Piston bowl geometry, cuff and top land interaction for reduced hydrocarbons, improved combustion efficiency, and piston temperature

Patent metadata

Field	Value
Publication number	US-11898488-B2
Application number	US-202117318543-A
Country	US
Kind code	B2
Filing date	May 12, 2021
Priority date	May 12, 2021
Publication date	Feb 13, 2024
Grant date	Feb 13, 2024

Abstract

A piston includes a swirl pocket that extends radially from the radially outer lip portion to a lower axial extremity spaced away from the radially outer lip portion a first axial distance. A convex arcuate surface extends downwardly and inwardly from the radially outer lip portion, a concave arcuate surface extends to the lower axial extremity from the convex arcuate surface, and a conical portion extends upwardly and inwardly from the concave arcuate surface to an apex that is spaced a second axial distance from the radially outer lip portion that is less than the first axial distance.

First claim

What is claimed is:

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 radially outer lip portion,
a swirl pocket that extends radially from the radially outer lip portion and defines a lower axial extremity that is spaced axially away from the radially outer lip portion a first axial distance, and the swirl pocket includes a convex arcuate surface extending axially downwardly and radially inwardly from the radially outer lip portion, a concave arcuate surface extending axially downwardly to the lower axial extremity, and radially inwardly from the convex arcuate surface, a conical portion that extends axially upwardly and radially inwardly from the concave arcuate surface to an apex, the apex being spaced a second axial distance from the radially outer lip portion, and a ratio of the second axial distance to the first axial distance ranges from 0.780 to 0.820; and
the radially outer lip portion defines a bowl rim diameter defined by a tangent to the concave arcuate surface in the plane intersecting with a planar squish surface of the radially outer lip portion, and the planar squish surface extending planarly and fully circumferentially around the longitudinal axis.

2. The piston of claim 1 , wherein the radially outer lip portion defines a bowl rim diameter, and a ratio of the first axial distance to the bowl rim diameter ranges from 0.180 to 0.210.

3. The piston of claim 2 , wherein the bowl rim diameter ranges from 235.0 mm to 250.0 mm, and the conical portion forms an angle with the radial direction ranging from 10.0 degrees to 15.0 degrees.

4. The piston of claim 1 , wherein the convex arcuate surface defines a convex radius of curvature in the plane containing the longitudinal axis and the radial direction, ranging from 20.0 mm to 30.0 mm.

5. The piston of claim 1 , wherein the concave arcuate surface defines a concave radius of curvature in the plane containing the longitudinal axis and the radial direction, ranging from 70.0 mm to 80.0 mm.

6. The piston of claim 1 , wherein the first axial distance ranges from 40.0 mm to 50.0 mm, and the second axial distance ranges from 35.0 millimeters to 40.0 millimeters.

7. 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 radially outer lip portion, and
a swirl pocket that extends radially from the radially outer lip portion and defines a lower axial extremity that is spaced axially away from the radially outer lip portion a first axial distance, and the swirl pocket includes a convex arcuate surface extending axially downwardly and radially inwardly from the radially outer lip portion, a concave arcuate surface extending axially downwardly to the lower axial extremity, and radially inwardly from the convex arcuate surface, a conical portion that extends axially upwardly and radially inwardly from the concave arcuate surface to an apex, the apex being spaced a second axial distance from the radially outer lip portion that is less than the first axial distance, and the radially outer lip portion defines a bowl rim diameter defined by a tangent to the concave arcuate surface in the plane intersecting with a planar squish surface of the radially outer lip portion, the planar squish surface extending planarly and fully circumferentially around the longitudinal axis, and a ratio of the first axial distance to the bowl rim diameter ranges from 0.185 to 0.197.

8. The piston of claim 7 , wherein a ratio of the second axial distance to the first axial distance ranges from 0.790 to 0.800.

9. The piston of claim 8 , wherein the first axial distance ranges from 40.0 mm to 50.0 mm, and the second axial distance ranges from 35.0 millimeters to 40.0 millimeters.

10. The piston of claim 7 , wherein the convex arcuate surface defines a convex radius of curvature in the plane containing the longitudinal axis and the radial direction, ranging from 20.0 mm to 30.0 mm.

11. The piston of claim 7 , wherein the apex is defined by a convex radius defining an apex radius of curvature ranging from 20.0 mm to 30.0 mm.

12. The piston of claim 7 wherein the concave arcuate surface defines a concave radius of curvature in the plane containing the longitudinal axis and the radial direction, ranging from 70.0 mm to 80.0 mm.

13. A combustion chamber of an engine comprising:
an annular cylinder liner defining 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, the piston including a crown portion 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 crown portion includes a radially outer lip portion, and a swirl pocket that extends radially from the radially outer lip portion and defines a lower axial extremity that is spaced axially away from the radially outer lip portion a first axial distance, and the swirl pocket includes a convex arcuate surface extending axially downwardly and radially inwardly from the radially outer lip portion, a concave arcuate surface extending axially downwardly to the lower axial extremity, and radially inwardly from the convex arcuate surface, a conical portion that extends axially upwardly and radially inwardly from the concave arcuate surface to an apex, the apex being spaced a second axial distance from the radially outer lip portion that is less than the first axial distance, and the radially outer lip portion defines a bowl rim diameter defined by a tangent to the concave arcuate surface that intersects a planar squish surface of the radially outer lip portion in the plane, the planar squish surface extending planarly around the longitudinal axis and a ratio of the bowl rim diameter to the bore diameter ranges from 0.805 to 0.815;
wherein the cylinder liner defines an axially upper and radially inner counterbore, and further comprising a cuff that is disposed in the axially upper and radially inner counterbore.

14. The combustion chamber of claim 13 , wherein the cuff defines an axially lower and radially outer chamfer.

15. The combustion chamber of claim 13 , wherein the swirl pocket lacks a reentrant surface.

16. The combustion chamber claim 13 , wherein the cylinder liner defines an upper axial extremity including a fire dam.

17. The combustion chamber of claim 16 , wherein the cylinder liner defines an axially upper and radially outer annular cavity, and further comprising a gasket that is disposed in the axially upper and radially outer annular cavity.

18. The combustion chamber of claim 17 , wherein the axially upper and radially outer annular cavity defines an axially extending surface, and a radially extending surface, and the gasket contacts both the axially extending surface, and the radially

Assignees

• Caterpillar Inc

Inventors

• Tooker Jonathan Kevin
• Batta Christopher L
• Fawcett Dylan S
• Fogle Shaun David

Classifications

• F02B23/0696 Primary

  W-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder wall · CPC title

• F02B23/0624

  Swirl flow · CPC title

• F02F3/26

  having combustion chamber in piston head (the surface thereof being covered F02F3/14) · CPC title

• F02F11/005

  involving cylinder liners · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title