Piston with advanced catalytic energy release

1. A piston, comprising:

an upper crown wall presenting an upper combustion surface,

a coating disposed on said upper combustion surface,

said coating including a thermal barrier layer disposed on said upper combustion surface,

said thermal barrier layer including a ceramic composition,

said coating including a sealant layer disposed on said thermal barrier layer,

said sealant layer including metal,

said coating including a catalytic layer disposed on said sealant layer, and

said catalytic layer including at least one of platinum, ruthenium, rhodium, palladium, osmium, and iridium.

2. The piston of claim 1 , wherein said catalytic layer includes platinum.

3. The piston of claim 1 , wherein said catalytic layer has a thickness of 10 to 1000 nm.

4. The piston of claim 1 , wherein said catalytic layer is disposed on regions of said upper combustion surface and on less than an entirety of said upper combustion surface.

5. The piston of claim 1 , wherein said ceramic composition of said thermal barrier layer includes partially stabilized zirconia.

6. The piston of claim 1 , wherein said sealant layer includes a nickel-based composition.

7. The piston of claim 1 , wherein said coating further includes a bond layer disposed between said upper combustion surface and said thermal barrier layer, and said bond layer includes metal.

8. The piston of claim 7 , wherein said bond layer includes a nickel-based composition.

9. The piston of claim 1 , wherein said coating has a total thickness of 500 microns or less.

10. The piston of claim 1 , wherein said coating further includes a bond layer disposed between said upper combustion surface and said thermal barrier layer, said bond layer includes metal, said bond layer has a thickness of 50 to 150 microns, said thermal barrier layer has a thickness of 150 to 350 microns, said sealant layer has a thickness of 50 to 100 microns, and said catalytic layer has a thickness of 10 to 1000 nm.

11. The piston of claim 1 , wherein said at least one of platinum, ruthenium, rhodium, palladium, osmium, and iridium is present in an amount of at least 10 weight percent, based on the total weight of the catalytic layer,

said coating further includes a bond layer disposed directly on said upper combustion surface,

said bond layer is disposed between said upper combustion surface and said thermal barrier layer,

said bond layer includes at least one of nickel chromium aluminum yttrium (NiCrAlY) and cobalt nickel chromium aluminum yttrium (CoNiCrAlY),

said bond layer is formed of powder,

said bond layer has a thickness of 50 to 150 microns,

said thermal barrier layer is disposed directly on said bond layer,

said ceramic composition of said thermal barrier layer includes ceria stabilized zirconia (CSZ),

said thermal barrier layer has a thickness of 150 to 350 microns,

said sealant layer is disposed directly on said thermal barrier layer,

said sealant layer is applied over an entire uppermost surface of said thermal barrier layer facing said sealant layer,

said sealant layer includes at least one of nickel chromium aluminum yttrium (NiCrAlY) and cobalt nickel chromium aluminum yttrium (CoNiCrAlY),

said sealant layer has a thickness of 50 to 100 microns,

said catalytic layer is disposed directly said sealant layer,

said catalytic layer has a thickness of 10 to 1000 nm, and

said coating has a total thickness of 500 microns or less.

12. The piston of claim 1 , wherein said piston includes a body formed of a single piece of steel,

said body includes said upper crown wall presenting said upper combustion surface,

said upper combustion surface is non-planar surface around a center axis,

said upper crown wall includes an undercrown surface facing opposite said upper combustion surface,

said undercrown surface is exposed from an underside of said piston,

said body includes a ring belt depending from said upper crown wall and extending circumferentially along an outer diameter of said piston,

said ring belt includes a plurality of lands separated from one another by ring grooves,

said body includes a pair of pin bosses depending from said undercrown surface inwardly of said ring belt,

said pin bosses define a pair of laterally spaced pin bores which are vertically spaced from said undercrown surface,

said body includes a pair of skirt panels depending from said ring belt and located diametrically opposite one another,

said skirt panels are connected to said pin bosses by struts,

said undercrown surface includes an inner undercrown region surrounded by said pin bosses and said skirt panels and said struts,

said undercrown surface includes a second region provided by outer pockets located outwardly of said pin bosses,

each one of said outer pockets is surrounded by one of said pin bosses, a portion of said ring belt, and said struts connecting said one pin boss to said skirt panels.

13. The piston of claim 1 , wherein said piston includes a body formed of steel,

said body extends circumferentially around a center axis and longitudinally along said center axis,

said body includes said upper wall presenting said upper combustion surface,

said upper combustion surface is non-planar surface around a center axis,

said upper crown wall includes an undercrown surface facing opposite said upper combustion surface,

said undercrown surface is exposed from an underside of said piston,

said body includes a ring belt depending from said upper crown wall and extending circumferentially along an outer diameter of said piston,

said ring belt includes a plurality of lands separated from one another by ring grooves,

said body includes a pair of pin bosses depending from said undercrown surface inwardly of said ring belt,

said pin bosses define a pair of laterally spaced pin bores which are vertically spaced from said undercrown surface,

said body includes a pair of skirt panels depending from said ring belt and located diametrically opposite one another,

said skirt panels are connected to said pin bosses by struts,

said body includes a top part joined to a bottom part presenting a cooling gallery therebetween,

said top part includes a top portion of said ring belt and an upper portion of an inner wall,

said bottom part includes a bottom portion of said ring belt and a lower portion of said inner wall and a lower wall,

said upper crown wall and said portions of said ring belt and said inner wall and said lower wall present said cooling gallery.

14. The piston of claim 1 , wherein said cooling gallery contains a cooling medium, and said cooling medium includes at least one solid powder and/or at least one liquid.

15. A method of manufacturing a piston, comprising the steps of:

disposing a coating on an upper combustion surface of an upper crown wall,

the coating including a thermal barrier layer disposed on the upper combustion surface,

the thermal barrier layer including a ceramic composition,

the coating including a sealant layer disposed on the thermal barrier layer,

the sealant layer including metal,

the coating including a catalytic layer disposed on the sealant layer, and

the catalytic layer including at least one of platinum, ruthenium, rhodium, palladium, osmium, and iridium.

16. The method of claim 15 , wherein the step of disposing the coating on the upper combustion surface includes applying the catalyst layer by electrodeposition or physical vapor deposition (PVD).

17. The method of claim 15 , wherein the step of disposing the coating on the upper combustion surface includes applying at least one of the thermal barrier layer and the sealant layer by thermal spraying.

18. The method of claim 17 , wherein the thermal spraying includes at least one of wire arc spraying, plasma spraying, and high velocity oxygen fuel (HVOF) spraying.

19. The method of claim 15 , wherein the step of disposing the coating on the upper combustion surface includes applying a bond layer between the upper combustion surface and the thermal barrier layer.

20. The method of claim 19 , wherein the step of applying the bond layer includes thermal spraying.