EP0902180B1 - Lightweight metal piston for an internal combustion engine - Google Patents

Lightweight metal piston for an internal combustion engine Download PDF

Info

Publication number
EP0902180B1
EP0902180B1 EP98117145A EP98117145A EP0902180B1 EP 0902180 B1 EP0902180 B1 EP 0902180B1 EP 98117145 A EP98117145 A EP 98117145A EP 98117145 A EP98117145 A EP 98117145A EP 0902180 B1 EP0902180 B1 EP 0902180B1
Authority
EP
European Patent Office
Prior art keywords
piston
light metal
hubs
faces
cavity
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP98117145A
Other languages
German (de)
French (fr)
Other versions
EP0902180A3 (en
EP0902180A2 (en
Inventor
Johannes Spermann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
KS Kolbenschmidt GmbH
Original Assignee
KS Kolbenschmidt GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by KS Kolbenschmidt GmbH filed Critical KS Kolbenschmidt GmbH
Publication of EP0902180A2 publication Critical patent/EP0902180A2/en
Publication of EP0902180A3 publication Critical patent/EP0902180A3/en
Application granted granted Critical
Publication of EP0902180B1 publication Critical patent/EP0902180B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/26Pistons  having combustion chamber in piston head
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/02Light metals
    • F05C2201/021Aluminium

Definitions

  • the invention relates to a light metal piston for Internal combustion engines with a roof-shaped piston crown a particularly asymmetrical combustion chamber bowl.
  • the piston crown has two flat piston crown surfaces inclined towards each other, which over a common ridge line that runs parallel to the piston pin axis runs, merge and thereby the roof shape form, so that viewed in the piston pin direction Gable shape results.
  • DE-A-41 10 306 describes a non-roof-shaped piston with a very flat combustion chamber bowl known, the outer Hub distance is 0.4 to 0.7 of the piston diameter, and each above the outer surfaces of the recessed hubs an open cavity is provided which extends towards the piston crown in the area behind the ring field stretched in, and the hub inner surfaces are trapezoidal or are stepped.
  • the shaft length is 0.30 - 0.50 on the pressure side of the piston Piston diameter and on the counter pressure side 0.15 - 0.30 des Piston diameter.
  • Firing bowl shape affects the top heaviness due to Material accumulation in the head area due to the roof shape as disadvantageous, especially prepares the Piston noise in operation problems and there must be one relatively long shaft length can be used to the To guide pistons in the cylinder and as a result of Evenly absorb head-heavy forces and to be able to derive.
  • the object of the invention is to a piston of the type described above improve that the problems mentioned do not occur.
  • the top-heavyness of the piston is reduced.
  • the Reset of the hubs is done radially outside the outer surface the hub space for training the weight-reducing Cavities created above the hubs. It has shown, that by a trapezoidal or step-like formation of the inner hub surfaces due to the hub reset deteriorated power transmission to the piston pin again can be compensated by at least in the upper range the hub has a sufficient wing between the hub and the bolt is available.
  • the cavities extending into the area behind the ring field preferably extend at least to the level of groove upper flank delimiting the upper ring groove. If it is If the combustion chamber trough is allowed to form, the cavity can become also extend deeper into the piston crown to get the to bring about advantageous weight reduction even more effectively. It has been shown that when the cavity extends circumferentially less than 60 °, preferably 50 - 55 °, a weakening or twisting of the piston crown and of the ring field as a result of tensile and compressive stresses not even in a disadvantageous way if the cavity extends up to the named level of the top Extending annular groove flank edge.
  • One of the roof shapes has proven to be particularly advantageous appropriately optimized design of the cavity has been proven, after which the depth of the cavity starting from the through Piston pin axis and piston longitudinal axis plane formed in Circumferential direction decreases in both directions, d. H. that the depth of the cavity is analogous to the shape of the roof and, preferably according to the slope of the roof shape Sides decreases.
  • In a very particularly preferred embodiment of the Invention go the outer surfaces of the hubs flush in the Wall areas delimiting the cavity. This will be a high coolant exchange during piston operation favors and the manufacture of the piston in the casting process simplified. They go in a particularly advantageous manner Outer surfaces of the hubs towards the piston crown Wall surfaces delimiting the cavity without any undercuts over, whereby the manufacture in the chill casting process under Use of an undercut-free die casting tool is possible.
  • Piston shank By improving the tribological properties Coating of sections forming the sliding surfaces Piston shank can be the clearance of the piston in the cylinder be kept small.
  • the coating in the form of a Lubricating varnish reduces that due to the tilting movements of the piston the impact pulses transmitted to the cylinder wall. This will the noise occurring during operation is reduced and it becomes a Reduced risk of seizure due to reduced friction the sliding surfaces even under unfavorable load conditions in motor operation causes.
  • the figures show a light metal piston with a roof-shaped piston head 2 with a combustion chamber trough 4. At the Piston plate 2 closes a ring field 6 forming Circumferential section 8.
  • the one-piece piston comprises two Shaft wall sections 12 which form sliding surfaces 10 and which adhere connect the section 8 forming the ring field 6 and over Bolt hubs 14 forming a total of 16 provided connecting wall sections in the circumferential direction merge.
  • the hubs 14 are set back in such a way that the distance of the outer hub surfaces 18 from one another is 65% of the piston diameter D k .
  • the inner hub surfaces 20 are trapezoidal, so that the hubs taper in the direction of the free shaft end.
  • the hub outer surfaces 18 merge without undercuts and flush into the wall surfaces 24 delimiting the cavities 22.
  • the height or depth of the cavities 22 measured in the longitudinal direction of the piston is such that they extend to the plane indicated by reference numeral 26 in FIG. 1, which is defined by the groove flank 28 delimiting the upper annular groove.
  • the shaft length L s is 42% of the piston diameter D k .
  • the piston is made of a light metal alloy, preferably a heat-resistant aluminum alloy with 11 - 13% by weight Si, 3.3 - 4.2% by weight Cu, 1.8 - 2.5% by weight Ni manufactured. Due to the shape described above the top heaviness of the piston can be provided by the Reduce voids 22 so that it is relatively short Shaft length can be chosen without being distracting Running noises occur or as a result of increased Tilting movements the lateral forces on the cylinder wall and thus the wear is increased. Forming on the sliding surfaces 10 Shaft wall sections 12 is also a tribological one Properties-improving coating 30 applied.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Description

