Piston assembly with offset tight land profile

1. A piston assembly, comprising:

a cylinder bore;

the cylinder bore extending from a thrust side to an antithrust side; and

a piston positioned within the cylinder bore, wherein the piston is configured to move in an axial direction within the cylinder bore;

the piston comprising a top land and a second land;

the piston comprising a skirt with a central skirt axis therethrough;

the piston comprising a tight land profile of the top land and/or the second land with a central land axis therethrough, wherein the tight land profile has a minimum clearance of 0 to 35 microns between the cylinder bore and the top land and/or the second land during rated operating temperatures; and

the tight land profile comprising an offset of the central land axis away from the central skirt axis toward the antithrust side, wherein the central skirt axis and the central land axis extend in the axial direction.

2. The piston assembly of claim 1 , wherein the top land comprises the offset of the central land axis of the top land away from the central skirt axis of the skirt toward the antithrust side.

3. The piston assembly of claim 1 , wherein the second land comprises the offset of the central land axis of the second land away from the central skirt axis of the skirt toward the antithrust side.

4. The piston assembly of claim 1 , wherein at least one of the top land or the second land is defined as an ellipse with an ellipse axis as the central land axis.

5. The piston assembly of claim 4 , wherein the offset comprises an amplitude constant and wherein the amplitude constant comprises ≥0.03% of a diameter of the cylinder bore.

6. The piston assembly of claim 5 , wherein the ellipse comprises a circle.

7. The piston assembly of claim 1 , wherein both the top land and the second land have the tight land profile.

8. The piston assembly of claim 1 , wherein the cylinder bore comprises a liner.

9. The piston assembly of claim 1 , wherein the piston comprises a top ring groove between the top land and the second land.

10. The piston assembly of claim 9 , wherein the piston comprises a top ring in the top ring groove.

11. The piston assembly of claim 1 , wherein the piston comprises a third land, the piston comprises a second ring groove between the second land and the third land, and the piston comprises a second ring in the second ring groove.

12. A piston assembly for a power generation system, comprising:

a cylinder liner;

the cylinder liner extending from a thrust side to an antithrust side; and

a piston positioned within the cylinder liner, wherein the piston is configured to move in an axial direction within the cylinder liner;

the piston comprising a skirt, a top land, and a second land; and

the top land and/or the second land comprising a central land axis offset away from a central skirt axis of the skirt towards the antithrust side, wherein the central skirt axis and the central land axis extend in the axial direction.

13. The piston assembly of claim 12 , wherein at least one of the top land or the second land is defined as an ellipse having the central land axis as an ellipse axis.

14. A system, comprising:

a piston configured to mount in a cylinder bore of an engine, wherein the piston comprises:

a skirt disposed about a central skirt axis;

a land disposed about a central land axis;

a ring groove disposed adjacent the land, wherein the central land axis is offset away from the central skirt axis toward the antithrust side to position the land off center relative to the cylinder bore such that the land is positioned closer to the antithrust side and further from the thrust side, and the central skirt axis and the central land axis extend in an axial direction along an axial path of travel of the piston in the cylinder bore.

15. The system of claim 14 , wherein the land is defined as an ellipse having an ellipse axis as the land axis.

16. The system of claim 14 , wherein the land comprises a tight land profile relative to the cylinder bore of the engine, wherein the tight land profile has a minimum clearance of 0 to 35 microns between the cylinder bore and the land during rated operating temperatures of the engine.

17. The system of claim 14 , wherein the piston comprises a plurality of lands including the land, the plurality of lands define a plurality of ring grooves including the ring groove, and each land of the plurality of lands has the central land axis offset away from the central skirt axis toward the antithrust side to position the respective land off center relative to the cylinder bore such that the land is positioned closer to the antithrust side and further from the thrust side.

18. The system of claim 14 , comprising the engine having the piston.