Zero oil cooled (ZOC) piston incorporating heat pipe technology

1. A piston, comprising:

a body formed of a metal material extending along a center axis from an upper end to a lower end, said body presenting an outer surface and an inner surface,

said body including a crown having an upper wall at said upper end;

said body including skirt walls extending longitudinally from said crown to said lower end, said skirt walls and said upper wall of said crown defining a plurality of heat sink wells extending axially from said upper wall toward said lower end of said skirt wall, each of said heat sink wells being at least partially filled with a cooling medium and sealed by said skirt wall and said upper wall of said crown and a lower wall at said lower end of said skirt wall;

said body including a plurality of ribs each extending radially inwardly from a first rib end at said inner surface of said skirt wall to a second rib end at said inner surface of said upper wall; and

said body presenting a piston height extending from said upper end to said lower end, said outer surface along said skirt walls presenting a piston diameter extending through and perpendicular to said center axis, a piston length and said piston diameter defining a K factor equal to said piston height divided by said piston diameter, and said K factor being within a range of 1.1 to 1.6.

2. The piston of claim 1 , wherein said heat sink wells are spaced from one another circumferential by a portion of said skirt wall, each rib is radially aligned with one of said heat sink wells and extends radially inwardly from said inner surface adjacent said radially aligned heat sink well.

3. The piston of claim 2 , wherein each rib is spaced from the adjacent rib by a void.

4. The piston of claim 2 , wherein each heat sink well presents a well width extending perpendicular to said center axis, and each rib presents a rib width extending parallel to said center axis being 0.5 to 1.5 times said well width of said adjacent heat sink well.

5. The piston of claim 1 , wherein said cooling medium at least partially filling said heat sink wells of said skirt walls is selected from oil, liquid coolant, sodium (Na), an alloy of sodium and potassium (NaK), and a tube formed of copper (Cu).

6. The piston of claim 1 , wherein said outer surface of said crown facing away from said center axis includes a plurality of ring grooves extending circumferentially around said center axis for holding a plurality of piston rings.

7. The piston of claim 6 including a piston ring having an L-shaped cross-section disposed in one of said ring grooves, said piston ring having an uppermost surface aligned with said outer surface of said upper wall at said upper end and an outermost surface disposed parallel to said outer surface of said crown facing away from said center axis.

8. The piston of claim 6 , wherein at least one of said crown and said skirt walls presents at least one oil opening disposed along or adjacent at least one of said ring grooves, said at least one oil opening extending radially from said outer surface to said inner surface for conveying oil toward said inner surface.

9. The piston of claim 1 including a thermal barrier coating applied to said outer surface of said upper wall at said upper end, said thermal barrier coating having a thickness of 0.1 mm to 1.0 mm, and said thermal barrier coating including partially stabilized zirconia (PSZ).

10. The piston of claim 1 , wherein the metal material of the body is steel.

11. The piston of claim 1 , wherein said body includes a pair of pin bosses having pin bores, and wherein said heat sink wells in said skirt walls are spaced circumferentially from said pin bosses.

12. A piston, comprising:

a body formed of a metal material extending along a center axis from an upper end to a lower end, said body presenting an outer surface and an inner surface,

said body including a crown having an upper wall at said upper end;

said body including skirt walls extending longitudinally from said crown to said lower end, said skirt walls and said upper wall of said crown defining a plurality of heat sink wells extending axially from said upper wall toward said lower end of said skirt wall, each of said heat sink wells being at least partially filled with a cooling medium and sealed by said skirt wall and said upper wall of said crown and a lower wall at said lower end of said skirt wall;

said body including a plurality of ribs each extending radially inwardly from a first rib end at said inner surface of said skirt wall to a second rib end at said inner surface of said upper wall;

said outer surface of said crown facing away from said center axis includes a plurality of ring grooves extending circumferentially around said center axis for holding a plurality of piston rings;

at least one of said crown and said skirt walls presenting at least one oil opening disposed along or adjacent at least one of said ring grooves, said at least one oil opening extending radially from said outer surface to said inner surface for conveying oil toward said inner surface; and

said body includes a tray for collecting oil extending radially inwardly from a first tray end at said inner surface axially below said at least one oil opening to a second tray end, said second tray end being a distal end spaced radially from said center axis.

