Oil retention in the bore/piston interfaces of ported cylinders in opposed-piston engines
US-9482153-B2 · Nov 1, 2016 · US
US10145331B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10145331-B2 |
| Application number | US-201213444220-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 11, 2012 |
| Priority date | Oct 14, 2009 |
| Publication date | Dec 4, 2018 |
| Grant date | Dec 4, 2018 |
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An internal-combustion engine has a crankcase, with at least one cylinder for accommodating a piston, the inner face of which cylinder is provided with a coating forming a running surface for the piston. The coating has a plurality of pores and the average size of the pores and/or the pore surface proportion varies over the length of the cylinder.
Opening claim text (preview).
What is claimed is: 1. A method of producing a crankcase for an internal-combustion engine having at least one cylinder, the method comprising the acts of: casting the crankcase of a light-metal material; precision-turning an inner face of the cylinder of the crankcase; roughening the-precision-turned inner face; applying a coating to the roughened inner face with a plurality of pores, an average pore size and a pore surface proportion being predeterminedly defined so as to vary over a length of the cylinder, said coating forming a running surface for a piston, wherein the roughened inner face of the cylinder has a surface roughness approximately in a range of Rz=30 μm to 200 μm. 2. The method according to claim 1 , wherein the light-metal material is an Al—Si alloy. 3. The method according to claim 1 , wherein the casting is a die casting of the crankcase. 4. The method according to claim 1 , wherein the act of roughening is carried out by at least one of a mechanical process and a chemical process. 5. The method according to claim 1 , wherein the act of roughening takes place by one of: machining; sandblasting or corundum-blasting; and high-pressure blasting via a fluid. 6. The method according to claim 1 , wherein the act of applying the coating is carried out by wire arc spraying of fusible droplets. 7. The method according to claim 6 , wherein the fusible droplets are sprayed via a carrier gas onto the roughened inner face of the cylinder, said carrier gas consisting essentially of air enriched with nitrogen. 8. The method according to claim 1 , wherein the applied coating is an iron-coating. 9. The method according to claim 8 , wherein the iron-based coating is an FeC coating. 10. The method according to claim 1 , wherein an oxide proportion of the coating varies, such that a hardness of the coating varies over the length of the cylinder approximately between 300 HV and 700 HV. 11. The method according to claim 1 , wherein the formed running surface is finished via a mechanical honing process. 12. The method according to claim 11 , wherein the finished honed running surface has a roughness value of at least one of: (a) Rpk is in a range of between 0.05 μm-2 μm; (b) Rvk is in a range=0.5 μm-15 μm; (c) V0 is in a range of between 0.1 μm-16 μm; and (d) Rk is in a range of between 0.05 μm-5 μm. 13. The method according to claim 1 , wherein the cylinder has an upper end near a cylinder head and a lower end near an oil pan, and further wherein the size of the pores and/or the pore surface proportion decreases from the lower end in a direction toward the upper end. 14. The method according to claim 1 , wherein the cylinder has an upper end near a cylinder head, a lower end near an oil pan, and a center area situated between the upper and lower ends, and further wherein the size of the pores and/or the pore surface proportion are largest in a center in the center area and decrease in directions toward both the upper and lower ends. 15. The method according to claim 1 , wherein the pore surface proportion increases from an upper cylinder end in a direction toward a lower cylinder end, and further wherein the average pore size is essentially constant over the length of the cylinder. 16. The method according to claim 1 , wherein the pore surface is smallest in a center area of the cylinder and increases in a direction toward upper and lower cylinder ends, and further wherein the average pore size is essentially constant over the length of the cylinder. 17. The method according to claim 1 , wherein some of the plurality of pores are oblong pores and some are round pores, the oblong pores being pores that have a length to width ratio of more than 4:1, the round pores being pores that have a length to width ratio of at most 4:1, and a ratio of the oblong pores to the round pores ranges between 0.1 and 2.5. 18. An internal-combustion engine, comprising: a crankcase having at least one cylinder operatively configured to accommodate a piston, wherein an inner face of the cylinder has a coating forming a running surface for the piston, the coating having a plurality of pores with an average size of the pores and a pore surface proportion being predeterminedly defined so as to vary over the length of the cylinder, wherein some of the plurality of pores are oblong pores and some are round pores, the oblong pores being pores that have a length to width ratio of more than 4:1, the round pores being pores that have a length to width ratio of at most 4:1, and a ratio of the oblong pores to the round pores ranges between 0.1 and 2.5. 19. The internal-combustion engine according to claim 18 , wherein the applied coating is an iron-based coating. 20. The internal-combustion engine according to claim 19 , wherein the iron-based coating is an FeC coating. 21. The internal-combustion engine according to claim 18 , wherein an oxide proportion of the coating varies, such that a hardness of the coating varies over the length of the cylinder approximately between 300 HV and 700 HV. 22. The internal-combustion engine according to claim 18 , wherein the formed running surface is a finished honed running surface. 23. The internal-combustion engine according to claim 22 , wherein the finished honed running surface has a roughness value of at least one of: (a) Rpk is in a range of between 0.05 μm-2 μm; (b) Rvk is in a range=0.5 μm-15 μm; (c) V0 is in a range of between 0.1 μm-16 μm; and (d) Rk is in a range of between 0.05 μm-5 μm. 24. The internal-combustion engine according to claim 18 , wherein the cylinder has an upper end near a cylinder head and a lower end near an oil pan, and further wherein the size of the pores and/or the pore surface proportion decreases from the lower end in a direction toward the upper end. 25. The internal-combustion engine according to claim 18 , wherein the cylinder has an upper end near a cylinder head, a lower end near an oil pan, and a center area situated between the upper and lower ends, and further wherein the size of the pores and/or the pore surface proportion are largest in a center in the center area and decrease in directions toward both the upper and lower ends. 26. The internal-combustion engine according to claim 18 , wherein the pore surface proportion increases from an upper cylinder end in a direction toward a lower cylinder end, and further wherein the average pore size is essentially constant over the length of the cylinder. 27. The internal-combustion engine according to claim 18 , wherein the pore surface is smallest in a center area of the cylinder and increases in a direction toward upper and lower cylinder ends, and further wherein the average pore size is essentially constant over the length of the cylinder.
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