EP1302630B1 - Device for changing the timing of gas exchange valves of an internal combustion engine, especially a rotary piston phasing device for changing the angle of a camshaft relative to a crank shaft - Google Patents

Device for changing the timing of gas exchange valves of an internal combustion engine, especially a rotary piston phasing device for changing the angle of a camshaft relative to a crank shaft Download PDF

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Publication number
EP1302630B1
EP1302630B1 EP02020920A EP02020920A EP1302630B1 EP 1302630 B1 EP1302630 B1 EP 1302630B1 EP 02020920 A EP02020920 A EP 02020920A EP 02020920 A EP02020920 A EP 02020920A EP 1302630 B1 EP1302630 B1 EP 1302630B1
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EP
European Patent Office
Prior art keywords
locking element
receptacle
drive wheel
pressure
internal combustion
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
EP02020920A
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German (de)
French (fr)
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EP1302630A2 (en
EP1302630A3 (en
Inventor
Eduard Golovatai-Schmidt
Andreas Strauss
Jens Schäfer
Martin Dr. Scheidt
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IHO Holding GmbH and Co KG
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Schaeffler KG
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Publication date
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Publication of EP1302630A3 publication Critical patent/EP1302630A3/en
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Publication of EP1302630B1 publication Critical patent/EP1302630B1/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
    • F01L1/34Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • F01L1/344Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear
    • F01L1/3442Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear using hydraulic chambers with variable volume to transmit the rotating force
    • 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
    • F01L1/34Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • F01L1/344Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear
    • F01L1/3442Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear using hydraulic chambers with variable volume to transmit the rotating force
    • F01L2001/34423Details relating to the hydraulic feeding circuit
    • F01L2001/34436Features or method for avoiding malfunction due to foreign matters in oil
    • 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
    • F01L1/34Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • F01L1/344Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear
    • F01L1/3442Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear using hydraulic chambers with variable volume to transmit the rotating force
    • F01L2001/3445Details relating to the hydraulic means for changing the angular relationship
    • F01L2001/34453Locking means between driving and driven members
    • F01L2001/34469Lock movement parallel to camshaft axis

