EP2561205B1 - Piston upper part of an assembled or welded piston with extended cooling spaces - Google Patents
Piston upper part of an assembled or welded piston with extended cooling spaces Download PDFInfo
- Publication number
- EP2561205B1 EP2561205B1 EP11703395.1A EP11703395A EP2561205B1 EP 2561205 B1 EP2561205 B1 EP 2561205B1 EP 11703395 A EP11703395 A EP 11703395A EP 2561205 B1 EP2561205 B1 EP 2561205B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- piston
- recesses
- piston upper
- cooling
- recess
- 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
- 238000001816 cooling Methods 0.000 title claims description 87
- 238000002485 combustion reaction Methods 0.000 claims description 38
- 238000005266 casting Methods 0.000 claims description 19
- 238000004519 manufacturing process Methods 0.000 claims description 14
- 238000000034 method Methods 0.000 claims description 10
- 238000005304 joining Methods 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 9
- 230000008569 process Effects 0.000 claims description 6
- 238000003754 machining Methods 0.000 claims description 4
- 238000005242 forging Methods 0.000 claims description 3
- 238000005520 cutting process Methods 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 239000002826 coolant Substances 0.000 description 13
- 230000000694 effects Effects 0.000 description 6
- 238000003801 milling Methods 0.000 description 4
- 238000000926 separation method Methods 0.000 description 4
- 230000007704 transition Effects 0.000 description 4
- 239000010687 lubricating oil Substances 0.000 description 3
- 230000003313 weakening effect Effects 0.000 description 3
- 238000004939 coking Methods 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 150000003839 salts Chemical group 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000035508 accumulation Effects 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 239000008186 active pharmaceutical agent Substances 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000009499 grossing Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
- 230000007480 spreading Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—PistonsĀ
- F02F3/0015—Multi-part pistons
- F02F3/003—Multi-part pistons the parts being connected by casting, brazing, welding or clamping
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/105—Salt cores
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—PistonsĀ
- F02F3/02—PistonsĀ having means for accommodating or controlling heat expansion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—PistonsĀ
- F02F3/16—PistonsĀ having cooling means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—PistonsĀ
- F02F3/16—PistonsĀ having cooling means
- F02F3/20—PistonsĀ having cooling means the means being a fluid flowing through or along piston
- F02F3/22—PistonsĀ having cooling means the means being a fluid flowing through or along piston the fluid being liquid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—PistonsĀ
- F02F3/16—PistonsĀ having cooling means
- F02F3/20—PistonsĀ having cooling means the means being a fluid flowing through or along piston
- F02F3/22—PistonsĀ having cooling means the means being a fluid flowing through or along piston the fluid being liquid
- F02F3/225—PistonsĀ having cooling means the means being a fluid flowing through or along piston the fluid being liquid the liquid being directed into blind holes
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49231—I.C. [internal combustion] engine making
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49249—Piston making
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49249—Piston making
- Y10T29/49252—Multi-element piston making
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49249—Piston making
- Y10T29/49256—Piston making with assembly or composite article making
Definitions
- the invention relates to a one-piece and two-piece piston of an internal combustion engine and a method for producing such pistons according to the respective preambles of the independent claims.
- the combustion temperatures and the combustion pressures are increased in order to optimize the combustion, so that the upper part of the piston in particular is subjected to high thermal loads.
- the operating temperature of the piston of such internal combustion engines can exceed the permissible limits of the piston material, associated with the risk of heat aging in which the alloy of the piston material loses strength and dimensional stability.
- pistons are used in which an annular cooling channel is integrated, in which a partial amount of the lubricating oil of the internal combustion engine is injected as a coolant via an injection nozzle, flows through the cooling channel and then exits.
- the DE 197 50 021 A1 discloses a cooling duct piston which, in the area of the annular field, encloses an annular cooling duct, radially offset from a lateral surface.
- the coolant flowing through the cooling channel effects heat dissipation, the effectiveness of this liquid cooling being essentially determined by the volume throughput of the cooling medium through the cooling channel.
- the DE 41 18 400 A1 a built-up piston which, starting from the cooling channel, includes cooling slots running in the direction of the piston crown with walls running parallel to one another.
- the invention is based on the object of optimizing the cooling effect of the upper piston part of a one-piece and of a two-part piston in thermally highly stressed zones by means of an inexpensive measure and accordingly specifying a piston and a method for producing such pistons.
- the present invention provides an upper piston part of a one-piece and a two-piece piston with integrated recesses according to the features of claims 1 and 2, as well as a method for producing the recesses according to the features of claims 12, 13 and 14.
- the two-part piston is designed as a liquid-cooled piston, consisting of a lower piston part and an upper piston part having a combustion chamber bowl. These piston components are supported by joining webs that are radially spaced from one another and form a parting plane and are preferably joined together in a materially bonded manner, preferably by means of a welded connection, or preferably frictionally, preferably by means of a screw connection.
- the assembled piston is thus preferably assembled from an upper piston part and a lower piston part, for example by means of a screw connection, or preferably welded together, for example by means of a welded connection.
- the upper piston part is an annular one that extends into the lower piston part Introduced cooling channel, which is in communication with an inner cooling space via connecting channels.
- the upper piston part includes recesses that are oriented in the direction of a piston crown and designed as a blind hole and connected to the cooling channel.
- the liquid-cooled piston of an internal combustion engine consists of a piston lower part and a piston upper part having a combustion chamber bowl, the piston being designed as a one-piece piston that has no parting plane.
- the at least one circumferential recess starting from the cooling duct is designed in the upper piston part so that its walls widen in a conically increasing manner.
- a maximum cross-section is established in the area of greatest depth of the recess.
- the invention advantageously increases the depth of the cooling space through which the coolant flows, while maintaining defined wall thicknesses, and thus optimizes the cooling of the upper piston part.
- a preferred structural shape of the recess according to the invention follows, at a distance, a central contour of the trough-shaped combustion bowl introduced in the piston head.
- the shaker effect can be improved and consequently the cooling effect can be increased.
- the size and extent of the recess according to the invention, which forms an extension of the cooling duct, is advantageously not limited by design-related requirements, for example the position and arrangement of the separation plane between the lower piston part and the upper piston part or the cooling duct, but can, for example, expand in a targeted manner in the direction of the combustion bowl .
- the recesses designed according to the invention are preferably intended for piston tops with a relatively small combustion bowl diameter in order to optimally cool the resulting large wall thicknesses and material accumulations in the piston crown.
- the exhaust gas requirements (Tier 3 and IMO) for assembled pistons with a small combustion bowl diameter can advantageously be achieved in conjunction with the measures to optimize the cooling of the upper piston part. It is advantageous to combine the upper piston part designed according to the invention with existing, tried and tested lower piston parts. In the case of a one-piece, liquid-cooled piston of an internal combustion engine, the type of piston lower part and the piston upper part are also designed to be suitable, as described above.
- the size and extent of the recess is not limited by the outer diameter of the joining webs or the support surfaces in the area of the plane of separation between the upper piston part and the lower piston part. Rather, the measure according to the invention enables the recess according to the invention intended for cooling to be expanded into the thermally highly stressed zone.
- the cross-sectional profile in the recess base consequently exceeds the cross-sectional profile in the area of a transition from the recess to the cooling channel due to the conical widening.
- the piston head preferably includes a plurality of recesses distributed around the circumference and connected to the cooling channel. These recesses, designed as blind holes and specifically enlarging the cooling space, bring about improved, efficient cooling of the upper piston part.
- the recesses lead, at least locally, to reduced wall thicknesses of the upper piston part, as compared with the combustion chamber bowl, the ring zone, the top land and the piston crown. Due to coordinated wall thicknesses between the recesses designed according to the invention and the adjacent thermally A structurally stable upper piston part that can withstand the highest demands is realized in areas subject to high loads.
- the measure according to the invention reduces the component temperature to a level below the flash point of conventional cooling oils, which at the same time reduces the risk of coking for the lubricating oil of the internal combustion engine, which is preferably used as the coolant.
