CYLINDER LINER AND METHODS CONSTRUCTION THEREOF AND IMPROVING ENGINE PERFORMANCE THEREWITH

Information

  • Patent Application
  • 20070246026
  • Publication Number
    20070246026
  • Date Filed
    April 03, 2007
    17 years ago
  • Date Published
    October 25, 2007
    17 years ago
Abstract
A cylinder liner for an internal combustion diesel engine and corresponding method of construction and method of improving engine performance therewith has a cylindrical inner wall providing a bore extending along a central axis for reciprocation of a piston therein. The inner wall has an axial lower portion and an axial upper portion. The lower portion has a first diameter below a top-dead-center plane and the upper portion has a second diameter provided by a material formed as one piece with the inner wall, wherein the first diameter is greater than the second diameter.
Description

BRIEF DISCUSSION OF THE DRAWINGS

These and other aspects, features and advantages will become readily apparent to those skilled in the art in view of the following detailed description of the presently preferred embodiments and best mode, appended claims, and accompanying drawings, in which:



FIG. 1 is a cross-sectional view of a cylinder liner constructed according to one presently preferred embodiment of the invention with a piston therein shown at a top-dead-center-position;



FIG. 2 is an enlarged fragmentary view of the encircled area of FIG. 1 shown in an initial state of use; and



FIG. 3 is a view similar to FIG. 2 shown after some use.





DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

Referring in more detail to the drawings, FIG. 1 illustrates a cylinder liner 10 constructed according to one presently preferred embodiment of the invention disposed in a cylinder block 12 of a diesel engine. The cylinder liner 10 has a body 14 with a cylindrical inner wall 16 defining a cylinder bore 18 for reciprocation of a piston 20 along a central axis 21 therein. The piston 20 typically has at least one annular ring groove 22 for floating receipt of a piston ring, wherein a top upper most piston ring 24 facilitates guiding the piston 20 during reciprocation, while also inhibiting the passage of oil upwardly from below the piston 20. FIG. 1 shows the piston 20 in a top-dead-center (TDC) position, with the top piston ring 24 having an upper surface 26 (FIGS. 2 and 3) coinciding with an imaginary annular TDC line or plane 28 that extends generally transversely to the central axis 21 about the inner wall 16. The TDC plane 28 separates two portions of the cylinder bore 18, with a lower portion 30 having a first diameter D being defined below the TDC plane 28, through which the piston reciprocates, and an upper portion 32 having a second diameter d1 being defined above the TDC plane. The upper portion 32 includes a material 34 that can be formed as one monolithic piece with the inner wall 16. The material 34 extends radially inwardly toward the central axis 21 of the cylinder bore 18 relative to an inner diameter D of the surface 16 of the lower portion 30.


The material 34 inhibits the flow of fluid and gases thereby, thus, reducing the amount of oil expelled via “oil-scrape” or “throw-off” (results from oil above the upper most piston ring being thrown upwards by the piston 20 and/or piston ring 24 during an upstroke of the piston) upwards into the exhaust emissions, while also acting to provide a labyrinth to combustion gases flowing toward the uppermost piston ring 24. Accordingly, any localized formation of oxidized lubrication is inhibited from building up on a back of the piston ring groove 22, which in turn, acts to prevent a condition know as “carbon jacking” of the rings 24, or “sticking” of the rings 24. Further, the material 34 acts to remove or scrape carbon buildup from an upper land portion 36 of the piston 20, wherein the upper land portion 36 is defined generally between the uppermost ring 24 and a crown 38 of the piston 20. This is particularly true after some use of the engine has occurred, wherein some desirable amount of carbon buildup (FIG. 3, showing build-up in the foreground with the background shown without build-up for illustration purposes only) has formed on the material 34. Accordingly, the cylinder liner 10 provides a cost effective mechanism in which to reduce exhaust emissions, improve oil consumption and extend the useful life of the engine.


The material 34 on the upper portion 32 of the liner 10 is preferably formed to provide a cold radial clearance (r) with the upper land 36 of the piston 20, down to about 0.100 mm. Generally, the material 34 is formed to the reduced inner diameter d1 over at least a section of the upper portion 32 by about 0.5-1.5% relative to the inner diameter D of the lower portion 30. The width (w) of the material 34 extends axially along the central axis 21, and can be varied in length of coverage, as desired, however, it preferably extends to an area of the cylinder upper portion 32 immediately adjacent the imaginary TDC plane 28. As such, scraping of the upper land 36 of the piston 20 is facilitated in use, as shown in FIG. 3.


