Minimizing Oil Leakage From Rocking Journal Bearings Of Two-Stroke Cycle Engines
US-2016356308-A1 · Dec 8, 2016 · US
US10309447B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10309447-B2 |
| Application number | US-201715468686-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 24, 2017 |
| Priority date | Mar 31, 2016 |
| Publication date | Jun 4, 2019 |
| Grant date | Jun 4, 2019 |
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A method for machining a surface of a metal component, in particular a connecting rod or a cam for a motor vehicle, including the following steps: providing a metal component which has a surface to be machined; premachining the surface to be machined; structuring the premachined surface by a laser beam in such a way that elevations but no depressions are formed as laser structures on the premachined surface with respect to the level thereof.
Opening claim text (preview).
What is claimed is: 1. A method for machining a surface of a metal component, comprising: machining a surface on a metal component and forming rectilinear structures in a circumferential direction, and structuring the machined surface using a laser beam, wherein the machined surface is laser-structured in such a way that elevations but no depressions are formed as laser structures with respect to a level of said surface, and the elevations are arranged in a row that is orthogonal to the rectilinear structures. 2. The method as claimed claim 1 , wherein the surface is an inner surface of an aperture in the metal component, wherein the laser beam is guided in a direction orthogonal to the circumferential direction of the inner surface. 3. The method as claimed in claim 1 , wherein the laser beam is operated in a pulsed manner along at least one machining track over the surface. 4. The method as claimed in claim 3 , wherein the elevations which are formed within a machining track are formed in an overlapping manner on the surface and have an overlap of greater than or equal to 60 percent. 5. The method as claimed in claim 3 , wherein the elevations are generated in a plurality of machining tracks of respectively overlapping elevations on the surface, wherein the machining tracks are spaced apart from one another free of overlap and have a spacing of at least 50 percent of a track width of the machining tracks. 6. The method as claimed in claim 3 , wherein the metal component is a steel component, the machined steel surface of which is laser-structured with an average beam power of 9±0.5 watt. 7. The method as claimed in claim 3 , wherein the metal component is a titanium component, the machined titanium surface of which is laser-structured with an average beam power of 8±0.5 watt. 8. The method as claimed in claim 1 , wherein the elevations have a round shape. 9. The method as claimed in claim 1 , wherein the elevations have a width of less than 100 μm. 10. The method as claimed in claim 1 , wherein the elevations lave a height of less than 20 μm. 11. The method as claimed in claim 1 , wherein the surface is an inner circumferential surface and the machining on the surface generates a surface structure which is oriented in the circumferential direction of the inner circumferential surface. 12. The method as claimed in claim 11 , wherein the inner circumferential surface is laser-structured in a plurality of spaced-apart angular sections. 13. The method as claimed in claim 1 , wherein the metal component is a connecting rod for a motor vehicle. 14. The method as claimed in claim 1 , wherein a height (R) of the rectilinear structures is greater than a height (h) of the elevations. 15. The method as claimed in claim 1 , wherein a plurality of elevations are disposed between adjacent rectilinear structures. 16. The method as claimed in claim 1 , wherein the elevations are arranged in a plurality of rows and the rectilinear structures are also arranged in a plurality of rows, and the plurality of rows of elevations are orthogonal to the plurality of rows of rectilinear structures.
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