EP1544420A2 - Internal combustion engine with hydraulic camshaft phasing device - Google Patents

Internal combustion engine with hydraulic camshaft phasing device Download PDF

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Publication number
EP1544420A2
EP1544420A2 EP04026407A EP04026407A EP1544420A2 EP 1544420 A2 EP1544420 A2 EP 1544420A2 EP 04026407 A EP04026407 A EP 04026407A EP 04026407 A EP04026407 A EP 04026407A EP 1544420 A2 EP1544420 A2 EP 1544420A2
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EP
European Patent Office
Prior art keywords
stator
walls
web walls
web
rotor
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
EP04026407A
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German (de)
French (fr)
Other versions
EP1544420A3 (en
EP1544420B1 (en
Inventor
Ulrich Wierl
Mike Kohrs
Rainer Ottersbach
Jochen Auchter
Hermann Wiehl
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
INA Schaeffler KG
Schaeffler KG
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Publication date
Application filed by INA Schaeffler KG, Schaeffler KG filed Critical INA Schaeffler KG
Publication of EP1544420A2 publication Critical patent/EP1544420A2/en
Publication of EP1544420A3 publication Critical patent/EP1544420A3/en
Application granted granted Critical
Publication of EP1544420B1 publication Critical patent/EP1544420B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/34Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • 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
    • F01L1/46Component parts, details, or accessories, not provided for in preceding subgroups
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/34Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • F01L1/344Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear
    • F01L1/3442Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear using hydraulic chambers with variable volume to transmit the rotating force
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L2301/00Using particular materials

Definitions

  • the invention relates to an internal combustion engine with a hydraulic device for the rotational angle adjustment of a camshaft with respect to a crankshaft, comprising: a rotor with wings arranged thereon, the non-rotatable with the camshaft is connected, a frontally provided with an end wall Stator rotatably with a driven by the crankshaft drive wheel is connected, provided on both sides of the wing pressure chambers are, in each case by web walls and inner and outer, in the circumferential direction, are concentric walls of the stator are limited and pressurizable via a hydraulic system with hydraulic fluid or be emptied.
  • This device consists of a rotor and a stator, of which the former, designed as an impeller, the camshaft includes and turns in sync with her.
  • the stator is on the one hand by an end wall, which Part of a housing surrounding the stator, and on the other hand closed by a drive wheel fluid-tight. It includes the rotor and rotates synchronously with the driven by the crankshaft drive wheel.
  • Essentially radially extending web walls in the stator allow only one limited rotational angle of the rotor and form with this several pressure chambers, which can be pressurized with hydraulic fluid or emptied.
  • a proposal for reducing the mass of the device for adjusting the angle of rotation For example, DE 101 48 687 A1 or DE 101 34 320 A1 be removed by parts of the device made of aluminum or a Made of aluminum alloy or another light metal.
  • This has the disadvantage that by different thermal expansion coefficients the leakage gaps can increase over the warming and thus one high leakage results.
  • aluminum is deformed with the same dimensions under load stronger than steel or iron. Especially if then the Individual parts must be clamped together by housing screws correspondingly large column allow a deformation. The housing screws represent an increased construction cost, thus causing higher costs and also result in a non-optimal power flow for the device.
  • the invention is therefore based on the object, a device for rotational angle adjustment a camshaft relative to a crankshaft for a To design an internal combustion engine such that on the one hand a mass reduction the device takes place on the other hand, while minimizing the Leakage.
  • the object is in a device for an internal combustion engine solved with the features of the preamble of claim 1 thereby that essential parts of the stator, in particular its web walls and its inner and outer walls, and optionally the housing with a possibly arranged therein sealing disc as non-cutting produced sheet metal parts are formed.
  • essential parts of the stator in particular its web walls and its inner and outer walls, and optionally the housing with a possibly arranged therein sealing disc as non-cutting produced sheet metal parts are formed.
  • sheet metal instead of sheet metal also used band be used in the following sheet as a generic term for sheet metal or tape becomes.
  • the solid sintered components as pressure chamber forming units of the drive side are thus replaced by thin-walled sheet metal and Blechumformmaschine. Because fewer sintered components must be manufactured, this results in a Reduction of cutting costs and reduction of external costs Oil leakage by eliminating the porous sintered parts.
  • the device despite its lower mass high rigidity and Resilience, these sheets can be local, along the load directions by formations or corresponding profiles ideally the load be adapted without requiring larger wall thicknesses globally and thus a high mass must be accepted.
  • this Across from a Masseredutation by using light metal such as proposed in DE 101 34 320 A1, this has the advantage that the thermal expansion coefficient All components remain the same and thus no leaks due to thermal effects.
  • the stator consists of inner and outer circumferentially extending Walls and web walls.
  • the web walls each connect two ends from adjacent inner and outer circumferentially Walls and extend substantially radially.
  • the web walls are not exactly radial, but one have certain angles to the radial or they are not flat, but recesses, for example, jamming of the wings in their final positions.
  • stator is made of thin-walled sheet metal, it is not so dimensionally stable like a sintered stator known in the art. It exists the possibility of the stator directly via cohesive connection options to attach to the torque transmitting component. To a comparable To achieve bending and compression stiffness like that of the sintered stator, but he can be used in a comprehensive housing him ( Figure 2a), which with connection technologies of the forming technology or by general force, shape and friction-locked technologies such as knurling, Flanging, welding, caulking, riveting, gluing or bent retaining lugs is connected to the drive wheel. The housing then takes over the Connection of the stator to the drive wheel as torque transmitting and Radial load-transferable component and the seal. It also prevents that occur at the stator due to introduced radial forces vibrations.
  • the housing seals the stator on one end face and forms one there Bulkhead. If the stator walls to the end wall no right angle form, the sealing of the pressure chambers is not completely guaranteed. To avoid leakage losses, it is therefore advantageous to use a sealing washer immediately before the front wall, so that after connecting the front wall with the stator and inserting the rotor with wings rectangular Pressure chambers arise. The stability of the housing can be additionally increased when you connect the sealing disc firmly to the front wall.
  • the Sealing disk is preferably profiled from thin-walled sheet metal and in size and shape of the stator adapted.
  • non-cutting parts made of metal strips. If necessary, as in the case of the stator, the strip must be at one point formed a ring and then firmly connected, for example by Welding.
  • the non-cutting production of the stator and the housing means of course not that these parts are not post-machined if very high accuracy is required.
  • a second way to increase the bending and compressive stiffness of the stator is to make the web walls so that they radial forces and / or Can transmit peripheral forces (Figure 3a).
  • the support of the radial chain or belt power can be internally between stator and rotor or externally between Camshaft or an extension of the rotor and sprocket or made from a combination of both possibilities. It's special here proven advantageous to form the web walls not exactly radially, but in a range of 10 ° to 30 ° to the radial, so that the wings in their end positions touch the radially outer web wall ends.
  • a third embodiment is a tubular stator whose web walls as retracted Webs are formed. Through the remaining, closed ring surface the housing is saved. This further reduces the mass. Between edge and the radially extending walls, the sealing disc inserted and then sealed the edge and firmly connected. At this Execution takes up the ring surface on the radial forces and prevents Swinging of the stator.
  • the radially extending Walls should also be designed as open ends, in which case for storage and Seal used in the rotor sliding shoes.
  • the sliding shoes are like that trained and arranged that they trained as retracted webs Support web walls against each other. They prevent bending the web walls.
  • the wall thickness of the radially extending walls of the stator can be further reduced be prevented if the wings of the rotor are prevented in their respective Strike end positions against the radially extending walls of the stator and put pressure on them.
  • a Verstellwinkelbegrenzung is necessary. This can for example via a related to the rotor Element for Verstellwinkelbegrenzung that in a corresponding backdrop engages, be realized.
  • the inventively designed device is thus opposite a device
  • the prior art lighter requires less cutting costs and thus reduces the manufacturing costs and can also be applied to a synthetic resin impregnation or steam treatment for sealing the now refrain from using any sintered material that is no longer required.
  • a hydraulic Device 1 for adjusting the angle of rotation of a camshaft 2 with respect to a not shown crankshaft, which is designed as a hydraulic actuator is.
  • This device 1 is driven by a drive wheel 3, for example connected by a chain not shown with the crankshaft is, driven.
  • the device 1 consists of a fixed with the drive wheel 3 connected to the stator 4, by an end wall 5 and the Drive wheel 3 is sealed fluid-tight, and one by an axial Central screw 21 rotatably connected to the camshaft 2 rotor 6, wherein the rotor 6 is designed as an impeller.
  • the stator 4 of the device 1 formed by web walls 7, 7 ', 7 “and by outer 8, 8', 8" and inner 9, 9 ', 9 “, circumferentially extending walls with the rotor 6 and its wings 10 first pressure chambers 11, 11 ', 11 "and second pressure chambers 12, 12', 12", which, filled with hydraulic fluid, an angular adjustment between the rotor. 6 and stator 4.
  • the rotor 6 and the stator 4 are in a housing 13th arranged, the first 11, 11 ', 11 "and second 12, 12', 12" pressure chambers seals to the outside.
  • a sealing washer 14 is inserted, which corresponds to the diameter of the stator 4 is adjusted.
  • the web walls 7, 7 ', 7 are not exactly formed radially, but at an angle of about 20 °, so that the wings 10 in their end positions the radially outer ends of the web walls 7, 7 ', 7 "touch the bending and compressive rigidity of the stator 4 increases and it is possible radial forces and to transmit circumferential forces
  • FIG. 3 shows a cross section of a second version of a tube Stators 4. It forms by its substantially radially extending Web walls 7, 7 ', 7 "and its inner 8, 8', 8" and outer 9, 9 ', 9 “, in the circumferential direction extending walls with the not shown in this figure Rotor 6, the first 11, 11 ', 11 "and second 12, 12', 12" pressure chambers.
  • Stator 4 itself is arranged in a cylindrical housing 13 such that the housing 13 and the outer, circumferentially extending walls 9, 9 ', 9 "touch, whereby the rigidity of the stator 4 is increased and Vibrations are damped due to radial forces.
  • the stiffness can be further increased by the formed by the housing 13 and stator 4 Hollow chambers or incisions 15, 15 ', 15 ", for example with metal foam are filled. So that the wings 10 do not jam in the end positions, it is advantageous to form radially extending web walls in two parts, such that they have at least a first, radially extending part 20, to which the wings strike and at least one other part.
  • FIGs 4a and 4b show a cross-section and a perspective view A third embodiment of a stator 4.
  • this third stator 4 is stiffer with respect to a radial force absorption. It is particularly advantageous to make the web walls such that the respective adjacent web walls 7, 7 'and the housing 13 prevent spreading under radial force (self-locking).
  • FIGS. 5a and 5b show a cross section and a perspective view a fourth type of stator 4.
  • the sealing disc 14 Figure 1 can be used, which is inserted on the front side of the stator 4 and the edge, for example can be crimped.
  • the web walls 7, 7 ', 7 are well formed by their open ends. They can also be designed as shown in FIG. 6b and then with Sliding shoes 19 to be sealed.
  • FIGs 6a and 6b show a perspective view of a part of a fifth and sixth stator 4, the variants of the fifth stator 4 represent.
  • These stator variants 4 are therefore inserted into a housing 13.
  • a similar rigidity as in the devices of the state The technique is illustrated by the illustrated embodiments of the stator. 4 reached.
  • the leakage losses are reduced because of porous Sintered components or on a complex steam treatment or resin impregnation can be waived.

