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EP2188513A1 - Two-piece piston for an internal combustion engine - Google Patents

Two-piece piston for an internal combustion engine

Info

Publication number
EP2188513A1
EP2188513A1 EP08801217A EP08801217A EP2188513A1 EP 2188513 A1 EP2188513 A1 EP 2188513A1 EP 08801217 A EP08801217 A EP 08801217A EP 08801217 A EP08801217 A EP 08801217A EP 2188513 A1 EP2188513 A1 EP 2188513A1
Authority
EP
European Patent Office
Prior art keywords
piston
solder joint
ring element
circumferential
ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP08801217A
Other languages
German (de)
French (fr)
Other versions
EP2188513B1 (en
Inventor
Jochen Kortas
Timo Estrum
Dieter Messmer
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.)
Mahle International GmbH
Original Assignee
Mahle International 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 Mahle International GmbH filed Critical Mahle International GmbH
Publication of EP2188513A1 publication Critical patent/EP2188513A1/en
Application granted granted Critical
Publication of EP2188513B1 publication Critical patent/EP2188513B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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 
    • F02F3/0015Multi-part pistons
    • F02F3/003Multi-part pistons the parts being connected by casting, brazing, welding or clamping
    • 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 
    • F02F3/16Pistons  having cooling means
    • F02F3/20Pistons  having cooling means the means being a fluid flowing through or along piston
    • F02F3/22Pistons  having cooling means the means being a fluid flowing through or along piston the fluid being liquid
    • 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 
    • F02F3/0015Multi-part pistons
    • F02F3/003Multi-part pistons the parts being connected by casting, brazing, welding or clamping
    • F02F2003/0038Multi-part pistons the parts being connected by casting, brazing, welding or clamping by brazing

Definitions

  • the invention relates to a two-part piston for an internal combustion engine according to the preamble of claim 1.
  • a multi-part piston for an internal combustion engine which has a base body, on the underside of two pin bosses are formed. On the underside of the body is connected to a piston skirt and on the top radially outward with a ring member.
  • a brazing process i.e., a brazing process.
  • the ring element has a first solder joint on the radial inner side of the part of the piston crown formed by the ring element. Since both the part of the piston crown formed by the main body and by the ring element are very thin-walled, there is the disadvantage that the solder joint also has a very small axial length and thus a very low strength.
  • the ring element On the side facing away from the piston crown, the ring element is also connected to the base body via a relatively long, lower solder joint seen in the radial direction. If in this case the piston crown due to a pressure load due to the taking place in the combustion chamber cavity, explosive combustion of the fuel-air mixture and because of prevailing in the region of the piston crown, very high temperatures in the radial direction partly pressure and partly due to temperature expands, the ring element widened funnel-shaped, and the lower solder joint is subjected to a large tensile load.
  • the known from the prior art piston has the disadvantage that in the area of the lower solder joint no constructive measures are provided to reduce this tensile load on the lower solder joint. To avoid these disadvantages of the prior art is an object of the invention. This problem is solved with the features in the characterizing part of the main claim. Advantageous embodiments of the invention are the subject of the dependent claims.
  • FIG. 1 is an exploded view of the piston according to the invention, consisting of a piston body and a ring member,
  • FIG. 2 is a perspective view of the piston according to the invention after its assembly
  • FIG. 3 shows a section through the piston along the piston axis and the line III-III in Fig. 2,
  • FIG. 6 shows a partial section through the piston blank in the region of the cooling channel.
  • FIG. 1 shows an exploded view of a piston 1, which consists of a piston base body 2 and a ring element 3.
  • the piston base body 2 and the ring element 3 are made of AFP steel, ie, of a microalloyed, precipitation-hardening, ferritic-pearlitic manganese-vanadium-based steel according to DIN EN 10267.
  • the piston main body 2 and the ring element 3 are used in the context of Assembly of the piston 1 soldered together.
  • the ring member 3 forms the essential part of the annular piston crown 4 and has on its radial outer side a ring portion 5 to Recording in the figure not shown piston rings.
  • a round opening 7 is introduced, which is bounded near the piston head 4 by a first, cylindrical surface 8, which serves as a soldering surface during assembly of the piston 1.
  • the piston main body 2 consists of a substantially plate-shaped and round center part 9, on its underside facing away from the piston bottom 4, two opposing shaft elements 10 and two opposing and this shaft elements 10 interconnecting pin bosses 11 are formed.
  • the radially outer end faces 12 of the pin bosses 11 are set back relative to the radially outer boundary 13 of the middle part 9 in the direction of the piston axis 6.
  • a peripheral, channel-shaped recess 14 is formed radially outwardly, surrounded by a circumferential inner annular rib 15 arranged radially on the upper side of the middle part 9, the interior of which forms the combustion recess 16 of the piston 1.
  • the annular rib 15 and the combustion bowl 16 are not rotationally symmetrical to the piston axis 6, but have radially outward a dent 17 whose purpose is to improve the combustion of the fuel-air mixture in the combustion bowl 16.
  • the piston crown side, the boundary of the annular rib 15 is circular, so that a part of the piston head 4 1 is formed thereof.
  • a radially outer, second cylindrical surface 18 is also formed, which also serves as a counterpart to the first surface 8 of the ring member 3 as a soldering surface and the surface 8 an upper solder joint (23, see Fig. 3) between the ring member 3 and the Piston body 2 forms.
  • annular, third surface 19 which serves as a soldering surface and with a not shown in Fig. 1, on - A -
  • the lower end face of the ring member 3, fourth and also serving as a soldering surface 20 forms a lower solder joint between the ring member 3 and the piston body 2. (See also Fig. 3.)
