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EP1561012B1 - Rotary actuator system for controlling the stroke of gas exchange valves in the cylinder head of an internal combustion engine - Google Patents

Rotary actuator system for controlling the stroke of gas exchange valves in the cylinder head of an internal combustion engine Download PDF

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Publication number
EP1561012B1
EP1561012B1 EP03795783A EP03795783A EP1561012B1 EP 1561012 B1 EP1561012 B1 EP 1561012B1 EP 03795783 A EP03795783 A EP 03795783A EP 03795783 A EP03795783 A EP 03795783A EP 1561012 B1 EP1561012 B1 EP 1561012B1
Authority
EP
European Patent Office
Prior art keywords
cylinder head
rotary actuator
gas exchange
head according
internal combustion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP03795783A
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German (de)
French (fr)
Other versions
EP1561012A2 (en
Inventor
Karl-Heinz Gaubatz
Johannes Meyer
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.)
Bayerische Motoren Werke AG
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Bayerische Motoren Werke AG
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Publication date
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Publication of EP1561012A2 publication Critical patent/EP1561012A2/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/02Valve drive
    • F01L1/04Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
    • F01L1/08Shape of cams
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L9/00Valve-gear or valve arrangements actuated non-mechanically
    • F01L9/20Valve-gear or valve arrangements actuated non-mechanically by electric means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L2305/00Valve arrangements comprising rollers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L9/00Valve-gear or valve arrangements actuated non-mechanically
    • F01L9/20Valve-gear or valve arrangements actuated non-mechanically by electric means
    • F01L9/22Valve-gear or valve arrangements actuated non-mechanically by electric means actuated by rotary motors

Definitions

  • the invention relates to a rotary actuator device for stroke control of at least two identical gas exchange valves in a cylinder head of an internal combustion engine according to the features in the preamble of patent claim 1.
  • a valve train for an internal combustion engine which is designed as a spring-mass vibration system. It consists essentially of a swivel motor with a longitudinally extending in the cylinder head shaft, and a lever-like exciter device for each gas exchange valve.
  • the exciter devices can be coupled to the shaft in accordance with the operating state of the internal combustion engine.
  • the swivel motor only performs a pivoting movement in the sense of a stroke of the gas exchange valves.
  • the shaft and the exciter devices which can be coupled thereto are virtually a camshaft with releasable cams. At the end of each cam, at the point of contact with the gas exchange valve, a roller is arranged to minimize friction.
  • the valve train has two mutually point mirrored swivel motors, each with associated camshaft for all the same gas exchange valves.
  • Object of the present invention is therefore to reduce the moving masses in a generic valve train.
  • the moving masses are reduced in the valve train.
  • the reduction in mass also reduces the resulting moments and thus the mechanical load on the entire valve train, as a result of which higher rotational speeds are possible.
  • the internal friction of the valve train is substantially reduced, whereby the fuel consumption of the internal combustion engine decreases.
  • the embodiment according to the claims 5 to 7 serves to reduce friction in the valve train with simultaneous backlash of the valve train components.
  • the support of the power transmission element, on the one hand on a hydraulic valve clearance compensation element and on the other hand on a gas exchange valve reduces the moving masses, since in this arrangement, the hydraulic valve clearance compensation element can be arranged in the cylinder head, whereby at the same time a safe and simple oil supply is ensured,
  • the cup in the embodiment according to the invention is completely eliminated, whereby this mass is eliminated from the moving valve train.
  • the axes of the spark plug holes in the extension region of a device can be entangled against each other in order to maintain good insertion and removal conditions of the ignition device, such as. a spark plug to obtain the smallest possible compact unit for the rotary actuator device.
  • the size of a device is again significantly reduced by this measure in the modular structure.
  • Fig. 1 shows a schematic plan view of two inlet and outlet side on a cylinder head 4, an internal combustion engine, not shown, built rotary actuator devices 1, 1a, for the stroke control of four equivalent gas exchange valves 2, 2 ', 3, 3'.
  • the structure consists essentially of the first rotary actuator device 1 and the second, for the first parallel shifted, rotary actuator device 1a.
  • the first bore 10 and the second bore 10 'are each arranged centrally to a cylinder, not shown.
  • the first bore 10 and the second bore 10 ' serve to receive an ignition device, not shown, for each cylinder.
  • the rotary actuator devices 1, 1a are identical and differ only by the location of the obstruction.
  • the rotary actuator device 1 is provided for an intake side, the rotary actuator device 1 a for an exhaust side of the internal combustion engine. In the following, only the rotary actuator device 1 will be explained in more detail, since all information can be transferred to the second rotary actuator device 1a.
  • the rotary actuator device 1 essentially has a first and a second, point-mirrored, half rotary actuator device 14, 14 'for the stroke control of two identical gas exchange valves.
  • the first half Drehaktor device 14 consists of a first pivot motor 5 with a stationary first shaft 6, to which two first actuating elements 7, 7a are arranged stationary.
  • the first actuating elements 7, 7a here cams, interact with a respective first force transmission element 8, 8a.
  • the power transmission elements 8, 8a are supported on one side each on a first clearance compensation element 9, 9a and on the opposite side in each case on a first gas exchange valve 2, 2 'from.
  • This consists of a second pivot motor 5 ', with a stationary second shaft 6'.
  • two further second actuating elements 7', 7a ' are arranged stationary. These are in interaction with two second power transmission elements 8 ', 8a', which in turn on the one hand to two second clearance compensation elements 9, 9a 'and on the other hand on two second gas exchange valves 3, 3' are supported.
  • the rotary actuator device 1, consisting of the first and the second half rotary actuator device 14, 14 ' is provided for two cylinders of the internal combustion engine.
  • Each half rotary actuator device 14, 14 ' actuates two identical gas exchange valves, here the inlet gas exchange valves for two cylinders of the internal combustion engine.
  • a half Drehaktor device 14, 14 ' may be provided only for a single gas exchange valve. Also, the use of a half Drehaktor device 14, 14 'for two cylinders, each with only one gas acting equivalent valve is possible.
  • first gas exchange valves 2, 2 'and the second gas exchange valves 3, 3' on a line, whereby the first shaft 6 and the second shaft 6 'and the first and second half Drehaktor device 14, 14' in parallel aligned with each other.
  • the gas exchange valves can also assume a different position, whereby slightly different geometric arrangements are conceivable.
  • the first power transmission elements 8, 8a and the second power transmission elements 8 ', 8a' are rocker arms, however, it is also possible to use rocker arms or roller rocker arms.
  • the first clearance compensation elements 9, 9a and the second clearance compensation elements 9 ', 9a' are hydraulic valve clearance compensation elements, which are preferably incorporated directly into the cylinder head 4. As a result, a simple hydraulic supply is possible. All features that are shown for the rotary actuator device 1, also apply to the second rotary actuator device 1a.
  • Fig. 2 shows a schematic side view of the two rotary actuator device 1, 1a. Between the rotary actuator device 1 and the second rotary actuator device 1a is the first bore 10, for a not shown ignition device for the first cylinder. As under Fig. 1 already described the two rotary actuator devices 1 and 1 a are identical and point-only mirrored to each other, only the rotary actuator device 1 will be explained in more detail below again.
  • an inlet gas exchange valve Above the valve stem end of the gas exchange valve 3, an inlet gas exchange valve, are juxtaposed the first half rotary anchor device 14, proximate to the first bore 10, and the second half rotary anchor device 14 ', further spaced from the first bore 10, on the cylinder head 4 attached.
  • the actuating element 7a ' rests on the schematically illustrated first force transmission element 8a'.
  • the power transmission element 8a ' is supported on the one hand on the clearance compensation element 9a' and on the other hand on the gas exchange valve 3, which is mounted in the cylinder head 4.
  • the gas exchange valve 3 is shown in the open position and closes in a closed position an intake passage 15 in the cylinder head 4.
  • the corresponding outlet gas exchange valve 2 is also shown in the open position and closes in the closed position an exhaust passage 16 in the cylinder head 4th
  • the enclosure is preferably greater than 180 °, but always less than 360 °, whereby the mutually parallel shafts 6, 6 'structurally closer.
  • This arrangement brings not only package advantages but also weight advantages.
  • a further reduction in size is possible because the first bore 10 with the first axis 11 and the second bore 10 'with the second axis 11' are interlocked with each other, since in the embodiment according to the invention on the inlet side and on the outlet side a gas exchange valve and a clearance compensation element, respectively which have different space requirements.

