Method for Processing a Cylinder
20200011418 ยท 2020-01-09
Inventors
Cpc classification
F02F1/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C23C4/02
CHEMISTRY; METALLURGY
B23B41/12
PERFORMING OPERATIONS; TRANSPORTING
F16J10/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J10/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B23P9/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
F16J10/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method for processing an inner wall of a cylinder of an internal combustion engine includes providing a cylinder and processing an inner wall of the cylinder. The cylinder extends along a cylinder axis. The inner wall of the cylinder is processed in such a manner that at least one first structural region and one second structural region are formed along the cylinder axis. A geometry of the first structural region differs in design from a geometry of the second structural region.
Claims
1. A method for processing an inner wall of a cylinder of an internal combustion engine, comprising the acts of: providing a cylinder, which extends along a cylinder axis; processing an inner wall of the cylinder in such a manner that at least one first structural region and one second structural region are formed along the cylinder axis, wherein a geometry of the first structural region differs in design from a geometry of the second structural region.
2. The method according to claim 1, further comprising the act of: introducing a parallel groove structure, which runs perpendicularly to the cylinder axis, for forming the first structural region.
3. The method according to claim 1, further comprising the act of: introducing a helical groove structure for forming the second structural region.
4. The method according to claim 1, further comprising the acts of: positioning/forming the first structural region in an upper portion of the cylinder; and positioning/forming the second structural region in a central portion of the cylinder.
5. The method according to claim 2, wherein the parallel groove structure comprises 2 to 8 webs.
6. The method according to claim 5, further comprising the acts of: forming an end web in a region of a subsequent bevel, in particular an inlet or outlet bevel, of the cylinder; and roughening at least the end web.
7. The method according to claim 6, further comprising the act of: processing the at least one first structural region and second structural region by forming.
8. The method according to claim 7, further comprising the act of: coating the inner wall.
9. The method according to claim 6, further comprising the act of: introducing a bevel in the region of the end web.
10. A structure of a crankcase, comprising: a cylinder that extends along a cylinder axis and has a coating, wherein the cylinder has at least one first structural region and one second structural region along the cylinder axis for fastening the coating, and a geometry of the first structural region differs in design from a geometry of the second structural region.
11. The structure according to claim 10, wherein the first structural region has a parallel groove structure which is oriented perpendicularly to the cylinder axis, and the second structural region has a helical groove structure.
12. The structure according to claim 10, wherein an upper and a lower end region of the cylinder have the first structural region, and a region located in between has the second structural region.
13. The structure according to claim 10, wherein the first structural region comprises 2 to 8 webs.
14. The structure according to claim 10, wherein the cylinder ends in an end web.
15. The structure according to claim 14, wherein the end web is beveled.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0048]
[0049]
DETAILED DESCRIPTION OF THE DRAWINGS
[0050]
[0051]
[0052]
LIST OF REFERENCE SIGNS
[0053] 10 Cylinder [0054] 12 Cylinder wall, inner wall [0055] 14 First structural region [0056] 16 Second structural region [0057] 30 Web [0058] 32 Groove [0059] 34 End web [0060] 36 (End) bevel, inlet/outlet bevel [0061] 40 Region [0062] 42 Critical region [0063] 50 Coating [0064] Z Cylinder axis
[0065] The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the embodiments of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.