  • the section shown in Fig. 3 by the piston along the piston axis 6 and the line IH-III in Fig. 2 shows a radially outside of the ring member 3, radially inwardly of the annular rib 15 and below of the recess 14 of the central part 9 of the piston main body second limited, annular, cooling channel 21, not shown in the figure and opening into the piston interior 22 ⁇ lzurios- and ⁇ lab Concretekanä- Ie. Shown are also formed by the first and second surfaces 8 and 18, axially aligned, upper solder joint 23 and formed by the third and fourth surfaces 19 and 20, radially oriented, lower solder joint 24 between the piston body 2 and the ring member third
  • the first surface 8 in this case represents the radially inner boundary of the piston crown 4 forming deck portion 25 of the ring member 3, wherein in the piston bottom side facing away from the deck area 25 an upwardly directed, circumferential recess 26 is formed, here a peripheral, upper, diluted wall portion 49 forms.
  • the ratio between the length b of the upper solder joint 23 and the minimum thickness a of the upper thinned wall portion 49 is between 1 and 3, that is, 1 ⁇ b / a ⁇ 3.
  • the fourth surface 20 which forms the lower end face of the ring element 3
  • the recess 27 is disposed between the ring portion 5 and the lower solder joint 24.
  • FIG. 4 an embodiment of the piston V in the region of the cooling channel 21 'is shown, in which the upper deck area 25' of the ring element 3 "in the region of the upper, thinned wall portion 49 extends radially inwards only up to the area of the smallest wall thickness a and
  • a radially inner, cylindrical surface 31 forms, which forms an upper solder joint 32 with a radially outer, cylindrical surface 29 of a piston crown side integrally formed on the annular rib 15, circumferential and radially outwardly directed collar 30.
  • the surface 29 is delimited by a step-shaped circumferential molding 34 on which the radially inner end of the cover region 25 'rests.
  • the piston bottom facing away from end face 20 'of the ring member 3 has in the embodiment of FIG. 4 radially inside a circumferential, stepped recess 35 which is dimensioned so that they on a piston bottom side on the radially outer boundary 13' of the central part 9 'integrally formed, circumferential Collar 36 fits, so that upon assembly of the piston 1 ', the ring member 3 "is pushed onto the collar 36 until the collar 36 is seated in the recess 35, and the cover portion 25' of the ring member 3" comes to rest on the Anformung 34.
  • An lower solder joint 33 is in the region of the end face facing away from the piston crown.
  • side 20 'of the ring element 3 "formed by the piston bottom side end face 51 of the collar 36 and the shaft-side inner surface 52 of the recess 35.
  • the recesses 47 and 48 are arranged between the lower solder joint 33 and the ring portion 5. .
  • Fig. 5 shows an embodiment of the piston 1 ", in which the solder joint 24 'of the conically tapering down, lower end face 37 of the ring member 3 1 and the conically tapered down surface 38 is formed, wherein the surface 38th the radially outer region of the central part 9 "limited piston bottom side.
  • the piston 1 according to the invention is produced by first forging a blank 39 for the piston main body 2 and a blank 40 for the ring element 3, as shown in FIG. 6, in which the two blanks 39 and 40 are hatched, and in FIG the piston 1 ultimately produced from this is shown in dashed lines within the hatched area.
  • the ring member 3 can also be made by the method of rolling or drawing.
  • the piston bottom side, radially inner edge of the blank 40 with a chamfer 41 and the piston bottom side, radially outer edge of the blank 39 are provided with a chamfer 42, which, as shown in FIG. 6, a wedge-shaped, circumferential recess 43 result, if the two blanks 39 and 40 are composed.
  • a circumferential, in section at least approximately rectangular projection 44 is integrally formed. Both the recess 43 and the projection 44 have in the context of the joining of the two blanks by means of the Lot explained below in more detail purpose.
  • the two blanks 39 and 40 are soldered together.
  • a gap having this width is already achieved in that both the surfaces 8 and 18 and the surface 19 and 20 are brought into contact with each other without positive engagement.
  • the recess 43 and the piston bottom side surface of the projection 44 are then coated with a nickel-based solder paste, after which the two blanks 39, 40 including solder paste to 1150 0 C are heated.
  • the solder paste liquefies here and penetrates due to the capillary effect between the surfaces 8 and 18 and the surfaces 19 and 20, wherein the liquefied solder enforces a gap with the above dimensions between the surfaces 8 and 18 and between the surfaces 19 and 20 due to the capillary action. As a result, the surfaces 8, 18, 19 and 20 are completely wetted.
  • the solder paste solidifies and results in a defect-free solder joint between the two partially processed blanks 39 and 40.
  • the gap between the surfaces 29 and 31 of the upper solder joint 32 of 10 ⁇ m to 200 ⁇ m, which gap is sufficient for an error-free solder joint, is achieved by the surfaces 29 and 31 being produced in the design of the piston body 2 'and the ring element 3 " be processed by means of a fine turning process to the extent that the gap between the two surfaces 29 and 31 has the dimensions given above of 10 .mu.m to 200 .mu.m, after the collar 36 is fixed in the recess 35 with close play.
  • the molding 34 on which the cover area 25 'of the ring element 3 "comes to rest during assembly of the piston 1 1 , ensures that the piston bottom-side end face 51 of the collar 36 and the shaft-side inner surface 52 of the recess 35 after the piston assembly have a distance of 10 .mu.m to 200 .mu.m from each other, so that here too results in a sufficiently wide gap for a defect-free solder joint.
  • a gap with a constant width of 10 ⁇ m to 200 ⁇ m between the surfaces 8 and 18 results for a secure upper solder joint 23 in that after a corresponding fine working the surfaces 8 and 18, the ring member 3 1 via the conically oriented, lower end face 37 is placed on the conically shaped, radially outer, piston bottom end face 38 of the piston body 2 ", wherein the ring member 3 'alone by the taper of the two surfaces 37 and 38 is aligned symmetrically to the piston axis.
  • the effect of the capillary effect is that the liquefied liquefied solder in the Gap between the surfaces 37 and 28 penetrates to securely solder these surfaces together.
  • the application of the soldering method for connecting the two piston parts has the advantage that the soldering temperature of 1150 0 C, to which the piston is heated in this case, equal to the forging temperature, with which the two blanks 39 and 40 are forged so that when cooling targeted can be adjusted for the AFP steel typical material properties.