- the piston upper part and consequently the entire piston are suitable for higher combustion temperatures and pressures, i.e. can be used in internal combustion engines with high power density.
- the large-volume, inexpensive to manufacture recesses, particularly in the case of small combustion bowl diameters advantageously reduce the weight of the upper piston part.
- a preferred embodiment of the recesses, according to the invention, which widen conically over the longitudinal extent provides that these are designed, distributed circumferentially in the upper piston part, in particular as slots, bores or channels.
- webs formed by the material of the upper piston part are provided between the recesses and the cooling channel.
- walls or support ribs can also be used, the walls or support ribs differing from the webs in their respective shape.
- the cold room is expanded spatially.
- the adjacent recesses designed according to the invention are made in the upper piston part in opposite directions, alternately in matching or differing geometric sizes and / or inclinations to one another. This measure enables a targeted extension of the recesses up to thermally highly stressed zones without the risk of component weakening.
- the walls of the recess are inclined at an angle of inclination " ā , ā " between 0 Ā° to 40 Ā°, preferably ā 15 Ā°, to a longitudinal piston axis to achieve largely matching wall thicknesses compared to the thermally highly stressed zones.
- ā , ā angle of inclination
- ā angle of inclination
- ā ā 15 Ā°
- the conically expanding recesses are each provided with a rounded recess base that has a positive effect on the structural strength.
- D maximum diameter of the tool used for the cutting process, for example a milling tool, for the rounded contour
- the double-rounded recess base can be designed in a stepped manner.
- the recess base can be a strongly undulating surface, which creates an enlarged surface, or as a finely undulating surface Surface. Additional machining manufacturing steps, for example milling cuts, reduce the stepped transition between the bulges, whereby the surface of the bulges is qualitatively improved by a lower waviness on the surface and whereby the size of the surface is reduced. It is thus possible to create a finely wavy surface with a larger number of cuts.
- the invention includes a beveled recess base. The recesses in the cooling duct also lead to increased turbulence of the coolant in the cooling duct.
- the cooling chamber can be adapted to the shape of the depression in the combustion chamber depression.
- the adaptation and configuration of the recess base is possible by means of the shape of the casting mold body, the shape of which in certain areas is the negative shape of the shape of the recess base.
- the recesses which are preferably designed as channels, bores or slots, to be arranged symmetrically or asymmetrically on the circumference in the upper piston part.
- the position, orientation and size of the recess can be adapted to the different thermal loads. For example, it is advisable to design the cooling space or cross-sectional volume of the recess on the pressure side (DS) to be different from the corresponding cross-sectional volume on the counterpressure side (GDS) of the piston upper part.
- the location and interpretation of the The recess is made in such a way that a weakening of the strength of the upper piston part is avoided. According to a method according to the invention according to claim 12, the following steps are provided for producing the recesses.
- a casting mold body corresponding to the shape of the recesses preferably a salt core, is fixed in position in the casting mold intended for the upper piston part. After the upper part of the piston has been cast and cooled, the casting mold body is removed by rinsing.
- a casting mold body corresponding to the shape of the recesses preferably a salt core, is fixed in position in the casting mold intended for the one-piece piston, which has a piston upper part and a piston lower part.
- the casting mold body is removed by rinsing.
- Another alternative method for producing the recesses provides for mechanical, three-dimensional machining.
- a turning and milling process is preferably suitable for this, with which cavities are introduced to represent recesses in the piston upper part. It is also a good idea to represent the recesses by means of milling or drilling tools.
- Figure 1 shows a longitudinal section through an upper piston part 1, which is, for example, a component made from a steel alloy by means of a forging process.
- the upper piston part 1 can also be made from aluminum, an aluminum alloy or an iron alloy.
- the upper piston part 1 can also be produced by means of any other desired forming process or primary forming process.
- the piston upper part 1 forms together with an in Figure 1 Piston lower part not shown, for example, a two-part piston that is built with a friction fit or welded with a material fit and is liquid-cooled.
- the upper piston part 1 is supported on corresponding joining webs of the lower piston part via two circumferential joining webs 2, 3 that are radially offset from one another.
- All joining webs together form a separation plane 4 via which the lower piston part and the upper piston part 1 are permanently connected to one another by means of a frictional connection, preferably by means of a screw connection, or by means of a material connection, preferably by means of a welded connection.
- a frictional connection preferably by means of a screw connection
- a material connection preferably by means of a welded connection.
- a combustion chamber bowl 7 which is delimited on the outside by a stepped bowl rim 8, is introduced concentrically to a piston longitudinal axis 5 in a piston head 6 of the upper piston part 1.
- the upper piston part 1 is enclosed by a top land 9 which adjoins the piston crown 6 and which is adjoined by an annular zone 10 intended to accommodate piston rings.
- an annular cooling channel 11 is provided in the area of the parting plane 4, which extends into the lower piston part and through which coolant, in particular lubricating oil of the internal combustion engine, circulates when the internal combustion engine is in operation.
- the cooling medium enters the cooling channel 11 via an inlet and leaves the cooling channel 11 via a plurality of connection channels 15, also known as transfer bores, via an outlet.
- the coolant supply can alternatively also take place via the center of the piston, that is to say the inner cooling space 16.
- the coolant is conducted into the cooling channel 11 via the connecting channels 15 and then flows out of the cooling channel 11 via drainage bores.
- the cooling channel 11 is connected to a plurality of recesses 12 distributed around the circumference and aligned in the direction of the piston head 6.
- These recesses 12, which are distributed around the circumference and are introduced in the manner of blind holes, are designed as channels, bores and / or slots and enlarge the cooling space in the piston upper part 1, which is acted upon by the coolant.
- the recesses 12 widen conically up to a maximum at a recess bottom 14.
- the recesses 12 are connected to a central inner cooling chamber 16 positioned below the combustion bowl 7 via connecting channels 15 positioned on the circumference.
- Figure 2 illustrates the geometric design of the recess 12 in an enlarged illustration.
- the recesses 12 distributed circumferentially in the upper piston part 1 can alternatively also be designed as cavities running around the periphery.
- the recess 12 according to the exemplary embodiment is made in the piston upper part 1 subsequently during production by means of the forging process by means of mechanical three-dimensional machining.
- the recess 12 forms a stepped recess base 14.
- the dome-like recess base forming a bowl vault. 14 includes a double-rounded contour enclosing the radius "R".
- the depth of the recess base 14 located between the radii "R" in the recess 12 can be adjusted by the number of cuts.
- the inner wall 17, which is closer to the piston longitudinal axis 5 in the radial direction, and the outer wall 18, which is farther away from the piston longitudinal axis 5 in the radial direction, are to be closed to the recess 12, in particular to adapt to the structural design of the upper piston part 1 as well as almost identical wall thicknesses compared to the thermally heavily loaded zones the piston longitudinal axis 5 is inclined.
- the angle of inclination ā of the inner wall 17 and the angle of inclination ā of the outer wall 18, the inner wall 17 and the outer wall 18 being inclined opposite to one another, can be designed to be the same or different from one another.
- Figure 3 shows the top view of the upper piston part 1 of a two-part piston in the direction of the two joining webs 2, 3.
- the upper piston part 1 has several slot-shaped recesses 19, in the example five slot-shaped recesses 19, arranged tangentially around the piston longitudinal axis 5 according to Figure 3 on.
- the tangential rotation around the piston longitudinal axis 5 is also known under the term radial rotation around the piston longitudinal axis 5.
- the piston upper part 1 has more than five or fewer than five slot-shaped recesses 19.
- the inner cooling space 16 is also shown, around which the five slot-shaped recesses 19 are arranged distributed around the circumference.
- the slot-shaped recesses 19 are not connected to one another, so that a spacing in the form of webs 20 exists between the respective slot-shaped recesses 19.
