EP2670955B2 - Shaft such as camshaft comprising a hollow section - Google Patents
Shaft such as camshaft comprising a hollow section Download PDFInfo
- Publication number
- EP2670955B2 EP2670955B2 EP12703756.2A EP12703756A EP2670955B2 EP 2670955 B2 EP2670955 B2 EP 2670955B2 EP 12703756 A EP12703756 A EP 12703756A EP 2670955 B2 EP2670955 B2 EP 2670955B2
- Authority
- EP
- European Patent Office
- Prior art keywords
- camshaft
- hollow shaft
- protection device
- shaft section
- splash protection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000000926 separation method Methods 0.000 claims description 12
- 239000000853 adhesive Substances 0.000 claims description 5
- 230000001070 adhesive effect Effects 0.000 claims description 5
- 238000002347 injection Methods 0.000 description 6
- 239000007924 injection Substances 0.000 description 6
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000007599 discharging Methods 0.000 description 4
- 230000010006 flight Effects 0.000 description 3
- 230000033001 locomotion Effects 0.000 description 3
- 239000002245 particle Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
- F01L1/02—Valve drive
- F01L1/04—Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
- F01L1/047—Camshafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
- F01L1/46—Component parts, details, or accessories, not provided for in preceding subgroups
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M13/00—Crankcase ventilating or breathing
- F01M13/04—Crankcase ventilating or breathing having means for purifying air before leaving crankcase, e.g. removing oil
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B67/00—Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for
- F02B67/04—Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for of mechanically-driven auxiliary apparatus
- F02B67/06—Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for of mechanically-driven auxiliary apparatus driven by means of chains, belts, or like endless members
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
- F01L1/02—Valve drive
- F01L1/04—Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
- F01L1/047—Camshafts
- F01L2001/0475—Hollow camshafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
- F01L1/02—Valve drive
- F01L1/04—Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
- F01L1/047—Camshafts
- F01L2001/0476—Camshaft bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M13/00—Crankcase ventilating or breathing
- F01M13/04—Crankcase ventilating or breathing having means for purifying air before leaving crankcase, e.g. removing oil
- F01M2013/0422—Separating oil and gas with a centrifuge device
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2101—Cams
Definitions
- the invention relates to a camshaft with a hollow shaft section which has at least one radial inlet opening for discharging a gas through the hollow shaft section and with a splash protection device which is arranged in the area of the at least one radial inlet opening on the hollow shaft section.
- blowby gas In relation to internal combustion engines, it is therefore common to direct the blow-by gas that occurs in the valve chamber back into the intake tract of the internal combustion engine. In order, on the one hand, to minimize the loss of oil due to blow-by gas and, on the other hand, to ensure optimal combustion and minimal environmental impact, it is known to subject the blow-by gas to oil separation and to lead the separated oil back into the oil circuit.
- the blow-by gas is removed through the hollow shaft section, and an oil separator device can also be integrated directly into the hollow shaft section.
- oil is often present in a wide variety of droplet sizes in the area surrounding a camshaft.
- large oil droplets or oil splashes are also often observed in the vicinity of a camshaft.
- Such large droplets or splashes can form, for example, if there is an oil bath or oil foam in the area of the camshaft.
- a jet of oil hits the shaft and in particular the hollow shaft section with the inlet opening for discharging the blow-by gas.
- a camshaft with a hollow shaft section which has at least one radial inlet opening for discharging a gas through the hollow shaft section and with a splash protection device which is arranged in the area of the radial inlet opening on the hollow shaft section is from the EP 1 880 085 B1 known, with a pre-separator and a swirl generator integrated into the hollow shaft section being provided as a final separator on the outer circumference of the shaft for separating oil.
- the pre-separator is funnel-shaped and covers several radial inlet openings of the hollow shaft section in the radial direction.
- the splash protection effect is imperfect because oil droplets or jets that inject at an angle cannot be prevented.
- the pre-separator is also comparatively complex in design and requires a considerable amount of space.
- a lubrication system for a shaft with an oil separator device is from the US 4,714,139 known.
- a pump wheel which enables a certain amount of splash protection, is formed as an integral part of a shaft body, resulting in a relatively complex shape.
- the invention is based on the object of specifying a camshaft with a hollow shaft section and at least one radial inlet opening in the hollow shaft section, in which the injection of large oil droplets or oil jets into the at least one inlet opening is at least largely prevented by a structurally simple splash protection device .
- the object of the invention and solution to the problem is a camshaft according to claim 1.
- the projections When the shaft rotates, the projections generate a gas flow in the direction of rotation, which allows the injection of oil droplets or even the injection of an oil jet initially into the passage openings of the splash protection device and accordingly also prevented to at least a certain extent in the at least one inlet opening of the hollow shaft section. Furthermore, it must be taken into account that large oil droplets and splashes cannot follow the rotation of the splash guard to the same extent as the blow-by gas. As the shaft rotates, oil droplets and splashes are increasingly deposited on the projections due to their inertia, while the blow-by gas can follow the rotational movement and flow into the passage openings.
- the passage openings are, to a certain extent, sealed off from the comparatively sluggish oil droplets and splashes by the projections which are arranged between the passage openings.
- the efficiency of this isolation depends on the one hand on the shape of the projections, in particular their height and orientation, and on the other hand on the volume flow of the blowby gas. As the volume flow of the blow-by gas increases, it may no longer be possible to completely prevent larger oil droplets from being carried along and ending up in the hollow shaft section. Nevertheless, the design of the camshaft according to the invention with the splash protection device described is characterized by a very efficient and extensive separation of larger oil particles. Even if the camshaft or even the splash guard is partially immersed in an oil bath, the ingress of oil can be effectively prevented. In practice, an oil bath in the area of a camshaft can occur when an engine is under extreme load, for example an increased oil level in the cylinder head or during strong acceleration or braking maneuvers.
- the splash protection device is designed so that the fine oil droplets of the blowby gas are not separated.
- a separation of the oil from the blowby gas preferably takes place in a separate, downstream oil separation device, which is provided, for example, in the form of a screw flight or several screw flights within the hollow shaft section.
- a downstream oil separation device is not additionally burdened by oil splashes or the like.
- the jacket has a sleeve-shaped central section from which the projections protrude.
- the sleeve-shaped middle section is expediently essentially cylindrical or light conically shaped.
- the jacket therefore has a simple shape on which the projections and passage openings can be easily formed.
- the splash protection device can be designed as a molded part, in particular a cast part, which enables simple production.
- the splash protection device can be shrunk on in a similar way to cams or fixed by expanding the hollow shaft section. However, since it is a component subject to comparatively little mechanical stress, simplified assembly is also possible.
- the splash protection device can also be formed from segments, in particular two longitudinally divided segments. The individual segments are then placed on the area of the hollow shaft section at the at least one radial inlet opening and clipped into place.
- the splash guard can be fixed to the hollow shaft section with adhesive or assembled from the segments. Additionally or alternatively, it is also possible to provide cooperating positive locking elements on the splash protection device and the hollow shaft section, which bring about a fixation.