Die Erfindung betrifft einen Leichtmetallkolben für Brennkraftmaschinen mit einem dachförmigen Kolbenboden mit einer insbesondere asymmetrisch ausgebildeten Brennraummulde.The invention relates to a light metal piston for Internal combustion engines with a roof-shaped piston crown a particularly asymmetrical combustion chamber bowl.

Ein derartiger Kolben ist bekannt. Der Kolbenboden weist zwei gegeneinander geneigte ebene Kolbenbodenflächen auf, die über eine gemeinsame Firstlinie, die parallel zur Kolbenbolzenachse verläuft, ineinander übergehen und hierdurch die Dachform bilden, so dass sich in Kolbenbolzenrichtung betrachtet eine Giebelform ergibt. Such a piston is known. The piston crown has two flat piston crown surfaces inclined towards each other, which over a common ridge line that runs parallel to the piston pin axis runs, merge and thereby the roof shape form, so that viewed in the piston pin direction Gable shape results.

Aus DE-A-41 10 306 ist ein nichtdachförmiger Kolben mit einer sehr flachen Brennraummulde bekannt, wobei der äußere Nabenabstand 0,4 bis 0,7 des Kolbendurchmessers beträgt, und jeweils oberhalb der Außenflächen der zurückgesetzten Naben ein offener Hohlraum vorgesehen ist, der sich in Richtung auf den Kolbenboden in den Bereich hinter dem Ringfeld hineinerstreckt, und wobei die Nabeninnenflächen trapezförmig oder stufenförmig abgesetzt ausgebildet sind. Die Schaftlänge beträgt auf der Druckseite des Kolbens 0,30 - 0,50 des Kolbendurchmessers und auf der Gegendruckseite 0,15 - 0,30 des Kolbendurchmessers.DE-A-41 10 306 describes a non-roof-shaped piston with a very flat combustion chamber bowl known, the outer Hub distance is 0.4 to 0.7 of the piston diameter, and each above the outer surfaces of the recessed hubs an open cavity is provided which extends towards the piston crown in the area behind the ring field stretched in, and the hub inner surfaces are trapezoidal or are stepped. The shaft length is 0.30 - 0.50 on the pressure side of the piston Piston diameter and on the counter pressure side 0.15 - 0.30 des Piston diameter.

