EP3441581B1 - Sliding cam system and method for operating a combustion engine - Google Patents

Sliding cam system and method for operating a combustion engine Download PDF

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Publication number
EP3441581B1
EP3441581B1 EP18181183.7A EP18181183A EP3441581B1 EP 3441581 B1 EP3441581 B1 EP 3441581B1 EP 18181183 A EP18181183 A EP 18181183A EP 3441581 B1 EP3441581 B1 EP 3441581B1
Authority
EP
European Patent Office
Prior art keywords
cam
limiting section
carrier
axial displacement
camshaft
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.)
Active
Application number
EP18181183.7A
Other languages
German (de)
French (fr)
Other versions
EP3441581A1 (en
Inventor
Sören Franke
Thilo Kowalschek
Fabian Zeil
Heiko Neukirchner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MAN Truck and Bus SE
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MAN Truck and Bus SE
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Filing date
Publication date
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Publication of EP3441581A1 publication Critical patent/EP3441581A1/en
Application granted granted Critical
Publication of EP3441581B1 publication Critical patent/EP3441581B1/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
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/0015Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
    • F01L13/0036Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque the valves being driven by two or more cams with different shape, size or timing or a single cam profiled in axial and radial direction
    • 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
    • F01L1/02Valve drive
    • F01L1/04Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
    • F01L1/047Camshafts
    • 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
    • F01L1/02Valve drive
    • F01L1/04Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
    • F01L1/047Camshafts
    • F01L1/053Camshafts overhead type
    • 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
    • F01L1/02Valve drive
    • F01L1/04Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
    • F01L1/08Shape of cams
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/06Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for braking
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D13/00Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing
    • F02D13/02Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation
    • F02D13/04Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation using engine as brake
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/12Transmitting gear between valve drive and valve
    • F01L1/18Rocking arms or levers
    • F01L1/185Overhead end-pivot rocking arms
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/0015Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
    • F01L13/0036Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque the valves being driven by two or more cams with different shape, size or timing or a single cam profiled in axial and radial direction
    • F01L2013/0052Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque the valves being driven by two or more cams with different shape, size or timing or a single cam profiled in axial and radial direction with cams provided on an axially slidable sleeve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L2013/10Auxiliary actuators for variable valve timing
    • F01L2013/101Electromagnets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L2305/00Valve arrangements comprising rollers