- the splash protection device With regard to the general shape of the splash protection device, it is advantageous if it is enlarged radially at one end and preferably at both ends when viewed in the longitudinal direction of the shaft, for which purpose, for example, flange-shaped formations can be provided. In the context of such a configuration, blow-by gas can easily flow against the radially exposed jacket, although oil injecting from immediately adjacent devices on the shaft, for example adjacent cams, can be effectively prevented by the widened ends of the splash protection device. When dimensioning the splash protection device, the installation space available in the longitudinal direction of the shaft and in the radial direction must be taken into account.
- the projections are designed as ribs that run straight or with a certain inclination in the longitudinal direction of the shaft.
- a camshaft always has a predetermined direction of rotation. If there is a predetermined direction of rotation, the projections are expediently aligned so that separated oil is thrown outwards during rotation in the predetermined direction of rotation. If the projections are designed as ribs, they can be tilted in such a way that the free ends of the ribs point away from the specified or preferred direction of rotation.
- the tilting relative to an alignment that runs exactly in the radial direction can be, for example, between 10° and 40°, in particular between 15° and 30°.
- the passage openings are protected due to the rotational movement by the projections arranged between the passage openings. Since the camshaft has a predetermined direction of rotation, it is advantageous if, viewed in the direction of rotation, a projection is provided immediately in front of each passage opening. The protection of the passage openings from injecting oil is further improved if the projections are inclined against the direction of rotation as described above and thus cover the passage openings to a certain extent when viewed precisely in the radial direction.
- the passage openings can be, for example, longitudinal slots that run essentially parallel to the longitudinal axis of the shaft.
- the combination with ribs running in the longitudinal direction of the shaft then results in a particularly advantageous embodiment.
- the splash protection device of the camshaft according to the invention is located upstream of the at least one radial inlet opening of the hollow shaft section in order to effectively prevent the oil from being injected. It is advantageous if a radial gap is provided between the jacket of the splash protection device with the passage openings provided therein and the hollow shaft section with the at least one passage opening. As part of such a configuration, there can be an offset in the longitudinal direction and/or circumferential direction of the shaft between the passage openings and the at least one inlet opening. The gap then forms a flow channel for the gas to be discharged, with the further deflection making it possible to separate oil. At least it is avoided that fast oil droplets can get directly into the at least one inlet opening of the hollow shaft section without being deflected.
- the passage openings must be distributed accordingly on the circumference of the jacket of the splash protection device.
- the number of passage openings can be an integral multiple of the number of inlet openings.
- the projections and passage openings are distributed around the circumference of the jacket in a uniform arrangement in groups, in particular in pairs.
- a first projection, a first passage opening, a second projection and a second passage opening are then arranged immediately one behind the other, viewed in the direction of rotation.
- a separate oil separation device is provided for the separation of the fine oil droplets from the blowby gas, which can be arranged within the hollow shaft section.
- a screw-shaped swirl generator with one or more screw flights can be provided, the fine oil droplets of the blow-by gas being thrown outwards by the swirling movement and separated accordingly.
- the pitch of the screw flights By varying the pitch of the screw flights, the flow speed in the direction of flow can also be increased.
- a bypass valve with an adjoining bypass channel can also be provided within the hollow shaft section, which leads the blow-by gas past the oil separator device.
- the Fig. 1 shows a ready-to-install camshaft module with a camshaft 1, which, according to its usual structure, has a large number of cams 2 and is held by bearing blocks 3.
- a splash protection device 4 is provided between two adjacent cams 2, the operation of which is explained in detail below.
- the splash protection device 4 is composed of two segments on a separating surface 5. Furthermore, it can be seen that the splash protection device 4 has flange-like widened ends 6a, 6b and has a sleeve-shaped, essentially cylindrical middle section 7 in between. On the middle section 7, passage openings 8 in the form of longitudinal slots and projections in the form of ribs 9 can be seen, which run in the longitudinal direction of the shaft.
- the purpose of the splash protection device 4 and the exact design of the camshaft 1 can be seen from the illustration Fig. 2 to 4 . They show Fig. 2 and 3 similar cross sections, whereby in the Fig. 2 The exact alignment of the ribs 9 and the passage openings 8 can be seen in the top view of the cross section. In the perspective view of the Fig. 3 is, however, with additional consideration of the Fig. 1 the course of the ribs 9 and openings 8 in the longitudinal direction of the shaft can be seen better.
- the camshaft 1 has a hollow shaft section 10, which has at least one, in the exemplary embodiment a total of six, radial inlet openings 11a, 11b for the discharge of a blow-by gas B through the hollow shaft section 10.
- the splash protection device 4 is intended to avoid the injection of large oil droplets or oil jets directly into the radial inlet openings 11a, 11b.
- the ribs 9 and passage openings 8 are provided.
- a gas flow is generated in the circumferential direction, which prevents the injection of large oil droplets or even the injection of an oil jet.
- blowby gas B can follow the rotation of the camshaft 1 and flow into the inlet openings 11a, 11b.
- the path of the blowby gas B is shown in the sectional views Fig. 2 to 4 indicated by dashed lines.
- Fig. 2 In this context it can be seen that, viewed in the direction of rotation D, there is a rib 9 in front of each passage opening 8. Large oil droplets, oil splashes and oil jets are first deposited on the ribs 9 before they can reach the passage openings 8.
- the ribs are tilted relative to the predetermined direction of rotation D in such a way that their free ends point away from the predetermined direction of rotation D.
- the tilting can be between 10°, for example and 40°, in particular between 15° and 30°. In the exemplary embodiment, the tilt is approximately 25°.
- the described tilting of the ribs 9 ensures that the passage opening 8, which is set back immediately next to each rib 9, is even better protected.
- oil that has settled on the rib 9 is effectively pushed outwards due to the centrifugal forces and ultimately thrown away.
- the hollow shaft section 10 has different inlet openings 11a, 11b.
- a radial gap 12 is formed between the middle section 7 of the splash protection device 4 and the hollow shaft section 10, through which the blowby gas B flows.
- Three inlet openings 11a lead to an annular area within the hollow shaft section 10, which supplies the blowby gas B to a swirl generator, not shown, for oil separation.
- a bypass valve 13 with an adjoining bypass channel 14 is arranged in the middle of the hollow shaft section 10. From the gap 12, the blowby gas B can reach the bypass valve 13 through further inlet openings 11b.
- the passage openings 8 and ribs 9 are arranged in groups each with two passage openings 8 and ribs 9. These six groups are then arranged so that the inlet openings 11b leading to the bypass valve 13 are arranged exactly between two adjacent groups.
- the splash protection device 4 is formed from segments, in the exemplary embodiment from two longitudinally divided segments.
- the separating surface 5 between the segments is in the Fig. 2 and 3 recognizable, wherein the segments can be connected, for example, with an adhesive, in particular a two-component adhesive.
- an adhesive can also be provided.
- cooperating positive locking elements 15 can also be provided on the splash protection device 4 and the hollow shaft section 10, which are exemplary in the Fig. 4 are shown.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Valve-Gear Or Valve Arrangements (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
Description
Die Erfindung betrifft eine Nockenwelle mit einem hohlen Wellenabschnitt, der zumindest eine radiale Eintrittsöffnung zur Abführung eines Gases durch den hohlen Wellenabschnitt aufweist und mit einer Spritzschutzeinrichtung, die im Bereich der zumindest einen radialen Eintrittsöffnung auf dem hohlen Wellenabschnitt angeordnet ist.The invention relates to a camshaft with a hollow shaft section which has at least one radial inlet opening for discharging a gas through the hollow shaft section and with a splash protection device which is arranged in the area of the at least one radial inlet opening on the hollow shaft section.