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

Abstract

The device has a rotor (6) with blades (10) fastened to the camshaft (2), and a stator (4) with end wall (5) fastened to a drive pulley (3) driven by the crankshaft. The stator, esp. its web walls, and its inner and outer peripheral walls, is a metal plate or band part, formed by a non-cutting process. The stator has local reinforcements of profiles, beads, etc. extending along direction of special loads. Stator, outer stator housing (13), and drive pulley are fastened to each other by e.g. forming technology. Pressure chambers between stator and rotor are closed at one end by a metal sealing plate (14). Hollows or cutouts in stator walls are filled with metal foam or injected plastic.

Description

Gebiet der ErfindungField of the invention

Die Erfindung betrifft eine Brennkraftmaschine mit einer hydraulischen Vorrichtung zur Drehwinkelverstellung einer Nockenwelle gegenüber einer Kurbelwelle, umfassend: einen Rotor mit daran angeordneten Flügeln, der drehfest mit der Nockenwelle verbunden ist, einen stirnseitig mit einer Stirnwand versehenen Stator, der drehfest mit einem von der Kurbelwelle angetriebenen Antriebsrad verbunden ist, wobei beiderseits der Flügel Druckkammern vorgesehen sind, die jeweils durch Stegwände und innere sowie äußere, in Umfangsrichtung, konzentrisch zueinander verlaufende Wände des Stators begrenzt sind und über ein Hydrauliksystem mit Hydraulikflüssigkeit druckbeaufschlagbar oder entleerbar sind.The invention relates to an internal combustion engine with a hydraulic device for the rotational angle adjustment of a camshaft with respect to a crankshaft, comprising: a rotor with wings arranged thereon, the non-rotatable with the camshaft is connected, a frontally provided with an end wall Stator rotatably with a driven by the crankshaft drive wheel is connected, provided on both sides of the wing pressure chambers are, in each case by web walls and inner and outer, in the circumferential direction, are concentric walls of the stator are limited and pressurizable via a hydraulic system with hydraulic fluid or be emptied.

Hintergrund der ErfindungBackground of the invention

Aus der DE 101 34 320 A1 ist eine Brennkraftmaschine mit einer gattungsgemäßen hydraulischen Vorrichtung zur Drehwinkelverstellung einer Nockenwelle bekannt, die die Phasenlage einer Nockenwelle gegenüber einer Kurbelwelle verändern kann. Diese Vorrichtung besteht aus einem Rotor und einem Stator, von denen ersterer, als Flügelrad ausgebildet, die Nockenwelle umfasst und sich synchron mit ihr dreht. Der Stator ist einerseits durch eine Stirnwand, welche Teil eines den Stator umgebenden Gehäuses sein kann, und andererseits durch ein Antriebsrad druckmitteldicht verschlossen. Er umfasst den Rotor und dreht sich synchron mit dem von der Kurbelwelle angetriebenen Antriebsrad. Im wesentlichen radial verlaufende Stegwände im Stator erlauben nur einen begrenzten Drehwinkel des Rotors und bilden mit diesem mehrere Druckkammern, die mit Hydraulikflüssigkeit druckbeaufschlagt oder entleert werden können.From DE 101 34 320 A1 an internal combustion engine with a generic hydraulic device for adjusting the angle of rotation of a camshaft known, the phase angle of a camshaft relative to a crankshaft can change. This device consists of a rotor and a stator, of which the former, designed as an impeller, the camshaft includes and turns in sync with her. The stator is on the one hand by an end wall, which Part of a housing surrounding the stator, and on the other hand closed by a drive wheel fluid-tight. It includes the rotor and rotates synchronously with the driven by the crankshaft drive wheel. Essentially radially extending web walls in the stator allow only one limited rotational angle of the rotor and form with this several pressure chambers, which can be pressurized with hydraulic fluid or emptied.