Definitions

  • the invention relates to a sliding cam system for a variable valve train, a variable valve train, a motor vehicle and a method for operating an internal combustion engine.
  • Valve-controlled internal combustion engines have one or more controllable intake and exhaust valves per cylinder.
  • Variable valve controls allow flexible control of the valves to change the opening time, closing time and / or the valve lift. As a result, engine operation can be adapted to a specific load situation, for example.
  • a valve train is known with which the actuation of a gas exchange valve with several different stroke curves is made possible.
  • a sliding cam with at least one cam section having a plurality of cam tracks is rotatably but axially displaceably mounted on the camshaft and has a stroke contour into which an actuator in the form of a pin is inserted from the outside radially to produce an axial displacement of the sliding cam. Due to the axial displacement of the slide cam, a different valve lift is set for the respective gas exchange valve.
  • the sliding cam After the axial displacement thereof relative to the camshafts, the sliding cam is locked in its axial relative position on the camshaft in that, depending on the axial relative position, at least one spring-loaded locking ball, which is received and supported in the camshaft, engages in at least one locking groove.
  • the axial displacement of the sliding cam to change the valve lift takes place exclusively in the so-called base circle of the or each cam section or the cam tracks of the same. This limits the switching speed of the valve train.
  • the internal combustion engine has a valve train with at least one rotatably mounted camshaft and with at least one sliding cam that can be axially displaced on the respective camshaft.
  • the respective sliding cam has at least one link section with at least one groove formed on an outer lateral surface of the respective link section, the respective sliding cam having at least one cam section with a plurality of cam tracks for setting different valve lifts.
  • an actuatable pin of an actuator is inserted from radially outside into a groove in the link section.
  • the axial displacement of the respective sliding cam is carried out depending on the axial displacement direction of the same and / or depending on a valve clearance outside a base circle of the or each cam section thereof.
  • the GB 2 545 257 A discloses an internal combustion engine with a cam shifting system comprising a switch unit that is rotationally fixed and axially movable with respect to a camshaft, the switch unit comprising at least two cams configured to be selectively brought into contact with a cam follower.
  • the cams are provided with a base circle and at least one cam lobe.
  • the cam follower contacts at least a part of at least one cam elevation outside the base circle.
  • the US 8 863 714 B1 , the DE 10 2012 209 860 A1 , the US 2015/075468 A1 and the US 2007/034182 A1 disclose further sliding cam systems.
  • the invention is based on the object of providing an alternative or improved sliding cam system and method for operating an internal combustion engine in which the forces which occur during the displacement process of the cam carrier are reduced in comparison with conventional systems.
  • the sliding cam system is designed for a variable valve train of an internal combustion engine of a motor vehicle, in particular a commercial vehicle.
  • the sliding cam system points a camshaft and a cam carrier.
  • the cam carrier is arranged on the camshaft in a rotationally fixed and axially displaceable manner between a first axial position and a second axial position and has a first cam, a second cam and a first engagement track for axially displacing the cam carrier.
  • the sliding cam system has a cam follower that is operatively connected to the first cam in the first axial position of the cam carrier and is operatively connected to the second cam in the second axial position of the cam carrier.
  • the sliding cam system has a first actuator, which has a retractable and extendable element, in particular a pin, for engagement in the first engagement track for axial displacement of the cam carrier.
  • the first cam and the second cam are offset from one another along a longitudinal axis of the camshaft arranged.
  • the first cam has a base circle area and a valve lift area with a boundary section which adjoins the base circle area of the first cam.
  • the second cam has a base circle area and a valve lift area with a boundary section which adjoins the base circle area of the second cam.
  • the boundary section of the first cam and the boundary section of the second cam are of identical design and are arranged at the same circumferential position around the longitudinal axis of the camshaft.
  • the first actuator, the cam follower and the first engagement track are arranged and designed in such a way that the cam carrier can be axially displaced while the cam follower is in operative connection with the boundary section of the first cam and / or the boundary section of the second cam.
  • the sliding cam system enables an extension of the time available for the axial displacement of the cam carrier by expansion into the limit sections of the cams. Due to the larger switching range, the accelerations and thus the inertial forces can be reduced for the axial shift at the same switching speed. On the one hand, this can be used, for example, to increase functional reliability and service life due to lower forces and pressures. On the other hand, this can be used, for example, to increase the maximum switching speed of the system.
  • the first cam can be formed directly adjacent to the second cam.
  • the first actuator, the cam follower and the first engagement track are arranged and designed such that an axial displacement of the cam carrier begins and / or ends while the cam follower is in operative connection with the boundary section of the first cam or the boundary section of the second cam .
  • the beginning and / or the end of the axial displacement of the cam carrier can thus be shifted into the boundary regions. The time available for axially displacing the cam carrier can thus be extended.
  • the boundary sections extend over a range greater than or equal to 1 ° camshaft angle.
  • the boundary sections extend over a range between 5 ° and 45 ° camshaft angles, in particular between 15 ° and 30 ° camshaft angles.
  • the boundary sections form a common flat ramp.
  • the boundary sections are arranged in an outlet area of the first and second cams.
  • the axial displacement of the cam carrier begins when the cam follower is in operative connection with the boundary section of the first cam or the second cam.
  • the axial displacement preferably ends while the cam follower is in operative connection with the base circle region of the first cam or of the second cam.
  • the axial displacement it is also possible for the axial displacement to end only in a further boundary section in an inlet region of the first or second cam, the further boundary sections of the first and second cams in turn being of the same design and arranged at the same circumferential position around the longitudinal axis of the camshaft.
  • the boundary sections are arranged in an inlet area of the first and second cams.
  • the axial displacement of the cam carrier ends when the cam follower is in operative connection with the boundary section of the first cam or the second cam.
  • the axial displacement of the cam carrier preferably begins while the cam follower is in operative connection with the base circle region of the first cam or the second cam.
  • the axial displacement already begins in another limit section in a run-out area of the first or second cam, the other limit sections of the first and second cam in turn having the same design and being arranged at the same circumferential position around the longitudinal axis of the camshaft.
  • the cam carrier has a second engagement track for axially displacing the cam carrier in a direction opposite to an axial displacement caused by the first engagement track.
  • the sliding cam system also has a second actuator, which has a retractable and extendable element, in particular a pin, for engagement in the second engagement track for axial displacement of the cam carrier.
  • the second actuator, the cam follower and the second engagement track are arranged and designed such that an axial displacement of the cam carrier can be carried out (in particular begins and / or ends) while the cam follower is in operative connection with the boundary section of the first cam or the boundary section of the second cam .
  • first actuator and the second actuator can be provided separately from one another.
  • first actuator and the second actuator can be provided in a common housing.
  • the first engagement track and the second engagement track can preferably be provided separately from one another. However, it is also possible for the first engagement track and the second engagement track to be arranged in the same area of the cam carrier. The first engagement track and the second engagement track can preferably intersect.
  • the first engagement track has a cross-sectional constriction to reduce play between the first engagement track and the retractable and extendable element of the first actuator when engaging (the extended element in the first engagement track).
  • the cross-sectional constriction is arranged such that the play reduction takes place before the cam follower comes into operative connection with the boundary section of the first cam or the second cam.
  • the section of the engagement track provided for reducing the play does not shorten the section of the engagement track provided for the axial displacement of the cam carrier.
  • the second engagement track to have a cross-sectional constriction to reduce play between the second engagement track and the retractable and extendable element of the second actuator when engaging (the extended element in the second engagement track).
  • the cross-sectional constriction is arranged such that the play reduction takes place before the cam follower comes into operative connection with the boundary section of the first cam or the second cam.
  • the first engagement track and / or the second engagement track extends spirally around the longitudinal axis of the camshaft.
  • the retractable and extendable element of the first actuator and / or the second actuator can be moved radially with respect to the longitudinal axis of the camshaft.
  • the invention also relates to a variable valve train for an internal combustion engine.
  • the variable valve train has a slide cam system as disclosed herein.
  • the variable valve train has a gas exchange valve, in particular an inlet valve or an outlet valve, which is operatively connected to the cam follower.
  • the first cam and the second cam cause different valve lifts, opening times and / or closing times of the gas exchange valve.
  • the gas exchange valve is an outlet valve.
  • the first cam is designed for normal operation of the internal combustion engine, in which the first cam keeps the exhaust valve open during the exhaust stroke.
  • the second cam is designed for engine braking operation of the internal combustion engine, in which, preferably, the exhaust valve is initially kept closed in the compression stroke and in the extension stroke and is opened before a piston movement reaches top dead center.
  • the second cam is designed so that the exhaust valve opens between 100 ° KW and 60 ° KW (crankshaft angle) before reaching top dead center.
  • the second cam is designed such that the exhaust valve closes in the region between top dead center and 30 ° CA after top dead center after opening in the extension stroke.
  • the second cam is designed such that the outlet valve closes after opening in the compression stroke in the range between bottom dead center and 30 ° CA after bottom dead center.
  • the invention also relates to a motor vehicle, in particular a commercial vehicle (for example a truck or bus), comprising the variable valve train as disclosed herein or the sliding cam system as disclosed herein.
  • a motor vehicle in particular a commercial vehicle (for example a truck or bus), comprising the variable valve train as disclosed herein or the sliding cam system as disclosed herein.
  • the invention also relates to a method for operating an internal combustion engine with a sliding cam system.
  • the sliding cam system has a cam carrier which is arranged on a camshaft in a rotationally fixed manner and is axially displaceable, with a first cam and a second cam.
  • the first cam and the second cam each have a base circle area and a valve lift area with a boundary section which is arranged adjacent to the respective base circle area.
  • the boundary section of the first cam and the boundary section of the second cam are of identical design and are arranged at the same circumferential position about a longitudinal axis of the camshaft.
  • the sliding cam system has a cam follower, which is optionally operatively connected to the first cam or the second cam.
  • the method has the axial displacement of the cam carrier, the axial displacement of the cam carrier being carried out, in particular starting or ending, while the cam follower is in operative connection with the boundary section of the first cam and / or the second cam.
  • the method offers the same advantages as the slide cam system disclosed herein.
  • the method has greater flexibility since it is not limited to the axial displacement of the cam carrier by means of the actuators and engagement tracks as disclosed herein.
  • the method can use the slide cam system disclosed herein, preferably with elements of actuators that can be moved in and out radially and engage in spiral engagement tracks, for axially displacing the cam carrier.
  • the method can use a different displacement system for axially displacing the cam carrier.
  • the axial displacement of the cam carrier begins while the cam follower is operatively connected to the boundary section of the first cam or the second cam, and / or ends while the cam follower is operatively connected to the base circle region of the first cam or the second cam.
  • the axial displacement of the cam carrier begins and / or ends while the cam follower is in operative connection with the base circle region of the first cam or second cam, and / or ends while the cam follower is in operative connection with the boundary section of the first cam or second cam.
  • variable valve train with a sliding cam system enables switching between different valve control curves of the actuated gas exchange valves.
  • the system disclosed by way of example relates to the actuation of exhaust valves of an internal combustion engine.
  • the principles disclosed herein are also applicable to a variable valve train for one or more intake valves.
  • variable valve train 10 In the Figures 1 and 2nd A variable valve train 10 is shown.
  • the variable valve train 10 has a camshaft 12 and a cam carrier 14.
  • the variable valve train 10 has first and second transmission devices 16 and 18 and first and second exhaust valves 20 and 22.
  • the variable valve train 10 has a first actuator 24 and a second actuator 26.
  • the cam carrier 14, the transmission devices 16 and 18 and the actuators 24 and 26 form a sliding cam system 11.
  • the camshaft 12 is designed as an output camshaft, which actuates the output valves 20 and 22.
  • the camshaft 12 is part of a double camshaft system (not shown in detail) which additionally has an intake camshaft (not shown) for actuating one or more intake valves.
  • the camshaft 12 is arranged together with the intake camshaft as an overhead camshaft.
  • DOHC system double overhead camshaft
  • the camshaft 12 could also form a so-called SOHC system (single overhead camshaft).
  • the camshaft 12 can also be arranged as an underlying camshaft.
  • the cam carrier 14 is arranged in a rotationally fixed manner on the camshaft 12.
  • the cam carrier 14 is additionally arranged axially displaceably along a longitudinal axis of the camshaft 12.
  • the cam carrier 14 can be axially displaceable between a first stop 28 and a second stop 30.
  • cam carrier 14 has three cams 32, 34 and 36 which are offset from one another in a longitudinal direction of the cam carrier 14 and the camshaft 12.
  • the first cam 32 is arranged at a first end of the cam carrier 14 and is designed for normal operation, as will be described in detail later by way of example.
  • the second cam 34 is arranged adjacent to the first cam 32 and is designed for engine braking operation, as will also be described later in detail by way of example.
  • the third cam 36 is spaced apart from the second cam 34 and the second end of the cam carrier 14.
  • the third cam 36 is designed for normal operation.
  • the third cam 36 is shaped like the first cam 32.
  • the cam carrier 14 also has a first cam-free section 38 and a second cam-free section 40.
  • the first cam-free section 38 is arranged at the second end of the cam carrier 14.
  • the second cam-free section 40 is arranged between the second cam 34 and the third cam 36.
  • a first engagement track (shift link) 42 extends spirally around a longitudinal axis of the cam carrier 14.
  • a second engagement track (shift link) 44 extends spirally around the longitudinal axis of the cam carrier 14.
  • the actuators 24 and 26 selectively engage (engage) with extendable elements (e.g. pin or pin; not shown in detail) in the engagement tracks 42, 44.
  • the first actuator 24 can selectively engage the first engagement track 42 to shift the cam carrier 14 from one axial position to another axial position.
  • the cam carrier 14 bears against the second stop 30.
  • the cam carrier 14 bears against the first stop 28.
  • the cam carrier is shown in the first axial position.
  • the second actuator 26 can in turn selectively engage the second engagement track 44. Then the cam carrier 14 is shifted from the first axial position to the second axial position.
  • the first actuator 24 and the second actuator 26 are controlled by a schematically represented control unit 27 ( Figures 1 and 2nd ) controlled.
  • the shift is triggered in that the extended pin of the respective actuator 24, 26 is stationary with respect to an axial direction of the camshaft 12.
  • the slidable cam carrier 14 is displaced in a longitudinal direction of the camshaft 12 due to the spiral shape of the engagement tracks 42, 44 when the extended pin is in the respective engagement track 42, 44 engages.
  • the pin of the respective actuator 24, 26 is guided by the respective engagement track 42, 44 opposite to the extension direction and thus retracted.
  • the pin of the respective actuator 24, 26 comes out of engagement with the respective engagement track 42, 44.
  • the first transmission device 16 and the second transmission device 18 establish an operative connection between the cam carrier 14 and the exhaust valves 20, 22.
  • the first exhaust valve 20 is operated (opened) when the first cam 32 or the second cam 34 presses the first transmission device 16 down.
  • the second exhaust valve 22 is operated (opened) when the third cam 36 pushes the second transmission device 18 down.
  • the cam carrier 14 is in the first axial position (as in FIGS Figures 1 to 4 ), the first transmission device 16 is operatively connected between the first cam 32 and the first exhaust valve 20 via a cam follower 16A. In other words, the first transmission device 16 is not operatively connected between the second cam 34 in the first axial position of the cam carrier 14 and the first exhaust valve 20.
  • the first exhaust valve 20 is actuated according to a contour of the first cam 32.
  • the first transmission device 16 is operatively connected via the cam follower 16A between the second cam 34 and the first exhaust valve 20.
  • the first exhaust valve 20 is actuated according to a contour of the second cam 34.
  • the second transmission device 18 In the first axial position of the cam carrier 14, the second transmission device 18 is operatively connected between the third cam 36 and the second exhaust valve 22 via a cam follower 18A.
  • the second exhaust valve 22 is actuated according to a contour of the third cam 36.
  • the second transmission device 18 In the second axial position of the cam carrier 14, the second transmission device 18 does not actuate the second exhaust valve 22.
  • the cam follower 18A of the second transmission device 18 lies at the same axial position with respect to the camshaft 12 as the first cam-free section 38.
  • the first cam-free section 38 has no elevation for actuating the second transmission device 18. If the cam carrier 14 is in the second axial position, the second exhaust valve 22 is not actuated.
  • the first cam-free section 38 thus has two functions. On the one hand, the first cam-free section 38 receives the first engagement track 42. On the other hand, the first serves cam-free Section 38 that no actuation of the second exhaust valve 22 takes place in the second axial position of the cam carrier 14. This functional integration is inexpensive for reasons of installation space.
  • the first transmission device 16 and the second transmission device 18 are each designed as a rocker arm. In other embodiments, the transmission devices 16 and 18 can be designed as rocker arms or tappets. In some embodiments, the transmission devices 16 and 18 can have rotatably mounted rollers, for example, as cam followers 16A, 18A.
  • the locking device 46 has an elastic element 48 and a locking body 50.
  • the elastic element 48 is arranged in a blind hole in the camshaft 12.
  • the elastic element 48 prestresses the locking body 50 against the cam carrier 14.
  • First and second recesses 52 and 54 are arranged in an inner peripheral surface of the cam carrier 14. To lock the cam carrier 14, the locking body 50 is pressed into the first recess 52 when the cam carrier 14 is in the first axial position. In the second axial position of the cam carrier 14, the locking body 50 is pressed into the second recess 54.
  • FIG 5A is a section through the second cam 34 along the line BB in Figure 4 shown.
  • the second cam 34 has a first base circle region 34A and a second base circle region 34C.
  • the base circle areas 34A, 34C are separated from one another by a first valve lift area 34B and on the other hand by a second valve lift area 34D.
  • the second valve lift area 34D has a boundary portion 34E that is directly adjacent to the first base circle area 34A.
  • the boundary section 34E forms a trailing edge (ramp) of the second cam 34.
  • FIG 5B is a section through the first cam 32 along the line CC in Figure 4 shown.
  • the first cam 32 has a base circle area 32A and a valve lift area 32B.
  • the valve lift area 32B has a boundary portion 32C that is directly adjacent to the base circle area 32A.
  • the boundary section 32C forms a trailing edge (ramp) of the first cam 32.
  • the boundary portion 32C of the first cam 32 and the boundary portion 34E of the second cam 34 are the same.
  • the boundary portion 32C of the first cam 32 and the Boundary portions 34E of the second cam 34 are arranged at a same circumferential position with respect to a longitudinal axis of the camshaft 12.
  • the boundary sections 32C, 34E form a common flat ramp.
  • the boundary sections 32C, 34E thus enable the cam carrier 14 to be axially displaced not only in the base circle region 32A, 34A, but also in the boundary section 32C, 34E.
  • a dotted curve A indicates a valve lift of the exhaust valve 20 according to a normal operation, as caused by the first cam 32.
  • the curve A thus corresponds to a rolled-up cam profile of the first cam 32.
  • the exhaust valve 20 is opened during the exhaust stroke (push-out stroke) for pushing out exhaust gas through the valve lift area 32B. Otherwise, the exhaust valve 20 remains closed due to the base circle area 32A of the first cam 32.
  • a solid curve B indicates a valve lift of the exhaust valve 20 according to an engine braking operation, as caused by the second cam 34.
  • the curve B thus corresponds to a rolled-up cam profile of the second cam 34.
  • the exhaust valve 20 is slightly opened at the end of the compression stroke in the area of the top dead center at around 60 ° KW to 100 ° KW before the top dead center by the first valve lift area 34B. This is in Figure 6 each shown at around -225 ° NW (camshaft angle) and at around 135 ° NW.
  • exhaust valve 20 is further opened by valve lift region 34B and closes at about bottom dead center at the end of the expansion stroke.
  • Opening the exhaust valve 20 at the end of the compression stroke causes the compressed air in the cylinder to be pushed through the opened exhaust valve 20 into the exhaust system by the piston moving to top dead center.
  • the compression work previously performed brakes the crankshaft and thus the internal combustion engine.
  • the open exhaust valve 20 during the expansion stroke causes air to be drawn back into the cylinder from the exhaust pipes.
  • the cylinder is essentially filled with air from the exhaust system.
  • the exhaust valve 20 can first be closed by the second base circle region 34C after reaching the bottom dead center at the end of the expansion cycle being held.
  • the outlet valve 20 opens in the area of the top dead center through the second valve lift area 34D.
  • the opening again takes place at around 60 ° KW to 100 ° KW before top dead center. This is in Figure 6 each shown at around -45 ° NW and at around 315 ° NW.
  • the closed exhaust valve 20 during the first portion of the extension stroke causes the air drawn in the expansion stroke to be compressed while doing work.
  • the cylinder pressure rises.
  • the compression work brakes the crankshaft and thus the internal combustion engine.
  • the opening of the exhaust valve 20 at the end of the push-out cycle results in the air being pushed into the exhaust system through the opened exhaust valve 20.
  • the cylinder is filled with air again through the open intake valve or valves. The cycle starts again.
  • first cam 32 and the second cam 34 are matched to one another such that the boundary section 32C of the first cam 32 and the boundary section 34E of the second cam 34 are of identical (identical) design.
  • This enables an axial displacement of the cam carrier 14 not only within the base circle areas 32A, 34A. Instead, the axial displacement can additionally take place while the cam follower 16A is operatively connected to one of the limit sections 32C, 34E. This means that the axial displacement can begin earlier. This can be seen from the curves C, D and E.
  • the dash-dotted curve C relates to a movement of the movable pin from one of the actuators 24 or 26 with respect to the cam carrier 14.
  • the dashed curve D relates to a movement of the respective engagement track 42 or 44 and thus of the cam carrier 14 along the longitudinal axis of the camshaft 12
  • the colon-dash curve E shows a course of a depth contour of the respective engagement track 42 or 44 (only in Figure 6 shown).
  • the movable pin of the first actuator 24 is extended in the direction of the first engagement track 42 and thereby tracks into the first engagement track 42.
  • the tracking is done by the trained depth contour of the first engagement track 42 enables (see curve E).
  • a cross-sectional narrowing of the first engagement track 42 leads to a play reduction between the pin of the first actuator 24 and the first engagement track 24.
  • the play reduction takes place in an area S (see Figure 7 ).
  • the area S is reached and traversed by the pin of the first actuator 24 before the cam follower 16A reaches the limit section 32C of the first cam 32.
  • the cam follower 16A finally reaches the limit section 32C of the first cam 32, the spiral shape begins in the first engagement track 42, which causes an axial displacement of the cam carrier 14.
  • the cam carrier 14 is already displaced in a first displacement region V1, while the cam follower 16A is in contact with the limit section 32C. This starts the axial displacement of the cam carrier 14 before the cam follower 16A reaches the base circle region 32A. In the base circle region 32A, 34A, the axial displacement of the cam follower 16A is carried out further (displacement region V2) and finally ended before the cam follower 16A reaches the first valve lift region 34B.
  • the axial displacement of the cam carrier 14 thus also takes place outside the base circle regions 32A, 34A in the boundary section 32C of the first cam 32 and the boundary section 34E of the second cam 34.
  • This increases the time range for the axial displacement of the cam carrier 14. Because of the increased displacement range, the accelerations and thus the inertial forces can be reduced for the axial displacement of the cam carrier 14 at the same switching speed. On the one hand, this can be used to increase functional reliability and service life due to lower forces and pressures. On the other hand, this can be used to increase the maximum switching speed of the system.
  • the additional displacement range V1 which is made possible by the identically configured limit sections 32C, 34E, extends over approximately 22 ° camshaft angles.
  • the cam-free section 38 which serves both as a zero cam and is provided with the second engagement track 42, with an additional axial tolerance range (clearance range).
  • the adjacent cam 36 is made correspondingly narrower. Then, during the axial displacement within the boundary portions 32C, 34E from the second axial position to the first axial position, the cam follower 18A axially shifted within this additional tolerance range. A collision of the cam follower 18A with a cam runout of the third cam 36 is prevented.
  • slide cam system described herein is not limited to the application described herein.
  • an identical design of the startup areas (inlet areas) of the cams can be provided in order to implement the boundary sections of the same design.
  • variable valve trains for intake valves of an internal combustion engine For example, a start-up area of a first cam for normal operation can be designed identically to a start-up area of a second cam for mill operation and can be positioned at the same circumferential position with respect to the longitudinal axis of the camshaft.
  • displacement device first actuator, second actuator, first engagement track, second engagement track
  • first actuator second actuator, first engagement track, second engagement track
  • a method for operating an internal combustion engine with any displacement device for the cam carrier can comprise displacing the cam carrier while the cam follower is in contact with the boundary region or regions.
  • an axial displacement can begin and / or end when the cam follower is in contact with a limit area.

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  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
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  • Combustion & Propulsion (AREA)
  • Valve Device For Special Equipments (AREA)

Description

Die Erfindung betrifft ein Schiebenockensystem für einen variablen Ventiltrieb, einen variablen Ventiltrieb, ein Kraftfahrzeug und ein Verfahren zum Betreiben eines Verbrennungsmotors.The invention relates to a sliding cam system for a variable valve train, a variable valve train, a motor vehicle and a method for operating an internal combustion engine.