Bei Verbrennungsmotoren und Kolbenverdichtern werden in der Praxis Leckageverluste beobachtet, die auf eine nicht vollständige Abdichtung zurückzuführen sind. Diese Leckageverluste werden als Blowby-Gas bezeichnet und enthalten einen erheblichen Anteil an Öl. Bezogen auf Verbrennungsmotoren ist es deshalb üblich, das im Ventilraum anfallende Blowby-Gas zurück in den Ansaugtrakt des Verbrennungsmotors zu leiten. Um einerseits den Verlust an Öl durch Blowby-Gas zu minimieren und andererseits eine optimale Verbrennung und eine minimale Umweltbelastung zu gewährleisten, ist es bekannt, das Blowby-Gas einer Ölabscheidung zu unterziehen und das abgeschiedene Öl zurück in den Ölkreislauf zu führen.In practice, leakage losses are observed in internal combustion engines and piston compressors, which can be attributed to incomplete sealing. These leakage losses are referred to as blowby gas and contain a significant proportion of oil. In relation to internal combustion engines, it is therefore common to direct the blow-by gas that occurs in the valve chamber back into the intake tract of the internal combustion engine. In order, on the one hand, to minimize the loss of oil due to blow-by gas and, on the other hand, to ensure optimal combustion and minimal environmental impact, it is known to subject the blow-by gas to oil separation and to lead the separated oil back into the oil circuit.
Bei einer Nockenwelle erfolgt die Abfuhr des Blowby-Gases durch den hohlen Wellenabschnitt, wobei in den hohlen Wellenabschnitt auch eine Ölabscheidevorrichtung unmittelbar integriert sein kann. Dabei ist zu berücksichtigen, dass in der Umgebung einer Nockenwelle Öl häufig in unterschiedlichsten Tröpfchengrößen vorliegt. Neben feinsten Öltröpfchen, die in dem Blowby-Gas enthalten und beispielsweise durch Drallerzeuger abzuscheiden sind, werden in der Umgebung einer Nockenwelle häufig auch große Öltröpfchen oder Ölspritzer beobachtet. Derartige große Tröpfchen oder Spritzer können sich beispielsweise bilden, wenn im Bereich der Nockenwelle ein Ölbad oder ein Ölschaum vorhanden ist. In ungünstigen Fällen kann es sogar vorkommen, dass ein Ölstrahl auf die Welle und insbesondere den hohlen Wellenabschnitt mit der Eintrittsöffnung zur Abführung des Blowby-Gases gelangt.In the case of a camshaft, the blow-by gas is removed through the hollow shaft section, and an oil separator device can also be integrated directly into the hollow shaft section. It should be taken into account that oil is often present in a wide variety of droplet sizes in the area surrounding a camshaft. In addition to the finest oil droplets that are contained in the blowby gas and have to be separated, for example, by swirl generators, large oil droplets or oil splashes are also often observed in the vicinity of a camshaft. Such large droplets or splashes can form, for example, if there is an oil bath or oil foam in the area of the camshaft. In unfavorable cases, it can even happen that a jet of oil hits the shaft and in particular the hollow shaft section with the inlet opening for discharging the blow-by gas.
Da eine nachträgliche Abscheidung von Öl mit einem hohen Aufwand verbunden ist, ist es von Vorteil, wenn bei einer Nockenwelle nach dem Anspruch 1 große Öltröpfchen, Ölspritzer und Ölstrahlen von der zumindest einen Eintrittsöffnung des hohlen Wellenabschnittes ferngehalten werden. Trotz der Belüftung und der Möglichkeit der Abführung des Blowby-Gases können dann der Verlust an Öl sowie Verschmutzungen der nachgelagerten Einrichtungen gering gehalten werden. Wenn gemäß einer bevorzugten Ausgestaltung eine nachgelagerte Ölabscheidevorrichtung, beispielsweise innerhalb des hohlen Wellenabschnittes, vorhanden ist, muss diese Ölabscheidevorrichtung nur die feinen Öltröpfchen aus dem Blowby-Gas abscheiden, wodurch insgesamt eine sehr effiziente und zuverlässige Entölung des Gases erreicht werden kann.Since subsequent separation of oil involves a great deal of effort, it is advantageous if large oil droplets, oil splashes and oil jets are kept away from the at least one inlet opening of the hollow shaft section in a camshaft according to
Eine Nockenwelle mit einem hohlen Wellenabschnitt, der zumindest eine radiale Eintrittsöffnung zur Abführung eines Gases durch den hohlen Wellenabschnitt aufweist und mit einer Spritzschutzeinrichtung, die im Bereich der radialen Eintrittsöffnung auf dem hohlen Wellenabschnitt angeordnet ist, ist aus der
Ein Schmiersystem für eine Welle mit einer Ölabscheidevorrichtung ist aus der
Vor diesem Hintergrund liegt der Erfindung die Aufgabe zugrunde, eine Nockenwelle mit einem hohlen Wellenabschnitt und zumindest einer radialen Eintrittsöffnung in dem hohlen Wellenabschnitt anzugeben, bei der durch eine konstruktiv einfach ausgestaltete Spritzschutzeinrichtung das Einspritzen großer Öltröpfchen oder Ölstrahlen in die zumindest eine Eintrittsöffnung zumindest weitgehend verhindert wird.Against this background, the invention is based on the object of specifying a camshaft with a hollow shaft section and at least one radial inlet opening in the hollow shaft section, in which the injection of large oil droplets or oil jets into the at least one inlet opening is at least largely prevented by a structurally simple splash protection device .