The cylinder liner 10, with the material 34 formed on the upper portion 32, can be further processed, such as machined, heat treated, whether cased hardened or through hardened, without any additional challenges. However, given that the inner diameter d1 of the upper portion 32 is reduced from the inner diameter D of the lower portion 30, it is generally preferred, and in some cases necessary to assemble the piston 20, with rings 24 assembled thereon, into the cylinder liner 10 from its underside, with the piston 20 being linked to the connecting rod (not shown), prior to assembling the cylinder block 12 to the engine block.


The material 34 extending radially inwardly from the inner wall 16 can be formed by one of several mechanisms. For example, the material 34 can be formed in an extruding process wherein the material of the inner wall 16 is extruded or knurled from the material of the cylinder liner to produce peaks 40 (FIGS. 2 and 3) extending radially inwardly relative to the inner diameter D of the lower portion 30 by a predetermined distance P, such that the peaks 40 define the second diameter d1, and valleys 42 extending radially outwardly relative to the inner diameter D of the lower portion 30 by a predetermined distance V to define a third diameter d2. With this construction of the material 34, the diameter D of the lower portion 30 is greater than the diameter d1 of the peaks 40 and the diameter d2 of the valleys 42 is greater than the diameter D of the lower portion 30. Preferably, a uniform pattern of the peaks 40 and valleys 42 is formed, such as in a diamond-like or cross-hatch pattern, for example. Other than extruding, the material 34 can be plastically formed utilizing other material upsetting processes, such as embossing or media blasting, for example. It should be recognized that masking can be used to prevent upsetting material on the inner surface of the lower portion 30, and thus, the formation of the material 34 can be restricted to the upper portion 32 of the inner wall 16. It should also be recognized that in addition to forming the material 34 as a monolithic piece with the upper surface 32, the material 34 can be formed by bonding a layer of additional material as one piece with the inner wall 16, such as by screen printing or spray coating, for example. Further, it should be recognized that where a separate material is applied to the inner wall 16, that the material 34 is selected from a suitable material to withstand the operating environment of the engine. It should also be recognized that regardless of how the radially inwardly extending material 34 is formed that it is preferably formed in accordance with the cold radial clearance parameters set forth above.


In use, the material 34 formed on the upper surface 32 acts to benefit operation of the engine in a number of ways. Initially, the material 32 provides a labyrinth to inhibit the downward flow of hot combustion gases and fluid toward the upper most piston ring 24 and groove 22. As such, the ingress of hot gases and fluid from the combustion chamber past the upper most piston ring 24 is inhibited, thereby retarding local oxidation of lubricant and diminishing carbon formation within and on the back side of the groove 22, thereby promoting proper functioning of the piston rings 24. As mentioned, this acts to reduce the likelihood of ring jacking or sticking from occurring, and thus, the useful life and efficiency of the engine between servicing is enhanced.


As use of the engine continues over time, the radially inwardly extending material 34 acts to attract and accumulate a desired amount of build up (FIG. 3), such as carbon deposits 44, thereon. The accumulation begins with oil being deposited on the surface of the material 34, wherein cohesion of the oil on the surface is enhanced by the undulating geometry of the peaks 40 and valleys 42, whereupon the oil is oxidized to begin forming the layers of carbon deposits 44. The build up of carbon deposits 44 serves as a mechanical barrier to gas penetration downwardly, while also acting as a barrier to oil scrape and throw-off upwardly. The amount of carbon build-up 44 is self-regulating as a result of an upper edge 46 of the piston top land 36 scraping away any excess build-up during an upward stroke of the piston 20. Accordingly, any carbon scraped off will be either consumed/burned during combustion or discharged during the exhaust stroke. Given the minute amounts of carbon formation per engine thermodynamic cycle, any excess is easily processed and consumed by the engine itself.


The mechanical barrier 44 formed by carbon build-up, which is facilitated by the material 34, thus, performs at least two important roles in increasing the running performance of the engine. First, it inhibits gas and fluid penetration downwards, and second, it inhibits oil scrape and throw-off upwards. The first of which acts to increase the useful life of the engine, such as by preventing the onset of ring jacking and sticking, while the second acts to improve the oil consumption of the engine and reduce exhaust emissions.