- the cooling space By varying the slot depth of the respective cooling slots 21, 22 of the recess 12, it is possible for the cooling space to be adapted to the bowl shape of the combustion bowl 7. The degree of smoothing is achieved by the number of slots between cooling slot 21 and cooling slot 22. In Figure 5 the inner cooling space 16 is also shown for the sake of clarity.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
Die Erfindung betrifft einen einteiligen und zweiteiligen Kolben einer Brennkraftmaschine und Verfahren zur Herstellung solcher Kolben gemĆ¤Ć den jeweiligen Oberbegriffen der unabhƤngigen PatentansprĆ¼che.The invention relates to a one-piece and two-piece piston of an internal combustion engine and a method for producing such pistons according to the respective preambles of the independent claims.
Zur Einhaltung von Emissionsgrenzwerten bzw. zur Erreichung von Emissionszielen und Verbrauchszielen werden zur Optimierung der Verbrennung die Verbrennungstemperaturen und die VerbrennungsdrĆ¼cke angehoben, wodurch insbesondere das Kolbenoberteil thermisch stark beansprucht wird. Die Betriebstemperatur des Kolbens derartiger Brennkraftmaschinen kann die zulƤssigen Grenzen von dem Kolbenwerkstoff Ć¼berschreiten, verbunden mit der Gefahr einer WƤrmealterung, bei der die Legierung des Kolbenwerkstoffs an Festigkeit und Formsteifigkeit verliert. Um die thermischen Belastungen des Kolbens zu minimieren, werden Kolben eingesetzt, in denen ein ringfƶrmiger KĆ¼hlkanal integriert ist, in dem als KĆ¼hlmittel eine Teilmenge von dem Schmierƶl der Brennkraftmaschine Ć¼ber eine EinspritzdĆ¼se eingespritzt wird, den KĆ¼hlkanal durchstrƶmt und dann austritt. Die
Mit zunehmender spezifischer Leistung der Brennkraftmaschine ist es erforderlich, bekannte Konzepte von flĆ¼ssigkeitsgekĆ¼hlten Kolben zu optimieren. ZusƤtzlich zu einem ringfƶrmigen KĆ¼hlkanal ist es daher erforderlich, weitere Bereiche des Kolbens gezielt mit KĆ¼hlmittel zu beaufschlagen. Zur Realisierung dieser MaĆnahme zeigt die
Der Erfindung liegt die Aufgabe zu Grunde, die KĆ¼hlwirkung des Kolbenoberteils eines einteiligen und eines zweiteiligen Kolbens in thermisch hochbelasteten Zonen durch eine kostengĆ¼nstige MaĆnahme zu optimieren und dementsprechend einen Kolben und Verfahren zur Herstellung solcher Kolben anzugeben.The invention is based on the object of optimizing the cooling effect of the upper piston part of a one-piece and of a two-part piston in thermally highly stressed zones by means of an inexpensive measure and accordingly specifying a piston and a method for producing such pistons.
Ausgehend von dem Stand der Technik stellt die vorliegende Erfindung ein Kolbenoberteil eines einteiligen und eines zweiteiligen Kolbens mit integrierten Ausnehmungen gemĆ¤Ć den Merkmalen des Patentanspruchs 1 und 2, sowie Verfahren zur Herstellung der Ausnehmungen gemĆ¤Ć den Merkmalen der PatentansprĆ¼che 12, 13 und 14 bereit.Based on the prior art, the present invention provides an upper piston part of a one-piece and a two-piece piston with integrated recesses according to the features of
Der zweiteilige Kolben ist als ein flĆ¼ssigkeitsgekĆ¼hlter Kolben, bestehend aus einem Kolbenunterteil und einem eine Brennraummulde aufweisenden Kolbenoberteil, ausgefĆ¼hrt. Diese Kolbenbauteile sind Ć¼ber radial zueinander beabstandete, eine Trennungsebene bildende FĆ¼gestege abgestĆ¼tzt und vorzugsweise stoffschlĆ¼ssig, bevorzugt mittels einer SchweiĆverbindung, oder vorzugsweise reibschlĆ¼ssig, bevorzugt mittels einer Schraubenverbindung, zusammengefĆ¼gt. Somit ist der zusammengefĆ¼gte Kolben aus einem Kolbenoberteil und Kolbenunterteil vorzugsweise zusammengebaut, beispielsweise mittels Schraubenverbindung, oder vorzugsweise zusammengeschweiĆt, beispielsweise mittels SchweiĆverbindung. In dem Kolbenoberteil ist ein ringfƶrmiger, sich bis in das Kolbenunterteil erstreckender KĆ¼hlkanal eingebracht, der Ć¼ber VerbindungskanƤle mit einem inneren KĆ¼hlraum in Verbindung steht. Zur KĆ¼hlraumvergrƶĆerung schlieĆt das Kolbenoberteil in Richtung eines Kolbenbodens ausgerichtete, als Sackloch ausgefĆ¼hrte, mit dem KĆ¼hlkanal verbundene Ausnehmungen ein.The two-part piston is designed as a liquid-cooled piston, consisting of a lower piston part and an upper piston part having a combustion chamber bowl. These piston components are supported by joining webs that are radially spaced from one another and form a parting plane and are preferably joined together in a materially bonded manner, preferably by means of a welded connection, or preferably frictionally, preferably by means of a screw connection. The assembled piston is thus preferably assembled from an upper piston part and a lower piston part, for example by means of a screw connection, or preferably welded together, for example by means of a welded connection. In the upper piston part is an annular one that extends into the lower piston part Introduced cooling channel, which is in communication with an inner cooling space via connecting channels. To enlarge the cooling space, the upper piston part includes recesses that are oriented in the direction of a piston crown and designed as a blind hole and connected to the cooling channel.
GemĆ¤Ć dem Patentanspruch 2 ist es auch mƶglich, dass der flĆ¼ssigkeitsgekĆ¼hlte Kolben einer Brennkraftmaschine aus einem Kolbenunterteil und einem eine Brennraummulde aufweisenden Kolbenoberteil besteht, wobei der Kolben als ein einteiliger Kolben ausgefĆ¼hrt ist, der keine Trennungsebene aufweist.According to
Zur Lƶsung der Problemstellung ist gemĆ¤Ć der Erfindung nach Anspruch 1 und Anspruch 2 vorgesehen, die zumindest eine von dem KĆ¼hlkanal ausgehende, umlaufend eingebrachte Ausnehmung in dem Kolbenoberteil so auszubilden, dass deren Wandungen sich konisch ansteigend aufweiten. Aufgrund der sich einstellenden Spreizung der Wandungen stellt sich ein maximaler Querschnitt in dem Bereich grƶĆter Tiefe der Ausnehmung ein. Vorteilhaft vergrƶĆert die Erfindung unter Einhaltung definierter WandstƤrken gegenĆ¼ber bisher bekannten Lƶsungen den von dem KĆ¼hlmittel durchstrƶmten, in der Tiefe erweiterten KĆ¼hlraum und optimiert somit die KĆ¼hlung des Kolbenoberteils. Eine bevorzugte konstruktive Formgebung der erfindungsgemƤĆen Ausnehmung folgt beabstandet einer zentrischen Kontur der wannenfƶrmig in dem Kolbenboden eingebrachten Brennraummulde. Verbunden mit einem groĆvolumigen, die KĆ¼hlmittelaufnahme vergrƶĆernden Hohlraum der Ausnehmung kann die Shakerwirkung verbessert und folglich die KĆ¼hlwirkung gesteigert werden. Die GrƶĆe und die Erstreckung der erfindungsgemƤĆen, eine Erweiterung des KĆ¼hlkanals bildende Ausnehmung ist vorteilhaft nicht durch konstruktiv bedingte Vorgaben, beispielsweise die Lage und Anordnung der Trennungsebene zwischen dem Kolbenunterteil und dem Kolbenoberteil oder dem KĆ¼hlkanal begrenzt, sondern kann sich beispielsweise gezielt in Richtung der Brennraummulde erweitern. Die erfindungsgemĆ¤Ć gestalteten Ausnehmungen sind bevorzugt fĆ¼r Kolbenoberteile mit einem relativ kleinen Brennraummulden-Durchmesser bestimmt, um die sich einstellenden groĆen WandstƤrken und MaterialanhƤufungen in dem Kolbenboden optimal zu kĆ¼hlen. Damit kann eine Verkokung bis zu einem Abbrand sowie eine Festigkeitsminderung des Werkstoffs vermieden werden. Vorteilhaft kƶnnen in Verbindung mit den MaĆnahmen zur Optimierung der KĆ¼hlung des Kolbenoberteils die Abgasforderungen (Tier 3 und IMO) fĆ¼r gebaute Kolben mit einem kleinen Brennraummulden-Durchmesser erreicht werden. Vorteilhaft bietet es sich an, das erfindungsgemĆ¤Ć gestaltete Kolbenoberteil mit vorhandenen erprobten Kolbenunterteilen zu kombinieren. Bei einem als einteilig ausgefĆ¼hrten flĆ¼ssigkeitsgekĆ¼hlten Kolben einer Brennkraftmaschine ist die Art des Kolbenunterteils und des Kolbenoberteils ebenso, wie vorhergehend beschrieben, passend gestaltet.To solve the problem, according to the invention according to
