Piston providing for reduced heat loss using cooling media

1. A piston for an internal combustion engine, comprising:

a body formed of a metal material;

said body including a crown presenting a combustion surface;

said crown including an outer side wall depending from said combustion surface, said outer side wall presenting an outer diameter of said body;

said crown including an outer cooling gallery and an undercrown cooling gallery;

said outer cooling gallery extending circumferentially along said outer side wall beneath said combustion surface, said outer cooling gallery being sealed and containing a first cooling media;

said undercrown cooling gallery being surrounded by said outer cooling gallery beneath a first undercrown surface, said undercrown cooling gallery containing a second cooling media; and

said crown including a lower wall extending along said undercrown cooling gallery, said lower wall including an inlet hole to said undercrown cooling gallery, and said inlet hole to said undercrown cooling gallery being tapered.

2. The piston of claim 1 , wherein said inlet hole to said undercrown cooling gallery has a diameter being from 1% to 25% of said outer diameter of said body.

3. The piston of claim 1 , wherein said inlet hole to said undercrown cooling gallery has a diameter being from 2% to 4% of said outer diameter of said body.

4. The piston of claim 1 , wherein said inlet hole to said undercrown cooling gallery is open.

5. The piston of claim 4 , wherein a diameter of said inlet hole increases or decreases in a direction moving away from said combustion surface.

6. The piston of claim 1 , wherein said inlet hole to said undercrown cooling gallery is sealed.

7. The piston of claim 1 , wherein each of said first cooling media and said second cooling media are selected from the group consisting of a solid, a liquid, a gas, air, and a partial vacuum.

8. The piston of claim 7 , wherein said outer cooling gallery is sealed, said first cooling media is at least one of a solid, a liquid, a gas, and air; and said inlet hole to said undercrown cooling gallery is open, and said second cooling media is air.

9. The piston of claim 7 , wherein said outer cooling gallery is sealed, said first cooling media consists of a solid, a liquid, a gas, air, and a partial vacuum; said inlet hole to said undercrown cooling gallery is open, said second cooling media consists of air, and the air fills 100% of a volume of said undercrown cooling gallery.

10. The piston of claim 1 further including a thermal barrier coating applied to at least one of said combustion surface, said first undercrown surface, and a second undercrown surface located beneath said undercrown cooling gallery; and said thermal barrier coating has a thermal conductivity being lower than a thermal conductivity of said metal material of said body.

11. The piston of claim 10 , wherein said thermal barrier coating is formed of an insulating material.

12. The piston of claim 1 , wherein said body is formed of steel and extends circumferentially around a center axis and longitudinally from an upper end to a lower end;

said crown includes an upper wall presenting said combustion surface and an inner side wall;

said upper wall, said lower wall, said outer side wall, and said inner side wall together define said outer cooling gallery;

said outer cooling gallery is spaced radially from said center axis;

said outer side wall and said inner side wall are formed by ribs joined together;

at least one of said outer side wall, said inner side wall, and said lower wall includes an opening for allowing cooling media to enter said outer cooling gallery, and said opening is sealed;

said lower wall presents a second undercrown surface beneath said undercrown cooling gallery;

said combustion surface presents an apex at said center axis, a bowl-shape surrounding said apex, and a bowl rim surrounding said bowl-shape;

said outer side wall includes a plurality of ring groves facing away from said center axis and extending circumferentially around said center axis, said ring grooves being spaced from one another by lands, and said lands presenting said outer diameter of said body;

said body includes a pair of pin bosses each depending from said crown, each of said pin bosses presenting a pin bore extending perpendicular to said center axis;

said body includes a pair of skirt sections depending from said crown and spaced from one another by said pin bosses;

said first cooling media fills 100% of a volume of said outer cooling gallery, and said first cooling media consists of air;

said upper wall, said lower wall, and said inner side wall together define said undercrown cooling gallery;

said undercrown cooling gallery is disposed at said center axis and extends radially outwardly to said outer cooling gallery;

said second cooling media fills 100% of a volume of said undercrown cooling gallery, and said second cooling media consists of air;

said inlet hole to said undercrown cooling gallery has a diameter being from 2% to 4% of a largest outer diameter of said body along said skirt sections;

and further including:

a thermal barrier coating applied to at least one of said combustion surface, said first undercrown surface, and said second undercrown surface; and

wherein said thermal barrier coating is formed of an insulating material, said insulating material including a partially stabilized zirconia.

13. A method of manufacturing a piston for an internal combustion engine, comprising the steps:

providing a body formed of a metal material, the body including a crown presenting a combustion surface, the crown including an outer side wall depending from the combustion surface, the outer side wall presenting an outer diameter of the body, the crown including an outer cooling gallery being sealed and an undercrown cooling gallery, the outer cooling gallery extending circumferentially along the outer side wall beneath the combustion surface, the undercrown cooling gallery being surrounded by the outer cooling gallery beneath a first undercrown surface, the crown including a lower wall extending along the undercrown cooling gallery, the lower wall including an inlet hole to the undercrown cooling gallery being tapered; and

providing a first cooling media in the outer cooling gallery and a second cooling media in the undercrown cooling gallery.

14. The method of claim 13 , wherein the first cooling media consists of air, the step of providing the first cooling media in the outer cooling gallery includes filling the outer cooling gallery with the air, and further including sealing the outer cooling gallery.

15. The method of claim 13 , wherein the step of providing the first cooling media in the outer cooling gallery includes filling the outer cooling gallery with at least one of argon, helium, xenon, and carbon dioxide.

16. The method of claim 13 , wherein the first cooling media includes a multiphase mixture of liquid and gas, and the step of providing the first cooling media in the outer cooling gallery includes disposing a liquid in the outer cooling gallery, and further including sealing the outer cooling gallery.

17. The method of claim 13 , wherein the second cooling media consists of air, and the step of providing the second cooling media in the undercrown cooling gallery includes filling the undercrown cooling gallery with the air.

18. The method of claim 13 , wherein the inlet hole to the undercrown cooling gallery is open, and the inlet hole has a diameter being from 2% to 4% of the outer diameter of the body.

19. The method of claim 13 including applying a thermal barrier coating to at least one of the combustion surface, the first undercrown surface, and a second undercrown surface located beneath the undercrown cooling gallery; and the thermal barrier coating has a thermal conductivity being lower than a thermal conductivity of the metal material of the body.

20. The method of claim 13 including sealing the inlet hole to the undercrown cooling gallery.

21. The method of claim 20 , wherein the sealing step includes at least one of the following steps: disposing a plug in the inlet hole, disposing an adhesive in the inlet hole, welding a material to the inlet hole, and brazing the inlet hole.

22. The method of claim 13 , wherein the step of providing the body includes forming the outer cooling gallery and the inner cooling gallery by joining an upper rib extending circumferentially around a center axis to a lower rib extending circumferentially around the center axis.