Aus DE-A-42 10 056 ist ein weiterer nichtdachförmiger Kolben bekannt, wobei der äußere Nabenabstand soweit aus der Zeichnung entnehmbar etwa 55 % des Kolbendurchmessers beträgt, und wobei jeweils oberhalb der Außenflächen der zurückgesetzten Naben ein offener Hohlraum vorgesehen ist, der sich in Richtung auf den Kolbenboden in den Bereich hinter dem Ringfeld bis zu der Ebene der die obere Ringnut begrenzenden Nutoberflanke hineinerstreckt.Another non-roof-shaped piston is known from DE-A-42 10 056 known, the outer hub distance as far from the Removable drawing is about 55% of the piston diameter, and each above the outer surfaces of the recessed hubs an open cavity is provided which towards the piston crown in the area behind the Ring field up to the level of the upper ring groove Grooved upper flank.

Bei dachförmigen Kolben mit einer im Hinblick auf das spezielle Verbrennungsverfahren optimierten Brennraummuldenform wirkt sich die Kopflastigkeit aufgrund der Materialanhäufung im Kopfbereich infolge der Dachform als nachteilig aus, insbesondere bereitet die Kolbengeräuschbildung im Betrieb Probleme, und es muss eine verhältnismäßig lange Schaftlänge verwendet werden, um den Kolben im Zylinder zu führen und die infolge der Kopflastigkeit auftretenden Kräfte gleichmäßig aufnehmen und ableiten zu können.With roof-shaped pistons with a view to that optimized special combustion processes Firing bowl shape affects the top heaviness due to Material accumulation in the head area due to the roof shape as disadvantageous, especially prepares the Piston noise in operation problems and there must be one relatively long shaft length can be used to the To guide pistons in the cylinder and as a result of Evenly absorb head-heavy forces and to be able to derive.

Hiervon ausgehend liegt der Erfindung die Aufgabe zugrunde, einen Kolben der eingangs beschriebenen Art dahingehend zu verbessern, dass die erwähnten Probleme nicht auftreten.Proceeding from this, the object of the invention is to a piston of the type described above improve that the problems mentioned do not occur.

Diese Aufgabe wird bei einem Kolben der genannten Art erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst.This task is carried out with a piston of the type mentioned solved according to the invention by the features of claim 1.

Mit den vorstehend genannten Merkmalen wird erfindungsgemäß die Kopflastigkeit des Kolben reduziert. Durch die Zurücksetzung der Naben wird radial außerhalb der Außenfläche der Naben Raum für die Ausbildung der gewichtsreduzierenden Hohlräume oberhalb der Naben geschaffen. Es hat sich gezeigt, dass durch eine trapezförmige oder stufenförmige Ausbildung der Nabeninnenflächen die infolge der Nabenzurücksetzung verschlechterte Kraftübertragung auf den Kolbenbolzen wieder ausgeglichen werden kann, indem zumindest im oberen Bereich der Nabe eine hinreichende Tragfläche zwischen Nabe und Bolzen zur Verfügung steht.With the features mentioned above, the invention the top-heavyness of the piston is reduced. Through the Reset of the hubs is done radially outside the outer surface the hub space for training the weight-reducing Cavities created above the hubs. It has shown, that by a trapezoidal or step-like formation of the inner hub surfaces due to the hub reset deteriorated power transmission to the piston pin again can be compensated by at least in the upper range the hub has a sufficient wing between the hub and the bolt is available.

