Thermally insulated steel piston crown and method of making using a ceramic coating

1. A piston, comprising:

a body portion formed of metal;

said body portion including a crown presenting a combustion surface;

a thermal barrier coating applied to said crown and extending from said combustion surface to an exposed surface;

said thermal barrier coating including a mixture of a metal bond material and a ceramic material;

the amount of ceramic material present in the mixture increasing toward said exposed surface, and

said thermal barrier coating has a thermal conductivity of less than 0.5 W/m·K.

2. The piston of claim 1 , wherein a porosity of said ceramic material is 2% by vol. to 25% vol., based on the total volume of said ceramic material.

3. The piston of claim 1 , wherein said thermal barrier coating has a thickness extending from said combustion surface to said exposed surface, and said thickness of said thermal barrier coating is less than 1 mm.

4. The piston of claim 1 , wherein said ceramic material of said thermal barrier coating includes at least one of ceria, ceria stabilized zirconia, yttria stabilized zirconia, calcia stabilized zirconia, magnesia stabilized zirconia, and zirconia stabilized by another oxide.

5. The piston of claim 1 , wherein said ceramic material consists of ceria stabilized zirconia.

6. The piston of claim 1 , wherein said thermal barrier coating includes a layer of said metal bond material applied directly to said combustion surface of said crown, said thermal barrier coating has a thickness extending from said combustion surface to said exposed surface, and 5% to 20% of said thickness of said thermal barrier coating consists of said layer of metal bond material;

said thermal barrier coating includes said mixture applied directly to said layer of metal bond material, the amount of said ceramic material present in said mixture increases continuously from said layer of said metal bond material toward said exposed surface; and

said thermal barrier coating includes a layer of said ceramic material applied directly to said mixture and extending to said exposed surface, and 5% to 50% of said thickness of said thermal barrier coating consists of said layer of said ceramic material.

7. The piston of claim 1 , wherein said metal bond material includes at least one alloy selected from the group consisting of CoNiCrAlY, NiCrAlY, NiCr, NiAl, NiCrAl, NiAlMo, and NiTi.

8. The piston of claim 1 , wherein said combustion surface of said crown to which said thermal barrier coating is applied is free of any features having a radius of less than 0.1 mm.

9. The piston of claim 1 , wherein said thermal barrier coating applied to said combustion surface has a bond strength of at least 2000 psi when tested according to ASTM C633.

10. The piston of claim 1 , wherein said thermal barrier coating is applied to a first portion of said combustion surface and not applied to a second portion of said combustion surface, and said thermal barrier coating has a thickness of not greater than 0.380 mm along said first portion.

11. The piston of claim 1 , wherein said body portion is formed of steel, said body portion includes no phosphate, and no phosphate is present on said combustion surface of said crown to which said thermal barrier coating is applied;

said crown extends circumferentially about a center axis from an upper end toward a lower end of said body portion;

said combustion surface of said crown includes a combustion bowl extending from an outer rim, and said combustion bowl includes an apex at said center axis;

said crown includes ring grooves located at an outer diameter surface and extending circumferentially about said center axis;

said crown includes ring lands spacing said ring grooves from one another and from said combustion surface;

said combustion surface of said crown to which said thermal barrier coating is applied is free of any features having a radius of less than 0.1 mm, or said crown includes a chamfer extending from said combustion surface to one of said ring lands located adjacent said combustion surface;

said body portion includes a pair of pin bosses spaced from one another about said center axis and depending from said crown to said lower end, each of said pin bosses defining a pin bore;

said body portion includes a pair of skirt sections spacing said pin bosses from one another about said center axis and depending from said crown to said lower end;

said thermal barrier coating is applied to at least one of said ring lands;

said ceramic material of said thermal barrier coating includes at least one of ceria, ceria stabilized zirconia, yttria stabilized zirconia, calcia stabilized zirconia, magnesia stabilized zirconia, and zirconia stabilized by another oxide;

said ceramic material has a porosity of 2% by vol. to 15% by vol., based on the total volume of said ceramic material;

said metal bond material includes at least one alloy selected from the group consisting of CoNiCrAlY, NiCrAlY, NiCr, NiAl, NiCrAl, NiAlMo, and NiTi;

said thermal barrier coating includes said metal bond material in an amount of 5% by vol. to 33% by vol. %, based on the total volume of said thermal barrier coating;

said thermal barrier coating includes a layer of said metal bond material applied directly to said combustion surface of said crown, said thermal barrier coating has a thickness extending from said combustion surface to an exposed surface, and 5% to 20% of said thickness of said thermal barrier coating consists of said layer of said metal bond material;

said thermal barrier coating includes said mixture applied directly to said layer of said metal bond material, 30% to 90% of said thickness of said thermal barrier coating consists of said mixture, the amount of said ceramic material present in said mixture increases continuously from said layer of said metal bond material toward said exposed surface;

said thermal barrier coating includes a layer of said ceramic material applied directly to said mixture and extending to said exposed surface, and 5% to 50% of said thickness of said thermal barrier coating consists of said layer of said ceramic material;

said thickness of said thermal barrier coating is not greater than 0.7 mm;

said thermal barrier coating has a specific heat of 480 J/kg·K to 610 J/kg·K at temperatures between 40 and 700° C.;

said thermal barrier coating applied to said combustion surface has a bond strength of at least 2000 psi when tested according to ASTM C633.

12. The piston of claim 1 , wherein the thermal barrier coating has a thickness of not greater than 0.38 mm.

13. The piston of claim 1 , wherein said exposed surface of said thermal barrier coating has a surface roughness Ra of less than 15 μm and a surface roughness Rz of not greater than ≤110 μm.

14. A piston, comprising:

a body portion formed of metal;

said body portion including a crown;

a thermal barrier coating applied to said crown;

said thermal barrier coating including a mixture of a metal bond material and a ceramic material;

said thermal barrier coating having a thermal conductivity of less than 0.5 W/m·K; and

an outer layer formed of metal applied to said thermal barrier coating.

15. The piston of claim 14 , wherein said outer layer includes nickel.

16. The piston of claim 14 , wherein said outer layer has a thickness of 1 to 50 microns.