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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)

Abstract

The invention relates to a rotary actuator system (1, 1a) for controlling the stroke of at least two gas exchange valves (2, 2', 3, 3') with an identical action in a cylinder head (4) of an internal combustion engine. Said system consists of a first pivoting motor (5), equipped with a first shaft (6), on which at least one first actuating element (7, 7a) is located and a second pivoting motor (5 ), equipped with a second shaft (6'), on which at least one second actuating element (7', 7a') is located. One actuating element (7, 7a, 7', 7a') is provided for at least one gas exchange valve (2, 2', 3, 3') and the first and second pivoting motors (5, 5') are point-symmetrical. A force transmission element (8, 8a, 8', 8a') is located between the actuating element (7, 7a, 7', 7a') and the gas exchange valve (2, 2', 3, 3'). The inventive configuration in the valve train reduces the masses that are displaced, permitting higher speeds during the operation of the internal combustion engine.

Description

Die Erfindung betrifft eine Drehaktor-Vorrichtung zur Hubsteuerung von zumindest zwei gleichwirkenden Gaswechselventilen in einem Zylinderkopf einer Brennkraftmaschine gemäß den Merkmalen im Oberbegriff des Patentanspruchs 1.The invention relates to a rotary actuator device for stroke control of at least two identical gas exchange valves in a cylinder head of an internal combustion engine according to the features in the preamble of patent claim 1.

