EP2041402A1 - Dispositif destiné à régler de manière variable les temps de commande des soupapes d'échanges des gaz d'un moteur à combustion interne - Google Patents

Dispositif destiné à régler de manière variable les temps de commande des soupapes d'échanges des gaz d'un moteur à combustion interne

Info

Publication number
EP2041402A1
EP2041402A1 EP07765536A EP07765536A EP2041402A1 EP 2041402 A1 EP2041402 A1 EP 2041402A1 EP 07765536 A EP07765536 A EP 07765536A EP 07765536 A EP07765536 A EP 07765536A EP 2041402 A1 EP2041402 A1 EP 2041402A1
Authority
EP
European Patent Office
Prior art keywords
pressure
pressure medium
rotor
angle limiting
control
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.)
Granted
Application number
EP07765536A
Other languages
German (de)
English (en)
Other versions
EP2041402B1 (fr
Inventor
Andreas Strauss
Michael Busse
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.)
Schaeffler Technologies AG and Co KG
Original Assignee
Schaeffler KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Schaeffler KG filed Critical Schaeffler KG
Publication of EP2041402A1 publication Critical patent/EP2041402A1/fr
Application granted granted Critical
Publication of EP2041402B1 publication Critical patent/EP2041402B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/34—Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • F01L1/344—Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear
    • F01L1/3442—Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear using hydraulic chambers with variable volume to transmit the rotating force
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/34—Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • F01L1/344—Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear
    • F01L1/3442—Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear using hydraulic chambers with variable volume to transmit the rotating force
    • F01L2001/34423—Details relating to the hydraulic feeding circuit
    • F01L2001/34426—Oil control valves