Definitions

  • the invention relates to a device for changing the timing of gas exchange valves of an internal combustion engine according to the preamble of forming features of claim 1, and it is particularly advantageous to rotary piston adjustment for rotational angle adjustment of a camshaft relative to a crankshaft realized.
  • valve timing control device which is attached to the drive end of a cylinder head mounted in an internal combustion engine camshaft and formed in principle as a function of various operating parameters of the internal combustion engine controllable hydraulic actuator.
  • This device consists essentially of a standing with a crankshaft of the internal combustion engine in drive connection drive wheel and a rotatably connected to a camshaft the internal combustion engine associated impeller, which are in drive connection with each other and transmit the torque of the crankshaft to the camshaft of the internal combustion engine.
  • the drive wheel has a hollow space formed by a hollow cylindrical peripheral wall and two side walls, in which two hydraulic working spaces are formed by two radial boundary walls extending to the longitudinal central axis of the device.
  • the impeller has at the periphery of its hub two radially extending into the working space wings, which divide the working spaces in each case an A-pressure chamber and a B-pressure chamber, which in case of selective or simultaneous pressurization with a hydraulic pressure means pivotal movement or fixation of the impeller relative to the drive wheel and thus cause the camshaft relative to the crankshaft.
  • the impeller when falling below a required for adjustment pressure fluid pressure, such as when switching off the engine by a separate locking element in a preferred base position within its adjustment range with the drive wheel mechanically coupled to, in particular when restarting the internal combustion engine to build up the required pressure medium pressure From the alternating torques of the camshaft resulting stop clatter of the impeller to avoid the boundary walls of the drive wheel.
  • This specifically designed as a stepped cylindrical locking pin locking element is arranged in a direction parallel to the longitudinal center axis of the device bore at the end of a blade of the impeller and displaceable by a spring element into a locking position within a receptacle in the camshaft side facing away from the drive wheel.
  • the formed with a larger diameter portion of the locking pin is formed by the inner wall of the bore in the wing and the formed with a smaller diameter portion of the locking pin, the locking side for exact position determination between the impeller and drive wheel is additionally conical, through an inserted into the bore guide bushing guided.
  • the inclusion of the locking pin is concretely incorporated as in the camshaft side facing away from the drive wheel elongated bore is formed, which extends in a direction transverse to the direction of rotation of the impeller and is connected via a groove with an A-pressure chamber of the device.
  • annular surface formed at the transition between the cylindrical portions of the locking pin is also connected via a radial bore to a B pressure chamber of the device so that both upon pressurization of the A pressure chambers of the device and upon pressurization of the B pressure chambers of the device, the locking pin is hydraulically actuated can be moved into a Entkoppelwolf within the bore in the wing of the impeller.
  • a disadvantage of this known device is that the arrangement of the locking pin in a hole at the end of a wing of the impeller requires a massive construction of the wing and thus limits the number of possible hydraulic working spaces in the device to a maximum of three to four when with Device a conventional adjustment angle of about 30 ° NW should be feasible.
  • the relatively large distance between the longitudinal axis of the bore in the impeller blade and the longitudinal center axis of the device is the cause that reduces the stiffness of the locked connection between the impeller and the drive wheel and that the locking pin is still subject to significant centrifugal forces in the engine operation related with the simultaneously increasing sensitivity to dirt of the lock by the rotationally attached at the end of the wings accumulating dirt particles in the hydraulic pressure medium, the function of the lock can adversely affect.
  • the embodiment of the lock with a stepped cylindrical locking pin which is connected to the annular surface formed between the cylindrical sections and with its locking-side annular surface to both the A-pressure chambers and the B-pressure chambers of the device, has proven to be disadvantageous, that a lock when stopping the engine is not possible because at least one of the two surfaces is still acted on the locking pin with the pressure of the pressure medium and thus holds the locking pin in its Entkoppelwolf in the bore in the wing of the impeller.
  • the device is not operable with a targeted locking and above all unsuitable for applications on SOHC engines or exhaust camshafts, in which a locking of the impeller or the camshaft in an "early" timing of the gas exchange valves of the internal combustion engine is necessary.
  • the locking side conical design of the locking pin with a constant cone angle has also in connection with its elongated receiving bore in the camshaft side facing away from the drive wheel has the disadvantage that in the locking high component loads on the impeller and the drive wheel of the device occur and that there is a danger in the unlocking in that there is a jamming of the locking pin in the receiving bore.
  • the increased space requirement and the relatively high production cost of the stepped locking pin is still to be mentioned as a disadvantage, since these are the cause of a limited applicability of the device in confined spaces in the engine compartment and relatively high production costs of the device.
  • the mechanical coupling is effected by a pin-like locking element movably arranged in an axial bore in the wheel hub of the impeller, which is movable by a spring element into a coupling position within a complementary receptacle in the side wall of the drive wheel.
  • the complementary recording of the locking element is disposed within the pressure medium guide to a volume-minimized A-pressure chamber of a hydraulic working space of the device, so that at the same time the recording of the locking element is pressurized at the start of the internal combustion engine by the pressurization of the A-pressure chambers of the hydraulic working chambers and this against the force its spring element hydraulically moved into its Entkoppelwolf in the axial bore in the wheel hub of the impeller.
  • the invention is therefore based on the object to design a device for changing the timing of gas exchange valves of an internal combustion engine, in particular rotary piston adjustment for rotational angle adjustment of a camshaft relative to a crankshaft, which between its impeller and its drive wheel a simple and inexpensive to produce lock with a has low space requirements, which is largely unaffected by centrifugal forces and insensitive to dirt and which is arranged or designed so that the locked connection between impeller and drive wheel has a high rigidity and that universal use of the device is also possible on SOHC engines or exhaust camshafts ,
  • the object is achieved in that the inclusion of the locking element in one of the side walls of the drive wheel has a quadrangular and formed in its surface by a defined all-sided game greater than the cross-sectional area of the locking element contour and is formed with an opening worm groove for supplying pressure medium, which is connected exclusively to a pressure-free in the locking position of the impeller A-pressure chamber of the device and via which the recording of the locking element can be acted upon only by pressurization of the A-pressure chambers with the pressure of the hydraulic pressure medium.
  • the object is achieved in that the locking element is formed with a chamfer and a rounding of its front edge and a hollow end, while in its rear end face a blind hole for fixing the an end of the preferably designed as a compression coil spring spring element whose other end is supported on an inserted into the axial bore and formed with a centering counter-holder with a Y-shaped profile cross-section, in which the longitudinal grooves formed between its profile legs are also provided for pressure fluid venting the axial bore.
  • the object is achieved in that the receptacle of the locking element is preferably incorporated in the camshaft side facing away from the drive wheel and positioned so that their square-shaped contour with mounted device below the radial end of one of the boundary walls the drive wheel is arranged, wherein its preferably with a quarter-circle course extending to the level of the stop surface of an adjacent boundary wall of the drive wheel worm groove is arranged opening from a lying in the direction of rotation of the impeller in the contour of the recording.
  • this object is achieved in a device according to the preamble of claim 1 such that the locking element is formed as uniform over its entire length locking pin and disposed in an axial bore in the wheel hub of the impeller whose longitudinal axis has a minimum possible distance from the longitudinal central axis of the device ,
  • the receptacle of the locking pin arranged in one of the sidewalls of the drive wheel has a quadrangular contour formed in its surface around a defined all-sided clearance greater than the cross-sectional area of the locking pin and is formed with an opening worm groove for supplying pressure medium is connected to a pressure-free in the locking position of the impeller A-pressure chamber of the device and thus causes the inclusion of the locking pin only when pressurized the pressure chambers of the device with the necessary for unlocking the locking pin pressure of the hydraulic pressure medium can be acted upon.
  • the locking pin is formed at its end facing the receiving end with a phase and a rounding of its front edge and a hollow end, while in its rear end face a blind hole for fixing the having an end of the spring element preferably designed as a compression coil spring.
  • the other end of the spring element is supported by a counter-holder inserted into the axial bore for the locking pin and formed with a centering tip, which preferably has a Y-shaped profile cross-section and in which the longitudinal grooves formed between its profile limbs simultaneously provide the pressure medium venting of the axial bore are.
  • the formation of the receiving end of the locking pin with the described defined contour serves to ensure that the entering during the unlocking process from a certain point torque load of the locking pin does not jamming of the same causes or allows a safe and accelerated unlocking of the locking pin.
  • the constantly increasing pressure of the hydraulic pressure means a relative rotation relative to the game inserted between the impeller and the drive wheel of the device and thereby exerts a shear force or torque on the locking pin occurring on the lateral surface of the locking pin contour edge of its recording.
  • the hollow design of the receiving side end face of the locking pin has proved to reduce the adhesion forces between the face of this end face and the stop surface in the receptacle of the locking pin to be advantageous and thereby contributes that only the adhesion forces between the resulting annular surface on the end face of the locking pin and the stop surface must be overcome in the recording, to a shortening of the unlocking at.
  • the pressure fluid venting takes place regardless of their execution advantageously always against the existing atmospheric pressure and is executable in the same way both chain-driven and belt-driven devices, the vented pressure medium in a chain drive is discharged directly into the cylinder head and belt drives via an additional flange seal on the camshaft-facing side wall of the device in a tank line in the camshaft.
  • the recording of the locking pin is also proposed with respect to the recording of the locking pin to incorporate this in the camshaft side facing away from the drive wheel and position such that the square-shaped contour is arranged at mounted device below the radial end of one of the boundary walls of the drive wheel and their with a quarter-circle course reaching up to the level of the stop surface of an adjacent boundary wall of the drive wheel worm groove opens from a direction of rotation of the impeller into the contour.
  • the side of the opening worm groove opposite side of the contour of the recording is additionally formed with a hardened inlet radius to facilitate the engagement of the locking pin in the recording, while the corners of the contour are rounded with a diameter of the locking pin adapted radius.
  • the reason of the recording also has two different depth levels, of which the upper level is formed as a stop surface for the receiving side end face of the locking pin.
  • the incorporated into the upper level lower level of the receiving ground has a transition to the inflowing worm groove and is provided for supplying the hydraulic pressure medium to the end face of the locking pin.
  • the entering worm groove preferably has a square or approximately square cross-section and is incorporated with a smaller depth than the receptacle in the side wall of the drive wheel.
  • other suitable cross-sections for the worm groove and / or an equal or uniform depth of the worm groove that merges into the lower plane of the receptacle are also conceivable here.
  • the as mentioned above in its surface by a defined game larger than the cross-sectional area of the locking pin formed contour of the recording serves, moreover, on the one hand the balance of the radial bearing clearance between the On the radial end faces of the boundary walls of the drive wheel mounted impeller and the drive wheel and on the other hand, the compensation of production-related position tolerances between the locking pin in the wheel hub of the impeller and its inclusion in the side wall of the drive wheel both in the radial and in the circumferential direction of the device.
  • it allows the enlarged trained recording to adjust during assembly of the device optimal clearance for the locking pin to avoid jamming of the locking pin in the recording.
  • the inventively designed device for changing the timing of gas exchange valves of an internal combustion engine, in particular rotary piston adjustment for rotational adjustment of a camshaft relative to a crankshaft thus has over the known from the prior art devices has the advantage that by the displacement of the locking of a wing of the impeller in the hub of the impeller or by the significant shortening of the distance between the longitudinal axis of the lock and the longitudinal center axis of the device on the one hand substantially increases the rigidity of the locked connection between the impeller and the drive wheel and on the other hand significantly reduces the forces acting on the locking pin during engine operation centrifugal forces become.
  • the inventively designed device has the advantage that the uniformly formed on its entire length locking pin is easy and inexpensive to produce and has a low space requirement, so that the manufacturing cost of the device are further reduced and the device even in confined spaces in the engine compartment is universally applicable.
  • the special design of the recording of the locking pin and standing with the recording operatively connected end face of the locking pin are the cause that no more component loads between the impeller and the drive wheel of the device occur during locking and that when unlocking a jamming of the locking pin in the Recording is no longer possible.
  • connection of the recording of the locking pin exclusively with one of the A-pressure chambers of the device has the particular advantage that a targeted locking of the device when stopping the engine is possible. Since when switching off the internal combustion engine and thus in de-energized control valve of the device, the pressure medium pressure applied to the B-pressure chambers of the device, the impeller is usually rotated under volume minimization of the respective A-pressure chambers of the device in the Necessary for the start of the engine base position in which the Locking pin then locks reliably.
  • the inventively designed device is thus both on intake camshafts with locking in “later "Timing of the gas exchange valves as well as exhaust camshafts and SOHC engines with locking in 'early' timing of the gas exchange valves used.
  • FIGS. 1 and 2 clearly shows a device 1 for changing the timing of gas exchange valves of an internal combustion engine, which is a rotary piston adjusting device for adjusting the rotational angle of a not shown Camshaft with respect to a likewise not shown crankshaft of an internal combustion engine is formed.
  • This device 1 is attached to the drive-side end of a camshaft mounted in the cylinder head of the engine and designed in principle as a hydraulic actuator, which in dependence on various operating parameters of the internal combustion engine by the in FIG. 1 33 is controlled hydraulic valve.
  • the device 1 consists essentially of a standing with the crankshaft of the engine drivingly connected drive wheel 2 and a rotatably connected to the camshaft of the engine impeller 3, wherein the impeller 3 is pivotally mounted in the drive wheel 2 and with this in drive connection stands.
  • the drive wheel 2 in this case has a cavity formed by a hollow cylindrical peripheral wall 4 and two side walls 5, 6, in which five equally circumferentially distributed hydraulic working chambers 9 are formed by five directed to the longitudinal center axis of the device 1 radial boundary walls.
  • the impeller 3 of the device 1 accordingly has on the circumference of its hub 10 five uniformly circumferentially distributed and each radially into a working space 9 of the drive wheel 2 extending wings 11, which divide the working spaces 9 in each case an A-pressure chamber 12 and a B-pressure chamber 13 that cause a pivotal movement or fixation of the impeller 3 with respect to the drive wheel 2 and thus a rotational angle adjustment or hydraulic clamping of the camshaft relative to the crankshaft with selective or simultaneous pressurization with a hydraulic pressure means.
  • the device 1 to avoid a resulting from the alternating torques of the camshaft stop clatter of the impeller 3 at start of the internal combustion engine has a separate locking element 14, with the impeller 3 falls below a required for adjustment pressure medium pressure in a preferred base position within its adjustment range with the Drive wheel 2 is mechanically coupled.
  • This locking element 14 is in arranged parallel to the longitudinal center axis of the device 1 bore in the impeller 3 and displaceable by a spring element 15 in a locking position within a receptacle 16 in the side wall 5 of the drive wheel 2.
  • FIGS. 1 to 3 is in this respect still be removed that the locking element 14 is formed according to the invention as uniform over its entire length locking pin, which is arranged in a continuous axial bore 17 in the hub 10 of the impeller 3.
  • the longitudinal axis of this axial bore 17 has the smallest possible distance from the longitudinal central axis of the device 1, in order to minimize the centrifugal force influences on the locking element 14 that arise during engine operation.
  • the locking element 14, as shown FIG. 3 emerges on the receiving side formed with a phase 19 and a rounding 20 of its front edge, which accelerate the axial movement of the locking element 14 in its unlocked position while avoiding it in jamming.
  • Adhesion forces of the locking element 14 in the receptacle 16 are additionally avoided by the hollow formation of the front end 21 of the locking element 14, which is also visible in FIG. 3.
  • the locking element 14 On its rear end face 22, however, the locking element 14 has a blind bore 23 in which, as well as from FIG. 3 can be removed, which is fixed one end of the compression spring designed as a spring element 15.
  • the other end of this spring element 15 is supported on an inserted into the axial bore 17 and formed with a centering tip 24 abutment 15, which has a Y-shaped profile cross-section and in which the longitudinal grooves formed between its profile legs 26 at the same time for pressure fluid venting the axial bore 17 are provided.
  • recognizable receptacle 16 of the locking element 14 further has according to the invention a quadrangular and in its surface by a defined all-sided game greater than the cross-sectional area of the locking member 14 formed contour and is formed with an opening worm groove 18, which only with an unpressurized in locking position A-pressure chamber 12 of the device 1 is connected. This ensures that the receptacle 16 of the locking element 14 is acted upon only upon pressurization of the A-pressure chambers 12 of the device 1 via the worm groove 18 with the pressure of the hydraulic pressure medium and thus the locking member 14 is moved to its unlocked position.
  • FIG. 4 It can be seen that the receptacle 16 of the locking element 14 is incorporated into the side wall 5 of the drive wheel 2 facing away from the camshaft and is positioned such that its quadrangular contour is arranged below the radial end face 27 of a limiting wall 7 of the drive wheel 2, indicated by dashed lines in the drawing.
  • the worm groove 18 has a quarter-circle course up to the level of the stop surface 28 of an adjacent boundary wall 8, also shown in phantom, and opens into the contour of the receptacle 16 from a side lying in the direction of rotation of the impeller 3.
  • the side of the worm groove 18 opposite side of the contour of the receptacle 16, however, as the magnifications of FIGS.
  • FIGS. 5 and 6 show, formed with a hardened inlet radius 29, which facilitates the engagement of the locking element 14 in the receptacle 16.
  • the unspecified corners of the contour with a diameter of the locking pin 14 corresponding radius are rounded and that the bottom of the receptacle 16 has two different depths levels 30, 31.
  • the upper level 30 is formed as a stop surface of the locking pin 14 in the receptacle 16, while the incorporated into the upper level 30 lower level 31 has a transition 32 to the opening worm groove 18 and is provided for supplying the hydraulic pressure medium to the end 21 of the locking element 14 ,

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve Device For Special Equipments (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Description

Bezeichnung der ErfindungName of the invention

Vorrichtung zum Verändern der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine, insbesondere Rotationskolben-Verstelleinrichtung zur Drehwinkelverstellung einer Nockenwelle gegenüber einer KurbelwelleDevice for changing the timing of gas exchange valves of an internal combustion engine, in particular rotary piston adjusting device for adjusting the rotational angle of a camshaft relative to a crankshaft

Beschreibungdescription Gebiet der ErfindungField of the invention

Die Erfindung betrifft eine Vorrichtung zum Verändern der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine nach den oberbegriffsbildenden Merkmalen des Anspruchs 1, und sie ist insbesondere vorteilhaft an Rotationskolben-Verstelleinrichtung zur Drehwinkelverstellung einer Nockenwelle gegenüber einer Kurbelwelle realisierbar.The invention relates to a device for changing the timing of gas exchange valves of an internal combustion engine according to the preamble of forming features of claim 1, and it is particularly advantageous to rotary piston adjustment for rotational angle adjustment of a camshaft relative to a crankshaft realized.

