Bore portion for receiving a reciprocating piston

Patent metadata

Field	Value
Publication number	US-11274626-B2
Application number	US-201916583114-A
Country	US
Kind code	B2
Filing date	Sep 25, 2019
Priority date	Sep 26, 2018
Publication date	Mar 15, 2022
Grant date	Mar 15, 2022

Abstract

Methods and systems are provided for a bore. In one example, a system includes a bore portion for receiving a reciprocating piston, the bore portion having first and second ends between which the piston travels in an axial direction. The bore portion comprises a plurality of recesses, axially spaced apart, and formed in a piston facing surface of the bore portion at a plurality of axial positions, with at least one recess being provided at each axial position. Widths of the plurality of recesses decrease in the axial direction away from a mid-stroke position toward the first and second ends, and depths of the plurality of recesses increase in the axial direction away from the mid-stroke position toward the first and second ends.

First claim

The invention claimed is:

1. A system, comprising:
a bore portion for receiving a reciprocating piston, the bore portion having first and second ends between which the piston travels in an axial direction,
wherein the bore portion comprises a plurality of recesses, axially spaced apart, formed in a piston facing surface of the bore portion at a plurality of axial positions, with at least one recess being provided at each axial position, and
wherein widths of the plurality of recesses decrease in the axial direction away from a mid-stroke position toward the first and second ends, and wherein depths of the plurality of recesses increase in the axial direction away from the mid-stroke position toward the first and second ends;
wherein an axial spacing between neighboring axial positions varies progressively along the axial direction of the bore portion from the mid-stroke position to a first end and from the mid-stroke position to a second end; and
wherein the axial spacing between neighboring axial positions increases from the mid-stroke position to a maximum value at a first transition point between the mid-stroke position and the first end and a second transition point between the mid-stroke position and the second end.

2. The system of claim 1 , wherein at least one recess of the plurality of recesses at each axial position defines a total recess volume at each axial position and the total recess volume at each axial position varies progressively along an axial length of the bore portion with the total recess volume at each axial position increasing away from a mid-stroke position and towards the first and second ends of the bore portion.

3. The system of claim 2 , wherein a recess volume-to-spacing ratio is defined by a ratio of the total recess volume at a first axial position to an axial spacing between the at least one recess at the first axial position and a neighboring recess at a second axial position, and wherein the recess volume-to-spacing ratio varies progressively along the axial direction of the bore portion, wherein the recess volume-to-spacing ratio increases away from the mid-stroke position toward the first end and the second end.

4. The system of claim 1 , wherein the axial spacing between neighboring axial positions increases at a greater rate between the first end and the first transition point than between the first transition point and the mid-stroke position.

5. The system of claim 1 , wherein the axial spacing between neighboring axial positions increases at a greater rate between the second end and the second transition point than between the second transition point and the mid-stroke position.

6. The system of claim 1 , wherein the reciprocating piston comprises a piston ring, and wherein the recesses arranged at the first and second transition points comprise widths greater than a width of the piston ring.

7. The system of claim 6 , wherein each recess has a length in a direction with a circumferential component, and the lengths of the recesses vary across the plurality of axial positions.

8. The system of claim 1 , wherein each recess has a length measured in a direction opposite the width, each of the length and the width defining separate diameters of each recess of the plurality of recesses, and wherein the lengths of the recesses are constant across a single axial position of the plurality of axial positions.

9. An engine system, comprising:
a plurality of pistons positioned to oscillate within a plurality of combustion chambers, wherein each piston comprises one or more piston rings and wherein each combustion chamber comprises a liner comprising a plurality of recesses, wherein a volume of the plurality of recesses increases toward a top-dead center position and a bottom-dead center position from a mid-stroke position of a piston;
wherein a first spacing between recesses decreases from the mid-stroke toward the top-dead center position and the bottom-dead center position, the first spacing measured along a circumference of the liner; and
wherein a second spacing between recesses increases from the top-dead center position to a first transition position at a higher rate than a rate of increase of the second spacing between the first transition position to the mid-stroke position, wherein the first transition position is between the top-dead center position and the mid-stroke, and wherein the second spacing is a distance between recesses of the plurality of recesses at different axial positions measured relative to an axial axis along which the piston reciprocates, and wherein the second spacing between recesses increases from the bottom-dead center position to a second transition position at a higher rate than a rate of increase of the second spacing between the second transition position to the mid-stroke position.

10. The engine system of claim 9 , wherein a maximum speed of the piston occurs at the mid-stroke position.

11. The engine system of claim 9 , wherein the volume of the plurality of recesses is lowest at the mid-stroke and highest at the top-dead center position and the bottom-dead center position.

12. The engine system of claim 9 , wherein a width of the plurality of recesses is highest at the mid-stroke and lowest at the top-dead center and bottom-dead center positions, wherein the width is measured along an axial axis about which the piston reciprocates.

13. The engine system of claim 12 , wherein the width at the mid-stroke is higher than a width of a piston ring of the piston.

14. The engine system of claim 12 , wherein a length of the plurality of recesses is fixed, wherein the length is measured along a circumference of the piston, and wherein the length and the width are equal at the mid-stroke.

15. The engine system of claim 9 , wherein a depth of the plurality of recesses increases from the mid-stroke position to each of the top-dead center and the bottom-dead center positions, and where in a number of the plurality of recesses decreases from the mid-stroke position to each of the top-dead center and bottom-dead center positions.

Assignees

• Ford Global Tech Llc

Inventors

• Tufail Khizer
• Gangopadhyay Arup Kumar
• Skipp David
• Reddyhoff Thomas
• Vladescu Sorin-Cristian
• Stark Roland Paul

Classifications

• F02F2003/0007

  Monolithic pistons; One piece constructions; Casting of pistons · CPC title

• F02F1/20 Primary

  characterised by constructional features providing for lubrication · CPC title

• F16J10/04

  Running faces; Liners · CPC title

• F02B75/04

  Engines with variable distances between pistons at top dead-centre positions and cylinder heads · CPC title

• F02F3/00

  Pistons · CPC title