiten der Nocken 5, 6 zu verstehen.The
Zur Umschaltung zwischen den Nocken 5 und 6 ist das Nockenstück 3 mit einer als Einzelteil hergestellten und mittels Pressverband gefügten Axialkulisse 8 versehen. Am Umfang der Axialkulisse 8 sind zwei sich axial gegenläufig erstreckende und in Umfangsrichtung der Axialkulisse 8 hintereinander angeordnete Kurvenbahnen 9, 10 in Form von Nuten ausgebildet, in die ein Betätigungselement 11 einkoppelbar ist. Dies geht näher aus den
Die Gestaltung der Kurvenbahnen 9, 10 ergibt sich aus einer Zusammenschau der
Die beiden Kurvenbahnen 9, 10 setzen sich jeweils aus aufeinander folgenden Bahnabschnitten mit unterschiedlichen Axialhüben (durchgezogene Linie in
Die Hubabschnitte B und E setzen sich jeweils aus aufeinander folgenden Teilhubabschnitten B1 und B2 bzw. E1 und E2 zusammen, die sich im Radialhub des Nutgrunds 13 (gestrichelte Linie in
Analog dazu erfolgt das Zurückschieben des Nockenstücks 3 entlang der zweiten Kurvenbahn 10, d.h. von den dann wirksamen Nocken 6 auf die Nocken 5 dadurch, dass der Zylinderstift 11 in den Einfahrabschnitt C eintaucht und anschließend den Rampenabschnitt D sowie den Hubabschnitt E durchläuft, während das rotierende und sich am Zylinderstift 11 abstützende Nockenstück 3 in seine erste Axialposition zurück verschoben wird. Auch hierbei wird der Zylinderstift 11 im Verlauf des zweiten Teilhubabschnitts E2 durch den radial ansteigenden Nutgrund 13 angehoben und gegen Ende des Verschiebevorgangs vollständig aus der Kurvenbahn 10 in seine eingriffslose Ruheposition ausgeworfen.Similarly, pushing back the
Wie aus den
Die in
Bei den Rastkörpern 15 handelt es sich um einseitig offene, dünnwandige Blechumformteile. Deren offenen Seite ist jeweils als in der Radialbohrung 14 gelagerter und das als Schraubendruckfeder ausgebildete Federmittel 18 umschließender Hohlzylinder ausgebildet, während es sich bei der daran anschließenden geschlossenen Seite jeweils um einen sich in Richtung der Rastnuten 16, 17 verjüngenden Hohlkörper handelt, der zunächst kegelförmig und stirnseitig kugelförmig gestaltet ist. Um während des Verschiebevorgangs des Nockenstücks 3 ein widerstandsarmes Einfahren der Rastkörper 15 in die Radialbohrung 14 zu gewährleisten, sind die Rastkörper 15 im kegelförmigen Bereich des Hohlkörpers mit einer Druckentlastungsöffnung 19 versehen.When the locking
Die Funktion der Rastiervorrichtung beschränkt sich nicht nur auf die Fixierung des Nockenstücks 3 in den beiden Axialpositionen, sondern umfasst auch ein Abbremsen des Nockenstücks 3 in dessen Axialbewegung gegen Ende der Teilhubabschnitte B2 und E2. Dieses Abbremsen wird durch Kontaktreibung der federbelasteten Rastkörper 15 an den beidseits des Scheitelpunkts 20 axial benachbart verlaufenden Nutwänden der Rastnuten 16, 17 erzeugt. Anders als in
- 11
- Nockenwellecamshaft
- 22
- Trägerwellecarrier wave
- 33
- Nockenstückcam piece
- 44
- Lagerstelledepository
- 55
- Nockencam
- 66
- Nockencam
- 77
- Nockenrollecam roller
- 88th
- Axialkulisseaxial slotted
- 99
- erste Kurvenbahnfirst curved track
- 1010
- zweite Kurvenbahnsecond curved track
- 1111
- Betätigungselement / ZylinderstiftActuator / cylinder pin
- 1212
- Nutwandgroove wall
- 1313
- Nutgrundgroove base
- 1414
- Radialbohrungradial bore
- 1515
- Rastkörperlatching body
- 1616
- Rastnutlocking groove
- 1717
- Rastnutlocking groove
- 1818
- Federmittel / SchraubendruckfederSpring means / helical compression spring
- 1919
- DruckentlastungsöffnungPressure relief opening
- 2020
- Scheitelpunkt der RastnutenVertex of Rastnuten
- AA
- Rampenabschnittramp section
- B1,2B1,2
- Hubabschnittstroke section
- CC
- Einfahrabschnittentry section
- DD
- Rampenabschnittramp section
- E1,2E1,2
- Hubabschnittstroke section
- FF
- Einfahrabschnittentry section
Claims (5)
- Valve drive of an internal combustion engine, having a camshaft (1) which comprises a carrier shaft (2) and a cam piece (3) arranged rotationally conjointly on said carrier shaft so as to be displaceable between a first and a second axial position, which cam piece has at least one cam group of directly adjacent cams (5, 6) with different cam elevations and has an axial slotted guide (8) with a first and a second cam track (9, 10), which cam tracks are each in the form of a groove and extend on the circumference of the axial slotted guide (8) axially in opposite directions, and having an actuation element (11) which can be coupled to the axial slotted guide (8) and which is in the form of a cylindrical pin which engages into the grooves (9, 10) and which displaces the cam piece (3) from the first axial position into the second axial position along the first cam track (9) and from the second axial position into the first axial position along the second cam track (10), characterized in that the two cam tracks (9, 10) are arranged in series along the circumference of the axial slotted guide (8), and not adjacent to one another.