Nachteilig bei dieser bekannten Vorrichtung ist jedoch, dass die Einzelteile der Vorrichtung vorwiegend aus Stahl oder Eisen bestehen, welche durch Sintern oder Zerspanen hergestellt sind. Daraus resultieren

  • 1. eine hohe Masse der Vorrichtung zur Drehwinkelverstellung,
  • 2. hohe Fertigungskosten durch den Zerspanungsaufwand bei der Fertigung der Sinterbauteile,
  • 3. eine unerwünschte, externe Ölleckage durch die porösen Sinterbauteile.
  • A disadvantage of this known device, however, is that the items of the device mainly consist of steel or iron, which are made by sintering or machining. This results
  • 1. a high mass of the device for adjusting the rotational angle,
  • 2. high production costs due to the machining outlay during the production of the sintered components,
  • 3. undesirable external oil leakage through the porous sintered components.
  • Weil in der Sintermetallurgie dünne Wandstärken, insbesondere im Zusammenhang mit Wandstärkenschwankungen hinsichtlich Dichteverteilung sowie Festigkeit und Steifigkeit problematisch sind und sich weiterhin komplexe Formen mit unterschiedlichen Füllhöhen oftmals nur mit teuren Schiebern im Werkzeug realisieren lassen, sind bisherige Vorrichtungen zur Drehwinkelverstellung meist aus relativ schweren und massiven Bauteilen gefertigt. Bei spanend hergestellten Vorrichtungen liegt die Problematik ähnlich; komplizierte, der Belastung angepasste Formen sind mit hohem Zerspanungsaufwand verbunden. Because in the sintered metallurgy thin wall thicknesses, especially in context with wall thickness variations in terms of density distribution as well Strength and rigidity are problematic and continue to be complex shapes with different filling heights often only with expensive sliders in the To implement tools are previous devices for the rotation angle adjustment usually made of relatively heavy and solid components. At cutting manufactured devices, the problem is similar; complicated, The load adapted forms are with high machining costs connected.

    Ein Vorschlag zur Massereduzierung der Vorrichtung zur Drehwinkelverstellung kann beispielsweise der DE 101 48 687 A1 oder der DE 101 34 320 A1 entnommen werden, indem Teile der Vorrichtung aus Aluminium oder aus einer Aluminiumlegierung oder einem anderen Leichtmetall gefertigt werden. Dies hat zum Nachteil, dass durch unterschiedliche Wärmeausdehnungskoeffizienten die Leckspalte über die Erwärmung zunehmen können und sich damit eine hohe Leckage ergibt. Außerdem verformt sich bei gleichen Abmessungen Aluminium unter Last stärker als Stahl bzw. Eisen. Insbesondere wenn dann die Einzelteile durch Gehäuseschrauben miteinander verspannt werden, müssen entsprechend große Spalte eine Verformung zulassen. Die Gehäuseschrauben stellen einen erhöhten Bauaufwand dar, verursachen demnach höhere Kosten und haben zudem einen nicht optimalen Kraftfluß für die Vorrichtung zur Folge.A proposal for reducing the mass of the device for adjusting the angle of rotation For example, DE 101 48 687 A1 or DE 101 34 320 A1 be removed by parts of the device made of aluminum or a Made of aluminum alloy or another light metal. This has the disadvantage that by different thermal expansion coefficients the leakage gaps can increase over the warming and thus one high leakage results. In addition, aluminum is deformed with the same dimensions under load stronger than steel or iron. Especially if then the Individual parts must be clamped together by housing screws correspondingly large column allow a deformation. The housing screws represent an increased construction cost, thus causing higher costs and also result in a non-optimal power flow for the device.

    Aufgabe der ErfindungObject of the invention

    Der Erfindung liegt deshalb die Aufgabe zugrunde, eine Vorrichtung zur Drehwinkelverstellung einer Nockenwelle gegenüber einer Kurbelwelle für eine Brennkraftmaschine derart zu konzipieren, dass einerseits eine Massereduzierung der Vorrichtung erfolgt bei andererseits gleichzeitiger Minimierung der Leckage.The invention is therefore based on the object, a device for rotational angle adjustment a camshaft relative to a crankshaft for a To design an internal combustion engine such that on the one hand a mass reduction the device takes place on the other hand, while minimizing the Leakage.

    Beschreibung der ErfindungDescription of the invention

    Erfindungsgemäß wird die Aufgabe bei einer Vorrichtung für eine Brennkraftmaschine mit den Merkmalen des Oberbegriffs von Anspruch 1 dadurch gelöst, dass wesentliche Teile des Stators, insbesondere seine Stegwände und seine inneren sowie äußeren Wände, sowie gegebenenfalls das Gehäuse mit einer eventuell darin angeordneten Dichtscheibe als spanlos hergestellte Blechteile ausgebildet sind. Selbstverständlich kann statt Blech auch Band verwendet werden, wobei im folgenden Blech als Oberbegriff für Blech oder Band verwendet wird.According to the invention, the object is in a device for an internal combustion engine solved with the features of the preamble of claim 1 thereby that essential parts of the stator, in particular its web walls and its inner and outer walls, and optionally the housing with a possibly arranged therein sealing disc as non-cutting produced sheet metal parts are formed. Of course, instead of sheet metal also used band be used in the following sheet as a generic term for sheet metal or tape becomes.

    Die massiven Sinterbauteile als Druckkammer bildende Einheiten der Antriebsseite werden somit durch dünnwandige Blech- und Blechumformteile ersetzt. Weil somit weniger Sinterbauteile gefertigt werden müssen, ergibt sich eine Verringerung des Zerspanungsaufwands und eine Verringerung der externen Ölleckage durch den Wegfall der porösen Sinterteile.The solid sintered components as pressure chamber forming units of the drive side are thus replaced by thin-walled sheet metal and Blechumformteile. Because fewer sintered components must be manufactured, this results in a Reduction of cutting costs and reduction of external costs Oil leakage by eliminating the porous sintered parts.

    Damit die Vorrichtung trotz ihrer geringeren Masse eine hohe Steifigkeit und Belastbarkeit aufweist, können diese Bleche lokal, entlang den Belastungsrichtungen durch Ausformungen oder entsprechende Profilierungen ideal der Belastung angepasst werden, ohne dass global größere Wandstärken erforderlich sind und damit eine hohe Masse in Kauf genommen werden muss. Gegenüber einer Massereduktion durch Verwendung von Leichtmetall wie beispielsweise in DE 101 34 320 A1 vorgeschlagen, hat dies zum Vorteil, dass der Wärmeausdehnungskoeffizient aller Bauteile gleich bleibt und somit keine Undichtigkeiten aufgrund thermischer Effekte entstehen können.Thus, the device despite its lower mass high rigidity and Resilience, these sheets can be local, along the load directions by formations or corresponding profiles ideally the load be adapted without requiring larger wall thicknesses globally and thus a high mass must be accepted. Across from a Massereduktion by using light metal such as proposed in DE 101 34 320 A1, this has the advantage that the thermal expansion coefficient All components remain the same and thus no leaks due to thermal effects.

    Der Stator besteht aus inneren und äußeren in Umfangsrichtung verlaufenden Wänden und aus Stegwänden. Die Stegwände verbinden jeweils zwei Enden von benachbarten inneren und äußeren in Umfangsrichtung verlaufenden Wänden und verlaufen im wesentlichen radial. Für einige Statorvarianten ist es vorteilhaft, wenn die Stegwände nicht genau radial verlaufen, sondern einen gewissen Winkel zur Radialen aufweisen oder sie nicht eben ausgebildet sind, sondern Vertiefungen aufweisen, um beispielsweise ein Verklemmen der Flügel in ihren Endstellungen zu verhindern.The stator consists of inner and outer circumferentially extending Walls and web walls. The web walls each connect two ends from adjacent inner and outer circumferentially Walls and extend substantially radially. For some stator variants it is advantageous if the web walls are not exactly radial, but one have certain angles to the radial or they are not flat, but recesses, for example, jamming of the wings in their final positions.