Gegenstand der Erfindung und Lösung der Aufgabe ist eine Nockenwelle gemäß Patentanspruch 1. Durch eine solche Ausgestaltung kann erreicht werden, dass im Wesentlichen nur Blowby-Gas in die Durchtrittsöffnungen und nachfolgend in die zumindest eine Eintrittsöffnung des hohlen Wellenabschnittes gelangt, während große Oltröpfchen, Ölspritzer und -strahlen abgehalten werden, wobei die Wirksamkeit der Spritzschutzeinrichtung üblicherweise mit ansteigender Drehzahl der Welle zunimmt.The object of the invention and solution to the problem is a camshaft according to
Die Vorsprünge erzeugen bei der Drehung der Welle einen Gasstrom in Drehrichtung, der das Einschleudern von Öltröpfchen oder sogar das Einspritzen eines Ölstrahls zunächst in die Durchtrittsöffnungen der Spritzschutzeinrichtung und entsprechend auch in die zumindest eine Eintrittsöffnung des hohlen Wellenabschnittes zumindest in einem gewissen Maße verhindert. Des Weiteren ist zu berücksichtigen, dass große Oltröpfchen und -spritzer der Drehung der Spritzschutzeinrichtung nicht im gleichen Maße folgen können wie das Blowby-Gas. So werden also Oltröpfchen und -spritzer bei der Drehung der Welle aufgrund ihrer Massenträgheit verstärkt an den Vorsprüngen abgeschieden, während das Blowby-Gas der Drehbewegung folgen und in die Durchtrittsöffnungen einströmen kann. Die Durchtrittsöffnungen werden also gewißermassen gegenüber den vergleichsweise trägen Oltröpfchen und -spritzern durch die Vorsprünge, die zwischen den Durchtrittsöffnungen angeordnet sind, abgeschottet. Die Effizienz dieser Abschottung ist einerseits von der Form der Vorspünge, insbesondere deren Höhe und Ausrichtung sowie andererseits von dem Volumenstrom des Blowby-Gases abhängig. Bei zunehmendem Volumenstrom des Blowby-Gases kann unter Umständen nicht mehr vollständig vermieden werden, dass auch größere Öltröpfchen mitgerissen werden und in den hohlen Wellenabschnitt gelangen. Dennoch zeichnet sich die erfindungsgemäße Ausgestaltung der Nockenwelle mit der beschriebenen Spritzschutzeinrichtung durch eine sehr effiziente und weitgehende Abtrennung größerer Ölpartikel aus. Selbst wenn die Nockenwelle oder sogar die Spritzschutzeinrichtung teilweise in ein Ölbad eintauchen, kann wirksam das Eindringen von Öl verhindert werden. Ein Ölbad im Bereich einer Nockenwelle kann in der Praxis bei extremen Belastungen eines Motors, beispielsweise einem erhöhten Ölstand im Zylinderkopf oder bei starken Beschleunigungs- oder Bremsmanövern auftreten.When the shaft rotates, the projections generate a gas flow in the direction of rotation, which allows the injection of oil droplets or even the injection of an oil jet initially into the passage openings of the splash protection device and accordingly also prevented to at least a certain extent in the at least one inlet opening of the hollow shaft section. Furthermore, it must be taken into account that large oil droplets and splashes cannot follow the rotation of the splash guard to the same extent as the blow-by gas. As the shaft rotates, oil droplets and splashes are increasingly deposited on the projections due to their inertia, while the blow-by gas can follow the rotational movement and flow into the passage openings. The passage openings are, to a certain extent, sealed off from the comparatively sluggish oil droplets and splashes by the projections which are arranged between the passage openings. The efficiency of this isolation depends on the one hand on the shape of the projections, in particular their height and orientation, and on the other hand on the volume flow of the blowby gas. As the volume flow of the blow-by gas increases, it may no longer be possible to completely prevent larger oil droplets from being carried along and ending up in the hollow shaft section. Nevertheless, the design of the camshaft according to the invention with the splash protection device described is characterized by a very efficient and extensive separation of larger oil particles. Even if the camshaft or even the splash guard is partially immersed in an oil bath, the ingress of oil can be effectively prevented. In practice, an oil bath in the area of a camshaft can occur when an engine is under extreme load, for example an increased oil level in the cylinder head or during strong acceleration or braking maneuvers.
Die Spritzschutzeinrichtung ist gemäß einer bevorzugten Ausgestaltung der Erfindung so ausgeführt, dass die feinen Öltröpfchen des Blowby-Gases nicht abgeschieden werden. Eine solche Abscheidung des Öles aus dem Blowby-Gas erfolgt bevorzugt in einer separaten, nachgelagerten Ölabscheidevorrichtung, die beispielsweise in Form eines Schneckenganges oder mehrerer Schneckengänge innerhalb des hohlen Wellenabschnittes vorgesehen ist. Es ergibt sich aber im Rahmen der Erfindung der Vorteil, dass eine solche nachgelagerte Ölabscheidevorrichtung nicht noch zusätzlich durch Ölspritzer oder dergleichen belastet ist.According to a preferred embodiment of the invention, the splash protection device is designed so that the fine oil droplets of the blowby gas are not separated. Such a separation of the oil from the blowby gas preferably takes place in a separate, downstream oil separation device, which is provided, for example, in the form of a screw flight or several screw flights within the hollow shaft section. However, within the scope of the invention there is the advantage that such a downstream oil separation device is not additionally burdened by oil splashes or the like.
Für die weitere Ausgestaltung der Nockenwelle mit der Spritzschutzeinrichtung ergeben sich im Rahmen der Erfindung verschiedene besonders vorteilhafte Möglichkeiten. Erfindungsgemäß weist der Mantel einen hülsenförmigen Mittelabschnitt auf, von dem die Vorsprünge abstehen. Der hülsenförmige Mittelabschnitt ist dabei zweckmäßigerweise im Wesentlichen zylindrisch oder leicht konisch ausgebildet. Der Mantel weist damit eine einfache Form auf, an der die Vorsprünge und Durchtrittsöffnungen leicht ausgebildet werden können.For the further design of the camshaft with the splash protection device, various particularly advantageous options arise within the scope of the invention. According to the invention, the jacket has a sleeve-shaped central section from which the projections protrude. The sleeve-shaped middle section is expediently essentially cylindrical or light conically shaped. The jacket therefore has a simple shape on which the projections and passage openings can be easily formed.
Die Spritzschutzeinrichtung kann als Formteil, insbesondere Gussteil ausgebildet sein, wodurch eine einfache Herstellung möglich ist. Die Spritzschutzeinrichtung kann ähnlich wie Nocken aufgeschrumpft oder durch die Aufweitung des hohlen Wellenabschnittes fixiert werden. Da es sich aber um ein mechanisch vergleichsweise gering belastetes Bauteil handelt, ist auch eine vereinfachte Montage möglich. So kann die Spritzschutzeinrichtung auch aus Segmenten, insbesondere zwei längsgeteilten Segmenten gebildet sein. Die einzelnen Segmente werden dann auf den Bereich des hohlen Wellenabschnittes an der zumindest einen radialen Eintrittsöffnung aufgesetzt und festgeclipst. Die Spritzschutzeinrichtung kann mit Klebstoff auf dem hohlen Wellenabschnitt fixiert bzw. aus den Segmenten zusammengefügt werden. Zusätzlich oder alternativ besteht auch die Möglichkeit an der Spritzschutzeinrichtung und dem hohlen Wellenabschnitt zusammenwirkende Formschlusselemente vorzusehen, welche eine Fixierung bewirken.The splash protection device can be designed as a molded part, in particular a cast part, which enables simple production. The splash protection device can be shrunk on in a similar way to cams or fixed by expanding the hollow shaft section. However, since it is a component subject to comparatively little mechanical stress, simplified assembly is also possible. The splash protection device can also be formed from segments, in particular two longitudinally divided segments. The individual segments are then placed on the area of the hollow shaft section at the at least one radial inlet opening and clipped into place. The splash guard can be fixed to the hollow shaft section with adhesive or assembled from the segments. Additionally or alternatively, it is also possible to provide cooperating positive locking elements on the splash protection device and the hollow shaft section, which bring about a fixation.
Je nach den zu erwartenden Belastungen kann für die Spritzschutzeinrichtung neben metallischen Werkstoffen auch ein Kunststoff, Keramik oder ein anderer widerstandsfähiger Werkstoff in Betracht gezogen werden.Depending on the expected loads, in addition to metallic materials, plastic, ceramic or another resistant material can also be considered for the splash protection device.