Landscapes

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

Abstract

The invention relates to a two-piece piston (1) for an internal combustion engine, comprising a piston base body (2) and a ring element (3), which is soldered to the piston base body (2) by an upper solder connection (23) having the length b, which is disposed on the radial inside of a piston crown (4) formed at least partially by the ring element (3), and by a lower solder connection (24) having the length c, which is disposed radially outside on the top of a center part (9). In order to improve the strength of the solder connections (23) and (24) due to pressure and temperature-related deformations of the upper piston part, the ring element (3) has a peripheral, upper, thinner wall region (49) in the region of the piston crown (4) radially outside the upper solder connection (23) and further a peripheral, lower, thinner wall region (50) between the ring section (5) and the lower solder connection (24), wherein the thickness a and b of the thinner wall regions (49) and (50) has a lower value than the length b and c of the solder connections (23) and (24).

Description

Zweiteiliger Kolben für einen Verbrennungsmotor Two-piece piston for an internal combustion engine
Die Erfindung betrifft einen zweiteiligen Kolben für einen Verbrennungsmotor nach dem Oberbegriff des Anspruches 1.The invention relates to a two-part piston for an internal combustion engine according to the preamble of claim 1.
Aus der Offenlegungsschrift DE-OS 24 34 902 ist ein mehrteiliger Kolbe für einen Verbrennungsmotor bekannt, der einen Grundkörper aufweist, an dessen Unterseite zwei Bolzennaben angeformt sind. Auf der Unterseite ist der Grundkörper mit einem Kolbenschaft und auf der Oberseite radial außen mit einem Ringelement verbunden. Bekannt ist aus obigerer DE-OS auch, zum Verbinden des Grundkörpers mit dem Kolbenschaft und mit dem Ringelement ein Lötschweißverfahren, d.h., ein Hartlötverfahren anzuwenden. Hierbei weist das Ringelement eine erste Lötverbindung auf der radialen Innenseite des vom Ringelement gebildeten Teiles des Kolbenbodens auf. Da sowohl der vom Grundkörper als auch der vom Ringelement gebildete Teil des Kolbenbodens sehr dünnwandig sind, ergibt sich der Nachteil, dass auch die Lötverbindung eine sehr geringe axiale Länge und damit eine sehr geringe Festigkeit aufweist.From the published patent application DE-OS 24 34 902 a multi-part piston for an internal combustion engine is known which has a base body, on the underside of two pin bosses are formed. On the underside of the body is connected to a piston skirt and on the top radially outward with a ring member. It is also known from the above DE-OS, for joining the main body to the piston skirt and to the ring element, to use a brazing process, i.e., a brazing process. In this case, the ring element has a first solder joint on the radial inner side of the part of the piston crown formed by the ring element. Since both the part of the piston crown formed by the main body and by the ring element are very thin-walled, there is the disadvantage that the solder joint also has a very small axial length and thus a very low strength.
Auf der dem Kolbenboden abgewandten Seite ist das Ringelement zudem über eine in radialer Richtung gesehen relativ lange, untere Lötverbindung mit dem Grundkörper verbunden. Wenn sich hierbei der Kolbenboden aufgrund einer Druckbelastung wegen der in der Brennraummulde stattfindenden, explosionsartigen Verbrennung des Kraftstoff-Luft-Gemisches und wegen der im Bereich des Kolbenbodens herrschenden, sehr hohen Temperaturen in radialer Richtung teils druck- und teils temperaturbedingt ausdehnt, weitete sich das Ringelement trichterförmig auf, und die untere Lötverbindung wird einer großen Zugbelastung ausgesetzt. Der aus dem vorliegenden Stand der Technik bekannte Kolben hat den Nachteil, dass im Bereich der unteren Lötverbindung keine konstruktiven Maßnahmen vorgesehen sind, um diese Zugbelastung auf die untere Lötverbindung zu verringern. Diese Nachteile des Stand der Technik zu vermeiden, ist Aufgabe der Erfindung. Gelöst wird diese Aufgabe mit den im Kennzeichen des Hauptanspruches stehenden Merkmalen. Zweckmäßige Ausgestaltungen der Erfindung sind Gegenstand der Unteransprüche.On the side facing away from the piston crown, the ring element is also connected to the base body via a relatively long, lower solder joint seen in the radial direction. If in this case the piston crown due to a pressure load due to the taking place in the combustion chamber cavity, explosive combustion of the fuel-air mixture and because of prevailing in the region of the piston crown, very high temperatures in the radial direction partly pressure and partly due to temperature expands, the ring element widened funnel-shaped, and the lower solder joint is subjected to a large tensile load. The known from the prior art piston has the disadvantage that in the area of the lower solder joint no constructive measures are provided to reduce this tensile load on the lower solder joint. To avoid these disadvantages of the prior art is an object of the invention. This problem is solved with the features in the characterizing part of the main claim. Advantageous embodiments of the invention are the subject of the dependent claims.
Hierbei werden bei einer trichterförmigen Aufweitung des Ringelementes nahe den Lötverbindungen angeordnete, verdünnte, umlaufende Wandbereiche scharnierartig verformt, was eine erheblich Verringerung der im Motorbetrieb auf die Lötverbindungen einwirkende Zugspannung mit sich bringt.Here, in a funnel-shaped widening of the ring element near the solder joints arranged, dilute, circumferential wall portions are hingedly deformed, which brings a significant reduction in the force acting on the braze joints in engine operation tension with it.
Einige Ausführungsbeispiele der Erfindung werden im Folgenden anhand derSome embodiments of the invention will be described below with reference to FIG
Zeichnungen beschrieben. Es zeigenDrawings described. Show it
Fig. 1 eine Explosionsdarstellung des Kolbens gemäß der Erfindung, bestehend aus einem Kolbengrundkörper und einem Ringelement,1 is an exploded view of the piston according to the invention, consisting of a piston body and a ring member,
Fig. 2 eine perspektivische Darstellung des erfindungsgemäßen Kolbens nach dessen Montage,2 is a perspective view of the piston according to the invention after its assembly,
Fig. 3 einen Schnitt durch den Kolben entlang der Kolbenachse und der Linie III-III in Fig. 2,3 shows a section through the piston along the piston axis and the line III-III in Fig. 2,
Fig. 4 einen Teilschnitt durch den Kolben im Bereich des Kühlkanals zur Darstellung einer Ausgestaltung der Lötverbindungen,4 shows a partial section through the piston in the region of the cooling channel to illustrate an embodiment of the solder joints,
Fig. 5 einen Teilschnitt durch den Kolben im Bereich des Kühlkanals zur Darstellung einer weiteren Ausgestaltung einer der Lötverbindungen und5 shows a partial section through the piston in the region of the cooling channel to illustrate a further embodiment of the solder joints and
Fig. 6 einen Teilschnitt durch den Kolbenrohling im Bereich des Kühlkanals.6 shows a partial section through the piston blank in the region of the cooling channel.