Sie geht von der deutschen Offenlegungsschrift DE 198 25 964 A1 aus. In dieser wird ein Ventiltrieb für eine Brennkraftmaschine vorgeschlagen, der als Feder-Masse-Schwingungssystem ausgebildet ist. Er besteht im Wesentlichen aus einem Schwenkmotor mit einer längs im Zylinderkopf verlaufenden Welle, sowie einer hebelartigen Erregervorrichtung für jedes Gaswechselventil. Die Erregervorrichtungen sind entsprechend dem Betriebszustand der Brennkraftmaschine mit der Welle koppelbar. Der Schwenkmotor führt lediglich eine Schwenkbewegung im Sinne eines Hubes der Gaswechselventile aus. Bei der Welle und den daran koppelbaren Erregervorrichtungen handelt es sich quasi um eine Nockenwelle mit lösbaren Nocken. Am Ende eines jeden Nockens, am Berührpunkt zum Gaswechselventil, ist zur Reibungsminimierung eine Rolle angeordnet. Der Ventiltrieb weist für alle gleichwirkenden Gaswechselventile zwei zueinander punktgespiegelte Schwenkmotoren mit jeweils zugehöriger Nockenwelle auf.It starts from the German publication DE 198 25 964 A1 out. In this, a valve train for an internal combustion engine is proposed, which is designed as a spring-mass vibration system. It consists essentially of a swivel motor with a longitudinally extending in the cylinder head shaft, and a lever-like exciter device for each gas exchange valve. The exciter devices can be coupled to the shaft in accordance with the operating state of the internal combustion engine. The swivel motor only performs a pivoting movement in the sense of a stroke of the gas exchange valves. The shaft and the exciter devices which can be coupled thereto are virtually a camshaft with releasable cams. At the end of each cam, at the point of contact with the gas exchange valve, a roller is arranged to minimize friction. The valve train has two mutually point mirrored swivel motors, each with associated camshaft for all the same gas exchange valves.

Nachteilig an der beschriebenen Ausführung sind die großen Massenkräfte und die daraus resultierenden Momente, die die maximale Drehzahl der Brennkraftmaschine begrenzen.A disadvantage of the described embodiment, the large inertial forces and the resulting moments that limit the maximum speed of the internal combustion engine.

Aufgabe der vorliegenden Erfindung ist es daher, die bewegten Massen in einem gattungsgemäßen Ventiltrieb zu reduzieren.Object of the present invention is therefore to reduce the moving masses in a generic valve train.

Diese Aufgabe wird durch die Merkmale im kennzeichnenden Teil des Patentanspruchs 1 gelöst.
In vorteilhafter Weise werden bei einer Ausgestaltung gemäß Patentanspruch 1 die bewegten Massen im Ventiltrieb reduziert. Durch die Massenreduzierung werden auch die hieraus resultierenden Momente und somit die mechanische Belastung des gesamten Ventiltriebs reduziert, wodurch höhere Drehzahlen möglich sind. Darüber hinaus wird die innere Reibung des Ventiltriebs wesentlich verringert, wodurch der Brennstoffverbrauch der Brennkraftmaschine sinkt.
This object is solved by the features in the characterizing part of patent claim 1.
Advantageously, in an embodiment according to claim 1, the moving masses are reduced in the valve train. The reduction in mass also reduces the resulting moments and thus the mechanical load on the entire valve train, as a result of which higher rotational speeds are possible. In addition, the internal friction of the valve train is substantially reduced, whereby the fuel consumption of the internal combustion engine decreases.

Bei der Ausgestaltung gemäß Patentanspruch 2 entsteht eine kompakte kleine Antriebseinheit für zwei Zylinder. Diese Einheit kann in Verbindung mit Patentanspruch 9 zu einem modularen Konzept ausgebaut werden, so dass diese Einheit für jede Brennkraftmaschine einsetzbar ist, deren Zylinderzahl pro Zylinderreihe durch 2 teilbar ist. Eine selektive bauliche Anpassung an die jeweilige Brennkraftmaschine ist bei dieser modularen Bauweise nicht notwendig.In the embodiment according to claim 2 creates a compact small drive unit for two cylinders. This unit can be expanded in conjunction with claim 9 to a modular concept, so that this unit can be used for any internal combustion engine whose number of cylinders per cylinder row is divisible by 2. A selective structural adaptation to the respective internal combustion engine is not necessary in this modular design.

Dieser modulare Aufbau wird in Patentanspruch 3 nochmals weiter ausgeführt. Bei dieser Ausgestaltungsvariante werden sowohl die Einlass- als auch die Auslassseite der einzelnen Zylinderpaare mit den gleichen modularen Baugruppen aufgebaut. Durch diese Maßnahme werden die Herstellkosten gesenkt.This modular structure is further elaborated in claim 3. In this embodiment variant, both the inlet and the outlet side of the individual cylinder pairs are constructed with the same modular assemblies. By this measure, the production costs are reduced.

Besonders hervorzuheben ist bei Patentanspruch 4, dass bei einer beidseitigen Verbauung der Ventiltriebsvorrichtung, sowohl einlass- als auch auslassseitig, nur eine Parallelverschiebung der Drehaktor-Vorrichtung durchgeführt werden muss. Weitere Anpassungsarbeiten am Zylinderkopf sind nicht notwendig.Particularly noteworthy is in claim 4, that in a two-sided obstruction of the valve drive device, both inlet and outlet side, only a parallel displacement of the rotary actuator device must be performed. Further adaptation work on the cylinder head is not necessary.