Definitions

  • the invention relates to a device for variably setting the timing of gas exchange valves of an internal combustion engine having an outer rotor and a rotatable inner rotor relative thereto, wherein one of the components in drive connection with the crankshaft and the other component is in driving connection with a camshaft, wherein at least one pressure chamber provided and each pressure chamber is divided into two oppositely acting pressure chambers, wherein one of the pressure chambers of each pressure chamber acts as Voreil- and the other pressure chamber as a retardation chamber, wherein by pressure medium supply to the Voreilhuntn, at the same pressure medium outflow of the retard chambers, the rotor cooperating with the camshaft relative is rotated to the cooperating with the crankshaft rotor in the direction of a maximum early position, wherein by pressure medium supply to the lag chambers, with simultaneous pressure medium discharge from the advance chambers, with the camshaft cooperating rotor relative to the cooperating with the crankshaft rotor is rotated in the direction of a maximum late position, wherein at
  • the device In modern internal combustion engines devices for variable adjustment of the timing of gas exchange valves are used to make the phase relation between the crankshaft and camshaft in a defined angular range, between a maximum early and a maximum late position variable.
  • the device is integrated in a drive train, via which torque is transmitted from the crankshaft to the camshaft.
  • This drive train can be realized for example as a belt, chain or gear drive.
  • the device comprises at least two rotors rotatable relative to one another, one rotor being in driving connection with the crankshaft and the other rotor being connected in a rotationally fixed manner to the camshaft.
  • the device comprises at least one pressure chamber, which is subdivided by means of a movable element into two counteracting pressure chambers.
  • the movable element is in operative connection with at least one of the rotors.
  • the pressure medium inflow to, or the pressure drain from the pressure chambers is controlled by means of a control unit, usually a hydraulic directional control valve (control valve).
  • the control unit is controlled by means of a regulator which, with the aid of sensors, determines the actual and desired position of the camshaft in the internal combustion engine and compares them with one another. If a difference is detected between the two positions, a signal is sent to the control unit which adapts the pressure medium flows to the pressure chambers to this signal.
  • the pressure in the pressure medium circuit of the internal combustion engine must exceed a certain value.
  • the pressure medium is usually provided by the oil pump of the internal combustion engine and the pressure provided thus increases synchronously with the speed of the internal combustion engine, below a certain speed of the oil pressure is still too low to change the phase position of the rotors targeted or keep. This may for example be the case during the starting phase of the internal combustion engine or during idling phases. During these phases, the device would make uncontrolled oscillations, resulting in increased noise emissions, increased wear, choppy running, and increased raw engine emissions.
  • mechanical locking devices can be provided which, during the critical operating phases of the internal combustion engine, couple the two rotors in a torque-proof manner with one another, wherein this coupling can be canceled by pressurizing the locking device. It has been found to be advantageous for the locking position to select a phase angle of the camshaft relative to the crankshaft, which is between the maximum early position and the maximum late position.
  • Such a device is known for example from US 2003/0121486 A1.
  • the device is designed in a rotary piston type, wherein an outer rotor is rotatably mounted on an inner rotor designed as an impeller.
  • two Drehwinkelbegrenzungsvor- directions provided, wherein a first rotation angle limiting device in the locked state allows an adjustment of the inner rotor to the outer rotor in an interval between a maximum late position and a defined center position (locking position).
  • the second rotational angle limiting device permits a rotation of the inner rotor to the outer rotor in an interval between the center position and the maximum early position.
  • Each of the rotational angle limiting devices consists of a spring-loaded locking pin, which is arranged in a receptacle of the outer rotor. Each locking pin is acted upon by a spring in the direction of the inner rotor with a force. On the inner rotor, a locking groove is formed, which faces the locking pins in certain operating positions of the devices. In these operating positions, the pins can engage in the locking groove. In this case, the respective rotation angle limiting device changes from the unlocked state.
  • Each of the rotation angle limiting devices can be transferred from the locked to the unlocked state by pressurizing the locking groove.
  • the pressure medium urges the locking pins back into their receptacle, whereby the mechanical coupling of the inner rotor to the outer rotor is canceled.
  • pressure medium is provided to one of the chambers and thus to ensure a sufficient supply of lubricant.
  • the inner rotor is hydraulically biased against the outer rotor. This can lead to jamming one of the locking pins on the edges of the locking groove, whereby a hydraulic unlocking difficult or possibly even prevented.
  • the invention has for its object to provide a device for variable adjustment of the timing of gas exchange valves of an internal combustion engine, wherein the inner rotor can be mechanically locked relative to the outer rotor in a central phase between the maximum early and the maximum late position.
  • the object is achieved in that the Verrieglungszu- state of the first rotation angle limiting device is controlled solely by the pressure prevailing in at least one of the pressure chambers and that the locking state of the second rotation angle limiting device is controlled by a separate control line, wherein the control line neither with the pressure medium channels the pressure chambers communicates.
  • the first rotational angle limiting device communicates via a connecting line with at least one of the pressure chambers or with one of the pressure medium channels.
  • the inner rotor is advantageously fixed in a locking position relative to the outer rotor.
  • the second rotational angle limiting device can restrict a phase angle of the rotor cooperating with the camshaft relative to the rotor interacting with the crankshaft to an angular range between the maximum early position and the droop position.
  • the first rotation angle limiting device in the locked state prevents the rotation of the cooperating with the Nockenwel- Ie rotor relative to the cooperating with the crankshaft rotor when taking the locking position in the direction of the maximum early position.
  • the first rotational angle limiting device in the locked state limits the phase position of the rotor cooperating with the camshaft relative to the rotor interacting with the crankshaft to an angular range between the maximum retarded position and the locked position.
  • a control valve is provided which controls the pressure medium supply to and the pressure medium discharge from the pressure medium channels and the control line.
  • control valve has two working ports, wherein the first working port communicates with the first pressure chambers and the second working port communicates with the second pressure chambers, and wherein the control line communicates on the valve side exclusively with a control port formed separately from the working ports.
  • a locking device is provided by means of which the outer rotor with the inner rotor in a locking position between a maximum early and a maximum late position is mechanically coupled.
  • two rotational angle limiting devices can be provided, wherein one of the rotational angle limiting devices in the locked state limits the relative phase position of the inner rotor to the outer rotor to a region between the maximum early and the locking position.