Es hat sich gezeigt, dass sich ein erfindungsgemäßer Kolben besonders für den Einsatz mit direkter Kraftstoffeinspritzung bei einem Otto-Motor eignet. It has been shown that a piston according to the invention especially for use with direct fuel injection suitable for an Otto engine.

Bei einer trapezförmigen Ausgestaltung der Nabeninnenflächen hat es sich als vorteilhaft erwiesen, wenn diese unter einem Winkel von 10 bis 15° zur Kolbenlängsachse geneigt verlaufen.With a trapezoidal design of the inner hub surfaces it has proven to be advantageous if this under one Angles of 10 to 15 ° to the longitudinal axis of the piston are inclined.

Die in den Bereich hinter dem Ringfeld erstreckten Hohlräume erstrecken sich vorzugsweise wenigstens bis über die Ebene der die obere Ringnut begrenzenden Nutoberflanke. Sofern es die Ausbildung der Brennraummulde zulässt, kann sich der Hohlraum auch tiefer in den Kolbenboden hineinerstrecken, um die vorteilhafte Gewichtsreduzierung noch effektiver zu bewirken. Es hat sich gezeigt, dass bei einer Erstreckung des Hohlraums in Umfangsrichtung von weniger als 60°, vorzugsweise von 50 - 55°, eine Schwächung bzw. eine Verwindung des Kolbenbodens und des Ringfelds infolge auftretender Zug- und Druckspannungen auch dann nicht in nachteiliger Weise bemerkbar macht, wenn sich der Hohlraum bis zu der genannten Ebene der die obere Ringnut begrenzenden Nutflanke erstreckt.The cavities extending into the area behind the ring field preferably extend at least to the level of groove upper flank delimiting the upper ring groove. If it is If the combustion chamber trough is allowed to form, the cavity can become also extend deeper into the piston crown to get the to bring about advantageous weight reduction even more effectively. It has been shown that when the cavity extends circumferentially less than 60 °, preferably 50 - 55 °, a weakening or twisting of the piston crown and of the ring field as a result of tensile and compressive stresses not even in a disadvantageous way if the cavity extends up to the named level of the top Extending annular groove flank edge.

Als ganz besonders vorteilhaft hat sich eine der Dachform entsprechend optimierte Ausgestaltung des Hohlraums erwiesen, wonach die Tiefe des Hohlraums ausgehend von der durch Kolbenbolzenachse und Kolbenlängsachse gebildeten Ebene in Umfangsrichtung nach beiden Richtungen hin abnimmt, d. h. dass die Tiefe des Hohlraums analog der Dachform verläuft und, vorzugsweise der Neigung der Dachform entsprechend, zu den Seiten hin abnimmt. One of the roof shapes has proven to be particularly advantageous appropriately optimized design of the cavity has been proven, after which the depth of the cavity starting from the through Piston pin axis and piston longitudinal axis plane formed in Circumferential direction decreases in both directions, d. H. that the depth of the cavity is analogous to the shape of the roof and, preferably according to the slope of the roof shape Sides decreases.

Bei einer ganz besonders bevorzugten Ausführungsform der Erfindung gehen die Außenflächen der Naben bündig in den Hohlraum begrenzende Wandflächen über. Hierdurch wird ein hoher Kühlmittelaustausch im Betrieb des Kolbens begünstigt und die Herstellung des Kolbens im Gießprozess wird vereinfacht. In ganz besonders vorteilhafter Weise gehen die Außenflächen der Naben in Richtung auf den Kolbenboden hinterschneidungsfrei in den Hohlraum begrenzende Wandflächen über, wodurch die Herstellung im Kokillengießverfahren unter Verwendung eines hinterschneidungsfreien Kokillengießwerkzeugs möglich ist.In a very particularly preferred embodiment of the Invention go the outer surfaces of the hubs flush in the Wall areas delimiting the cavity. This will be a high coolant exchange during piston operation favors and the manufacture of the piston in the casting process simplified. They go in a particularly advantageous manner Outer surfaces of the hubs towards the piston crown Wall surfaces delimiting the cavity without any undercuts over, whereby the manufacture in the chill casting process under Use of an undercut-free die casting tool is possible.

