Applicant claims priority under 35 U.S.C. §119 of German Application No. 10 2005 042 003.6 filed Sep. 5, 2005. Applicant also claims priority under 35 U.S.C. §365 of PCT/DE2006/001548 filed Sep. 2, 2006. The international application under PCT article 21(2) was not published in English.
The invention relates to a liquid-cooled composite piston in accordance with the preamble of the claim.
A liquid-cooled composite piston that consists of an upper part forming the piston head and a lower part having the piston skirt is known from the Offenlegungsschrift [examined patent application published for public scrutiny] DE 41 31 275 A1. The upper part and the lower part are connected with one another by means of an expansion screw, whereby a sleeve is disposed between the head of the expansion screw and a collar of the lower part that serves to support the expansion screw, which sleeve has radial bores by way of which cooling oil that has collected in an inner cooling chamber can drain off.
It is a disadvantage, in this connection, for one thing, that the expansion screw requires a relatively large amount of space, which prevents a reduction in the compression height and thus a reduction in the axial dimensions of the piston. For another thing, unhindered draining of cooling oil out of the inner cooling chamber requires an additional sleeve having radial bores, which makes the assembly of the piston known from the state of the art rather complicated.
It is the task of the invention to avoid these disadvantages of the state of the art.
This task is accomplished with the characteristics standing in the characterizing part of the claim.
The invention will be described below, using the drawings. These show
A two-part, liquid-cooled composite piston 1 is shown in
Two pin bosses 8, 8′ each having a pin bore 9, 9′ are disposed on the underside of the lower part 3 that faces away from piston crown 4. In this connection, the radially outer face surfaces 29, 29′ of the pin bosses 8, 8′ are offset radially inward with regard to the ring wall 5. The pin bosses 8, 8′ are connected with one another by way of skirt elements 10, 10′.
The upper part 2 and the lower part 3 of the piston 1 are connected with one another by way of a radially inner, ring-shaped contact surface 11 and by way of a radially outer, ring-shaped contact surface 12, disposed concentric to the former. The radially outer contact surface 12 is formed by the piston-crown-side face surface of a support land 14 that runs radially on the outside, and is formed on, on the piston crown side, partially onto the skirt elements 10, 10′ (
During assembly of the piston 1, its upper part 2 and its lower part 3 can be aligned coaxially with one another in that the inner side of the lower face of the ring wall 5 has a cylindrical recess 31, the inside shape of which is complementary to the shape of the step 30 of the outer contact surface 12, so that during assembly of the piston 1, the step 30 can be introduced into the recess 31, thereby achieving coaxial alignment of the upper part and lower part of the piston 1.
The inner contact surface 11 is formed by the ring-shaped, piston-crown-side face of a lower part foot 15 that runs on the circumference radially within the support land 14, and, like the support land 14, is formed on, partly onto the skirt elements 10, 10′ (
An outer cooling channel 13 disposed in the piston-crown-side edge region of the piston 1 is formed by the upper part 2 and by the lower part 3 of the piston 1, the radially outer delimitation of which channel is formed partly by the ring wall 5 and partly by the support land 14, the radially inner delimitation by the lower part foot 15, the axially upper delimitation by the piston crown 4, and the axially lower delimitation by the lower part 3 of the piston 1. Cooling oil is passed into the outer cooling channel 13 by way of at least one oil feed channel 16 that opens into the piston interior 28.
The piston 1 has another ring-shaped inner cooling channel 18, disposed coaxial to the piston axis 17, which has a lesser radial diameter than the outer cooling channel 13, and is disposed within the outer cooling channel 13, seen in the radial direction. Axially at the top, the inner cooling channel 18 is delimited by the piston crown 4, radially on the outside partly by the lower part foot 15 and partly by a formed-on part 33 that narrows conically in the direction facing away from the piston crown, disposed radially on the inside of the lower part foot 15, axially at the bottom by a hexagonal nut 19 that will be explained in greater detail below, and radially on the inside by a pin 20 configured cylindrically, which is disposed on the underside of the piston crown 4, coaxial to the piston axis 17. The outer cooling channel 13 is connected with the inner cooling channel 18 by way of groove-shaped overflow channels 22, 22′ worked into the inner contact surface 11. The outer cooling channel 13 and the inner cooling channel 18 can also be connected with one another by way of bores made in the lower part foot 15.
The mantle surface of the pin 20 has an end region facing away from the piston crown, having an outside thread 23 (
In this connection, the hexagonal nut 19 consists of a threaded part 24 having the inside thread 34 and an outer surface that is hexagonal, seen in the radially horizontal cross-section, and a collar 25 formed onto it on the piston crown side, which, in the present exemplary embodiment, has two radially disposed bores or millings 26, 27 that lie opposite one another, which connect the inner cooling channel 18 with the piston interior 28. Once the hexagonal nut 19 has been screwed tight, the piston-crown-side face of the collar 25 lies against the face of the formed-on part 33 that faces away from the piston crown side.
Proceeding from the piston interior 28, this results in a continuous oil channel by way of the oil feed channel 16, the outer cooling channel 13, the overflow channels 22, 22′, the inner cooling channel 18, and the bores (millings) 26 and 27 in the collar 25 of the hexagonal nut 19, back to the piston interior 28.
Number | Date | Country | Kind |
---|---|---|---|
10 2005 042 003 | Sep 2005 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/DE2006/001548 | 9/2/2006 | WO | 00 | 6/17/2008 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2007/028364 | 3/15/2007 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3358657 | Herrmann | Dec 1967 | A |
3465651 | Tromel | Sep 1969 | A |
4375782 | Schieber | Mar 1983 | A |
5081968 | Bruni | Jan 1992 | A |
6729291 | Scharp et al. | May 2004 | B1 |
20080121204 | Scharp | May 2008 | A1 |
20090260593 | Messmer | Oct 2009 | A1 |
Number | Date | Country |
---|---|---|
14 76 111 | Oct 1970 | DE |
29 36 630 | Mar 1981 | DE |
41 31 275 | Mar 1993 | DE |
102 57 022 | Jun 2004 | DE |
0 604 223 | Jun 1994 | EP |
1 037 133 | Sep 1953 | FR |
Number | Date | Country | |
---|---|---|---|
20090139481 A1 | Jun 2009 | US |