  • the other rotational angle limiting device allows a phase position between the locking and the maximum retarded position in the locked state.
  • this may be embodied as a locking element, wherein a locking pin of the locking element engages in the locking position in a recess adapted to the locking pin or a blind hole. This ensures that the inner rotor can be mechanically fixed relative to the outer rotor in a middle phase position.
  • Each of the rotation angle limiting devices can be transferred by pressure medium from the locked to the unlocked state.
  • the control line is separate from the Pressure medium lines and the pressure medium channels executed, which supply the pressure chambers with pressure medium.
  • one of the rotation angle limiting devices is supplied with pressure medium via at least one of the pressure chambers, the number of control positions which have to be provided on the control valve can be reduced to a minimum.
  • the number of switching points to be determined decreases, whereby the control effort during operation of the internal combustion engine drops significantly.
  • the ranges of the individual control positions of the control valve designed as a proportional valve can be increased, which in turn reduces the control effort and increases the reliability.
  • the device during the shutdown in a defined interval, which includes the Verrieglungsposition turn off.
  • the inner rotor automatically enters the locking position, wherein the mechanical connection between the rotors is produced by means of the rotation angle limiting devices.
  • both rotational angle limiting devices can be connected to the tank during the starting phase, wherein a pressure medium channel communicates neither with the tank nor with the pump.
  • an automatic unlocking of the device can be prevented.
  • the leakage oil entering via the control valve into the pressure medium lines can be sucked in by a small oscillating movement of the inner rotor relative to the outer rotor, thereby ensuring adequate supply of the device with lubricant even during the starting phase.
  • the low oscillatory movement of the inner rotor to the outer rotor results from the acting on the camshaft alternating torques in combination with a low locking clearance of the rotation angle limiting devices.
  • FIG. 1 shows very schematically an internal combustion engine
  • FIG. 2a shows a cross section through an embodiment according to the invention of a device for changing the timing of gas exchange valves of an internal combustion engine incl.
  • a connected hydraulic circuit
  • FIG. 2b shows a longitudinal section through the device from FIG. 2a along the line IIb-IIb, FIG.
  • FIG. 2c shows a cross section through the device from FIG. 2b along the line I-Ic
  • FIG. 3 shows a first control logic of a control valve of the invention
  • FIG. 4 shows a second control logic of a control valve of the device according to the invention
  • FIG. 5 is a perspective view of a control valve for the control valve for controlling the device according to the invention.
  • FIG. 6 shows a partial longitudinal section through the control valve from FIG. 5,
  • Figure 6a-6g shows a longitudinal section through the essential parts of the control valve of Figure 6 in its various control positions.
  • crankshaft 2 is in the illustrated embodiment via a respective traction drive 5 with an intake camshaft 6 and exhaust camshaft 7 in combination, with a first and a second device 10 for a relative rotation between the crankshaft 2 and the camshafts 6, 7 can provide.
  • Cams 8 of the camshafts 6, 7 actuate one or more intake gas exchange valves 9a or one or more exhaust gas exchange valves 9b.
  • it may be provided to equip only one of the camshafts 6, 7 with a device 10, or to provide only one camshaft 6, 7, which is provided with a device 10.
  • FIGS 2a and 2b show an embodiment of a device 10 according to the invention in transverse or in longitudinal section.
  • the device 10 has an outer rotor 22, an inner rotor 23 and two side covers 24, 25.
  • the inner rotor 23 is designed in the form of an impeller and has a substantially cylindrically designed hub member 26, extend from the outer cylindrical surface in the illustrated embodiment, five wings 27 in the radial direction outwards. In this case, the wings 27 may be integrally formed with the hub member 26.
  • a plurality of projections 30 extend radially inwardly.
  • the projections 30 are integrally formed with the peripheral wall 29.
  • the outer rotor 22 is mounted by means of radially inner circumferential walls of the projections 30 relative to the inner rotor 23 rotatably mounted on this.
  • a sprocket 21 is arranged, by means of which, via a chain drive, not shown, torque can be transmitted from the crankshaft 2 to the outer rotor 22.
  • the sprocket 21 may be formed as a separate component and rotatably connected to the inner rotor 23 or formed integrally therewith. Alternatively, a belt or gear drive can be provided.
  • Each of the side covers 24, 25 is arranged on one of the axial side surfaces of the outer rotor 22 and fixed in a rotationally fixed manner thereto.
  • an axial opening 31 is provided for this purpose, wherein each axial opening 31 is penetrated by a fastening element 32, for example a bolt or a screw, which serves for the rotationally fixed fixing of the side cover 24, 25 on the outer rotor 22.
  • a pressure space 33 is formed, which in the circumferential direction of opposite, substantially radially extending boundary walls 34 adjacent projections 30, in the axial direction of the side covers 24, 25, radially inwardly of the hub member 26 and radially outwardly bounded by the peripheral wall 29.
  • each of the pressure chambers 33 projects a wing 27, wherein the wings 27 are formed such that they abut both on the side walls 24, 25, and on the peripheral wall 29.
  • Each wing 27 thus divides the respective pressure chamber 33 into two oppositely acting pressure chambers 35, 36.
  • the outer rotor 22 is rotatably arranged in a defined Winkeibreich to the inner rotor 23.
  • the angular range is limited in a rotational direction of the outer rotor 22 in that each wing 27 at one as early stop 34 a trained boundary wall 34 of the pressure chamber 33 comes to rest.
  • the angular range in the other direction of rotation is limited by the fact that each wing 27 comes to rest on the other boundary wall 34 of the pressure chamber 33, which serves as a late stop 34b.
  • a rotation limiting device may be provided which limits the rotation angle range of the outer rotor 22 to the inner rotor 23.
  • the phase angle of the outer rotor 22 to the inner rotor 23 can be varied.
  • the phase position of the two rotors 22, 23 are kept constant to each other.
  • it can be provided to pressurize none of the pressure chambers 35, 36 during phases of constant phase position with pressure medium.
  • hydraulic pressure medium usually the lubricating oil of the internal combustion engine 1 is used.
  • a pressure medium system For pressure medium supply to or pressure medium removal from the pressure chambers 35, 36, a pressure medium system is provided which comprises a pressure medium pump, not shown, a likewise not shown tank, a control valve 37 and a plurality of pressure medium lines 38a, 38b, 38p. Pressure medium conveyed by the pressure medium pump is supplied to the control valve 38 via the third pressure medium line 38p. Depending on the control state of the control valve 37, the third pressure medium line 38p is connected to the first pressure medium line 38a, the second pressure medium line 38b or to both or none of the pressure medium lines 38a, 38b.
  • the inner rotor 23 is formed with two groups of pressure medium channels 39a, 39b, wherein each pressure medium channel 39a, 39b extends from an inner circumferential surface of a receptacle 40 of the inner rotor 23 to one of the pressure chambers 35, 36.
  • the first pressure medium line 38a communicates with the first pressure medium channels 39a.
  • the second pressure medium line 38b communicates with the second pressure medium channels 39b.