Accordingly, a cylinder liner 10 constructed within the scope of the present invention, as defined by the claims, provides at least the benefits of the bands discussed in the background section above, which, as mentioned, require complex and precise machining and secondary installation, without having to incur the negative aspects associated therewith. Further, it is believed that the useful life of the engine between servicing can be further enhanced relative to the useful life attainable through the use of the aforementioned bands. Also, cylinder liners of any size and thickness can benefit from the invention herein, unlike the use of separate bands, which require that the cylinder liners are of suitable thickness to form the radially outwardly extending grooves or recess for their receipt therein.


It is to be understood that other embodiments of the invention which accomplish the same function are incorporated herein within the scope of any ultimately allowed patent claims.

Claims
  • 1. A cylinder liner for an internal combustion diesel engine, comprising: a cylindrical inner wall providing a bore extending along a central axis for reciprocation of a piston therein, said inner wall having an axial lower portion and an axial upper portion separated from one another by a plane extending transversely to said central axis at a top-dead-center position of an upper piston ring, said lower portion having a first diameter below said plane and said upper portion having a second diameter defined by a material formed as one piece with said inner wall, said first diameter being greater than said second diameter.
  • 2. The cylinder liner of claim 1 wherein said material is extruded material from said inner wall.
  • 3. The cylinder liner of claim 2 wherein said extruded material defines a pattern of radially inwardly extending peaks and radially outwardly extending valleys.
  • 4. The cylinder liner of claim 3 wherein said peaks define said second diameter and said valleys define a third diameter, said third diameter being greater than said first diameter.
  • 5. The cylinder liner of claim 3 wherein said pattern is generally diamond shaped.
  • 6. The cylinder liner of claim 1 wherein said material is bonded to said inner wall.
  • 7. The cylinder liner of claim 1 wherein said second diameter is reduced from said first diameter between about 0.5 and 1.5 percent.
  • 8. A method of inhibiting gas and fluid flow axially beyond a portion of a cylinder liner inner wall, the inner wall having a lower portion through which a piston reciprocates and an upper portion separated axially from the lower portion by a top-dead-center position of a top piston ring, the method comprising: forming a surface of material on at least a portion of the upper portion, said surface of material extending radially inwardly from the lower portion to inhibit gas and fluid flow thereby.
  • 9. The method of claim 8 further including forming said surface of material by extruding the inner wall material.
  • 10. The method of claim 9 further including forming a uniform pattern in the surface of material.
  • 11. The method of claim 9 further including forming a plurality of peaks extending radially inwardly relative to said lower portion in the extruding step.
  • 12. The method of claim 11 further including forming a plurality of valleys extending radially outwardly relative to said lower portion in the extruding step.
  • 13. The method of claim 8 further including forming said surface of material by bonding a layer of material to the inner wall.
  • 14. The method of claim 13 further including spray coating said layer of material to the inner wall.
  • 15. The method of claim 13 further including screen printing said layer of material to the inner wall.
  • 16. The method of claim 8 further including embossing the inner wall to form said surface of material.
  • 17. The method of claim 8 further including providing the lower portion with a first diameter and forming said surface of material having a second diameter that is reduced from said first diameter between about 0.5 and 1.5 percent.
  • 18. A method of constructing a cylinder liner, comprising: forming a bore in a cylinder block, said bore having an inner wall extending along a central axis, said inner wall having an axial lower portion with a first diameter for reciprocation of a piston therein and an axial upper portion separated from said lower portion by a plane extending transversely to said central axis at a top-dead-center position of an upper piston ring; andforming a surface of material on said upper portion, said surface of material having a second diameter that is reduced from said first diameter.
  • 19. The method of claim 18 further including forming said surface of material by extruding the inner wall of the cylinder block material.
  • 20. The method of claim 19 further including forming a plurality of peaks extending radially inwardly relative to said lower portion and a plurality of valleys extending radially outwardly relative to said lower portion in the extruding step.
  • 21. The method of claim 18 further including forming said surface of material by bonding a layer of material to the inner wall.
  • 22. The method of claim 18 further including forming said second diameter having a diameter that is reduced from said first diameter between about 0.5 and 1.5 percent.
CROSS-REFERENCE TO RELATED APPLICATION

This application claims the benefit of U.S. Provisional Application Ser. No. 60/794,363, filed Apr. 24, 2006, which is incorporated herein by reference in its entirety.

Provisional Applications (1)
Number Date Country
60794363 Apr 2006 US