BORON DOPED TA-C COATING FOR ENGINE COMPONENTS
An engine component, for example a piston ring, including a wear resistant coating applied by physical vapor deposition (PVD) is provided. The coating includes tetrahedral amorphous carbon (ta-C), the carbon of the coating includes sp 3 hybrid orbitals, and the coating includes boron in an amount of 0.1 wt. % to 4.0 wt. %, based on the total weight of the coating. The doped boron makes the coating less sensitive to the ion energy during the physical vapor deposition (PVD) process, improves adhesion of the coating, and expected to reduce compressive stress in the coating. Thus, the boron-doped ta-C coating can be applied to a greater thickness compared to ta-C coatings without the doped boron. In addition, there is a strong indication that the addition of boron will maintain a high level of sp 3 bonded carbon and a high microhardness.
1 . A component for an engine, comprising:
a base body presenting an outer surface,
a coating applied to said outer surface of said base body,
said coating including tetrahedral amorphous carbon (ta-C), the carbon of said coating including sp a hybrid orbitals,
said coating including boron in an amount of 0.1 wt. % to 4.0 wt. %, based on the total weight of said coating.
2 . The component of claim 1 , wherein said component is a piston ring, piston pin, crank shaft, or tappet.
3 . The component of claim 2 , wherein said base body of said piston ring presents an inner surface surrounding a center axis, said base body presents said outer surface facing opposite said center axis, said base body is formed of a metal material, and said metal material is cast iron, steel, or cast steel.
4 . The component of claim 1 , wherein the carbon of said coating is diamond-like carbon (DLC).
5 . The component of claim 1 , wherein said coating is homogenous.
6 . The component of claim 1 , wherein the coating includes a ratio of sp 2 hybrid orbitals to sp a hybrid orbitals ranging from 1:99 to 99:1.
7 . The component of claim 1 , wherein greater than 50% of the carbon present in said coating includes the sp 3 hybrid orbitals.
8 . The component of claim 1 , wherein the carbon of the coating comprises carbon atoms including sp 3 hybrid orbitals bonded to other carbon atoms including sp 3 hybrid orbitals.
9 . The component of claim 1 , wherein said coating is free of hydrogen,
10 . The component of claim 1 , wherein said coating has a thickness of 1 to 60 microns and a friction coefficient of 0.01 to 0.30.
11 . The component of claim 1 , wherein an adhesive layer is disposed between said outer surface and said coating, and a finish layer is applied to said coating.
12 . The component of claim 1 , wherein said component is a piston ring,
said base body of said piston ring presents an inner surface surrounding a center axis,
said base body presents said outer surface facing opposite said center axis,
said base body is formed of a metal material, said metal material is cast iron, steel, or cast steel,
the carbon of said coating is diamond-like carbon (DLC),
said coating is homogenous,
said coating includes a ratio of sp 2 hybrid orbitals to sp 3 hybrid orbitals ranging from 1:99 to 99:1;
the carbon of said coating comprises carbon atoms comprising sp 3 hybrid orbitals bonded to other carbon atoms including sp 3 hybrid orbitals,
said coating is free of hydrogen,
said coating has a thickness of 1 to 60 microns, and
said coating has a friction coefficient of 0.01 to 0.30.
13 . A method of manufacturing a component for an engine, comprising:
applying a coating to an outer surface of a base body, the coating including tetrahedral amorphous carbon (ta-C), the carbon of the coating including sp 3 hybrid orbitals, and the coating including boron in an amount of 0.1 wt. % to 4.0 wt. %, based on the total weight of the coating.
14 . The method of claim 13 , wherein the step of applying the coating to the outer surface includes physical vapor deposition.
15 . The method of claim 14 , wherein the physical vapor deposition step includes at least one of plasma-assisted high vacuum process, laser arc vapor deposition, magnetically enhanced arc vapor deposition, filtered arc vapor deposition, and magnetron sputtering.
16 . The method of claim 13 including forming a cathode by mixing particles of carbon or graphite and particles of the boron in an amount of 0.1 wt. % to 4.0 wt. %, based on the total weight of the mixture, and
wherein the step of applying the coating to the outer surface includes applying a gas including positive ions to the cathode so that the mixture of the cathode deposits on the outer surface and forms the coating.
17 . The method of claim 13 including forming a cathode of graphite, and wherein the step of applying the coating to the outer surface includes applying a gas including positive ions and boron to the cathode so that the tetrahedral amorphous carbon (ta-C) and the boron deposits on the outer surface and forms the coating.
18 . The method of claim 13 , wherein the component is a piston ring, piston pin, crank shaft, or tappet.
19 . The component of claim 13 , wherein the carbon of the coating comprises carbon atoms including sp 3 hybrid orbitals bonded to other carbon atoms including sp 3 hybrid orbitals.
20 . The method of claim 13 , wherein said component is a piston ring,
the base body of the piston ring presents an inner surface surrounding a center axis,
the base body presents the outer surface facing opposite the center axis,
the base body is formed of a metal material, the metal material is cast iron, steel, or cast steel,
the carbon of the coating is diamond-like carbon (DLC),
the coating is homogenous,
the coating includes a ratio of sp 2 hybrid orbitals to sp 3 hybrid orbitals ranging from 1:99 to 99:1;
the carbon of the coating comprises carbon atoms comprising sp 3 hybrid orbitals bonded to other carbon atoms including sp 3 hybrid orbitals,
the coating is free of hydrogen,
the coating has a thickness of 1 to 60 microns, and
the coating has a friction coefficient of 0.01 to 0.30.