The present invention generally relates to a piston. More particularly, the present invention pertains to a miniaturized piston having improved properties required for the piston.
In recent years, reductions in weight have been demanded for internal combustion pistons for purposes of improving fuel economy, and some progress has been made in achieving reductions in size. On the other hand, requirements in respect of properties such as abrasion resistance, seizure resistance, and low friction have become increasingly strict. From these view points, in a conventional piston, light-weight materials such as aluminum and aluminum alloys have been utilized in order to reduce the weight of the piston, and then the surface of the piston has been reinforced in order to enhance properties such as abrasion resistance and seizure resistance.
JPH10-331970A proposes that, if a surface of a piston made of cast aluminum alloy containing Si is covered with a sintered resin film including a solid lubrication agent, aluminum adhesion resistance, peel strength, and abrasion resistance of the piston can all be improved. However, in the piston according to JPH10-331970A, if the temperature rises at a time of combustion, the sintered resin film tends to become carbonized, and satisfactory durability cannot be obtained.
JPH11-022545A and JP2001-73869A propose that, if a ring carrier made of an iron-based sintered alloy or an aluminum alloy is inserted in a top ring groove of a piston made of aluminum alloy, abrasion resistance of the piston can be improved. However, in the pistons according to JPH11-022545A and JP2001-73869A, machining processes for putting a component into a predetermined shape after insertion become difficult, and this causes a rise in the costs of machining. Additional disadvantages are an increase in weight and a deterioration in thermal conductivity.
JP2003-013802A and JP2001-271704A propose that, if an anodic oxide film (illustrated in
A need thus exists for a miniaturized piston having improved properties which can satisfy requirements for pistons. The present invention has been made in view of the above circumstances and provides such a piston.
According to an aspect of the present invention, a piston has a piston body made of a material selected from any one of aluminum, an aluminum alloy, magnesium, and a magnesium alloy. An entire surface or a predetermined portion of the surface of the piston body is covered with a plasma oxide film.
According to a further aspect of the present invention, a piston has a piston body made of a material selected from either one of aluminum and an aluminum alloy. An entire surface or a predetermined portion of the surface of the piston body is covered with a plasma oxide film containing α-alumina.
The foregoing and additional features and characteristics of the present invention will become more apparent from the following detailed description considered with reference to the accompanying drawings, wherein:
An embodiment of the present invention will be explained with reference to drawing figures.
A piston 1 is utilized for an internal combustion. A piston 1 is made of a Si-aluminum alloy. However, it is not limited. The piston 1 can also be made of aluminum, magnesium, or a magnesium alloy, or the like. The piston 1 includes plural piston ring groove portions (a top ring groove 12, a second ring groove 13 and an oil ring groove 14) formed on a cylinder surface near an upper surface portion 11. The piston 1 includes a skirt portion 15 formed under the oil ring groove 14. The piston 1 includes a pin boss portion 16 formed at a predetermined position of the skirt portion 15 to be connected with a piston pin (not illustrated).
A plasma oxide film 17 is provided onto a surface of the top ring groove 12 of the piston ring groove portions. In addition, the plasma oxide film 17 can be provided onto an entire surface of the piston 1, in addition to the surface of the top ring groove 12. Further, the plasma oxide film 17 can be provided onto any one, or more of the second ring groove 13, the oil ring groove 14, the skirt portion 15, and the pin boss portion 16. The plasma oxide film 17 is formed at a predetermined portion of the piston body 10 that has been made of materials described above by means of plasma oxidation treatment.