  • a pressure medium distributor may be provided, which is arranged in the receptacle 40.
  • the control valve 37 is formed as a central valve and arranged in the receptacle 40, in which case the Control valve 37, the third pressure medium line 38p connects directly to the pressure medium channels 39a, 39b.
  • the pressure medium supplied to the control valve 37 via the third pressure medium line 38p via the first pressure medium channels 39a and optionally the first pressure medium line 38a to the group of the first pressure chambers 35th directed.
  • pressure medium from the group of second pressure chambers 36 reaches the control valve 37 via the second pressure medium channels 39b and optionally the second pressure medium line 38b and is ejected into the tank.
  • the wings 27 are displaced in the direction of the early stop 34a, whereby a rotary movement of the inner rotor 23 to the outer rotor 22 in the direction of rotation of the device 10 is achieved.
  • the pressure medium supplied to the control valve 37 via the third pressure medium line 38p is conducted via the second pressure medium channels 39b and possibly the second pressure medium line 38b to the group of the second pressure chambers 36.
  • pressure medium from the group of the first pressure chambers 35 reaches the control valve 37 via the first pressure medium channels 39a and optionally the first pressure medium line 38a and is ejected into the tank.
  • the wings 27 are displaced in the direction of the late stop 34a, whereby a rotary movement of the inner rotor 23 to the outer rotor 22 opposite to the direction of rotation of the device 10 is achieved.
  • the pressure medium supply to all pressure chambers 35, 36 is either prevented or permitted.
  • the wings 27 are hydraulically clamped within the respective pressure chambers 33, and thus prevents a rotational movement of the inner rotor 23 to the outer rotor 22.
  • a locking mechanism 41 is provided which establishes a mechanical connection between the two rotors 22, 23.
  • a locking pin is arranged in one of the rotors 22, 23, while in the other rotor 22, 23 a link is formed. If the inner rotor 23 is in a defined phase position (locking position) relative to the outer rotor 22, then the locking pin can engage in the connecting link and thus produce a mechanical rotationally fixed connection between the two rotors 22, 23.
  • FIG. 2c This consists of a first and a second rotational angle limiting device 42, 43.
  • each of the rotational angle limiting devices 42, 43 consists of an axially displaceable locking pin 44, wherein each of the locking pins 44 is received in a bore of the inner rotor 23.
  • 24 two scenes 45 are formed in the form of circumferentially extending grooves in the first side wall. These are indicated in Figure 2c in the form of broken lines.
  • Each of the locking pins 44 is acted upon by means of a spring element 46 with a force in the direction of the first side cover 24. If the inner rotor 23 to the outer rotor 22 assumes a position in which a locking pin 44 faces in the axial direction of the associated link 45, this is forced into the link 45 and the respective rotational angle limiting device 42, 43 transferred from an unlocked to a locked state.
  • the link 45 of the first rotational angle limiting device 42 is designed such that the phase position of the inner rotor 23 is limited to the outer rotor 22, with locked first rotational angle limiting device 42, on a range between a maximum late and the locking position.
  • the gate 45 of the second rotational angle limiting device 43 is designed such that when locked second Drehwinkelbegrenzungsvor- direction 43, the phase angle of the inner rotor 23 to the outer rotor 22 is limited to a range between a maximum advanced position and the locking position.
  • the respective link 45 is subjected to pressure medium.
  • the respective locking pin 44 is pushed back against the force of the spring element 46 into the bore and thus eliminates the rotation angle limitation.
  • the backdrop 45 of the first rotation angle limiting device 42 which prevents the rotation of the inner rotor 23 to the outer rotor 22 at the locking position in the direction of early in the locked state via one of the first pressure chambers 35 and a connecting line 47 with pressure medium.
  • the link 45 of the second rotational angle limiting device 43 can be acted upon by the pressure medium via the control line 48 and the channel 49.
  • the control valve 37 controls both the pressure medium flows to and from the first and second pressure chambers 35, 36, as well as to and from the control line 48.
  • the control valve 37 consists of an actuating unit 50 and a hydraulic section 51.
  • the hydraulic section 51 consists of a valve housing 52 of an intermediate sleeve 53 and a control piston 54.
  • On the valve housing 52 is a first working port A, a second working port B, an inlet port P, a control port S, an axial and a radial drain port T formed.
  • the first working port A communicates with the first pressure medium line 38a.
  • the second working port B communicates with the second pressure medium line 38b.
  • the inlet connection P communicates with the third pressure medium line 38p.
  • the control terminal S communicates with the control line 48.
  • About the drain connections T can flow off pressure medium into a tank (not shown).
  • the intermediate sleeve 53 is disposed within the valve housing 52, fixed thereto.
  • a control groove 57 On the outer circumferential surface of a working groove 56, a control groove 57, five working openings 56a-e and three control openings 57a-c are formed.
  • the working groove 56 and the control groove 57 extend in the circumferential direction of the intermediate sleeve 53 in each case in a defined angular interval, wherein the two grooves 56, 57 are hydraulically separated from each other.
  • the working connections A, B and the inlet connection P are formed as radial openings in the valve housing 52, wherein the radial openings are formed exclusively in the region of the angular segment occupied by the working groove 56.
  • the control connection S is realized by means of one or more radial openings, which are formed exclusively in the region of the angular segment taken by the control groove 57.
  • the working opening 56a-e communicate on the one hand with the interior of the intermediate sleeve 53 and on the other hand with the first working port A (first working opening 56a), the inflow port P (second working port 56b), the working groove 56 (third and fourth working port 56c, d) and radial tank connection T (fifth working opening 56e).
  • the working groove 56 additionally communicates with the second working connection B.
  • the control openings 57a-c communicate on the one hand with the inner of the intermediate sleeve 53 and on the other hand with the control groove 57, which in turn communicates with the control port S.
  • the control piston 54 is designed substantially hollow cylindrical and disposed within the intermediate sleeve 53, wherein this is displaceable by the actuator 50 against the force of a spring 55 in the axial direction relative to the intermediate sleeve 53 and the valve housing 52.
  • the control piston 54 has three annular grooves 58a-c, first and second openings 59a, b.
  • the actuating unit 50 may be formed, for example, as an electrical actuating unit, wherein a magnetized armature is arranged within a coil. By energizing the coil, the armature can be moved within in the axial direction. About a push rod 50 a, this movement can be transmitted to the control piston 54.
  • the working ports A, B and the control port S can be selectively connected to the inlet port P, the drain port T or neither.
  • FIG. 3 shows a control logic of the control valve 37 shown in FIG. 5 or FIG. 6.
  • the connections of the first working connection A, of the second working connection B and of the control connection S with the pressure medium pump or the tank are shown as a function of the excitation of the actuating unit 50 or the axial deflection D of the control piston 54 within the intermediate sleeve 53.
