This application is filed pursuant to 35 USC 371 claiming priority benefit to PCT/EP2016/069170 filed Aug. 11, 2016 and German patent application 102015215313.4 filed Aug. 11, 2015, the entire contents of both applications herein incorporated by reference in their entirety.
The invention relates to a piston for an internal combustion engine.
A piston for internal combustion engines is known from DE 197 40 065 A1 which forms the generic type. In the case of this piston, the hubs are set back in the bolt axial direction in such a manner that the outer hub spacing is 60% to 65% of the piston diameter or less. The hub outer surfaces which connect the two sliding surfaces to each other have a rectilinear (linear) profile, as viewed over the height of the sliding surfaces. In the case of this piston, the hub outer surfaces (also called box walls) are basically not flat, but rather curved, specifically both in sections parallel to and also perpendicularly to the piston axis. However, the direction of curvature of the surface in sections perpendicular to the piston axis is always constant for the entire surface of the box wall. As the spacing between the box walls becomes smaller upwardly (in the direction of the piston head), this results in an upwardly decreasing width of the supporting sliding surface.
DE 197 40 065 A1 therefore discloses a light metal piston for internal combustion engines comprising a roof-shaped piston head with a combustion space depression, wherein the hubs are set back in the bolt axial direction in such a manner that the outer hub spacing is 60% to 65% of the piston diameter or less, and wherein an open cavity enclosing an angle of between 45° and 60° in the circumferential direction is provided above the outer surfaces of the set-back hubs, said cavity extending in the direction of the piston head into the region behind the ring field, and wherein the hub inner surfaces are formed trapezoidally or recessed in a stepped manner, and the skirt length is 40% to 45% of the piston diameter.
Furthermore, a piston is known from DE 101 45 589 A1. Said piston has a piston head which consists of a ring field with a plurality of annular grooves and optionally a combustion space depression. In the direction of movement of the piston, a piston skirt is arranged under the piston head, wherein said piston skirt consists of two skirt wall sections which support the piston during operation in the internal combustion engine and which serve to guide the piston in the cylinder of the internal combustion engine. The skirt wall sections are connected to one another via set-back connecting walls, wherein the connecting walls do not have a connection to the running surface of the cylinder.
In the piston in said DE 101 45 589 A1, the connecting walls have a curved profile which may be convex, concave or a combination of said curves. Furthermore, in the region of the connecting walls in this known piston the lower edge of the ring field is formed so as to protrude beyond said connecting walls (projecting length) and is at least partially hollowed out there such that a free space is produced in order to save weight.
The invention is based on the object of producing a piston for an internal combustion engine with a reduction in the piston mass and improved distribution of stresses in the box region of the piston.
According to the invention, it is provided that the piston has a spacing between the box walls of between 35% and 51% of the piston diameter on its pressure side, and/or that the piston has a spacing between the box walls of between 26% and 39% of the piston diameter on its counterpressure side.
Pressure side refers to that side of the piston or cylinder on which the piston is supported during the combustion. The pressure side is opposed to the direction of rotation of the crankshaft. The counterpressure side is that side of the piston or cylinder which lies opposite the pressure side. By means of the skirt support designed according to the invention, a more homogeneous distribution of stresses within the piston is achieved. Even larger ring field undercuts can therefore be made. The mass of the piston is significantly reduced, but at the same time withstands the demands of current internal combustion engines having extremely high thermal and mechanical loads.
Furthermore, it is provided according to the invention that the piston has a spacing between the box walls of between 40% and 51%, preferably between 46% and 49% of the piston diameter, on its pressure side. It is also provided according to the invention that the piston has a spacing between the box walls of between 30% and 39%, preferably between 34% and 37% of the piston diameter, on its counterpressure side. By this means, the box walls move closer to each other, as a result of which this leads to a further saving on material. Smaller skirt surfaces on the pressure side and counterpressure side of the piston lead to the reduction in the friction.