    Weil der Stator aus dünnwandigem Blech hergestellt ist, ist er nicht so formstabil wie ein aus dem Stand der Technik bekannter, gesinterter Stator. Es besteht die Möglichkeit, den Stator direkt über stoffschlüssige Verbindungsmöglichkeiten an die momentenübertragende Komponente anzubringen. Um eine vergleichbare Biege- und Drucksteifigkeit wie die des gesinterten Stators zu erzielen, kann er aber in ein ihn umfassendes Gehäuse eingesetzt werden (Figur 2a), das mit Verbindungstechnologien der Umformtechnik bzw. durch allgemein kraft-, form-, reibstoffschlüssige Technologien wie beispielsweise Rändeln, Bördeln, Schweißen, Verstemmen, Vernieten, Kleben oder umgebogene Haltenasen an das Antriebsrad angebunden ist. Das Gehäuse übernimmt dann die Anbindung des Stators an das Antriebsrad als momentenübertragendes und radiallastübertragbares Bauteil und die Abdichtung. Es verhindert auch, dass am Stator aufgrund von eingebrachten Radialkräften Schwingungen auftreten.Because the stator is made of thin-walled sheet metal, it is not so dimensionally stable like a sintered stator known in the art. It exists the possibility of the stator directly via cohesive connection options to attach to the torque transmitting component. To a comparable To achieve bending and compression stiffness like that of the sintered stator, but he can be used in a comprehensive housing him (Figure 2a), which with connection technologies of the forming technology or by general force, shape and friction-locked technologies such as knurling, Flanging, welding, caulking, riveting, gluing or bent retaining lugs is connected to the drive wheel. The housing then takes over the Connection of the stator to the drive wheel as torque transmitting and Radial load-transferable component and the seal. It also prevents that occur at the stator due to introduced radial forces vibrations.

    Das Gehäuse dichtet den Stator auf einer Stirnseite ab und bildet dort eine Stirnwand. Wenn die Statorwände zur Stirnwand keinen rechtwinkligen Winkel bilden, ist die Abdichtung der Druckkammern nicht vollständig gewährleistet. Um Leckageverluste zu vermeiden, ist es daher vorteilhaft, eine Dichtscheibe unmittelbar vor der Stirnwand anzuordnen, so dass nach Verbinden der Stirnwand mit dem Stator und Einsetzen des Rotors mit Flügeln rechtwinklige Druckkammern entstehen. Die Stabilität des Gehäuses kann zusätzlich erhöht werden, wenn man die Dichtscheibe fest mit der Stirnwand verbindet. Die Dichtscheibe ist vorzugsweise aus dünnwandigem Blech profiliert und an Größe und Form des Stators angepasst.The housing seals the stator on one end face and forms one there Bulkhead. If the stator walls to the end wall no right angle form, the sealing of the pressure chambers is not completely guaranteed. To avoid leakage losses, it is therefore advantageous to use a sealing washer immediately before the front wall, so that after connecting the front wall with the stator and inserting the rotor with wings rectangular Pressure chambers arise. The stability of the housing can be additionally increased when you connect the sealing disc firmly to the front wall. The Sealing disk is preferably profiled from thin-walled sheet metal and in size and shape of the stator adapted.

    Der Zusammenhalt der Teile Stator, Gehäuse und Dichtscheibe wird durch oben angeführte Verbindungstechnologien der Umformtechnik gewährleistet. Gegenüber der axialen, kraftschlüssigen Schraubverbindung werden Druckspannungsverformungen reduziert; außerdem wird vorteilhafterweise kein zusätzliches Bauteil benötigt und der Montageaufwand vermindert.The cohesion of the parts stator, housing and sealing disc is through above-mentioned joining technologies of forming technology ensured. Compared to the axial, non-positive screw connection are compressive stress deformations reduced; In addition, advantageously no additional Component needed and reduced assembly costs.

    Es ist zweckmäßig, die spanlos hergestellten Teile aus Blechstreifen zu formen. Gegebenenfalls muss - wie beim Stator - an einer Stelle der Streifen zu einem Ring geformt und dann fest verbunden werden, beispielsweise durch Verschweißen. Die spanlose Herstellung des Stators und des Gehäuses bedeutet selbstverständlich nicht, dass diese Teile nicht spanend nachbearbeitet werden, sofern eine sehr hohe Genauigkeit erforderlich sein sollte.It is expedient to form the non-cutting parts made of metal strips. If necessary, as in the case of the stator, the strip must be at one point formed a ring and then firmly connected, for example by Welding. The non-cutting production of the stator and the housing means of course not that these parts are not post-machined if very high accuracy is required.

    Eine zweite Möglichkeit, um die Biege und Drucksteifigkeit des Stators zu erhöhen, ist es, die Stegwände so auszubilden, dass sie Radialkräfte und/oder Umfangskräfte übertragen können (Figur 3a). Die Abstützung der radialen Ketten- bzw. Riemenkraft kann intern zwischen Stator und Rotor oder extern zwischen Nockenwelle bzw. einer Verlängerung des Rotors und Kettenrad oder aus einer Kombination beider Möglichkeiten erfolgen. Dabei hat es besonders vorteilhaft erwiesen, die Stegwände nicht genau radial auszubilden, sondern in einem Bereich von 10° bis 30° zur Radialen anzustellen, so dass die Flügel in ihren Endstellungen die radial außen liegenden Stegwandenden berühren.A second way to increase the bending and compressive stiffness of the stator, is to make the web walls so that they radial forces and / or Can transmit peripheral forces (Figure 3a). The support of the radial chain or belt power can be internally between stator and rotor or externally between Camshaft or an extension of the rotor and sprocket or made from a combination of both possibilities. It's special here proven advantageous to form the web walls not exactly radially, but in a range of 10 ° to 30 ° to the radial, so that the wings in their end positions touch the radially outer web wall ends.

    Eine dritte Ausbildung ist ein rohrförmiger Stator, dessen Stegwände als eingezogene Stege ausgebildet sind. Durch die verbleibende, geschlossene Ringfläche wird das Gehäuse eingespart. Dadurch wird die Masse weiter verringert. Zwischen Rand und den radial verlaufenden Wänden kann die Dichtscheibe eingelegt und dann der Rand abgedichtet und fest verbunden werden. Bei dieser Ausführung nimmt die Ringfläche die Radialkräfte auf und verhindert ein Schwingen des Stators.A third embodiment is a tubular stator whose web walls as retracted Webs are formed. Through the remaining, closed ring surface the housing is saved. This further reduces the mass. Between edge and the radially extending walls, the sealing disc inserted and then sealed the edge and firmly connected. At this Execution takes up the ring surface on the radial forces and prevents Swinging of the stator.

    Um eine bessere Umformbarkeit zu erreichen, können die radial verlaufenden Wände auch als offene Enden ausgebildet sein, wobei dann zur Lagerung und Abdichtung im Rotor Gleitschuhe verwendet werden. Die Gleitschuhe sind derart ausgebildet und angeordnet, dass sie die als eingezogene Stege ausgebildeten Stegwände gegeneinander abstützen. Sie verhindern damit ein Verbiegen der Stegwände.To achieve better formability, the radially extending Walls should also be designed as open ends, in which case for storage and Seal used in the rotor sliding shoes. The sliding shoes are like that trained and arranged that they trained as retracted webs Support web walls against each other. They prevent bending the web walls.

    Die zwischen den Stegwänden sich befindenden Räume, entweder Hohlräume oder Einschnitte, werden mit Kunststoff um- oder ausgespritzt oder Metall geschäumt. Dadurch wird das Profil der im wesentlichen radial verlaufenden Stegwände versteift und eine hohe Dichtheit der Druckkammern untereinander sowie nach außen sicher gestellt.The spaces between the web walls, either cavities or cuts, are plastic-injected or sprayed or foamed metal. As a result, the profile of the substantially radially extending Web walls stiffened and a high tightness of the pressure chambers with each other as well as externally ensured.