Hintergrund der ErfindungBackground of the invention

Aus der DE 196 23 818 A1 ist eine gattungsbildende Ventilsteuerzeiten-Regel-vorrichtung bekannt, die am antriebsseitigen Ende einer im Zylinderkopf einer Brennkraftmaschine gelagerten Nockenwelle befestigt und im Prinzip als in Abhängigkeit verschiedener Betriebsparameter der Brennkraftmaschine steuerbarer hydraulischer Stellantrieb ausgebildet ist. Diese Vorrichtung besteht im Wesentlichen aus einem mit einer Kurbelwelle der Brennkraftmaschine in Antriebsverbindung stehenden Antriebsrad und aus einem drehfest mit einer Nockenwelle der Brennkraftmaschine verbundenen Flügelrad, welche miteinander in Antriebsverbindung stehen und das Drehmoment der Kurbelwelle auf die Nockenwelle der Brennkraftmaschine übertragen. In einer bevorzugten Ausführungsform weist dabei das Antriebsrad einen durch eine hohlzylindrische Umfangswand und zwei Seitenwände gebildeten Hohlraum auf, in dem durch zwei sich zur Längsmittelachse der Vorrichtung erstreckende radiale Begrenzungswände zwei hydraulische Arbeitsräume gebildet werden. Das Flügelrad weist dementsprechend am Umfang seiner Radnabe zwei sich radial in die Arbeitsräume erstreckende Flügel auf, welche die Arbeitsräume in jeweils eine A-Druckkammer und eine B-Druckkammer unterteilen, die bei wahlweiser oder gleichzeitiger Druckbeaufschlagung mit einem hydraulischen Druckmittel eine Schwenkbewegung oder Fixierung des Flügelrades gegenüber dem Antriebsrad und damit der Nockenwelle gegenüber der Kurbelwelle bewirken. Darüber hinaus ist das Flügelrad bei Unterschreitung eines zur Verstellung erforderlichen Druckmitteldrucks, wie beispielsweise beim Abschalten der Brennkraftmaschine, durch ein gesondertes Verriegelungselement in einer bevorzugten Basisposition innerhalb seines Verstellbereiches mit dem Antriebsrad mechanisch koppelbar, um insbesondere beim Neustart der Brennkraftmaschine bis zum Aufbau des erforderlichen Druckmitteldrucks ein aus den Wechselmomenten der Nockenwelle resultierendes Anschlagklappern des Flügelrades an den Begrenzungswänden des Antriebsrades zu vermeiden. Dieses, konkret als abgestufter zylindrischer Verriegelungsstift ausgebildetes Verriegelungselement ist in einer zur Längsmittelachse der Vorrichtung parallelen Bohrung am Ende eines Flügels des Flügelrades angeordnet und durch ein Federelement in eine Verriegelungsstellung innerhalb einer Aufnahme in der nockenwellenabgewandten Seitenwand des Antriebsrades verschiebbar. Dabei wird der mit einem größeren Durchmesser ausgebildete Abschnitt des Verriegelungsstiftes durch die Innenwandung der Bohrung im Flügel und der mit einem geringeren Durchmesser ausgebildete Abschnitt des Verriegelungsstiftes, der verriegelungsseitig zur exakten Lagebestimmung zwischen Flügelrad und Antriebsrad zusätzlich konisch ausgeführt ist, durch eine in die Bohrung eingesetzte Führungsbuchse geführt. Die Aufnahme des Verriegelungsstiftes ist konkret als in die nockenwellenabgewandte Seitenwand des Antriebsrades eingearbeitete längliche Bohrung ausgebildet, die sich in eine Richtung quer zur Drehrichtung des Flügelrades erstreckt und über eine Nut mit einer A-Druckkammer der Vorrichtung verbunden ist. Zusätzlich ist die am Übergang zwischen den zylindrischen Abschnitten des Verriegelungsstiftes entstehende Ringfläche über eine Radialbohrung auch mit einer B-Druckkammer der Vorrichtung verbunden, so dass sowohl bei Druckbeaufschlagung der A-Druckkammern der Vorrichtung als auch bei Druckbeaufschlagung der B-Druckkammern der Vorrichtung der Verriegelungsstift hydraulisch in eine Entkoppelstellung innerhalb der Bohrung im Flügel des Flügelrades bewegt werden kann.From the DE 196 23 818 A1 is a generic type valve timing control device known, which is attached to the drive end of a cylinder head mounted in an internal combustion engine camshaft and formed in principle as a function of various operating parameters of the internal combustion engine controllable hydraulic actuator. This device consists essentially of a standing with a crankshaft of the internal combustion engine in drive connection drive wheel and a rotatably connected to a camshaft the internal combustion engine associated impeller, which are in drive connection with each other and transmit the torque of the crankshaft to the camshaft of the internal combustion engine. In a preferred embodiment, the drive wheel has a hollow space formed by a hollow cylindrical peripheral wall and two side walls, in which two hydraulic working spaces are formed by two radial boundary walls extending to the longitudinal central axis of the device. Accordingly, the impeller has at the periphery of its hub two radially extending into the working space wings, which divide the working spaces in each case an A-pressure chamber and a B-pressure chamber, which in case of selective or simultaneous pressurization with a hydraulic pressure means pivotal movement or fixation of the impeller relative to the drive wheel and thus cause the camshaft relative to the crankshaft. In addition, the impeller when falling below a required for adjustment pressure fluid pressure, such as when switching off the engine by a separate locking element in a preferred base position within its adjustment range with the drive wheel mechanically coupled to, in particular when restarting the internal combustion engine to build up the required pressure medium pressure From the alternating torques of the camshaft resulting stop clatter of the impeller to avoid the boundary walls of the drive wheel. This, specifically designed as a stepped cylindrical locking pin locking element is arranged in a direction parallel to the longitudinal center axis of the device bore at the end of a blade of the impeller and displaceable by a spring element into a locking position within a receptacle in the camshaft side facing away from the drive wheel. In this case, the formed with a larger diameter portion of the locking pin is formed by the inner wall of the bore in the wing and the formed with a smaller diameter portion of the locking pin, the locking side for exact position determination between the impeller and drive wheel is additionally conical, through an inserted into the bore guide bushing guided. The inclusion of the locking pin is concretely incorporated as in the camshaft side facing away from the drive wheel elongated bore is formed, which extends in a direction transverse to the direction of rotation of the impeller and is connected via a groove with an A-pressure chamber of the device. In addition, the annular surface formed at the transition between the cylindrical portions of the locking pin is also connected via a radial bore to a B pressure chamber of the device so that both upon pressurization of the A pressure chambers of the device and upon pressurization of the B pressure chambers of the device, the locking pin is hydraulically actuated can be moved into a Entkoppelstellung within the bore in the wing of the impeller.

Nachteilig bei dieser bekannten Vorrichtung ist es jedoch, dass die Anordnung des Verriegelungsstiftes in einer Bohrung am Ende eines Flügels des Flügelrades eine massive Bauweise der Flügel bedingt und somit die Zahl der möglichen hydraulischen Arbeitsräume in der Vorrichtung auf maximal drei bis vier begrenzt, wenn mit der Vorrichtung ein üblicher Verstellwinkel von ca. 30° NW realisierbar sein soll. Darüber hinaus ist die relativ große Entfernung zwischen der Längsachse der Bohrung im Flügel des Flügelrades und der Längsmittelachse der Vorrichtung ursächlich dafür, dass sich die Steifigkeit der verriegelten Verbindung zwischen Flügelrad und Antriebsrad verringert und dass der Verriegelungsstift im Motorbetrieb noch erheblichen Fliehkräften unterliegt, die im Zusammenhang mit der gleichzeitig steigenden Schmutzempfindlichkeit der Verriegelung durch die sich rotationsbedingt am Ende der Flügel anlagernden Schmutzpartikel im hydraulischen Druckmittel die Funktion der Verriegelung nachteilig beeinträchtigen können. Ebenso hat sich die Ausführung der Verriegelung mit einem abgestuften zylindrischen Verriegelungsstift, der mit der zwischen den zylindrischen Abschnitten entstehenden Ringfläche und mit seiner verriegelungsseitigen Ringfläche sowohl mit den A-Druckkammern als auch mit den B-Druckkammern der Vorrichtung verbunden ist, dahingehend als nachteilig erwiesen, dass eine Verriegelung beim Abstellen des Motors nicht möglich ist, da mindestens eine der beiden Flächen am Verriegelungsstift noch mit dem Druck des Druckmittels beaufschlagt ist und somit den Verriegelungsstift in seiner Entkoppelstellung in der Bohrung im Flügel des Flügelrades hält. Dadurch ist die Vorrichtung nicht mit einer gezielten Verriegelung betreibbar und vor allem für Anwendungen an SOHC-Motoren oder an Auslassnockenwellen ungeeignet, bei denen eine Verriegelung des Flügelrades beziehungsweise der Nockenwelle in einer "frühen" Steuerzeitenlage der Gaswechselventile der Brennkraftmaschine notwendig ist. Die verriegelungsseitig konische Ausführung des Verriegelungsstiftes mit einem konstanten Kegelwinkel hat darüber hinaus im Zusammenhang mit dessen länglicher Aufnahmebohrung in der nockenwellenabgewandten Seitenwand des Antriebsrades den Nachteil, dass bei der Verriegelung hohe Bauteilbelastungen am Flügelrad und am Antriebsrad der Vorrichtung auftreten und dass bei der Entriegelung die Gefahr besteht, dass es zum Verklemmen des Verriegelungsstiftes in der Aufnahmebohrung kommt. Zusätzlich ist der erhöhte Bauraumbedarf und der relativ hohe Fertigungsaufwand für den abgestuften Verriegelungsstift noch als Nachteil zu nennen, da diese ursächlich für eine beschränkte Anwendbarkeit der Vorrichtung bei beengten Platzverhältnissen im Motorraum und für relativ hohe Herstellungskosten der Vorrichtung sind.A disadvantage of this known device, however, is that the arrangement of the locking pin in a hole at the end of a wing of the impeller requires a massive construction of the wing and thus limits the number of possible hydraulic working spaces in the device to a maximum of three to four when with Device a conventional adjustment angle of about 30 ° NW should be feasible. In addition, the relatively large distance between the longitudinal axis of the bore in the impeller blade and the longitudinal center axis of the device is the cause that reduces the stiffness of the locked connection between the impeller and the drive wheel and that the locking pin is still subject to significant centrifugal forces in the engine operation related with the simultaneously increasing sensitivity to dirt of the lock by the rotationally attached at the end of the wings accumulating dirt particles in the hydraulic pressure medium, the function of the lock can adversely affect. Likewise, the embodiment of the lock with a stepped cylindrical locking pin, which is connected to the annular surface formed between the cylindrical sections and with its locking-side annular surface to both the A-pressure chambers and the B-pressure chambers of the device, has proven to be disadvantageous, that a lock when stopping the engine is not possible because at least one of the two surfaces is still acted on the locking pin with the pressure of the pressure medium and thus holds the locking pin in its Entkoppelstellung in the bore in the wing of the impeller. As a result, the device is not operable with a targeted locking and above all unsuitable for applications on SOHC engines or exhaust camshafts, in which a locking of the impeller or the camshaft in an "early" timing of the gas exchange valves of the internal combustion engine is necessary. The locking side conical design of the locking pin with a constant cone angle has also in connection with its elongated receiving bore in the camshaft side facing away from the drive wheel has the disadvantage that in the locking high component loads on the impeller and the drive wheel of the device occur and that there is a danger in the unlocking in that there is a jamming of the locking pin in the receiving bore. In addition, the increased space requirement and the relatively high production cost of the stepped locking pin is still to be mentioned as a disadvantage, since these are the cause of a limited applicability of the device in confined spaces in the engine compartment and relatively high production costs of the device.

