Piston geometry for reduced smoke and cylinder head component temperatures

Patent metadata

Field	Value
Publication number	US-11230992-B2
Application number	US-202016839423-A
Country	US
Kind code	B2
Filing date	Apr 3, 2020
Priority date	Apr 3, 2020
Publication date	Jan 25, 2022
Grant date	Jan 25, 2022

Abstract

The piston has a contoured combustion bowl with a radially inner shelf portion that is spaced axially away from the radially outer lip portion a first axial distance, and a swirl pocket that extends radially from the radially inner shelf portion and defines a lower axial extremity that is spaced axially away from the radially outer lip portion a second axial distance that is greater than the first axial distance. The swirl pocket defines a tangent extending in the radially outer direction, forming an acute angle with the radially outer lip portion ranging from 70 degrees to 80 degrees.

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, and
the contoured combustion bowl includes a radially inner shelf portion that is spaced axially away from the radially outer lip portion a first axial distance, and
a swirl pocket that extends radially from the radially inner shelf portion and defines a lower axial extremity that is spaced axially away from the radially outer lip portion a second axial distance that is greater than the first axial distance, the swirl pocket defining an edge extending in the radially outer direction and that forms an acute angle with the radially outer lip portion ranging from 70 degrees to 80 degrees, and the swirl pocket includes a first conical surface extending radially and axially from the planar shelf surface, forming the edge that defines the acute angle with the planar squish surface projected onto the plane containing the longitudinal axis and the radial direction.

2. The piston of claim 1 wherein the crown portion is defined solely by revolving the radially outer lip portion and the contoured combustion bowl in the plane containing the longitudinal axis and the radial direction about the longitudinal axis an amount of 360 degrees.

3. The piston of claim 1 wherein the radially outer lip portion includes a planar squish surface, the radially inner shelf portion includes a planar shelf surface that is spaced axially away from the planar squish surface the first axial distance, the swirl pocket includes a bottom concave arcuate surface defining the lower axial extremity that is spaced axially away from the planar squish surface the second axial distance, and a ratio of the first axial distance to the second axial distance ranges from 10% to 15%.

4. The piston of claim 3 wherein the swirl pocket includes a second conical surface extending from the bottom concave surface toward the longitudinal axis, forming an outside obtuse angle with the longitudinal axis ranging from 110 degrees to 130 degrees projected onto the plane containing the longitudinal axis and the radial direction.

5. The piston of claim 3 wherein the first axial distance ranges from 1.5 millimeters to 3.5 millimeters.

6. The piston of claim 3 wherein the bottom concave arcuate surface defines a radius of curvature ranging from 15.0 mm to 25.0 mm in the plane containing the longitudinal axis and the radial direction.

7. The piston of claim 3 wherein the contoured combustion bowl further includes a radially outer blend extending tangentially from the planar shelf surface axially upwardly toward the planar squish surface.

8. The piston of claim 7 wherein the radially outer blend defines an outer blend radius of curvature ranging from 5.0 mm to 10.0 mm in the plane containing the longitudinal axis and the radial direction.

9. The piston of claim 1 wherein the radially outer blend connects to the top squish surface at a cusp, and the contoured combustion bowl defines a combustion bowl radius ranging from 65.0 mm to 80.0 mm that is measured from the cusp to the longitudinal axis.

10. 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 including a top squish surface, and
the contoured combustion bowl includes a radially inner planar shelf surface that is spaced axially away from the top squish surface a first axial distance, and that is connected to the top squish surface by a concave blend that is tangent to the radially inner planar shelf surface and extends axially upwardly to the top squish surface, and
a swirl pocket that includes a bottom concave arcuate surface extending axially downwardly and radially inwardly from the radially inner planar shelf surface and defining a lower axial extremity that is spaced axially away from the top squish surface a second axial distance, and a ratio of the first axial distance to the second axial distance ranges from 10% to 15%;
wherein the swirl pocket includes a first conical surface that is interposed radially and axially between the radially inner planar shelf surface and the bottom concave arcuate surface.

11. The piston of claim 10 wherein the defines a tangent that forms an acute angle with the top squish surface projected onto the plane containing the longitudinal axis and the radial direction ranging from 70 degrees to 80 degrees.

12. The piston of claim 11 wherein the swirl pocket includes a second conical surface extending tangentially from the bottom concave arcuate surface toward the longitudinal axis, forming an outside obtuse angle with the longitudinal axis ranging from 110 degrees to 130 degrees when projected onto the plane containing the longitudinal axis and the radial direction.

13. The piston of claim 12 further including a peak extending from the second conical surface and that is centered at the longitudinal axis, the peak being spaced axially away from the top squish surface an axial offset distance projected onto the plane containing the longitudinal axis and the radial direction ranging from 3.5 mm to 6.0 mm.

14. The piston of claim 13 wherein the peak is formed by a convex arcuate surface or a circular planar surface.

15. 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 including a top squish surface defining a first radial dimension, and
the contoured combustion bowl includes a radially inner planar shelf surface that is spaced axially away from the top squish surface a first axial distance, and that is connected to the top squish surface by an undulating transitional surface that is tangent to the radially inner planar shelf surface and extends radially outwardly and axially downwardly to a trough point and then axially upwardly and radially outwardly to the top squish surface, and
a swirl pocket that includes a bottom concave arcuate surface extending axially downwardly and radially inwardly from the radially inner planar shelf surface and defining a lower axial extremity that is spaced axially away from the top squish surface a second axial distance, and a ratio of the first axial distance to the second axial distance ranges from 10% to 15%.

16. The piston of claim 15 wherein the trough point is spaced axially away from the top squish surface a third axial distance that is greater than the first axial distance but is less than the second axial distance.

17. The piston of claim 16 wherein the swirl pocket includes a first conical surface that is interposed radially and axially between the ra

Assignees

• Caterpillar Inc

Inventors

• Schroeder Eric L
• Gehrke Christopher R
• Pierpont David A

Classifications

• F02F3/28

  Other pistons with specially-shaped head · CPC title

• F02F3/26 Primary

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

• F02B23/0624

  Swirl flow · CPC title

• F02B23/0621 Primary

  Squish flow · CPC title

• F02B31/00

  Modifying induction systems for imparting a rotation to the charge in the cylinder (air intakes or induction systems for internal-combustion engines F02M35/10) · CPC title