    Die Wandstärke der radial verlaufenden Wände des Stators kann weiter reduziert werden, wenn verhindert wird, dass die Flügel des Rotors in ihren jeweiligen Endpositionen an die radial verlaufenden Wände des Stators anschlagen und Druck auf diese ausüben. Dazu ist eine Verstellwinkelbegrenzung notwendig. Diese kann beispielsweise über ein mit dem Rotor in Verbindung stehendes Element zur Verstellwinkelbegrenzung, das in eine korrespondierende Kulisse eingreift, realisiert werden.The wall thickness of the radially extending walls of the stator can be further reduced be prevented if the wings of the rotor are prevented in their respective Strike end positions against the radially extending walls of the stator and put pressure on them. For this purpose, a Verstellwinkelbegrenzung is necessary. This can for example via a related to the rotor Element for Verstellwinkelbegrenzung that in a corresponding backdrop engages, be realized.

    Die erfindungsgemäß ausgebildete Vorrichtung ist also gegenüber einer Vorrichtung des Standes der Technik leichter, benötigt weniger Zerspanungsaufwand und reduziert damit die Fertigungskosten und kann auch auf eine Kunstharzimprägnierung oder Wasserdampfbehandlung des zur Abdichtung des nun nicht mehr benötigten Sinterwerkstoffs verzichten.The inventively designed device is thus opposite a device The prior art lighter, requires less cutting costs and thus reduces the manufacturing costs and can also be applied to a synthetic resin impregnation or steam treatment for sealing the now refrain from using any sintered material that is no longer required.

    Kurze Beschreibung der ZeichnungenBrief description of the drawings

    Die Erfindung wird nachfolgend anhand von Ausführungsbeispielen näher erläutert und in den dazu gehörigen Zeichnungen schematisch dargestellt.
    Es zeigen

    Figur 1
    einen Längsschnitt einer Vorrichtung zur Drehwinkelverstellung, wobei ein spanlos ausgebildeter Stator in einem Außengehäuse eingesetzt ist;
    Figur 2
    einen Querschnitt durch eine Vorrichtung zur Drehwinkelverstellung,
    Figur 3
    einen Querschnitt einer zweiten Ausführung eines Stators,
    Figur 4a
    einen Querschnitt einer dritten Ausführung eines Stators,
    Figur 4b
    eine perspektivische Ansicht des Stators gemäß Figur 4a,
    Figur 5a
    einen Querschnitt einer vierten Ausführung eines Stators, dessen äußere Ringfläche geschlossen ist,
    Figur 5b
    eine perspektivische Ansicht des Stators gemäß Figur 5a,
    Figur 6a
    eine perspektivische Ansicht auf eine äußere, in Umfangsrichtung verlaufende Wand und nach außen ausgeformte Stegwände einer fünften Ausführung eines Stators
    Figur 6b
    eine perspektivische Ansicht auf eine äußere, in Umfangsrichtung verlaufende Wand und nach innen ausgeformte Stegwände einer sechsten Ausführung eines Stators mit einem Gleitschuh.
    The invention will be explained in more detail with reference to embodiments and shown schematically in the accompanying drawings.
    Show it
    FIG. 1
    a longitudinal section of a device for adjusting the rotational angle, wherein a chipless formed stator is inserted in an outer housing;
    FIG. 2
    a cross section through a device for adjusting the rotational angle,
    FIG. 3
    a cross section of a second embodiment of a stator,
    FIG. 4a
    a cross section of a third embodiment of a stator,
    FIG. 4b
    a perspective view of the stator according to Figure 4a,
    FIG. 5a
    a cross section of a fourth embodiment of a stator whose outer annular surface is closed,
    FIG. 5b
    a perspective view of the stator according to Figure 5a,
    FIG. 6a
    a perspective view of an outer, circumferentially extending wall and outwardly shaped web walls of a fifth embodiment of a stator
    FIG. 6b
    a perspective view of an outer, circumferentially extending wall and inwardly molded web walls of a sixth embodiment of a stator with a sliding block.

    Ausführliche Beschreibung der ZeichnungenDetailed description of the drawings

    Aus den Figuren 1 und 2 gehen die wesentlichen Teile einer hydraulischen Vorrichtung 1 zur Drehwinkelverstellung einer Nockenwelle 2 gegenüber einer nicht dargestellten Kurbelwelle hervor, die als hydraulischer Stellantrieb ausgebildet ist. Diese Vorrichtung 1 wird durch ein Antriebsrad 3, das beispielsweise durch eine nicht näher dargestellte Kette mit der Kurbelwelle verbunden ist, angetrieben. Im wesentlichen besteht die Vorrichtung 1 aus einem fest mit dem Antriebsrad 3 verbundenen Stator 4, der durch eine Stirnwand 5 und das Antriebsrad 3 druckmitteldicht verschlossen ist, und einem durch eine axiale Zentralschraube 21 drehfest mit der Nockenwelle 2 verbundenen Rotor 6, wobei der Rotor 6 als Flügelrad ausgebildet ist. Der Stator 4 der Vorrichtung 1 bildet durch Stegwände 7, 7', 7" und durch äußere 8, 8', 8" und innere 9, 9', 9", in Umfangsrichtung verlaufende Wände mit dem Rotor 6 und dessen Flügeln 10 erste Druckkammern 11, 11', 11" und zweite Druckkammern 12, 12', 12", die, mit Hydraulikflüssigkeit befüllt, eine Winkelverstellung zwischen Rotor 6 und Stator 4 herstellen. Der Rotor 6 und der Stator 4 sind in einem Gehäuse 13 angeordnet, das die ersten 11, 11', 11" und zweiten 12, 12', 12" Druckkammern nach außen abdichtet. Durch ein mit dem Rotor 6 in Verbindung stehendes Element 16 zur Verstellwinkelbegrenzung, das in eine korrespondierende Kulisse 17 eingreift, erfolgt ein Begrenzen des Verstellbereichs des Rotors 6, was die Belastungen des Stators 4 herabsetzt.From Figures 1 and 2 go the essential parts of a hydraulic Device 1 for adjusting the angle of rotation of a camshaft 2 with respect to a not shown crankshaft, which is designed as a hydraulic actuator is. This device 1 is driven by a drive wheel 3, for example connected by a chain not shown with the crankshaft is, driven. In essence, the device 1 consists of a fixed with the drive wheel 3 connected to the stator 4, by an end wall 5 and the Drive wheel 3 is sealed fluid-tight, and one by an axial Central screw 21 rotatably connected to the camshaft 2 rotor 6, wherein the rotor 6 is designed as an impeller. The stator 4 of the device 1 formed by web walls 7, 7 ', 7 "and by outer 8, 8', 8" and inner 9, 9 ', 9 ", circumferentially extending walls with the rotor 6 and its wings 10 first pressure chambers 11, 11 ', 11 "and second pressure chambers 12, 12', 12", which, filled with hydraulic fluid, an angular adjustment between the rotor. 6 and stator 4. The rotor 6 and the stator 4 are in a housing 13th arranged, the first 11, 11 ', 11 "and second 12, 12', 12" pressure chambers seals to the outside. By a standing with the rotor 6 in connection Element 16 for Verstellwinkelbegrenzung, which in a corresponding Setting 17 engages, is carried out limiting the adjustment of the rotor 6, which reduces the loads on the stator 4.

    Zwecks Abdichtung der Druckkammern 11, 11', 11", 12, 12', 12" ist zwischen Gehäuse 13 und Stator 4 eine Dichtscheibe 14 eingelegt, welche dem Durchmesser des Stators 4 angepasst ist.For the purpose of sealing the pressure chambers 11, 11 ', 11 ", 12, 12', 12" is between Housing 13 and stator 4, a sealing washer 14 is inserted, which corresponds to the diameter of the stator 4 is adjusted.

