Piston With A Structured Design

Abstract

Piston (1) of an internal combustion engine, which piston is designed in structured construction, comprising two oppositely arranged load-bearing skirt wall portions (2), wherein a connecting wall (3) respectively extends, starting from a pin boss (4), in the direction of the side edge of the load-bearing skirt wall portions (2), characterized in that in an interior of the piston (1) is (are) disposed at least one rib (5, 6, 7), preferably three ribs (5, 6, 7), and the material of the regions around the at least one rib (5, 6, 7) is reduced.

Claims

1. A piston (1) of an internal combustion engine, which piston is designed in structured construction, comprising two oppositely arranged load-bearing skirt wall portions (2), wherein a connecting wall (3) respectively extends, starting from a respective one of two pin bosses (4), in the direction of a side edge of the load-bearing skirt wall portions (2), characterized in that in an interior of the piston (1) is disposed at least one of a first rib (5), a second rib (6), or a third rib (7) and wherein a material thickness of a region around the at least one of the first, the second or the third rib is reduced.

2. The piston (1) of claim 1, wherein the at least one rib comprises the first rib (5), disposed on an inner side of the respective load-bearing skirt wall portion (2).

3. The piston (1) of claim 1, wherein the at least one rib comprises the second rib (6) which connects the two pin bosses (4) to one another.

4. The piston (1) of claim 1, wherein the at least one rib comprises a third rib (7) oriented transversely to a pin bore axis.

5. The piston (1) of claim 1, wherein an inward facing side of each of the two pin bosses (4) defines a recess (8) positioned around one of an upper or lower apex thereof.

6. The piston (1) of claim 5, characterized in that, around the first rib (5), the load-bearing skirt wall portion (2) has a reduced wall thickness (RW).

7. The piston (1) of claim 5, wherein each of the two pin bosses (4) define a draft groove (10) positioned opposite the respective recess (8).

8. The piston (1) of claim 1 wherein the piston (1) further defines at least one opening (11) for a cooling medium, wherein around the opening (11) is positioned a circumferential bead (12).

9. The piston (1) of claim 8, characterized in that in a section around the at least one opening (11), together with a section of the circumferential bead (12), defines a trough (13).

10. (canceled)

11. A method for producing a piston blank, comprising a main body, in a forging process, wherein, during the forging process, a protruding collar is created, deformed, and subsequently a free circumferential end of the deformed collar is integrally connected to the main body of the piston blank, characterized in that the piston blank is provided in an interior at specific places with at least one rib, and wherein regions around the at least one rib are reduced in terms of a wall thickness in relation to the wall thickness without ribs.

12. The method of claim 11 further comprising forming a recess in a region of an inner facing side of a pin boss defining a pin bore, the recess extending around an upper and lower apex of the pin bore.

13. The method of claim 11, wherein the piston blank further comprises a main body, a collar portion connected to the main body and defining a first annual groove and a second annular groove positioned below the first annual groove, the collar further having a free circumferential marginal region, the main body defining a third annular groove positioned below the second annular groove, the method further comprising joining the collar free circumferential marginal region to the main body at a a joining region positioned between the third annular groove and the second annular groove.

14. The method of claim 13 wherein after the joining of the collar free circumferential marginal region to the main body of the piston blank, the method further comprising finishing to size of the piston blank.

15. The piston (1) of claim 2 wherein the at least one rib further comprises the second rib (6) which connects the two pin bosses (4) to one another.

16. The piston (1) of claim 15, wherein the at least one rib further comprises the third rib (7) oriented transversely to a pin bore axis.

17. The piston (1) of claim 16, wherein an inward facing side of each of the two pin bosses (4) defines a recess (8) positioned around one of a pin boss upper or lower apex thereof.

18. The piston (1) of claim further comprising: a main body; and a collar portion connected to the main body, the collar portion having a free circumferential marginal region, the collar defining a first annular groove (15) and a second annular groove (16) positioned below the first annular groove, the main body defining a third annular groove (17) positioned below the second annular groove, wherein the collar circumferential marginal region is connected to the main body at a joining region (18A) positioned between the second and the third annular groove.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0014] FIG. 1 is a bottom perspective view of one example of the invention.

[0015] FIG. 2 is an alternate bottom perspective view of FIG. 1.

[0016] FIG. 3 is an alternate bottom perspective view of FIG. 1.

[0017] FIG. 4 is an alternate bottom perspective view of FIG. 2.

[0018] FIG. 5 is a partial cross-sectional view of a prior art piston.

[0019] FIG. 6 is a partial cross-sectional view of an example of the present invention.

DETAILED DESCRIPTION

[0020] An illustrative embodiment by which the structured construction and the recess on the inner side of the pin boss is discernible is shown in FIGS. 1 to 4.