  • the control logic can be subdivided into seven control positions. With increasing excitation of the actuating unit 50 (axial displacement of the control piston 54), the control valve 37 passes through the control positions in the order start position S1, unlock position S2, retard position, S3, first intermediate position S4, stop position S5, second intermediate position S6 and advance position S7.
  • the positions of the control piston 54 relative to the valve housing 52 and the intermediate sleeve 53 in the various control positions S1 -S7 are shown in FIGS. 6a-g.
  • the control port S (via the second working opening 56b, the first annular groove 58a, the first opening 59a, the interior of the control piston 54, the second opening 59b, the third annular groove 58c , the second control port 57b and the control groove 57) are connected to the pump.
  • the first working port A further communicates with the axial discharge port T, while the second working port B is still closed (analogous to Figure 6a).
  • the first working port A (via the second working port 56b, the first annular groove 58a and the first working port 56a) is connected to the inflow port P, while the second working port B and the control port S are closed (analogously FIG. 6e).
  • the second working port B and the control port S are connected to the radial discharge port T and the first working port A connected to the inlet port P (analogous to Figure 6f).
  • the control valve 37 is in the starting position S1. In this phase, the hydraulic clamping of the wings 27 is not guaranteed within the pressure chambers 33 due to low system pressure in general. For this reason, the inner rotor 23 will perform oscillatory movements in the circumferential direction relative to the outer rotor 22.
  • oscillations are caused by the alternating torques acting on the camshaft 6, 7, the oscillations occurring even in the locked state of the device 10. Their amplitude is determined by the locking game.
  • the oscillations result in a pumping action whereby residual oil present in the pressure medium channels 39a, b or the pressure medium lines 38a, b can be conveyed into the pressure chambers 35, 36.
  • pressure values can be achieved which are sufficient to convert the rotational angle limiting devices 42, 43 into the unlocked state. By connecting the first working port A and the control port S to the tank this is prevented.
  • the first pressure chambers 35, the corresponding pressure medium channels 39a, the first pressure medium line 38a and the control line 48 are emptied and thus a pressure build-up, and thus the unwanted Disentriegelung during the start phase, in the scenes 45 of the rotation angle limiting devices 42, 43 prevented.
  • the second pressure chambers 36 are not acted upon by pressure medium. This prevents the locking pin 44 of the second rotational angle limiting device 43 from being forced against the end of the link 45, which could lead to jamming. On the other hand, it is prevented that the pressure medium in the second pressure medium channels 39b can flow to the tank. This ensures that 27 small amounts of pressure medium are promoted by the oscillations of the wings in the second pressure chambers 36, whereby the device 10 is sufficiently supplied with lubricant.
  • the device 10 At the end of a defined period of time after which the starting process has ended completely or when a sufficient pressure level in the lubricant circuit is reached. run of the internal combustion engine 1 is detected, and the engine control specifies a phase change, the device 10 is in a controlled state until the pressure in the lubricant circuit falls again below a predetermined level.
  • the actuating unit 50 of the control valve 37 is energized such that it passes through the Enthegel ein S2 in the control positions S3 to S7 and is controlled depending on the specification of the phase angle by the engine control in one of these control positions S3-S7.
  • the control valve 37 assumes the control positions S3-S7 in the regulated state of the device 10. If the engine control unit specifies a shift in the phase position in the direction of later intake times, the control valve 37 is energized in such a way that it assumes the retard position S3. In this position, the first pressure chambers 35 are connected to the tank and the second pressure chambers 36 are connected to the pump. At the same time pressure medium is directed to the backdrop 45 of the second rotation angle limiting device 43.
  • the locking pin 44 of the second rotation angle limiting device 43 is held in the unlocked state, while the pressure medium is applied to the second pressure chambers 36 with simultaneous emptying of the first pressure chambers 35 to a rotation of the inner rotor 23 relative to the outer rotor 22 against the direction of rotation of the device 10 leads.
  • the control valve 37 is transferred to the holding position S5. In this position, no pressure medium exchange between the pressure chambers 35, 36 and the backdrop 45 of the second rotation angle limiting device 43 with the tank or the pressure medium pump instead.
  • the wings 27 are hydraulically in the pressure chamber 33rd clamped and the Drehwinkelbegrenzungsvorhchtitch 42, 43 held in the unlocked position.
  • control valve 37 is brought into the advance position S7. In this control position becomes the first
  • Pressure chambers 35 supplied pressure medium, while both the backdrop 45 of the second rotation angle limiting device 43 and the second
  • Pressure chambers 36 pressure medium is discharged to the tank.
  • Rotation angle limiting device 43 engage in the corresponding link 45 when they face each other.
  • one group of the pressure chamber 35, 36 is acted upon by pressure medium, while no pressure medium exchange takes place between the other group of pressure chambers 35, 36 and the pump and the tank. It is thereby achieved that the hydraulic clamping of the vanes 27 within the pressure chambers 33 is maintained during the taking of the holding position S5 or its leaving.
  • the control valve 37 is transferred to the advance position S7 and kept a defined period beyond their standstill in this.
  • pressure medium is conducted to the first pressure chambers 35, while pressure medium from the second pressure chambers 36 can flow to the tank.
  • This causes a relative rotation of the inner rotor 23 to the outer rotor 22, wherein the inner rotor 23 comes to a position between the locking position and the maximum early position.
  • the control port S and thus the gate 45 of the second rotation angle limiting device 43 are connected to the tank, whereby the second rotation angle limiting device 43 is transferred to the locked state. This ensures that the inner rotor 23 during the entire stop and the pause in operation of the internal combustion engine 1 in a position ment adjusted between the locking position and the maximum early position and then held in this.
  • the inner rotor 23 is rotated, due to the drag torques acting on the camshaft 6, 7, relative to the outer rotor 22 in the direction of the maximum retarded position.
  • This movement is stopped by the locked second rotation angle limiting device 43 at the locking position.
  • the first rotation angle limiting device 42 is also in this locked position in the locked state, whereby a mechanical fixing of the inner rotor 22 is made relative to the outer rotor 23 in the locking position.
  • this process can take place during the starting phase of the internal combustion engine 1, in which the control valve 37 assumes the starting position S1.
  • control states S3-S7 it is ensured on the basis of the control logic illustrated in FIG. 3 that when a group of pressure chambers 35, 36 is actuated, the associated rotation angle limiting device 42, 43 is in the unlocked state. Thus, a secure adjustment of the device 10 over the locking position is guaranteed.
  • FIG. 4 shows an alternative control logic to the control logic shown in FIG. 3, the only difference being that the sequence of the control positions S1-S7 are reversed.
  • the starting position S1 is taken in this embodiment at maximum energized actuator 50, while the advance position S7 is taken at non-energized actuator 50.
  • valve housing 53 intermediate sleeve
  • control groove 57 control groove 57 a first control opening