Ventilgesteuerte Brennkraftmaschinen weisen eines oder mehrere steuerbare Ein- und Auslassventile je Zylinder auf. Variable Ventilsteuerungen ermöglichen ein flexibles Ansteuern der Ventile zum Verändern der Öffnungszeit, Schließzeit und/oder des Ventilhubs. Dadurch kann der Motorbetrieb beispielsweise an eine spezifische Lastsituation angepasst werden.Valve-controlled internal combustion engines have one or more controllable intake and exhaust valves per cylinder. Variable valve controls allow flexible control of the valves to change the opening time, closing time and / or the valve lift. As a result, engine operation can be adapted to a specific load situation, for example.

Aus der DE 196 11 641 C1 ist ein Ventiltrieb bekannt, mit dem die Betätigung eines Gaswechselventils mit mehreren unterschiedlichen Hubkurven ermöglicht wird. Hierzu ist auf der Nockenwelle ein Schiebenocken mit mindestens einem, mehrere Nockenbahnen aufweisenden Nockenabschnitt drehfest aber axial verschieblich gelagert, der eine Hubkontur aufweist, in die ein Aktuator in Form eines Stifts von radial außen zur Erzeugung einer axialen Verschiebung des Schiebenockens eingeführt wird. Durch die axiale Verschiebung des Schiebenockens wird beim jeweiligen Gaswechselventil ein unterschiedlicher Ventilhub eingestellt. Der Schiebenocken wird nach der axialen Verschiebung desselben relativ zur Nockenwellen dadurch in seiner axialen Relativposition auf der Nockenwelle rastiert, dass abhängig von der axialen Relativposition mindestens eine federbeaufschlagte Rastkugel, die in der Nockenwelle aufgenommen und gelagert ist, in mindestens eine Rastnut eingreift. Die axiale Verschiebung des Schiebenockens zur Veränderung des Ventilhubs erfolgt ausschließlich im sogenannten Grundkreis des oder jedes Nockenabschnitts bzw. der Nockenbahnen desselben. Hierdurch wird die Schaltdrehzahl des Ventiltriebs beschränkt.From the DE 196 11 641 C1 A valve train is known with which the actuation of a gas exchange valve with several different stroke curves is made possible. For this purpose, a sliding cam with at least one cam section having a plurality of cam tracks is rotatably but axially displaceably mounted on the camshaft and has a stroke contour into which an actuator in the form of a pin is inserted from the outside radially to produce an axial displacement of the sliding cam. Due to the axial displacement of the slide cam, a different valve lift is set for the respective gas exchange valve. After the axial displacement thereof relative to the camshafts, the sliding cam is locked in its axial relative position on the camshaft in that, depending on the axial relative position, at least one spring-loaded locking ball, which is received and supported in the camshaft, engages in at least one locking groove. The axial displacement of the sliding cam to change the valve lift takes place exclusively in the so-called base circle of the or each cam section or the cam tracks of the same. This limits the switching speed of the valve train.

Je kürzer die miteinander übereinstimmenden Grundkreise der Nocken sind, desto weniger Zeit steht zum axialen Verschieben des Schiebenockens zur Verfügung. Umso weniger Zeit zum axialen Verschieben des Schiebenockensystem Verfügung steht, desto steiler muss die Rampe der Schaltkulisse (Eingriffsspur) ausgeführt werden. Beim axialen Verschieben des Schiebenockens können teilweise erhebliche Kräfte beim Kontakt zwischen dem Stift des Aktuators und der Schaltkulisse auftreten. Insbesondere bei steilen Rampen können besonders große Kräfte auftreten, die eine Lebensdauer des Schiebenockensystems negativ beeinflussen können und/oder eine maximale Schaltdrehzahl begrenzen.The shorter the matching base circles of the cams are, the less time is available for axially displacing the sliding cam. The less time is available for axially shifting the sliding cam system, the steeper the ramp of the shift gate (engagement track) must be. When the sliding cam is axially displaced, considerable forces can sometimes arise in the contact between the pin of the actuator and the shifting gate. Particularly with steep ramps, particularly large forces can occur which can negatively influence the service life of the sliding cam system and / or limit a maximum switching speed.

Aus der DE 10 2012 112 482 A1 ist ein Verfahren zum Betreiben einer Brennkraftmaschine mit mehreren Zylindern offenbart. Die Brennkraftmaschine weist zur Betätigung von Gaswechselventilen einen Ventiltrieb mit mindestens einer drehbar gelagerten Nockenwelle und mit mindestens einem auf der jeweiligen Nockenwelle axial verschiebbaren Schiebenocken auf. Der jeweilige Schiebenocken weist mindestens einen Kulissenabschnitt mit mindestens einer an einer äußeren Mantelfläche des jeweiligen Kulissenabschnitts ausgebildeten Nut auf, wobei der jeweilige Schiebenocken mindestens einen Nockenabschnitt mit mehreren Nockenbahnen zur Einstellung unterschiedlicher Ventilhübe aufweist. Zur Bewirkung einer axialen Verschiebung des jeweiligen Schiebenockens wird ein betätigbarer Stift eines Aktuators von radial außen in eine Nut des Kulissenabschnitts eingeführt. Die axiale Verschiebung des jeweiligen Schiebenockens wird abhängig von der axialen Verschieberichtung desselben und/oder abhängig von einem Ventilspiel außerhalb eines Grundkreises des oder jedes Nockenabschnitts desselben durchgeführt.From the DE 10 2012 112 482 A1 discloses a method of operating an internal combustion engine with a plurality of cylinders. To operate gas exchange valves, the internal combustion engine has a valve train with at least one rotatably mounted camshaft and with at least one sliding cam that can be axially displaced on the respective camshaft. The respective sliding cam has at least one link section with at least one groove formed on an outer lateral surface of the respective link section, the respective sliding cam having at least one cam section with a plurality of cam tracks for setting different valve lifts. In order to effect an axial displacement of the respective sliding cam, an actuatable pin of an actuator is inserted from radially outside into a groove in the link section. The axial displacement of the respective sliding cam is carried out depending on the axial displacement direction of the same and / or depending on a valve clearance outside a base circle of the or each cam section thereof.

Die GB 2 545 257 A offenbart einen Verbrennungsmotor mit einem Nockenschiebesystem aufweisend eine Schalteinheit, die drehfest und axial in Bezug auf eine Nockenwelle beweglich ist, wobei die Schalteinheit mindestens zwei Nocken umfasst, die konfiguriert sind, um selektiv mit einem Nockenfolger in Kontakt gebracht zu werden. Die Nocken sind mit einem Grundkreis und mit mindestens einer Nockenerhebung versehen. Während einer axialen Verschiebung der Schalteinheit kontaktiert der Nockenfolger mindestens einen Teil mindestens einer Nockenerhebung außerhalb des Grundkreises.The GB 2 545 257 A discloses an internal combustion engine with a cam shifting system comprising a switch unit that is rotationally fixed and axially movable with respect to a camshaft, the switch unit comprising at least two cams configured to be selectively brought into contact with a cam follower. The cams are provided with a base circle and at least one cam lobe. During an axial displacement of the switching unit, the cam follower contacts at least a part of at least one cam elevation outside the base circle.

Die US 8 863 714 B1 , die DE 10 2012 209 860 A1 , die US 2015/075468 A1 und die US 2007/034182 A1 offenbaren weitere Schiebenockensysteme.The US 8 863 714 B1 , the DE 10 2012 209 860 A1 , the US 2015/075468 A1 and the US 2007/034182 A1 disclose further sliding cam systems.

Der Erfindung liegt die Aufgabe zu Grunde, ein alternatives oder verbessertes Schiebenockensystem und Verfahren zum Betreiben eines Verbrennungsmotors zu schaffen, bei der die auftretenden Kräfte während des Verschiebevorgangs des Nockenträgers im Vergleich zu herkömmlichen Systemen verringert werden.The invention is based on the object of providing an alternative or improved sliding cam system and method for operating an internal combustion engine in which the forces which occur during the displacement process of the cam carrier are reduced in comparison with conventional systems.

Die Aufgabe wird gelöst durch ein Schiebenockensystem und ein Verfahren gemäß den unabhängigen Ansprüchen. Vorteilhafte Weiterbildungen sind in den abhängigen Ansprüchen und der Beschreibung angegeben.The object is achieved by a sliding cam system and a method according to the independent claims. Advantageous further developments are specified in the dependent claims and the description.

Das Schiebenockensystem ist für einen variablen Ventiltrieb eines Verbrennungsmotors eines Kraftfahrzeugs, insbesondere Nutzfahrzeugs, ausgebildet. Das Schiebenockensystem weist eine Nockenwelle und einen Nockenträger auf. Der Nockenträger ist auf der Nockenwelle drehfest und axial verschiebbar zwischen einer ersten Axialposition und einer zweiten Axialposition angeordnet und weist einen ersten Nocken, einen zweiten Nocken und eine erste Eingriffsspur zum axialen Verschieben des Nockenträgers auf. Das Schiebenockensystem weist einen Nockenfolger, der in der ersten Axialposition des Nockenträgers in Wirkverbindung mit dem ersten Nocken steht und in der zweiten Axialposition des Nockenträgers in Wirkverbindung mit dem zweiten Nocken steht, auf. Das Schiebenockensystem weist einen ersten Aktor, der ein ein- und ausfahrbares Element, insbesondere einen Stift, zum Einspuren in die erste Eingriffsspur zum axialen Verschieben des Nockenträgers aufweist, auf. Der erste Nocken und der zweite Nocken sind entlang einer Längsachse der Nockenwelle versetzt zueinander angeordnet. Der erste Nocken weist einen Grundkreisbereich und einen Ventilhubbereich mit einem Grenzabschnitt, der an den Grundkreisbereich des ersten Nockens angrenzt, auf. Der zweite Nocken weist einen Grundkreisbereich und einen Ventilhubbereich mit einem Grenzabschnitt, der an den Grundkreisbereich des zweiten Nockens angrenzt, auf. Der Grenzabschnitt des ersten Nockens und der Grenzabschnitt des zweiten Nockens sind gleich ausgebildet und an einer gleichen Umfangsposition um die Längsachse der Nockenwelle angeordnet. Der erste Aktor, der Nockenfolger und die erste Eingriffsspur sind so angeordnet und ausgebildet, dass eine Axialverschiebung des Nockenträgers durchführbar ist, während der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens und/oder dem Grenzabschnitt des zweiten Nockens steht.The sliding cam system is designed for a variable valve train of an internal combustion engine of a motor vehicle, in particular a commercial vehicle. The sliding cam system points a camshaft and a cam carrier. The cam carrier is arranged on the camshaft in a rotationally fixed and axially displaceable manner between a first axial position and a second axial position and has a first cam, a second cam and a first engagement track for axially displacing the cam carrier. The sliding cam system has a cam follower that is operatively connected to the first cam in the first axial position of the cam carrier and is operatively connected to the second cam in the second axial position of the cam carrier. The sliding cam system has a first actuator, which has a retractable and extendable element, in particular a pin, for engagement in the first engagement track for axial displacement of the cam carrier. The first cam and the second cam are offset from one another along a longitudinal axis of the camshaft arranged. The first cam has a base circle area and a valve lift area with a boundary section which adjoins the base circle area of the first cam. The second cam has a base circle area and a valve lift area with a boundary section which adjoins the base circle area of the second cam. The boundary section of the first cam and the boundary section of the second cam are of identical design and are arranged at the same circumferential position around the longitudinal axis of the camshaft. The first actuator, the cam follower and the first engagement track are arranged and designed in such a way that the cam carrier can be axially displaced while the cam follower is in operative connection with the boundary section of the first cam and / or the boundary section of the second cam.

Das Schiebenockensystem ermöglicht eine Verlängerung der zur Verfügung stehenden Zeitspanne zum axialen Verschieben des Nockenträgers durch Ausdehnung in die Grenzabschnitte der Nocken. Aufgrund des größeren Schaltbereichs können die Beschleunigungen und somit die Massenkräfte bei gleicher Schaltdrehzahl für die axiale Verschiebung reduziert werden. Einerseits kann dies beispielsweise dazu genutzt werden, um die Funktionssicherheit und Lebensdauer aufgrund geringerer Kräfte und Pressungen zu erhöhen. Andererseits kann dies beispielsweise dazu genutzt werden, um die maximale Schaltdrehzahl des Systems zu erhöhen.The sliding cam system enables an extension of the time available for the axial displacement of the cam carrier by expansion into the limit sections of the cams. Due to the larger switching range, the accelerations and thus the inertial forces can be reduced for the axial shift at the same switching speed. On the one hand, this can be used, for example, to increase functional reliability and service life due to lower forces and pressures. On the other hand, this can be used, for example, to increase the maximum switching speed of the system.

Insbesondere kann der erste Nocken direkt angrenzend an den zweiten Nocken ausgebildet sein.In particular, the first cam can be formed directly adjacent to the second cam.

In einem besonders bevorzugten Ausführungsform sind der erste Aktor, der Nockenfolger und die erste Eingriffsspur so angeordnet und ausgebildet, dass eine Axialverschiebung des Nockenträgers beginnt und/oder endet, während der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder dem Grenzabschnitt des zweiten Nockens steht. Damit kann insbesondere der Beginn und/oder das Ende der axialen Verschiebung des Nockenträgers in die Grenzbereiche verlagert werden. Somit kann die zur Verfügung stehende Zeitdauer zum axialen Verschieben des Nockenträgers verlängert werden.In a particularly preferred embodiment, the first actuator, the cam follower and the first engagement track are arranged and designed such that an axial displacement of the cam carrier begins and / or ends while the cam follower is in operative connection with the boundary section of the first cam or the boundary section of the second cam . In particular, the beginning and / or the end of the axial displacement of the cam carrier can thus be shifted into the boundary regions. The time available for axially displacing the cam carrier can thus be extended.