Durch eine die tribologischen Eigenschaften verbessernde Beschichtung von Gleitflächen bildenden Abschnitten des Kolbenschafts kann das Einbauspiel des Kolbens im Zylinder klein gehalten werden. Die Beschichtung in Form eines Gleitlacks vermindert die durch Kippbewegungen des Kolbens an die Zylinderwand übertragenen Aufschlagimpulse. Dadurch wird das im Betrieb auftretende Geräusch reduziert und es wird eine Verminderung der Fressgefahr durch herabgesetzte Reibkräfte an den Gleitflächen auch unter ungünstigen Lastzuständen im motorischen Betrieb bewirkt.By improving the tribological properties Coating of sections forming the sliding surfaces Piston shank can be the clearance of the piston in the cylinder be kept small. The coating in the form of a Lubricating varnish reduces that due to the tilting movements of the piston the impact pulses transmitted to the cylinder wall. This will the noise occurring during operation is reduced and it becomes a Reduced risk of seizure due to reduced friction the sliding surfaces even under unfavorable load conditions in motor operation causes.

Weitere Merkmale, Einzelheiten und Vorteile der Erfindung ergeben sich aus den beigefügten Ansprüchen und der zeichnerischen Darstellung und nachfolgenden Beschreibung einer bevorzugten Ausführungsform des erfindungsgemäßen Kolbens.

Figur 1
zeigt einen Längsschnitt durch die von Kolbenlängsachse und Kolbenbolzenachse gebildete Ebene; und
Figur 2
zeigt eine Ansicht auf die Ebene II-II in Figur 1; und
Figur 3
eine Seitenansicht des Kolbens in Richtung der Kolbenbolzenachse.
Further features, details and advantages of the invention result from the appended claims and the drawing and the following description of a preferred embodiment of the piston according to the invention.
Figure 1
shows a longitudinal section through the plane formed by the longitudinal piston axis and piston pin axis; and
Figure 2
shows a view of the plane II-II in Figure 1; and
Figure 3
a side view of the piston in the direction of the piston pin axis.

Die Figuren zeigen einen Leichtmetallkolben mit einem dachförmigen Kolbenboden 2 mit einer Brennraummulde 4. An den Kolbenboden 2 schließt sich ein das Ringfeld 6 bildender Umfangsabschnitt 8 an. Der einteilige Kolben umfasst zwei Gleitflächen 10 bildende Schaftwandabschnitte 12, die sich an den das Ringfeld 6 bildenden Abschnitt 8 anschließen und über Bolzennaben 14 bildende insgesamt mit dem Bezugszeichen 16 versehene Verbindungswandabschnitte in Umfangsrichtung ineinander übergehen.The figures show a light metal piston with a roof-shaped piston head 2 with a combustion chamber trough 4. At the Piston plate 2 closes a ring field 6 forming Circumferential section 8. The one-piece piston comprises two Shaft wall sections 12 which form sliding surfaces 10 and which adhere connect the section 8 forming the ring field 6 and over Bolt hubs 14 forming a total of 16 provided connecting wall sections in the circumferential direction merge.

