Piston design for flow re-direction

Patent metadata

Field	Value
Publication number	US-10876464-B2
Application number	US-201816140871-A
Country	US
Kind code	B2
Filing date	Sep 25, 2018
Priority date	Sep 25, 2018
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

A piston for an internal combustion engine includes a crown portion having a bowl that includes a plurality of protrusions. Each of the plurality of protrusions includes a first side surface and a second side surface. Other features including at least one ledge formed between protrusions in segments, and a generally flat, inward facing surface on the protrusions may also be used.

First claim

We claim:

1. An internal combustion engine, comprising:
an engine block having a cylinder bore;
a cylinder head having a flame deck surface disposed at one end of the cylinder bore;
an air intake valve associated with the cylinder head and configured to open and allow a flow of intake charge into the cylinder bore;
a piston connected to a rotatable crankshaft and configured to reciprocate within the cylinder bore along a longitudinal direction, the piston having a crown portion facing the flame deck surface along the longitudinal direction such that a combustion chamber is defined within the cylinder bore and between a top surface of the crown portion and the flame deck surface, the crown portion including a piston bowl having a generally concave shape and extending within the crown portion and a piston wall, the piston wall extending peripherally around the piston along a circumferential direction, an inner face of the piston wall facing a center of the piston bowl along a radial direction, the radial direction being perpendicular to the longitudinal direction;
a fuel injector having a nozzle tip disposed in fluid communication with the combustion chamber, the nozzle tip having a plurality of nozzle openings configured to inject a plurality of fuel jets into the combustion chamber, each fuel jet of the plurality of fuel jets being provided along a respective fuel jet centerline;
a plurality of protrusions disposed in the piston bowl adjacent to the piston wall, each protrusion of the plurality of protrusions including
an apex,
a first side surface extending from the piston wall to the apex, and
a second side surface extending from the piston wall to the apex, the second side surface facing away from the first side surface along the circumferential direction, the apex being disposed closer to the center of the piston bowl than the piston wall along the radial direction; and

at least one ledge defined by a ledge wall and a ledge floor,
the ledge floor extending from the inner face of the piston wall and away from the center of the piston bowl along the radial direction, the ledge floor being disposed between the top surface of the piston and a bottom of the piston bowl along the longitudinal direction,
the ledge wall extending from the ledge floor toward the top surface of the piston along the longitudinal direction, the ledge wall facing the center of the piston bowl along the radial direction,
wherein the apex of each protrusion is defined by a flat inner face, the flat inner face being flat in a reference plane defined exclusively by the radial direction and the circumferential direction,
wherein each protrusion has a minimum circumferential thickness along the circumferential direction, a radial location of the minimum circumferential thickness being located between the flat inner face and the piston wall along the radial direction, and
wherein a width of the flat inner face along the circumferential direction is greater than the minimum circumferential thickness.

2. The internal combustion engine of claim 1 , wherein the at least one ledge is disposed between two adjacent protrusions from the plurality of protrusions and occupies a length along an inner periphery of the piston wall.

3. The internal combustion engine of claim 1 , wherein the at least one ledge is formed in segments, each segment spanning a chordal distance along an inner circumference of the piston wall between adjacent protrusions.

4. The internal combustion engine of claim 3 , wherein each segment is curved to follow a contour of the piston wall.

5. The internal combustion engine of claim 4 , wherein the piston wall has a thickness extending from the inner face of the piston wall to an outer face of the piston wall along the radial direction,
each segment has a radial width extending from the inner face of the piston wall to the ledge wall along the radial direction, and
the radial width of each segment is less than the thickness of the piston wall.

6. The internal combustion engine of claim 1 , wherein the flat inner face is disposed between the first side surface and the second side surface along the circumferential direction.

7. The internal combustion engine of claim 1 , wherein the flat inner face is defined between two sharp edges.

8. The internal combustion engine of claim 7 , wherein the two sharp edges are disposed along interfaces between the flat inner face and the first and second side surfaces of the corresponding protrusion.

9. A piston for an internal combustion engine, the piston comprising:
a piston body;
a crown portion extending below a top surface of the piston body along a longitudinal direction, the crown portion including a piston bowl having a generally concave shape and extending within the crown portion and a piston wall, the piston wall extending peripherally around the piston body along a circumferential direction, an inner face of the piston wall facing a center of the piston bowl along a radial direction, the radial direction being perpendicular to the longitudinal direction;
a plurality of protrusions disposed in the piston bowl adjacent to the piston wall, each protrusion of the plurality of protrusions including
an apex,
a first side surface extending from the piston wall to the apex, and
a second side surface extending from the piston wall to the apex, the second side surface facing away from the first side surface along the circumferential direction, the apex being disposed closer to the center of the piston bowl than the piston wall along the radial direction; and

at least one ledge defined by a ledge wall and a ledge floor,
the ledge floor extending from the inner face of the piston wall and away from the center of the piston bowl along the radial direction, the ledge floor being disposed between the top surface of the piston and a bottom of the piston bowl along the longitudinal direction,
the ledge wall extending from the ledge floor toward the top surface of the piston along the longitudinal direction, the ledge wall facing the center of the piston bowl along the radial direction,
wherein the apex of each protrusion is defined by a flat inner face, the flat inner face being flat in a reference plane defined exclusively by the radial direction and the circumferential direction,
wherein each protrusion has a minimum circumferential thickness along the circumferential direction, a radial location of the minimum circumferential thickness being located between the flat inner face and the piston wall along the radial direction, and
wherein a width of the flat inner face along the circumferential direction is greater than the minimum circumferential thickness.

10. The piston of claim 9 , wherein the at least one ledge is disposed between two adjacent protrusions from the plurality of protrusions and occupies a length along an inner periphery of the piston wall.

11. The piston of claim 9 , wherein the at least one ledge is formed in segments, each segment spanning a chordal distance along an inner circumference of the piston wall between adjacent protrusions.

12. The piston of claim 11 , wherein each segment is curved to follow a contour of the piston wall.

13. The piston of claim 12 , wherein the piston wall has a thickness extending from the inner face of the piston wall to an outer face of the piston wall along the radial direction,
each segment has a radial width extending from the inner face of the piston wall to the ledge wall along the radial direction, and
the radial width of each segment is less than the thickness of the piston wall.

14. The piston of claim 9 , wherein the flat inner face

Assignees

• Caterpillar Inc

Inventors

• Svensson Kenth I
• Anders Jonathan W
• Dempsey Adam

Classifications

• F02B23/0651 Primary

  the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space · CPC title

• F02B23/0666

  having a single fuel spray jet per injector nozzle · CPC title

• F02B23/0624

  Swirl flow · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F02B23/0693

  the combustion space consisting of step-wise widened multiple zones of different depth · CPC title