This application is the National Stage of PCT/DE2008/001394 filed on Aug. 23, 2008, which claims priority under 35 U.S.C. §119 of German Application No. 10 2007 044 106.3 filed on Sep. 15, 2007. The international application under PCT article 21(2) was not published in English.
The invention relates to a two-part piston for an internal combustion engine, in accordance with the preamble of claim 1.
A multi-part piston for an internal combustion engine is known from the Offenlegungsschrift [German unexamined patent application published for public scrutiny] DE-OS 24 34 902, which has a base body on the underside of which two pin bosses are formed. On the underside, the base body is connected with a piston skirt, and on the top, radially on the outside, it is connected with a ring element. It is also known from the above DE-OS to use a soldering/welding method, i.e. a hard-soldering method, to connect the base body with the piston skirt and with the ring element. In this connection, the ring element has a first solder connection on the radial inside of the part of the piston crown formed by the ring element. Since both the part of the piston crown formed by the base body and the part formed by the ring element have very thin walls, the disadvantage results that the solder connection also has a very short axial length and thus a very low strength.
On the side facing away from the piston crown, the ring element is furthermore connected with the base body by way of a relatively long, lower solder connection, seen in the radial direction. If, in this connection, the piston crown expands in the radial direction, partly due to pressure and partly due to temperature, due to a pressure stress caused by the explosion-like combustion of the fuel/air mixture that takes place in the combustion chamber bowl, and due to the very high temperatures that prevail in the region of the piston crown, the ring element widens in funnel shape, and the lower solder connection is exposed to great tensile stress. The piston known from the present state of the art has the disadvantage that in the region of the lower solder connection, no design measures are provided to reduce this tensile stress on the lower solder connection.
It is the task of the invention to avoid these disadvantages of the state of the art. This task is accomplished with the characteristics that stand in the characterizing part of the main claim. Practical embodiments of the invention are the object of the dependent claims.
In this connection, in the case of a funnel-shaped widening of the ring element, thinned, circumferential wall regions that lie close to the solder connections are deformed in hinge-like manner, and this brings with it a significant reduction in the tensile stress that acts on the solder connections during engine operation.
Some exemplary embodiments of the invention will be described in the following, using the drawings. These show:
The ring element 3 forms the essential part of the piston crown 4 that is configured in ring shape, and has a ring belt 5 on its radial outside, for accommodation of piston rings, not shown in the figure. A round opening 7 is made in the ring element 3, centered and with rotation symmetry relative to the piston axis 6, which opening is delimited, close to the piston crown 4, by a first, cylindrical surface 8 that serves as a solder surface during assembly of the piston 1.
The piston base body 2 consists of an essentially plate-shaped and round center part 9, on the underside of which, facing away from the piston crown 4, two skirt elements 10 that lie opposite one another and two pin bosses 11 that lie opposite one another and connect these skirt elements 10 with one another are formed on. The radially outer face sides 12 of the pin bosses 11 are set back in the direction of the piston axis 6, relative to the radially outer delimitation 13 of the center part 9.
A circumferential, channel-shaped recess 14 is formed into the top of the center part 9, surrounding a circumferential ring rib 15 disposed on the top of the center part 9, the interior of which rib forms the combustion bowl 16 of the piston 1.
In the present exemplary embodiment of the piston 1, the ring rib 15 and the combustion bowl 16 are not configured with rotation symmetry relative to the piston axis 6, but rather have an indentation 17 radially on the outside, the purpose of which consists in improving the combustion of the fuel/air mixture in the combustion bowl 16.
On the piston crown side, the delimitation of the ring rib 15 is configured to be circular, so that a part of the piston crown 4′is formed by it. Furthermore, a second cylindrical surface 18 that lies radially on the outside is formed by it, which also serves, as a counterpart to the first surface 8 of the ring element 3, as a solder surface, and forms an upper solder connection (23, see
Radially on the outside, the center part 9 has a ring-shaped, third surface 19 on its top, which serves as a solder surface and forms a lower solder connection between the ring element 3 and the piston base body 2, together with a fourth surface 20, not shown in
Once the ring element 3 has been set onto the piston base body 2 and soldered to it, the piston 1 shown in
The section through the piston along the piston axis 6 and the line III-III in
In this connection, the first surface 8 represents the radially inner delimitation of the cover region 25 of the ring element 3 that forms the piston crown 4, whereby a circumferential recess 26, directed upward, is formed into the side of the cover region 25 that faces away from the piston crown, which recess forms a circumferential, upper, thinned wall region 49 here. In this connection, the ratio between the length b of the upper solder connection 23 and the minimal thickness a of the upper, thinned wall region 49 lies between 1 and 3, i.e. 1<b/a<3.
On the piston crown side, the fourth surface 20, which forms the lower face side of the ring element 3, is followed by another circumferential recess 27, directed radially outward, which is formed into the radial inside of the ring element 3, and forms a lower, circumferential, thinned wall region 50 here, whereby the ratio between the length c of the lower solder connection 24 and the minimal thickness d of the lower, thinned wall region 50 also lies between 1 and 3, i.e. 1<c/d<3. The recess 27 is disposed between the ring belt 5 and the lower solder connection 24.