Furthermore, it is provided according to the invention that a spacing between an upper edge of a fire land and a vertex of a free space transversely with respect to a bolt bore axis of the piston is smaller than the extent of the fire land. Furthermore, it is provided according to the invention that the spacing between the upper edge of the fire land and the vertex of the free space parallel to the bolt bore axis is smaller than the extent of the fire land. The larger undercuts in the weight pockets of the ring field permit the use of optimized casting mold technology.
Furthermore, it is provided according to the invention that the spacing between the upper edge of the fire land and the vertex of the free space transversely with respect to the bolt bore axis of the piston and/or a spacing between the upper edge of the fire land and the vertex of the free space parallel to the bolt bore axis are/is between 50% and 95%, preferably between 65% and 90%, smaller the extent of the fire land. By this means, a saving on material and a reduction in the piston mass are achieved.
Furthermore, it is provided according to the invention that a radial depth of a lift-out groove has a size of greater than or equal to 2 millimeters (mm), preferably greater than or equal to 3 mm, in particular greater than or equal to 4 mm By means of as large a radial depth as possible of the lift-out groove, the piston mass is reduced in this region.
Furthermore, it is provided according to the invention that a spacing between a center line of the box wall on the pressure side and a center line of the piston transversely with respect to the bolt bore axis is greater than a distance between a center line of the box wall on the pressure side and the center line of the piston transversely with respect to the bolt bore axis on the circumference of the piston. By means of the box walls designed according to the invention, a reduction in the extraction slope for the casting mold inserts has been realized. This in turn permits an enlargement of the free spaces behind the ring field, which leads to a reduction in the piston mass.
Furthermore, it is provided according to the invention that a spacing between a center line of the box wall on the counterpressure side and the center line of the piston transversely with respect to the bolt bore axis is smaller than the spacing between the center line of the box wall on the pressure side and the center line of the piston transversely with respect to the bolt bore axis. By means of the box walls designed according to the invention, a reduction in the extraction slope for the casting mold inserts has been realized. This in turn permits an enlargement of the free spaces behind the ring field, which leads to a reduction in the piston mass.
Furthermore, it is provided according to the invention that a spacing between the center line of the box wall on the counterpressure side and the center line of the piston transversely with respect to the bolt bore axis on the circumference of the piston is smaller than the spacing between the center line of the box wall on the counterpressure side and the center line of the piston transversely with respect to the bolt bore axis. By means of the box walls designed according to the invention, a reduction in the extraction slope for the casting mold inserts has been realized. This in turn permits an enlargement of the free spaces behind the ring field, which leads to a reduction in the piston mass.
Furthermore, it is provided according to the invention the spacing between the center line of the box wall on the pressure side and the center line of the piston transversely with respect to the bolt bore axis and the center line of the box wall is 10% to 35%, preferably 15% to 30%, in particular 20% to 25% of the piston diameter. The curved hub in conjunction with the newly designed skirt connection makes it possible, by means of the resulting support of the head, to minimize stresses in the combustion space depression in the case of highly loaded direct injection internal combustion engines.
Hub end surfaces fully integrated in the box contour. In comparison to the prior art, a reduction in mass by approximately 15% because of the homogeneous box wall design is an improved distribution of stresses is obtained.
By means of the use of suitable piston alloys, in particular the applicant's piston alloy KS 309, and the consequent adaption of the piston design to the resulting material-specific advantages, the wall thickness of the piston head could be reduced by up to 30%. This achieves a reduction in the mass of the piston.
The basic concept is explained below with reference to the figures. Further details of the invention are described below in the figures with reference to illustrated exemplary embodiments.
The illustration of
The piston skirt 2 consists of skirt wall sections 5 which support the piston 1, wherein the skirt wall sections 5 are connected to one another by means of set-back connecting walls 6. The connecting walls 6 have a curved profile, wherein different configurations can be provided with respect to the curved profile of the connecting walls 6. Reference is made to said curved profile (concave and/or convex from one skirt wall section to the other skirt wall section and/or in its profile in the piston stroke axis 11) since said profile is particularly important in terms of saving weight while simultaneously retaining the necessary strength. The set-back connecting walls 6 also have a bolt bore 7 for receiving a bolt for connecting the piston 1 to a connecting rod (not illustrated). A bolt bore axis 8 is depicted within the bolt bore 7. The piston head 3 has an optional combustion space depression 10. Furthermore, it is shown that there is a free space 21 in the region of the piston head 3, set back behind the ring field 4 and above the bolt bore 7.
