Internal-combustion engine piston ring, process for obtaining a piston ring, and internal-combustion engine
US-2017306469-A1 · Oct 26, 2017 · US
US10370755B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10370755-B2 |
| Application number | US-201414896179-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 10, 2014 |
| Priority date | Jun 4, 2013 |
| Publication date | Aug 6, 2019 |
| Grant date | Aug 6, 2019 |
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A piston ring is produced in which a piston ring base body made of cast iron or cast steel is coated with at least one PVD layer having a variable layer thickness, such that an increased layer thickness is present in the region of the ring ends compared to the remaining circumferential region of the piston ring base body, wherein the piston ring base body is configured so that, in the cold operating state with the engine not running, the radial pressure distribution of the piston ring base body is such that the ring ends exhibit substantially no radial pressure across a defined circumferential angle, and the variable layer thickness of the PVD layer is set so that a substantially uniform radial pressure distribution is present along the entire ring circumference of the piston ring at a piston ring temperature above 150° C.
Opening claim text (preview).
The invention claimed is: 1. A method for producing a piston ring, comprising providing a piston ring base body made of cast iron or cast steel and having ends separated by a gap comprising a joint, coating an outer circumferential surface of the piston ring base body with at least one PVD layer of varying thickness which is greater in a region of each of the ring ends of predetermined circumferential angle than in a remaining circumferential region of the circumferential surface thereby to produce the piston ring having a running face formed of the at least one PVD layer, wherein the piston ring base body is configured so that, installed in a cold engine which is not running, a radial pressure distribution of the piston ring is such that the ring ends over said predetermined circumferential angle exhibit substantially no radial pressure and the varying of the thickness of the at least one PVD layer is predetermined so that radial pressure over the entire piston ring circumference at a piston ring temperature above 150° C. is substantially uniform. 2. The method according to claim 1 , wherein the thickness of the at least one PVD layer in the region of the ring ends is <100 μm and the thickness of the at least one PVD layer in the remaining circumferential region of the piston ring base body is <60 μm provided that in all instances the thickness of the at least one PVD layer is substantially greater in the piston ring ends region than in the remaining circumferential region of the piston ring. 3. The method according to claim 1 , wherein the at least one PVD layer is a PVD multi-layer system. 4. The method according to claim 1 , wherein the at least one PVD layer is a homogeneous layer comprising CrN, CrN(O) or CrN having an oxygen content of up to 15% by weight. 5. The method according to claim 1 , wherein the at least one PVD layer is carbon-based layer. 6. The method according to claim 1 , wherein the at least one PVD layer has a coefficient of expansion <4×10 −6 /K in a temperature range from 100 to 200° C. and is applied to a piston ring base having a coefficient of expansion <15×10 −6 /K in the temperature range from 100 to 200° C. 7. The method according to claim 1 , wherein the thickness of the at least one PVD layer in the ring ends region is 20 to 40% greater than in the remaining circumferential region of the piston ring. 8. The method according to claim 1 , wherein the thickness of the at least one PVD layer in the piston ring ends region is <60 μm and in the remaining circumferential region of the piston ring is <40 μm. 9. The method according to claim 1 , wherein the multi-layer system comprises a layer of AlTiN and a layer of CrN. 10. A piston ring produced according to the method of claim 1 . 11. The piston ring according to claim 10 , wherein the thickness of the at least one PVD layer in the region of the ring ends is from 20 to 40% greater than in the remaining circumferential region. 12. The piston ring according to claim 11 , wherein the thickness of the at least one PVD layer in the region of the ring ends is from 40 to 100 μm and from 5 to 60 μm in the remaining circumferential region. 13. The piston ring according to claim 12 , wherein the region of each of the ring ends in which the thickness of the at least one PVD layer is greater in a circumferential region of the ring beginning at the ring ends and extending away from the ring end from 10 to 40°. 14. The piston ring according to claim 13 , wherein the piston ring base body is made of a steel having a coefficient of thermal expansion <15×10 −6 /K in a temperature range of 100 to 200° C. 15. The piston ring according to claim 10 , wherein the at least one PVD layer is as a multi-layer system comprised of a layer of AlTiN and a layer of CrN or a homogeneous layer of CrN, CrN(O) or CrN having an oxygen content of up to 15% by weight, wherein the at least one PVD layer has a coefficient of thermal expansion <4×10 −6 /K in a temperature range of 100 to 200° C., the thickness of the at least one PVD layer in the region of the joint ends is in a range of 40 to <100 μm and in a range of 5 to <40 μm in the remaining circumferential region. 16. The piston ring according to claim 14 , wherein the at least one PVD layer is carbon-based and has a coefficient of thermal expansion <2×10 −6 /K in a temperature range of 100 to 200° C., the thickness of the at least one PVD layer is a maximum of 30 μm in the region of the ring ends and is in a range of >1 and 20 μm in the remaining circumferential region of the piston ring. 17. The piston ring according to claim 10 , wherein the at least one PVD layer comprises nanoparticles. 18. The piston ring according to claim 13 , wherein the region of each of the ring ends in which the thickness of the at least one PVD layer is greater extends away from the ring end 10 to 20°.
Nitrides (C23C14/0617 takes precedence) · CPC title
AIII BV compounds, where A is Al, Ga, In or Tl and B is N, P, As, Sb or Bi · CPC title
characterised by the use of particular materials · CPC title
of non-metals · CPC title
characterised by the coating material ({C23C14/0021} , C23C14/04 take precedence) · CPC title
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