In einer Ausführungsform erstrecken sich die Grenzabschnitte über einen Bereich größer oder gleich 1° Nockenwellenwinkel.In one embodiment, the boundary sections extend over a range greater than or equal to 1 ° camshaft angle.

In einer Weiterbildung erstrecken sich die Grenzabschnitte über einen Bereich zwischen 5° und 45° Nockenwellenwinkel, insbesondere zwischen 15° und 30° Nockenwellenwinkel.In a further development, the boundary sections extend over a range between 5 ° and 45 ° camshaft angles, in particular between 15 ° and 30 ° camshaft angles.

In einer weiteren Ausführungsform bilden die Grenzabschnitte eine gemeinsame flächige Rampe.In a further embodiment, the boundary sections form a common flat ramp.

In einer Ausführungsvariante sind die Grenzabschnitte in einem Auslaufbereich des ersten und zweiten Nockens angeordnet. Alternativ oder zusätzlich beginnt die Axialverschiebung des Nockenträgers, wenn der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder des zweiten Nockens steht. Vorzugsweise endet die axiale Verschiebung, während der Nockenfolger in Wirkverbindung mit dem Grundkreisbereich des ersten Nockens oder des zweiten Nockens steht. Es ist allerdings auch möglich, dass die axiale Verschiebung erst in einem weiteren Grenzabschnitt in einem Einlaufbereich des ersten oder zweiten Nockens endet, wobei die weiteren Grenzabschnitte des ersten und zweiten Nockens wiederum gleich ausgebildet und an einer gleichen Umfangsposition um die Längsachse der Nockenwelle angeordnet sind.In one embodiment variant, the boundary sections are arranged in an outlet area of the first and second cams. Alternatively or additionally, the axial displacement of the cam carrier begins when the cam follower is in operative connection with the boundary section of the first cam or the second cam. The axial displacement preferably ends while the cam follower is in operative connection with the base circle region of the first cam or of the second cam. However, it is also possible for the axial displacement to end only in a further boundary section in an inlet region of the first or second cam, the further boundary sections of the first and second cams in turn being of the same design and arranged at the same circumferential position around the longitudinal axis of the camshaft.

In einer weiteren Ausführungsvariante sind die Grenzabschnitte in einem Einlaufbereich des ersten und zweiten Nockens angeordnet. Alternativ oder zusätzlich endet die Axialverschiebung des Nockenträgers, wenn der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder des zweiten Nockens steht. Vorzugsweise beginnt die axiale Verschiebung des Nockenträgers während der Nockenfolger in Wirkverbindung mit dem Grundkreisbereich des ersten Nockens oder des zweiten Nockens steht. Es ist allerdings auch möglich, die die axiale Verschiebung bereits in einem anderen Grenzabschnitt in einem Auslaufbereich des ersten oder zweiten Nockens beginnt, wobei die anderen Grenzabschnitte des ersten und zweiten Nockens wiederum gleich ausgebildet und an einer gleichen Umfangsposition um die Längsachse der Nockenwelle angeordnet sind.In a further embodiment variant, the boundary sections are arranged in an inlet area of the first and second cams. Alternatively or additionally, the axial displacement of the cam carrier ends when the cam follower is in operative connection with the boundary section of the first cam or the second cam. The axial displacement of the cam carrier preferably begins while the cam follower is in operative connection with the base circle region of the first cam or the second cam. However, it is also possible that the axial displacement already begins in another limit section in a run-out area of the first or second cam, the other limit sections of the first and second cam in turn having the same design and being arranged at the same circumferential position around the longitudinal axis of the camshaft.

In einem Ausführungsbeispiel weist der Nockenträger eine zweite Eingriffsspur zum axialen Verschieben des Nockenträgers in einer Richtung entgegengesetzt zu einer von der ersten Eingriffsspur bewirkten axialen Verschiebung auf. Das Schiebenockensystem weist ferner einen zweiten Aktor auf, der ein ein- und ausfahrbares Element, insbesondere einen Stift, zum Einspuren in die zweite Eingriffsspur zum axialen Verschieben des Nockenträgers aufweist. Der zweite Aktor, der Nockenfolger und die zweite Eingriffsspur sind so angeordnet und ausgebildet, dass eine Axialverschiebung des Nockenträgers durchführbar ist (insbesondere beginnt und/oder endet), während der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder dem Grenzabschnitt des zweiten Nockens steht.In one exemplary embodiment, the cam carrier has a second engagement track for axially displacing the cam carrier in a direction opposite to an axial displacement caused by the first engagement track. The sliding cam system also has a second actuator, which has a retractable and extendable element, in particular a pin, for engagement in the second engagement track for axial displacement of the cam carrier. The second actuator, the cam follower and the second engagement track are arranged and designed such that an axial displacement of the cam carrier can be carried out (in particular begins and / or ends) while the cam follower is in operative connection with the boundary section of the first cam or the boundary section of the second cam .

Insbesondere können der erste Aktor und der zweite Aktor separat voneinander vorgesehen sein. Es ist allerdings auch möglich, dass der erste Aktor und der zweite Aktor in einem gemeinsamen Gehäuse vorgesehen sind.In particular, the first actuator and the second actuator can be provided separately from one another. However, it is also possible for the first actuator and the second actuator to be provided in a common housing.

Vorzugsweise können die erste Eingriffsspur und die zweite Eingriffsspur separat voneinander vorgesehen sein. Es ist allerdings auch möglich, dass die erste Eingriffsspur und die zweite Eingriffsspur in einem gleichen Bereich des Nockenträgers angeordnet sind. Bevorzugt können sich die erste Eingriffsspur und die zweite Eingriffsspur kreuzen.The first engagement track and the second engagement track can preferably be provided separately from one another. However, it is also possible for the first engagement track and the second engagement track to be arranged in the same area of the cam carrier. The first engagement track and the second engagement track can preferably intersect.

In einem weiteren Ausführungsbeispiel weist die erste Eingriffsspur eine Querschnittsverengung zur Spielreduzierung zwischen der ersten Eingriffsspur und dem ein- und ausfahrbaren Element des ersten Aktors beim Einspuren (des ausgefahrenen Elements in die erste Eingriffsspur) auf. Die Querschnittsverengung ist so angeordnet, dass die Spielreduzierung stattfindet, bevor der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder des zweiten Nockens gelangt. Damit verkürzt der für die Spielreduzierung vorgesehene Abschnitt der Eingriffsspur den für die axiale Verschiebung des Nockenträgers vorgesehenen Abschnitt der Eingriffsspur nicht.In a further exemplary embodiment, the first engagement track has a cross-sectional constriction to reduce play between the first engagement track and the retractable and extendable element of the first actuator when engaging (the extended element in the first engagement track). The cross-sectional constriction is arranged such that the play reduction takes place before the cam follower comes into operative connection with the boundary section of the first cam or the second cam. Thus, the section of the engagement track provided for reducing the play does not shorten the section of the engagement track provided for the axial displacement of the cam carrier.

Zum Erzielen der gleichen Vorteile ist es auch möglich, dass die zweite Eingriffsspur eine Querschnittsverengung zur Spielreduzierung zwischen der zweiten Eingriffsspur und dem ein- und ausfahrbaren Element des zweiten Aktors beim Einspuren (des ausgefahrenen Elements in die zweite Eingriffsspur) aufweist. Die Querschnittsverengung ist so angeordnet, dass die Spielreduzierung stattfindet, bevor der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder des zweiten Nockens gelangt.To achieve the same advantages, it is also possible for the second engagement track to have a cross-sectional constriction to reduce play between the second engagement track and the retractable and extendable element of the second actuator when engaging (the extended element in the second engagement track). The cross-sectional constriction is arranged such that the play reduction takes place before the cam follower comes into operative connection with the boundary section of the first cam or the second cam.

In einer besonders bevorzugten Ausführungsform erstreckt sich die erste Eingriffsspur und/oder die zweite Eingriffsspur spiralförmig um die Längsachse der Nockenwelle.In a particularly preferred embodiment, the first engagement track and / or the second engagement track extends spirally around the longitudinal axis of the camshaft.

In einer weiteren Ausführungsform ist das ein- und ausfahrbare Element des ersten Aktors und/oder des zweiten Aktors radial bezüglich der Längsachse der Nockenwelle bewegbar.In a further embodiment, the retractable and extendable element of the first actuator and / or the second actuator can be moved radially with respect to the longitudinal axis of the camshaft.

Die Erfindung betrifft auch einen variablen Ventiltrieb für einen Verbrennungsmotor. Der variable Ventiltrieb weist ein Schiebenockensystem wie hierin offenbart auf. Der variable Ventiltrieb weist ein Gaswechselventil, insbesondere ein Einlassventil oder ein Auslassventil, das in Wirkverbindung mit dem Nockenfolger steht, auf. Der erste Nocken und der zweite Nocken bewirken unterschiedliche Ventilhübe, Öffnungszeiten und/oder Schließzeiten des Gaswechselventils.The invention also relates to a variable valve train for an internal combustion engine. The variable valve train has a slide cam system as disclosed herein. The variable valve train has a gas exchange valve, in particular an inlet valve or an outlet valve, which is operatively connected to the cam follower. The first cam and the second cam cause different valve lifts, opening times and / or closing times of the gas exchange valve.

In einer Weiterbildung ist das Gaswechselventil ein Auslassventil. Der erste Nocken ist für einen Normalbetrieb des Verbrennungsmotors ausgebildet, bei dem der erste Nocken das Auslassventil im Ausschubtakt offen hält. Der zweite Nocken ist für einen Motorbremsbetrieb des Verbrennungsmotors ausgebildet, bei dem, vorzugsweise, das Auslassventil im Verdichtungstakt und im Ausschubtakt zunächst geschlossen gehalten und vor Erreichen eines oberen Totpunkts einer Kolbenbewegung geöffnet wird.In one development, the gas exchange valve is an outlet valve. The first cam is designed for normal operation of the internal combustion engine, in which the first cam keeps the exhaust valve open during the exhaust stroke. The second cam is designed for engine braking operation of the internal combustion engine, in which, preferably, the exhaust valve is initially kept closed in the compression stroke and in the extension stroke and is opened before a piston movement reaches top dead center.

In einem bevorzugten Ausführungsbeispiel ist der zweite Nocken so ausgebildet, dass das Auslassventil zwischen 100° KW und 60° KW (Kurbelwellenwinkel) vor dem Erreichen des oberen Totpunkts öffnet. Alternativ oder zusätzlich ist der zweite Nocken so ausgebildet, dass das Auslassventil nach dem Öffnen im Ausschubtakt im Bereich zwischen dem oberem Totpunkt und 30° KW nach dem oberen Totpunkt schließt. Alternativ oder zusätzlich ist der zweite Nocken so ausgebildet, dass das Auslassventil nach dem Öffnen im Verdichtungstakt im Bereich zwischen dem unteren Totpunkt und 30° KW nach dem unteren Totpunkt schließt.In a preferred embodiment, the second cam is designed so that the exhaust valve opens between 100 ° KW and 60 ° KW (crankshaft angle) before reaching top dead center. As an alternative or in addition, the second cam is designed such that the exhaust valve closes in the region between top dead center and 30 ° CA after top dead center after opening in the extension stroke. Alternatively or additionally, the second cam is designed such that the outlet valve closes after opening in the compression stroke in the range between bottom dead center and 30 ° CA after bottom dead center.

Die Erfindung betrifft auch ein Kraftfahrzeug, insbesondere Nutzfahrzeug (zum Beispiel Lastkraftwagen oder Omnibus), aufweisend den variablen Ventiltrieb wie hierin offenbart oder das Schiebenockensystem wie hierin offenbart.The invention also relates to a motor vehicle, in particular a commercial vehicle (for example a truck or bus), comprising the variable valve train as disclosed herein or the sliding cam system as disclosed herein.

Die Erfindung betrifft auch ein Verfahren zum Betreiben eines Verbrennungsmotors mit einem Schiebenockensystem. Das Schiebenockensystem weist einen auf einer Nockenwelle drehfest angeordneten und axial verschiebbaren Nockenträger mit einem ersten Nocken und einem zweiten Nocken auf. Der erste Nocken und der zweite Nocken weisen jeweils einen Grundkreisbereich und einen Ventilhubbereich mit einem Grenzabschnitt, der angrenzend an den jeweiligen Grundkreisbereich angeordnet ist, auf. Der Grenzabschnitt des ersten Nockens und der Grenzabschnitt des zweiten Nockens sind gleich ausgebildet und an einer gleichen Umfangsposition um eine Längsachse der Nockenwelle angeordnet. Das Schiebenockensystem weist einen Nockenfolger, der wahlweise in Wirkverbindung mit dem ersten Nocken oder dem zweiten Nocken steht, auf. Das Verfahren weist das axiale Verschieben des Nockenträgers auf, wobei das axiale Verschieben des Nockenträgers durchgeführt wird, insbesondere beginnt oder endet, während der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens und/oder des zweiten Nockens steht.The invention also relates to a method for operating an internal combustion engine with a sliding cam system. The sliding cam system has a cam carrier which is arranged on a camshaft in a rotationally fixed manner and is axially displaceable, with a first cam and a second cam. The first cam and the second cam each have a base circle area and a valve lift area with a boundary section which is arranged adjacent to the respective base circle area. The boundary section of the first cam and the boundary section of the second cam are of identical design and are arranged at the same circumferential position about a longitudinal axis of the camshaft. The sliding cam system has a cam follower, which is optionally operatively connected to the first cam or the second cam. The method has the axial displacement of the cam carrier, the axial displacement of the cam carrier being carried out, in particular starting or ending, while the cam follower is in operative connection with the boundary section of the first cam and / or the second cam.

