Heat Input Zone Of A Piston, Having A Groove Flank Positioned In Said Heat Input Zone

Abstract

The invention relates to a piston of an internal combustion engine including at least one peripheral annular groove. The piston includes an upper part and a lower part permanently joined in the region of a joining plane by a friction welding method. The joining plane may be located between the upper flank and the lower flank of the annular groove. A heat-affected zone is generated due to the use of the friction welding and includes at least one of the upper flank or the lower flank of the annular groove. Where multiple annual grooves are used, the joining plane and heat-affected zone may be positioned on alternate annular grooves.

Claims

1. A piston of an internal combustion engine, comprising an upper portion and a lower portion which are joined together in a non-releasable manner in the region of a joining plane through a friction welding method, wherein the piston has at least one peripheral annular groove, characterized in that the joining plane is located between an upper flank and a lower flank of the at least one peripheral annular groove and a heat-affected zone which is produced as a result of the use of the friction welding method includes at least one of the upper flank or the lower flank of the at least one peripheral annular groove.

2. The piston as claimed in claim 1, wherein the joining plane is located centrally between the upper flank and the lower flank of the at least one peripheral annular groove, and the heat-affected zone includes the upper flank and the lower flank of the at least one peripheral annular groove.

3. The piston as claimed in claim 1, wherein the joining plane is located in a plane of the upper flank of the at least one peripheral annular groove, and the heat-affected zone includes the upper flank of the at least one peripheral annular groove.

4. The piston as claimed in claim 1, wherein the joining plane is located in a plane of the lower flank of the at least one peripheral annular groove, and the heat-affected zone includes the lower flank of the at least one peripheral annular groove.

5. The piston as claimed in claim 1, wherein the at least one peripheral annular groove comprises a lowest positioned peripheral annual groove having an upper flank and a lower flank, the joining plane is located centrally between the upper flank and the lower flank of the lowest peripheral annular groove, and the heat-affected zone includes the upper flank and the lower flank of the lowest peripheral annular groove.

6. The piston as claimed in claim 1, wherein the joining plane is located precisely centrally between the upper flank and the lower flank of the at least one peripheral annular groove.

7. The piston as claimed in claim 1, wherein the joining plane is located by less than or equal to 30% of a height of the at least one peripheral annular groove away from a center between the upper flank and the lower flank of the annular groove.

8. A piston for use in an internal combustion engine, the piston comprising: an upper portion; a lower portion connected to the upper portion along a joining plane through friction welding; a peripheral annual groove having an upper flank and a lower flank, the joining plane intersecting the peripheral annual groove; and a heat-affected zone in communication with the joining plane at the peripheral annual groove.

9. The piston of claim 8 wherein the peripheral annual groove comprises at least an upper groove and a lowest positioned groove, each groove having an upper flank and a lower flank, wherein the joining plane is positioned to intersect the lowest positioned peripheral annular groove.

10. The piston of claim 8 wherein the joining plane intersects the upper flank, and wherein the heat-affected zone further comprises the upper flank and a portion of a groove base connecting the upper flank and the lower flank.

11. The piston of claim 8 wherein the joining plane intersects the lower flank, and wherein the heat-affected zone further comprises the lower flank and a portion of a groove base connecting the upper flank and the lower flank.

12. The piston of claim 8 wherein the joining plane intersects a center of the peripheral annular groove positioned equally between the upper flank and the lower flank.

13. The piston of claim 12 wherein the heat-affected zone comprises the upper flank, the lower flank and a groove base connecting the upper and the lower flank.

14. The piston of claim 13 wherein a weld bead is generated in an area where the peripheral annular groove is formed.

15. The piston of claim 8 wherein the joining plane intersects the annular groove at a position distant from a center equally between the upper flank and the lower flank by less than or equal to 30% of a height defined between the upper flank and the lower flank.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The invention is described in greater detail below and with reference to the Figures.

[0015] FIG. 1 is a schematic partial side view of a piston showing one example of a joining plane and heat-affected zone.

[0016] FIG. 2 is an alternate example of the piston shown in FIG. 1.

[0017] FIG. 3 is an alternate example of the piston shown in FIG. 1.

[0018] FIG. 4 is an alternate example of the piston shown in FIG. 1.

[0019] FIG. 5 is an alternate example of the piston shown in FIG. 1.

[0020] FIG. 6 is an alternate example of the piston shown in FIG. 1.

DETAILED DESCRIPTION

[0021] FIG. 1 shows a piston which comprises an upper portion 1 and a lower portion 2.

[0022] The construction of these two portions 1, 2 is exemplary and the invention is not limited thereto.

[0023] The two portions 1 and 2 have joining faces which face each other and which are joined together in a non-releasable manner in a joining plane 3 by means of a friction welding method.