Hinsichtlich der allgemeinen Form der Spritzschutzeinrichtung ist es von Vorteil, wenn diese in Längsrichtung der Welle gesehen an einem Ende und vorzugsweise an beiden Enden radial vergrössert ist, wozu beispielsweise flanschförmige Ausformungen vorgesehen sein können. Im Rahmen einer solchen Ausgestaltung kann Blowby-Gas den radial freiliegenden Mantel ohne Weiteres anströmen wobei jedoch durch die verbreiterten Enden der Spritzschutzeinrichtung einspritzendes Öl von unmittelbar benachbarten Einrichtungen der Welle, beispielsweise benachbarter Nocken, effektiv abgehalten werden kann. Bei der Dimensionierung der Spritzschutzeinrichtung ist dabei der in Längsrichtung der Welle sowie in radialer Richtung zur Verfügung stehende Bauraum zu beachten.With regard to the general shape of the splash protection device, it is advantageous if it is enlarged radially at one end and preferably at both ends when viewed in the longitudinal direction of the shaft, for which purpose, for example, flange-shaped formations can be provided. In the context of such a configuration, blow-by gas can easily flow against the radially exposed jacket, although oil injecting from immediately adjacent devices on the shaft, for example adjacent cams, can be effectively prevented by the widened ends of the splash protection device. When dimensioning the splash protection device, the installation space available in the longitudinal direction of the shaft and in the radial direction must be taken into account.
Hinsichtlich der konkreten Ausgestaltung der Spritzschutzeinrichtung ist es von Vorteil, wenn die Vorsprünge als Rippen ausgebildet sind, die gerade oder auch mit einer gewissen Schrägstellung in Längsrichtung der Welle verlaufen.With regard to the specific design of the splash protection device, it is advantageous if the projections are designed as ribs that run straight or with a certain inclination in the longitudinal direction of the shaft.
Eine Nockenwelle weist stets eine vorgegebene Drehrichtung auf. Wenn eine vorgegebene Drehrichtung vorliegt, sind die Vorsprünge zweckmäßigerweise so ausgerichtet, dass abgeschiedenes Öl bei der Drehung in der vorgegebenen Drehrichtung nach außen geschleudert wird. Bei einer Ausgestaltung der Vorsprünge als Rippen können diese also derart verkippt sein, dass die freien Enden der Rippen von der vorgegebenen bzw. bevorzugten Drehrichtung wegweisen. Die Verkippung gegenüber einer genau in radialer Richtung verlaufenden Ausrichtung kann beispielsweise zwischen 10° und 40° , insbesondere zwischen 15 ° und 30 ° betragen.A camshaft always has a predetermined direction of rotation. If there is a predetermined direction of rotation, the projections are expediently aligned so that separated oil is thrown outwards during rotation in the predetermined direction of rotation. If the projections are designed as ribs, they can be tilted in such a way that the free ends of the ribs point away from the specified or preferred direction of rotation. The tilting relative to an alignment that runs exactly in the radial direction can be, for example, between 10° and 40°, in particular between 15° and 30°.
Wie zuvor erläutert, sind die Durchtrittsöffnungen aufgrund der Drehbewegung durch die zwischen den Durchtrittsöffnungen angeordneten Vorsprünge geschützt. Da die Nockenwelle eine vorgegebene Drehrichtung aufweist, ist es von Vorteil, wenn in Drehrichtung gesehen unmittelbar vor jeder Durchtrittsöffnung ein Vorsprung vorgesehen ist. Der Schutz der Durchtrittsöffnungen vor einspritzendem Öl wird noch zusätzlich verbessert, wenn die Vorsprünge wie zuvor beschrieben entgegen der Drehrichtung schräg gestellt sind und so genau in radialer Richtung gesehen die Durchtrittsöffnungen in einem gewissen Masse verdecken.As explained above, the passage openings are protected due to the rotational movement by the projections arranged between the passage openings. Since the camshaft has a predetermined direction of rotation, it is advantageous if, viewed in the direction of rotation, a projection is provided immediately in front of each passage opening. The protection of the passage openings from injecting oil is further improved if the projections are inclined against the direction of rotation as described above and thus cover the passage openings to a certain extent when viewed precisely in the radial direction.
Die Durchtrittsöffnungen können beispielsweise Längsschlitze sein, die im Wesentlichen parallel zur Längsachse der Welle verlaufen. In der Kombination mit in Längsrichtung der Welle verlaufenden Rippen ergibt sich dann eine besonders vorteilhafte Ausgestaltung.The passage openings can be, for example, longitudinal slots that run essentially parallel to the longitudinal axis of the shaft. The combination with ribs running in the longitudinal direction of the shaft then results in a particularly advantageous embodiment.
Die Spritzschutzeinrichtung der erfindungsgemäßen Nockenwelle ist der zumindest einen radialen Eintrittsöffnung des hohlen Wellenabschnittes vorgelagert, um ein Einspritzen des Öles effektiv abzuhalten. Dabei ist es von Vorteil, wenn zwischen dem Mantel der Spritzschutzeinrichtung mit den darin vorgesehenen Durchtrittsöffnungen und dem hohlen Wellenabschnitt mit der zumindest einen Durchtrittsöffnung ein radialer Spalt vorgesehen ist. Im Rahmen einer solchen Ausgestaltung kann nämlich zwischen den Durchtrittsöffnungen und der zumindest einen Eintrittsöffnung ein Versatz in Längsrichtung und/oder Umfangrichtung der Welle vorhanden sein. Der Spalt bildet dann einen Strömungskanal für das abzuführende Gas, wobei durch die weitere Umlenkung eine Abscheidung von Öl möglich ist. Zumindest wird vermieden, dass schnelle Oltröpfchen ohne eine Ablenkung direkt in die zumindest eine Eintrittsöffnung des hohlen Wellenabschnittes gelangen können.The splash protection device of the camshaft according to the invention is located upstream of the at least one radial inlet opening of the hollow shaft section in order to effectively prevent the oil from being injected. It is advantageous if a radial gap is provided between the jacket of the splash protection device with the passage openings provided therein and the hollow shaft section with the at least one passage opening. As part of such a configuration, there can be an offset in the longitudinal direction and/or circumferential direction of the shaft between the passage openings and the at least one inlet opening. The gap then forms a flow channel for the gas to be discharged, with the further deflection making it possible to separate oil. At least it is avoided that fast oil droplets can get directly into the at least one inlet opening of the hollow shaft section without being deflected.
Üblicherweise sind an dem hohlen Wellenabschnitt mehrere Eintrittsöffnungen vorgesehen, die gleichmäßig um den Umfang verteilt sind. Um dann den beschriebenen Versatz in Längs- und/oder Umfangrichtung zu erreichen, sind die Durchtrittsöffnungen an dem Umfang des Mantels der Spritzschutzeinrichtung entsprechend zu verteilen. Insbesondere kann die Anzahl der Durchtrittsöffnungen ein ganzteiliges Vielfaches der Anzahl der Eintrittsöffnungen sein.Typically, several inlet openings are provided on the hollow shaft section, which are evenly distributed around the circumference. In order to then achieve the described offset in the longitudinal and/or circumferential direction, the passage openings must be distributed accordingly on the circumference of the jacket of the splash protection device. In particular, the number of passage openings can be an integral multiple of the number of inlet openings.