GemĆ¤Ć der Erfindung wird die GrƶĆe und die Erstreckung der Ausnehmung nicht durch den ƤuĆeren Durchmesser der FĆ¼gestege beziehungsweise der AbstĆ¼tzflƤchen im Bereich der Trennungsebene zwischen dem Kolbenoberteil und dem Kolbenunterteil begrenzt. Vielmehr ermƶglicht die erfindungsgemƤĆe MaĆnahme die zur KĆ¼hlung bestimmte erfindungsgemƤĆe Ausnehmung bis in thermisch hochbelasteten Zone auszudehnen. Das Querschnittsprofil in dem Ausnehmungsgrund Ć¼bertrifft aufgrund der konischen Aufweitung folglich das Querschnittsprofil im Bereich eines Ćbergangs der Ausnehmung zu dem KĆ¼hlkanal. Bevorzugt schlieĆt der Kolbenboden mehrere umfangsverteilt positionierte, mit dem KĆ¼hlkanal in Verbindung stehende Ausnehmungen ein. Diese als Sackloch ausgefĆ¼hrten, den KĆ¼hlraum gezielt vergrƶĆernden Ausnehmungen bewirken eine verbesserte, effiziente KĆ¼hlung des Kolbenoberteils. Dabei fĆ¼hren die Ausnehmungen zumindest lokal zu reduzierten WandstƤrken des Kolbenoberteils, wie gegenĆ¼ber der Brennraummulde, dem Ringfeld, dem Feuersteg sowie dem Kolbenboden. Bedingt durch abgestimmte WandstƤrken zwischen den erfindungsgemĆ¤Ć ausgefĆ¼hrten Ausnehmungen und den benachbarten thermisch stark beanspruchten Zonen wird ein strukturfestes, hƶchsten Anforderungen standhaltendes Kolbenoberteil realisiert.According to the invention, the size and extent of the recess is not limited by the outer diameter of the joining webs or the support surfaces in the area of the plane of separation between the upper piston part and the lower piston part. Rather, the measure according to the invention enables the recess according to the invention intended for cooling to be expanded into the thermally highly stressed zone. The cross-sectional profile in the recess base consequently exceeds the cross-sectional profile in the area of a transition from the recess to the cooling channel due to the conical widening. The piston head preferably includes a plurality of recesses distributed around the circumference and connected to the cooling channel. These recesses, designed as blind holes and specifically enlarging the cooling space, bring about improved, efficient cooling of the upper piston part. In this case, the recesses lead, at least locally, to reduced wall thicknesses of the upper piston part, as compared with the combustion chamber bowl, the ring zone, the top land and the piston crown. Due to coordinated wall thicknesses between the recesses designed according to the invention and the adjacent thermally A structurally stable upper piston part that can withstand the highest demands is realized in areas subject to high loads.
Die erfindungsgemƤĆe MaĆnahme reduziert die Bauteiltemperatur auf ein Niveau unterhalb von dem Flammpunkt Ć¼blicher KĆ¼hlƶle, wodurch sich gleichzeitig die Gefahr einer Verkokung fĆ¼r das bevorzugt als KĆ¼hlmittel eingesetzte Schmierƶl der Brennkraftmaschine verringert. AuĆerdem besteht keine Gefahr, dass sich eine isolierende, die KĆ¼hlwirkung herabsetzende Ćlkohleschicht bildet, sowie eine nachteilige thermische Kolben-Deformation aufgrund einer abgesenkten Festigkeit des Kolbenwerkstoffs einstellt. Durch die entscheidend verbesserte WƤrmeabfuhr und damit KĆ¼hlwirkung der erfindungsgemƤĆen Ausnehmung ist das Kolbenoberteil und folglich der gesamte Kolben fĆ¼r hƶhere Verbrennungstemperaturen und VerbrennungsdrĆ¼cke, d.h. in Brennkraftmaschinen mit hoher Leistungsdichte einsetzbar. AuĆerdem verringern die groĆvolumig gestalteten, kostengĆ¼nstig herstellbaren Ausnehmungen insbesondere bei kleinen Brennraummulden-Durchmessern vorteilhaft das Gewicht des Kolbenoberteils.The measure according to the invention reduces the component temperature to a level below the flash point of conventional cooling oils, which at the same time reduces the risk of coking for the lubricating oil of the internal combustion engine, which is preferably used as the coolant. In addition, there is no risk of an insulating oil carbon layer which reduces the cooling effect forming, and of disadvantageous thermal piston deformation due to a reduced strength of the piston material. Due to the decisively improved heat dissipation and thus the cooling effect of the recess according to the invention, the piston upper part and consequently the entire piston are suitable for higher combustion temperatures and pressures, i.e. can be used in internal combustion engines with high power density. In addition, the large-volume, inexpensive to manufacture recesses, particularly in the case of small combustion bowl diameters, advantageously reduce the weight of the upper piston part.
Eine bevorzugte AusfĆ¼hrungsform der erfindungsgemĆ¤Ć sich Ć¼ber die LƤngserstreckung konisch aufweitenden Ausnehmungen sieht vor, dass diese im Kolbenoberteil umfangsverteilt insbesondere als Schlitze, Bohrungen oder KanƤle gestaltet sind. Dabei sind zwischen den Ausnehmungen und dem KĆ¼hlkanal von dem Material des Kolbenoberteils gebildete Stege vorgesehen. Alternativ zu den Stegen kƶnnen auch Wandungen oder StĆ¼tzrippen verwendet werden, wobei sich die Wandungen oder StĆ¼tzrippen durch ihre jeweilige Form von den Stegen unterscheiden. Zur Erzielung einer hohen Strukturfestigkeit des Kolbenoberteils bietet es sich an, die konisch aufgeweiteten Ausnehmungen als tortenfƶrmige KĆ¼hlraumkammern mit einer Wabenstruktur auszubilden, die gleichzeitig die KĆ¼hleigenschaften positiv beeinflusst und die zu einer VergrƶĆerung der KĆ¼hloberflƤche fĆ¼hrt. ZusƤtzlich wird dadurch auch der KĆ¼hlraum rƤumlich erweitert.A preferred embodiment of the recesses, according to the invention, which widen conically over the longitudinal extent provides that these are designed, distributed circumferentially in the upper piston part, in particular as slots, bores or channels. In this case, webs formed by the material of the upper piston part are provided between the recesses and the cooling channel. As an alternative to the webs, walls or support ribs can also be used, the walls or support ribs differing from the webs in their respective shape. In order to achieve a high structural strength of the piston upper part, it is advisable to design the conically widened recesses as pie-shaped cooling chamber chambers with a honeycomb structure, which at the same time positively influences the cooling properties and which leads to an increase in the cooling surface. In addition, the cold room is expanded spatially.
