Internal combustion engine and piston having stepped combustion bowl with non-axisymmetric profile

Patent metadata

Field	Value
Publication number	US-11274628-B2
Application number	US-202016889958-A
Country	US
Kind code	B2
Filing date	Jun 2, 2020
Priority date	Jun 2, 2020
Publication date	Mar 15, 2022
Grant date	Mar 15, 2022

Abstract

An internal combustion engine system includes an engine housing having a combustion cylinder, and a piston movable within the combustion cylinder to increase a pressure therein to an autoignition threshold for injected fuel. The piston includes a piston crown having a combustion face forming a combustion bowl, and varied in profile to form jet-jet interaction limiters at locations offset from fuel spray jet paths from a fuel injector. The jet-jet interaction limiters include a bowl component and a step component protruding, respectively, within the combustion bowl and a step located transitioning between the combustion bowl and a circumferential rim of the piston. Limiting jet-jet interaction limits soot production in exhaust produced by the engine.

First claim

What is claimed is:

1. A piston for an internal combustion engine comprising:
a piston crown defining a piston center axis extending between a first piston axial end, and a second piston axial end having a combustion face;
the combustion face forming a combustion bowl having a center cone and a bowl peripheral edge, a circumferential rim having a rim inner peripheral edge and a rim outer peripheral edge, and a step having a first step surface transitioning with the bowl peripheral edge and a second step surface transitioning with the rim inner peripheral edge;
the combustion face having a profile of rotation around the piston center axis that is varied to form jet-jet interaction limiters at spaced angular orientations around the piston center axis;
the jet-jet interaction limiters each including a bowl component protruding, within the combustion bowl, to limit interaction between adjacent spray jets of combusting fuel advanced radially outward through the combustion bowl; and
the jet-jet interaction limiters each further including a step component protruding, within the step, to limit interaction between the adjacent spray jets of combusting fuel once advanced from the combustion bowl into the step and spread azimuthally.

2. The piston of claim 1 wherein the bowl component and the step component are rounded, in an axial projection, and the bowl component and the step component in each of the jet-jet interaction limiters are symmetric about a common plane of symmetry that is parallel to and intersects the piston center axis.

3. The piston of claim 2 wherein:
the combustion bowl includes a bowl floor and a bowl outer wall extending from the bowl floor to the bowl peripheral edge;
the bowl component of each of the jet-jet interaction limiters extends axially between the bowl floor and the bowl peripheral edge, and radially inward from the bowl outer wall; and
the step component extends axially between the first step surface and the rim inner peripheral edge and radially inward from the second step surface.

4. The piston of claim 3 wherein the first step surface is formed in part upon the bowl component of each of the jet-jet interaction limiters, and the circumferential rim is formed in part upon the step component of each of the jet-jet interaction limiters.

5. The piston of claim 1 wherein:
the first step surface extends from the bowl peripheral edge to the second step surface and defines a step width dimension;
the second step surface extends from the first step surface to the rim inner peripheral edge and defines a step depth dimension; and
a top land extends circumferentially around the piston center axis and defines a piston diameter dimension.

6. The piston of claim 5 wherein each of the step width dimension and the step depth dimension is from about 3% to about 8% of the piston diameter dimension.

7. The piston of claim 1 wherein the combustion face profile includes a limiter profile at locations of the jet-jet interaction limiters and formed by each respective bowl component and step component, and a base profile at locations circumferentially between the jet-jet interaction limiters, and the limiter profile is congruous with the base profile.

8. The piston of claim 7 wherein a number of the jet-jet interaction limiters is from 3 to 8 and the jet-jet interaction limiters are in a regular distribution around the piston center axis.

9. The piston of claim 7 wherein the bowl peripheral edge defines a first radius of curvature, and the rim inner peripheral edge defines a second radius of curvature that is larger than the first radius of curvature, and wherein the combustion bowl is reentrant.

10. An internal combustion engine system comprising:
an engine housing having a combustion cylinder formed therein;
a fuel injector supported in the engine housing and having a plurality of spray orifices formed therein each defining a spray jet path; and
a piston within the combustion cylinder and including a piston crown defining a piston center axis extending between a first piston axial end, and a second piston axial end having a combustion face;
the combustion face forming a combustion bowl having a center cone and a bowl peripheral edge, a circumferential rim having a rim inner peripheral edge and a rim outer peripheral edge, and a step having a first step surface transitioning with the bowl peripheral edge and a second step surface transitioning with the rim inner peripheral edge;
the combustion face having a profile of rotation around the piston center axis that is varied to form jet-jet interaction limiters;
the jet-jet interaction limiters being arranged at locations offset from the spray jet paths and each including a bowl component protruding, within the combustion bowl to limit interaction between adjacent spray jets of combusting fuel injected from the plurality of spray orifices advanced radially outward through the combustion bowl, and a step component protruding, within the step, to limit interaction between the adjacent spray jets of combusting fuel once advanced from the combustion bowl into the step and spread azimuthally; and
the combustion face profile includes a limiter profile at locations of the jet-jet interaction limiters, and a base profile at locations circumferentially between the jet-jet interaction limiters, and the limiter profile is congruous with the base profile.

11. The engine system of claim 10 wherein a number of each of the spray orifices and the jet-jet interaction limiters is from 3 to 8, and the spray jet paths and the jet-jet interaction limiters are in an alternating arrangement circumferentially around the piston center axis.

12. The engine system of claim 11 wherein the spray jet paths intersect the piston, in an axial projection, at locations equidistant from adjacent ones of the jet-jet interaction limiters.

13. The engine system of claim 10 wherein the bowl component and the step component have rounded shapes, in an axial projection, and the bowl component and the step component in each of the jet-jet interaction limiters are symmetric about a common plane of symmetry that is parallel to and intersects the piston center axis.

14. The engine system of claim 13 wherein:
the combustion bowl includes a bowl floor and a bowl outer wall extending from the bowl floor to the bowl peripheral edge;
the bowl component of each of the jet-jet interaction limiters extends axially between the bowl floor and the bowl peripheral edge, and radially inward from the bowl outer wall;
the step component extends axially between the first step surface and the rim inner peripheral edge and radially inward from the second step surface; and
the first step surface is formed in part upon the bowl component of each of the jet-jet interaction limiters, and the circumferential rim is formed in part upon the step component of each of the jet-jet interaction limiters.

15. The engine system of claim 10 wherein:
the first step surface extends from the bowl peripheral edge to the second step surface and defines a step width dimension;
the second step surface extends from the first step surface to the rim inner peripheral surface and defines a step depth dimension;
a top land extends circumferentially around the piston center axis and defines a piston diameter dimension; and
each of the step width dimension and the step depth dimension is from about 3% to about 8% of the piston diameter dimension.

16. A piston crown for a piston in an internal combustion engine comprising:
a piston crown body including a piston outer surface having a top land and extendi

Assignees

• Caterpillar Inc
• Uchicago Argonne Llc

Inventors

• Anders Jonathan William
• Kavuri Naga Krishna Chaitanya
• John Bobby
• Mohammad Hyderuddin
• Xu Chao
• Kundu Prithwish

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F02F3/28 Primary

  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

• F02B23/0678 Primary

  Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets · CPC title

• F02B23/0645

  Details related to the fuel injector or the fuel spray · CPC title