- Valve drive according to Claim 1, characterised in that the cam tracks (9, 10) are each made up of successive track sections (F, A, B and C, D, E respectively) with different axial excursions of the groove walls (12) which delimit the groove, specifically a run-in section (F and C respectively) without axial excursion, a ramp section (A and D respectively) and an excursion section (B and E respectively), wherein the excursion section (B and E respectively) exhibits a considerably higher axial acceleration than the ramp section (A and D respectively).
- Valve drive according to Claim 2, characterized in that the cams (5, 6) have a common base circle region which begins at the latest with the ramp section (A) of the first cam track (9) and ends at the earliest with the excursion section (E) of the second cam track (10).
- Valve drive according to Claim 2, characterized in that the excursion sections (B, E) are each made up of successive partial excursion sections (B1, B2 and E1, E2 respectively) with different radial excursions of the groove base (13) which delimits the groove, specifically a first partial excursion section (B1 and E1 respectively) without radial excursion and a second partial excursion section (B2 and E2 respectively) with a groove base (13) that rises in a radially outward direction.
- Valve drive according to Claim 4, characterized in that, in each case, the second partial excursion section (B2 and E2 respectively) and the run-in section (C and F respectively) directly adjoin one another, wherein, at the transition from the second partial excursion section (B2 and E2 respectively) to the run-in section (C and F respectively), the groove base (13) runs in a radially steeply falling manner and, in relation to the circumference of the axial slotted guide (8), preferably a perpendicularly falling manner.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL10704501T PL2396522T3 (en) | 2009-02-14 | 2010-02-01 | Valve train of an internal combustion engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009009080A DE102009009080A1 (en) | 2009-02-14 | 2009-02-14 | Valve gear of an internal combustion engine |
PCT/EP2010/000582 WO2010091798A1 (en) | 2009-02-14 | 2010-02-01 | Valve drive of an internal combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2396522A1 EP2396522A1 (en) | 2011-12-21 |
EP2396522B1 true EP2396522B1 (en) | 2015-06-17 |
Family
ID=41720375
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10704501.5A Active EP2396522B1 (en) | 2009-02-14 | 2010-02-01 | Valve train of an internal combustion engine |
Country Status (8)
Country | Link |
---|---|
US (1) | US8584639B2 (en) |
EP (1) | EP2396522B1 (en) |
KR (1) | KR101602989B1 (en) |
CN (1) | CN102282341B (en) |
DE (2) | DE102009009080A1 (en) |
HU (1) | HUE025402T2 (en) |
PL (1) | PL2396522T3 (en) |
WO (1) | WO2010091798A1 (en) |
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DE102011075537A1 (en) * | 2011-05-10 | 2012-11-15 | Schaeffler Technologies AG & Co. KG | Reciprocating internal combustion engine with camshaft adjusting device |
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-
2009
- 2009-02-14 DE DE102009009080A patent/DE102009009080A1/en not_active Withdrawn
- 2009-02-14 DE DE202009015465U patent/DE202009015465U1/en not_active Expired - Lifetime
-
2010
- 2010-02-01 CN CN201080004890.3A patent/CN102282341B/en not_active Expired - Fee Related
- 2010-02-01 WO PCT/EP2010/000582 patent/WO2010091798A1/en active Application Filing
- 2010-02-01 KR KR1020117018843A patent/KR101602989B1/en active IP Right Grant
- 2010-02-01 US US13/139,813 patent/US8584639B2/en active Active
- 2010-02-01 EP EP10704501.5A patent/EP2396522B1/en active Active
- 2010-02-01 PL PL10704501T patent/PL2396522T3/en unknown
- 2010-02-01 HU HUE10704501A patent/HUE025402T2/en unknown
Also Published As
Publication number | Publication date |
---|---|
KR20110124236A (en) | 2011-11-16 |
KR101602989B1 (en) | 2016-03-11 |
DE102009009080A1 (en) | 2010-08-19 |
DE202009015465U1 (en) | 2010-02-25 |
PL2396522T3 (en) | 2015-11-30 |
US20110247577A1 (en) | 2011-10-13 |
HUE025402T2 (en) | 2016-02-29 |
CN102282341B (en) | 2014-08-20 |
US8584639B2 (en) | 2013-11-19 |
EP2396522A1 (en) | 2011-12-21 |
CN102282341A (en) | 2011-12-14 |
WO2010091798A1 (en) | 2010-08-19 |
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