Einer weiteren konstruktiven Auslegung gemĆ¤Ć werden die erfindungsgemĆ¤Ć gestalteten, benachbarten Ausnehmungen entgegengesetzt wechselweise in Ć¼bereinstimmenden oder voneinander abweichenden geometrischen GrƶĆen und/oder Neigungen zueinander in dem Kolbenoberteil eingebracht. Diese MaĆnahme ermƶglicht eine gezielte Erstreckung der Ausnehmungen bis in thermisch hoch belastete Zonen, ohne die Gefahr einer BauteilschwƤchung.According to a further structural design, the adjacent recesses designed according to the invention are made in the upper piston part in opposite directions, alternately in matching or differing geometric sizes and / or inclinations to one another. This measure enables a targeted extension of the recesses up to thermally highly stressed zones without the risk of component weakening.
GemĆ¤Ć einer bevorzugten Auslegung sind zur Erzielung weitestgehend Ć¼bereinstimmender WandstƤrken gegenĆ¼ber den thermisch stark belasteten Zonen die Wandungen der Ausnehmung in einem Neigungswinkel "Ī±, Ī²" zwischen 0Ā° bis 40Ā°, vorzugsweise von ā¤ 15Ā° zu einer KolbenlƤngsachse geneigt ausgerichtet. Dem konstruktiven Aufbau des Kolbenbodens angepasst, bietet es sich weiterhin an, die Neigungswinkel von gegenĆ¼berliegenden Wandungen, insbesondere einer inneren Wandung und einer ƤuĆeren Wandung, Ć¼bereinstimmend oder voneinander abweichend auszulegen.According to a preferred design, the walls of the recess are inclined at an angle of inclination "Ī±, Ī²" between 0 Ā° to 40 Ā°, preferably ā¤ 15 Ā°, to a longitudinal piston axis to achieve largely matching wall thicknesses compared to the thermally highly stressed zones. Adapted to the design of the piston head, it is also advisable to design the angles of inclination of opposing walls, in particular an inner wall and an outer wall, to match or differ from one another.
Zur kostenoptimierten Fertigung und Vermeidung einer BauteilschwƤchung ist vorgesehen, die sich konisch spreizenden Ausnehmungen jeweils mit einem gerundeten, die Strukturfestigkeit positiv beeinflussenden Ausnehmungsgrund zu versehen. FĆ¼r die gerundete Kontur ist bevorzugt ein Radius "R" zwischen 1,5 mm und D/2 (D = maximaler Durchmesser des verwendeten Werkzeugs fĆ¼r das spanabhebende Verfahren, beispielsweise eines FrƤswerkzeugs, fĆ¼r die gerundete Kontur) vorgesehen. Alternativ dazu bietet es sich an, den Ausnehmungsgrund mit einer doppelt gerundeten, ein kuppelartiges Muldengewƶlbe bildenden Kontur zu versehen. Weiterhin kann zur Anpassung an den konstruktiven Aufbau des Kolbenbodens der doppelt gerundete Ausnehmungsgrund gestuft gestaltet werden. Der Ausnehmungsgrund kann dabei als stark wellenfƶrmige OberflƤche, wodurch eine vergrƶĆerte OberflƤche erzeugt wird, oder als eine fein wellenfƶrmige OberflƤche ausgefĆ¼hrt werden. Durch zusƤtzliche spanabhebende Fertigungsschritte, beispielsweise FrƤsschnitte, wird der gestufte Ćbergang zwischen den Wƶlbungen verringert, wodurch die OberflƤche der Wƶlbungen qualitativ durch eine geringere Welligkeit auf der OberflƤche verbessert wird und wodurch die GrƶĆe der OberflƤche verringert wird. Somit ist es mƶglich, durch eine grƶĆere Anzahl der Schnitte eine feinwellige OberflƤche zu erzeugen. Alternativ zu einer gerundeten Endkontur schlieĆt die Erfindung einen abgeschrƤgt ausgebildeten Ausnehmungsgrund ein. Durch die Ausnehmungen in dem KĆ¼hlkanal kommt es zusƤtzlich auch zu einer verstƤrkten Verwirbelung des KĆ¼hlmittels in dem KĆ¼hlkanal. Durch eine Anpassung der OberflƤche des Ausnehmungsgrundes und eine Verkleinerung des Durchmessers des Ausnehmungsgrundes ist es mƶglich, die Emissionen bei dem Betrieb des Kolbens zu verringern bzw. zu optimieren. Auch kƶnnen durch die Anpassung des gestuften Ćbergangs die Emissionen beim Betrieb verringert werden. Durch die Variation der Tiefe der Ausnehmung, von dem Kolbenunterteil in Richtung Kolbenoberteil gesehen, kann eine Anpassung des KĆ¼hlraums an die Form der Mulde der Brennraummulde erfolgen. Bei einem einteiligen Kolben ist die Anpassung und Ausgestaltung des Ausnehmungsgrundes mittels der Form des GieĆformkƶrpers mƶglich, dessen Form in bestimmten Bereichen die Negativ-Form der Form des Ausnehmungsgrundes ist.For cost-optimized production and avoidance of component weakening, the conically expanding recesses are each provided with a rounded recess base that has a positive effect on the structural strength. For the rounded contour, a radius "R" between 1.5 mm and D / 2 (D = maximum diameter of the tool used for the cutting process, for example a milling tool, for the rounded contour) is preferably provided. As an alternative to this, it is advisable to provide the bottom of the recess with a double-rounded contour that forms a dome-like hollow vault. Furthermore, to adapt to the structural design of the piston head, the double-rounded recess base can be designed in a stepped manner. The recess base can be a strongly undulating surface, which creates an enlarged surface, or as a finely undulating surface Surface. Additional machining manufacturing steps, for example milling cuts, reduce the stepped transition between the bulges, whereby the surface of the bulges is qualitatively improved by a lower waviness on the surface and whereby the size of the surface is reduced. It is thus possible to create a finely wavy surface with a larger number of cuts. As an alternative to a rounded end contour, the invention includes a beveled recess base. The recesses in the cooling duct also lead to increased turbulence of the coolant in the cooling duct. By adapting the surface of the recess base and reducing the diameter of the recess base, it is possible to reduce or optimize the emissions during operation of the piston. By adapting the stepped transition, emissions during operation can also be reduced. By varying the depth of the recess, viewed from the lower piston part in the direction of the upper piston part, the cooling chamber can be adapted to the shape of the depression in the combustion chamber depression. In the case of a one-piece piston, the adaptation and configuration of the recess base is possible by means of the shape of the casting mold body, the shape of which in certain areas is the negative shape of the shape of the recess base.
Eine weitere Ausgestaltung der Erfindung sieht vor, die bevorzugt als KanƤle, Bohrungen oder Schlitze ausgebildeten Ausnehmungen umfangsseitig symmetrisch oder unsymmetrisch in dem Kolbenoberteil anzuordnen. Die Lage, Ausrichtung und GrƶĆe der Ausnehmung kann dabei den unterschiedlichen thermischen Belastungen angepasst werden. Beispielsweise bietet es sich an, das KĆ¼hlraum- bzw. Querschnittsvolumen der Ausnehmung auf der Druckseite (DS) gegenĆ¼ber dem entsprechenden Querschnittsvolumen auf der Gegendrucksseite (GDS) des Kolbenoberteils voneinander abweichend auszulegen. Die Lage und Auslegung der Ausnehmung erfolgt so, dass eine SchwƤchung der Festigkeit des Kolbenoberteils vermieden wird.
GemĆ¤Ć einem erfindungsgemƤĆen Verfahren nach Anspruch 12 sind zur Herstellung der Ausnehmungen folgende Schritte vorgesehen. ZunƤchst wird ein der Form der Ausnehmungen entsprechender GieĆformkƶrper, vorzugsweise ein Salzkern, in die fĆ¼r das Kolbenoberteil bestimmte GieĆform lagefixiert. Nach erfolgtem Guss und Erkalten des Kolbenoberteils wird der GieĆformkƶrper durch AusspĆ¼len entfernt.Another embodiment of the invention provides for the recesses, which are preferably designed as channels, bores or slots, to be arranged symmetrically or asymmetrically on the circumference in the upper piston part. The position, orientation and size of the recess can be adapted to the different thermal loads. For example, it is advisable to design the cooling space or cross-sectional volume of the recess on the pressure side (DS) to be different from the corresponding cross-sectional volume on the counterpressure side (GDS) of the piston upper part. The location and interpretation of the The recess is made in such a way that a weakening of the strength of the upper piston part is avoided.