Aus der DE 199 29 393 A1 ist eine weitere Ventilsteuerzeiten-Regel-vorrichtung bekannt. Hier erfolgt die mechanische Koppelung durch ein in einer Axialbohrung in der Radnabe des Flügelrades beweglich angeordnetes pinartiges Verriegelungselement, welches durch ein Federelement in eine Koppelstellung innerhalb einer komplementären Aufnahme in der Seitenwand des Antriebsrades bewegbar ist. Die komplementäre Aufnahme des Verriegelungselementes ist innerhalb der Druckmittelführung zu einer volumenminimierten A-Druckkammer eines hydraulischen Arbeitsraumes der Vorrichtung angeordnet, so dass beim Start der Brennkraftmaschine durch die Druckbeaufschlagung der A-Druckkammern der hydraulischen Arbeitsräume gleichzeitig die Aufnahme des Verriegelungselementes druckbeaufschlagt wird und dieses entgegen der Kraft seines Federelementes hydraulisch in seine Entkoppelstellung in der Axialbohrung in der Radnabe des Flügelrades bewegt.From the DE 199 29 393 A1 another valve timing control device is known. Here, the mechanical coupling is effected by a pin-like locking element movably arranged in an axial bore in the wheel hub of the impeller, which is movable by a spring element into a coupling position within a complementary receptacle in the side wall of the drive wheel. The complementary recording of the locking element is disposed within the pressure medium guide to a volume-minimized A-pressure chamber of a hydraulic working space of the device, so that at the same time the recording of the locking element is pressurized at the start of the internal combustion engine by the pressurization of the A-pressure chambers of the hydraulic working chambers and this against the force its spring element hydraulically moved into its Entkoppelstellung in the axial bore in the wheel hub of the impeller.

Aufgabe der ErfindungObject of the invention

Der Erfindung liegt deshalb die Aufgabe zu Grunde, eine Vorrichtung zum Verändern der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine, insbesondere Rotationskolben-Verstelleinrichtung zur Drehwinkelverstellung einer Nockenwelle gegenüber einer Kurbelwelle, zu konzipieren, welche zwischen ihrem Flügelrad und ihrem Antriebsrad eine einfache und kostengünstig herstellbare Verriegelung mit einem geringen Bauraumbedarf aufweist, die weitestgehend von Fliehkräften unbeeinflussbar sowie schmutzunempfindlich ist und welche so angeordnet bzw. ausgebildet ist, dass die verriegelte Verbindung zwischen Flügelrad und Antriebsrad eine hohe Steifigkeit aufweist und dass ein universeller Einsatz der Vorrichtung auch an SOHC-Motoren oder an Auslassnockenwellen möglich ist.The invention is therefore based on the object to design a device for changing the timing of gas exchange valves of an internal combustion engine, in particular rotary piston adjustment for rotational angle adjustment of a camshaft relative to a crankshaft, which between its impeller and its drive wheel a simple and inexpensive to produce lock with a has low space requirements, which is largely unaffected by centrifugal forces and insensitive to dirt and which is arranged or designed so that the locked connection between impeller and drive wheel has a high rigidity and that universal use of the device is also possible on SOHC engines or exhaust camshafts ,

Zusammenfassung der ErfindungSummary of the invention

In einer ersten Ausführungsform der Vorrichtung nach dem Oberbegriff des Anspruchs 1 wird die Aufgabe erfindungsgemäß dadurch gelöst, dass die Aufnahme des Verriegelungselementes in einer der Seitenwände des Antriebsrades eine viereckförmige und in ihrer Fläche um ein definiertes allseitiges Spiel größer als die Querschnittsfläche des Verriegelungselementes ausgebildete Kontur aufweist und mit einer einmündenden Wurmnut zur Druckmittelzuführung ausgebildet ist, die ausschließlich mit einer in Verriegelungsstellung des Flügelrades drucklosen A-Druckkammer der Vorrichtung verbunden ist und über welche die Aufnahme des Verriegelungselementes nur bei Druckbeaufschlagung der A-Druckkammern mit dem Druck des hydraulischen Druckmittels beaufschlagbar ist.In a first embodiment of the device according to the preamble of claim 1, the object is achieved in that the inclusion of the locking element in one of the side walls of the drive wheel has a quadrangular and formed in its surface by a defined all-sided game greater than the cross-sectional area of the locking element contour and is formed with an opening worm groove for supplying pressure medium, which is connected exclusively to a pressure-free in the locking position of the impeller A-pressure chamber of the device and via which the recording of the locking element can be acted upon only by pressurization of the A-pressure chambers with the pressure of the hydraulic pressure medium.

In einer weiteren Ausführungsform der Vorrichtung nach dem Oberbegriff des Anspruchs 1 wird die Aufgabe erfindungsgemäß dadurch gelöst, dass das Verriegelungselement mit einer Fase und einer Verrundung seiner stirnseitigen Kante sowie mit einer hohlen Stirnseite ausgebildet ist, während es in seiner rückseitigen Stirnseite eine Grundbohrung zur Fixierung des einen Endes des bevorzugt als Druckschraubenfeder ausgebildeten Federelementes aufweist dessen anderes Ende sich an einem in die Axialbohrung eingesetzten und mit einer Zentrierspitze ausgebildeten Gegenhalter mit einem Y-förmigen Profilquerschnitt abstützt, bei welchem die zwischen seinen Profilschenkeln gebildeten Längsnuten zugleich zur Druckmittel-Entlüftung der Axialbohrung vorgesehen sind.In a further embodiment of the device according to the preamble of claim 1, the object is achieved in that the locking element is formed with a chamfer and a rounding of its front edge and a hollow end, while in its rear end face a blind hole for fixing the an end of the preferably designed as a compression coil spring spring element whose other end is supported on an inserted into the axial bore and formed with a centering counter-holder with a Y-shaped profile cross-section, in which the longitudinal grooves formed between its profile legs are also provided for pressure fluid venting the axial bore.

In einer weiteren Ausführungsform der Vorrichtung nach dem Oberbegriff des Anspruchs 1 wird die Aufgabe erfindungsgemäß dadurch gelöst, dass die Aufnahme des Verriegelungselementes bevorzugt in die nockenwellenabgewandte Seitenwand des Antriebsrades eingearbeitet und derart positioniert ist, dass deren viereckförmige Kontur bei montierter Vorrichtung unterhalb der Radialstirnseite einer der Begrenzungswände des Antriebsrades angeordnet ist, wobei deren bevorzugt mit einem viertelkreisförmigen Verlauf bis in Höhe der Anschlagfläche einer benachbarten Begrenzungswand des Antriebsrades reichende Wurmnut von einer in Drehrichtung des Flügelrades liegenden Seite aus in die Kontur der Aufnahme einmündend angeordnet ist.In a further embodiment of the device according to the preamble of claim 1, the object is achieved in that the receptacle of the locking element is preferably incorporated in the camshaft side facing away from the drive wheel and positioned so that their square-shaped contour with mounted device below the radial end of one of the boundary walls the drive wheel is arranged, wherein its preferably with a quarter-circle course extending to the level of the stop surface of an adjacent boundary wall of the drive wheel worm groove is arranged opening from a lying in the direction of rotation of the impeller in the contour of the recording.

Erfindungsgemäß wird diese Aufgabe bei einer Vorrichtung nach dem Oberbegriff des Anspruchs 1 derart gelöst, dass das Verriegelungselement als auf seiner gesamten Länge gleichmäßig zylindrischer Verriegelungsstift ausgebildet und in einer Axialbohrung in der Radnabe des Flügelrades angeordnet ist, deren Längsachse einen geringstmöglichen Abstand zur Längsmittelachse der Vorrichtung aufweist.According to the invention, this object is achieved in a device according to the preamble of claim 1 such that the locking element is formed as uniform over its entire length locking pin and disposed in an axial bore in the wheel hub of the impeller whose longitudinal axis has a minimum possible distance from the longitudinal central axis of the device ,

In zweckmäßiger Weiterbildung der erfindungsgemäß ausgebildeten Vorrichtung weist dabei die in einer der Seitenwände des Antriebsrades angeordnete Aufnahme des Verriegelungsstiftes eine viereckförmige und in ihrer Fläche um ein definiertes allseitiges Spiel größer als die Querschnittsfläche des Verriegelungsstiftes ausgebildete Kontur auf und ist mit einer einmündenden Wurmnut zur Druckmittelzuführung ausgebildet die mit einer in Verriegelungsstellung des Flügelrades drucklosen A-Druckkammer der Vorrichtung verbunden ist und somit bewirkt, dass die Aufnahme des Verriegelungsstiftes nur bei Druckbeaufschlagung der Druckkammern der Vorrichtung mit dem zur Entriegelung des Verriegelungsstiftes notwendigen Druck des hydraulischen Druckmittels beaufschlagbar ist.In an expedient development of the device according to the invention, the receptacle of the locking pin arranged in one of the sidewalls of the drive wheel has a quadrangular contour formed in its surface around a defined all-sided clearance greater than the cross-sectional area of the locking pin and is formed with an opening worm groove for supplying pressure medium is connected to a pressure-free in the locking position of the impeller A-pressure chamber of the device and thus causes the inclusion of the locking pin only when pressurized the pressure chambers of the device with the necessary for unlocking the locking pin pressure of the hydraulic pressure medium can be acted upon.