Die Naben 14 sind derart zurückgesetzt, dass der Abstand der Nabenaußenflächen 18 voneinander 65 % des Kolbendurchmessers Dk aufweist. Wie aus der Figur 1 ersichtlich verlaufen die Nabeninnenflächen 20 trapezförmig, so dass sich die Naben in Richtung auf das freie Schaftende verjüngen. Durch die Zurücksetzung der Naben 14 bzw. der Nabenaußenflächen 18 entstehen in Umfangsrichtung auf Breite der Naben und senkrecht zur Kolbenbolzenachse x Freiräume für die Ausbildung eines im Wesentlichen senkrecht zur Kolbenbolzenachse x in Richtung auf den Kolbenboden 2 erstreckten Hohlraums 22. Die Hohlräume 22 überspannen in Umfangsrichtung ein Kreisbogensegment von 55°. Sie sind zur Kolbenbolzenlängsachse x symmetrisch ausgebildet. Die Nabenaußenflächen 18 gehen hinterschneidungsfrei und bündig in die Hohlräume 22 begrenzende Wandflächen 24 über. Die Höhe bzw. Tiefe der Hohlräume 22 in Kolbenlängsrichtung gemessen ist derart, dass sie sich bis zu der mit dem Bezugszeichen 26 in der Figur 1 angedeuteten Ebene erstrecken, welche durch die die obere Ringnut begrenzende Nutflanke 28 definiert ist.The hubs 14 are set back in such a way that the distance of the outer hub surfaces 18 from one another is 65% of the piston diameter D k . As can be seen from FIG. 1, the inner hub surfaces 20 are trapezoidal, so that the hubs taper in the direction of the free shaft end. By resetting the hubs 14 or the hub outer surfaces 18, in the circumferential direction on the width of the hubs and perpendicular to the piston pin axis x, free spaces are created for the formation of a cavity 22 which extends essentially perpendicular to the piston pin axis x in the direction of the piston crown 2. The cavities 22 span in the circumferential direction a circular arc segment of 55 °. They are symmetrical to the longitudinal axis x of the piston pin. The hub outer surfaces 18 merge without undercuts and flush into the wall surfaces 24 delimiting the cavities 22. The height or depth of the cavities 22 measured in the longitudinal direction of the piston is such that they extend to the plane indicated by reference numeral 26 in FIG. 1, which is defined by the groove flank 28 delimiting the upper annular groove.

Die Schaftlänge Ls beträgt 42 % des Kolbendurchmessers Dk.The shaft length L s is 42% of the piston diameter D k .

Der Kolben ist aus einer Leichtmetalllegierung, vorzugsweise einer hochwarmfesten Aluminiumlegierung mit insbesondere 11 - 13 Gew.% Si, 3,3 - 4,2 Gew.% Cu, 1,8 - 2,5 Gew.% Ni hergestellt. Durch die vorstehend beschriebene Formgebung lässt sich die Kopflastigkeit des Kolbens durch Vorsehen der Hohlräume 22 reduzieren, so dass eine verhältnismäßig kurze Schaftlänge gewählt werden kann, ohne dass störende Laufgeräusche auftreten oder infolge verstärkter Kippbewegungen die Seitenkräfte auf die Zylinderwand und damit der Verschleiß erhöht wird. Auf die Geitflächen 10 bildenden Schaftwandabschnitte 12 ist zusätzlich eine die tribologischen Eigenschaften verbessernde Beschichtung 30 aufgebracht.The piston is made of a light metal alloy, preferably a heat-resistant aluminum alloy with 11 - 13% by weight Si, 3.3 - 4.2% by weight Cu, 1.8 - 2.5% by weight Ni manufactured. Due to the shape described above the top heaviness of the piston can be provided by the Reduce voids 22 so that it is relatively short Shaft length can be chosen without being distracting Running noises occur or as a result of increased Tilting movements the lateral forces on the cylinder wall and thus the wear is increased. Forming on the sliding surfaces 10 Shaft wall sections 12 is also a tribological one Properties-improving coating 30 applied.

Claims (8)

