Applicant claims priority under 35 U.S.C. §119 of German Application No. 103 46 822.6 filed Oct. 6, 2003. Applicant also claims priority under 35 U.S.C. §365 of PCT/DE2004/002209 filed Oct. 4, 2004. The international application under PCT article 21(2) was not published in English.
The invention relates to a piston for an internal combustion engine, in accordance with the preamble of claim 1.
A piston having a cooling channel disposed in the edge region of the piston crown is known from the European Patent EP 0 799 373 B1, which is covered on the skirt side by a two-part cover ring that stands under mechanical stress. The very complicated assembly of the cover ring, in particular, is disadvantageous in this connection. For assembly, the two elements of the cover ring, shaped as semi-circles, must first be biased using a relatively complicated special tool, so that they can be introduced into supports on the piston head, intended for this purpose, in the biased state.
It is the task of the present invention to avoid this disadvantage of the state of the art.
The problem is solved with the characteristics contained in the characterizing part of the main claim. Practical embodiments of the invention are the object of the dependent claims.
It is advantageous, for one thing, that the cover of the cooling channel, consisting of two half-shells, according to the invention, has a groove that is directed inward, by way of which the half-shells can be quickly and easily pushed onto a projection on the outside of the piston, which is shaped complementary to the groove shape. For another thing, the half-shells have snap-in connections in the region of the contact surfaces, by means of which the half-shells can be quickly connected with one another.
An exemplary embodiment of the invention will be described in the following, using the drawings. These show:
Above the pin boss supports 9, 9′, one pin boss 11, 11′ with a pin bore 3, 3′, in each instance, are each molded onto the piston crown 4. The faces 12 of the pin bosses 11, 11′ are disposed set back relative to the ring wall 7, in the direction of the piston longitudinal axis 13. The pin bosses 11, 11′ are connected with one another by way of skirt elements 14, 14′, which are each molded onto the piston crown 4 by way of a shaft connection 10, 10′. Between the skirt elements 14, 14′ and the ring wall 7, the piston 1 has recesses 15
On the radially outer side of the pin bosses 11 and 11′, and on the shaft connection 10, 10′, a circumferential, projection 16 is molded on, which has a cross-sectional shape formed in essentially rectangular manner, and the function of which consists in serving as a holding rail for two half-shells 17 and 17′, by which the cooling channel 6 is closed off, and by which the recesses 15 are furthermore covered in the region of the skirt elements 14 and 14′. For this purpose, the half-shells 17, 17′ each have a circumferential groove 18 on their insides, the inside surface of which groove is configured complementary to the outside surface of the projection 16, to such an extent that the half-shells 17, 17′ can be pushed onto the projection 16 by way of their grooves 18. In the present exemplary embodiment, the half-shells 17, 17′ consist of a heat-resistant plastic and are produced using the injection-molding method. It lies within the scope of the invention that the half-shells 17, 17′ can also consist of a different material, such as steel or aluminum, for example, whereby the half-shells can be cast or forged.
As will be explained below, the cross-sectional shape of the half-shells 17, 17′ varies as a function of whether they cover the cooling channel 6 in the region of the faces 12 of the pin bosses 11, 11′, as shown in the left half of
The function of the two aprons 19 and 21, 21′ consists in supporting the half-shells 17, 17′ partly relative to the skirt-side face 20 of the ring wall 7, and partly relative to the steps 22 of the skirt elements 14, 14′ on the piston crown side, particularly during faster back and forth movements of the piston, and thereby reliably fixing them in place in the axial direction. Furthermore, the half-shells 17, 17′, if they consist of steel, form a support for the ring wall 7 and therefore for the edge of the piston crown 4, making it possible to prevent bending of the piston crown edge in the direction of the pin bosses 11, 11′ in the case of greater stresses on the piston 1.
The section through the piston 1 and through the two half-shells 17 and 17′ along the line A-A or IV-IV, respectively, in
In
The snap-in connections 25, 25′ each consist of undercuts 27, 27′ made in the region of the one contact surfaces 28, 28′ of the half-shell 17, 17′, on its outside, and of snap-in arms 24, 24′ having snap-in hooks 29, 29′, directed inward and molded on in the region of the other contact surfaces 26, 26′ of the half-shells 17, 17′, in each instance, which snap into the undercuts 27, 27′ of the other half-shell 17′, 17, in each instance, when the two half-shells 17, 17′ are joined together. In the region of the contact surfaces 28, 28′, holder brackets 30, 30′ (see also
Furthermore, the half-shells 17, 17′ have semi-circular recesses 31, 31′ in cross-section, whereby one of the recesses 31′ corresponds to a recess 40 that is also semi-circular in cross-section and affixed in the region of the projections 16 on the piston outside, and thereby forms a circular opening 32 in cross-section. Furthermore, little feet 35 to 38 molded onto the half-shells shells 17, 17′ are shown in
Using
The perspective representation of the joined half-shells 17 and 17′ according to
Number | Date | Country | Kind |
---|---|---|---|
103 46 822 | Oct 2003 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/DE2004/002209 | 10/4/2004 | WO | 00 | 5/16/2006 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2005/035960 | 4/21/2005 | WO | A |
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6659062 | Issler | Dec 2003 | B1 |
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20050072394 | Gabriel et al. | Apr 2005 | A1 |
Number | Date | Country |
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662 863 | Oct 1987 | CH |
38 30 033 | Jun 1989 | DE |
197 20 958 | Nov 1998 | DE |
102 47 218 | Jul 2003 | DE |
102 09 168 | Sep 2003 | DE |
0 799 373 | Jan 1999 | EP |
WO 03085251 | Oct 2003 | WO |
Number | Date | Country | |
---|---|---|---|
20090250033 A1 | Oct 2009 | US |