Als vorteilhafte Ausgestaltung der erfindungsgemäß ausgebildeten Vorrichtung wird es darüber hinaus vorgeschlagen, dass der Verriegelungsstift an seinem zur Aufnahme weisenden Ende mit einer Phase und einer Verrundung seiner stirnseitigen Kante sowie mit einer hohlen Stirnseite ausgebildet ist, während er in seiner rückseitigen Stirnseite eine Grundbohrung zur Fixierung des einen Endes des bevorzugt als Druckschraubenfeder ausgebildeten Federelementes aufweist. Das andere Ende des Federelementes stützt sich dabei an einem in die Axialbohrung für den Verriegelungsstift eingesetzten und mit einer Zentrierspitze ausgebildeten Gegenhalter ab, der bevorzugt einen Y-förmigen Profilquerschnitt aufweist und bei welchem die zwischen seinen Profilschenkeln gebildeten Längsnuten zugleich zur Druckmittel-Entlüftung der Axialbohrung vorgesehen sind.
Die Ausbildung des aufnahmeseitigen Endes des Verriegelungsstiftes mit der beschriebenen definierten Kontur dient dabei der Sicherstellung, dass die während des Entriegelungsvorgangs ab einem bestimmten Punkt eintretende Drehmomentbelastung des Verriegelungsstiftes nicht ein Verklemmen des selben verursacht bzw. ein sicheres und beschleunigtes Entriegeln des Verriegelungsstiftes ermöglicht. An diesem, kurz nach beginnender Druckbeaufschlagung der A-Druckkammern der Vorrichtung und der mit diesen verbundenen Aufnahme des Verriegelungsstiftes entsprechenden Punkt weist der Verriegelungsstift eine noch nicht vollständig in seine Entriegelungsstellung verschobene Stellung auf, in der durch den ständig ansteigenden Druck des hydraulischen Druckmittels eine spielbedingte Relativverdrehung zwischen dem Flügelrad und dem Antriebsrad der Vorrichtung einsetzt und die dadurch auf die Mantelfläche des Verriegelungsstiftes auftretende Konturkante seiner Aufnahme eine Scherkraft bzw. ein Drehmoment auf den Verriegelungsstift ausübt. Da das aufnahmeseitige Ende des Verriegelungsstiftes an diesem Punkt jedoch die erwähnte Phase und die sich anschließende Verrundung der stirnseitigen Kante aufweist, wird somit einerseits ein Verklemmen des Verriegelungsstiftes vermieden und andererseits ein zusätzlicher abrollbedingter Katapulteffekt erzeugt, bei welchem das wirkende Drehmoment in eine Axialkraft umgewandelt und zur Beschleunigung der Axialbewegung des Verriegelungsstiftes in seine Entriegelungsstellung genutzt wird.
As an advantageous embodiment of the device according to the invention, it is also proposed that the locking pin is formed at its end facing the receiving end with a phase and a rounding of its front edge and a hollow end, while in its rear end face a blind hole for fixing the having an end of the spring element preferably designed as a compression coil spring. The other end of the spring element is supported by a counter-holder inserted into the axial bore for the locking pin and formed with a centering tip, which preferably has a Y-shaped profile cross-section and in which the longitudinal grooves formed between its profile limbs simultaneously provide the pressure medium venting of the axial bore are.
The formation of the receiving end of the locking pin with the described defined contour serves to ensure that the entering during the unlocking process from a certain point torque load of the locking pin does not jamming of the same causes or allows a safe and accelerated unlocking of the locking pin. At this, shortly after the beginning of pressurizing the A-pressure chambers of the device and the corresponding associated with this recording of the locking pin point of the locking pin has not yet completely shifted into its unlocked position, in the game by the constantly increasing pressure of the hydraulic pressure means a relative rotation relative to the game inserted between the impeller and the drive wheel of the device and thereby exerts a shear force or torque on the locking pin occurring on the lateral surface of the locking pin contour edge of its recording. Since the receiving end of the locking pin at this point, however, the mentioned phase and the subsequent rounding of the front edge, thus on the one hand jamming of the locking pin is avoided and on the other hand creates an additional roll-induced catapult effect, in which the acting torque is converted into an axial force and used to accelerate the axial movement of the locking pin in its unlocked position.

Die hohle Ausbildung der aufnahmeseitigen Stirnseite des Verriegelungsstiftes hat sich dagegen zur Verringerung der Adhäsionskräfte zwischen der Fläche dieser Stirnseite und der Anschlagfläche in der Aufnahme des Verriegelungsstiftes als vorteilhaft erwiesen und trägt dadurch, dass nur noch die Adhäsionskräfte zwischen der entstehenden Ringfläche an der Stirnseite des Verriegelungsstiftes und der Anschlagfläche in der Aufnahme überwunden werden müssen, zu einer Verkürzung der Entriegelungszeit bei.The hollow design of the receiving side end face of the locking pin, however, has proved to reduce the adhesion forces between the face of this end face and the stop surface in the receptacle of the locking pin to be advantageous and thereby contributes that only the adhesion forces between the resulting annular surface on the end face of the locking pin and the stop surface must be overcome in the recording, to a shortening of the unlocking at.

Hinsichtlich der in der rückseitigen Stirnseite des Verriegelungsstiftes angeordneten Grundbohrung, in der das eine Ende des als Druckschraubenfeder ausgebildeten Federelementes fixiert wird, besteht alternativ auch die Möglichkeit, diese komplett wegfallen zulassen, wenn die verwendete Druckschraubenfeder nicht wie vorgesehen im Durchmesser kleiner als der Verriegelungsstift sondern annähernd den gleichen Durchmesser aufweist oder wenn anstelle der Druckschraubenfeder beispielsweise eine einseitig den Durchmesser des Verriegelungsstiftes aufweisende Kegelfeder zur Anwendung kommt. Ebenso ist es möglich, das andere Ende des Federelementes statt an der Zentrierspitze des beschriebenen Gegenhalters an einem als eingesetzte Buchse oder in anderer geeigneter Weise ausgebildeten Gegenhalter abzustützen, welcher eine zentrische und/oder mehrere konzentrische Bohrungen zur Druckmittel-Entlüftung der Axialbohrung aufweist, oder auch die Axialbohrung als Stufenbohrung auszubilden, bei welcher der entstehende Absatz der Bohrung zur Abstützung des anderen Endes des Federelementes genutzt wird und die Druckmittel-Entlüftung durch den durchmesserverringerten Teil der Axialbohrung erfolgt. Die Druckmittel-Entlüftung erfolgt dabei unabhängig von deren Ausführung vorteilhafter weise immer gegen den bestehenden atmosphärischen Druck und ist in gleicher Weise sowohl an kettengetriebenen als auch an riemengetriebenen Vorrichtungen ausführbar, wobei das entlüftete Druckmittel bei einem Kettentrieb direkt in den Zylinderkopf und bei Riementrieben über eine zusätzliche Flanschdichtung an der nockenwellenzugewandten Seitenwand der Vorrichtung in eine Tankleitung in der Nockenwelle abgeführt wird.With regard to the arranged in the rear end face of the locking pin bottom hole in which one end of the spring coil formed as a compression spring element is fixed, alternatively there is also the possibility to completely omit them, if the compression coil spring used not smaller than intended in diameter smaller than the locking pin but approximate has the same diameter or if instead of the compression coil spring, for example, a one-sided the diameter of the locking pin having conical spring is used. It is also possible to support the other end of the spring element instead of the centering of the described counter-holder on a used as a socket or other suitable counter-holder, which has a central and / or more concentric bores for pressure medium venting of the axial bore, or form the axial bore as a stepped bore, in which the resulting shoulder of the bore is used to support the other end of the spring element and the pressure medium venting takes place through the diameter-reduced part of the axial bore. The pressure fluid venting takes place regardless of their execution advantageously always against the existing atmospheric pressure and is executable in the same way both chain-driven and belt-driven devices, the vented pressure medium in a chain drive is discharged directly into the cylinder head and belt drives via an additional flange seal on the camshaft-facing side wall of the device in a tank line in the camshaft.

Als weitere zweckmäßige Weiterbildung der erfindungsgemäß ausgebildeten Vorrichtung wird es hinsichtlich der Aufnahme des Verriegelungsstiftes noch vorgeschlagen, diese in die nockenwellenabgewandte Seitenwand des Antriebsrades einzuarbeiten und derart zu positionieren, dass deren viereckförmige Kontur bei montierter Vorrichtung unterhalb der Radialstirnseite einer der Begrenzungswände des Antriebsrades angeordnet ist und deren mit einem viertelkreisförmigen Verlauf bis in Höhe der Anschlagfläche einer benachbarten Begrenzungswand des Antriebsrades reichende Wurmnut von einer Drehrichtungsseite des Flügelrades aus in die Kontur einmündet. Die der Seite mit der einmündenden Wurmnut gegenüberliegende Seite der Kontur der Aufnahme ist dabei zusätzlich mit einem gehärteten Einlaufradius zur Erleichterung des Einrastens des Verriegelungsstiftes in die Aufnahme ausgebildet, während die Ecken der Kontur mit einem den Durchmesser des Verriegelungsstiftes angepassten Radius abgerundet sind. Der Grund der Aufnahme weist darüber hinaus zwei unterschiedlich tiefe Ebenen auf, von denen die obere Ebene als Anschlagfläche für die aufnahmeseitige Stirnseite des Verriegelungsstiftes ausgebildet ist. Die in die obere Ebene eingearbeitete untere Ebene des Aufnahmegrundes weist dagegen einen Übergang zur einmündenden Wurmnut auf und ist zur Zuleitung des hydraulischen Druckmittels zur Stirnseite des Verriegelungsstiftes vorgesehen. Dabei weist die einmündende Wurmnut bevorzugt einen quadratischen oder annähern quadratischen Querschnitt auf und ist mit einer geringeren Tiefe als die Aufnahme in die Seitenwand des Antriebsrades eingearbeitet. Denkbar sind hierbei jedoch auch andere geeignete Querschnitte für die Wurmnut und/oder eine gleiche bzw. gleichmäßig in die untere Ebene der Aufnahme übergehende Tiefe der Wurmnut.As a further expedient development of the device according to the invention, it is also proposed with respect to the recording of the locking pin to incorporate this in the camshaft side facing away from the drive wheel and position such that the square-shaped contour is arranged at mounted device below the radial end of one of the boundary walls of the drive wheel and their with a quarter-circle course reaching up to the level of the stop surface of an adjacent boundary wall of the drive wheel worm groove opens from a direction of rotation of the impeller into the contour. The side of the opening worm groove opposite side of the contour of the recording is additionally formed with a hardened inlet radius to facilitate the engagement of the locking pin in the recording, while the corners of the contour are rounded with a diameter of the locking pin adapted radius. The reason of the recording also has two different depth levels, of which the upper level is formed as a stop surface for the receiving side end face of the locking pin. The incorporated into the upper level lower level of the receiving ground, however, has a transition to the inflowing worm groove and is provided for supplying the hydraulic pressure medium to the end face of the locking pin. In this case, the entering worm groove preferably has a square or approximately square cross-section and is incorporated with a smaller depth than the receptacle in the side wall of the drive wheel. However, other suitable cross-sections for the worm groove and / or an equal or uniform depth of the worm groove that merges into the lower plane of the receptacle are also conceivable here.

Die wie eingangs erwähnt in ihrer Fläche um ein definiertes Spiel größer als die Querschnittsfläche des Verriegelungsstiftes ausgebildete Kontur der Aufnahme dient im Übrigen einerseits dem Ausgleich des Radiallagerspiels zwischen dem auf den Radialstirnseiten der Begrenzungswände des Antriebsrades gelagerten Flügelrad und dem Antriebsrad sowie andererseits dem Ausgleich von fertigungsbedingten Positionstoleranzen zwischen dem Verriegelungsstift in der Radnabe des Flügelrades und dessen Aufnahme in der Seitenwand des Antriebsrades sowohl in Radial- als auch in Umfangsrichtung der Vorrichtung. Außerdem ermöglicht es die vergrößert ausgebildete Aufnahme, bei der Montage der Vorrichtung ein optimales Spiel für den Verriegelungsstift einzustellen, um ein Verklemmen des Verriegelungsstiftes in der Aufnahme zu vermeiden. Die Abdichtung der vergrößerten Aufnahme und der einmündenden Wurmnut gegen interne Druckmittel-Leckagen erfolgt dabei durch die nockenwellenabgewandte Seitenfläche der Radnabe des Flügelrades, die bei montierter Vorrichtung an der Innenfläche der nockenwellenabgewandten Seitenwand des Antriebsrades anliegt.The as mentioned above in its surface by a defined game larger than the cross-sectional area of the locking pin formed contour of the recording serves, moreover, on the one hand the balance of the radial bearing clearance between the On the radial end faces of the boundary walls of the drive wheel mounted impeller and the drive wheel and on the other hand, the compensation of production-related position tolerances between the locking pin in the wheel hub of the impeller and its inclusion in the side wall of the drive wheel both in the radial and in the circumferential direction of the device. In addition, it allows the enlarged trained recording to adjust during assembly of the device optimal clearance for the locking pin to avoid jamming of the locking pin in the recording. The sealing of the enlarged receptacle and the entering worm groove against internal pressure medium leaks takes place through the side of the wheel hub of the impeller facing away from the camshaft, which rests against the inner surface of the camshaft side wall of the drive wheel when the device is mounted.