Fig. 1 zeigt einen Kolben 1 in Explosionsdarstellung, der aus einem Kolbengrund kör- per 2 und einem Ringelement 3 besteht. Der Kolbengrundkörper 2 und das Ringelement 3 sind aus AFP-Stahl gefertigt, d.h., aus einem mikrolegierten, ausscheidungs- härtenden, ferritisch-perlitischen Stahl auf Mangan-Vanadin-Basis nach DIN EN 10267. Der Kolbengrundkörper 2 und das Ringelement 3 werden im Rahmen der Montage des Kolbens 1 miteinander verlötet.FIG. 1 shows an exploded view of a piston 1, which consists of a piston base body 2 and a ring element 3. The piston base body 2 and the ring element 3 are made of AFP steel, ie, of a microalloyed, precipitation-hardening, ferritic-pearlitic manganese-vanadium-based steel according to DIN EN 10267. The piston main body 2 and the ring element 3 are used in the context of Assembly of the piston 1 soldered together.
Das Ringelement 3 bildet den wesentlichen Teil des ringförmig ausgebildeten Kolbenbodens 4 und weist auf seiner radialen Außenseite eine Ringpartie 5 zur Aufnahme in der Figur nicht dargestellter Kolbenringe auf. In das Ringelement 3 ist mittig und rotationssymmetrisch zur Kolbenachse 6 eine rund Öffnung 7 eingebracht, die nahe dem Kolbenboden 4 von einer ersten, zylinderförmigen Fläche 8 begrenzt wird, die bei der Montage des Kolbens 1 als Lötfläche dient.The ring member 3 forms the essential part of the annular piston crown 4 and has on its radial outer side a ring portion 5 to Recording in the figure not shown piston rings. In the ring member 3 is centrally and rotationally symmetrical to the piston axis 6, a round opening 7 is introduced, which is bounded near the piston head 4 by a first, cylindrical surface 8, which serves as a soldering surface during assembly of the piston 1.
Der Kolbengrundkörper 2 besteht aus einem im Wesentlichen plattenförmigen und runden Mittenteil 9, an dessen dem Kolbenboden 4 abgewandte Unterseite zwei einander gegenüberliegende Schaftelemente 10 und zwei einander gegenüberliegende und diese Schaftelemente 10 miteinander verbindende Bolzennaben 11 angeformt sind. Die radial äußeren Stirnseiten 12 der Bolzennaben 11 sind gegenüber der radial äußeren Begrenzung 13 des Mittenteils 9 in Richtung der Kolbenachse 6 zurückgesetzt.The piston main body 2 consists of a substantially plate-shaped and round center part 9, on its underside facing away from the piston bottom 4, two opposing shaft elements 10 and two opposing and this shaft elements 10 interconnecting pin bosses 11 are formed. The radially outer end faces 12 of the pin bosses 11 are set back relative to the radially outer boundary 13 of the middle part 9 in the direction of the piston axis 6.
In die Oberseite des Mittenteils 9 ist radial außen eine umlaufende, kanalförmige Ausnehmung 14 eingeformt, von der eine radial innen liegende und auf der Oberseite des Mittenteils 9 angeordnete, umlaufende Ringrippe 15 umgeben ist, deren Innenraum die Verbrennungsmulde 16 des Kolbens 1 bildet.In the upper side of the middle part 9, a peripheral, channel-shaped recess 14 is formed radially outwardly, surrounded by a circumferential inner annular rib 15 arranged radially on the upper side of the middle part 9, the interior of which forms the combustion recess 16 of the piston 1.
Im vorliegenden Ausführungsbeispiel des Kolbens 1 sind die Ringrippe 15 und die Verbrennungsmulde 16 nicht rotationssymmetrisch zur Kolbenachse 6 ausgebildet, sondern weisen radial außen eine Eindellung 17 auf, deren Zweck darin besteht, die Verbrennung des Kraftstoff-Luft-Gemisches in der Verbrennungsmulde 16 zu verbessern.In the present embodiment of the piston 1, the annular rib 15 and the combustion bowl 16 are not rotationally symmetrical to the piston axis 6, but have radially outward a dent 17 whose purpose is to improve the combustion of the fuel-air mixture in the combustion bowl 16.
Kolbenbodenseitig ist die Begrenzung der Ringrippe 15 kreisförmig ausgebildet, sodass hiervon ein Teil des Kolbenbodens 41 gebildet wird. Hiervon wird zudem eine radial außen liegende, zweite zylinderförmige Fläche 18 gebildet, die als Gegenstück zur ersten Fläche 8 des Ringelementes 3 ebenfalls als Lötfläche dient und mit der Fläche 8 eine obere Lötverbindung (23, siehe Fig. 3) zwischen dem Ringelement 3 und dem Kolbengrundkörper 2 bildet.The piston crown side, the boundary of the annular rib 15 is circular, so that a part of the piston head 4 1 is formed thereof. Of this, a radially outer, second cylindrical surface 18 is also formed, which also serves as a counterpart to the first surface 8 of the ring member 3 as a soldering surface and the surface 8 an upper solder joint (23, see Fig. 3) between the ring member 3 and the Piston body 2 forms.
Radial außen weist das Mittenteil 9 auf seiner Oberseite eine ringförmige, dritte Fläche 19 auf, die als Lötfläche dient und mit einer in Fig. 1 nicht dargestellten, auf - A -Radially outward, the center part 9 on its upper side an annular, third surface 19, which serves as a soldering surface and with a not shown in Fig. 1, on - A -
der unteren Stirnseite des Ringelementes 3 angeordneten, vierten und ebenfalls als Lötfläche dienender Fläche 20 eine untere Lötverbindung zwischen dem Ringelement 3 und dem Kolbengrundkörper 2 bildet. (Siehe auch hierzu Fig. 3.)the lower end face of the ring member 3, fourth and also serving as a soldering surface 20 forms a lower solder joint between the ring member 3 and the piston body 2. (See also Fig. 3.)
Ist das Ringelement 3 auf den Kolbengrundkörper 2 aufgesetzt und damit verlötet, ergibt sich der in Fig. 2 dargestellte Kolben 1 , der den Kolbenboden 4, 4', die Verbrennungsmulde 16, die Ringpartie 5, ein Schaftelement 10 und eine Bolzennabe 11 erkennen lässt.If the ring element 3 is placed on the piston base body 2 and soldered therewith, the piston 1 shown in FIG. 2 results, which reveals the piston crown 4, 4 ', the combustion bowl 16, the ring section 5, a shaft element 10 and a pin boss 11.
Der in Fig. 3 dargestellte Schnitt durch den Kolben entlang der Kolbenachse 6 und der Linie IH-III in Fig. 2 zeigt einen radial außen vom Ringelement 3, radial innen von der Ringrippe 15 und unten von der Ausnehmung 14 des Mittelteils 9 des Kolbengrundkörpers 2 begrenzten, ringförmigen, Kühlkanal 21 , der in der Figur nicht dargestellte und in den Kolbeninnenraum 22 mündende Ölzuführ- und Ölabführkanä- Ie aufweist. Dargestellt sind auch die von der ersten und zweiten Fläche 8 und 18 gebildete, axial ausgerichtete, obere Lötverbindung 23 und die von der dritten und vierten Fläche 19 und 20 gebildete, radial ausgerichtete, untere Lötverbindung 24 zwischen dem Kolbengrundkörper 2 und dem Ringelement 3.The section shown in Fig. 3 by the piston along the piston axis 6 and the line IH-III in Fig. 2 shows a radially outside of the ring member 3, radially inwardly of the annular rib 15 and below of the recess 14 of the central part 9 of the piston main body second limited, annular, cooling channel 21, not shown in the figure and opening into the piston interior 22 Ölzuführ- and Ölabführkanä- Ie. Shown are also formed by the first and second surfaces 8 and 18, axially aligned, upper solder joint 23 and formed by the third and fourth surfaces 19 and 20, radially oriented, lower solder joint 24 between the piston body 2 and the ring member third