Die Ausgestaltung gemäß der Patentansprüche 5 bis 7 dient der Verringerung von Reibung im Ventiltrieb bei gleichzeitiger Spielfreiheit der Ventiltriebsbauteile. Die Abstützung des Kraftübertragungselementes, einerseits auf einem hydraulischen Ventilspielausgleichselement und andererseits auf einem Gaswechselventil, reduziert die bewegten Massen, da bei dieser Anordnung das hydraulische Ventilspielausgleichselement im Zylinderkopf angeordnet werden kann, wodurch gleichzeitig eine sichere und einfache Ölversorgung gewährleistet ist, Gegenüber dem Stand der Technik, bei dem zwischen Drehmittel und Gaswechselventil ein Tassenstößel angeordnet ist, entfällt die Tasse bei der erfindungsgemäßen Ausgestaltung komplett, wodurch diese Masse aus dem bewegten Ventiltrieb entfällt.The embodiment according to the claims 5 to 7 serves to reduce friction in the valve train with simultaneous backlash of the valve train components. The support of the power transmission element, on the one hand on a hydraulic valve clearance compensation element and on the other hand on a gas exchange valve, reduces the moving masses, since in this arrangement, the hydraulic valve clearance compensation element can be arranged in the cylinder head, whereby at the same time a safe and simple oil supply is ensured, Compared to the prior art, in which a bucket tappet is arranged between the rotating means and gas exchange valve, the cup in the embodiment according to the invention is completely eliminated, whereby this mass is eliminated from the moving valve train.

Um eine kompakte Bauweise zu erzielen, können gemäß Patentanspruch 8 die Achsen der Zündkerzenbohrungen im Erstreckungsbereich einer Vorrichtung gegeneinander verschränkt werden, um bei unverändert guten Ein- und Ausbaubedingungen der Zündeinrichtung, wie z.B. einer Zündkerze, die kleinstmögliche kompakte Baueinheit für die Drehaktor-Vorrichtung zu erhalten. Die Baugröße einer Vorrichtung wird durch diese Maßnahme beim modularen Aufbau nochmals wesentlich verringert.In order to achieve a compact design, according to claim 8, the axes of the spark plug holes in the extension region of a device can be entangled against each other in order to maintain good insertion and removal conditions of the ignition device, such as. a spark plug to obtain the smallest possible compact unit for the rotary actuator device. The size of a device is again significantly reduced by this measure in the modular structure.

Eine weitere Reduzierung der Baugröße wird durch die Ausgestaltung gemäß Patentanspruch 10 erzielt, da bei einer derartigen Ausführung der den Rotor umgebenden Stator sich nicht über 360° radial am Umfang erstreckt. Durch diese Ausgestaltungsvariante wird die höchste Packungsdichte von Bauteilen erzielt.A further reduction of the size is achieved by the embodiment according to claim 10, since in such an embodiment, the stator surrounding the rotor does not extend over 360 ° radially on the circumference. By this design variant, the highest packing density of components is achieved.

Im Folgenden ist die Erfindung anhand eines bevorzugten Ausführungsbeispieles in zwei Figuren näher erläutert.

Fig. 1
zeigt eine schematische Darstellung einer Aufsicht auf zwei einlasssowie auslassseitig auf einem Zylinderkopf einer Brennkraftmaschine verbauten Drehaktor-Vorrichtung,
Fig. 2
zeigt eine schematische Darstellung einer Seitenansicht von zwei einlass- sowie auslassseitig auf einem Zylinderkopf einer Brennkraftmaschine verbauten Drehaktor-Vorrichtung.
In the following the invention with reference to a preferred embodiment is explained in more detail in two figures.
Fig. 1
shows a schematic representation of a plan view of two inlet and outlet side installed on a cylinder head of an internal combustion engine Drehaktor device,
Fig. 2
shows a schematic representation of a side view of two inlet and outlet side installed on a cylinder head of an internal combustion engine rotary actuator device.

Die Bezugszeichen in Fig. 1 gelten auch für dieselben Bauteile in Fig. 2.The reference numerals in Fig. 1 also apply to the same components in Fig. 2 ,

Fig. 1 zeigt eine schematische Aufsicht auf zwei einlass- sowie auslassseitig auf einem Zylinderkopf 4, einer nicht dargestellten Brennkraftmaschine, verbauten Drehaktor-Vorrichtungen 1, 1a, zur Hubsteuerung von jeweils vier gleichwirkenden Gaswechselventilen 2, 2', 3, 3'. Der Aufbau besteht im Wesentlichen aus der ersten Drehaktor-Vorrichtung 1 sowie der zweiten, zur ersten parallel verschobenen, Drehaktor-Vorrichtung 1a. Zwischen den Drehaktor-Vorrichtungen 1 und 1a sind, in dem nicht näher dargestellten Zylinderkopf 4, eine erste Bohrung 10 und eine zweite Bohrung 10' angeordnet. Die erste Bohrung 10 und die zweite Bohrung 10' sind jeweils mittig zu einem nicht dargestellten Zylinder angeordnet. Die erste Bohrung 10 und die zweite Bohrung 10' dienen zur Aufnahme einer nicht dargestellten Zündvorrichtung für jeden Zylinder. Die Drehaktor-Vorrichtungen 1, 1a sind baugleich und unterscheiden sich nur durch den Ort der Verbauung. Die Drehaktor-Vorrichtung 1 ist für eine Einlassseite, die Drehaktor-Vorrichtung 1a für eine Auslassseite der Brennkraftmaschine vorgesehen. Im Weiteren wird nur die Drehaktor-Vorrichtung 1 näher erläutert, da alle Angaben auf die zweite Drehaktor-Vorrichtung 1a übertragbar sind. Fig. 1 shows a schematic plan view of two inlet and outlet side on a cylinder head 4, an internal combustion engine, not shown, built rotary actuator devices 1, 1a, for the stroke control of four equivalent gas exchange valves 2, 2 ', 3, 3'. The structure consists essentially of the first rotary actuator device 1 and the second, for the first parallel shifted, rotary actuator device 1a. Between the rotary actuator devices 1 and 1a, in the cylinder head 4, not shown, a first bore 10 and a second bore 10 'are arranged. The first bore 10 and the second bore 10 'are each arranged centrally to a cylinder, not shown. The first bore 10 and the second bore 10 'serve to receive an ignition device, not shown, for each cylinder. The rotary actuator devices 1, 1a are identical and differ only by the location of the obstruction. The rotary actuator device 1 is provided for an intake side, the rotary actuator device 1 a for an exhaust side of the internal combustion engine. In the following, only the rotary actuator device 1 will be explained in more detail, since all information can be transferred to the second rotary actuator device 1a.