Die erfindungsgemäß ausgebildete Vorrichtung zum Verändern der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine, insbesondere Rotationskolben-Verstelleinrichtung zur Drehwinkelverstellung einer Nockenwelle gegenüber einer Kurbelwelle weist somit gegenüber den aus dem Stand der Technik bekannten Vorrichtungen den Vorteil auf, dass durch die Verlagerung der Verriegelung von einem Flügel des Flügelrades in die Radnabe des Flügelrades bzw. durch die erhebliche Verkürzung der Entfernung zwischen der Längsachse der Verriegelung und der Längsmittelachse der Vorrichtung einerseits sich die Steifigkeit der verriegelten Verbindung zwischen dem Flügelrad und dem Antriebsrad wesentlich erhöht und andererseits die im Motorbetrieb auf den Verriegelungsstift wirkenden Fliehkräfte erheblich verringert werden. Da die Verriegelung somit auch nicht mehr im Bereich der Druckkammern der Vorrichtung sowie außerhalb der Druckmittelleitungen zu diesen Druckkammern angeordnet ist, sind sowohl fliehkraftbedingte als auch durch sich anlagernde Schmutzpartikel im hydraulischen Druckmittel bedingte Funktionsstörungen der Verriegelung nahezu ausgeschlossen. Ebenso ist es dadurch möglich, die Flügel des Flügelrades weniger massiv beispielsweise in Plattenform auszubilden und somit die Herstellungskosten der Vorrichtung zu senken sowie die Zahl der möglichen Arbeitsräume in der Vorrichtung zu erhöhen.The inventively designed device for changing the timing of gas exchange valves of an internal combustion engine, in particular rotary piston adjustment for rotational adjustment of a camshaft relative to a crankshaft thus has over the known from the prior art devices has the advantage that by the displacement of the locking of a wing of the impeller in the hub of the impeller or by the significant shortening of the distance between the longitudinal axis of the lock and the longitudinal center axis of the device on the one hand substantially increases the rigidity of the locked connection between the impeller and the drive wheel and on the other hand significantly reduces the forces acting on the locking pin during engine operation centrifugal forces become. Since the lock is thus no longer located in the area of the pressure chambers of the device and outside of the pressure medium lines to these pressure chambers, both centrifugal force as well as by accumulating dirt particles in the hydraulic pressure fluid related malfunction of the lock are almost impossible. Likewise, it is thereby possible to form the wings of the impeller less massive, for example in plate form and thus to reduce the manufacturing cost of the device and to increase the number of possible work spaces in the device.

Darüber hinaus hat die erfindungsgemäß ausgebildete Vorrichtung den Vorteil, dass der auf seiner gesamten Länge gleichmäßig zylindrisch ausgebildete Verriegelungsstift einfach und kostengünstig herstellbar ist sowie einen geringen Bauraumbedarf aufweist, so dass die Herstellungskosten der Vorrichtung noch weiter gesenkt werden und die Vorrichtung auch bei beengten Platzverhältnissen im Motorraum universell einsetzbar ist. Die spezielle Ausführung der Aufnahme des Verriegelungsstiftes und der mit der Aufnahme in Wirkverbindung stehenden Stirnseite des Verriegelungsstiftes sind dabei ursächlich dafür, dass bei der Verriegelung keinerlei Bauteilbelastungen mehr zwischen dem Flügelrad und dem Antriebsrad der Vorrichtung auftreten und dass bei der Entriegelung ein Verklemmen des Verriegelungsstiftes in der Aufnahme nicht mehr möglich ist.In addition, the inventively designed device has the advantage that the uniformly formed on its entire length locking pin is easy and inexpensive to produce and has a low space requirement, so that the manufacturing cost of the device are further reduced and the device even in confined spaces in the engine compartment is universally applicable. The special design of the recording of the locking pin and standing with the recording operatively connected end face of the locking pin are the cause that no more component loads between the impeller and the drive wheel of the device occur during locking and that when unlocking a jamming of the locking pin in the Recording is no longer possible.

Außerdem hat die Verbindung der Aufnahme des Verriegelungsstiftes ausschließlich mit einer der A-Druckkammern der Vorrichtung den besonderen Vorteil, dass dadurch eine gezielte Verriegelung der Vorrichtung beim Abstellen der Brennkraftmaschine möglich ist. Da beim Abstellen der Brennkraftmaschine und somit bei stromlosen Steuerventil der Vorrichtung der Druckmitteldruck auf den B-Druckkammern der Vorrichtung anliegt, wird das Flügelrad zumeist unter Volumenminimierung der jeweiligen A-Druckkammern der Vorrichtung in die für den Start der Brennkraftmaschine notwenige Basisposition verdreht, in welcher der Verriegelungsstift dann zuverlässig einriegelt. Bei Einhaltung einer solchen Schaltlogik für das Steuerventil, das heißt, den Druckmitteldruck bei abgestellter Brennkraftmaschine immer auf die Druckkammern der Vorrichtung zu schalten, die das Flügelrad noch in die gewünschte Basisposition verdrehen, ist die erfindungsgemäß ausgebildete Vorrichtung somit sowohl an Einlassnockenwellen mit Verriegelung in "später" Steuerzeitenlage der Gaswechselventile als auch bei Auslassnockenwellen und an SOHC-Motoren mit Verriegelung in "früher" Steuerzeitenlage der Gaswechselventile einsetzbar.In addition, the connection of the recording of the locking pin exclusively with one of the A-pressure chambers of the device has the particular advantage that a targeted locking of the device when stopping the engine is possible. Since when switching off the internal combustion engine and thus in de-energized control valve of the device, the pressure medium pressure applied to the B-pressure chambers of the device, the impeller is usually rotated under volume minimization of the respective A-pressure chambers of the device in the Necessary for the start of the engine base position in which the Locking pin then locks reliably. In compliance with such a logic for the control valve, that is, always switch the pressure medium pressure when the internal combustion engine to the pressure chambers of the device, which still rotate the impeller in the desired base position, the inventively designed device is thus both on intake camshafts with locking in "later "Timing of the gas exchange valves as well as exhaust camshafts and SOHC engines with locking in 'early' timing of the gas exchange valves used.

Beim Einsatz der erfindungsgemäß ausgebildeten Vorrichtung an Auslassnockenwellen oder an SOHC-Motoren hat es sich darüber hinaus noch als vorteilhaft erwiesen, dass in Richtung "spät", also in Richtung von der Basisposition weg wirkende Schleppmoment der Nockenwelle zum Ausgleich der Verstellzeiten der Vorrichtung und zur Unterstützung der Drehbewegung des Flügelrades in die Basisposition der Brennkraftmaschine durch ein zusätzliches Federelement auszugleichen, dass am Antriebsrad und am Flügelrad angreift und zwischen diesen ein Vorlastmoment erzeugt. Bei der erfindungsgemäß ausgebildeten Vorrichtung kann dies besonders vorteilhaft durch eine außen vor der nockenwellenabgewandten Seitenwand des Antriebsrades angeordnete Flachband-Spiralfeder realisiert werden, deren äußerer Aufhängungspunkt durch eine verlängerte Befestigungsschraube für die Seitenwände gebildet wird und deren innerer Aufhängungspunkt mit der Zentralaschraube der Vorrichtung verbunden ist.When using the inventively designed device on exhaust camshafts or on SOHC engines, it still has more than beneficial proven that in the direction of "late", so in the direction of the base position away acting drag torque of the cam to compensate for the adjustment of the device and to support the rotational movement of the impeller in the base position of the internal combustion engine by an additional spring element compensate for that on the drive wheel and the impeller attacks and generates a preload torque between them. In the case of the device designed according to the invention, this can be realized in a particularly advantageous manner by a flat strip coil spring arranged outside the camshaft side wall of the drive wheel whose outer suspension point is formed by an elongated fastening screw for the side walls and whose inner suspension point is connected to the central screw of the device.

Kurze Beschreibung der ZeichnungenBrief description of the drawings

Die Erfindung wird nachfolgend anhand eines Ausführungsbeispiels näher erläutert und ist in den zugehörigen Zeichnungen schematisch dargestellt. Dabei zeigen:

Figur 1
einen Längsschnitt B-B nach Figur 2 durch eine erfindungsgemäß ausgebildete Vorrichtung;
Figur 2
einen Querschnitt A-A nach Figur 1 durch eine erfindungsgemäß ausgebildete Vorrichtung;
Figur 3
eine vergrößerte Ansicht der Einzelheit X gemäß Figur 1 auf den Verriegelungsstift der erfindungsgemäß ausgebildeten Vorrichtung;
Figur 4
eine Draufsicht auf die Innenseite der nockenwellenabgewandten Seitenwand des Antriebsrades der erfindungsgemäß ausgebildeten Vorrichtung;
Figur 5
eine vergrößerte Ansicht der Einzelheit V gemäß Figur 4 auf die Aufnahme des Verriegelungsstiftes der erfindungsgemäß ausgebildeten Vorrichtung;
Figur 6
einen Querschnitt VI-VI nach Figur 5 durch die Aufnahme des Verriegelungsstiftes der erfindungsgemäß ausgerichteten Vorrichtung.
The invention will be explained in more detail with reference to an embodiment and is shown schematically in the accompanying drawings. Showing:
FIG. 1
a longitudinal section BB after FIG. 2 by a device designed according to the invention;
FIG. 2
a cross section AA after FIG. 1 by a device designed according to the invention;
FIG. 3
an enlarged view of the detail X according to FIG. 1 on the locking pin of the device according to the invention;
FIG. 4
a plan view of the inside of the camshaft side facing away from the drive wheel of the inventive device;
FIG. 5
an enlarged view of the detail V according to FIG. 4 to the inclusion of the locking pin of the inventively designed device;
FIG. 6
a cross-section VI-VI after FIG. 5 by receiving the locking pin of the device according to the invention.