According to a method according to the invention according to
GemĆ¤Ć einem weiteren alternativen erfindungsgemƤĆen Verfahren nach Anspruch 13 sind zur Herstellung der Ausnehmungen folgende Schritte bei einem einteiligen Kolben vorgesehen. ZunƤchst wird ein der Form der Ausnehmungen entsprechender GieĆformkƶrper, vorzugsweise ein Salzkern, in die fĆ¼r den einteiligen Kolben, der ein Kolbenoberteil und ein Kolbenunterteil aufweist, bestimmte GieĆform lagefixiert. Nach erfolgtem Guss und Erkalten des einteiligen Kolbens wird der GieĆformkƶrper durch AusspĆ¼len entfernt.According to a further alternative method according to the invention according to
Ein weiteres alternatives Verfahren zur Herstellung der Ausnehmungen sieht eine mechanische, dreidimensionale zerspannende Bearbeitung vor. Dazu eignet sich bevorzugt eine Dreh- und FrƤsbearbeitung, mit der HohlrƤume zur Darstellung von Ausnehmungen in dem Kolbenoberteil eingebracht werden. AuĆerdem bietet es sich an, die Ausnehmungen mittels einer FrƤsung oder mit Bohrwerkzeugen darzustellen.Another alternative method for producing the recesses provides for mechanical, three-dimensional machining. A turning and milling process is preferably suitable for this, with which cavities are introduced to represent recesses in the piston upper part. It is also a good idea to represent the recesses by means of milling or drilling tools.
Ein beispielhaft ausgestaltetes Kolbenoberteil gemĆ¤Ć der Erfindung, auf den diese jedoch nicht beschrƤnkt ist, ist im Folgenden beschrieben und anhand der Figuren erlƤutert.An exemplary designed upper piston part according to the invention, to which this is not limited, is described below and explained with reference to the figures.
Es zeigen:
- Figur 1:
- ein Kolbenoberteil in einem LƤngsschnitt mit einer erfindungsgemĆ¤Ć gestalteten Ausnehmung,
- Figur 2:
- ein Detail des Kolbenoberteils gemƤĆ
Figur 1 in einem vergrƶĆerten MaĆstab, - Figur 3:
- die Draufsicht auf ein Kolbenoberteil mit mehreren schlitzfƶrmigen Ausnehmungen,
- Figur 4:
- eine rƤumliche Darstellung von KĆ¼hlschlitzen in einem Kolbenoberteil und
- Figur 5:
- eine rƤumliche Darstellung eines Kolbenoberteils mit erweiterten KĆ¼hlschlitzen.
- Figure 1:
- an upper piston part in a longitudinal section with a recess designed according to the invention,
- Figure 2:
- a detail of the piston top according to
Figure 1 on an enlarged scale, - Figure 3:
- the top view of an upper piston part with several slot-shaped recesses,
- Figure 4:
- a three-dimensional representation of cooling slots in a piston upper part and
- Figure 5:
- a three-dimensional representation of an upper piston part with expanded cooling slots.
In
In
In
In
Durch die Variation der Schlitztiefe der jeweiligen KĆ¼hlschlitze 21, 22 der Ausnehmung 12 ist es mƶglich, dass eine Anpassung des KĆ¼hlraums an die Muldenform der Brennraummulde 7 erfolgt. Der Grad der GlƤttung wird durch die Anzahl der Schlitze zwischen KĆ¼hlschlitz 21 und KĆ¼hlschlitz 22 erreicht. In
- 11
- KolbenoberteilPiston top
- 22
- FĆ¼gestegJoining web
- 33
- FĆ¼gestegJoining web
- 44th
- TrennungsebeneLevel of separation
- 55
- KolbenlƤngsachsePiston longitudinal axis
- 66th
- KolbenbodenPiston crown
- 77th
- BrennraummuldeCombustion bowl
- 88th
- MuldenrandTrough edge
- 99
- FeuerstegTop land
- 1010
- RingfeldRing field
- 1111
- KĆ¼hlkanalCooling duct
- 1212
- AusnehmungRecess
- 1313
- Stegweb
- 1414th
- AusnehmungsgrundRecess reason
- 1515th
- VerbindungskanalConnection channel
- 1616
- Innerer KĆ¼hlraumInner fridge
- 1717th
- Innere WandungInner wall
- 1818th
- ĆuĆere WandungOuter wall
- 1919th
- schlitzfƶrmige Ausnehmungslot-shaped recess
- 2020th
- Stegweb
- 2121st
- KĆ¼hlschlitzCooling slot
- 2222nd
- KĆ¼hlschlitzCooling slot
Claims (16)
- Piston of an internal combustion engine, designed as a liquid-cooled piston, composed of a piston lower part and of a piston upper part (1) which has a combustion chamber depression (7), which piston lower part and piston upper part are supported and joined together by means of joining webs (2, 3) which are radially spaced apart from one another and which form a parting plane (4), wherein, in the piston upper part (1), there is formed a ring-shaped cooling channel (11) which extends into the piston lower part and which is connected via connecting channels (15) to an internal cooling chamber (16) and which has recesses (12) which are oriented in the direction of a piston crown (6) and which are formed as blind holes and which form cooling chambers, characterized in that the recesses (12) are designed to conically widen proceeding from the cooling channel (11) to a recess base (14) of the respective recess (12).
- Piston of an internal combustion engine, designed as a single-part liquid-cooled piston, having a piston lower part and a piston upper part (1) which has a combustion chamber depression (7), wherein, in the piston upper part (1), there is formed a ring-shaped cooling channel (11) which is connected via connecting channels (15) to an internal cooling chamber (16) and which has recesses (12) which are oriented in the direction of a piston crown (6) and which are designed as blind holes and which form cooling chambers, characterized in that the recesses (12) are designed to conically widen proceeding from the cooling channel (11) to a recess base (14) of the respective recess (12).
- Piston according to Claim 1, characterized in that the piston upper part (1) and the piston lower part are joined together cohesively, preferably by means of a welded connection, or in frictionally locking fashion, preferably by means of a screw connection.
- Piston according to any of Claims 1 to 3, characterized in that the recesses (12) which are formed in a circumferentially distributed manner in the piston upper part (1) and which are designed to rise in a conical shape are formed as bores, channels and/or slots.
- Piston according to any of Claims 1 to 4, characterized in that webs (13, 20) formed from a material of the piston upper part (1) are provided between the recesses (12) and the cooling channel (11).
- Piston according to any of Claims 1 to 5, characterized in that the recesses (12) formed in a circumferentially distributed manner in the piston upper part (1) form a honeycomb structure.
- Piston according to any of Claims 1 to 6, characterized in that recesses (12) formed adjacently in the piston upper part (1) are arranged so as to be inclined alternately radially inwards or radially outwards.
- Piston according to any of Claims 1 to 7, characterized in that the recesses (12) have oppositely inclined walls, in particular an inner wall (17) and an outer wall (18), the corresponding or mutually different angles of inclination "Ī±, Ī²" of which amount to between 0Ā° to 40Ā°.
- Piston according to any of Claims 1 to 8, characterized in that the recesses (12) have a recess base (14) which is of rounded or bevelled form with a radius "R" between 1.5 mm and D/2.
- Piston according to any of Claims 1 to 9, characterized in that the recesses (12) include a recess base (14) which is doubly rounded and/or rounded in a stepped manner.
- Piston according to any of Claims 1 to 10, characterized in that the conically widened recesses (12) formed as a bore, channel or slot are integrated in a circumferentially symmetrical or asymmetrical manner in the piston upper part (1).