Die erste Fläche 8 stellt hierbei die radial innere Begrenzung des den Kolbenboden 4 bildenden Deckbereiches 25 des Ringelementes 3 dar, wobei in die kolbenbodenab- gewandte Seite des Deckbereiches 25 eine nach oben gerichtete, umlaufende Ausnehmung 26 eingeformt ist, die hier einen umlaufenden, oberen, verdünnten Wandbereich 49 bildet. Hierbei liegt das Verhältnis zwischen der Länge b der oberen Lötverbindung 23 und der minimalen Dicke a des oberen, verdünnten Wandbereiches 49 zwischen 1 und 3, d.h., 1<b/a<3.The first surface 8 in this case represents the radially inner boundary of the piston crown 4 forming deck portion 25 of the ring member 3, wherein in the piston bottom side facing away from the deck area 25 an upwardly directed, circumferential recess 26 is formed, here a peripheral, upper, diluted wall portion 49 forms. Here, the ratio between the length b of the upper solder joint 23 and the minimum thickness a of the upper thinned wall portion 49 is between 1 and 3, that is, 1 <b / a <3.
Kolbenbodenseitig schließt sich an die vierte Fläche 20, die die untere Stirnseite des Ringelementes 3 bildet, eine weitere, in die radiale Innenseite des Ringelementes 3 eingeformte und nach radial außen gerichtete, umlaufende Ausnehmung 27 an, die hier einen unteren, umlaufenden, verdünnten Wandbereich 50 bildet, wobei das Verhältnis zwischen der Länge c der unteren Lötverbindung 24 und der minimalen Dicke d des unteren, verdünnten Wandbereiches 50 ebenfalls zwischen 1 und 3 liegt, d.h., 1<c/d<3. Die Ausnehmung 27 ist zwischen der Ringpartie 5 und der unteren Lötverbindung 24 angeordnet.On the piston crown side adjoins the fourth surface 20, which forms the lower end face of the ring element 3, another, formed in the radial inner side of the ring member 3 and directed radially outward, circumferential recess 27, here a lower, circumferential, thinned wall portion 50th wherein the ratio between the length c of the lower solder joint 24 and the minimum thickness d of the lower, thinned wall portion 50 is also between 1 and 3, ie, 1 <c / d <3. The recess 27 is disposed between the ring portion 5 and the lower solder joint 24.
Bei einer Temperatur- und/oder Druckbelastung des Kolbens 1 , 1', 1" ergibt sich, wie es in Fig. 5 zur Verdeutlichung des Sachverhaltes vergrößert dargestellt ist, eine Aufweitung 28 des oberen Teiles des Kolbens 1 , 1', 1". Die hierbei auf die Lötverbindungen 23, 24, 24' einwirkende Zugbelastung wird von den verdünnten und damit elastisch nachgiebigen Bereiche des Ringelementes 3, 3', die von den Ausnehmungen 26 und 27 gebildeten werden, und die sich bei der Aufweitung 28 des Kolbenoberteils scharnierartige verformen, insoweit verringert, dass die Lötverbindungen 23, 24, 24' auch nach längerem Motorbetrieb halten.At a temperature and / or pressure load of the piston 1, 1 ', 1 "results, as shown in Fig. 5 is enlarged to illustrate the facts, a widening 28 of the upper part of the piston 1, 1', 1". The tensile load acting on the solder joints 23, 24, 24 'in this case is deformed by the thinned and thus elastically yielding regions of the ring element 3, 3', which are formed by the recesses 26 and 27, and which hinge at the widening 28 of the upper piston part in that reduced, that the solder joints 23, 24, 24 'hold even after prolonged engine operation.
In Fig. 4 ist eine Ausgestaltung des Kolbens V im Bereich des Kühlkanals 21' dargestellt, bei der der obere Deckbereich 25' des Ringelementes 3" im Bereich des oberen, verdünnten Wandbereiches 49 radial innen nur bis zu dem Bereich der geringsten Wandstärke a reicht und hier eine radial innen liegende, zylinderförmige Fläche 31 bildet, die mit einer radial außen liegenden, zylinderförmigen Fläche 29 eines kolbenbodenseitig an die Ringrippe 15 angeformten, umlaufenden und nach radial außen gerichteten Kragens 30 eine obere Lötverbindung 32 bildet.4, an embodiment of the piston V in the region of the cooling channel 21 'is shown, in which the upper deck area 25' of the ring element 3 "in the region of the upper, thinned wall portion 49 extends radially inwards only up to the area of the smallest wall thickness a and Here, a radially inner, cylindrical surface 31 forms, which forms an upper solder joint 32 with a radially outer, cylindrical surface 29 of a piston crown side integrally formed on the annular rib 15, circumferential and radially outwardly directed collar 30.
Auf der kolbenbodenabgewandten Seite wird die Fläche 29 von einer stufenförmigen, umlaufenden Anformung 34 begrenzt, auf der das radial innere Ende des Deckbereiches 25' aufliegt.On the side facing away from the piston crown, the surface 29 is delimited by a step-shaped circumferential molding 34 on which the radially inner end of the cover region 25 'rests.
Die kolbenbodenabgewandte Stirnseite 20' des Ringelementes 3" weist im Ausführungsbeispiel gemäß Fig. 4 radial innen eine umlaufende, stufenförmige Ausnehmung 35 auf, die so dimensioniert ist, dass sie auf einen kolbenbodenseitig auf der radial äußeren Begrenzung 13' des Mittenteils 9' angeformten, umlaufenden Kragen 36 passt, sodass beim Zusammenbau des Kolbens 1' das Ringelement 3" auf den Kragen 36 geschoben wird, bis der Kragen 36 in der Ausnehmung 35 sitzt, und der Deckbereich 25' des Ringelementes 3" auf der Anformung 34 zur Anlage gelangt. Eine untere Lötverbindung 33 wird im Bereich der kolbenbodenabgewandten Stirn- seite 20' des Ringelementes 3" von der kolbenbodenseitigen Stirnfläche 51 des Kragens 36 und von der schaftseitigen Innenfläche 52 der Ausnehmung 35 gebildet.The piston bottom facing away from end face 20 'of the ring member 3 "has in the embodiment of FIG. 4 radially inside a circumferential, stepped recess 35 which is dimensioned so that they on a piston bottom side on the radially outer boundary 13' of the central part 9 'integrally formed, circumferential Collar 36 fits, so that upon assembly of the piston 1 ', the ring member 3 "is pushed onto the collar 36 until the collar 36 is seated in the recess 35, and the cover portion 25' of the ring member 3" comes to rest on the Anformung 34. An lower solder joint 33 is in the region of the end face facing away from the piston crown. side 20 'of the ring element 3 "formed by the piston bottom side end face 51 of the collar 36 and the shaft-side inner surface 52 of the recess 35.
Hierdurch wird erreicht, dass das Ringelement 3" beim Aufschieben auf den Kolbengrundkörper 2' nicht nur über die Flächen 29 und 31 der oberen Lötverbindung 32 geführt und zentriert wird, sondern dass bei der Montage des Kolbens 1' eine zusätzliche Führung und Zentrierung des Ringelementes 3" auch über die Ausnehmung 35 und den Kragen 36 der unteren Lötverbindung 33 erreicht wird.This ensures that the ring member 3 "when sliding on the piston body 2 'is not only guided and centered over the surfaces 29 and 31 of the upper solder joint 32, but that in the assembly of the piston 1' an additional guide and centering of the ring element. 3 is achieved via the recess 35 and the collar 36 of the lower solder joint 33.