Accordingly, in the piston according to the embodiment, it is preferable that the amount of Si contained in the aluminum alloy be equal to, or more than, 12% by weight, and equal to, or less than, 25% by weight. In order to ensure strength of a piston, in general terms it is essential that the amount of Si contained be set at a relatively high level. However, conventionally, when an anodic oxidation process was performed on a piston, it was not possible for the amount of Si to be set at a high level. According to the embodiment, because the piston body 10 is treated by means of the plasma oxidation process, the amount of Si contained can be set at a high level. In other words, by making the amount of Si contained in the aluminum alloy equal to, or more than, 12% by weight, it is possible to further increase the strength of the piston body 10, and in turn this can enhance the rigidity of the piston and thus contribute to making a piston thinner and lighter. Further, by increasing the amount of Si contained, it is possible to achieve a reduction on the degree of thermal expansion of the piston. Accordingly, the extent of a clearance between a cylinder and the piston, and/or a piston pin and the piston, can be reduced, and this in turn can lead to a diminution in the level of vibrations and/or noises generated by the piston. In contrast, when a piston is made of an aluminum alloy containing Si in an amount less than 12% by weight, the piston can acquire only a degree of rigidity equivalent to that of a conventional piston made of an aluminum alloy. In addition, when the amount of Si contained in the aluminum alloy is more than 25% by weight, it becomes difficult to form a plasma oxide film on the piston body 10, and thus tends to result in a reduction in the degree of smoothness of the film.
The plasma oxide film 17 contains α-Al2O3 (α-alumina) and γ-Al2O3 (γ-alumina). In this case, the amount of the α-Al2O3 contained in the plasma oxide film 17 can be from 0.5 to 95% by weight. For assuming composition of the plasma oxide film 17, X-ray diffraction patterns of the plasma oxide film 17 and that of a standard reagent (in which the α-Al2O3 and the γ-Al2O3 are mixed at a predetermined ratio) were compared. For the comparison, area ratios were calculated between a peak at 2θ=43.31° corresponding to α-Al2O3 of each X-ray diffraction pattern, and between each peak at 2θ=45.78° and 66.86° corresponding to γ-Al2O3 of each X-ray diffraction pattern. As a result, composition of the plasma oxide film 17 is assumed to be 0.5 to 95% by weight of the α-Al2O3 and 5 to 99.5% by weight of the γ-Al2O3. The plasma oxide film 17 in which the α-Al2O3 is generated at this ratio can be highly hard (HV1200 to 1400). Thus, positions of the piston ring groove portions (in particular, the top ring groove 12) can be closer toward a combustion chamber. In addition, in the plasma oxide film 17, a part of the α-Al2O3 is assumed to become amorphous. Accordingly, though the amount of the α-Al2O3 detected by the X-ray diffraction is small, it can be assumed that several times the amount of the α-Al2O3 described above is contained in actual. With reference to
A thickness of the plasma oxide film 17 is 1 to 100 μm. Preferably, the thickness of the plasma oxide film 17 is 10 to 20 μm. If the thickness is less than 1 μm, sufficient energy cannot be obtained to generate the α-phase, then the α-phase would not be generated or it would be difficult to generate the α-phase. Accordingly, sufficient strength of the film cannot be obtained. If the thickness of the plasma oxide film 17 is more than 100 μm, the degree of roughness of the film is increased and gas sealability of the film would be lost.
Next, the plasma oxidation treatment will be explained.
In the plasma oxidation treatment, a degreasing process, a rough washing process, a finish washing process, a plasma oxidation process, a washing process, and a drying process are performed in an order described above.
In the degreasing process, for example, the surface of the piston is washed with use of an alkaline solution for removing a working oil or the like adhered on the surface of the piston. In the rough washing process, for example, ultrasonic cleaning is conducted with use of a detergent. In the finish washing process, for example, ultrasonic cleaning is conducted with use of a deionized water (or an ultra pure water). After the finish washing process, a mask is formed on the surface of the piston where the plasma oxide film is not to be formed. In addition, in a case that the plasma oxide film is to be formed on entire surface of the piston, it is not needed to form the mask.
In the plasma oxidation process, the piston is infiltrated in a treating liquid as a work, and the plasma oxidation process is performed. Thus, the plasma oxide film is formed. In this case, the treating liquid is a weak alkaline electrolytic solution containing water as a main component and further containing following additions on the basis of the water: (1) 1 to 10 g/l of sodium phosphate (Na3PO4); (2) 1 to 20 g/l of the water of sodium silicate (Na2SiO3); (3) 1 to 10 g/l of the water of sodium hydroxide (NaOH); and (4) 1 to 30 ml/l of hydrogen peroxide solution (containing 30% of H2O2). In the plasma oxidation process, the plasma oxide film can be formed by supplying pulsed alternating current of high current density in the treating liquid described above.