Die Drehaktor-Vorrichtung 1 weist im Wesentlichen eine erste und eine zweite, zueinander punktgespiegelte, halbe Drehaktor-Vorrichtung 14, 14' zur Hubsteuerung von zwei gleichwirkenden Gaswechselventilen auf. Die erste halbe Drehaktor-Vorrichtung 14 besteht aus einem ersten Schwenkmotor 5 mit einer ortsfesten ersten Welle 6, an die zwei erste Betätigungselemente 7, 7a ortsfest angeordnet sind. Die ersten Betätigungselemente 7, 7a, hier Nocken, stehen in Wechselwirkung mit jeweils einem ersten Kraftübertragungselement 8, 8a. Die Kraftübertragungselemente 8, 8a stützen sich auf einer Seite jeweils auf einem ersten Spielausgleichselement 9, 9a und auf der gegenüberliegenden Seite jeweils auf einem ersten Gaswechselventil 2, 2' ab. Dasselbe gilt auch für die zweite halbe Drehaktor-Vorrichtung 14'. Diese besteht aus einem zweiten Schwenkmotor 5', mit einer ortsfesten zweiten Welle 6'. An die zweite Welle 6' sind zwei weitere zweite Betätigungselemente 7', 7a' ortsfest angeordnet. Diese stehen in Wechselwirkung mit zwei zweiten Kraftübertragungselementen 8', 8a', die wiederum einerseits auf zwei zweiten Spielausgleichselementen 9, 9a' und andererseits auf zwei zweiten Gaswechselventilen 3, 3' abgestützt sind.The rotary actuator device 1 essentially has a first and a second, point-mirrored, half rotary actuator device 14, 14 'for the stroke control of two identical gas exchange valves. The first half Drehaktor device 14 consists of a first pivot motor 5 with a stationary first shaft 6, to which two first actuating elements 7, 7a are arranged stationary. The first actuating elements 7, 7a, here cams, interact with a respective first force transmission element 8, 8a. The power transmission elements 8, 8a are supported on one side each on a first clearance compensation element 9, 9a and on the opposite side in each case on a first gas exchange valve 2, 2 'from. The same applies to the second half rotary actuator device 14 '. This consists of a second pivot motor 5 ', with a stationary second shaft 6'. To the second shaft 6 ', two further second actuating elements 7', 7a 'are arranged stationary. These are in interaction with two second power transmission elements 8 ', 8a', which in turn on the one hand to two second clearance compensation elements 9, 9a 'and on the other hand on two second gas exchange valves 3, 3' are supported.

Im vorliegenden Ausführungsbeispiel ist die Drehaktor-Vorrichtung 1, bestehend aus der ersten und der zweiten halben Drehaktor-Vorrichtung 14, 14' für zwei Zylinder der Brennkraftmaschine vorgesehen. Jede halbe Drehaktor-Vorrichtung 14, 14' betätigt zwei gleichwirkende Gaswechselventile, hier die Einlass-Gaswechselventile für zwei Zylinder der Brennkraftmaschine. In einem weiteren Ausführungsbeispiel kann eine halbe Drehaktor-Vorrichtung 14, 14' auch nur für ein einzelnes Gaswechselventil vorgesehen sein. Auch die Verwendung einer halbe Drehaktor-Vorrichtung 14, 14' für zwei Zylinder, mit jeweils nur einem gleichwirkenden Gaswechselventil ist möglich.In the present embodiment, the rotary actuator device 1, consisting of the first and the second half rotary actuator device 14, 14 'is provided for two cylinders of the internal combustion engine. Each half rotary actuator device 14, 14 'actuates two identical gas exchange valves, here the inlet gas exchange valves for two cylinders of the internal combustion engine. In a further embodiment, a half Drehaktor device 14, 14 'may be provided only for a single gas exchange valve. Also, the use of a half Drehaktor device 14, 14 'for two cylinders, each with only one gas acting equivalent valve is possible.

Im vorliegenden Ausführungsbeispiel liegen die ersten Gaswechselventile 2, 2' und die zweiten Gaswechselventile 3, 3' auf einer Linie, wodurch die erste Welle 6 und die zweite Welle 6' bzw. die erste und die zweite halbe Drehaktor-Vorrichtung 14, 14' parallel zueinander ausgerichtet sind. In weiteren Varianten können die Gaswechselventile jedoch auch eine andere Lage einnehmen, wodurch geringfügig andere geometrische Anordnungen denkbar sind.In the present embodiment, the first gas exchange valves 2, 2 'and the second gas exchange valves 3, 3' on a line, whereby the first shaft 6 and the second shaft 6 'and the first and second half Drehaktor device 14, 14' in parallel aligned with each other. However, in other variants, the gas exchange valves can also assume a different position, whereby slightly different geometric arrangements are conceivable.