- Method for producing a piston upper part (1) of a liquid-cooled piston of an internal combustion engine, which piston upper part is joined together with a piston lower part, wherein the piston upper part (1) has a combustion chamber depression (7) and a cooling channel (11) which is connected to recesses (12) which are oriented in the direction of a piston crown (6) and which are formed as blind holes, characterized in that, for the production of the recesses (12), the following steps are provided:- inserting a casting mould body which corresponds to the shape of the recess (12) and which is designed to conically widen proceeding from the cooling channel (11) to a recess base (14) of the respective recess (12) and which, prior to a casting process, is positioned in a casting mould designed for the piston upper part (1);- removing the casting mould body after casting has been performed, and cooling the piston upper part (12) by rinsing.
- Method for producing a single-piece liquid-cooled piston of an internal combustion engine, having a piston upper part (1) and a piston lower part, wherein the piston upper part (1) has a combustion chamber depression (7) and a cooling channel (11) which is connected to recesses (12) which are oriented in the direction of a piston crown (6) and which are formed as blind holes, characterized in that, for the production of the recesses (12), the following steps are provided:- inserting a casting mould body which corresponds to the shape of the recess (12) and which is designed to conically widen proceeding from the cooling channel (11) to a recess base (14) of the respective recess (12) and which, prior to a casting process, is positioned in a casting mould designed for the piston upper part (1) of the single-piece piston;- removing the casting mould body after casting has been performed, and cooling the piston upper part (12) of the single-piece piston by rinsing.
- Method for producing a piston upper part (1) of a liquid-cooled piston of an internal combustion engine, which piston upper part is joined together with a piston lower part, wherein the piston upper part (1) has a combustion chamber depression (7) and a cooling channel (11) which is connected to recesses (12) which are oriented in the direction of a piston crown (6) and which are formed as blind holes, characterized in that the production of the recesses (12) in the piston upper part (1) is performed by means of a mechanical, three-dimensional cutting machining process, such that the recesses (12) are designed to conically widen proceeding from the cooling channel (11) to a recess base (14) of the respective recess (12).
- Method according to Claim 14, characterized in that the piston upper part (1) is, prior to the formation of the recesses (12), produced by means of a deformation process, preferably by means of a forging process.
- Method according to Claim 12, 14 or 15, characterized in that the piston upper part (1) and the piston lower part are joined together cohesively, preferably by means of a welded connection, or in frictionally locking fashion, preferably by means of a screw connection.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102010015568A DE102010015568A1 (en) | 2010-04-19 | 2010-04-19 | Piston upper part of a built or welded piston with extended cooling chambers |
PCT/EP2011/000505 WO2011131266A1 (en) | 2010-04-19 | 2011-02-04 | Piston upper part of an assembled or welded piston with extended cooling spaces |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2561205A1 EP2561205A1 (en) | 2013-02-27 |
EP2561205B1 true EP2561205B1 (en) | 2020-09-23 |
Family
ID=43983548
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11703395.1A Active EP2561205B1 (en) | 2010-04-19 | 2011-02-04 | Piston upper part of an assembled or welded piston with extended cooling spaces |
Country Status (6)
Country | Link |
---|---|
US (1) | US8973548B2 (en) |
EP (1) | EP2561205B1 (en) |
KR (1) | KR101867631B1 (en) |
CN (1) | CN102859165B (en) |
DE (1) | DE102010015568A1 (en) |
WO (1) | WO2011131266A1 (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9464592B2 (en) | 2011-04-18 | 2016-10-11 | Achates Power, Inc. | Piston thermal management in an opposed-piston engine |
DE102011119525A1 (en) * | 2011-11-26 | 2013-05-29 | Mahle International Gmbh | Piston for an internal combustion engine |
WO2014001256A1 (en) * | 2012-06-27 | 2014-01-03 | Ks Kolbenschmidt Gmbh | Particular arrangement of a cooling duct connecting bore of a cooling duct |
JP6401188B2 (en) * | 2013-02-18 | 2018-10-03 | ćć§ćć©ć«āć¢ć¼ć°ć«ć»ćŖććććć»ć©ć¤ć¢ććŖćć£ć»ć«ć³ććć¼ļ¼¦ļ½ ļ½ļ½ ļ½ļ½ļ½āļ¼ļ½ļ½ļ½ļ½ ļ¼¬ļ½ļ½ | Complex shaped piston oil gallery with piston crown made by cast metal or powder metal process |
CN103925104B (en) * | 2014-05-07 | 2016-06-08 | å¹æč„æēę“ęŗåØč”份ęéå ¬åø | Piston cooling structure |
DE102015004688A1 (en) * | 2015-04-10 | 2016-10-13 | Caterpillar Motoren Gmbh & Co. Kg | Piston crown with injector pocket for combustion engines |
DE102015006642A1 (en) * | 2015-05-22 | 2016-11-24 | Caterpillar Motoren Gmbh & Co. Kg | PISTON-SUPPORTING ASSEMBLY |
US9797337B2 (en) | 2015-07-10 | 2017-10-24 | Mahle International Gmbh | Oil-cooled piston for an internal combustion engine |
US10294887B2 (en) | 2015-11-18 | 2019-05-21 | Tenneco Inc. | Piston providing for reduced heat loss using cooling media |
MX2018013353A (en) * | 2016-05-04 | 2019-02-20 | Ks Kolbenschmidt Gmbh | Piston. |
DE102016225632A1 (en) * | 2016-12-20 | 2018-06-21 | Mahle International Gmbh | Piston of an internal combustion engine |
US11067033B2 (en) | 2017-05-17 | 2021-07-20 | Tenneco Inc. | Dual gallery steel piston |
US10648425B2 (en) * | 2017-08-23 | 2020-05-12 | Tenneco Inc. | Piston with broad ovate gallery |
CN109519298B (en) * | 2017-09-19 | 2021-04-23 | å¼ŗčč | Combined piston |
US20200080587A1 (en) * | 2018-09-12 | 2020-03-12 | Pai Industries, Inc. | Forged Steel Cross-Head Piston |
US11326549B2 (en) * | 2020-01-21 | 2022-05-10 | Ford Global Technologies, Llc | 218-0266 volcano-shaped inlet of piston oil-cooling gallery |
CN114278455B (en) * | 2020-09-27 | 2023-12-19 | 马åę±½č½¦ęęÆļ¼äøå½ļ¼ęéå ¬åø | Piston with split-flow internal cooling flow channel |
DE102021203241A1 (en) * | 2021-03-30 | 2022-10-06 | Mahle International Gmbh | Piston for an internal combustion engine and method of manufacturing the piston |
DE102021128792B3 (en) | 2021-11-05 | 2022-07-07 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Piston for a reciprocating engine, corresponding engine and motor vehicle with such |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2882106A (en) * | 1954-06-24 | 1959-04-14 | Maschf Augsburg Nuernberg Ag | Piston for internal combustion engines |
DE2919638A1 (en) * | 1979-05-16 | 1980-11-20 | Schmidt Gmbh Karl | PISTON FOR INTERNAL COMBUSTION ENGINES |
DE102006024098A1 (en) * | 2006-05-23 | 2007-12-20 | Ks Kolbenschmidt Gmbh | Piston for internal combustion engine has cooling channel enclosing access channel narrowing in cross-section towards piston floor, inclined to annular field, leading directly or indirectly to annular support |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE411840C (en) * | 1924-09-07 | 1925-04-14 | Grimme | Device for returning a value from a counter arranged in a slide into the setting mechanism that drives this movement |
US3240193A (en) * | 1964-07-30 | 1966-03-15 | Gen Motors Corp | Piston and piston cooling means |
DE1245640B (en) * | 1964-11-25 | 1967-07-27 | Mahle Kg | Pistons for internal combustion engines |
US3613521A (en) * | 1968-11-07 | 1971-10-19 | Komatsu Mfg Co Ltd | Piston for internal combustion engine |
US4502422A (en) * | 1982-12-27 | 1985-03-05 | General Motors Corporation | High output oil cooled floating piston |
DE3518721C3 (en) * | 1985-05-24 | 1997-09-04 | Man B & W Diesel Ag | Oil-cooled, multi-part plunger of an internal combustion engine |
US5107807A (en) * | 1989-09-28 | 1992-04-28 | Nissan Motor Company, Ltd. | Piston for internal combustion engine |
DE4118400A1 (en) | 1990-06-29 | 1992-01-02 | Kolbenschmidt Ag | BUILT OIL-COOLED PISTON FOR DIESEL ENGINES |
DE19603589A1 (en) | 1996-02-01 | 1997-08-07 | Kolbenschmidt Ag | Pendulum shaft piston |
DE19750021A1 (en) | 1997-11-12 | 1999-05-20 | Mahle Gmbh | Cooled ring carrier |
GB9909034D0 (en) * | 1999-04-19 | 1999-06-16 | Seneca Tech Ltd | Piston coolant path |
GB2366607B (en) * | 2000-09-06 | 2004-06-09 | Federal Mogul Bradford Ltd | Piston for internal combustion engine |
US7356925B2 (en) * | 2002-06-25 | 2008-04-15 | Mahle Gmbh | Method for producing a cooled ring carrier |
DE10244513A1 (en) * | 2002-09-25 | 2004-04-08 | Mahle Gmbh | Multi-part cooled piston for an internal combustion engine and method for its production |
DE10244512A1 (en) | 2002-09-25 | 2004-04-15 | Mahle Gmbh | Multi-part cooled piston for an internal combustion engine |