13. A piston, comprising:

a body formed of a steel material and extending circumferentially around a center axis and longitudinally along said center axis from an upper end to a lower end, said body defining a piston height extending from said upper end to said lower end;

said body presenting an outer surface and an oppositely facing inner surface, said outer surface presenting a piston diameter extending through and perpendicular to said center axis;

a piston length and said piston diameter defining a K factor, said K factor being equal to said piston height divided by said piston diameter, said K factor being within a range of 1.1 to 1.6;

said body including a crown at said upper end;

said crown including an upper wall at said upper end for facing a combustion chamber, said outer surface of said upper wall including an apex at said center axis and a bowl-shaped configuration surrounding said apex;

a thermal barrier coating applied to said outer surface of said upper wall, said thermal barrier coating having a thickness of 0.1 mm to 1.0 mm, and said thermal barrier coating including partially stabilized zirconia (PSZ);

said outer surface of said crown facing away from said center axis including a plurality of ring grooves extending circumferentially around said center axis for holding a plurality of piston rings;

said ring grooves including a top ring groove and a bottom ring groove, said top ring groove being disposed above said apex of said upper wall and said bottom ring groove being disposed below said apex of said upper wall;

said body including a pair of pin bosses extending longitudinally from said crown to said lower end, said pin bosses being spaced from one another and extending circumferentially about said center axis;

each of said pin bosses defining a pin bore for receiving a wrist pin, said pin bores each surrounding a bore axis extending perpendicular to said center axis of said body;

said body including a pair of skirt walls extending longitudinally from said crown to said lower end, said skirt walls being spaced from one another by said pin bosses and extending circumferentially about said center axis;

said skirt walls and said upper wall of said crown presenting a plurality of heat sink wells extending axially and continuously from said upper wall of said crown to said lower end of said skirt wall, each of said heat sink wells being at least partially filled with a cooling medium, said heat sink wells being sealed by said surrounding skirt wall and said upper wall of said crown and a lower wall at said lower end of said skirt wall, at least a portion of said heat sink wells being parallel to said center axis and spaced from one another circumferential about said center axis by a portion of said skirt wall formed of said steel material, each of said heat sink wells presenting a width extending perpendicular to said center axis, and each of said heat sink wells presenting a circumferential shape;

said body including a plurality of ribs each extending radially inwardly and upwardly at an angle from a first rib end at said inner surface of said skirt wall to a second rib end at said inner surface along a boss of said upper wall, each rib being radially aligned with one of said heat sink wells and extending radially inwardly from said inner surface of said skirt wall adjacent said radially aligned heat sink well, said ribs being spaced from one another circumferentially about said center axis, each of said ribs being spaced from the adjacent rib at said first rib end by said portion of said skirt wall spacing said heat sink well from the adjacent heat sink well, said second rib ends being disposed closer to one another than said first rib ends, each of said ribs being spaced from the adjacent rib between said first rib end and said second rib end by a void free of a solid or liquid material, each of said ribs presenting a width extending parallel to said center axis, said width being 0.5 to 1.5 times said width of said adjacent heat sink well; and

said cooling medium at least partially filling said heat sink wells of said skirt walls being selected from oil, liquid coolant, sodium (Na), an alloy of sodium and potassium (NaK), and a tube formed of copper (Cu).

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

providing a body formed of a metal material extending along a center axis from an upper end to a lower end, the body presenting an outer surface and an inner surface, the body including a crown having an upper wall at the upper end, the body including skirt walls extending longitudinally from the crown to the lower end, the skirt walls and the upper wall of the crown defining a plurality of heat sink wells extending axially from the upper wall toward the lower end of the skirt wall, each of the heat sink wells being hollow and sealed by the skirt wall and the upper wall of the crown and the lower wall at the lower end of the skirt wall; the body including a plurality of ribs each extending radially inwardly from a first rib end at the inner surface of the skirt wall to a second rib end at the inner surface of the upper wall; the body presenting a piston height extending from the upper end to the lower end, the outer surface along the skirt walls presenting a piston diameter extending through and perpendicular to the center axis, a piston length and the piston diameter defining a K factor equal to the piston height divided by the piston diameter, and the K factor being within a range of 1.1 to 1.6.

15. The method of claim 14 , wherein the step of providing the piston body includes casting or forging metal material to form the crown, the skirt walls, the heat sink wells, and the ribs.

16. The method of claim 15 , wherein the step of providing the piston body includes casting, and including the step of casting a plurality of copper tubes in the heat sink wells of the skirt walls.

17. The method of claim 14 , wherein the step of providing the piston body includes casting or forging metal material to form the crown and the skirt walls, and drilling the heat sink wells into the skirt walls.

18. The method of claim 14 , wherein the step of providing the piston body includes welding an upper portion of the piston body including the crown to a lower portion of the piston body including the skirt portions.

19. The method of claim 14 , including spraying a thermal barrier coating onto the outer surface of the upper wall to a thickness of 0.1 mm to 1.0 mm, wherein the thermal barrier coating includes partially stabilized zirconia (PSZ).

20. The method of claim 14 , wherein the heat sink wells are spaced from one another circumferential by a portion of the skirt wall, each rib is radially aligned with one of the heat sink wells and extends radially inwardly from the inner surface adjacent the radially aligned heat sink well, each rib presents an enlarged portion of the heat sink well along the inner surface of the upper wall and is spaced from the adjacent rib by a void, each heat sink well presents a well width extending perpendicular to the center axis, and each rib presents a rib width extending parallel to the center axis being 0.5 to 1.5 times the well width of the adjacent heat sink well.