Das Verfahren bietet die gleichen Vorteile wie das hierin offenbarte Schiebenockensystem. Zusätzlich weist das Verfahren eine höhere Flexibilität auf, da es nicht auf die axiale Verschiebung des Nockenträgers mittels der Aktoren und Eingriffsspuren wie hierin offenabrt beschränkt ist.The method offers the same advantages as the slide cam system disclosed herein. In addition, the method has greater flexibility since it is not limited to the axial displacement of the cam carrier by means of the actuators and engagement tracks as disclosed herein.

Insbesondere kann das Verfahren das hierin offenbarte Schiebenockensystem vorzugsweise mit radial ein- und ausfahrbaren Elementen von Aktoren, die in spiralförmige Eingriffspuren eingreifen, zum axialen Verschieben des Nockenträgers verwenden. Es ist allerdings auch möglich, dass das Verfahren ein anderes Verschiebesystem zum axialen Verschieben des Nockenträgers verwendet.In particular, the method can use the slide cam system disclosed herein, preferably with elements of actuators that can be moved in and out radially and engage in spiral engagement tracks, for axially displacing the cam carrier. However, it is also possible for the method to use a different displacement system for axially displacing the cam carrier.

In einer bevorzugten Ausführungsform beginnt das axiale Verschieben des Nockenträgers, während der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder des zweiten Nockens steht, und/oder endet, während der Nockenfolger in Wirkverbindung mit dem Grundkreisbereich des ersten Nockens oder des zweiten Nockens steht.In a preferred embodiment, the axial displacement of the cam carrier begins while the cam follower is operatively connected to the boundary section of the first cam or the second cam, and / or ends while the cam follower is operatively connected to the base circle region of the first cam or the second cam.

Alternativ oder zusätzlich beginnt das axiale Verschieben des Nockenträgers, während der Nockenfolger in Wirkverbindung mit dem Grundkreisbereich des ersten Nockens oder des zweiten Nockens steht, und/oder endet, während der Nockenfolger in Wirkverbindung mit dem Grenzabschnitt des ersten Nockens oder des zweiten Nockens steht.Alternatively or additionally, the axial displacement of the cam carrier begins and / or ends while the cam follower is in operative connection with the base circle region of the first cam or second cam, and / or ends while the cam follower is in operative connection with the boundary section of the first cam or second cam.

Die zuvor beschriebenen bevorzugten Ausführungsformen und Merkmale der Erfindung sind beliebig miteinander kombinierbar. Weitere Einzelheiten und Vorteile der Erfindung werden im Folgenden unter Bezug auf die beigefügten Zeichnungen beschrieben. Es zeigen:

Figur 1
eine perspektivische Ansicht eines beispielhaften variablen Ventiltriebs;
Figur 2
eine weitere perspektivische Ansicht des beispielhaften variablen Ventiltriebs;
Figur 3
eine Draufsicht auf eine Nockenwelle des beispielhaften variablen Ventiltriebs;
Figur 4
eine Längsschnittansicht der Nockenwelle von Figur 3 entlang der Linie A-A;
Figur 5A
eine erste Querschnittansicht der Nockenwelle von Figur 4 entlang der Linie B-B;
Figur 5B
eine zweite Querschnittansicht der Nockenwelle von Figur 4 entlang der Linie C-C;
Figur 6
ein Weg-Nockenwellenwinkel-Diagramm; und
Figur 7
eine Vergrößerung eines Bereichs des Weg-Nockenwellenwinkel-Diagramms von Figur 6.
The preferred embodiments and features of the invention described above can be combined with one another as desired. Further details and advantages of the invention are described below with reference to the accompanying drawings. Show it:
Figure 1
a perspective view of an exemplary variable valve train;
Figure 2
another perspective view of the exemplary variable valve train;
Figure 3
a plan view of a camshaft of the exemplary variable valve train;
Figure 4
a longitudinal sectional view of the camshaft of Figure 3 along the line AA;
Figure 5A
a first cross-sectional view of the camshaft of Figure 4 along the line BB;
Figure 5B
a second cross-sectional view of the camshaft of Figure 4 along line CC;
Figure 6
a displacement camshaft angle diagram; and
Figure 7
an enlargement of a range of the displacement-camshaft angle diagram of Figure 6 .

Die in den Figuren gezeigten Ausführungsformen stimmen zumindest teilweise überein, so dass ähnliche oder identische Teile mit den gleichen Bezugszeichen versehen sind und zu deren Erläuterung auch auf die Beschreibung der anderen Ausführungsformen bzw. Figuren verwiesen wird, um Wiederholungen zu vermeiden.The embodiments shown in the figures correspond at least partially, so that similar or identical parts are provided with the same reference numerals and for their explanation reference is also made to the description of the other embodiments or figures in order to avoid repetitions.

Nachfolgend ist unter Bezugnahme auf Figur 1 bis Figur 4 zunächst ein variabler Ventiltrieb mit Schiebenockensystem beschrieben. Das Schiebenockensystem ermöglicht eine Umschaltung zwischen verschiedenen Ventilsteuerkurven der betätigten Gaswechselventile. Das hierin beispielhaft offenbarte System bezieht sich auf die Betätigung von Auslassventilen eines Verbrennungsmotors. Die hierin offenbarten Prinzipien sind jedoch auch bei einem variablen Ventiltrieb für ein oder mehrere Einlassventile anwendbar.The following is with reference to Figure 1 to Figure 4 First, a variable valve train with a sliding cam system is described. The sliding cam system enables switching between different valve control curves of the actuated gas exchange valves. The system disclosed by way of example relates to the actuation of exhaust valves of an internal combustion engine. However, the principles disclosed herein are also applicable to a variable valve train for one or more intake valves.

In den Figuren 1 und 2 ist ein variabler Ventiltrieb 10 gezeigt. Der variable Ventiltrieb 10 weist eine Nockenwelle 12 und einen Nockenträger 14 auf. Zusätzlich weist der variable Ventiltrieb 10 eine erste und zweite Übertragungsvorrichtung 16 und 18 sowie ein erstes und zweites Auslassventil 20 und 22 auf. Zudem weist der variable Ventiltrieb 10 einen ersten Aktor 24 und einen zweiten Aktor 26 auf. Der Nockenträger 14, die Übertragungsvorrichtungen 16 und 18 sowie die Aktoren 24 und 26 bilden ein Schiebenockensystem 11.In the Figures 1 and 2nd A variable valve train 10 is shown. The variable valve train 10 has a camshaft 12 and a cam carrier 14. In addition, the variable valve train 10 has first and second transmission devices 16 and 18 and first and second exhaust valves 20 and 22. In addition, the variable valve train 10 has a first actuator 24 and a second actuator 26. The cam carrier 14, the transmission devices 16 and 18 and the actuators 24 and 26 form a sliding cam system 11.

Die Nockenwelle 12 ist als eine Ausgangsnockenwelle ausgebildet, die die Ausgangsventile 20 und 22 betätigt. Die Nockenwelle 12 ist Teil eines Doppelnockenwellensystems (nicht im Detail dargestellt), das zusätzlich eine Einlassnockenwelle (nicht dargestellt) zur Betätigung von einem oder mehreren Einlassventilen aufweist. Die Nockenwelle 12 ist gemeinsam mit der Einlassnockenwelle als obenliegende Nockenwelle angeordnet. Die Nockenwelle 12 und die Einlassnockenwelle bilden somit ein sogenanntes DOHC-System (engl. double overhead camshaft). Alternativ könnte die Nockenwelle 12 auch ein sogenanntes SOHC-System bilden (engl. single overhead camshaft). In anderen Ausführungsformen kann die Nockenwelle 12 auch als untenliegende Nockenwelle angeordnet sein.The camshaft 12 is designed as an output camshaft, which actuates the output valves 20 and 22. The camshaft 12 is part of a double camshaft system (not shown in detail) which additionally has an intake camshaft (not shown) for actuating one or more intake valves. The camshaft 12 is arranged together with the intake camshaft as an overhead camshaft. The camshaft 12 and the intake camshaft thus form a so-called DOHC system (double overhead camshaft). Alternatively, the camshaft 12 could also form a so-called SOHC system (single overhead camshaft). In other embodiments, the camshaft 12 can also be arranged as an underlying camshaft.

Auf der Nockenwelle 12 ist der Nockenträger 14 drehfest angeordnet. Der Nockenträger 14 ist zusätzlich axial verschiebbar entlang einer Längsachse der Nockenwelle 12 angeordnet. Der Nockenträger 14 kann zwischen einem ersten Anschlag 28 und einem zweiten Anschlag 30 axial verschiebbar sein.The cam carrier 14 is arranged in a rotationally fixed manner on the camshaft 12. The cam carrier 14 is additionally arranged axially displaceably along a longitudinal axis of the camshaft 12. The cam carrier 14 can be axially displaceable between a first stop 28 and a second stop 30.

Unter Bezugnahme auf die Figuren 1 bis 4 ist nachfolgend der Nockenträger 14 beschrieben. Der Nockenträger 14 weist drei Nocken 32, 34 und 36 auf, die in einer Längsrichtung des Nockenträgers 14 und der Nockenwelle 12 voneinander versetzt sind. Der erste Nocken 32 ist an einem ersten Ende des Nockenträgers 14 angeordnet und für einen Normalbetrieb ausgebildet, wie später beispielhaft im Detail beschrieben. Der zweite Nocken 34 ist angrenzend an den ersten Nocken 32 angeordnet und für einen Motorbremsbetrieb ausgebildet, wie später ebenfalls beispielhaft im Detail beschrieben. Der dritte Nocken 36 ist beabstandet zu dem zweiten Nocken 34 und dem zweiten Ende des Nockenträgers 14 angeordnet. Der dritte Nocken 36 ist für den Normalbetrieb ausgebildet. Der dritte Nocken 36 ist wie der ersten Nocken 32 geformt.With reference to the Figures 1 to 4 cam carrier 14 is described below. The cam carrier 14 has three cams 32, 34 and 36 which are offset from one another in a longitudinal direction of the cam carrier 14 and the camshaft 12. The first cam 32 is arranged at a first end of the cam carrier 14 and is designed for normal operation, as will be described in detail later by way of example. The second cam 34 is arranged adjacent to the first cam 32 and is designed for engine braking operation, as will also be described later in detail by way of example. The third cam 36 is spaced apart from the second cam 34 and the second end of the cam carrier 14. The third cam 36 is designed for normal operation. The third cam 36 is shaped like the first cam 32.

Der Nockenträger 14 weist zudem einen ersten nockenfreien Abschnitt 38 und einen zweiten nockenfreien Abschnitt 40 auf. Der erste nockenfreie Abschnitt 38 ist am zweiten Ende des Nockenträgers 14 angeordnet. Der zweite nockenfreie Abschnitt 40 ist zwischen dem zweiten Nocken 34 und dem dritten Nocken 36 angeordnet. Im ersten nockenfreien Abschnitt 38 erstreckt sich eine erste Eingriffsspur (Schaltkulisse) 42 spiralförmig um eine Längsachse des Nockenträgers 14. Im zweiten nockenfreien Abschnitt 40 erstreckt sich eine zweite Eingriffsspur (Schaltkulisse) 44 spiralförmig um die Längsachse des Nockenträgers 14.The cam carrier 14 also has a first cam-free section 38 and a second cam-free section 40. The first cam-free section 38 is arranged at the second end of the cam carrier 14. The second cam-free section 40 is arranged between the second cam 34 and the third cam 36. In the first cam-free section 38, a first engagement track (shift link) 42 extends spirally around a longitudinal axis of the cam carrier 14. In the second cam-free section 40, a second engagement track (shift link) 44 extends spirally around the longitudinal axis of the cam carrier 14.

Zum Verschieben des Nockenträgers 14 zwischen den Anschlägen 28 und 30 können die Aktoren 24 und 26 (Figuren 1 und 2) mit ausfahrbaren Elementen (z.B. Stift oder Pin; nicht im Detail gezeigt) selektiv in die Eingriffsspuren 42, 44 eingreifen (einspuren). Im Einzelnen kann der erste Aktor 24 selektiv in die erste Eingriffsspur 42 zum Verschieben des Nockenträgers 14 von einer Axialposition zu einer anderen Axialposition eingreifen. In einer ersten Axialposition liegt der Nockenträger 14 an dem zweiten Anschlag 30 an. In einer zweiten Axialposition liegt der Nockenträger 14 an dem ersten Anschlag 28 an. In den Figuren 1 bis 4 ist der Nockenträger in der ersten Axialposition dargestellt. Der zweite Aktor 26 wiederum kann selektiv in die zweite Eingriffsspur 44 eingreifen. Dann wird der Nockenträger 14 von der ersten Axialposition zu der zweiten Axialposition verschoben. Der erste Aktor 24 und der zweite Aktor 26 werden von einer schematisch dargestellten Steuereinheit 27 (Figuren 1 und 2) angesteuert.To move the cam carrier 14 between the stops 28 and 30, the actuators 24 and 26 ( Figures 1 and 2nd ) selectively engage (engage) with extendable elements (e.g. pin or pin; not shown in detail) in the engagement tracks 42, 44. Specifically, the first actuator 24 can selectively engage the first engagement track 42 to shift the cam carrier 14 from one axial position to another axial position. In a first axial position, the cam carrier 14 bears against the second stop 30. In a second axial position, the cam carrier 14 bears against the first stop 28. In the Figures 1 to 4 the cam carrier is shown in the first axial position. The second actuator 26 can in turn selectively engage the second engagement track 44. Then the cam carrier 14 is shifted from the first axial position to the second axial position. The first actuator 24 and the second actuator 26 are controlled by a schematically represented control unit 27 ( Figures 1 and 2nd ) controlled.