Landscapes

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

Abstract

L'invention concerne un dispositif (10) destiné à régler de manière variable les temps de commande de soupapes d'échange des gaz (9a, 9b) d'un moteur à combustion interne, comprenant un rotor externe (22) et un rotor interne, disposé de manière à pouvoir tourner par rapport au rotor externe. Un des composants est relié de manière commandée à l'arbre-manivelle (2) et l'autre composant est relié de manière commandée à l'arbre à cames (6, 7). Au moins une chambre de pression (33) est utilisée et chaque chambre de pression (33) est divisée en deux chambres (35, 36) de pression antagonistes. Une des chambres de pression (35, 36) agit comme une chambre en avance de phase et l'autre chambre de pression (35, 36) agit comme une chambre en retard de phase. Au moins deux dispositifs (42, 43) de limitation de l'angle de rotation sont utilisés, chacun pouvant passer d'une position débloquée à une position bloquée. La position bloquée peut être réglée grâce à l'ajout ou à la suppresion d'un fluide sous pression vers les dispositifs et à partir des dispositifs (42, 43) de limitation de l'angle de rotation.
EP07765536A 2006-07-08 2007-06-21 Dispositif destiné à régler de manière variable les temps de commande des soupapes d'échanges des gaz d'un moteur à combustion interne Active EP2041402B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006031593A DE102006031593A1 (de) 2006-07-08 2006-07-08 Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
PCT/EP2007/056190 WO2008006684A1 (fr) 2006-07-08 2007-06-21 Dispositif destiné à régler de manière variable les temps de commande des soupapes d'échanges des gaz d'un moteur à combustion interne