Anstelle einer einzige, radial innen angeordneten Ausnehmung 27 gemäß dem in den Fig. 3 und 5 dargestellten Ausführungsbeispiel des Kolbens 1 , 1" weist das Ausführungsbeispiel des Kolbens 11 gemäß Fig. 4 oberhalb der unteren Lötverbindung 33 sowohl auf der Innenseite als auch auf der Außenseite des Ringelementes 3" je eine umlaufende Ausnehmung 47 und 48 auf, die hier einen unteren, verdünnten Wandbereich 50' mit der Dicke d schaffen, der sich bei einer Aufweitung 28 des Kolbenoberteils (gemäß Fig. 5) scharnierartige verformt und damit die sich hierbei ergebende Zugbelastung auf die untere Lötverbindung 33 verringert. Die Ausnehmungen 47 und 48 sind zwischen der unteren Lötverbindung 33 und der Ringpartie 5 angeordnet. ,Instead of a single, radially inwardly disposed recess 27 according to the embodiment shown in FIGS. 3 and 5 of the piston 1, 1 ", the embodiment of the piston 1 1 shown in FIG. 4 above the lower solder joint 33 on both the inside and on the Outside of the ring member 3 "per a circumferential recess 47 and 48, which here create a lower, thinned wall portion 50 'with the thickness d, which deforms at a widening 28 of the piston upper part (as shown in FIG. 5) hinge-like and thus hereby resulting tensile load on the lower solder joint 33 is reduced. The recesses 47 and 48 are arranged between the lower solder joint 33 and the ring portion 5. .
Fig. 5 zeigt eine Ausgestaltung des Kolbens 1", bei dem die Lötverbindung 24' von der konisch sich nach unten verjüngenden, unteren Stirnseite 37 des Ringelementes 31 und von der ebenfalls konisch sich nach unten verjüngenden Fläche 38 gebildet wird, wobei die Fläche 38 den radial äußeren Bereich des Mittenteils 9" kolbenbo- denseitig begrenzt. Hierdurch wird eine Vergrößerung der Flächen 37 und 38 und damit eine Vergrößerung der unteren, konisch sich nach unten verjüngenden Lötverbindung 24' mit der Länge c erreicht, was zu einer weiteren Verbesserung der Festigkeit der unteren Lötverbindung 24' führt.Fig. 5 shows an embodiment of the piston 1 ", in which the solder joint 24 'of the conically tapering down, lower end face 37 of the ring member 3 1 and the conically tapered down surface 38 is formed, wherein the surface 38th the radially outer region of the central part 9 "limited piston bottom side. As a result, an enlargement of the surfaces 37 and 38 and thus an enlargement of the lower, tapered downwardly tapered solder joint 24 'is achieved with the length c, which leads to a further improvement in the strength of the lower solder joint 24'.
Hergestellt wird der erfindungsgemäße Kolben 1 , indem zunächst ein Rohling 39 für den Kolbengrundkörper 2 und ein Rohling 40 für das Ringelement 3 geschmiedet werden, wie sie in Fig. 6 dargestellt sind, in der die beiden Rohlinge 39 und 40 schraffiert gezeichnet sind, und in der der letztlich hieraus hergestellte Kolben 1 innerhalb der schraffierten Fläche gestrichelt eingezeichnet ist. Das Ringelement 3 kann auch durch das Verfahren des Walzens oder des Ziehens hergestellt werden. Hierbei werden die kolbenbodenseitige, radial innere Kante des Rohlings 40 mit einer Fase 41 und die kolbenbodenseitige, radial äußere Kante des Rohlings 39 mit einer Fase 42 versehen, die, wie Fig. 6 zeigt, eine im Schnitt keilförmige, umlaufende Ausnehmung 43 ergeben, wenn die beiden Rohlinge 39 und 40 zusammengesetzt sind.The piston 1 according to the invention is produced by first forging a blank 39 for the piston main body 2 and a blank 40 for the ring element 3, as shown in FIG. 6, in which the two blanks 39 and 40 are hatched, and in FIG the piston 1 ultimately produced from this is shown in dashed lines within the hatched area. The ring member 3 can also be made by the method of rolling or drawing. Here, the piston bottom side, radially inner edge of the blank 40 with a chamfer 41 and the piston bottom side, radially outer edge of the blank 39 are provided with a chamfer 42, which, as shown in FIG. 6, a wedge-shaped, circumferential recess 43 result, if the two blanks 39 and 40 are composed.
Weiterhin wird im Rahmen des Schmiedens des Rohlings 39 an die radial äußere, kolbenbodenseitige Kante der dritten Fläche 19 ein umlaufender, im Schnitt zumindest näherungsweise rechteckiger Vorsprung 44 angeformt. Sowohl die Ausnehmung 43 als auch der Vorsprung 44 haben im Rahmen des Verbindens der beiden Rohlinge mittels Lot den weiter unten näher erläuterten Zweck.Furthermore, as part of the forging of the blank 39 to the radially outer, piston bottom side edge of the third surface 19, a circumferential, in section at least approximately rectangular projection 44 is integrally formed. Both the recess 43 and the projection 44 have in the context of the joining of the two blanks by means of the Lot explained below in more detail purpose.
Im Anschluss daran werden in die radial äußere Fläche der Ringrippe 15 des Rohlings 39 und in die Oberfläche des Mittenteils 9 die insbesondere in Fig. 1 dargestellten rotationssymmetrischen Konturen eingedreht, wobei auch die Ausnehmung 14 hergestellt wird. Die in Fig. 1 dargestellte Eindellung 17 wird in die radiale Außenseite der Ringrippe 15 eingefräst. Durch Drehen werden dann auch die rotationssymmetrischen Konturen der radialen Innenfläche 45 des Ringelementes 3 und insbesondere die Ausnehmungen 26, 27, 47, 48 hergestellt.Subsequently, in the radially outer surface of the annular rib 15 of the blank 39 and in the surface of the central part 9, the rotationally symmetrical contours shown in particular in Fig. 1 are screwed, wherein the recess 14 is made. The indentation 17 shown in FIG. 1 is milled into the radial outer side of the annular rib 15. By turning then the rotationally symmetrical contours of the radial inner surface 45 of the ring member 3 and in particular the recesses 26, 27, 47, 48 are made.
Im Anschluss daran werden die beiden Rohlinge 39 und 40 miteinander verlötet. Hierbei ist es zunächst erforderlich, die Rohlinge 39 und 40 so zusammenzusetzen, dass sich zwischen den Flächen 8 und 18 und zwischen den Fläche 19 und 20, jeweils ein Spalt ergibt, der zwischen 10 μm und 200 μm breit ist. Beim Zusammensetzen der Rohlinge 39 und 40 wird ein Spalt mit dieser Breite bereits dadurch erreicht, dass sowohl die Flächen 8 und 18 und die Fläche 19 und 20 ohne Form- schluss miteinander in Kontakt gebracht werden.Following this, the two blanks 39 and 40 are soldered together. In this case, it is first necessary to assemble the blanks 39 and 40 in such a way that, between the surfaces 8 and 18 and between the surfaces 19 and 20, a gap results which is between 10 μm and 200 μm wide. When assembling the blanks 39 and 40, a gap having this width is already achieved in that both the surfaces 8 and 18 and the surface 19 and 20 are brought into contact with each other without positive engagement.
Die Ausnehmung 43 und die kolbenbodenseitige Fläche des Vorsprungs 44 werden dann mit einer Lotpaste auf Nickelbasis bestrichen, wonach die beiden Rohlinge 39, 40 inklusive Lotpaste auf 1150 0C erhitzt werden. Die Lotpaste verflüssigt sich hierbei und dringt aufgrund des Kapillareffektes zwischen den Flächen 8 und 18 und den Flächen 19 und 20 ein, wobei sich das verflüssigte Lot einen Spalt mit den oben angegebenen Maßen zwischen den Flächen 8 und 18 und zwischen den Flächen 19 und 20 aufgrund der Kapillarwirkung erzwingt. Hierdurch werden die Flächen 8, 18, 19 und 20 komplett benetzt. Im Rahmen der daran erfolgenden, gezielten Abkühlung des Kolbens 1 verfestigt sich die Lotpaste und ergibt eine fehlerfreie Lötverbindung zwischen den beiden teilbearbeiteten Rohlingen 39 und 40.The recess 43 and the piston bottom side surface of the projection 44 are then coated with a nickel-based solder paste, after which the two blanks 39, 40 including solder paste to 1150 0 C are heated. The solder paste liquefies here and penetrates due to the capillary effect between the surfaces 8 and 18 and the surfaces 19 and 20, wherein the liquefied solder enforces a gap with the above dimensions between the surfaces 8 and 18 and between the surfaces 19 and 20 due to the capillary action. As a result, the surfaces 8, 18, 19 and 20 are completely wetted. As part of the targeted cooling of the piston 1, the solder paste solidifies and results in a defect-free solder joint between the two partially processed blanks 39 and 40.