Ausführliche Beschreibung der ZeichnungenDetailed description of the drawings

Aus den Figuren 1 und 2 geht deutliche eine Vorrichtung 1 zum Verändern der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine hervor, die als Rotationskolben-Verstelleinrichtung zur Drehwinkelverstellung einer nicht dargestellten Nockenwelle gegenüber einer ebenfalls nicht dargestellten Kurbelwelle einer Brennkraftmaschine ausgebildet ist. Diese Vorrichtung 1 ist am antriebsseitigen Ende einer im Zylinderkopf der Brennkraftmaschine gelagerten Nockenwelle befestigt und im Prinzip als hydraulischer Stellantrieb ausgebildet, der in Abhängigkeit von verschiedenen Betriebsparametern der Brennkraftmaschine durch das in Figur 1 mit 33 bezeichnete Hydraulikventil gesteuert wird.From the FIGS. 1 and 2 clearly shows a device 1 for changing the timing of gas exchange valves of an internal combustion engine, which is a rotary piston adjusting device for adjusting the rotational angle of a not shown Camshaft with respect to a likewise not shown crankshaft of an internal combustion engine is formed. This device 1 is attached to the drive-side end of a camshaft mounted in the cylinder head of the engine and designed in principle as a hydraulic actuator, which in dependence on various operating parameters of the internal combustion engine by the in FIG. 1 33 is controlled hydraulic valve.

Des weiteren ist in den Figuren 1 und 2 zu sehen, dass die Vorrichtung 1 im Wesentlichen aus einem mit der Kurbelwelle der Brennkraftmaschine in Antriebsverbindung stehenden Antriebsrad 2 und aus einem drehfest mit der Nokkenwelle der Brennkraftmaschine verbundenen Flügelrad 3 besteht, wobei das Flügelrad 3 im Antriebsrad 2 schwenkbar gelagert ist und mit diesem in Antriebsverbindung steht. Das Antriebsrad 2 weist dabei einen durch eine hohlzylindrische Umfangswand 4 und zwei Seitenwände 5, 6 gebildeten Hohlraum auf, in dem durch fünf zur Längsmittelachse der Vorrichtung 1 gerichtete radiale Begrenzungswände 7 und 8 fünf gleichmäßig umfangverteilte hydraulische Arbeitsräume 9 gebildet werden. Das Flügelrad 3 der Vorrichtung 1 weist dementsprechend am Umfang seiner Radnabe 10 fünf gleichmäßig umfangsverteilte und sich jeweils radial in einen Arbeitsraum 9 des Antriebsrades 2 erstreckende Flügel 11 auf, welche die Arbeitsräume 9 in jeweils eine A-Druckkammer 12 und eine B-Druckkammer 13 unterteilen, die bei wahlweiser oder gleichzeitiger Druckbeaufschlagung mit einem hydraulischen Druckmittel eine Schwenkbewegung oder Fixierung des Flügelrades 3 gegenüber dem Antriebsrad 2 und damit eine Drehwinkelverstellung oder hydraulische Einspannung der Nockenwelle gegenüber der Kurbelwelle bewirken.Furthermore, in the FIGS. 1 and 2 to see that the device 1 consists essentially of a standing with the crankshaft of the engine drivingly connected drive wheel 2 and a rotatably connected to the camshaft of the engine impeller 3, wherein the impeller 3 is pivotally mounted in the drive wheel 2 and with this in drive connection stands. The drive wheel 2 in this case has a cavity formed by a hollow cylindrical peripheral wall 4 and two side walls 5, 6, in which five equally circumferentially distributed hydraulic working chambers 9 are formed by five directed to the longitudinal center axis of the device 1 radial boundary walls. The impeller 3 of the device 1 accordingly has on the circumference of its hub 10 five uniformly circumferentially distributed and each radially into a working space 9 of the drive wheel 2 extending wings 11, which divide the working spaces 9 in each case an A-pressure chamber 12 and a B-pressure chamber 13 that cause a pivotal movement or fixation of the impeller 3 with respect to the drive wheel 2 and thus a rotational angle adjustment or hydraulic clamping of the camshaft relative to the crankshaft with selective or simultaneous pressurization with a hydraulic pressure means.

Weiterhin ist insbesondere aus Figur 1 ersichtlich, dass die Vorrichtung 1 zur Vermeidung eines aus den Wechselmomenten der Nockenwelle resultierenden Anschlagklapperns des Flügelrades 3 beim Start der Brennkraftmaschine ein gesondertes Verriegelungselement 14 aufweist, mit dem das Flügelrad 3 bei Unterschreitung eines zur Verstellung erforderlichen Druckmitteldrucks in einer bevorzugten Basisposition innerhalb seines Verstellbereiches mit dem Antriebsrad 2 mechanisch koppelbar ist. Dieses Verriegelungselement 14 ist in einer zur Längsmittelachse der Vorrichtung 1 parallelen Bohrung im Flügelrad 3 angeordnet und durch ein Federelement 15 in eine Verriegelungsstellung innerhalb einer Aufnahme 16 in der Seitenwand 5 des Antriebsrades 2 verschiebbar. Durch eine Verbindung der Aufnahme 16 des Verriegelungselementes 14 mit zumindest einer Druckkammer 12 oder 13 innerhalb der Vorrichtung 1 ist es möglich, das Verriegelungselement 14 bei Druckbeaufschlagung der Druckkammern 12, 13 wieder hydraulisch in seiner Entriegelungsstellung innerhalb der Bohrung im Flügelrad 3 zu bewegen.Furthermore, in particular FIG. 1 It can be seen that the device 1 to avoid a resulting from the alternating torques of the camshaft stop clatter of the impeller 3 at start of the internal combustion engine has a separate locking element 14, with the impeller 3 falls below a required for adjustment pressure medium pressure in a preferred base position within its adjustment range with the Drive wheel 2 is mechanically coupled. This locking element 14 is in arranged parallel to the longitudinal center axis of the device 1 bore in the impeller 3 and displaceable by a spring element 15 in a locking position within a receptacle 16 in the side wall 5 of the drive wheel 2. By connecting the receptacle 16 of the locking element 14 with at least one pressure chamber 12 or 13 within the device 1, it is possible to hydraulically move the locking element 14 in pressurizing the pressure chambers 12, 13 again in its unlocked position within the bore in the impeller 3.

Insbesondere den Figuren 1 bis 3 ist diesbezüglich noch entnehmbar, dass das Verriegelungselement 14 erfindungsgemäß als auf seiner gesamten Länge gleichmäßig zylindrischer Verriegelungsstift ausgebildet ist, der in einer durchgehenden Axialbohrung 17 in der Radnabe 10 des Flügelrades 3 angeordnet ist. In Figur 2 ist dabei deutlich zu sehen, dass die Längsachse dieser Axialbohrung 17 einen geringstmöglichen Abstand zur Längsmittelachse der Vorrichtung 1 aufweist, um die im Motorbetrieb entstehenden Fliehkrafteinflüsse auf das Verriegelungselement 14 zu minimieren. Darüber hinaus ist das Verriegelungselement 14, wie aus Figur 3 hervorgeht, aufnahmeseitig mit einer Phase 19 und einer Verrundung 20 seiner stirnseitigen Kante ausgebildet, welche die Axialbewegung des Verriegelungselementes 14 in seine Entriegelungsstellung beschleunigen und dabei in Verklemmen desselben vermeiden sollen. Ein durch Adhäsionskräfte bedingtes "Kleben" des Verriegelungselementes 14 in der Aufnahme 16 wird dabei zusätzlich durch die ebenfalls in Figur 3 sichtbare hohle Ausbildung der vorderen Stirnseite 21 des Verriegelungselementes 14 vermieden. An seiner rückseitigen Stirnseite 22 weist das Verriegelungselement 14 dagegen eine Grundbohrung 23 auf, in der, wie ebenso aus Figur 3 entnehmbar ist, das eine Ende des als Druckschraubenfeder ausgebildeten Federelementes 15 fixiert wird. Das andere Ende dieses Federelementes 15 stützt sich dabei an einem in die Axialbohrung 17 eingesetzten und mit einer Zentrierspitze 24 ausgebildeten Gegenhalter 15 ab, der einen Y-förmigen Profilquerschnitt aufweist und bei welchem die zwischen seinen Profilschenkeln gebildeten Längsnuten 26 zugleich zur Druckmittel-Entlüftung der Axialbohrung 17 vorgesehen sind.In particular the FIGS. 1 to 3 is in this respect still be removed that the locking element 14 is formed according to the invention as uniform over its entire length locking pin, which is arranged in a continuous axial bore 17 in the hub 10 of the impeller 3. In FIG. 2 It can clearly be seen that the longitudinal axis of this axial bore 17 has the smallest possible distance from the longitudinal central axis of the device 1, in order to minimize the centrifugal force influences on the locking element 14 that arise during engine operation. In addition, the locking element 14, as shown FIG. 3 emerges on the receiving side formed with a phase 19 and a rounding 20 of its front edge, which accelerate the axial movement of the locking element 14 in its unlocked position while avoiding it in jamming. Adhesion forces of the locking element 14 in the receptacle 16 are additionally avoided by the hollow formation of the front end 21 of the locking element 14, which is also visible in FIG. 3. On its rear end face 22, however, the locking element 14 has a blind bore 23 in which, as well as from FIG. 3 can be removed, which is fixed one end of the compression spring designed as a spring element 15. The other end of this spring element 15 is supported on an inserted into the axial bore 17 and formed with a centering tip 24 abutment 15, which has a Y-shaped profile cross-section and in which the longitudinal grooves formed between its profile legs 26 at the same time for pressure fluid venting the axial bore 17 are provided.

Die in Figur 4 erkennbare Aufnahme 16 des Verriegelungselementes 14 weist des weiteren erfindungsgemäß eine viereckförmige und in ihrer Fläche um eine definiertes allseitiges Spiel größer als die Querschnittsfläche des Verriegelungselementes 14 ausgebildete Kontur auf und ist mit einer einmündenden Wurmnut 18 ausgebildet, die ausschließlich mit einer in Verriegelungsstellung drucklosen A-Druckkammer 12 der Vorrichtung 1 verbunden ist. Dadurch ist sichergestellt, dass die Aufnahme 16 des Verriegelungselementes 14 nur bei Druckbeaufschlagung der A-Druckkammern 12 der Vorrichtung 1 über die Wurmnut 18 mit dem Druck des hydraulischen Druckmittels beaufschlagt und somit das Verriegelungselement 14 in seine Entriegelungsstellung bewegt wird.In the FIG. 4 recognizable receptacle 16 of the locking element 14 further has according to the invention a quadrangular and in its surface by a defined all-sided game greater than the cross-sectional area of the locking member 14 formed contour and is formed with an opening worm groove 18, which only with an unpressurized in locking position A-pressure chamber 12 of the device 1 is connected. This ensures that the receptacle 16 of the locking element 14 is acted upon only upon pressurization of the A-pressure chambers 12 of the device 1 via the worm groove 18 with the pressure of the hydraulic pressure medium and thus the locking member 14 is moved to its unlocked position.

