1. Technical Field
This invention relates generally to internal combustion engines, and more particularly to cylinder liners for diesel engines.
2. Related Art
It is known to cool cylinder liners with water in a water-cooling jacket extending about a portion of an outer surface of the cylinder liner. Unfortunately, the outer surface portion of the cylinder liner that comes in contact with the cooling water typically exhibits erosion from cavitation. The cavitation results from localized pressure variations brought on by vibration transmitted throughout the cylinder liner. As a result of these changes in pressure, the formation and disappearance of bubbles (known as cavitation) imparts mechanical forces in the form of shocks to the outer surface of the cylinder liner, which in turn, results in erosion of the cylinder liner outer wall. As expected, the cavitation, and thus, erosion, is typically most severe in regions of greatest vibration, which generally coincides with a region of the cylinder liner wall through which a piston reciprocates.
In an attempt to combat the onset of cavitation erosion, layers of plating have been formed on the outer surface of the cylinder liner, such as chromium, or ceramic layers have been used. However, these attempts are encumbered with increased costs brought on by both relatively expensive materials and inefficient manufacturing processes. Other attempts have incorporated an outer layer of white cast iron, with an underlying layer of martensitic and sorbitic microstructure, followed by the underlying parent material.
A cylinder liner manufactured according to the present invention overcomes or greatly minimizes any limitations of the prior art described above, and provides cylinder liners that can operate in heavy duty applications, while reducing their propensity for cavitation erosion, and thus, improving their useful life, all at a reduced overall cost.
A cast iron cylinder liner for an internal combustion engine manufactured in accordance with one presently preferred aspect of the invention reduces the potential for cavitation erosion of an outer surface of the liner at a minimal cost in manufacture, thereby providing an economically feasible way to increase the useful life of the cylinder liner between servicing. The cast iron cylinder liner has a wall providing a bore extending along a central axis for reciprocation of a piston therein and an outer surface shaped for receipt in a cylinder block. At least a portion of the outer surface opposite the portion of the bore through which the piston reciprocates is exposed to a cooling jacket in the cylinder block to reduce the operating temperature of the cylinder liner and piston. The portion of the outer surface exposed to the cooling jacket has a purely martensitic microstructure forming a hardened layer of a predetermined thickness to inhibit cavitation erosion of the outer surface.
Another aspect of the invention includes providing the martensitic hardened layer with a depth of about 10 percent or less of a thickness of the wall of the cylinder liner.
Yet another aspect of the invention includes a method of constructing a cylinder liner. The method includes casting a cylinder liner body having a cylinder wall and rough machining an inner surface of a cylinder bore and an outer surface of the cylinder wall. Then, finish machining at least a portion of the outer surface which will be exposed to water within a cooling jacket of a cylinder block. Then, heat treating the finish machined outer surface to provide a hardened layer of purely martensitic microstructure. And, if required, the method can also include hardening the cylinder bore. Then, tempering the hardened surfaces, if necessary. Lastly, finish machining the cylinder bore and a cylinder flange, along with any sealing areas, as necessary.
Accordingly, cylinder liners produced in accordance with the invention are useful for inhibiting the formation of cavitation erosion on an outer surface thereof. In addition, the cylinder liners are economical in manufacture, in assembly, and in use. Accordingly, the total cost to implement a mechanism to reduce the onset of cavitation erosion to the cylinder liner, and to increase the useful life of the cylinder liner, is reduced.
These and other aspects, features and advantages provided by cylinder liners manufactured in accordance with the invention 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, wherein like reference numerals are used to identify like features, in which:
Referring in more detail to the drawings,
In
To inhibit the cavitation in the cooling jacket 32 from eroding the outer surface 26, the hardened outer layer 30 is formed on a section of the portion 42, 43 most exposed to the potential damaging effects caused by the cavitation, and is shown here, for example, as extending over the entire axial length of the respective portion 42, 43 received within the cooling jacket 32. The hardened outer layer 30 is formed by heat treating the portion 42, 43 sufficiently to form a completely martensitic microstructure to a predetermined depth, and preferably to a depth up to about 10 percent of a thickness (t) of the wall 15 or less, which generally corresponds to about 0.5 to 1.5 mm in depth. The hardened outer layer 30 is formed having a hardness between about 42 to 55 Rc and with a smooth internal stress gradient to inhibit crack formation and crack propagation.
The manufacture of the cylinder liner 10 begins by casting iron to form a rough cast of the cylinder body 14, and then rough machining the necessary surfaces, depending on the application, such as the inner surface 16, outer surface 26, and possibly the primary and secondary mount flanges 34, 38. Then, heat treating the machined portion 42, 43 of the outer surface in an induction heating process to form the martensitic hardened outer layer 30. If desired, the inner surface 16 forming the cylinder bore 18 can also be heat treated. Further, tempering the hardened outer layer 30 to the desired hardness between about 42-52 Rc to the desired depth between about 0.5 to 1.5 mm. Lastly, finish machining the desired critical surfaces requiring close tolerances, such as the primary and secondary flanges 34, 38, the inner surface 16, and any other surfaces engaged with the cylinder block 12.
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.
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Number | Date | Country | |
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20080314353 A1 | Dec 2008 | US |