  1. Light metal piston for internal-combustion engines with a roof-shaped piston head (2) with two flat piston head faces inclined toward one another and forming the roof shape, and with a combustion chamber hollow (4), wherein the hubs (14) are set back in the pin axis direction (x) in such a way that the outer hub spacing is 60 to 65% of the piston diameter (Dk) or less and in that above the respective outer faces (18) of the set-back hubs (14) an open cavity (22) enclosing an angle (α) between 45 and 60° in the peripheral direction is provided, extending in the direction of the piston head (2) into the region behind the annular field (6) at least up to the plane (26) of the upper groove flank (28) delimiting the upper annular groove, and the depth of the cavity (22) starting from the plane formed by the piston pin axis and longitudinal axis of the piston decreases in the peripheral direction to both sides and wherein the internal faces of the hubs (20) are designed to be trapezoidal or offset in a step-like manner and the shaft length (Ls) amounts to 40 to 45% of the piston diameter (Dk).
  2. Light metal piston according to claim 1, characterised in that the internal faces (20) of the hubs (14) extend inclined at an angle of 10 to 15° to the longitudinal axis of the piston.
  3. Light metal piston according to claim 1 or 2, characterised in that the depth of the cavities (22) decreases according to the inclination of the roof shape of the piston head (2).
  4. Light metal piston according to any one of the preceding claims, characterised in that the external faces (18) of the hubs pass flush into the wall faces (24) delimiting the cavity (22).
  5. Light metal piston according to any one of the preceding claims, characterised in that the external faces (18) of the hubs (14) pass without an undercut into the wall faces (24) delimiting the cavity (22) in the direction of the piston head (2).
  6. Light metal piston according to any one of the preceding claims, characterised in that portions (12) of the piston shaft forming sliding faces (10) have a coating (30) improving the tribological characteristics.
  7. Light metal piston according to any one of the preceding claims, characterised in that it is cast from an aluminium alloy with 11 to 13% by weight Si, 3.3 to 4.2% by weight Cu and 1.8 to 2.5% by weight Ni.
  8. Light metal piston according to claim 7, characterised in that it is produced by the chill casting method.
EP98117145A 1997-09-12 1998-09-10 Lightweight metal piston for an internal combustion engine Expired - Lifetime EP0902180B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19740065A DE19740065A1 (en) 1997-09-12 1997-09-12 Light alloy pistons for internal combustion engines
DE19740065 1997-09-12

Publications (3)

Publication Number Publication Date
EP0902180A2 EP0902180A2 (en) 1999-03-17
EP0902180A3 EP0902180A3 (en) 1999-12-15
EP0902180B1 true EP0902180B1 (en) 2002-11-13

Family

ID=7842099

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98117145A Expired - Lifetime EP0902180B1 (en) 1997-09-12 1998-09-10 Lightweight metal piston for an internal combustion engine

Country Status (2)

Country Link
EP (1) EP0902180B1 (en)
DE (2) DE19740065A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10865734B2 (en) 2017-12-06 2020-12-15 Ai Alpine Us Bidco Inc Piston assembly with offset tight land profile

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002327624A (en) * 2001-02-28 2002-11-15 Honda Motor Co Ltd Internal combustion engine
DE10145589B4 (en) * 2001-09-15 2006-09-14 Ks Kolbenschmidt Gmbh Piston for an internal combustion engine
US6745745B2 (en) * 2002-02-22 2004-06-08 General Motors Corporation Combustion chamber for reverse tumble spark ignition direct injection engine
JP2005248949A (en) * 2004-02-06 2005-09-15 Yamaha Motor Co Ltd Internal combustion engine
KR20080063269A (en) * 2005-08-29 2008-07-03 카에스 콜벤슈미트 게엠베하 Lightweight piston
DE102013009415A1 (en) * 2013-06-05 2014-12-11 Man Diesel & Turbo Se Piston of an internal combustion engine
WO2017025608A1 (en) 2015-08-11 2017-02-16 Ks Kolbenschmidt Gmbh Piston for an internal combustion engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2295199A (en) * 1941-12-27 1942-09-08 Wright Aeronautical Corp Piston
DE3723005C2 (en) * 1987-07-11 1996-12-05 Eberhard Fezer Plunger pistons for internal combustion engines
DE4110306A1 (en) * 1990-09-20 1992-03-26 Mahle Gmbh SUBMERSIBLE ALLOY PISTON FOR OTTO ENGINES
DE4210056A1 (en) * 1992-03-27 1993-09-30 Mahle Gmbh Reciprocating piston of an internal combustion engine
DE4229071A1 (en) * 1992-09-01 1994-03-03 Kolbenschmidt Ag Light alloy piston, for internal combustion engines - comprises insert made of pressed, sintered chips of metallic material
DE4434994C2 (en) * 1994-09-30 1998-02-19 Porsche Ag Pistons for internal combustion engines
DE19510050A1 (en) * 1995-03-20 1996-09-26 Mahle Gmbh Lightweight, cast piston for IC engine
DE19530631B4 (en) * 1995-08-21 2005-09-22 Mahle Gmbh Piston for internal combustion engines with a split piston pin
DE19537028A1 (en) * 1995-10-05 1997-04-10 Iav Gmbh Roll-shaped combustion cavity for diesel engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10865734B2 (en) 2017-12-06 2020-12-15 Ai Alpine Us Bidco Inc Piston assembly with offset tight land profile