R1 indicates the radius of the box wall 14 above the bolt bore 7. The radius of the box wall 14 on the pressure side 12 of the piston 1 is referred to by R2. R3 in turn stands for the radius of the box wall 14 on the counterpressure side 13 of the piston 1.
“A” denotes the spacing between the center line 15 of the box wall 14 on the pressure side 12 and the center line 25 of the piston 1 transversely with respect to the bolt bore axis 8. “B” indicates the spacing between the center line 15 of the box wall 14 on the pressure side 12 and the center line 25 of the piston 1 transversely with respect to the bolt bore axis 8 on the circumference of the piston 1. “C” stands for the spacing between the center line 16 of the box wall 14 on the counterpressure side 13 and the center line 25 of the piston transversely with respect to the bolt bore axis 8. “D” is the spacing between the center line 16 of the box wall 14 on the counterpressure side 13 and the center line 25 of the piston 1 transversely with respect to the bolt bore axis 8 on the circumference of the piston 1.
Spacing with the applicable conditions
Spacing A: 20% to 25% of the piston diameter 20
Spacing B: B<A
Spacing C: C<A
Spacing D: D<C
“X1” denotes a spacing between the box walls on the counterpressure side according to DE 10 2005 041 002 A1. “X2” indicates the spacing between the box walls on the counterpressure side according to the exemplary embodiment from
The following conditions are applicable:
X1>X2 and Y1>Y2
“W1” denotes the angle of the extraction slope 22 on the pressure side 12 of the piston 1. “W2” indicates the angle of the extraction slope 22 on the counterpressure side 13 of the piston 1.
The following condition is applicable:
W1>W2
The pressure side 12 has a spacing between the skirt surfaces or box wall spacing 27 of between 46% and 51% of the piston diameter 20. On the counterpressure side 13, there is a spacing between the skirt surfaces or a box wall spacing 28 of between 34% and 39% of the piston diameter 20.
Spacings between the skirt surfaces on the pressure side of between 52% and 57% and on the counterpressure side of between 40% and 45% of the piston diameter 20 are known from the prior art DE 10 2005 041 002 A1. A significant reduction in the skirt surfaces has therefore been achieved.
“X” describes the spacing between the upper edge of the fire land 29 and the vertex 30 of the free space 21 transversely with respect to the bolt bore axis 8. “Y” in turn depicts the spacing between the upper edge of the fire land 29 and the vertex 30 of the free space 21 parallel to the bolt bore axis 8. “FS” illustrates the dimension of the fire land 29. The dimension X and/or the dimension Y are/is smaller than the dimension FS, preferably between 65% and 90%.
The following conditions are applicable
FS>X and FS>Y
Number | Date | Country | Kind |
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10 2015 215 313 | Aug 2015 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2016/069170 | 8/11/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2017/025608 | 2/16/2017 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
6659063 | Nomura | Dec 2003 | B2 |
20100147251 | Blau et al. | Jun 2010 | A1 |
20130233270 | Brandt et al. | Sep 2013 | A1 |
Number | Date | Country |
---|---|---|
204327307 | May 2015 | CN |
204851463 | Dec 2015 | CN |
1974065 | Dec 1967 | DE |
10145589 | Apr 2003 | DE |
102005041002 | Mar 2007 | DE |
102011080822 | Feb 2013 | DE |
102011085448 | May 2013 | DE |
102014114785 | Apr 2015 | DE |
2029318 | Mar 2009 | EP |
H0299245 | Aug 1990 | JP |
2002317691 | Oct 2002 | JP |
Number | Date | Country | |
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20180306139 A1 | Oct 2018 | US |