Combustion cylinder end face components including thermal barrier coatings
An apparatus for a combustion cylinder of a reciprocating piston engine includes a combustion cylinder end face component including a first side configured to face the combustion cylinder and extending in a radial direction of the combustion cylinder and a pocket recessed into the first side and including a recessed pocket surface. The combustion cylinder end face component may be one of a piston and a cylinder head. A thermal barrier coating is inlaid in the pocket. The thermal barrier coating includes a ceramic-metallic layer directly coating the recessed pocket surface and a ceramic layer directly coating the ceramic-metallic layer and including an outer surface facing the combustion cylinder.
1. An apparatus for a combustion cylinder of a reciprocating piston engine, the apparatus comprising:
a combustion cylinder end face component including a first side configured to face the combustion cylinder and extending in a radial direction of the combustion cylinder and a pocket recessed into the first side and including a recessed pocket surface, the combustion cylinder end face component being one of a piston and a cylinder head; and
a thermal barrier coating inlaid in the pocket, the thermal barrier coating comprising a ceramic-metallic layer directly coating the recessed pocket surface and a ceramic layer directly coating the ceramic-metallic layer and including an outer surface facing the combustion cylinder, the thermal barrier coating filling the pocket to define a planar surface including at least a portion of the first side and the thermal barrier coating.
2. The apparatus of claim 1 , wherein the combustion cylinder end face component is the cylinder head.
3. The apparatus of claim 2 , wherein the outer surface of the ceramic layer has a roughness equal to or less than a roughness of a surface of the first side of the cylinder head.
4. The apparatus of claim 2 , wherein a diameter of the pocket in the radial direction is equal to a diameter of the combustion cylinder.
5. The apparatus of claim 2 , wherein the ceramic-metallic layer has an average thickens of 125 μm+/−20%.
6. The apparatus of claim 2 , wherein the ceramic layer has an average thickens of 350 μm+/−20%.
7. The apparatus of claim 2 , comprising a valve including an outer valve face configured to face the combustion cylinder and being covered with the thermal barrier coating.
8. The apparatus of claim 2 , wherein the thermal barrier coating is the only thermal barrier coating of the cylinder head.
9. The apparatus of claim 2 , wherein the outer surface of the thermal barrier coating is co-planar with a plane bounding the first side of the cylinder head.
10. The apparatus of claim 1 , wherein the thermal barrier coating consists essentially of the ceramic-metallic layer and the ceramic layer.
11. The apparatus of claim 1 , wherein the combustion cylinder end face component is the piston.
12. The apparatus of claim 11 , wherein the first side of the piston includes a centrally positioned piston bowl and a crown positioned radially outward from the centrally positioned piston bowl, and the pocket is recessed into the crown.
13. The apparatus of claim 12 , wherein the pocket is defined intermediate a radially outer annular portion of the crown and a radially inner annular portion of the crown.
14. A reciprocating piston engine comprising:
a cylinder head located at a first end of a combustion cylinder, the cylinder head including:
a first side oriented toward the combustion cylinder,
a first pocket recessed into the first side, and
a first thermal barrier coating inlaid in the first pocket and including a first outer surface facing the combustion cylinder; and
a piston located at a second end of the combustion cylinder, the piston including:
a second side oriented toward the combustion cylinder and including a centrally positioned piston bowl and a crown positioned radially outward from the centrally positioned piston bowl,
a second pocket recessed into the crown of the second side, and
a second thermal barrier coating inlaid in the second pocket and including a second outer surface facing the combustion cylinder,
wherein at least one of: (a) the first thermal barrier coating fills the first pocket to provide a first planar surface including at least a portion of the first side and the first thermal barrier coating, and (b) the second thermal barrier coating fills the second pocket to provide a second planar surface including at least a portion of the second side and the second thermal barrier coating.
15. The reciprocating piston engine of claim 14 , wherein the first thermal barrier coating comprises a first ceramic-metallic layer directly coating a recessed surface of the first pocket and a first ceramic layer directly coating the first ceramic-metallic layer and including the first outer surface.
16. The reciprocating piston engine of claim 14 , wherein the second thermal barrier coating comprises a second ceramic-metallic layer directly coating a recessed surface of the second pocket and a second ceramic layer directly coating the second ceramic-metallic layer and including the second outer surface.
17. The reciprocating piston engine of claim 14 , wherein the second pocket is positioned intermediate a radially outer annular base metal portion of the crown and a radially inner annular base metal portion of the crown.
18. The reciprocating piston engine of claim 14 , comprising: a valve located at a port defined in the cylinder head, the valve including a third side facing the combustion cylinder and a third thermal barrier coating directly coating the third side and including a third outer surface oriented to face the combustion cylinder.
19. The reciprocating piston engine of claim 18 , wherein the third thermal barrier coating comprises a third ceramic-metallic layer directly coating the third side and a third ceramic layer directly coating the third ceramic-metallic layer and including a third outer surface facing the combustion cylinder.
20. The reciprocating piston engine of claim 18 , wherein the first thermal barrier, the second thermal barrier, and the third thermal barrier are the only thermal barrier portions of the cylinder head, the piston and the valve.