Die erste Welle 6 und die zweite Welle 6' sind Nockenwellen und die ersten Betätigungselemente 7, 7a und die zweiten Betätigungselemente 7', 7a' sind Nocken. Die ersten Kraftübertragungselemente 8, 8a und die zweiten Kraftübertragungselemente 8', 8a', sind Kipphebel, es können jedoch auch Schlepphebel oder Rollenschlepphebel eingesetzt werden. Die ersten Spielausgleichselemente 9, 9a und die zweiten Spielausgleichselemente 9', 9a' sind hydraulische Ventilspielausgleichselemente, die vorzugsweise direkt in den Zylinderkopf 4 eingearbeitet sind. Hierdurch ist eine einfache Hydraulikversorgung möglich. Alle Merkmale, die für die Drehaktor-Vorrichtung 1 dargestellt sind, gelten auch für die zweite Drehaktor-Vorrichtung 1a.The first shaft 6 and the second shaft 6 'are camshafts and the first actuators 7, 7a and the second actuators 7', 7a 'are cams. The first power transmission elements 8, 8a and the second power transmission elements 8 ', 8a', are rocker arms, however, it is also possible to use rocker arms or roller rocker arms. The first clearance compensation elements 9, 9a and the second clearance compensation elements 9 ', 9a' are hydraulic valve clearance compensation elements, which are preferably incorporated directly into the cylinder head 4. As a result, a simple hydraulic supply is possible. All features that are shown for the rotary actuator device 1, also apply to the second rotary actuator device 1a.

Fig. 2 zeigt eine schematische Seitenansicht der zwei Drehaktor-Vorrichtung 1, 1a. Zwischen der Drehaktor-Vorrichtung 1 und der zweiten Drehaktor-Vorrichtung 1a befindet sich die erste Bohrung 10, für eine nicht dargestellte Zündeinrichtung für den ersten Zylinder. Da wie unter Fig. 1 bereits beschrieben die zwei Drehaktor-Vorrichtungen 1 und 1 a baugleich und nur zueinander punktgespiegelt sind, wird im Folgenden wiederum nur die Drehaktor-Vorrichtung 1 näher erläutert. Fig. 2 shows a schematic side view of the two rotary actuator device 1, 1a. Between the rotary actuator device 1 and the second rotary actuator device 1a is the first bore 10, for a not shown ignition device for the first cylinder. As under Fig. 1 already described the two rotary actuator devices 1 and 1 a are identical and point-only mirrored to each other, only the rotary actuator device 1 will be explained in more detail below again.

Oberhalb des Ventilschaftendes des Gaswechselventils 3, einem Einlass-Gaswechselventil, sind nebeneinander die erste halbe Drehanker-Vorrichtung 14, in der Nähe zur ersten Bohrung 10, und die zweite halbe Drehanker-Vorrichtung 14', von der ersten Bohrung 10 weiter beabstandet, am Zylinderkopf 4 befestigt. Am ersten Schwenkmotor 5 ist ein erster Stator 12 und ein erster Rotor 13 erkennbar, am zweiten Schwenkmotor 5' ist nur der zweite Stator 12' erkennbar, dessen zweiter Rotor 13' ist von der zentrisch angeordneten zweiten Welle 6', sowie dem zweiten Betätigungselement 7a' verdeckt. Das Betätigungselement 7a' liegt auf dem schematisch dargestellten ersten Kraftübertragungselement 8a' auf. Das Kraftübertragungselement 8a' ist einerseits auf dem Spielausgleichselement 9a' und andererseits auf dem Gaswechselventil 3 abgestützt, welches im Zylinderkopf 4 gelagert ist. Das Gaswechselventil 3 ist in Offenstellung dargestellt und verschließt in einer Schließstellung einen Einlasskanal 15 im Zylinderkopf 4. Das korrespondierende Auslass-Gaswechselventil 2 ist ebenfalls in Offenstellung dargestellt und verschließt in Schließstellung einen Auslasskanal 16 im Zylinderkopf 4.Above the valve stem end of the gas exchange valve 3, an inlet gas exchange valve, are juxtaposed the first half rotary anchor device 14, proximate to the first bore 10, and the second half rotary anchor device 14 ', further spaced from the first bore 10, on the cylinder head 4 attached. On the first pivot motor 5, a first stator 12 and a first rotor 13 can be seen, on the second pivot motor 5 'only the second stator 12' can be seen, the second rotor 13 'is of the centrally disposed second shaft 6', and the second actuator 7a 'obscured. The actuating element 7a 'rests on the schematically illustrated first force transmission element 8a'. The power transmission element 8a 'is supported on the one hand on the clearance compensation element 9a' and on the other hand on the gas exchange valve 3, which is mounted in the cylinder head 4. The gas exchange valve 3 is shown in the open position and closes in a closed position an intake passage 15 in the cylinder head 4. The corresponding outlet gas exchange valve 2 is also shown in the open position and closes in the closed position an exhaust passage 16 in the cylinder head 4th

