The present disclosure relates to marine engines and particularly to marine engines having a cylinder block with one or more cylinder liners.
The following U.S. Patents are incorporated herein by reference in entirety:
U.S. Pat. No. 4,776,303 discloses a two cycle internal combustion engine having a cylinder liner. A fuel-air flow passage is provided from the crankcase to the exhaust bridge in the cylinder liner and the exhaust bridge in the cylinder block along the interface between the cylinder liner and the cylinder block. A plurality of apertures is provided through the cylinder liner communicating with the fuel-air flow passage. A second fuel-air flow passage is provided between the piston and the cylinder liner and in communication with the apertures to facilitate fuel-air mixture flow through the exhaust bridge to improve lubrication and cooling thereof.
U.S. Pat. No. 5,303,682 discloses a hypereutectic aluminum-silicon alloy cylinder bore liner produced by feeding the molten alloy into a metal mold having an inner shell sand cup, while rotating the mold at a speed in excess of 1,000 rpm, to cause the molten alloy to be thrown outwardly by centrifugal force to form a cylindrical liner. On solidification of the alloy, discrete silicon particles are precipitated and the use of the sand shell increases the fluid life of the alloy to enable the lighter weight silicon particles to migrate inwardly under the centrifugal force of rotation, to produce a solidified liner having a greater volume fraction of silicon particles in the inner portion of the liner where greater wear resistance is desired.
U.S. Pat. No. 7,000,584 discloses an engine provided with a plurality of cylinders and cylinder liners that are shaped to define a plurality of spaces between the liners and the cylinder block. These spaces provided an insulative barrier that at least partially restricts the flow of heat from the liner into the cylinder block. This allows the liners to operate at elevated temperatures while avoiding a deleterious increase in the cooling water temperature as it flows through passages within the cylinder block.
U.S. Pat. No. 7,191,770 discloses an engine made by providing a layer of material between the outer surface of a cylinder liner and the inner surface of the cylinder opening within a cylinder block. The material can be a polymer or a ceramic. Polyether ether ketone or polyethylene terephthalate can be a polymer used for these purposes. Zirconia or yttria can be ceramic used for these purposes. An electro-deposited paint can serve as the layer of thermally insulative material.
This Summary is provided to introduce a selection of concepts that are further described herein below in the Detailed Description. This Summary is not intended to identify key or essential features of the claimed subject matter, nor is it intended to be used as an aid in limiting the scope of the claimed subject matter. In examples disclosed herein, a marine engine comprises a cylinder block that defines a cylinder bore; a piston that reciprocates in the cylinder bore under force of combustion in the marine engine; and a liner disposed in the cylinder bore between the piston and the cylinder block. The liner provides a running surface for the piston. The liner has a cylindrical liner body that is sized to fit snugly within the cylinder bore and a pair of diametrically opposing tabs axially extends from liner body into the cylinder bore. Exemplary methods of making a marine engine are also disclosed herein.
The present disclosure is described with reference to the following Figures. The same numbers are used throughout the figures to reference like features and like components.
Each piston 20 has a piston body (including peripheral sealing rings) 22 and a piston skirt 24 that axially extends from the piston body 22. A connecting rod 26 is disposed in the cylinder bore 16 and is coupled to the piston skirt 24 via a pin aperture 28 extending through the piston skirt 24. The connecting rod 26 connects the piston 20 to a vertically extending crankshaft 25 such that reciprocation of the pistons 20 in the cylinder bores 16 causes rotation of the crankshaft 25 about its own axis 27, all as is conventional. Each piston 20 is oriented in its respective cylinder bore 16 such that the pin aperture 28 is oriented parallel to the vertically extending axis 27. The piston skirt 24 has a pair of diametrically opposing side surfaces 30 that axially extend from the piston body 22. Each of the side surfaces 30 includes a bottom edge 32 and opposing side edges 34 that taper towards each other from the piston body 22 to the bottom edge 32.
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The present disclosure thus provides a marine engine having a cylinder block that defines a cylinder bore, a piston that reciprocates in the cylinder bore under force of combustion in the marine engine, and a liner disposed in the cylinder bore between the piston and the cylinder block. The liner provides a running surface for the piston and includes a cylindrical liner body that is sized to fit snuggly within the cylinder bore and a pair of diametrically opposing tabs that axially extend from the liner into the cylinder bore. The piston has a piston body and a piston skirt. The piston skirt has a pair of diametrically opposing side surfaces that axially extend from the piston body. Each of the diametrically opposing side surfaces comprises a bottom edge and opposing side edges that taper towards each other from the piston body to the bottom edge. The pair of diametrically opposing tabs on the liner is radially aligned with the diametrically opposing side surfaces on the piston skirt so as to provide a bearing surface for the piston skirt as the piston axially reciprocates in the liner. The liner has a lower edge profile that extends peripherally around the cylindrical liner body, including along the pair of diametrically opposing tabs. The cylinder bore thus forms a bearing surface that radially abuts and supports the liner. The bearing surface follows the lower edge profile of the liner. Recessed cutouts are formed on opposite sides of each of the pair of diametrically opposing tabs. The recessed cutouts follow the lower edge of the profile of the liner so that the bearing surfaces radially abuts all portions of the liner, including the liner body and the pair of diametrically opposing tabs.
The present disclosure provides a method of making a marine engine including forming the cylinder block including the cylinder bore, providing the piston, which reciprocates in the cylinder bore under force of combustion, and disposing the liner in the cylinder bore between the piston and the cylinder block. The method includes forming recessed cutouts in the cylinder bore on opposite sides of each of the opposing tabs, which follow the lower edge profile of the liner so that the bearing surface radially abuts all portions of the liner, including the liner body and the pair of diametrically opposing tabs. These measures advantageously save weight of the liner and the cylinder block. The cylinder block can be formed of aluminum and the liner formed of iron.
In the above description, certain terms have been used for brevity, clarity, and understanding. No unnecessary limitations are to be inferred therefrom beyond the requirement of the prior art because such terms are used for descriptive purposes and are intended to be broadly construed. The different systems and method steps described herein may be used alone or in combination with other systems and methods. It is to be expected that various equivalents, alternatives and modifications are possible within the scope of the appended claims.
Number | Name | Date | Kind |
---|---|---|---|
4452194 | Watanabe | Jun 1984 | A |
4776303 | Hundertmark | Oct 1988 | A |
5134976 | Towner et al. | Aug 1992 | A |
5303682 | Donahue et al. | Apr 1994 | A |
7000584 | Wynveen et al. | Feb 2006 | B1 |
7191770 | Anderson et al. | Mar 2007 | B1 |
7240608 | Schaefer | Jul 2007 | B2 |