    In Figur 2 sind die Stegwände 7, 7', 7" nicht genau radial ausgebildet, sondern in einem Winkel von etwa 20°, so dass die Flügel 10 in ihren Endstellungen die radial außen liegenden Enden der Stegwände 7, 7', 7" berühren. Damit wird die Biege und Drucksteifigkeit des Stators 4 erhöht und es ist möglich, Radialkräfte und Umfangskräfte zu übertragenIn Figure 2, the web walls 7, 7 ', 7 "are not exactly formed radially, but at an angle of about 20 °, so that the wings 10 in their end positions the radially outer ends of the web walls 7, 7 ', 7 "touch the bending and compressive rigidity of the stator 4 increases and it is possible radial forces and to transmit circumferential forces

    Figur 3 zeigt einen Querschnitt einer zweiten Version eines als Rohr ausgebildeten Stators 4. Er bildet durch seine im wesentlichen radial verlaufenden Stegwände 7, 7', 7" und seine inneren 8, 8', 8" und äußeren 9, 9', 9", in Umfangsrichtung verlaufenden Wände mit dem in dieser Figur nicht dargestellten Rotor 6 die ersten 11, 11', 11" und zweiten 12, 12', 12" Druckkammern. Der Stator 4 selbst ist in einem zylindrischen Gehäuse 13 derart angeordnet, dass das Gehäuse 13 und die äußeren, in Umfangsrichtung verlaufenden Wände 9, 9', 9" sich berühren, wodurch die Steifigkeit des Stators 4 erhöht wird und Schwingungen infolge radialer Kräfte gedämpft werden. Die Steifigkeit kann weiter erhöht werden, indem die durch die Gehäuse 13 und Stator 4 gebildeten Hohlkammern bzw. Einschnitte 15, 15', 15" beispielsweise mit Metallschaum gefüllt sind. Damit sich die Flügel 10 in den Endstellungen nicht verklemmen, ist es vorteilhaft, radial verlaufende Stegwände zweiteilig auszubilden, derart, dass sie zumindest einen ersten, radial verlaufenden Teil 20 aufweisen, an den die Flügel anschlagen und mindestens einen weiteren Teil.FIG. 3 shows a cross section of a second version of a tube Stators 4. It forms by its substantially radially extending Web walls 7, 7 ', 7 "and its inner 8, 8', 8" and outer 9, 9 ', 9 ", in the circumferential direction extending walls with the not shown in this figure Rotor 6, the first 11, 11 ', 11 "and second 12, 12', 12" pressure chambers. Of the Stator 4 itself is arranged in a cylindrical housing 13 such that the housing 13 and the outer, circumferentially extending walls 9, 9 ', 9 "touch, whereby the rigidity of the stator 4 is increased and Vibrations are damped due to radial forces. The stiffness can be further increased by the formed by the housing 13 and stator 4 Hollow chambers or incisions 15, 15 ', 15 ", for example with metal foam are filled. So that the wings 10 do not jam in the end positions, it is advantageous to form radially extending web walls in two parts, such that they have at least a first, radially extending part 20, to which the wings strike and at least one other part.

    Die Figuren 4a und 4b zeigen einen Querschnitt und eine perspektivische Ansicht einer dritten Ausführungsform eines Stators 4. Gegenüber der in Figur 2 dargestellten Ausführung ist dieser dritte Stator 4 steifer bezüglich einer Radialkraftaufnahme. Besonders vorteilhaft ist es, die Stegwände derart anzustellen, dass die jeweiligen benachbarten Stegwände 7, 7' und das Gehäuse 13 ein Aufspreizen unter Radialkraft verhindern (Selbsthemmung).Figures 4a and 4b show a cross-section and a perspective view A third embodiment of a stator 4. Compared to that in Figure 2 illustrated embodiment, this third stator 4 is stiffer with respect to a radial force absorption. It is particularly advantageous to make the web walls such that the respective adjacent web walls 7, 7 'and the housing 13 prevent spreading under radial force (self-locking).

    Die Figuren 5a und 5b zeigen einen Querschnitt und eine perspektivische Ansicht einer vierten Bauart eines Stators 4. Die Stegwände 7, 7', 7" sind als in den Stator 4 eingezogene Stege ausgebildet. Sie bilden mit den in Umfangsrichtung verlaufenden Wänden 8, 8', 8", 9, 9', 9" dieses Stators 4 gleichzeitig einen Teil des Gehäuses 13. Besonders vorteilhaft an dieser Ausbildung ist, dass durch die verbleibende, geschlossene Ringfläche, die kreisrunde Außenwand 18, das Gehäuse 13 mit Ausnahme der Stirnwand 5 eingespart werden kann. Als Stirnwand 5 kann die Dichtscheibe 14 (Figur 1) verwendet werden, die stirnseitig auf den Stator 4 eingesetzt ist und deren Rand beispielsweise gebördelt werden kann. Aus der kreisrunden Außenwand 18 entstehen durch beispielsweise Stanzen die Stegwände 7, 7' die dann nach innen gebogen sind. Die Stegwände 7, 7', 7" sind durch ihre offenen Enden gut umformbar. Sie können auch wie in Figur 6b dargestellt ausgebildet sein und dann mit Gleitschuhen 19 abgedichtet sein.FIGS. 5a and 5b show a cross section and a perspective view a fourth type of stator 4. The web walls 7, 7 ', 7 "are as in formed the stator 4 retracted webs. They form with the in the circumferential direction extending walls 8, 8 ', 8 ", 9, 9', 9" of this stator 4 at the same time a part of the housing 13. Particularly advantageous in this embodiment, that through the remaining, closed annular surface, the circular outer wall 18, the housing 13 with the exception of the end wall 5 can be saved can. As a front wall 5, the sealing disc 14 (Figure 1) can be used, which is inserted on the front side of the stator 4 and the edge, for example can be crimped. From the circular outer wall 18 arise through For example, punching the web walls 7, 7 'then bent inward are. The web walls 7, 7 ', 7 "are well formed by their open ends. They can also be designed as shown in FIG. 6b and then with Sliding shoes 19 to be sealed.

    Die Figuren 6a und 6b zeigen eine perspektivische Ansicht eines Teils eines fünften und sechsten Stators 4, die Varianten des fünften Stators 4 darstellen. Die Stegwände 7, 7' sind einmal nach innen, das andere Mal nach außen gebogen. Diese Statorvarianten 4 werden deshalb in ein Gehäuse 13 eingesetzt. Die Stegwände 7,7' werden jeweils durch Gleitschuhe 19 (Figur 6b) abgedichtet. Letztere stützen die Stegwände 7,7' ab und verhindern ein Verformen durch eingebrachte externe Radialkräfte.Figures 6a and 6b show a perspective view of a part of a fifth and sixth stator 4, the variants of the fifth stator 4 represent. The web walls 7, 7 'are bent once inwards, the other times outwards. These stator variants 4 are therefore inserted into a housing 13. The web walls 7, 7 'are each sealed by sliding shoes 19 (FIG. 6 b). The latter support the web walls 7, 7 'and prevent deformation by external radial forces introduced.

    Zusammenfassend ergibt sich durch die spanlos hergestellten Bauteile, insbesondere durch wesentliche Teile des Stators 4, eine große Massereduzierung der Vorrichtung. Eine ähnliche Steifigkeit wie bei den Vorrichtungen des Standes der Technik wird durch die dargestellten Ausführungsformen des Stators 4 erreicht. Gleichzeitig werden die Leckageverluste gemindert, da auf poröse Sinterbauteile bzw. auf eine aufwändige Wasserdampfbehandlung oder Kunstharzimprägnierung verzichtet werden kann. In summary, results from the non-cutting produced components, in particular through substantial parts of the stator 4, a large mass reduction the device. A similar rigidity as in the devices of the state The technique is illustrated by the illustrated embodiments of the stator. 4 reached. At the same time, the leakage losses are reduced because of porous Sintered components or on a complex steam treatment or resin impregnation can be waived.