Darüber hinaus ist aus Figur 4 ersichtlich, dass die Aufnahme 16 des Verriegelungselementes 14 in die nockenwellenabgewandte Seitenwand 5 des Antriebsrades 2 eingearbeitet und derart positioniert ist, dass deren viereckförmige Kontur bei montierter Vorrichtung 1 unterhalb der in der Zeichnung gestrichelt angedeuteten Radialstirnseite 27 einer Begrenzungswand 7 des Antriebsrades 2 angeordnet ist. Dabei weist die Wurmnut 18 einen viertelkreisförmigen Verlauf bis in Höhe der ebenfalls gestrichelt dargestellten Anschlagfläche 28 einer benachbarten Begrenzungswand 8 auf und mündet von einer in Drehrichtung des Flügelrades 3 liegenden Seite aus in die Kontur der Aufnahme 16 ein. Die der Seite mit der Wurmnut 18 gegenüberliegende Seite der Kontur der Aufnahme 16 ist dagegen, wie die Vergrößerungen der Figuren 5 und 6 zeigen, mit einem gehärteten Einlaufradius 29 ausgebildet, der das Einrasten des Verriegelungselementes 14 in die Aufnahme 16 erleichtert. Ebenso wird in den Figuren 5 und 6 gezeigt, dass die nicht näher bezeichneten Ecken der Kontur mit einem dem Durchmesser des Verriegelungsstiftes 14 entsprechenden Radius abgerundet sind und dass der Grund der Aufnahme 16 zwei unterschiedlich tiefe Ebenen 30, 31 aufweist. Die obere Ebene 30 ist dabei als Anschlagfläche des Verriegelungsstiftes 14 in der Aufnahme 16 ausgebildet, während die in die obere Ebene 30 eingearbeitete untere Ebene 31 einen Übergang 32 zur einmündenden Wurmnut 18 aufweist und zur Zuleitung des hydraulischen Druckmittels zur Stirnseite 21 des Verriegelungselementes 14 vorgesehen ist.In addition, is off FIG. 4 It can be seen that the receptacle 16 of the locking element 14 is incorporated into the side wall 5 of the drive wheel 2 facing away from the camshaft and is positioned such that its quadrangular contour is arranged below the radial end face 27 of a limiting wall 7 of the drive wheel 2, indicated by dashed lines in the drawing. In this case, the worm groove 18 has a quarter-circle course up to the level of the stop surface 28 of an adjacent boundary wall 8, also shown in phantom, and opens into the contour of the receptacle 16 from a side lying in the direction of rotation of the impeller 3. The side of the worm groove 18 opposite side of the contour of the receptacle 16, however, as the magnifications of FIGS. 5 and 6 show, formed with a hardened inlet radius 29, which facilitates the engagement of the locking element 14 in the receptacle 16. Likewise, in the FIGS. 5 and 6 shown that the unspecified corners of the contour with a diameter of the locking pin 14 corresponding radius are rounded and that the bottom of the receptacle 16 has two different depths levels 30, 31. The upper level 30 is formed as a stop surface of the locking pin 14 in the receptacle 16, while the incorporated into the upper level 30 lower level 31 has a transition 32 to the opening worm groove 18 and is provided for supplying the hydraulic pressure medium to the end 21 of the locking element 14 ,

BezugszahlenlisteLIST OF REFERENCE NUMBERS

11
Vorrichtungcontraption
22
Antriebsraddrive wheel
33
Flügelradimpeller
44
Umfangswandperipheral wall
55
SeitenwandSide wall
66
SeitenwandSide wall
77
Begrenzungswandboundary wall
88th
Begrenzungswandboundary wall
99
Arbeitsraumworking space
1010
Radnabewheel hub
1111
Flügelwing
1212
A-DruckkammerA pressure chamber
1313
B-DruckkammerB-pressure chamber
1414
Verriegelungselementlocking element
1515
Federelementspring element
1616
Aufnahmeadmission
1717
Axialbohrungaxial bore
1818
Wurmnutworm groove
1919
Phasephase
2020
Verrundungrounding
2121
hohle Stirnseitehollow front side
2222
rückseitige Stirnseiteback end face
2323
Grundbohrungblind hole
2424
Zentrierspitzecentering
2525
Gegenhalterbackstop
2626
Längsnutenlongitudinal grooves
2727
RadialstirnseiteRadial front end
2828
Anschlagflächestop surface
2929
Einlaufradiusentry radius
3030
obere Ebeneupper level
3131
untere Ebenelower level
3232
Übergangcrossing
3333
Hydraulikventilhydraulic valve

Claims (4)

  1. Device for varying the control times of gas exchange valves of an internal combustion engine, in particular a rotary-piston adjustment device for adjusting the angle of rotation of a camshaft with respect to a crankshaft, having the following features:
    ■ the device (1) is attached to the drive-side end of a camshaft mounted in the cylinder head of the internal combustion engine and is designed in principle as a hydraulic actuator which can be controlled as a function of various operating parameters of the internal combustion engine;
    ■ the device (1) is composed substantially of a drive wheel (2), which is drive-connected to a crankshaft of the internal combustion engine, and a vane wheel (3) which is rotationally fixedly connected to a camshaft of the internal combustion engine;
    ■ the drive wheel (2) has a cavity formed by a hollow cylindrical peripheral wall (4) and two side walls (5, 6), in which cavity at least one hydraulic working chamber (9) is formed by at least two radial boundary walls (7, 8);
    ■ the vane wheel (3) has, on the periphery of its wheel hub (10), at least one vane (11) which extends radially into a working chamber (9) of the drive wheel (2) and which divides said working chamber (9) respectively into an A pressure chamber (12) and a B pressure chamber (13);
    ■ the pressure chambers (12, 13), upon being pressurized selectively or simultaneously with a hydraulic pressure medium, effect a pivoting movement or a fixing of the vane wheel (3) with respect to the drive wheel (2), and therefore of the camshaft with respect to the crankshaft;
    ■ if the pressure of the pressure medium falls below a pressure required for adjustment, the vane wheel (3) can be mechanically coupled, in a preferred base position within its range of adjustment, to the drive wheel (2) by a separate locking element (14);
    ■ the locking element (14) is arranged in a bore, which is parallel to the longitudinal central axis of the device (1), in the vane wheel (3) and can be moved by a spring element (15) into a locked position within a receptacle (16) in one of the side walls (5, 6) of the drive wheel (2);
    ■ the receptacle (16) of the locking element (14) is connected to at least one pressure chamber (12 or 13) within the device (1), such that, upon pressurization of said pressure chamber (12 or 13), the locking element (14) can be moved hydraulically into an unlocked position within the bore in the vane wheel (3);
    ■ with the locking element (14) being designed as a locking pin which is uniformly cylindrical along its entire length, and being arranged in an axial bore (17) in the wheel hub (10) of the vane wheel (3), the longitudinal axis of which axial bore (17) is at the smallest possible distance from the longitudinal central axis of the device (1),
    characterized in that
    ■ the receptacle (16) of the locking element (14) has, in one of the side walls (5, 6) of the drive wheel (2), a tetragonal contour which is designed so as to be larger in terms of area, by a defined play on all sides, than the cross-sectional area of the locking element (14), and said receptacle (16) is formed with an opening-in worm groove (18) for the supply of pressure medium,
    ■ which worm groove (18) is connected exclusively to an A pressure chamber (12), which is unpressurized in the locked position of the vane wheel (3), of the device (1) and via which the receptacle (16) of the locking element (14) can be acted on with the pressure of the hydraulic pressure medium only upon pressurization of the A pressure chambers (12).
  2. Device according to the preamble of Claim 1, characterized in that
    ■ the locking element (14) is formed with a chamfer (19) and with a rounding (20) of its end-side edge and also with a hollow end side (21), while said locking element (14) has, in its rear end side (22), a base bore (23) for fixing the one end of the spring element (15) which is preferably designed as a coil pressure spring,
    ■ the other end of which spring element (15) is supported on a counter bracket (25), which is inserted into the axial bore (17) and is formed with a centring tip (24) and has a Y-shaped profile cross section, in which the longitudinal grooves (26) which are formed between the profile limbs of said Y-shaped profile cross section are simultaneously provided for pressure medium ventilation of the axial bore (17).
  3. Device according to the preamble of Claim 1, characterized in that
    ■ the receptacle (16) of the locking element (14) is preferably formed into that side wall (5) of the drive wheel (2) which faces away from the camshaft, and said receptacle (16) is preferably positioned such that, when the device (1) is assembled, the tetragonal contour of said receptacle (16) is arranged below the radial end side (27) of one of the boundary walls (7 or 8) of the drive wheel (2),
    ■ with the worm groove (18), which preferably extends with a profile in the shape of a quadrant of a circle up to the level of the stop surface (28) of an adjacent boundary wall (8 or 7) of the drive wheel (2), of said receptacle (16) being arranged so as to open out into the contour of the receptacle (16) from a side situated in the rotational direction of the vane wheel (3).
  4. Device according to Claim 3, characterized in that
    ■ that side of the contour of the receptacle (16) which is situated opposite the side with the worm groove (18) is formed with a surface-hardened run-in radius (29), while the corners of the contour are rounded with a radius which is adapted to the locking element (14), and the base of the receptacle (16) has two planes (30, 31) of different depths,
    ■ of which planes (30, 31) the upper plane (30) is designed as a stop surface of the locking element (14) while the lower plane (31), which is formed into the upper plane (30), has a transition (32) to the opening-in worm groove (18) and is provided for conducting the hydraulic pressure medium to the end side (21) of the locking element (14).
EP02020920A 2001-10-15 2002-09-19 Device for changing the timing of gas exchange valves of an internal combustion engine, especially a rotary piston phasing device for changing the angle of a camshaft relative to a crank shaft Expired - Lifetime EP1302630B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10150856A DE10150856B4 (en) 2001-10-15 2001-10-15 Device for changing the timing of gas exchange valves of an internal combustion engine, in particular rotary piston adjusting device for adjusting the rotational angle of a camshaft relative to a crankshaft
DE10150856 2001-10-15

Publications (3)

Publication Number Publication Date
EP1302630A2 EP1302630A2 (en) 2003-04-16
EP1302630A3 EP1302630A3 (en) 2003-11-26
EP1302630B1 true EP1302630B1 (en) 2009-05-06

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EP02020920A Expired - Lifetime EP1302630B1 (en) 2001-10-15 2002-09-19 Device for changing the timing of gas exchange valves of an internal combustion engine, especially a rotary piston phasing device for changing the angle of a camshaft relative to a crank shaft

Country Status (5)

Country Link
US (1) US6805080B2 (en)
EP (1) EP1302630B1 (en)
JP (1) JP2003120231A (en)
DE (2) DE10150856B4 (en)
ES (1) ES2324598T3 (en)

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Also Published As

Publication number Publication date
DE10150856A1 (en) 2003-04-24
DE50213520D1 (en) 2009-06-18
EP1302630A2 (en) 2003-04-16
JP2003120231A (en) 2003-04-23
ES2324598T3 (en) 2009-08-11
US20030084863A1 (en) 2003-05-08
US6805080B2 (en) 2004-10-19
DE10150856B4 (en) 2005-08-11
EP1302630A3 (en) 2003-11-26

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