Die Verschiebung wird dadurch ausgelöst, dass der ausgefahrene Stift des jeweiligen Aktors 24, 26 bezüglich einer Axialrichtung der Nockenwelle 12 ortsfest ist. Folglich wird der verschiebbare Nockenträger 14 aufgrund der Spiralform der Eingriffsspuren 42, 44 in einer Längsrichtung der Nockenwelle 12 verschoben, wenn der ausgefahrene Stift in die jeweilige Eingriffsspur 42, 44 eingreift. Am Ende des Verschiebevorgangs wird der Stift des jeweiligen Aktors 24, 26 von der jeweiligen Eingriffsspur 42, 44 entgegengesetzt zu der Ausfahrrichtung geführt und somit eingefahren. Der Stift des jeweiligen Aktors 24, 26 gelangt außer Eingriff mit der jeweiligen Eingriffsspur 42, 44.The shift is triggered in that the extended pin of the respective actuator 24, 26 is stationary with respect to an axial direction of the camshaft 12. As a result, the slidable cam carrier 14 is displaced in a longitudinal direction of the camshaft 12 due to the spiral shape of the engagement tracks 42, 44 when the extended pin is in the respective engagement track 42, 44 engages. At the end of the displacement process, the pin of the respective actuator 24, 26 is guided by the respective engagement track 42, 44 opposite to the extension direction and thus retracted. The pin of the respective actuator 24, 26 comes out of engagement with the respective engagement track 42, 44.

Die erste Übertragungsvorrichtung 16 und die zweite Übertragungsvorrichtung 18 (Figuren 1 und 2) stellen eine Wirkverbindung zwischen dem Nockenträger 14 und den Auslassventilen 20, 22 her. Das erste Auslassventil 20 wird betätigt (geöffnet), wenn der erste Nocken 32 oder der zweite Nocken 34 die erste Übertragungsvorrichtung 16 nach unten drückt. Das zweite Auslassventil 22 wird betätigt (geöffnet) wenn der dritte Nocken 36 die zweite Übertragungsvorrichtung 18 nach unten drückt.The first transmission device 16 and the second transmission device 18 ( Figures 1 and 2nd ) establish an operative connection between the cam carrier 14 and the exhaust valves 20, 22. The first exhaust valve 20 is operated (opened) when the first cam 32 or the second cam 34 presses the first transmission device 16 down. The second exhaust valve 22 is operated (opened) when the third cam 36 pushes the second transmission device 18 down.

Befindet sich der Nockenträger 14 in der ersten Axialposition (wie in den Figuren 1 bis 4 gezeigt), ist die erste Übertragungsvorrichtung 16 über einen Nockenfolger 16A in Wirkverbindung zwischen dem ersten Nocken 32 und dem ersten Auslassventil 20. Mit anderen Worten gesagt, ist die erste Übertragungsvorrichtung 16 in der ersten Axialposition des Nockenträgers 14 nicht in Wirkverbindung zwischen dem zweiten Nocken 34 und dem ersten Auslassventil 20. Das erste Auslassventil 20 wird gemäß einer Kontur des ersten Nockens 32 betätigt. In der zweiten Axialposition des Nockenträgers 14 ist die erste Übertragungsvorrichtung 16 über den Nockenfolger 16A in Wirkverbindung zwischen dem zweiten Nocken 34 und dem ersten Auslassventil 20. Das erste Auslassventil 20 wird gemäß einer Kontur des zweiten Nockens 34 betätigt.The cam carrier 14 is in the first axial position (as in FIGS Figures 1 to 4 ), the first transmission device 16 is operatively connected between the first cam 32 and the first exhaust valve 20 via a cam follower 16A. In other words, the first transmission device 16 is not operatively connected between the second cam 34 in the first axial position of the cam carrier 14 and the first exhaust valve 20. The first exhaust valve 20 is actuated according to a contour of the first cam 32. In the second axial position of the cam carrier 14, the first transmission device 16 is operatively connected via the cam follower 16A between the second cam 34 and the first exhaust valve 20. The first exhaust valve 20 is actuated according to a contour of the second cam 34.

In der ersten Axialposition des Nockenträgers 14 ist die zweite Übertragungsvorrichtung 18 über einen Nockenfolger 18A in Wirkverbindung zwischen dem dritten Nocken 36 und dem zweiten Auslassventil 22. Das zweite Auslassventil 22 wird gemäß einer Kontur des dritten Nockens 36 betätigt. In der zweiten Axialposition des Nockenträgers 14 betätigt die zweite Übertragungsvorrichtung 18 das zweite Auslassventil 22 nicht. In der zweiten Axialposition des Nockenträgers 14 liegt der Nockenfolger 18A der zweiten Übertragungsvorrichtung 18 an der gleichen Axialposition bezüglich der Nockenwelle 12 wie der erste nockenfreie Abschnitt 38. Der erste nockenfreie Abschnitt 38 weist keine Erhebung zum Betätigen der zweiten Übertragungsvorrichtung 18 auf. Ist der Nockenträger 14 in der zweiten Axialposition, wird das zweite Auslassventil 22 nicht betätigt.In the first axial position of the cam carrier 14, the second transmission device 18 is operatively connected between the third cam 36 and the second exhaust valve 22 via a cam follower 18A. The second exhaust valve 22 is actuated according to a contour of the third cam 36. In the second axial position of the cam carrier 14, the second transmission device 18 does not actuate the second exhaust valve 22. In the second axial position of the cam carrier 14, the cam follower 18A of the second transmission device 18 lies at the same axial position with respect to the camshaft 12 as the first cam-free section 38. The first cam-free section 38 has no elevation for actuating the second transmission device 18. If the cam carrier 14 is in the second axial position, the second exhaust valve 22 is not actuated.

Der erste nockenfreie Abschnitt 38 hat somit zwei Funktionen. Einerseits nimmt der erste nockenfreie Abschnitt 38 die erste Eingriffsspur 42 auf. Andererseits dient der erste nockenfreie Abschnitt 38 dazu, dass keine Betätigung des zweiten Auslassventils 22 in der zweiten Axialposition des Nockenträgers 14 erfolgt. Diese Funktionsintegration ist aus Bauraumgründen günstig.The first cam-free section 38 thus has two functions. On the one hand, the first cam-free section 38 receives the first engagement track 42. On the other hand, the first serves cam-free Section 38 that no actuation of the second exhaust valve 22 takes place in the second axial position of the cam carrier 14. This functional integration is inexpensive for reasons of installation space.

In der dargestellten Ausführungsform sind die erste Übertragungsvorrichtung 16 und die zweite Übertragungsvorrichtung 18 jeweils als ein Schlepphebel ausgebildet. In anderen Ausführungsformen können die Übertragungsvorrichtungen 16 und 18 als Kipphebel oder Stößel ausgebildet sein. In einigen Ausführungsformen können die Übertragungsvorrichtungen 16 und 18 als Nockenfolger 16A, 18A beispielsweise drehbar gelagerte Rollen aufweisen.In the illustrated embodiment, the first transmission device 16 and the second transmission device 18 are each designed as a rocker arm. In other embodiments, the transmission devices 16 and 18 can be designed as rocker arms or tappets. In some embodiments, the transmission devices 16 and 18 can have rotatably mounted rollers, for example, as cam followers 16A, 18A.

Unter Bezugnahme auf Figur 4 ist eine Arretierungsvorrichtung 46 gezeigt. Die Arretierungsvorrichtung 46 weist ein elastisches Element 48 und einen Sperrkörper 50 auf. Das elastische Element 48 ist in einem Sackloch der Nockenwelle 12 angeordnet. Das elastische Element 48 spannt den Sperrkörper 50 gegen den Nockenträger 14 vor. In einer Innenumfangsfläche des Nockenträgers 14 sind eine erste und zweite Ausnehmung 52 und 54 angeordnet. Zum Arretieren des Nockenträgers 14 wird der Sperrkörper 50 in die erste Ausnehmung 52 gedrückt, wenn der Nockenträger 14 in der ersten Axialposition ist. In der zweiten Axialposition des Nockenträgers 14 wird der Sperrkörper 50 in die zweite Ausnehmung 54 gedrückt.With reference to Figure 4 A locking device 46 is shown. The locking device 46 has an elastic element 48 and a locking body 50. The elastic element 48 is arranged in a blind hole in the camshaft 12. The elastic element 48 prestresses the locking body 50 against the cam carrier 14. First and second recesses 52 and 54 are arranged in an inner peripheral surface of the cam carrier 14. To lock the cam carrier 14, the locking body 50 is pressed into the first recess 52 when the cam carrier 14 is in the first axial position. In the second axial position of the cam carrier 14, the locking body 50 is pressed into the second recess 54.

In Figur 5A ist ein Schnitt durch den zweiten Nocken 34 entlang der Linie B-B in Figur 4 dargestellt. Der zweite Nocken 34 weist einen ersten Grundkreisbereich 34A und einen zweiten Grundkreisbereich 34C auf. Die Grundkreisbereiche 34A, 34C sind einerseits durch einen ersten Ventilhubbereich 34B und andererseits durch einen zweiten Ventilhubbereich 34D voneinander getrennt. Der zweite Ventilhubbereich 34D weist einen Grenzabschnitt 34E auf, der direkt an den ersten Grundkreisbereich 34A angrenzt. Der Grenzabschnitt 34E bildet eine auslaufende Flanke (Rampe) des zweiten Nockens 34.In Figure 5A is a section through the second cam 34 along the line BB in Figure 4 shown. The second cam 34 has a first base circle region 34A and a second base circle region 34C. The base circle areas 34A, 34C are separated from one another by a first valve lift area 34B and on the other hand by a second valve lift area 34D. The second valve lift area 34D has a boundary portion 34E that is directly adjacent to the first base circle area 34A. The boundary section 34E forms a trailing edge (ramp) of the second cam 34.

In Figur 5B ist ein Schnitt durch den ersten Nocken 32 entlang der Linie C-C in Figur 4 dargestellt. Der erste Nocken 32 weist einen Grundkreisbereich 32A und einen Ventilhubbereich 32B auf. Der Ventilhubbereich 32B weist einen Grenzabschnitt 32C auf, der direkt an den Grundkreisbereich 32A angrenzt. Der Grenzabschnitt 32C bildet eine auslaufende Flanke (Rampe) des ersten Nockens 32.In Figure 5B is a section through the first cam 32 along the line CC in Figure 4 shown. The first cam 32 has a base circle area 32A and a valve lift area 32B. The valve lift area 32B has a boundary portion 32C that is directly adjacent to the base circle area 32A. The boundary section 32C forms a trailing edge (ramp) of the first cam 32.

Der Grenzabschnitt 32C des ersten Nockens 32 und der Grenzabschnitt 34E des zweiten Nockens 34 sind gleich ausgebildet. Der Grenzabschnitt 32C des ersten Nockens 32 und der Grenzabschnitt 34E des zweiten Nockens 34 sind an einer gleichen Umfangsposition bezüglich einer Längsachse der Nockenwelle 12 angeordnet. Die Grenzabschnitte 32C, 34E bilden eine gemeinsame flächige Rampe. Damit ermöglichen die Grenzabschnitte 32C, 34E, dass eine Axialverschiebung des Nockenträgers 14 nicht nur im Grundkreisbereich 32A, 34A stattfindet, sondern zusätzlich im Grenzabschnitt 32C, 34E.The boundary portion 32C of the first cam 32 and the boundary portion 34E of the second cam 34 are the same. The boundary portion 32C of the first cam 32 and the Boundary portions 34E of the second cam 34 are arranged at a same circumferential position with respect to a longitudinal axis of the camshaft 12. The boundary sections 32C, 34E form a common flat ramp. The boundary sections 32C, 34E thus enable the cam carrier 14 to be axially displaced not only in the base circle region 32A, 34A, but also in the boundary section 32C, 34E.

In der Figur 6 sind verschiedene Kurven A bis E in einem Weg-Nockenwellenwinkel-Diagramm dargestellt. In Figur 7 ist eine Vergrößerung eines Bereichs des Diagramms von Figur 6 dargestellt, in dem insbesondere die Grenzabschnitte 32C, 34E dargestellt sind.In the Figure 6 Various curves A to E are shown in a path-camshaft angle diagram. In Figure 7 is an enlargement of a portion of the graph of Figure 6 in which in particular the boundary sections 32C, 34E are shown.

Eine gepunktete Kurve A gibt einen Ventilhub des Auslassventils 20 gemäß einem Normalbetrieb an, wie vom ersten Nocken 32 bewirkt. Die Kurve A entspricht somit einem abgerollten Nockenprofil des ersten Nockens 32. Im Normalbetrieb wird das Auslassventil 20 während des Auslasstaktes (Ausschiebetaktes) zum Ausschieben von Abgas durch den Ventilhubbereich 32B geöffnet. Im Übrigen bleibt das Auslassventil 20 aufgrund des Grundkreisbereichs 32A des ersten Nockens 32 geschlossen.A dotted curve A indicates a valve lift of the exhaust valve 20 according to a normal operation, as caused by the first cam 32. The curve A thus corresponds to a rolled-up cam profile of the first cam 32. In normal operation, the exhaust valve 20 is opened during the exhaust stroke (push-out stroke) for pushing out exhaust gas through the valve lift area 32B. Otherwise, the exhaust valve 20 remains closed due to the base circle area 32A of the first cam 32.