Zweckmäißg ist es in diesem Zusammenhang auch, wenn die Vorsprünge und Durchtrittsöffnungen um den Umfang des Mantels in einer gleichmäßigen Anordnung gruppenweise, insbesondere paarweise verteilt sind. Bei einer paarweisen Anordnung sind dann jeweils in Drehrichtung gesehen ein erster Vorsprung, eine erste Durchtrittsöffnung, ein zweiter Vorsprung und eine zweite Durchtrittsöffnung unmittelbar hintereinander angeordnet.In this context, it is also expedient if the projections and passage openings are distributed around the circumference of the jacket in a uniform arrangement in groups, in particular in pairs. When arranged in pairs, a first projection, a first passage opening, a second projection and a second passage opening are then arranged immediately one behind the other, viewed in the direction of rotation.
Wie bereits eingangs erläutert, ist es von Vorteil, wenn für die Abscheidung der feinen Öltröpfchen aus dem Blowby-Gas eine separate Ölabscheidevorrichtung vorgesehen ist, die innerhalb des hohlen Wellenabschnittes angeordnet sein kann. Hierzu kann beispielsweise ein schneckenförmiger Drallerzeuger mit einem oder mehreren Schneckengängen vorgesehen sein, wobei durch die Drallbewegung die feinen Öltröpfchen des Blowby-Gases nach außen geschleudert und entsprechend abgeschieden werden. Durch eine Variation der Steigung der Schneckengänge kann auch die Strömungsgeschwindigkeit in Strömungsrichtung erhöht werden.As already explained at the beginning, it is advantageous if a separate oil separation device is provided for the separation of the fine oil droplets from the blowby gas, which can be arranged within the hollow shaft section. For this purpose, for example, a screw-shaped swirl generator with one or more screw flights can be provided, the fine oil droplets of the blow-by gas being thrown outwards by the swirling movement and separated accordingly. By varying the pitch of the screw flights, the flow speed in the direction of flow can also be increased.
Um einen zu hohen Überdruck im Bereich der Nockenwelle zu vermeiden, kann innerhalb des hohlen Wellenabschnittes auch ein Bypass-Ventil mit einem daran anschließenden Bypass-Kanal vorgesehen sein, welches das BlowbyGas an der Ölabscheidevorrichtung vorbeiführt.In order to avoid excessive overpressure in the area of the camshaft, a bypass valve with an adjoining bypass channel can also be provided within the hollow shaft section, which leads the blow-by gas past the oil separator device.
Die Erfindung wird im Folgenden anhand einer lediglich ein Ausführungsbeispiel darstellenden Zeichnung erläutert: Es zeigen:
- Fig. 1
- ein einbaufertiges Nockenwellenmodul mit einer Nockenwelle, welcher mit eine Spritzschutzeinrichtung versehen ist,
- Fig. 2
- einen Schnitt entlang der Linie A-A der
Fig. 1 in einer Draufsicht, - Fig. 3
- der Schnitt gemäß der
Fig. 2 in einer perspektivischen Ansicht, - Fig. 4
- ein Längsschnitt durch die Nockenwelle im Bereich der Spritzschutzeinrichtung.
- Fig. 1
- a ready-to-install camshaft module with a camshaft, which is provided with a splash protection device,
- Fig. 2
- a cut along line AA of the
Fig. 1 in a top view, - Fig. 3
- the cut according to the
Fig. 2 in a perspective view, - Fig. 4
- a longitudinal section through the camshaft in the area of the splash guard.
Die
Der
Der Zweck der Spritzschutzeinrichtung 4 sowie die genaue Ausgestaltung der Nockenwelle 1 ergibt sich aus der Darstellung der
In den Schnittdarstellungen ist zunächst zu erkennen, dass die Nockenwelle 1 einen hohlen Wellenabschnitt 10 aufweist, der zumindest eine, in dem Ausführungsbeispiel insgesamt sechs radiale Eintrittsöffnungen 11a, 11b für die Abführung eines Blowby-Gases B durch den hohlen Wellenabschnitt 10 aufweist. Die Spritzschutzeinrichtung 4 ist dabei dazu vorgesehen, das Einspritzen von großen Öltröpfchen oder Ölstrahlen direkt in die radialen Eintrittsöffnungen 11a, 11b hinein zu vermeiden.In the sectional views it can first be seen that the
Zu diesem Zweck sind die Rippen 9 und Durchtrittsöffnungen 8 vorgesehen. Bei der Drehung der Nockenwelle 1 in der vorgegebenen Drehrichtung D wird in Umfangrichtung ein Gasstrom erzeugt, der das Einschleudern von großen Öltröpfchen oder sogar das Einspritzen eines Ölstrahls verhindert. Blowby-Gas B kann aber bei einem entsprechenden Überdruck der Drehung der Nockenwelle 1 folgen und in die Eintrittsöffnungen 11a, 11b einströmen. Der Weg des Blowby-Gases B ist in den Schnittdarstellungen der
Neben der Erzeugung eines Gasstromes durch die Rippen 9 ist auch zu berücksichtigen, dass aufgrund der Drehung der Spritzschutzeinrichtung 4 und der Trägheit größerer Partikel oder Strahlen diese sich an den Rippen 9 absetzen. Der
Der
Der genaue Aufbau des hohlen Wellenabschnittes 10 ist in der
Gemäß der
Hinsichtlich der weiteren Eintrittsöffnungen 11b, durch welche das Blowby-Gas B zu dem Bypass-Ventil 13 gelangen kann, liegt gemäß der
Wie bereits im Zusammenhang mit der
Um die Spritzschutzeinrichtung 4 an der Nockenwelle 1 zu befestigen, kann auch ein Klebstoff vorgesehen sein. Zusätzlich oder alternativ können an der Spritzschutzeinrichtung 4 und dem hohlen Wellenabschnitt 10 auch zusammenwirkende Formschlusselemente 15 vorgesehen sein, die exemplarisch in der
Claims (12)
- A camshaft (1) with a hollow shaft section (10), which comprises at least one radial inlet opening (11a, 11b) for the removal of a gas through the hollow shaft section (10) and with a splash protection device (4), which is disposed in the region of the at least one radial inlet opening (11a, 11b) on the hollow shaft section (10), wherein the splash protection device (4) comprises a radially exposed casing with radial through-openings (8) and projections between the through-openings (8), and wherein the projections protrude radially opposite the through-openings, and that the casing comprises a sleeve-shaped middle section (7), from which the projections protrude.
- The camshaft according to claim 1, characterised in that the projections are constituted as ribs (9) which run in the longitudinal direction of the camshaft.
- The camshaft according to claim 2, characterised in that the shaft has a preselected or preferred rotational direction (D), wherein the ribs (9) are tilted in such a way that their free ends point away from the preselected or preferred rotational direction (D).
- The camshaft according to any one of claims 1 to 3, characterised in that the camshaft has a preselected or preferred rotational direction (D) and that, viewed in the rotational direction (D), a projection is provided in front of each through-opening (8).
- The camshaft according to any one of claims 1 to 4, characterised in that the through-openings (8) are constituted as elongated slots.
- The camshaft according to any one of claims 1 to 5, characterised in that a radial gap (12) is provided between the casing of the splash protection device (4) and the hollow shaft section (10) with the at least one inlet opening (11a, 11b), wherein an offset in the longitudinal direction and/or circumferential direction of the camshaft is provided between the through-opening (8) and the at least one inlet opening (11a, 11b).