DE10244511A1 (en) * | 2002-09-25 | 2004-04-15 | Mahle Gmbh | Multi-part cooled piston for an internal combustion engine |
DE102004057625A1 (en) * | 2004-11-30 | 2006-06-01 | Mahle International Gmbh | Two-part piston for combustion engine, has upper part configured in essentially annular manner, where upper part enlarges combustion chamber at piston head end while delimiting same in radially outward direction similar to flange |
DE102005061075A1 (en) * | 2005-12-21 | 2007-06-28 | Mahle International Gmbh | Piston for internal combustion engine has hub cooling channels arranged in bolt hub regions close to bottom of piston and each connected to cooling channel |
DE102007013183A1 (en) * | 2006-07-07 | 2008-01-17 | Ks Kolbenschmidt Gmbh | Cooling channel piston for an internal combustion engine |
DE102007018932A1 (en) * | 2007-04-21 | 2008-10-23 | Ks Kolbenschmidt Gmbh | Load-optimized interior of a piston |
JP4510061B2 (en) * | 2007-09-18 | 2010-07-21 | ēē éé ę Ŗå¼ä¼ē¤¾ | Manufacturing method of piston for internal combustion engine |
DE102008056203A1 (en) * | 2008-11-06 | 2010-05-12 | Mahle International Gmbh | Multi-part piston for an internal combustion engine and method for its production |
-
2010
- 2010-04-19 DE DE102010015568A patent/DE102010015568A1/en not_active Ceased
-
2011
- 2011-02-02 US US13/642,001 patent/US8973548B2/en active Active
- 2011-02-04 KR KR1020127026972A patent/KR101867631B1/en active IP Right Grant
- 2011-02-04 WO PCT/EP2011/000505 patent/WO2011131266A1/en active Application Filing
- 2011-02-04 CN CN201180014411.0A patent/CN102859165B/en active Active
- 2011-02-04 EP EP11703395.1A patent/EP2561205B1/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2882106A (en) * | 1954-06-24 | 1959-04-14 | Maschf Augsburg Nuernberg Ag | Piston for internal combustion engines |
DE2919638A1 (en) * | 1979-05-16 | 1980-11-20 | Schmidt Gmbh Karl | PISTON FOR INTERNAL COMBUSTION ENGINES |
DE102006024098A1 (en) * | 2006-05-23 | 2007-12-20 | Ks Kolbenschmidt Gmbh | Piston for internal combustion engine has cooling channel enclosing access channel narrowing in cross-section towards piston floor, inclined to annular field, leading directly or indirectly to annular support |
Also Published As
Publication number | Publication date |
---|---|
EP2561205A1 (en) | 2013-02-27 |
KR20130062904A (en) | 2013-06-13 |
WO2011131266A1 (en) | 2011-10-27 |
CN102859165B (en) | 2019-05-14 |
CN102859165A (en) | 2013-01-02 |
DE102010015568A1 (en) | 2011-10-20 |
KR101867631B1 (en) | 2018-06-14 |
US8973548B2 (en) | 2015-03-10 |
US20130032104A1 (en) | 2013-02-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2561205B1 (en) | Piston upper part of an assembled or welded piston with extended cooling spaces | |
DE4112889C2 (en) | Process for producing a piston head with cooling for a multi-part, articulated piston for internal combustion engines, and piston head produced thereafter | |
EP1778964B1 (en) | Lightweight piston comprising heat pipes | |
EP1561023B1 (en) | Multi-part cooled piston for an internal combustion engine and method for producing the same | |
EP1680256B1 (en) | Method for producing a piston for an internal combustion engine | |
EP3339617B1 (en) | Cylinder housing, method for producing a cylinder housing and casting core | |
EP2761210B1 (en) | Two-part steel piston for internal combustion engines | |
DE102006056013A1 (en) | Piston for internal-combustion engine, has radially rotating cooling ducts spaced apart from each other and integrated to piston head and ring zone, and forming vertically aligned cross sectional profile | |
WO2004029442A1 (en) | Multi-part cooled piston for an internal combustion engine | |
EP3394469B1 (en) | Internally ventilated brake disc | |
DE102009044812A1 (en) | hollow channels | |
DE102011085476A1 (en) | Functionally optimized design of a cylinder liner | |
DE102006022413B4 (en) | Ringbearer cooling channel | |
EP2738377B1 (en) | Process for manufacturing a cylinder crankcase | |
DE102004003980A1 (en) | Enclosed coolant tube manufacturing method for use in piston, involves incorporating coolant tube with circular opening in piston, and fixing tube cover in opening using adhesives to cover opening, where tube is made of forged steel | |
EP2440760A1 (en) | Light-metal piston having a multiple omega-shaped combustion bowl | |
DE102012000694A1 (en) | Method for preparing piston for combustion engine, involves preparing layer for forming recess portion for cooling medium and/or for forming determination element | |
DE10235910B4 (en) | Composite of cylinder liners made of light metal alloy, method for producing a composite and method for pouring a composite | |
DE112012001145T5 (en) | Motor arrangement for improved cooling | |
DE102017205384A1 (en) | Cylinder crankcase and internal combustion engine with such a cylinder crankcase | |
EP2890883B1 (en) | Piston | |
DE102009041392A1 (en) | Piston for internal combustion engine, particularly reciprocating piston engine, has upper piston area, which has ring carrier with ring groove and piston bowl | |
DE102014010156A1 (en) | Arrangement of a piston in a cylinder of a reciprocating internal combustion engine and piston for a reciprocating internal combustion engine | |
WO2020048883A1 (en) | Cylinder head for an internal combustion engine and method for the production thereof | |
WO2018184895A1 (en) | Piston of an internal combustion engine |
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: 20120911 |
|
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) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20180305 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20200424 |
|
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 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502011016911 Country of ref document: DE |
|
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: AT Ref legal event code: REF Ref document number: 1316609 Country of ref document: AT Kind code of ref document: T Effective date: 20201015 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20200923 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: 20200923 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: 20200923 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: 20201224 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: 20201223 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: 20201223 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20200923 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: 20200923 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20200923 |
|
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: 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: 20200923 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: 20200923 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: 20200923 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: 20210125 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: 20200923 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: 20200923 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: 20200923 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20200923 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: 20200923 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: 20210123 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: 20200923 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502011016911 Country of ref document: DE |
|
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: 20200923 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
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: 20200923 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: 20200923 |
|
26N | No opposition filed |
Effective date: 20210624 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20200923 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20210204 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20210228 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20210204 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210228 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210228 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: 20200923 |
|
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: 20210204 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210204 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210228 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1316609 Country of ref document: AT Kind code of ref document: T Effective date: 20210204 |
|
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: 20210204 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210228 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20110204 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: 20200923 |
|
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: 20200923 |
|
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: 14 |