Eine durchgezogene Kurve B gibt einen Ventilhub des Auslassventils 20 gemäß einem Motorbremsbetrieb an, wie vom zweiten Nocken 34 bewirkt. Die Kurve B entspricht somit einem abgerollten Nockenprofil des zweiten Nockens 34. Im Motorbremsbetrieb wird das Auslassventil 20 zum Ende des Verdichtungstaktes im Bereich des oberen Totpunkts bei rund 60° KW bis 100° KW vor dem oberen Totpunkt durch den ersten Ventilhubbereich 34B leicht geöffnet. Dies ist in Figur 6 jeweils bei rund -225° NW (Nockenwellenwinkel) und bei rund 135° NW dargestellt. Am oberen Totpunkt wird das Auslassventil 20 weiter durch den Ventilhubbereich 34B geöffnet und schließt am Ende des Expansionstaktes ungefähr am unteren Totpunkt. Das Öffnen des Auslassventils 20 zum Ende des Verdichtungstaktes bewirkt, dass die verdichtete Luft im Zylinder durch das geöffneten Auslassventil 20 in das Abgassystem durch den sich zum oberen Totpunkt bewegenden Kolben geschoben wird. Die zuvor verrichtete Verdichtungsarbeit bremst die Kurbelwelle und somit den Verbrennungsmotor. Das offene Auslassventil 20 während des Expansionstaktes bewirkt, dass Luft aus den Abgasleitungen zurück in den Zylinder gesaugt wird. Am Ende des Expansionstaktes ist der Zylinder im Wesentlichen mit Luft aus dem Abgassystem gefüllt.A solid curve B indicates a valve lift of the exhaust valve 20 according to an engine braking operation, as caused by the second cam 34. The curve B thus corresponds to a rolled-up cam profile of the second cam 34. In the engine braking mode, the exhaust valve 20 is slightly opened at the end of the compression stroke in the area of the top dead center at around 60 ° KW to 100 ° KW before the top dead center by the first valve lift area 34B. This is in Figure 6 each shown at around -225 ° NW (camshaft angle) and at around 135 ° NW. At top dead center, exhaust valve 20 is further opened by valve lift region 34B and closes at about bottom dead center at the end of the expansion stroke. Opening the exhaust valve 20 at the end of the compression stroke causes the compressed air in the cylinder to be pushed through the opened exhaust valve 20 into the exhaust system by the piston moving to top dead center. The compression work previously performed brakes the crankshaft and thus the internal combustion engine. The open exhaust valve 20 during the expansion stroke causes air to be drawn back into the cylinder from the exhaust pipes. At the end of the expansion stroke, the cylinder is essentially filled with air from the exhaust system.

Im Motorbremsbetrieb kann das Auslassventil 20 nach Erreichen des unteren Totpunkts am Ende des Expansionstaktes zunächst durch den zweiten Grundkreisbereich 34C geschlossen gehalten werden. Zum Ende des Ausschiebetaktes (Auslasstaktes) öffnet sich das Auslassventil 20 im Bereich des oberen Totpunkts durch den zweiten Ventilhubbereich 34D. Die Öffnung erfolgt wiederum bei rund 60° KW bis 100° KW vor dem oberen Totpunkt. Dies ist in Figur 6 jeweils bei rund -45° NW und bei rund 315° NW dargestellt. Das geschlossene Auslassventil 20 während des ersten Abschnitts des Ausschiebetakts bewirkt, dass die im Expansionstakt angesaugte Luft unter Verrichtung von Arbeit verdichtet wird. Der Zylinderdruck steigt an. Die Verdichtungsarbeit bremst die Kurbelwelle und somit den Verbrennungsmotor. Die Öffnung des Auslassventils 20 zum Ende des Ausschiebetaktes führt dazu, dass die Luft durch das geöffnete Auslassventil 20 in das Abgassystem geschoben wird. Im Ansaugtakt wird der Zylinder wieder mit Luft durch das oder die geöffneten Einlassventile gefüllt. Der Zyklus beginnt erneut.In engine braking operation, the exhaust valve 20 can first be closed by the second base circle region 34C after reaching the bottom dead center at the end of the expansion cycle being held. At the end of the extension stroke (exhaust stroke), the outlet valve 20 opens in the area of the top dead center through the second valve lift area 34D. The opening again takes place at around 60 ° KW to 100 ° KW before top dead center. This is in Figure 6 each shown at around -45 ° NW and at around 315 ° NW. The closed exhaust valve 20 during the first portion of the extension stroke causes the air drawn in the expansion stroke to be compressed while doing work. The cylinder pressure rises. The compression work brakes the crankshaft and thus the internal combustion engine. The opening of the exhaust valve 20 at the end of the push-out cycle results in the air being pushed into the exhaust system through the opened exhaust valve 20. In the intake stroke, the cylinder is filled with air again through the open intake valve or valves. The cycle starts again.

Wie oben stehend erläutert ist, kommt es durch den Einsatz des zweiten Nockens 34 zur Steuerung des Auslassventils 20 zu einer zweifachen Kompression mit anschließender Dekompression, sodass eine Motorbremsfunktionalität gewährleistet wird.As explained above, the use of the second cam 34 to control the exhaust valve 20 results in double compression with subsequent decompression, so that engine brake functionality is guaranteed.

Wie insbesondere der Figur 7 zu entnehmen ist, sind der erste Nocken 32 und der zweite Nocken 34 so aneinander angepasst, dass der Grenzabschnitt 32C des ersten Nockens 32 und der Grenzabschnitt 34E des zweiten Nockens 34 gleich (identisch) ausgebildet sind. Dies ermöglicht, dass eine Axialverschiebung des Nockenträgers 14 nicht nur innerhalb der Grundkreisbereiche 32A, 34A durchführbar ist. Stattdessen kann die Axialverschiebung zusätzlich stattfinden, während der Nockenfolger 16A in Wirkverbindung mit einem der Grenzabschnitte 32C, 34E steht. Damit kann die Axialverschiebung früher beginnen. Dies kann anhand der Kurven C, D und E nachvollzogen werden.Like especially the Figure 7 As can be seen, the first cam 32 and the second cam 34 are matched to one another such that the boundary section 32C of the first cam 32 and the boundary section 34E of the second cam 34 are of identical (identical) design. This enables an axial displacement of the cam carrier 14 not only within the base circle areas 32A, 34A. Instead, the axial displacement can additionally take place while the cam follower 16A is operatively connected to one of the limit sections 32C, 34E. This means that the axial displacement can begin earlier. This can be seen from the curves C, D and E.

Die strichpunktierte Kurve C bezieht sich auf eine Bewegung des bewegbaren Stifts von einem der Aktoren 24 oder 26 bezüglich des Nockenträgers 14. Die gestrichelte Kurve D bezieht sich auf eine Bewegung der jeweiligen Eingriffsspur 42 oder 44 und damit des Nockenträgers 14 entlang der Längsachse der Nockenwelle 12. Die Doppelpunkt-Strich-Kurve E zeigt einen Verlauf einer Tiefenkontur der jeweiligen Eingriffsspur 42 oder 44 (nur in Figur 6 dargestellt). Nachfolgend ist eine axiale Verschiebung des Nockenträgers 14 bei der ersten Axialposition zu der zweiten Axialposition beschrieben. Eine axiale Verschiebung des Nockenträgers 14 von der zweiten Axialposition zu der ersten Axialposition erfolgt analog.The dash-dotted curve C relates to a movement of the movable pin from one of the actuators 24 or 26 with respect to the cam carrier 14. The dashed curve D relates to a movement of the respective engagement track 42 or 44 and thus of the cam carrier 14 along the longitudinal axis of the camshaft 12 The colon-dash curve E shows a course of a depth contour of the respective engagement track 42 or 44 (only in Figure 6 shown). An axial displacement of the cam carrier 14 in the first axial position to the second axial position is described below. Axial displacement of the cam carrier 14 from the second axial position to the first axial position takes place analogously.

Zunächst wird der bewegbare Stift des ersten Aktors 24 in Richtung zu der ersten Eingriffsspur 42 ausgefahren und spurt dabei in die erste Eingriffsspur 42 ein. Das Einspuren wird durch die ausgebildete Tiefenkontur der ersten Eingriffsspur 42 ermöglicht (siehe Kurve E). Nach dem Einspuren kommt es durch eine Querschnittsverengung der ersten Eingriffsspur 42 zu einer Spielreduzierung zwischen dem Stift des ersten Aktors 24 und der ersten Eingriffsspur 24. Die Spielreduzierung findet in einem Bereich S statt (siehe Figur 7). Der Bereich S wird von dem Stift des ersten Aktors 24 erreicht und durchfahren, bevor der Nockenfolger 16A den Grenzabschnitt 32C des ersten Nockens 32 erreicht. Erreicht der Nockenfolger 16A schließlich den Grenzabschnitt 32C des ersten Nockens 32 beginnt in der ersten Eingriffsspur 42 die Spiralform, womit eine Axialverschiebung des Nockenträgers 14 bewirkt wird. Somit kommt es bereits zu einer Verschiebung des Nockenträgers 14 in einem ersten Verschiebebereich V1, während der Nockenfolger 16A in Kontakt mit dem Grenzabschnitt 32C ist. Damit erfolgt ein Beginn der Axialverschiebung des Nockenträgers 14 bevor der Nockenfolger 16A den Grundkreisbereich 32A erreicht. Im Grundkreisbereich 32A, 34A wird die axiale Verschiebung des Nockenfolgers 16A weiter durchgeführt (Verschiebebereich V2) und schließlich beendet, bevor der Nockenfolger 16A den ersten Ventilhubbereich 34B erreicht.First of all, the movable pin of the first actuator 24 is extended in the direction of the first engagement track 42 and thereby tracks into the first engagement track 42. The tracking is done by the trained depth contour of the first engagement track 42 enables (see curve E). After the engagement, a cross-sectional narrowing of the first engagement track 42 leads to a play reduction between the pin of the first actuator 24 and the first engagement track 24. The play reduction takes place in an area S (see Figure 7 ). The area S is reached and traversed by the pin of the first actuator 24 before the cam follower 16A reaches the limit section 32C of the first cam 32. When the cam follower 16A finally reaches the limit section 32C of the first cam 32, the spiral shape begins in the first engagement track 42, which causes an axial displacement of the cam carrier 14. Thus, the cam carrier 14 is already displaced in a first displacement region V1, while the cam follower 16A is in contact with the limit section 32C. This starts the axial displacement of the cam carrier 14 before the cam follower 16A reaches the base circle region 32A. In the base circle region 32A, 34A, the axial displacement of the cam follower 16A is carried out further (displacement region V2) and finally ended before the cam follower 16A reaches the first valve lift region 34B.

Die axiale Verschiebung des Nockenträgers 14 findet somit auch außerhalb der Grundkreisbereiche 32A, 34A in dem Grenzabschnitt 32C des ersten Nockens 32 und dem Grenzabschnitt 34E des zweiten Nockens 34 statt. Dadurch vergrößert sich der Zeitbereich für die axiale Verschiebung des Nockenträgers 14. Aufgrund des vergrößerten Verschiebebereichs können die Beschleunigungen und somit die Massenkräfte bei gleicher Schaltdrehzahl für die axiale Verschiebung des Nockenträgers 14 reduziert werden. Dies kann einerseits genutzt werden, um die Funktionssicherheit und Lebensdauer aufgrund geringerer Kräfte und Pressungen zu erhöhen. Andererseits kann dies genutzt werden, um die maximale Schaltdrehzahl des Systems zu erhöhen.The axial displacement of the cam carrier 14 thus also takes place outside the base circle regions 32A, 34A in the boundary section 32C of the first cam 32 and the boundary section 34E of the second cam 34. This increases the time range for the axial displacement of the cam carrier 14. Because of the increased displacement range, the accelerations and thus the inertial forces can be reduced for the axial displacement of the cam carrier 14 at the same switching speed. On the one hand, this can be used to increase functional reliability and service life due to lower forces and pressures. On the other hand, this can be used to increase the maximum switching speed of the system.

Im dargestellten Beispiel erstreckt sich der zusätzliche Verschiebebereich V1, der durch die gleich ausgebildeten Grenzabschnitte 32C, 34E ermöglicht wird, über ungefähr 22° Nockenwellenwinkel.In the example shown, the additional displacement range V1, which is made possible by the identically configured limit sections 32C, 34E, extends over approximately 22 ° camshaft angles.

Um eine axiale Verschiebung des in den Figuren dargestellten Nockenträgers 14 zu ermöglichen, kann es notwendig sein, den nockenfreien Abschnitt 38, der sowohl als Nullnocken dient als auch mit der zweiten Eingriffsspur 42 versehen ist, mit einem zusätzlichen axialen Toleranzbereich (Freigangbereich) auszuführen. Der benachbarte Nocken 36 ist entsprechend schmaler ausgeführt. Während der axialen Verschiebung innerhalb der Grenzabschnitte 32C, 34E von der zweiten Axialposition zu der ersten Axialposition wird dann der Nockenfolger 18A innerhalb dieses zusätzlichen Toleranzbereichs axial verschoben. So wird eine Kollision des Nockenfolgers 18A mit einem Nockenauslauf des dritten Nockens 36 verhindert.In order to enable an axial displacement of the cam carrier 14 shown in the figures, it may be necessary to design the cam-free section 38, which serves both as a zero cam and is provided with the second engagement track 42, with an additional axial tolerance range (clearance range). The adjacent cam 36 is made correspondingly narrower. Then, during the axial displacement within the boundary portions 32C, 34E from the second axial position to the first axial position, the cam follower 18A axially shifted within this additional tolerance range. A collision of the cam follower 18A with a cam runout of the third cam 36 is prevented.

