The disclosure relates to a piston for an internal combustion engine, configured as a two-piece gallery-cooled piston that comprises a main body and a ring element.
A piston for internal combustion engines is exposed to high thermal stresses and high alternating mechanical stresses caused by gas and mass forces that require suitable dimensioning and design. Severely stressed zones of the piston, for example, the combustion bowl in the piston crown and the ring zone, require effective cooling. To this end it is known to integrate a cooling gallery in the piston. A cooling medium, such as the lubricating oil for the internal combustion engine, circulates through the cooling gallery cavity. The efficacy of piston cooling is determined. in particular, by the volume of cooling medium exchanged in the cooling gallery.
A two-piece piston is known from DD 123 962 A1 which includes a main body and a ring element. The separate, circular ring element, which includes comprises the top land and the ring zone of the piston and delimits the cooling gallery to the outside, is attached to the main body by means of a screw thread. The ring element is fixed in position in the installed state by means of dowels or threaded pins that are used between the main body and the ring element. U.S. Pat. No. 6,155,157 discloses a cooling gallery piston with two components that can be produced separately and then joined in a material-to-material bond using friction welding.
It would be desirable to create a two-piece cooling-gallery piston that includes a permanent connection of the individual components.
A piston has the ring element and the main body jointly forming two circumferential dividing planes offset to each other to which end two respective corresponding interacting joining webs of the ring element and of the main body are joined in a material-to-material bond. The ring element is supported on dedicated joining webs of the main body through two joining webs positioned in different locations and offset in height. This design principle permits a piston construction with which a permanent joining of the individual piston components can be realized. At the same time, the concept has the advantage of optimizing the cooling gallery through appropriate design of the ring element to improve piston cooling and to realize a piston that can tolerate higher thermal loads.
Additionally, using this design, the construction or the design of the separate ring element, in particular with respect to wall thicknesses of individual piston sections, can be manipulated to reduce piston weight, for example. The possibility further exists of optimizing the top land, the ring zone or the ring carrier of the ring element. This construction offers the possibility of locating the dividing planes between the main body and the ring element in such a way that an optimal location results with respect to component strength and/or welding.
The piston design further offers the possibility of specially configuring the thermally and mechanically highly stressed ring element. The ring element including the top land and the ring zone for the piston rings can be optimized with respect to durability and wear resistance.
In accordance with one aspect of the piston, no defined position for the dividing planes is provided. The interacting, circumferential dividing planes can be advantageously configured in such a way that the dividing planes are both offset to each other and aligned diverging from each other.
Depending on the layout criteria, for example, optimal cooling gallery design, an optimized location for welding or taking strength into consideration, a piston can have matching or differently shaped dividing planes. Accordingly, the piston offers the opportunity of providing two dividing planes between the ring element and the main body, offset in height, of which one can run vertically and the other horizontally.
A piston, in another aspect, has at least one of the two dividing planes is aligned obliquely, or inclined. With two inclined dividing planes the dividing planes can run in the same direction or counter to each other. Advantageously there is no specification for the direction for the respective dividing plane. With dividing planes inclined in opposite directions, a centering effect of these components can continue to be used when the ring element and the main body are joined.
For a piston design with one vertical and one horizontal dividing plane, a vertically aligned dividing plane can be provided in the piston crown between the ring element and the main body and a horizontally aligned dividing plane can be provided below the ring zone of the ring element. A maximum vertical offset results between the two dividing planes with this piston construction.
In accordance with another aspect, the main body forms a circumferential step on the outside whose joining web running concentric to a longitudinal axis of the piston is enclosed by the joining web of the ring element to form a vertical dividing plane. In this aspect, the length of the dividing plane can be advantageously affected by the axial length of the step, or ledge, wherein this concept simultaneously brings about a centering effect on the components when they are joined.
Another aspect further provides for the matching, interacting joining webs of the ring element and of the main body to have constant wall thicknesses. The effect of joining webs with at least approximately identically dimensioned wall thicknesses is a desirable optimal equalization of tension, or distribution of tension in the piston upper part.
The piston furthermore offers the advantage of producing the ring element and the main body from an identical material or from different materials. A multi-piece piston provides this advantage, wherein the choice of material can be made with respect to the particular thermal and/or mechanical stress. The ring element can be produced from a hard wearing, specifically thermally stable material. In order to save weight, a less hard wearing material, a light alloy for example, can be chosen as the material for the main body.
A method is additionally proposed to produce a piston that includes the following steps. First of all, a main body and a ring element are produced separately as blanks. These components can be produced as forged or cast blanks, by stamping or pressing, from a semi-finished material of a steel material. As an alternative, extrusion, forging or casting is suitable for producing the main body and the ring element. The production process for the main body and the ring element includes forming the joining webs without reworking. The main body and the ring element can be produced from a matching material or from different materials. With the subsequent pre-machining, the combustion bowl and a piston pin bore can be introduced into the main body along with piston ring grooves in the ring belt of the ring element.
Then the main body and the ring element are joined until two respective matching joining webs abut and form two dividing planes offset to each other. The main body is joined to the ring element in a material-to-material bond by subsequent welding of the joining webs.
Different methods can be employed for the material-to-material bond of the main body and the ring element. Friction welding, or multi-orbital or multi-linear friction welding is can be used. Alternatively, electron beam welding, resistance press welding, condenser discharge welding or laser welding is suitable. Soldering can be used, in addition, for material-to-material joining of the matching joining webs. After the welding process is complete, the weld seams that have formed externally are removed. Final machining and cleaning of the piston follows as the last step.
Additional features can be found in the following description and the drawings which show aspects of the present piston. Unless otherwise stated, identical or functionally identical components are given the same reference numerals.
For example, multi-orbital friction welding is employed in which, because of the extremely small, circular orbital movements, no, or only minor, weld beads 8, 9 are formed in the area of the dividing planes 4a, 5a that require no, or only minor, reworking. The wall thickness S1, S2 of the joining webs 6a, 6b and the joining webs 7a, 7b is can be constant as far as possible. A maximum height offset H results between the vertically aligned dividing plane 5a and the horizontally running dividing plane 4a. The main body 2 of the piston 1 includes a combustion bowl 12 introduced into a piston crown 10 eccentric or rotationally symmetrical to a longitudinal axis 11. A piston skirt 13 of the main body 2 includes two diametrically opposed piston pin bores 4 that are intended to receive a piston pin (not shown). An intermediate wall 16 surrounding the combustion bowl 12 delimits a cooling gallery 15 on the inside that is enclosed on the outside by the ring element 3. The cooling gallery 15 is closed circumferentially by the main body 2 with the ring element 3 after welding has been performed. When the engine is operating, a cooling medium can be selectively applied to the cooling gallery 15 through at least one inlet and one outlet (not shown). The ring element 3 has a top land 17 on the piston crown side to which a ring belt 18 is attached with ring grooves 19 that are intended to receive piston rings (not shown).
In accordance with
The piston 1 in
Number | Date | Country | Kind |
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10 2012 217 599.7 | Sep 2012 | DE | national |
This continuation application claims priority benefit to U.S. patent application Ser. No. 14/431,635 the entire contents of which are incorporated herein by reference.
Number | Date | Country | |
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Parent | 14431635 | Mar 2015 | US |
Child | 15616104 | US |