Low compression natural gas engine piston bowl for improved combustion stability

1. A piston configured to reciprocate in the bore of an engine, the piston comprising:

an annular body including a crown portion defining a longitudinal axis, a radial direction perpendicular to the longitudinal axis, a plane containing the longitudinal axis and the radial direction, and a contoured combustion bowl;

wherein in the plane containing the longitudinal axis and the radial direction

the crown portion includes a top squish surface, and

a swirl pocket having a reentrant surface that extends axially downwardly and radially outwardly from the top squish surface defining a tangent that forms a reentrant angle with the top squish surface that ranges from 33.0 degrees to 37.0 degrees.

2. The piston of claim 1 , wherein the reentrant surface is conical.

3. The piston of claim 1 , wherein the swirl pocket further includes a concave arcuate surface extending from the reentrant surface, defining a concave arcuate surface radius of curvature that ranges from 4.0 millimeters to 6.0 millimeters in the plane containing the longitudinal axis and the radial direction.

4. The piston of claim 3 , wherein the concave arcuate surface is an exact radius.

5. The piston of claim 4 , wherein the swirl pocket further comprises a cylindrical surface extending axially downwardly from the concave arcuate surface, a concave bottom extremity defining surface extending from the cylindrical surface, a convex arcuate surface extending upwardly from the concave bottom extremity defining surface to a plateau surface that is perpendicular to the longitudinal axis.

6. The piston of claim 5 , wherein the plateau surface is formed by a convex arcuate surface, and the concave bottom extremity is formed by a concave radius.

7. The piston of claim 6 , wherein the cylindrical surface defines a maximum diameter of the swirl pocket, the concave radius defines a concave radius of curvature ranging from 6.6 mm to 8.6 mm, and the convex arcuate surface defines a convex radius of curvature ranging from 53.0 mm to 55.0 mm.

8. A piston configured to reciprocate in the bore of an engine, the piston comprising:

an annular body including a crown portion defining a longitudinal axis, a radial direction perpendicular to the longitudinal axis, a plane containing the longitudinal axis and the radial direction, and a contoured combustion bowl;

wherein in the plane containing the longitudinal axis and the radial direction, the contoured combustion bowl is radially surrounded by an annular cooling gallery that defines a maximum annular radial width, the contoured combustion bowl has a swirl pocket including a cylindrical surface defining a maximum diameter of the swirl pocket radially proximate to the maximum annular radial width of the annular cooling gallery, and a ratio of the maximum diameter of swirl pocket to the maximum annular radial width ranges from 15.86 to 19.19.

9. The piston of claim 8 , wherein the annular cooling gallery defines a radially inner cylindrical surface, and a radially outer cylindrical surface that defines the maximum annular radial width of the annular cooling gallery.

10. The piston of claim 8 , wherein the swirl pocket further includes a conical converging surface extending radially inwardly, and axially upwardly from the cylindrical surface of the swirl pocket.

11. The piston of claim 10 , wherein the swirl pocket further comprises a concave arcuate surface extending between the conical converging surface, and the cylindrical surface.

12. The piston of claim 11 , wherein the swirl pocket further comprise an undulating surface that extends axially downwardly and radially inwardly from the cylindrical surface of the swirl pocket to a bottom extremity of the swirl pocket, and then radially inwardly and axially upwardly to a peak disposed at the longitudinal axis.

13. A piston configured to reciprocate in the bore of an engine, the piston comprising:

an annular body including a crown portion defining a longitudinal axis, a radial direction perpendicular to the longitudinal axis, a plane containing the longitudinal axis and the radial direction, and a contoured combustion bowl;

wherein in the plane containing the longitudinal axis and the radial direction, the contoured combustion bowl defines a maximum axial depth measured from a planar squish surface to a bottom concave arcuate surface defining a bottom extremity of a swirl pocket, and a minimum axial depth measured from a plateau surface to the planar squish surface, and a ratio of the maximum axial depth of the contoured combustion bowl to the minimum axial depth ranges from 1.87 to 2.26.

14. The piston of claim 13 , wherein the contoured combustion bowl further comprises a cylindrical side surface that defines a maximum diameter of the swirl pocket that ranges from 103.3 millimeters to 107.3 millimeters.

15. The piston of claim 13 , wherein the planar squish surface defines an entry diameter that ranges from 98.0 millimeters to 102.0 millimeters.

16. The piston of claim 13 , further comprising a radius extending axially upwardly toward the planar squish surface that defines a radius of curvature ranging from 3.0 millimeters to 7.0 millimeters.

17. The piston of claim 13 , wherein the maximum axial depth of the contoured combustion bowl ranges from 30.7 millimeters to 34.7 millimeters.

18. A combustion chamber of an engine comprising:

a bore of the engine with a bore diameter, a longitudinal axis, a radial direction perpendicular to the longitudinal axis; and

a piston configured to reciprocate in the bore of the engine from a top dead center position to a bottom dead position defining a compression height therebetween, the piston including

an annular body including a crown portion and defining a plane containing the longitudinal axis and the radial direction, and a contoured combustion bowl;

wherein in the plane containing the longitudinal axis and the radial direction, the contoured combustion bowl defines a maximum axial depth measured from a planar squish surface to a bottom concave arcuate surface defining a bottom extremity of a swirl pocket, and a ratio of the compression height to the maximum axial depth ranges from 10.0 to 12.0.

19. The combustion chamber of claim 18 , wherein the contoured combustion bowl includes a reentrant surface extending from the planar squish surface at a reentrant angle in the plane containing the longitudinal axis and the radial direction, and a concave arcuate side surface that extends axially downwardly from the reentrant surface to a cylindrical side surface, that leads axially downwardly an undulating surface.

20. The combustion chamber of claim 19 , wherein the reentrant angle ranges from 30.0 degrees to 40.0 degrees.