METHODS AND APPARATUS FOR OPERATING AN INTERNAL COMBUSTION ENGINE

• US 20090020958A1
• Filed: 03/31/2006
• Published: 01/22/2009
• Est. Priority Date: 03/31/2006
• Status: Abandoned Application

• Current Assignee: Dieseltech, LLC
• Original Assignee: Dieseltech, LLC
• Inventors: Soul, David F.
• Application Number:
  US11/278,320
• Publication Number:
  US 20090020958A1
• Time in Patent Office: Days
• US Class Current: 277/434
• CPC Class Codes: F01B 7/14 acting on different main shafts
• CPC Class Codes: F02B 75/28 Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders arranged oppositely relative to main shaft F02B75/24
• CPC Class Codes: F02F 5/00 Piston rings, e.g. associated with piston crown not used see F16J9/00

Abstract

A piston ring assembly for an internal combustion engine is provided. The piston ring assembly includes a plurality of seal rings, i.e., a first seal ring and a second seal ring. The seal rings are positioned on at least a portion of a piston crown periphery axially and radially adjacent to each other within the internal combustion engine and at least a portion of the first seal ring at least partially extends over at least a portion of the second seal ring.

Claims

1. A piston ring assembly for an internal combustion engine comprising a plurality of seal rings positioned on at least a portion of a piston crown periphery.

2. A piston ring assembly in accordance with claim 1 wherein said plurality of seal rings comprise a first seal ring and a second seal ring.

3. A piston ring assembly in accordance with claim 2 wherein said first seal ring comprises a high temperature and substantially wear resistant material.

4. A piston ring assembly in accordance with claim 3 wherein said wear resistant material comprises a stainless steel alloy.

5. A piston ring assembly in accordance with claim 2 wherein said first and second seal rings are positioned axially and radially adjacent to each other within said internal combustion engine, at least a portion of said first seal ring at least partially extends over at least a portion of said second seal ring.

6. A piston ring assembly in accordance with claim 2 wherein said first seal ring is substantially circular with a circumferential periphery and comprises at least one wall, said wall comprises at least one split defined within said wall, said wall defining at least one integral protrusion, said split extends obliquely at a predetermined angle to at least a portion of the circumferential periphery, said first seal ring positioned within said internal combustion engine such that said first seal ring split is positioned with substantially circumferential opposition to a second seal ring split defined within said second seal ring, said first seal ring split facilitates contact avoidance between said first seal ring and at least a portion of at least one exhaust port, said integral protrusion facilitates substantially circumferential opposition between said first seal ring split and the second seal ring split.

7. A piston ring assembly in accordance with claim 6 wherein said seal ring wall comprises a substantially wear resistant material layer extending over at least a portion of said seal ring wall.

8. A piston ring assembly in accordance with claim 7 wherein said wear resistant material layer comprises a molybdenum alloy.

9. A piston ring assembly in accordance with claim 2 wherein said second seal ring is substantially circular with a circumferential periphery and comprises at least one wall having at least one split defined therein, said wall defines a substantially rectangular circumferential profile, said split extends obliquely at a predetermined angle to at least a portion of the circumferential periphery, said second seal ring positioned within said internal combustion engine such that said second seal ring split positioned with substantially circumferential opposition to a first seal ring split defined within said first seal ring, said second seal ring split facilitates contact avoidance between said second seal ring and at least a portion of at least one exhaust port.

10. A method of operating an internal combustion engine comprising positioning a piston ring assembly on at least a portion of a piston crown periphery, said positioning a piston ring assembly comprises positioning a first seal ring and a second seal ring such that the first seal ring is a first axial distance from the combustion chamber and the second seal ring is a second axial distance from the combustion chamber, the second distance is greater than the first distance, the first seal ring comprising a high temperature material.

11. A method of operating an internal combustion engine in accordance with claim 10 wherein positioning a first seal ring comprises positioning the first seal ring on at least a portion of the piston crown periphery such that the first seal ring is coupled to the portion of the piston crown via an interference fit.

12. A method of operating an internal combustion engine in accordance with claim 10 wherein positioning a first seal ring and a second seal ring comprises positioning the first and second seal rings within the internal combustion engine such that a first seal ring split is positioned with substantially circumferential opposition to a second seal ring split.

13. An internal combustion engine comprising:

at least one substantially cylindrical housing; and

a plurality of opposed piston assemblies enclosed within said cylindrical housing, said plurality of opposed piston assemblies comprising a plurality of seal rings, said seal rings positioned on at least a portion of a piston crown periphery.

14. An engine in accordance with claim 13 wherein said plurality of seal rings comprise a first seal ring and a second seal ring.

15. An engine in accordance with claim 14 wherein said first seal ring comprises a high temperature and substantially wear resistant material.

16. An engine in accordance with claim 15 wherein said wear resistant material comprises a stainless steel alloy.

17. An engine in accordance with claim 14 wherein said first and second seal rings are positioned axially and radially adjacent to each other within said diesel engine, at least a portion of said first seal ring at least partially extends over at least a portion of said second seal ring.

18. An engine in accordance with claim 14 wherein said first seal ring is substantially circular with a circumferential periphery and comprises at least one wall, said wall comprises at least one split defined within said wall, said wall defining at least one integral protrusion, said split extends obliquely at a predetermined angle to at least a portion of the circumferential periphery, said first seal ring positioned within said diesel engine such that said first seal ring split is positioned with substantially circumferential opposition to a second seal ring split defined within said second seal ring, said first seal ring split facilitates contact avoidance between said first seal ring and at least a portion of at least one exhaust port, said at least one integral protrusion facilitates substantially circumferential opposition between said first seal ring split and the second seal ring split.

19. An engine in accordance with claim 18 wherein said seal ring wall comprises a substantially wear resistant material layer extending over at least a portion of said seal ring wall.

20. An engine in accordance with claim 14 wherein said second seal ring is substantially circular with a circumferential periphery and comprises at least one wall, said wall comprises at least one split defined within said wall, said wall defines a substantially rectangular circumferential profile, said split extends obliquely at a predetermined angle to at least a portion of the circumferential periphery, said second seal ring is positioned within said diesel engine such that said second seal ring split is positioned with substantially circumferential opposition to a first seal ring split defined within said first seal ring, said second seal ring split facilitates contact avoidance between said second seal ring and at least a portion of at least one exhaust port.