Fachleute werden indes erkennen, dass das hierin beschriebene Schiebenockensystem nicht auf die hierin beschriebene Anwendung begrenzt ist. Beispielsweise kann alternativ oder zusätzlich zu der gleichen Gestaltung der Ablaufbereiche (Auslaufbereiche) eine gleiche Gestaltung der Anlaufbereiche (Einlaufbereiche) der Nocken zur Verwirklichung der gleich ausgebildeten Grenzabschnitte vorgesehen werden. Es ist auch möglich, die hierin beschriebenen Prinzipien bei variablen Ventiltrieben für Einlassventile eines Verbrennungsmotors zu verwenden. So kann beispielsweise ein Anlaufbereich eines ersten Nockens für einen Normalbetrieb identisch zu einem Anlaufbereich eines zweiten Nockens für einen Millerbetrieb gestaltet und an der gleichen Umfangsposition bezüglich der Längsachse der Nockenwelle positioniert sein. Hervorzuheben ist weiterhin, dass zum Verlängern des Schaltbereichs zum axialen Verschieben des Nockenträgers nicht zwangsläufig die hierin offenbarte der Verschiebevorrichtung (erster Aktor, zweiter Aktor, erste Eingriffsspur, zweite Eingriffsspur) verwendet werden muss. Vielmehr kann beispielsweise ein Verfahren zum Betreiben eines Verbrennungsmotors mit jeglicher Verschiebevorrichtung für den Nockenträger das Verschieben des Nockenträgers, während der Nockenfolger in Kontakt mit dem oder den Grenzbereichen ist, aufweisen. Insbesondere kann eine Axialverschiebung beginnen und/oder enden, wenn der Nockenfolger in Kontakt mit einem Grenzbereich ist.However, those skilled in the art will recognize that the slide cam system described herein is not limited to the application described herein. For example, as an alternative or in addition to the same design of the outlet areas (outlet areas), an identical design of the startup areas (inlet areas) of the cams can be provided in order to implement the boundary sections of the same design. It is also possible to use the principles described herein with variable valve trains for intake valves of an internal combustion engine. For example, a start-up area of a first cam for normal operation can be designed identically to a start-up area of a second cam for mill operation and can be positioned at the same circumferential position with respect to the longitudinal axis of the camshaft. It should also be emphasized that the displacement device (first actuator, second actuator, first engagement track, second engagement track) disclosed here does not necessarily have to be used to extend the switching range for axially displacing the cam carrier. Rather, for example, a method for operating an internal combustion engine with any displacement device for the cam carrier can comprise displacing the cam carrier while the cam follower is in contact with the boundary region or regions. In particular, an axial displacement can begin and / or end when the cam follower is in contact with a limit area.

BezugszeichenlisteReference list

1010th
Variabler VentiltriebVariable valve train
1111
SchiebenockensystemSliding cam system
1212th
Nockenwellecamshaft
1414
NockenträgerCam carrier
1616
Erste Übertragungsvorrichtung (erster Schlepphebel)First transmission device (first rocker arm)
16A16A
NockenfolgerCam follower
1818th
Zweite Übertragungsvorrichtung (zweiter Schlepphebel)Second transmission device (second rocker arm)
18A18A
NockenfolgerCam follower
2020th
Erstes AuslassventilFirst exhaust valve
2222
Zweites AuslassventilSecond exhaust valve
2424th
Erster AktorFirst actuator
2626
Zweiter AktorSecond actuator
2727
SteuereinheitControl unit
2828
Erster AnschlagFirst stop
3030th
Zweiter AnschlagSecond attack
3232
Erster NockenFirst cam
32A32A
GrundkreisbereichBase circle area
32B32B
VentilhubbereichValve lift range
32C32C
Grenzabschnitt des Ventilhubbereichs 32BBoundary portion of the valve lift area 32B
3434
Zweiter NockenSecond cam
34A34A
Erster GrundkreisbereichFirst base circle area
34B34B
Erster VentilhubbereichFirst valve lift range
34C34C
Zweiter GrundkreisbereichSecond base circle area
34D34D
Zweiter VentilhubbereichSecond valve lift range
34E34E
Grenzabschnitt des zweiten Ventilhubbereichs 34DBoundary portion of the second valve lift range 34D
3636
Dritter NockenThird cam
3838
Erster nockenfreier AbschnittFirst cam-free section
4040
Zweiter nockenfreier AbschnittSecond cam-free section
4242
Erste EingriffsspurFirst engagement trace
4444
Zweite EingriffsspurSecond engagement lane
4646
ArretierungsvorrichtungLocking device
4848
Elastisches ElementElastic element
5050
SperrkörperBlocking body
5252
Erste AusnehmungFirst recess
5454
Zweite AusnehmungSecond recess
AA
Ventilsteuerkurve gemäß Nocken 32Valve control curve according to cam 32
BB
Ventilsteuerkurve gemäß Nocken 34Valve control curve according to cam 34
CC.
StiftbewegungPen movement
DD
Eingriffsspur-/NockenträgerbewegungEngagement track / cam carrier movement
EE
Tiefenkontur der EingriffsspurDepth contour of the engagement track
SS
SpielreduzierungsbereichGame reduction area
V1V1
Erster (Axial-) VerschiebebereichFirst (axial) displacement range
V2V2
Zweiter (Axial-) VerschiebebereichSecond (axial) displacement range

Claims (15)

  1. A sliding cam system (11) for a variable valve train (10) of an internal combustion engine of a motor vehicle, in particular a commercial vehicle, comprising:
    a camshaft (12);
    a cam carrier (14) which is arranged on the camshaft (12) fixedly so as to rotate with it and axially displaceably between a first axial position and a second axial position, and comprises a first cam (32), a second cam (34) and a first engagement track (42) for the axial displacement of the cam carrier (14) ;
    a cam follower (16A) which is operatively connected to the first cam (32) in the first axial position of the cam carrier (14) and is operatively connected to the second cam (34) in the second axial position of the cam carrier (14); and
    a first actuator (24) which comprises an element which can be retracted and extended, in particular a pin, for engaging into the first engagement track (42) for the axial displacement of the cam carrier (14) ;
    the first cam (32) and the second cam (34) being arranged offset with respect to one another along a longitudinal axis of the camshaft (12);
    the first cam (32) comprising a base circle region (32A) and a valve lift region (32B) with a limiting section (32C) which adjoins the base circle region (32A) of the first cam (32);
    the second cam (34) comprising a base circle region (34A) and a valve lift region (34D) with a limiting section (34E) which adjoins the base circle region (34A) of the second cam (34);
    the limiting section (32C) of the first cam (32) and the limiting section (34E) of the second cam (34) being of identical configuration and being arranged at an identical circumferential position about the longitudinal axis of the camshaft (12); and
    the first actuator (24), the cam follower (16A) and the first engagement track (42) being arranged and configured in such a way that an axial displacement of the cam carrier (14) can be carried out while the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) and/or the limiting section (34E) of the second cam (34)
    characterized in that
    the first engagement track (42) comprises a cross-sectional constriction for the reduction of the play between the first engagement track (42) and that element of the first actuator (24) which can be retracted and extended during the engagement, which cross-sectional constriction is arranged in such a way that the reduction of the play takes place before the cam follower (16A) passes into an operative connection with the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34).
  2. The sliding cam system (11) according to Claim 1, the first actuator (24), the cam follower (16A) and the first engagement track (42) being arranged and configured in such a way that an axial displacement of the cam carrier (14) begins or ends while the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34).
  3. The sliding cam system (11) according to Claim 1 or Claim 2:
    the limiting section (32C) of the first cam (32) and the limiting section (34E) of the second cam (34) extending over a region of greater than or equal to 1° camshaft angle; and/or
    the limiting section (32C) of the first cam (32) and the limiting section (34E) of the second cam (34) extending over a region of between 5° and 45° camshaft angle, in particular between 15° and 30° camshaft angle.
  4. The sliding cam system (11) according to one of the preceding claims, the limiting section (32C) of the first cam (32) and the limiting section (34E) of the second cam (34) forming a common flat ramp.
  5. The sliding cam system (11) according to one of the preceding claims:
    the limiting section (32C) of the first cam (32) being arranged in a run-out region of the first cam (32) and the limiting section (34E) of the second cam (34) being arranged in a run-out region of the second cam (34); and/or
    the axial displacement of the cam carrier (14) beginning when the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34), and preferably ending while the cam follower (16A) is operatively connected to the base circle region (32A) of the first cam (32) or the base circle region (34A) of the second cam (34).
  6. The sliding cam system (11) according to one of the preceding claims:
    the limiting section (32C) of the first cam (32) being arranged in a run-in region of the first cam (32) and the limiting section (34E) of the second cam (34) being arranged in a run-in region of the second cam (34); and/or
    the axial displacement of the cam carrier (14) ending when the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34), and preferably beginning while the cam follower (16A) is operatively connected to the base circle region (32A) of the first cam (32) or the base circle region (34A) of the second cam (34).
  7. The sliding cam system (11) according to one of the preceding claims, the cam carrier (14) comprising a second engagement track (44) for the axial displacement of the cam carrier (14) in an opposed direction with respect to an axial displacement which is brought about by the first engagement track (42), and the sliding cam system (11) comprising, furthermore:
    a second actuator (26) which comprises an element which can be retracted and extended, in particular a pin, for engaging into the second engagement track (44) for the axial displacement of the cam carrier (14) ;
    the second actuator (26), the cam follower (16A) and the second engagement track (44) being arranged and configured in such a way that an axial displacement of the cam carrier (14) can be carried out while the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34).
  8. The sliding cam system (11) according to Claim 7:
    the second engagement track (44) comprising a cross-sectional constriction for the reduction of the play between the second engagement track (44) and that element of the second actuator (26) which can be retracted and extended during the engagement, which cross-sectional constriction is arranged in such a way that the reduction of the play takes place before the cam follower (16A) passes into an operative connection with the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34).
  9. The sliding cam system (11) according to one of the preceding claims:
    the first engagement track (42) and/or the second engagement track (44) extending spirally about the longitudinal axis of the camshaft (12); and/or
    it being possible for that element of the first actuator (24) and/or the second actuator (26) which can be retracted and extended to be moved radially with regard to the longitudinal axis of the camshaft (12) .
  10. A variable valve train (10) for an internal combustion engine, having:
    a sliding cam system (11) according to one of the preceding claims; and
    a gas exchange valve (20), in particular an inlet valve or an outlet valve, which is operatively connected to the cam follower (16A),
    the first cam (32) and the second cam (34) bringing about different valve lifts, opening times and/or closing times of the gas exchange valve (20).
  11. The variable valve train (10) according to Claim 10:
    the gas exchange valve (20) being an outlet valve;
    the first cam (32) being configured for a normal operation mode of the internal combustion engine, in the case of which the first cam (32) holds the outlet valve open in the exhaust stroke; and
    the second cam (34) being configured for an engine braking operation mode of the internal combustion engine, in the case of which the outlet valve is first of all held closed in the compression stroke and in the exhaust stroke, and is opened before a top dead centre of a piston movement is reached.
  12. The variable valve train (10) according to Claim 10 or Claim 11, the second cam (34) being configured in such a way that:
    the outlet valve opens between 100° crank angle and 60° crank angle before the top dead centre is reached; and/or,
    after opening in the exhaust stroke, the outlet valve closes in the region between the top dead centre and 30° crank angle after the top dead centre; and/or,
    after opening in the compression stroke, the outlet valve closes in the region between the bottom dead centre and 30° crank angle after the bottom dead centre.
  13. A motor vehicle, in particular a commercial vehicle, comprising the variable valve train (10) according to one of Claims 10 to 12 or the sliding cam system (11) according to one of Claims 1 to 9.
  14. A method for operating an internal combustion engine having a sliding cam system (11) according to one of Claims 1 to 9, the method comprising:
    axial displacement of the cam carrier (14), the axial displacement of the cam carrier (14) being carried out, in particular beginning or ending, while the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) and/or the limiting section (34E) of the second cam (34).
  15. The method according to Claim 14:
    the axial displacement of the cam carrier (14) beginning while the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34), and/or ending while the cam follower (16A) is operatively connected to the base circle region (32A) of the first cam (32) or the base circle region (34A) of the second cam (34); and/or
    the axial displacement of the cam carrier (14) beginning while the cam follower (16A) is operatively connected to the base circle region (32A) of the first cam (32) or the base circle region (34A) of the second cam (34), and/or ending while the cam follower (16A) is operatively connected to the limiting section (32C) of the first cam (32) or the limiting section (34E) of the second cam (34) .
EP18181183.7A 2017-07-27 2018-07-02 Sliding cam system and method for operating a combustion engine Active EP3441581B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102017116987.3A DE102017116987A1 (en) 2017-07-27 2017-07-27 Sliding cam system and method for operating an internal combustion engine

Publications (2)

Publication Number Publication Date
EP3441581A1 EP3441581A1 (en) 2019-02-13
EP3441581B1 true EP3441581B1 (en) 2020-04-22

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EP18181183.7A Active EP3441581B1 (en) 2017-07-27 2018-07-02 Sliding cam system and method for operating a combustion engine

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US (1) US10612434B2 (en)
EP (1) EP3441581B1 (en)
CN (1) CN109306881B (en)
BR (1) BR102018014697B1 (en)
DE (1) DE102017116987A1 (en)
RU (1) RU2770348C2 (en)

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KR102439627B1 (en) * 2017-12-12 2022-09-05 현대자동차주식회사 Variable valve device for engine
DE102019133590A1 (en) * 2019-12-09 2021-06-10 Bayerische Motoren Werke Aktiengesellschaft Lift actuator for a variable lift valve train with two working positions

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DE102008060167B4 (en) * 2008-11-27 2021-05-27 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Valve train of an internal combustion engine
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CN109306881A (en) 2019-02-05
BR102018014697A2 (en) 2019-03-26
RU2018127535A3 (en) 2021-11-30
RU2770348C2 (en) 2022-04-15
US20190032524A1 (en) 2019-01-31
DE102017116987A1 (en) 2019-01-31
BR102018014697B1 (en) 2023-04-18
US10612434B2 (en) 2020-04-07
RU2018127535A (en) 2020-01-27
EP3441581A1 (en) 2019-02-13
CN109306881B (en) 2021-12-28

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