PISTON AND METHOD FOR PRODUCING SAME
20230023170 · 2023-01-26
Inventors
Cpc classification
F02F3/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F3/027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
The present invention relates to pistons (10) for use in internal combustion engines, having: a piston crown (12) which is adjoined by a piston skirt (14), wherein the piston skirt (14) has surfaces (18) which abut the cylinder wall during use of the piston, wherein the surfaces (16) have one or more friction-reducing coatings (18) and wherein depressions (20) are provided in the coating, which are arranged such that the spacing S between each two adjacent depressions (20) along the axial direction (A) of the piston and the width L of the depressions (20) along the axial direction (A) of the piston satisfy the formula S>2L.
Claims
1. The piston for use in internal combustion engines, comprising: a piston crown, which is adjoined by a piston skirt, wherein the piston skirt has surfaces which abut a cylinder wall during use of the piston, wherein the surfaces have one or more friction-reducing coatings and wherein a plurality of depressions are provided in the coating, which are arranged in such a way that a spacing S between each two adjacent depressions along the axial direction (A) of the piston and the width L of the depressions along the axial direction (A) of the piston satisfy the formula S>2L, wherein one or more of the depressions are enclosed by the coating in which they are formed, wherein the plurality of the depressions is provided in alignment along the circumference of the piston in one of the one or more coatings.
2. The piston according to claim 1, wherein the depressions extend through the coating such that they reach the material of the piston skirt.
3. The piston according to claim 1, wherein boundary surfaces of the depressions extend at an angle with respect to the coating and the material of the surfaces they adjoin.
4. The piston according to claim 1, wherein a length of extension E of at least some of the depressions along the circumferential direction is shorter than a length of extension E′ along the circumferential direction of the coating in which these are formed.
5. The piston according to claim 4, wherein the depressions that are adjacent to one another in the axial direction are offset relative to one another in the circumferential direction.
6. The piston according to claim 1, wherein the depressions have a substantially rectangular form.
7. The piston according to claim 1, wherein the depressions have a width L of less than 2 mm.
8. A method for producing a piston according to claim 1, wherein the coating including the depressions is applied by screen-printing.
9. The piston according to claim 1, wherein all of the depressions are enclosed by the coating.
10. The piston according to claim 4, wherein the length of extension (E) of all of the depressions in the circumferential direction is shorter than the length of extension (F) in the circumferential direction.
11. The piston according to claim 7, wherein the width L is in the range of 0.6 to 0.8 mm.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0025]
[0026]
[0027]
[0028]
[0029]
DETAILED DESCRIPTION OF THE DRAWINGS
[0030]
[0031] The cylindrical surfaces 16 abut the cylinder wall of the internal combustion engine during use of the piston and have a friction-reducing coating 18 of a polymer material containing graphite. The coating 18 is only provided on one part of the convex surface 16. The convex surface 16 adjoins the annular region with the annular grooves 13 of the piston. The coating 18 extends along the circumference of the piston over a length E′.
[0032] Rectangular depressions 20 are provided in the coating 18, which extend through the coating material such that the material of the piston is exposed through the depressions 20. The ends of the rectangular depressions may be rounded. A plurality of depressions 20 is lined up along the circumferential direction. There is a plurality of such rows of lined-up depressions 20, which are offset relative to one another along the circumferential direction such that the axially adjacent depressions 20 are offset relative to one another along the circumferential direction.
[0033] The depressions 20 are shown in more detail in
[0034]
[0035] It has been ascertained that a piston 10 designed as shown in
[0036]
[0037]
[0038]
[0039]
[0040] The coatings 18 to 18 III shown in