    BezugszahlenlisteLIST OF REFERENCE NUMBERS

    11
    hydraulische Vorrichtung zur Drehwinkelverstellunghydraulic device for adjusting the angle of rotation
    22
    Nockenwellecamshaft
    33
    Antriebsraddrive wheel
    44
    Statorstator
    55
    Stirnwandbulkhead
    66
    Rotorrotor
    7, 7', 7"7, 7 ', 7 "
    Stegwändeweb walls
    8, 8', 8"8, 8 ', 8 "
    äußere, in Umfangsrichtung verlaufende Wändeouter, circumferentially extending walls
    9,9',9"9,9 ', 9 "
    innere, in Umfangsrichtung verlaufende Wändeinner, circumferentially extending walls
    1010
    Flügelwing
    11, 11', 11"11, 11 ', 11 "
    erste Druckkammernfirst pressure chambers
    12, 12', 12"12, 12 ', 12 "
    zweite Druckkammernsecond pressure chambers
    1313
    Außengehäuseouter casing
    1414
    Dichtscheibesealing washer
    15, 15', 15"15, 15 ', 15 "
    Hohlkammern oder EinschnitteHollow chambers or incisions
    1616
    Element zur VerstellwinkelbegrenzungElement for adjustment angle limitation
    1717
    Kulissescenery
    1818
    kreisrunde Außenwandcircular outer wall
    1919
    Gleitschuhshoe
    2020
    erster, radial verlaufender Teil der Stegwandfirst, radially extending part of the web wall
    2121
    axiale Zentralschraubeaxial central screw

    Claims (18)

    Brennkraftmaschine mit einer hydraulischen Vorrichtung (1) zur Drehwinkelverstellung einer Nockenwelle (2) gegenüber einer Kurbelwelle, umfassend: Einen Rotor (6) mit daran angeordneten Flügeln (10), der drehfest mit der Nockenwelle (2) verbunden ist, einen an zumindest einer Stirnseite mit einer Stirnwand (5) versehenen, im wesentlichen eine zylindrische Außenkontur aufweisenden Stator (4), der drehfest mit einem von der Kurbelwelle angetriebenen Antriebsrad (3) verbunden ist, wobei beiderseits der Flügel (10) Druckkammern (11, 11', 11", 12, 12', 12") vorgesehen sind, die jeweils durch Stegwände (7, 7', 7") und innere (9, 9', 9") sowie äußere (8, 8', 8"), in Umfangsrichtung, konzentrisch zueinander verlaufende Wände des Stators (4) begrenzt sind und über ein Hydrauliksystem mit Hydraulikflüssigkeit druckbeaufschlagbar oder entleerbar sind, dadurch gekennzeichnet, dass der Stator (4), insbesondere seine Stegwände (7, 7', 7") und seine inneren sowie äußeren, in Umfangsrichtung verlaufenden Wände (8, 8', 8", 9, 9', 9"), als spanlos hergestelltes Band- oder Blechteil ausgebildet ist.Internal combustion engine having a hydraulic device (1) for adjusting the rotational angle of a camshaft (2) with respect to a crankshaft, comprising: a rotor (6) with vanes (10) arranged thereon, which is non-rotatably connected to the camshaft (2), one on at least one end face provided with an end wall (5), substantially cylindrical outer contour having a stator (4) rotatably connected to a driven by the crankshaft drive wheel (3), both sides of the wing (10) pressure chambers (11, 11 ', 11 " , 12, 12 ', 12 ") are provided, in each case by web walls (7, 7', 7") and inner (9, 9 ', 9 ") and outer (8, 8', 8"), in the circumferential direction , concentrically extending walls of the stator (4) are limited and can be pressurized or emptied via a hydraulic system with hydraulic fluid, characterized in that the stator (4), in particular its web walls (7, 7 ', 7 ") and its inner and outer , in circumferential direction ung running walls (8, 8 ', 8 ", 9, 9', 9"), formed as a chipless manufactured strip or sheet metal part. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass der Stator (4) an besonders belasteten Stellen lokal, entlang den Belastungsrichtungen durch Ausformungen, Sicken oder entsprechende Profilierungen verstärkt ist.Apparatus according to claim 1, characterized in that the stator (4) is reinforced at particularly stressed points locally, along the load directions by formations, beads or corresponding profiles. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass der Stator (4) ein vorzugsweise rohrförmiges und als Blechteil ausgebildetes Außengehäuse (13) aufweist, das die Stegwände (7, 7', 7") und die äußeren (8, 8', 8") sowie inneren (9, 9', 9") Wände in Umfangsrichtung umfasst.Apparatus according to claim 1, characterized in that the stator (4) has a preferably tubular and formed as a sheet metal part outer housing (13), the web walls (7, 7 ', 7 ") and the outer (8, 8', 8" ) and inner (9, 9 ', 9 ") walls in the circumferential direction. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Teile Stator (4), Gehäuse (13) und Antriebsrad (3) durch Verbindungstechnologien der Umformtechnik, beispielsweise Rändeln, Bördeln, Schweißen, Verstemmen, Vernieten, Kleben oder umgebogene Haltenasen aneinander befestigt sind.Apparatus according to claim 1, characterized in that the parts stator (4), housing (13) and drive wheel (3) by connection technologies of the forming technology, such as knurling, flanging, welding, caulking, riveting, gluing or bent retaining lugs are attached to each other. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Druckkammern (11, 11', 11", 12, 12', 12") stirnseitig durch eine kreisringförmige, als Blechteil ausgebildete Dichtscheibe (14) verschlossen sind.Apparatus according to claim 1, characterized in that the pressure chambers (11, 11 ', 11 ", 12, 12', 12") are closed at the end by an annular, designed as a sheet metal part sealing disc (14). Vorrichtung nach Anspruch 5, dadurch gekennzeichnet, dass die Dichtscheibe (14) mit der Stirnwand (5) fest verbunden ist, welche einteilig mit dem Außengehäuse (13) ausgebildet ist.Apparatus according to claim 5, characterized in that the sealing disc (14) with the end wall (5) is fixedly connected, which is formed integrally with the outer housing (13). Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass im Rotor (6) ein Element (16) zur Verstellwinkelbegrenzung angeordnet ist, welches in eine korrespondierende Kulisse (17) eingreift.Apparatus according to claim 1, characterized in that in the rotor (6) an element (16) is arranged for Verstellwinkelbegrenzung, which engages in a corresponding link (17). Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass der Stator (4) aus abwechselnd äußeren, in Umfangsrichtung verlaufenden Wänden (8, 8', 8") und inneren, in Umfangsrichtung verlaufenden Wänden (9, 9', 9"), welche jeweils Abschnitte eines Kreiszylinders sind, besteht, wobei jeweils benachbarte äußere (8, 8', 8") und innere (9, 9', 9"), in Umfangsrichtung verlaufende Wände durch Stegwände (7, 7', 7") verbunden sind, welche gemeinsam mit einem kreisförmigen, in den Stator eingesetzten Rotor (6) und den darin angeordneten Flügeln (10) Druckkammern (11, 11', 11", 12, 12', 12") bilden und an ihren von den Druckkammern abgewandten Seiten Hohlräume oder Einschnitte (15, 15', 15") bilden.Apparatus according to claim 1, characterized in that the stator (4) consists of alternately outer, circumferentially extending walls (8, 8 ', 8 ") and inner, circumferentially extending walls (9, 9', 9"), respectively Are sections of a circular cylinder consists, wherein in each case adjacent outer (8, 8 ', 8 ") and inner (9, 9', 9"), circumferentially extending walls by web walls (7, 7 ', 7 ") are connected, which, together with a circular rotor (6) inserted into the stator and the vanes (10) arranged therein, form pressure chambers (11, 11 ', 11 ", 12, 12', 12") and have cavities on their sides facing away from the pressure chambers or incisions (15, 15 ', 15 ") form. Vorrichtung nach Anspruch 8, dadurch gekennzeichnet, dass die Hohlräume oder Einschnitte (15, 15', 15") mit Metallschäumen gefüllt sind oder mit Kunststoff um- oder ausgespritzt sind.Apparatus according to claim 8, characterized in that the cavities or incisions (15, 15 ', 15 ") are filled with metal foams or with plastic or injected. Vorrichtung nach Anspruch 8, dadurch gekennzeichnet, dass die Stegwände (7, 7', 7") derart verlaufen oder ausgebildet sind, dass die Flügel (10) in den Endstellungen an die Stegwände (7, 7', 7") entweder nur an ihrem radial äußeren, nur an ihrem radial inneren Ende oder nur in einem mittleren Bereich anschlagen.Apparatus according to claim 8, characterized in that the web walls (7, 7 ', 7 ") run or are formed such that the wings (10) in the end positions of the web walls (7, 7', 7") either only on strike its radially outer, only at its radially inner end or only in a central region. Vorrichtung nach Anspruch 8, dadurch gekennzeichnet, dass die Stegwände (7, 7', 7") aus der Umfangswand eines Außenzylinders oder Innenzylinders paarweise als nach innen eingezogene oder nach außen ausgezogene Stege gebildet sind.Apparatus according to claim 8, characterized in that the web walls (7, 7 ', 7 ") from the peripheral wall of an outer cylinder or inner cylinder are formed in pairs as retracted or withdrawn outwardly webs. Vorrichtung nach Anspruch 11, dadurch gekennzeichnet, dass die Stegwände (7, 7',7") aus der inneren oder äußeren Umfangswand des Stators (4) ausgestanzt sind und paarweise in radiale Richtung, nach außen oder innen, gebogen sind.Apparatus according to claim 11, characterized in that the web walls (7, 7 ', 7 ") are punched out of the inner or outer peripheral wall of the stator (4) and in pairs in the radial direction, outwardly or inwardly, are bent. Vorrichtung nach Anspruch 12, dadurch gekennzeichnet, dass die Stegwände (7, 7', 7") paarweise durch einen sie abstützenden Gleitschuh (19) verbunden sind und Hohlräume (15, 15', 15") bilden.Apparatus according to claim 12, characterized in that the web walls (7, 7 ', 7 ") are connected in pairs by a sliding shoe (19) supporting them and form cavities (15, 15', 15"). Vorrichtung nach Anspruch 13, dadurch gekennzeichnet, dass die Hohlräume (15, 15', 15") durch Metallschäumen gefüllt sind oder mit Kunststoff um- oder ausgespritzt sind.Apparatus according to claim 13, characterized in that the cavities (15, 15 ', 15 ") are filled by metal foams or molded or sprayed with plastic. Vorrichtung nach Anspruch 8, dadurch gekennzeichnet, dass die Stegwände (7, 7', 7") zur Radialen einen Winkel von 10° bis 30° bilden, so dass die Flügel in ihren Endstellungen nur die radial außen liegenden Enden der Stegwände (7, 7', 7") berühren.Apparatus according to claim 8, characterized in that the web walls (7, 7 ', 7 ") form an angle of 10 ° to 30 ° to the radial, so that the wings in their end positions only the radially outer ends of the web walls (7, 7 ', 7 "). Brennkraftmaschine mit einer hydraulischen Vorrichtung (1) zur Drehwinkelverstellung einer Nockenwelle (2) gegenüber einer Kurbelwelle, umfassend: Einen Rotor (6) mit daran angeordneten Flügeln (10), der drehfest mit der Nockenwelle (2) verbunden ist, einen an zumindest einer Stirnseite mit einer Stirnwand (5) versehenen, im wesentlichen eine zylindrische Außenkontur aufweisenden Stator (4), der drehfest mit einem von der Kurbelwelle angetriebenen Antriebsrad (3) verbunden ist, wobei beiderseits der Flügel (10) Druckkammern (11, 11', 11", 12, 12', 12") vorgesehen sind, die jeweils durch Stegwände (7, 7', 7") und innere (9, 9', 9") sowie äußere (8, 8', 8"), in Umfangsrichtung, konzentrisch zueinander verlaufende Wände des Stators (4) begrenzt sind und über ein Hydrauliksystem mit Hydraulikflüssigkeit druckbeaufschlagbar oder entleerbar sind, dadurch gekennzeichnet, dass der Stator (4) einschließlich seiner Stegwände (7, 7', 7") und seiner äußeren (8, 8', 8") und inneren (9, 9', 9"), in Umfangsrichtung verlaufenden Wände und/oder ein ihn umfassendes Gehäuse (13) als spanlos hergestellte Blechteile ausgebildet sind.Internal combustion engine having a hydraulic device (1) for adjusting the rotational angle of a camshaft (2) with respect to a crankshaft, comprising: a rotor (6) with vanes (10) arranged thereon, which is non-rotatably connected to the camshaft (2), one on at least one end face provided with an end wall (5), substantially cylindrical outer contour having a stator (4) rotatably connected to a driven by the crankshaft drive wheel (3), both sides of the wing (10) pressure chambers (11, 11 ', 11 " , 12, 12 ', 12 ") are provided, in each case by web walls (7, 7', 7") and inner (9, 9 ', 9 ") and outer (8, 8', 8"), in the circumferential direction , concentrically extending walls of the stator (4) are limited and can be pressurized or emptied via a hydraulic system with hydraulic fluid, characterized in that the stator (4) including its web walls (7, 7 ', 7 ") and its outer (8, 8 ', 8 ") and inner (9 , 9 ', 9 "), extending in the circumferential direction walls and / or a housing comprising it (13) are formed as non-cutting produced sheet metal parts. Vorrichtung nach Anspruch 16, dadurch gekennzeichnet, dass die Druckkammern (11, 11', 11", 12, 12', 12") stirnseitig durch eine kreisringförmige, als Blechteil ausgebildete Dichtscheibe (14) verschlossen sind.Apparatus according to claim 16, characterized in that the pressure chambers (11, 11 ', 11 ", 12, 12', 12") are closed at the end by an annular, designed as a sheet metal part sealing disc (14). Vorrichtung nach Anspruch 17, dadurch gekennzeichnet, dass die Dichtscheibe (14) mit der Stirnwand (5) fest verbunden ist, welche einteilig mit dem Gehäuse (13) ausgebildet ist.Apparatus according to claim 17, characterized in that the sealing disc (14) with the end wall (5) is fixedly connected, which is formed integrally with the housing (13).
    EP04026407A 2003-12-16 2004-11-06 Internal combustion engine with hydraulic camshaft phasing device Expired - Lifetime EP1544420B1 (en)