[0024] In this embodiment, the joining plane 3 is located substantially centrally between an upper flank and a lower flank of an annular groove 4. In this instance, the position of the joining plane 3 is precisely centrally between these two flanks, wherein the position of the joining plane 3 may also be displaced from this central position upward or downward (when FIG. 1 is viewed). The joining plane 3 may even be provided in the same plane in which the upper flank or lower flank of the annular groove 4 is arranged.

[0025] As a result of the friction welding method, a heat-affected zone 5 is produced (illustrated in dark grey), wherein firstly after the joining of the two portions 1, 2 by means of the friction welding method, the annular groove 4 is not yet present. This groove is first introduced (for example, plunge-cut) into the heat-affected zone 5 which is produced by means of a suitable processing operation, for example, a machining method. The geometry (cross-section) of the annular groove 4 is in this instance selected in such a manner that it is located completely inside the heat-affected zone 5 which is produced. On the groove base of the annular groove 4 there is formed a friction weld bead 6 which is arranged in a cooling channel 7. The cooling channel 7 may, but does not have to, be formed together by the upper portion 1 and the lower portion 2. Since after the non-releasable joining of these two portions 1, 2 the inner space of the cooling channel 7 is no longer available, the friction weld bead 6 remains in this region. The friction weld bead which is produced in an outward direction is removed either by introducing the annular groove 4 or preferably beforehand in a separate step. In this embodiment, the joining plane 3 is consequently located between the upper flank and the lower flank of the annular groove 4, wherein in this specific case the joining plane 3 is located centrally between the upper flank and the lower flank of the annular groove 4. This central arrangement of the joining plane 3 may also be displaced in the direction of the upper flank or the lower flank of the annular groove 4. It is even conceivable for the joining plane 3 to be located in the plane of the upper flank of the annular groove 4 or the joining plane 3 to be located in the plane of the lower flank of the annular groove 4.

[0026] In FIG. 1, the heat-affected zone 5 which is produced includes both the upper flank and the lower flank of the annular groove 4 and extends over a specific region even further in an upward direction and in a downward direction (when viewing FIG. 1).

[0027] In the embodiment according to FIG. 2, the joining plane 3 is located in the plane of the upper flank of the annular groove 4 and the heat-affected zone 5 which is produced includes the upper flank of the annular groove 4.

[0028] The same applies alternatively if the joining plane 3 is located in the plane of the lower flank of the annular groove 4 and the heat-affected zone 5 which is produced includes the lower flank of the annular groove 4.

[0029] Whilst with the above description it has been assumed that the heat-affected zone includes at least the lower flank and/or the upper flank and furthermore other regions of the annular groove 4, the heat-affected zone 5 of course also includes the groove base as far as the internal wall of the cooling channel 7.

[0030] In FIGS. 3 and 4, a similar situation is illustrated to the one shown in FIGS. 1 and 2, but in this instance when the central annular groove is used. This applies in a comparable manner to FIGS. 5 (similarly to FIGS. 2 and 4) and 6 (similarly to FIGS. 1 and 3) in which the position of the joining planes and the heat-affected zones which are produced on the lowest annular groove are illustrated.

[0031] It is self-evident that a piston may have more than three or less than two annular grooves and the invention can be used not only with one annular groove but also with at least two annular grooves.

[0032] In the Figures at the top, the hardening of the second upper groove flank as a result of the friction welding is shown, wherein during friction welding the heat-affected zone (HAZ) is produced.

[0033] In FIG. 5 or 6, in particular the upper groove flank of the third (lowest) annular groove is hardened by the friction welding which is particularly advantageous with a three-part oil ring.

[0034] In the above-mentioned embodiments, depending on the construction type of the two portions 1, 2 either there is provided only a single joining plane 3 in which the joining faces of the two portions 1, 2 face each other prior to the friction welding operation and are subsequently brought together and non-releasably connected to each other, or there are provided more than one joining plane with correspondingly constructed mutually facing joining faces of the two portions 1, 2, wherein the at least two joining planes are located in the same plane or in different planes.

[0035] In these exemplary variants, to which the invention is not, however, limited, the joining plane of the external or single friction weld connection between the upper portion and lower portion is not located centrally in the web between two annular grooves (as in DE 10 2010 033 881 A1), but instead the friction weld zone and consequently the heat-affected zone extends into the annular groove and where applicable also regions located therebehind (as far as the beginning of the cooling channel).

[0036] Whilst in the two illustrations of the Figures the heat-affected zone is shown in the region of the respective upper groove flank, it can also be envisaged to provide the heat-affected zone in the region of a lower groove flank.

[0037] In any case, the heat input can advantageously be used by the friction welding process for the subsequent hardening operation. [0038] 1. Upper portion [0039] 2. Lower portion [0040] 3. Joining plane [0041] 4. Annular groove [0042] 5. Heat-affected zone