Um eine möglichst hohe Bauteildichte und somit eine kleine Baugröße zu erreichen, umschließen der erste Stator 12, bzw. der zweite Stator 12' den ersten Rotor 13 bzw. den zweiten Rotor 13' radial nicht am gesamten Umfang, sondern nur zu etwa 270°. Der Umschließungsgrad ist vorzugsweise größer als 180°, jedoch immer kleiner als 360°, wodurch die parallel zueinander verlaufenden Wellen 6, 6' baulich näher angeordnet sind. Diese Anordnung bringt neben Packagevorteilen auch Gewichtsvorteile. Eine weitere Baugrößenverkleinerung ist dadurch möglich, dass die erste Bohrung 10 mit der ersten Achse 11 und die zweite Bohrung 10' mit der zweiten Achse 11' zueinander verschränkt sind, da sich bei der erfindungsgemäßen Ausgestaltung einlassseitig und auslassseitig jeweils ein Gaswechselventil und ein Spielausgleichselement gegenüberliegen, die unterschiedliche Platzbedürfnisse haben.In order to achieve the highest possible component density and thus a small size, the first stator 12 or the second stator 12 'surround the first rotor 13 and the second rotor 13' radially not on the entire circumference, but only approximately 270 °. The enclosure is preferably greater than 180 °, but always less than 360 °, whereby the mutually parallel shafts 6, 6 'structurally closer. This arrangement brings not only package advantages but also weight advantages. A further reduction in size is possible because the first bore 10 with the first axis 11 and the second bore 10 'with the second axis 11' are interlocked with each other, since in the embodiment according to the invention on the inlet side and on the outlet side a gas exchange valve and a clearance compensation element, respectively which have different space requirements.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Drehaktor-VorrichtungRotary actuator device
1a1a
Zweite Drehaktor-VorrichtungSecond rotary actuator device
2, 2'2, 2 '
Erstes GaswechselventilFirst gas exchange valve
3, 3'3, 3 '
Zweites GaswechselventilSecond gas exchange valve
44
Zylinderkopfcylinder head
55
Erster SchwenkmotorFirst swing motor
5'5 '
Zweiter SchwenkmotorSecond swing motor
66
Erste WelleFirst wave
6'6 '
Zweite WelleSecond wave
7, 7a7, 7a
Erstes BetätigungselementFirst actuator
7', 7a'7 ', 7a'
Zweites BetätigungselementSecond actuator
8, 8a8, 8a
Erstes KraftübertragungselementFirst power transmission element
8', 8a'8 ', 8a'
Zweites KraftübertragungselementSecond power transmission element
9, 9a9, 9a
Erstes SpielausgleichselementFirst clearance compensation element
9', 9a'9 ', 9a'
Zweites SpielausgleichselementSecond clearance compensation element
1010
Erste BohrungFirst drilling
10'10 '
Zweite BohrungSecond hole
1111
Erste AchseFirst axle
11'11 '
Zweite AchseSecond axis
1212
Erster StatorFirst stator
12'12 '
Zweiter StatorSecond stator
1313
Erster RotorFirst rotor
13'13 '
Zweiter RotorSecond rotor
1414
Erste halbe DrehankervorrichtungFirst half rotary anchor device
14'14 '
Zweite halbe DrehankervorrichtungSecond half rotary anchor device
1515
Einlasskanalinlet channel
1616
Auslasskanalexhaust port

Claims (9)

  1. A cylinder head comprising a rotary actuator (1, 1a) for controlling the stroke of at least two equally acting gas change valves (2, 2', 3, 3') in a cylinder head (4) of an internal combustion engine, the actuator comprising a first swivel motor (5) with a first shaft (6) on which at least one first actuating element (7, 7a) is disposed and a second swivel motor (5') with a second shaft (6') on which at least one second actuating element (7', 7a') is disposed, wherein an actuating element (7, 7a, 7', 7a') is provided for at least one gas change valve (2, 2', 3, 3') and the first and the second swivel motor (5, 5') are disposed in point mirror arrangement,
    characterised in that a force transmitting element (8, 8a, 8', 8a') is disposed between the actuating element (7, 7a, 7', 7a') and the gas change valve (2,2', 3,3'), wherein the engine comprises at least one first cylinder with a first ignition device in a bore in the cylinder head and one second cylinder with a second ignition device in a bore in the cylinder head and wherein at least a first axis (11) of the first bore (10) crosses or overlaps a second axis (11') of the second bore (10').
  2. A cylinder head according to claim 1, wherein the engine has at least two cylinders,
    characterised in that at least one rotary actuator (1) is provided for two cylinders.
  3. A cylinder head according to claim 1 or claim 2, wherein each cylinder has an inlet side and an outlet side,
    characterised in that the inlet side is associated with at least one first actuator (1) and/or the outlet side is associated with at least one second actuator (1a).
  4. A cylinder head according to claim 3,
    characterised in that the second rotary actuator (1a) is offset in parallel with the first actuator (1).
  5. A cylinder head according to any of the previously-mentioned claims,
    characterised in that the force transmitting element (8, 8a, 8', 8a') is a drag lever or a roller drag lever or a rocker arm.
  6. A cylinder head according to any of the previously-mentioned claims,
    characterised in that the force transmitting element (8, 8a, 8', 8a') abuts a clearance compensating element (9, 9', 9a, 9a') on one side and a gas change valve (2, 2', 3, 3') on the other side.
  7. A cylinder head according to claim 6,
    characterised in that the clearance compensating element (9, 9', 9a, 9a') is a hydraulic valve clearance compensating element.
  8. A cylinder head according to any of the previously-mentioned claims,
    characterised in that at least two rotary actuators (1, 1a) are disposed in line with one another along a longitudinal axis of the engine.
  9. A cylinder head according to any of the previously-mentioned claims, wherein the swivel motor comprises a stator and a rotor,
    characterised in that the stator (12) extends at least 180 radially round the rotor (13).
EP03795783A 2002-11-14 2003-10-15 Rotary actuator system for controlling the stroke of gas exchange valves in the cylinder head of an internal combustion engine Expired - Lifetime EP1561012B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10252997 2002-11-14
DE10252997A DE10252997A1 (en) 2002-11-14 2002-11-14 Electrical actuator system for inlet and exhaust valves for internal combustion engine may control lift of four valves using two reciprocating actuator motors rotating cams engaging valves
PCT/EP2003/011408 WO2004044391A2 (en) 2002-11-14 2003-10-15 Rotary actuator system for controlling the stroke of gas exchange valves in the cylinder head of an internal combustion engine