Bei der Ausgestaltung des Kolbengrund körpers 2' und des Ringelementes 3" gemäß Fig. 4 wird der für eine fehlerfreie Lötverbindung ausreichende Spalt zwischen den Flächen 29 und 31 der oberen Lötverbindung 32 von 10 μm bis 200 μm dadurch erreicht, dass die Flächen 29 und 31 mittels eines Feindrehverfahrens insoweit bearbeitet werden, dass der Spalt zwischen den beiden Flächen 29 und 31 die oben angegebenen Maße von 10 μm bis 200 μm aufweist, nachdem der Kragen 36 mit engem Spiel in der Ausnehmung 35 fixiert ist.4, the gap between the surfaces 29 and 31 of the upper solder joint 32 of 10 μm to 200 μm, which gap is sufficient for an error-free solder joint, is achieved by the surfaces 29 and 31 being produced in the design of the piston body 2 'and the ring element 3 " be processed by means of a fine turning process to the extent that the gap between the two surfaces 29 and 31 has the dimensions given above of 10 .mu.m to 200 .mu.m, after the collar 36 is fixed in the recess 35 with close play.
Die Anformung 34, auf der bei der Montage des Kolbens 11 der Deckbereich 25' des Ringelementes 3" zur Anlage gelangt, sorgt hierbei dafür, dass die kolbenbodenseiti- ge Stirnfläche 51 des Kragens 36 und die schaftseitige Innenfläche 52 der Ausnehmung 35 nach der Kolbenmontage einen Abstand von 10 μm bis 200 μm voneinander aufweisen, sodass auch hier ein für eine fehlerfreie Lötverbindung ausreichend breiter Spalt ergibt.The molding 34, on which the cover area 25 'of the ring element 3 "comes to rest during assembly of the piston 1 1 , ensures that the piston bottom-side end face 51 of the collar 36 and the shaft-side inner surface 52 of the recess 35 after the piston assembly have a distance of 10 .mu.m to 200 .mu.m from each other, so that here too results in a sufficiently wide gap for a defect-free solder joint.
Bei der Ausgestaltung des Kolbengrundkörpers 2" und des Ringelementes 3' gemäß Fig. 5 ergibt sich für eine sichere, oberen Lötverbindung 23 ein Spalt mit der konstanten Breite von 10 μm bis 200 μm zwischen den Flächen 8 und 18 dadurch, dass nach einer entsprechenden Feinbebarbeitung der Flächen 8 und 18 das Ringelement 31 über dessen konisch ausgerichtete, untere Stirnseite 37 auf die gleichermaßen konisch geformte, radial äußere, kolbenbodenseitige Stirnfläche 38 des Kolbengrundkörpers 2" aufgesetzt wird, wobei das Ringelement 3' alleine durch die Konizität der beiden Flächen 37 und 38 symmetrisch zur Kolbenachse ausgerichtet wird. Hierbei bewirkt der Kapillareffekt, dass das nach Erhitzen verflüssigte Lot in den Spalt zwischen den Flächen 37 und 28 eindringt, um auch diese Flächen sicher miteinander zu verlöten.In the embodiment of the piston base body 2 "and of the ring element 3 'according to FIG. 5, a gap with a constant width of 10 μm to 200 μm between the surfaces 8 and 18 results for a secure upper solder joint 23 in that after a corresponding fine working the surfaces 8 and 18, the ring member 3 1 via the conically oriented, lower end face 37 is placed on the conically shaped, radially outer, piston bottom end face 38 of the piston body 2 ", wherein the ring member 3 'alone by the taper of the two surfaces 37 and 38 is aligned symmetrically to the piston axis. The effect of the capillary effect is that the liquefied liquefied solder in the Gap between the surfaces 37 and 28 penetrates to securely solder these surfaces together.
Die Anwendung des Lötverfahrens zum Verbinden der beiden Kolbenteile hat den Vorteil, dass die Löttemperatur von 1150 0C, auf die der Kolben hierbei erhitzt wird, gleich der Schmiedetemperatur ist, mit der die beiden Rohlinge 39 und 40 geschmiedet werden, sodass beim Abkühlen gezielt die für den AFP-Stahl typischen Werkstoffeigenschaften eingestellt werden können.The application of the soldering method for connecting the two piston parts has the advantage that the soldering temperature of 1150 0 C, to which the piston is heated in this case, equal to the forging temperature, with which the two blanks 39 and 40 are forged so that when cooling targeted can be adjusted for the AFP steel typical material properties.
Im Anschluss daran wird der Kolben 1 fertiggestellt, indem die in Fig. 6 gestrichelt eingezeichneten, rotationssymmetrischen Außenkonturen des Kolbens 1 durch Drehen und die ebenfalls gestrichelt eingezeichneten, nicht-rotationssymmetrischen Begrenzungsflächen 46 der Verbrennungsmulde 16 durch Fräsen hergestellt werden. Hierbei ist es auch möglich, den Kolbengrundkörper 2, 2', 2" und das Ringelement 3, 3', 3" miteinander zu verschweißen. Thereafter, the piston 1 is completed by the dashed lines in Fig. 6, rotationally symmetrical outer contours of the piston 1 by turning and also drawn dashed, non-rotationally symmetric boundary surfaces 46 of the combustion bowl 16 are made by milling. In this case it is also possible to weld the piston base body 2, 2 ', 2 "and the ring element 3, 3', 3" together.
BezugszeichenlisteLIST OF REFERENCE NUMBERS
a Dicke des oberen, verdünnten Wandbereiches 49 b Länge der oberen Lötverbindunga thickness of the upper, thinned wall portion 49 b length of the upper solder joint
C Länge der unteren Lötverbindung d Dicke des unteren, verdünnten Wandbereiches 50, 50C length of the lower solder joint d thickness of the lower, thinned wall portion 50, 50
1 , 1", 1" Kolben1, 1 ", 1" piston
2, 2\ 2" Kolbengrundkörper2, 2 \ 2 "piston body
3, 3\ 3" Ringelement3, 3 \ 3 "ring element
4, 4' Kolbenboden4, 4 'piston crown
5 Ringpartie5 ring game
6 Kolbenachse6 piston axis
7 Öffnung7 opening
8 erste Fläche8 first area
9, 9\ 9" Mittelteil9, 9 \ 9 "midsection
10 Schaftelement10 shaft element
11 Bolzennabe11 pin hub
12 Stirnseite der Bolzennabe 1112 end face of the pin boss 11
13, 131 Begrenzung des Mittenteils 913, 13 1 Limitation of the middle part 9
14 Ausnehmung14 recess
15 Ringrippe15 ring rib
16 Verbrennungsmulde16 combustion bowl
17 Eindellung17 Dentation
18 zweite Fläche18 second area
19 dritte Fläche19 third area
20, 20' vierte Fläche20, 20 'fourth surface
21 , 21' Kühlkanal21, 21 'cooling channel
22 Kolbeninnenraum22 piston interior
23 obere Lötverbindung23 upper solder joint
24, 24' untere Lötverbindung24, 24 'lower solder joint
25, 25" Deckbereich25, 25 "deck area
26, 27 Ausnehmung26, 27 recess
28 Aufweitung Fläche Kragen Fläche obere Lötverbindung untere Lötverbindung Anformung Ausnehmung Kragen Fläche, untere Stirnseite des Ringelementes 3' Fläche, Stirnfläche Rohling für den Kolbengrundkörper 2 Rohling für das Ringelement 3 , 42 Fase Ausnehmung Vorsprung Innenfläche des Ringelementes 3 Begrenzungsfläche der Verbrennungsmulde 16, 48 Ausnehmung oberer, verdünnter Wandbereich , 50' unterer, verdünnter Wandbereich kolbenbodenseitige Stirnfläche des Kragens 36 schaftseitige Innenfläche der Ausnehmung 35 28 expansion Surface collar surface upper solder joint lower solder joint Anformung recess collar surface, lower end face of the ring element 3 'surface, face blank for the piston body 2 blank for the ring member 3, 42 chamfer recess projection inner surface of the ring member 3 boundary surface of the combustion recess 16, 48 recess upper, thinner Wall area, 50 'lower, thinned wall area piston-bottom-side end face of the collar 36 shank-side inner surface of the recess 35th