    Applications Claiming Priority (2)

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    DE10358888 2003-12-16
    DE10358888.4A DE10358888B4 (en) 2003-12-16 2003-12-16 Internal combustion engine with a hydraulic device for adjusting the rotational angle of a camshaft relative to a crankshaft

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    EP1544420A2 true EP1544420A2 (en) 2005-06-22
    EP1544420A3 EP1544420A3 (en) 2008-08-27
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    JP (1) JP4608300B2 (en)
    KR (1) KR101119457B1 (en)
    CN (1) CN100439663C (en)
    AT (1) ATE475783T1 (en)
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    US20050155567A1 (en) 2005-07-21
    KR20050061354A (en) 2005-06-22
    CN1629453A (en) 2005-06-22
    KR101119457B1 (en) 2012-03-15
    JP4608300B2 (en) 2011-01-12
    JP2005180434A (en) 2005-07-07
    EP1544420A3 (en) 2008-08-27
    EP1544420B1 (en) 2010-07-28
    BRPI0406256B1 (en) 2017-04-04
    ATE475783T1 (en) 2010-08-15
    DE10358888B4 (en) 2018-12-27
    DE10358888A1 (en) 2005-07-21
    CN100439663C (en) 2008-12-03
    RU2004136796A (en) 2006-05-27
    BRPI0406256A (en) 2005-09-06
    RU2353782C2 (en) 2009-04-27
    US7284516B2 (en) 2007-10-23
    DE502004011438D1 (en) 2010-09-09

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