- The camshaft according to any one of claims 1 to 6, characterised in that the splash protection device (4) comprises ends (6a, 6b) which are radially enlarged as viewed in the longitudinal direction of the camshaft.
- The camshaft according to any one of claims 1 to 7, characterised in that the projections and through-openings (8) are distributed in groups, in particular in pairs, around the circumference of the casing in a uniform arrangement.
- The camshaft according to any one of claims 1 to 8, characterised in that a bypass valve (13) and/or an oil separation device are provided inside the hollow shaft section (10).
- The camshaft according to any one of claims 1 to 9, characterised in that the splash protection device (4) is constituted by segments, in particular by two longitudinally split segments.
- The camshaft according to any one of claims 1 to 10, characterised in that the splash protection device (4) is fixed with adhesive on the hollow shaft section (10).
- The camshaft according to any one of claims 1 to 11, characterised in that the splash protection device (4) and the hollow shaft section (10) comprise interacting form-fit elements (15).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011000458A DE102011000458A1 (en) | 2011-02-02 | 2011-02-02 | Shaft, in particular camshaft with a hollow shaft section |
PCT/EP2012/051800 WO2012104391A1 (en) | 2011-02-02 | 2012-02-02 | Shaft, particularly a cam shaft, comprising a hollow shaft section |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2670955A1 EP2670955A1 (en) | 2013-12-11 |
EP2670955B1 EP2670955B1 (en) | 2014-12-31 |
EP2670955B2 true EP2670955B2 (en) | 2023-09-20 |
Family
ID=45592357
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12703756.2A Active EP2670955B2 (en) | 2011-02-02 | 2012-02-02 | Shaft such as camshaft comprising a hollow section |
Country Status (5)
Country | Link |
---|---|
US (1) | US9803514B2 (en) |
EP (1) | EP2670955B2 (en) |
CN (1) | CN103415676B (en) |
DE (1) | DE102011000458A1 (en) |
WO (1) | WO2012104391A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102013108770A1 (en) | 2013-08-13 | 2015-02-19 | Thyssenkrupp Presta Teccenter Ag | Camshaft assembly and camshaft assembly |
DE102014104885A1 (en) * | 2014-04-07 | 2015-10-08 | Thyssenkrupp Presta Teccenter Ag | Camshaft with improved lubrication |
CN103939178B (en) * | 2014-04-10 | 2015-12-23 | 安徽全柴动力股份有限公司 | A kind of high efficiency, low cost diesel engine oil gas separating device |
DE102015203991B4 (en) | 2015-03-05 | 2018-07-26 | Volkswagen Aktiengesellschaft | Closed hollow shaft |
US10473206B2 (en) * | 2015-07-02 | 2019-11-12 | Deere & Company | Transmission vent |
DE102016008299B4 (en) * | 2016-07-06 | 2020-12-31 | Neander Motors Ag | Oil separator for an internal combustion engine |
DE102017105241B4 (en) | 2017-03-13 | 2019-12-19 | Thyssenkrupp Ag | Centrifugal oil separator, oil separator and internal combustion engine |
DE102019102894B3 (en) | 2019-02-06 | 2020-06-18 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Centrifugal separator |
US11719326B2 (en) * | 2021-04-19 | 2023-08-08 | The Boeing Company | Demister for a gearing system and method |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1955966A1 (en) † | 1968-11-06 | 1970-06-11 | Socete Nationale d'Etude et de Construction de Moteurs d*Aviation, Paris | Gas cleaning device |
US5114446A (en) † | 1991-02-15 | 1992-05-19 | United Technologies Corporation | Deoiler for jet engine |
US5716423A (en) † | 1995-12-21 | 1998-02-10 | United Technologies Corporation | Multi-stage deoiler with porous media |
DE10140301A1 (en) † | 2001-08-16 | 2003-02-27 | Daimler Chrysler Ag | Crankcase venting device has separating wall perpendicular to axis of rotation as baffle |
DE102004045630A1 (en) † | 2004-09-21 | 2006-04-06 | Daimlerchrysler Ag | Oil mist centrifugal dis-entrainment unit, for an internal combustion engine crankcase breather, reduces load on main separator by use of a rotating vane inlet pre-separator |
DE102005034273A1 (en) † | 2005-07-22 | 2006-06-14 | Daimlerchrysler Ag | Combustion engine e.g. for motor vehicle, has two cam shafts in cylinder head with first cam shaft having longitudinal bore hole for conveying Blow-By-Gas and oil separating device provided |
WO2006119737A1 (en) † | 2005-05-10 | 2006-11-16 | Mahle International Gmbh | Centrifugal oil mist separation device integrated in an axial hollow shaft of an internal combustion engine |
KR20100052770A (en) † | 2008-11-11 | 2010-05-20 | 현대자동차주식회사 | Oil separator unit integrated with cam shaft of vehicle |
DE102009012401A1 (en) † | 2009-03-10 | 2010-09-23 | Thyssenkrupp Presta Teccenter Ag | Hollow body with integrated oil separator |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4217120A (en) * | 1977-10-20 | 1980-08-12 | Sundstrand Corporation | Air-oil separator for aircraft gearbox |
DE3535107A1 (en) | 1985-10-02 | 1987-04-09 | Mtu Muenchen Gmbh | WAREHOUSE SUPPLY SYSTEM |
US5273163A (en) * | 1992-01-23 | 1993-12-28 | Luzenac America, Inc. | Centrifugal particle classifier having uniform influx distributor |
JPH07150924A (en) * | 1993-12-01 | 1995-06-13 | Nissan Motor Co Ltd | Oil separator for blow-by gas |
DE19803872C2 (en) | 1998-01-31 | 2001-05-10 | Daimler Chrysler Ag | Ventilation device for a crankcase of an internal combustion engine |
DE19931740C2 (en) * | 1999-07-08 | 2001-06-13 | Daimler Chrysler Ag | Reciprocating internal combustion engine with a camshaft |
JP4207046B2 (en) * | 2006-01-19 | 2009-01-14 | トヨタ自動車株式会社 | Camshaft support structure for internal combustion engine |
DE102007052249B4 (en) * | 2007-11-02 | 2023-12-14 | Mercedes-Benz Group AG | Internal combustion engine valve train switching device |
DE102009012402A1 (en) * | 2009-03-10 | 2010-09-23 | Thyssenkrupp Presta Teccenter Ag | Shaft body with integrated oil separator |
-
2011
- 2011-02-02 DE DE102011000458A patent/DE102011000458A1/en not_active Ceased
-
2012
- 2012-02-02 WO PCT/EP2012/051800 patent/WO2012104391A1/en active Application Filing
- 2012-02-02 CN CN201280007408.0A patent/CN103415676B/en active Active
- 2012-02-02 US US13/979,401 patent/US9803514B2/en active Active
- 2012-02-02 EP EP12703756.2A patent/EP2670955B2/en active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1955966A1 (en) † | 1968-11-06 | 1970-06-11 | Socete Nationale d'Etude et de Construction de Moteurs d*Aviation, Paris | Gas cleaning device |
US5114446A (en) † | 1991-02-15 | 1992-05-19 | United Technologies Corporation | Deoiler for jet engine |
US5716423A (en) † | 1995-12-21 | 1998-02-10 | United Technologies Corporation | Multi-stage deoiler with porous media |
DE10140301A1 (en) † | 2001-08-16 | 2003-02-27 | Daimler Chrysler Ag | Crankcase venting device has separating wall perpendicular to axis of rotation as baffle |
DE102004045630A1 (en) † | 2004-09-21 | 2006-04-06 | Daimlerchrysler Ag | Oil mist centrifugal dis-entrainment unit, for an internal combustion engine crankcase breather, reduces load on main separator by use of a rotating vane inlet pre-separator |
WO2006119737A1 (en) † | 2005-05-10 | 2006-11-16 | Mahle International Gmbh | Centrifugal oil mist separation device integrated in an axial hollow shaft of an internal combustion engine |