Publications (2)

Publication Number Publication Date
EP2041402A1 true EP2041402A1 (fr) 2009-04-01
EP2041402B1 EP2041402B1 (fr) 2010-01-20

Family

ID=38657971

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07765536A Active EP2041402B1 (fr) 2006-07-08 2007-06-21 Dispositif destiné à régler de manière variable les temps de commande des soupapes d'échanges des gaz d'un moteur à combustion interne

Country Status (5)

Country Link
US (1) US8006660B2 (fr)
EP (1) EP2041402B1 (fr)
JP (1) JP5082164B2 (fr)
DE (2) DE102006031593A1 (fr)
WO (1) WO2008006684A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007058491A1 (de) * 2007-12-05 2009-06-10 Schaeffler Kg Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
JP2010127252A (ja) * 2008-11-28 2010-06-10 Toyota Motor Corp 内燃機関の可変動弁装置
DE102009037976A1 (de) 2009-08-18 2011-02-24 Schaeffler Technologies Gmbh & Co. Kg Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
US8662039B2 (en) * 2011-03-16 2014-03-04 Delphi Technologies, Inc. Camshaft phaser with coaxial control valves
DE102013203244A1 (de) * 2013-02-27 2014-08-28 Schaeffler Technologies Gmbh & Co. Kg Nockenwellenversteller
US8893677B2 (en) 2013-03-14 2014-11-25 Borgwarner Inc. Dual lock pin phaser
DE112014002471B4 (de) 2013-06-19 2017-01-19 Borgwarner Inc. Variabler Nockenwellenverstellmechanismus mit durch Öldruck eingerücktem Verriegelungsstift
DE102014204566B4 (de) * 2014-03-12 2021-05-12 Schaeffler Technologies AG & Co. KG Zentralventil für einen Nockenwellenversteller mit Mittenverriegelung
CN109209548B (zh) 2017-06-30 2022-01-25 博格华纳公司 具有两个锁定位置的可变凸轮轴正时装置

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3164007B2 (ja) * 1997-02-14 2001-05-08 トヨタ自動車株式会社 内燃機関のバルブタイミング調整装置
JPH11280427A (ja) * 1998-03-31 1999-10-12 Aisin Seiki Co Ltd 弁開閉時期制御装置
JP3918971B2 (ja) * 1998-04-27 2007-05-23 アイシン精機株式会社 弁開閉時期制御装置
JP4465846B2 (ja) * 2000-09-27 2010-05-26 アイシン精機株式会社 弁開閉時期制御装置
JP4411814B2 (ja) * 2001-03-30 2010-02-10 株式会社デンソー バルブタイミング調整装置
DE10213831A1 (de) 2001-03-28 2002-11-07 Denso Corp Variables Ventilsteuerzeitengerät
JP4487449B2 (ja) 2001-06-28 2010-06-23 アイシン精機株式会社 弁開閉時期制御装置
JP4177297B2 (ja) 2004-06-25 2008-11-05 株式会社日立製作所 内燃機関のバルブタイミング制御装置
JP2006170025A (ja) 2004-12-14 2006-06-29 Aisin Seiki Co Ltd 内燃機関の弁開閉時期制御装置
DE102005023228B4 (de) 2005-05-20 2017-09-07 Schaeffler Technologies AG & Co. KG Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
JP4605473B2 (ja) 2005-12-27 2011-01-05 アイシン精機株式会社 弁開閉時期制御装置

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2008006684A1 *

Also Published As

Publication number Publication date
EP2041402B1 (fr) 2010-01-20
DE502007002686D1 (de) 2010-03-11
JP5082164B2 (ja) 2012-11-28
WO2008006684A1 (fr) 2008-01-17
DE102006031593A1 (de) 2008-01-10
JP2009542967A (ja) 2009-12-03
US20090314234A1 (en) 2009-12-24
US8006660B2 (en) 2011-08-30