Also Published As

Publication number Publication date
DE19740065A1 (en) 1999-03-18
DE59806259D1 (en) 2002-12-19
EP0902180A3 (en) 1999-12-15
EP0902180A2 (en) 1999-03-17

Similar Documents

Publication Publication Date Title
DE60220925T2 (en) ONE PIECE PISTON FOR DIESEL ENGINES
DE69711375T2 (en) PISTON FOR AN INTERNAL COMBUSTION ENGINE
EP0714479B1 (en) Piston for internal combustion engines, especially diesel engines
EP0171825B1 (en) Light-metal piston for an internal-combustion engine
DE2253868B2 (en) One-piece cast iron piston connected to a connecting rod
DE102007013183A1 (en) Cooling channel piston for an internal combustion engine
EP1483493A1 (en) Multi-part, cooled piston for an internal combustion engine
EP0902180B1 (en) Lightweight metal piston for an internal combustion engine
EP2129899B1 (en) Piston for an internal combustion engine
DE19848649C2 (en) Carbon pistons for an internal combustion engine
DE19726922A1 (en) Balance shafts with minimal mass
WO2017025608A1 (en) Piston for an internal combustion engine
DE4010805A1 (en) REINFORCED PISTON
WO2010142389A1 (en) Light-metal piston having a multiple omega-shaped combustion bowl
DE102012008690B4 (en) Arrangement of a piston and a piston pin for a passenger car diesel engine
DE10216329A1 (en) Combustion engine assembly sequence starts by pre-assembly of drive group with bearings with crossways oil channel grooved out in crankcase and branched out to main crankshaft bearing
DE102005004486B4 (en) Bushing for pouring into an engine block
EP0705968A1 (en) Piston for internal combustion engine
DE4441450B4 (en) Light metal pistons for internal combustion engines
DE19540763C1 (en) Casing for reciprocating piston engine
DE19908670C2 (en) Pistons for internal combustion engines
DE60216631T2 (en) PISTON FOR INTERNAL COMBUSTION ENGINE
DE102019219378A1 (en) Cylinder liner for an internal combustion engine
DE3243882C2 (en)
DE3820473A1 (en) Trunk piston for internal combustion engines

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

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): DE FR GB IT

AX Request for extension of the european patent

Free format text: AL;LT;LV;MK;RO;SI

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

17P Request for examination filed

Effective date: 19990917

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

AX Request for extension of the european patent

Free format text: AL;LT;LV;MK;RO;SI

RIC1 Information provided on ipc code assigned before grant

Free format text: 6F 02F 3/00 A, 6F 02F 3/26 B

AKX Designation fees paid

Free format text: DE FR GB IT

17Q First examination report despatched

Effective date: 20010924

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

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 PRE;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.SCRIBED TIME-LIMIT

Effective date: 20021113

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REF Corresponds to:

Ref document number: 59806259

Country of ref document: DE

Date of ref document: 20021219

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20030221

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

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

26N No opposition filed

Effective date: 20030814

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

Ref country code: GB

Payment date: 20060921

Year of fee payment: 9

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

Ref country code: FR

Payment date: 20060922

Year of fee payment: 9

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

Effective date: 20070910

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20080531

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

Ref country code: FR

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

Effective date: 20071001

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

Ref country code: GB

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

Effective date: 20070910

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

Ref country code: DE

Payment date: 20100922

Year of fee payment: 13

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 59806259

Country of ref document: DE

Effective date: 20120403

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

Ref country code: DE

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

Effective date: 20120403