Publications (2)

Publication Number Publication Date
EP1561012A2 EP1561012A2 (en) 2005-08-10
EP1561012B1 true EP1561012B1 (en) 2008-12-10

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP03795783A Expired - Lifetime EP1561012B1 (en) 2002-11-14 2003-10-15 Rotary actuator system for controlling the stroke of gas exchange valves in the cylinder head of an internal combustion engine

Country Status (4)

Country Link
US (1) US7007647B2 (en)
EP (1) EP1561012B1 (en)
DE (2) DE10252997A1 (en)
WO (1) WO2004044391A2 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005033653B3 (en) * 2005-07-19 2006-11-30 Dr.Ing.H.C. F. Porsche Ag Forcible valve drive for internal combustion engine has cam with axis of rotation at right angle to direction of lift movement
DE102006005943A1 (en) * 2006-02-09 2007-08-23 Bayerische Motoren Werke Ag Internal combustion engine with an electric valve train
DE102006013100A1 (en) * 2006-03-20 2007-09-27 Lsp Innovative Automotive Systems Gmbh Segment motor for valve train
DE102006023652B4 (en) * 2006-05-18 2008-10-30 Esa Patentverwertungsagentur Sachsen-Anhalt Gmbh Electromotive device for actuating gas exchange valves
GB2447034A (en) * 2007-02-28 2008-09-03 Dakota Ltd Gibraltar Camshaft Drive

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GB1201214A (en) * 1968-02-01 1970-08-05 Ford Motor Co Overhead camshaft internal combustion engine
DE3203791A1 (en) * 1982-02-04 1983-08-11 Volkswagenwerk Ag, 3180 Wolfsburg VALVE DRIVE, ESPECIALLY FOR A MOTOR VEHICLE INTERNAL COMBUSTION ENGINE
DE3210165A1 (en) * 1982-03-19 1983-09-29 Bayerische Motoren Werke AG, 8000 München VALVE DRIVE
DE3932293C1 (en) * 1989-09-28 1991-01-24 Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De
DE4212263A1 (en) * 1992-04-11 1993-10-14 Bayerische Motoren Werke Ag Actuating gear for lifting valves in IC engine - has valve lifter shaft, which is longitudinally displaced to couple neighbouring valve lifters via switching elements
JPH0726911A (en) * 1993-05-13 1995-01-27 Sumitomo Electric Ind Ltd Camshaft
DE4327068A1 (en) * 1993-08-12 1995-02-16 Bayerische Motoren Werke Ag Valve gear of an internal combustion engine
CA2122188A1 (en) * 1994-04-26 1995-10-27 Peter Hinsperger Fabric-vented greenhouse
JP3354314B2 (en) 1994-09-30 2002-12-09 本田技研工業株式会社 Engine camshaft support structure
DE19825964A1 (en) * 1998-06-10 1999-12-16 Schaeffler Waelzlager Ohg Valve drive for internal combustion engine
EP0979928A1 (en) * 1998-08-11 2000-02-16 Wenko AG Burgdorf Internal combustion engine with rocker operated valve drive
US6446589B1 (en) * 2001-01-16 2002-09-10 Chinh T. Nguyen Cam actuated continuous simultaneously variable valve timing and lifting assembly
DE10140461A1 (en) 2001-08-17 2003-02-27 Bayerische Motoren Werke Ag Rotary actuator device for stroke control of a gas exchange valve in the cylinder head of an internal combustion engine
US6722326B1 (en) * 2002-10-14 2004-04-20 Ford Global Technologies, Llc Variable lift cylinder valve system for internal combustion engine

Also Published As

Publication number Publication date
WO2004044391A2 (en) 2004-05-27
US7007647B2 (en) 2006-03-07
US20050211211A1 (en) 2005-09-29
EP1561012A2 (en) 2005-08-10
WO2004044391A3 (en) 2004-06-17
DE10252997A1 (en) 2004-05-27
DE50310913D1 (en) 2009-01-22

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