[0021] FIG. 1 shows in a three-dimensional view a piston 1 from below, wherein opposite load-bearing skirt wall portions are denoted by 2 and connecting walls which connect the load-bearing skirt wall portions 2 one to another are denoted by 3. In each case, a connecting wall 3 extends, starting from a pin boss 4, in the direction of the side edge of the load-bearing skirt wall portions 2.

[0022] At this point, it should be pointed out that, in the production of this piston 1, the method according to DE 10 2004 031 513 A1 can be applied, but does not have to be applied. Since the piston main body which forms the subsequent finished piston 1 is forged, care should be taken to ensure that the elements involved (such as skirt wall portions 2, connecting walls 3, pin bosses 4 and the like) have the draft angles necessary for the forging operation. Instead of a forging operation, production by a casting operation can also, of course, be considered.

[0023] The structured construction of the piston 1 is characterized by at least one rib at a suitable place.

[0024] The ribs are constituted by a first rib 5 which is disposed on the inner side of the respective load-bearing skirt wall portion 2, and/or by a second rib 6 which in the interior connects the two pin bosses 4 one to another, and/or by a third rib 7 which runs transversely to a pin bore axis.

[0025] Particular preference is given to the combination of ribs 5, 6, 7 as are represented in FIG. 1.

[0026] In combination or, where appropriate, also in isolation, the piston 1 can have on the inward facing side of the pin boss 4, around the upper and/or lower apex thereof, respectively a recess 8. As a result of this recess 8, weight savings are made, yet the strength of the pin boss 4 is not compromised.

[0027] The above-stated measures are represented in combination also in FIG. 2. In this, in particular the course and arrangement of the first rib 5 and/or of the second rib 6 and/or of the third rib 7 is discernible. In this context, it should be pointed out that it is of particular inventive importance that, in the regions around the ribs 5, 6, 7, the wall thicknesses or the material thickness are reduced. With respect to the load-bearing skirt wall portions 2, it is displayed that, around the rib 5, the load-bearing skirt wall portion 2 has a reduced wall thickness RW.

[0028] For further clarification, in FIG. 2 a draft groove is denoted by 10 and an opening for a cooling medium which can be introduced into a cooling duct (not represented here) of the piston, and evacuated therefrom, is denoted by 11. FIG. 3 is based on the piston 1 according to FIG. 1, wherein, in order to clarify the course of the ribs 5, 6, 7 and their transition into regions with reduced wall thickness RW, gridlines are displayed.

[0029] The same applies to FIG. 4, which is based on the piston 1 according to FIG. 2. Here it is additionally displayed and apparent that around the opening 11 is arranged a circumferential bead 12, wherein in a section around the opening 11, together with a section of the circumferential bead 12, is formed a depression (trough 13). As a result, not only can weight be reduced, but also cooling medium can be collected in the trough 13 when this cooling medium, upon the up and down movement of the piston 1 in the cylinder of the internal combustion engine, is injected into the opening 11 and around this. The circumferential bead 12 thus effects a stiffening, and the trough 13 effects not only a material reduction, but also a storage reservoir for the cooling medium with a view to further improved cooling of the piston 1. By 14 is denoted, within the cooling duct (not represented in detail), a jet splitter, which can be present, but does not have to be present.

[0030] While in FIGS. 1 to 4 the two possible measures comprising the structured construction and the recess on the inner side of the pin boss are shown, in FIGS. 5 and 6 the change in terms of the location of the joining region is discernible.

[0031] FIG. 5 shows the situation in the case of the piston as is known from DE 10 2004 031 513 A1. This known piston has three annular grooves, first annular groove 15, second annular groove 16, third annular groove 17, wherein the free circumferential marginal region of the deformed collar is integrally connected in a joining region 18 to the main body of the piston blank. This joining region 18 lies in the region of the bottommost (third) annular groove 17.

[0032] In contrast hereto, the piston 1 according to the invention as is represented in FIG. 6 is altered to the effect that the joining region 18A has been shifted into the region between the middle (second) annular groove 16 and the bottommost (third) annular groove 17.

[0033] By 19 is denoted a cooling duct which runs in an annular course behind the ring field of the piston 1.

REFERENCE SYMBOL LIST

[0034] 1 piston [0035] 2 load-bearing skirt wall portion [0036] 3 connecting wall [0037] 4 pin boss [0038] 5 rib [0039] 6 rib [0040] 7 rib [0041] 8 recess [0042] 9 pin bore [0043] 10 draft groove [0044] 11 opening [0045] 12 circumferential bead [0046] 13 trough [0047] 14 jet splitter [0048] 15 annular groove [0049] 16 annular groove [0050] 17 annular groove [0051] 18 joining region [0052] 19 cooling duct