DE102005034273A1 (en) † | 2005-07-22 | 2006-06-14 | Daimlerchrysler Ag | Combustion engine e.g. for motor vehicle, has two cam shafts in cylinder head with first cam shaft having longitudinal bore hole for conveying Blow-By-Gas and oil separating device provided |
KR20100052770A (en) † | 2008-11-11 | 2010-05-20 | 현대자동차주식회사 | Oil separator unit integrated with cam shaft of vehicle |
DE102009012401A1 (en) † | 2009-03-10 | 2010-09-23 | Thyssenkrupp Presta Teccenter Ag | Hollow body with integrated oil separator |
Also Published As
Publication number | Publication date |
---|---|
US20140007736A1 (en) | 2014-01-09 |
CN103415676A (en) | 2013-11-27 |
WO2012104391A1 (en) | 2012-08-09 |
US9803514B2 (en) | 2017-10-31 |
EP2670955B1 (en) | 2014-12-31 |
DE102011000458A1 (en) | 2012-08-02 |
CN103415676B (en) | 2016-03-09 |
EP2670955A1 (en) | 2013-12-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2670955B2 (en) | Shaft such as camshaft comprising a hollow section | |
DE102006038700B4 (en) | Device for separating liquids from gases | |
EP2603674B1 (en) | Hollow body with integrated oil separator | |
DE102013015052B4 (en) | Cyclone filter device | |
EP3652419B1 (en) | Cylinder head oil separator for an internal combustion engine (flow-controlled oil separator) | |
DE1955966A1 (en) | Gas cleaning device | |
DE10063903A1 (en) | Free jet centrifuge with integrated oil separator | |
EP2302174A2 (en) | Gas turbine shroud labyrinth seal | |
EP3011150B1 (en) | Oil separator, in particular for the crankcase ventilation of an engine | |
WO2010102688A1 (en) | Shaft body comprising an integrated oil separator unit | |
EP2821599A1 (en) | Jet engine with at least one oil separator | |
EP3507468B1 (en) | Oil separator device, ventilation system for an internal combustion engine, and internal combustion engine comprising such an oil separator | |
DE19607919B4 (en) | Centrifugal oil separator for the blow-by gases of an internal combustion engine | |
DE102005003037A1 (en) | Separating device for separating liquid particles from a gaseous medium | |
EP1627993A1 (en) | Exhaust turbine cleaning device | |
WO2017153136A1 (en) | Liquid mist precipitation device | |
DE202017007184U1 (en) | Separating | |
DE102016216826A1 (en) | Fluid mist separator and crankcase ventilation device | |
DE102012213558A1 (en) | piston | |
EP3033499B1 (en) | Camshaft assembly and camshaft arrangement | |
EP3371420B1 (en) | Arrangement for separation of lubricant flows and exhaust gas turbocharger comprising such arrangement | |
WO2019007858A1 (en) | Hollow shaft and method for separating a fluid | |
DE102009032629B4 (en) | Bearing arrangement with a rotary separator | |
EP1558359A1 (en) | Device for separating particles from a gas flow | |
DE102016224242A1 (en) | oil separator |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20130712 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
DAX | Request for extension of the european patent (deleted) | ||
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20140917 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502012001972 Country of ref document: DE Effective date: 20150212 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 704545 Country of ref document: AT Kind code of ref document: T Effective date: 20150215 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150331 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: VDEP Effective date: 20141231 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150401 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150430 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150202 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R026 Ref document number: 502012001972 Country of ref document: DE Ref country code: CH Ref legal event code: PL |
|
PLBI | Opposition filed |
Free format text: ORIGINAL CODE: 0009260 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20150228 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20150228 |
|
26 | Opposition filed |
Opponent name: MAHLE INTERNATIONAL GMBH Effective date: 20150930 |
|
PLAX | Notice of opposition and request to file observation + time limit sent |
Free format text: ORIGINAL CODE: EPIDOSNOBS2 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20150202 |
|
PLBB | Reply of patent proprietor to notice(s) of opposition received |
Free format text: ORIGINAL CODE: EPIDOSNOBS3 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 5 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20120202 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20150501 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20150228 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
APAH | Appeal reference modified |
Free format text: ORIGINAL CODE: EPIDOSCREFNO |
|
APBM | Appeal reference recorded |
Free format text: ORIGINAL CODE: EPIDOSNREFNO |
|
APBP | Date of receipt of notice of appeal recorded |
Free format text: ORIGINAL CODE: EPIDOSNNOA2O |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 7 |
|
APBQ | Date of receipt of statement of grounds of appeal recorded |
Free format text: ORIGINAL CODE: EPIDOSNNOA3O |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 704545 Country of ref document: AT Kind code of ref document: T Effective date: 20170202 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170202 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141231 |
|
APBU | Appeal procedure closed |
Free format text: ORIGINAL CODE: EPIDOSNNOA9O |
|
PLAY | Examination report in opposition despatched + time limit |
Free format text: ORIGINAL CODE: EPIDOSNORE2 |
|
PLAH | Information related to despatch of examination report in opposition + time limit modified |
Free format text: ORIGINAL CODE: EPIDOSCORE2 |
|
PLAT | Information related to reply to examination report in opposition deleted |
Free format text: ORIGINAL CODE: EPIDOSDORE3 |
|
PLBC | Reply to examination report in opposition received |
Free format text: ORIGINAL CODE: EPIDOSNORE3 |
|
PLBC | Reply to examination report in opposition received |
Free format text: ORIGINAL CODE: EPIDOSNORE3 |
|
PLAH | Information related to despatch of examination report in opposition + time limit modified |
Free format text: ORIGINAL CODE: EPIDOSCORE2 |
|
PLAT | Information related to reply to examination report in opposition deleted |
Free format text: ORIGINAL CODE: EPIDOSDORE3 |
|
PLAH | Information related to despatch of examination report in opposition + time limit modified |
Free format text: ORIGINAL CODE: EPIDOSCORE2 |
|
PLBC | Reply to examination report in opposition received |
Free format text: ORIGINAL CODE: EPIDOSNORE3 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230530 |
|
PUAH | Patent maintained in amended form |
Free format text: ORIGINAL CODE: 0009272 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: PATENT MAINTAINED AS AMENDED |
|
27A | Patent maintained in amended form |
Effective date: 20230920 |
|
AK | Designated contracting states |
Kind code of ref document: B2 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R102 Ref document number: 502012001972 Country of ref document: DE |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20240219 Year of fee payment: 13 Ref country code: GB Payment date: 20240219 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20240221 Year of fee payment: 13 |