Claims

Patentansprüche claims
1. Zweiteiliger Kolben (1 , 1 ', 1 ") für einen Verbrennungsmotor,1. Two-piece piston (1, 1 ', 1 ") for an internal combustion engine,
- bestehend aus einem Kolbengrundkörper (2, 2', 2") und einem Ringelement (3, 3\ 3"),consisting of a piston main body (2, 2 ', 2 ") and a ring element (3, 3 \ 3"),
- wobei der Kolbengrund körper (2, 2\ 2") ein rundes im Wesentlichen platten- förmiges Mittenteil (9, 9\ 9") aufweist, dessen radialer Durchmesser zumindest näherungsweise identisch ist mit dem radialen Durchmesser des Kolbens (1 , V, 1"),- wherein the piston base body (2, 2 \ 2 ") has a round substantially plate-shaped center part (9, 9 \ 9") whose radial diameter is at least approximately identical to the radial diameter of the piston (1, V, 1 ")
- wobei an der Unterseite des Mittelteils (9, 9', 9") zwei einander gegenüberliegende Schaftelemente (10) und zwei einander gegenüberliegende und die Schaftelemente (10) miteinander verbindende Bolzennaben (11) angeformt sind, und- Wherein on the underside of the central part (9, 9 ', 9 ") are formed two opposing shaft elements (10) and two opposing and the shaft elements (10) interconnecting pin bosses (11), and
- wobei an der Oberseite des Mittelteils (9, 9\ 9") eine umlaufende, gegenüber dem radial äußeren Rand des Mittenteils (9, 9\ 9") in Richtung Kolbenachse (6) zurückgesetzte Ringrippe (15) angeformt ist, die die radial äußere Begrenzung einer Verbrennungsmulde (16) bildet,- Wherein on the upper side of the central part (9, 9 \ 9 ") a circumferential, with respect to the radially outer edge of the central part (9, 9 \ 9") in the direction of the piston axis (6) recessed annular rib (15) is formed, which is the radial outer boundary of a combustion bowl (16) forms,
- wobei das Ringelement (3, 3\ 3") auf seiner radialen Außenfläche eine Ringpartie (5) aufweist, und- Wherein the ring element (3, 3 \ 3 ") on its radial outer surface has a ring portion (5), and
- wobei das Ringelement (3, 3', 3") über eine obere Lötverbindung (23, 32) mit der Länge b, die auf der radialen Innenseite eines vom Ringelement (3, 3', 3") zumindest teilweise gebildeten Kolbenbodens (4) angeordnete ist, und über eine untere Lötverbindung (24, 24', 33) mit der Länge c, die radial außen auf der Oberseite des Mittenteils (9, 9', 9") angeordnet ist, mit dem Kolbengrundkörper (2, 21, 2") verlötet ist, dadurch gekennzeichnet, dass das Ringelement (3, 3', 3") zum einen im Bereich des Kolbenbodens (4) radial außerhalb der oberen Lötverbindung (23, 32) einen umlaufenden, oberen, verdünnten Wandbereich (49) und zum anderen zwischen der Ringpartie (5) und der unteren Lötverbindung (24, 24', 33) einen umlaufenden, unteren, verdünnten Wandbereich (50, 50') aufweist, wobei die Dicke (a, d) der verdünnten Wandbereiche (49, 50, 50') einen geringeren Wert hat als die Länge (b, c) der Lötverbindungen (23, 24, 24", 32, 33). - wherein the ring element (3, 3 ', 3 ") via an upper solder joint (23, 32) with the length b, on the radially inner side of a ring element (3, 3', 3") at least partially formed piston crown (4th ) is arranged, and via a lower solder joint (24, 24 ', 33) with the length c, which is arranged radially outwardly on the upper side of the central part (9, 9', 9 "), with the piston main body (2, 2 1 , 2 ") is soldered, characterized in that the ring element (3, 3 ', 3") on the one hand in the region of the piston head (4) radially outside the upper solder joint (23, 32) has a circumferential, upper, thinned wall portion (49 ) and on the other between the ring portion (5) and the lower solder joint (24, 24 ', 33) has a circumferential, lower, thinned wall portion (50, 50'), wherein the thickness (a, d) of the thinned wall portions (49 , 50, 50 ') has a lower value than the length (b, c) of the solder joints (23, 24, 24 ", 32, 33).
2. Kolben (1 , 11, 1") nach Anspruch 1 , dadurch gekennzeichnet, dass das Verhältnis zwischen der Länge b der oberen Lötverbindung (23, 32) und der Dicke a des oberen, verdünnten Wandbereiches (49) größer 1 und kleiner 3 ist, sodass gilt, 1 < b/a < 3.Second piston (1, 1 1 , 1 ") according to claim 1, characterized in that the ratio between the length b of the upper solder joint (23, 32) and the thickness a of the upper, thinned wall portion (49) is greater than 1 and smaller 3, so that 1 <b / a <3.
3. Kolben (1 , 1', 1") nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass das Verhältnis zwischen der Länge c der unteren Lötverbindung (24, 24', 33) und der Dicke d des unteren, verdünnten Wandbereiches (50, 50') größer 1 und kleines 3 ist, sodass gilt 1 < c/d < 3.3. piston (1, 1 ', 1 ") according to claim 1 or 2, characterized in that the ratio between the length c of the lower solder joint (24, 24', 33) and the thickness d of the lower, thinned wall portion (50 , 50 ') is greater than 1 and small is 3, so that 1 <c / d <3.
4. Kolben (1 , 1") nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das Ringelement (3, 31) einen den Kolbenboden (4) teilweise bildenden Deckenbereich (25) aufweist, wobei in die kolbenbodenabgewandte Seite des Deckenbereiches (25) eine nach oben gerichtete, umlaufende Ausnehmung (26) eingeformt ist, die den oberen, verdünnten Wandbereich (49) bildet.4. Piston (1, 1 ') according to one of the preceding claims, characterized in that the ring element (3, 3 1 ) has a piston bottom (4) partially forming ceiling region (25), wherein in the piston bottom side facing away from the ceiling region (25 ) is formed an upwardly directed, circumferential recess (26) which forms the upper, thinned wall portion (49).
5. Kolben (1 , 1") nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass zwischen der unteren Lötverbindung (24, 24') und der Ringpartie (5) in die radiale Innenseite des Ringelementes (3, 3') eine nach radial außen gerichtete, umlaufende Ausnehmung (27) eingeformt ist, die den unteren verdünnten Wandbereich (50) bildet.5. Piston (1, 1 ') according to any one of the preceding claims, characterized in that between the lower solder joint (24, 24') and the ring portion (5) in the radial inner side of the ring element (3, 3 ') a radially outwardly directed, circumferential recess (27) is formed, which forms the lower thinned wall portion (50).
6. Kolben (1') nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass zwischen der unteren Lötverbindung (33) und der Ringpartie (5) in die radiale Innenseite des Ringelementes (3") eine umlaufende, nach radial außen gerichtete Ausnehmung (47) und in die radiale Außenseite des Ringelementes (3") eine umlaufende, nach radial innen gerichtete Ausnehmung (48) eingeformt sind, und dass die beiden Ausnehmungen (47, 48) einander gegenüberliegen und den unteren verdünnten Wandbereich (50') bilden.6. piston (1 ') according to one of claims 1 to 4, characterized in that between the lower solder joint (33) and the ring portion (5) in the radial inner side of the ring element (3 ") a circumferential, radially outwardly directed recess (47) and in the radial outer side of the ring element (3 ") a circumferential, radially inwardly directed recess (48) are formed, and that the two recesses (47, 48) face each other and the lower thinned wall portion (50 ') form ,
7. Kolben (1") nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die untere Lötverbindung (241) von einer konisch sich nach un- ten verjüngenden, unteren Stirnseite (37) des Ringelementes (3') und von einer ebenfalls konisch sich nach unten verjüngenden und den radial äußeren Bereich des Mittenteils (9") kolbenbodenseitig begrenzenden Fläche (38) gebildet wird. 7. piston (1 '') according to any one of the preceding claims, characterized in that the lower solder joint (24 1 ) of a conically Tapered, lower end face (37) of the ring element (3 ') and of a conically also downwardly tapering and the radially outer region of the central part (9 ") piston bottom side defining surface (38) is formed.
EP08801217.4A 2007-09-15 2008-08-23 Two-piece piston for an internal combustion engine Active EP2188513B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007044106A DE102007044106A1 (en) 2007-09-15 2007-09-15 Two-piece piston for an internal combustion engine
PCT/DE2008/001394 WO2009033446A1 (en) 2007-09-15 2008-08-23 Two-piece piston for an internal combustion engine

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EP2188513A1 true EP2188513A1 (en) 2010-05-26
EP2188513B1 EP2188513B1 (en) 2017-03-01

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US (1) US8225765B2 (en)
EP (1) EP2188513B1 (en)
JP (1) JP5295245B2 (en)
KR (1) KR101484352B1 (en)
CN (1) CN101802381B (en)
DE (1) DE102007044106A1 (en)
WO (1) WO2009033446A1 (en)

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Also Published As

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JP5295245B2 (en) 2013-09-18
CN101802381B (en) 2015-11-25
KR101484352B1 (en) 2015-01-19
US8225765B2 (en) 2012-07-24
WO2009033446A1 (en) 2009-03-19
KR20100069646A (en) 2010-06-24
EP2188513B1 (en) 2017-03-01
JP2010539369A (en) 2010-12-16
CN101802381A (en) 2010-08-11
DE102007044106A1 (en) 2009-03-19
US20100307445A1 (en) 2010-12-09

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