In the event of a temperature stress and/or pressure stress on the piston 1, 1′, 1″, widening 28 of the upper part of the piston 1, 1′, 1″ occurs, as shown enlarged in
In
On the side facing away from the piston crown, the surface 29 is delimited by a step-shaped, circumferential formed-on part 34 on which the radially inner end of the cover region 25′ rests.
The face side 20′ of the ring element 3′″, which faces away from the piston crown, has a circumferential, step-shaped recess 35 radially on the inside, in the exemplary embodiment according to
In this way, the result is achieved that the ring element 3″ is not only guided and centered over the surfaces 29 and 31 of the upper solder connection 32 when it is pushed onto the piston base body 2′, but that additional guidance and centering of the ring element 3″ is achieved also by way of the recess 35 and the collar 36 of the lower solder connection, during assembly of the piston 1′.
In place of a single recess 27, disposed radially on the inside, according to the exemplary embodiment of the piston 1, 1″ shown in
The piston 1 according to the invention is produced in that first, a blank 39 for the piston base body 2 and a blank 40 for the ring element 3 are forged, as they are shown in
Furthermore, within the scope of forging the blank 39, a circumferential projection 44 that is at least approximately rectangular in cross-section is formed onto the radially outer piston-crown-side edge of the third surface 19. Both the recess 43 and the projection 44 have the purpose explained further below, within the framework of connecting the two blanks by means of solder.
Subsequent to this, the rotation-symmetrical contours particularly shown in
Subsequent to this, the two blanks 39 and 40 are then soldered to one another. In this connection, it is first of all necessary to put the blanks 39 and 40 together in such a manner that a gap occurs between the surfaces 8 and 18 and between the surfaces 19 and 20, in each instance, which is between 10 μm and 200 μm wide. When the blanks 39 and 40 are put together, a gap having this width is already achieved in that both the surfaces 8 and 18 and the surfaces 19 and 20 are brought into contact with one another without shape fit.
The recess 43 and the piston-crown-side surface of the projection 44 are then coated with a solder paste on the basis of nickel, after which the two blanks 39, 40 including the solder paste are heated to 1150° C. In this connection, the solder paste liquefies and penetrates between the surfaces 8 and 18 and the surfaces 19 and 20 due to the capillary effect, whereby the liquefied solder forces a gap having the dimensions indicated above to form between the surfaces 8 and 18 and the surfaces 19 and 20, due to the capillary effect. As a result, the surfaces 8, 18, 19, and 20 are wetted completely. Within the scope of the targeted cooling of the piston 1 that takes place afterwards, the solder paste solidifies and yields a defect-free solder connection between the two partly machined blanks 39 and 40.
In the embodiment of the piston base body 2′ and the ring element 3″ according to
The formed-on part 34, on which the cover region 35′ of the ring element 3″ comes to rest during assembly of the piston 1′, ensures, in this connection, that the piston-crown-side face surface 51 of the collar 36 and the skirt-side inner surface 52 of the recess 35 have a gap of 10 μm to 200 μm from one another after piston assembly, so that here, too, a gap that is broad enough for a defect-free solder connection is obtained.
In the embodiment of the piston base body 2″ and the ring element 3′ according to
The use of the soldering method for connecting the two piston parts has the advantage that the soldering temperature of 1150° C., to which the piston is heated in this connection, is equal to the forging temperature at which the two blanks 39 and 40 are forged, so that during cooling, the material characteristics that are typical for AFP steel can be set during cooling, in targeted manner.
Subsequent to this, the piston 1 is finished, in that the rotation-symmetrical outer contours of the piston 1, drawn in with broken lines in
Reference Symbol List
Number | Date | Country | Kind |
---|---|---|---|
10 2007 044 106 | Sep 2007 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/DE2008/001394 | 8/23/2008 | WO | 00 | 7/21/2010 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2009/033446 | 3/19/2009 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3349672 | Meier et al. | Oct 1967 | A |
4011797 | Cornet | Mar 1977 | A |
4356800 | Moebus | Nov 1982 | A |
4581983 | Moebus | Apr 1986 | A |
4651631 | Avezou | Mar 1987 | A |
6026777 | Kemnitz et al. | Feb 2000 | A |
6327962 | Kruse | Dec 2001 | B1 |
6698391 | Kemnitz | Mar 2004 | B1 |
7971355 | Scharp | Jul 2011 | B2 |
20080134880 | Lapp et al. | Jun 2008 | A1 |
Number | Date | Country |
---|---|---|
24 34 902 | Feb 1975 | DE |
27 30 120 | Jan 1979 | DE |
29 19 638 | Nov 1980 | DE |
198 46 152 | Apr 2000 | DE |
102 09 331 | Sep 2003 | DE |
600 28 870 | Jan 2007 | DE |
1 061 249 | Dec 2000 | EP |
1 077 324 | Feb 2001 | EP |
2 163 072 | Feb 1986 | GB |
WO 2007093289 | Aug 2007 | WO |
Number | Date | Country | |
---|---|---|---|
20100307445 A1 | Dec 2010 | US |