Similar Documents

Publication Publication Date Title
EP2041403B1 (fr) Dispositif destiné à réguler de manière variable les temps de commande de soupapes d'échanges des gaz d'un moteur à combustion interne
EP2041402B1 (fr) Dispositif destiné à régler de manière variable les temps de commande des soupapes d'échanges des gaz d'un moteur à combustion interne
EP2238319B1 (fr) Dispositif de réglage variable des temps d'ouverture et de fermeture des soupapes d'échange des gaz d'un moteur à combustion interne
EP2118453B1 (fr) Dispositif de réglage variable des temps de commande de soupapes d'échange gazeux d'un moteur à combustion interne
EP2220345B1 (fr) Dispositif de réglage variable de la distribution de soupapes de renouvellement des gaz d'un moteur à combustion interne
EP2041404B1 (fr) Soupape de commande hydraulique
DE102014212617B4 (de) Mittenverriegelung für einen Nockenwellenversteller
EP2220346B1 (fr) Dispositif de réglage variable de la distribution des soupapes de renouvellement des gaz d'un moteur à combustion interne
DE102009056020A1 (de) Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
DE60013549T2 (de) Variable Ventilsteuerungseinrichtung mit einem Verriegelungsschieber
DE102007028187A1 (de) Hydraulischer Nockenwellenversteller zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
EP2118455A1 (fr) Dispositif combiné de verrouillage et de limitation d'angle de rotation d'un variateur d'arbre à cames
DE102009016186A1 (de) Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
EP2504534B1 (fr) Dispositif de dephasage de soupapes pour moteur a combustion interne
DE102005023204A1 (de) Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
DE102005023228A1 (de) Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
DE102005024242B4 (de) Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
EP2453112B1 (fr) Dispositif de déphasage d'arbres à came pour moteur à combustion interne
DE102010009392A1 (de) Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine
EP2324212A1 (fr) Dispositif de réglage d'arbre à came pour un moteur à combustion interne
DE102017112471B3 (de) Nockenwellenversteller
DE202008009417U1 (de) Vorrichtung zur variablen Einstellung der Steuerzeiten von Gaswechselventilen einer Brennkraftmaschine

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20090209

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK RS

DAX Request for extension of the european patent (deleted)
RBV Designated contracting states (corrected)

Designated state(s): DE FR GB HU IT

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB HU IT

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REF Corresponds to:

Ref document number: 502007002686

Country of ref document: DE

Date of ref document: 20100311

Kind code of ref document: P

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: SCHAEFFLER TECHNOLOGIES GMBH & CO. KG

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20101021

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E008755

Country of ref document: HU

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

Free format text: REGISTERED BETWEEN 20110407 AND 20110413

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 502007002686

Country of ref document: DE

Owner name: SCHAEFFLER TECHNOLOGIES AG & CO. KG, DE

Free format text: FORMER OWNER: SCHAEFFLER TECHNOLOGIES GMBH & CO. KG, 91074 HERZOGENAURACH, DE

Effective date: 20120828

Ref country code: DE

Ref legal event code: R081

Ref document number: 502007002686

Country of ref document: DE

Owner name: SCHAEFFLER TECHNOLOGIES GMBH & CO. KG, DE

Free format text: FORMER OWNER: SCHAEFFLER TECHNOLOGIES GMBH & CO. KG, 91074 HERZOGENAURACH, DE

Effective date: 20120828

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 502007002686

Country of ref document: DE

Owner name: SCHAEFFLER TECHNOLOGIES AG CO. KG, DE

Free format text: FORMER OWNER: SCHAEFFLER TECHNOLOGIES AG CO. KG, 91074 HERZOGENAURACH, DE

Effective date: 20140214

Ref country code: DE

Ref legal event code: R081

Ref document number: 502007002686

Country of ref document: DE

Owner name: SCHAEFFLER TECHNOLOGIES GMBH & CO. KG, DE

Free format text: FORMER OWNER: SCHAEFFLER TECHNOLOGIES AG & CO. KG, 91074 HERZOGENAURACH, DE

Effective date: 20140214

Ref country code: DE

Ref legal event code: R081

Ref document number: 502007002686

Country of ref document: DE

Owner name: SCHAEFFLER TECHNOLOGIES AG & CO. KG, DE

Free format text: FORMER OWNER: SCHAEFFLER TECHNOLOGIES AG & CO. KG, 91074 HERZOGENAURACH, DE

Effective date: 20140214

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 502007002686

Country of ref document: DE

Owner name: SCHAEFFLER TECHNOLOGIES AG & CO. KG, DE

Free format text: FORMER OWNER: SCHAEFFLER TECHNOLOGIES GMBH & CO. KG, 91074 HERZOGENAURACH, DE

Effective date: 20150401

REG Reference to a national code

Ref country code: HU

Ref legal event code: FH1C

Free format text: FORMER REPRESENTATIVE(S): MESZAROSNE DONUSZ KATALIN, S.B.G & K. SZABADALMI UEGYVIVOEI IRODA, HU

Representative=s name: SBGK SZABADALMI UEGYVIVOEI IRODA, HU

Ref country code: HU

Ref legal event code: GB9C

Owner name: SCHAEFFLER TECHNOLOGIES AG & CO. KG, DE

Free format text: FORMER OWNER(S): SCHAEFFLER TECHNOLOGIES GMBH & CO. KG, DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20180629

Year of fee payment: 12

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190630

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: HU

Payment date: 20220617

Year of fee payment: 16

Ref country code: GB

Payment date: 20220627

Year of fee payment: 16

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230522

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20230623

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20230821

Year of fee payment: 17

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20230621

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230622

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230621