In the washing process, for example, ultrasonic cleaning is performed with use of a deionized water (or an ultra pure water). In the drying process, a cleaning liquid (a deionized water or an ultra pure water) is evaporated.
Next, an example will be explained. Tests of the piston according to the example of the present invention will be explained in comparison with a comparative example with reference to drawing figures.
Next, the block-on-ring type abrasion tests will be explained. In the block-on-ring type abrasion tests, changes of friction coefficients of the test pieces with time were measured with use of an abrasion unit-testing machine. Then, the degree of wear of each test piece was measured. As the test piece corresponding to the piston according to the example of the present invention, an aluminum alloy (JIS A6061) treated by the plasma oxidation treatment (having the plasma oxide film of 10 μm in thickness) was utilized. As another test piece according to the comparative example, an aluminum alloy (JIS A6061) treated by the anodic oxidation treatment was utilized. Both test pieces according to the example and the comparative example were block shapes (rectangular solid) and had identical dimensions. As a mating part material (ring material) with the test pieces, high-carbon steel (JIS SUJ2) was utilized. The block-on-ring type abrasion tests were performed in an engine oil under the conditions: 15 to 60 kgf of load; constant sliding speed; and constant sliding distance.
With reference to
Next, the engine durability abrasion tests will be explained. In the engine durability abrasion tests, an engine in which the piston as a test piece was installed was operated for the test under the condition of constant rotational frequency and constant duration. After that, the piston was extracted from the engine. Then, the degree of wear at the piston ring groove portions of the piston was measured. As a piston according to the example of the present invention, a piston was utilized made of a cast aluminum alloy (JIS AC8A) with a piston ring groove portion (top ring groove) treated by the plasma oxidation treatment (thickness of the plasma oxide film was 10 μm). As a piston according to the comparative example, a piston was utilized made of a cast aluminum alloy (JIS AC8A) treated by the anodic oxidation treatment. Pistons according to the example and the comparative example had identical shape and dimensions. With reference to
Further, in the comparative example, surface roughness (average roughness at ten points) measured 16 Rz. On the other hand, in the example according to the present invention, surface roughness (average roughness at ten points) measured 5.5 Rz. Thus, according to the embodiment of the present invention, the piston showed superior degree of smoothness of the surface in comparison with those of conventional pistons.
According to an aspect of the present invention, a piston is made of a material selected from any one of aluminum, an aluminum alloy, magnesium, and a magnesium alloy. An entire surface or a predetermined portion of the surface of the piston is covered with a plasma oxide film.
According to a further aspect of the present invention, a piston is made of a material selected from either one of aluminum and an aluminum alloy. An entire surface or a predetermined portion of the surface of the piston is covered with a plasma oxide film containing α-alumina.
According to a further aspect of the present invention, the surface of the piston is covered with the plasma oxide film, thus enhancing the properties required of the piston in terms of aspects such as abrasion resistance and low friction. Accordingly, for example, when the piston is utilized for an engine, a desired engine output property can be obtained over a protracted period. Further, because the piston is covered with the plasma oxide film, the piston can have an abrasion resistance property without the need for filtration of the resin or the like onto the plasma oxide film. Accordingly, the piston can also have an outstanding seizure resistance. Further, because the surface of the piston is covered with the plasma oxide film, smoothness of the film can be improved and the degree of surface roughness reduced. Accordingly, for example, when the piston is utilized for an engine, a desired engine output property can be obtained after a short trial period.
According to a further aspect of the present invention, by covering the piston ring groove portion with the plasma oxide film, abrasion resistance of the piston groove portion can be improved. This makes it possible to place the piston ring groove closer to a combustion chamber when the piston is utilized for an engine. Accordingly, it becomes possible to enhance combustion efficiency of the engine, and this in turn leads to a further improvement in fuel economy, further miniaturization and further reductions in weight. In other words, a fuel gas that has entered a clearance defined by three surfaces, the piston, the piston ring, and the cylinder, can be exhausted without being combusted by plug ignitions. When the piston ring groove is positioned closer to the combustion chamber, the clearance can be reduced in size. Thus, the amount of fuel gas exhausted without being combusted decreases, and this leads to improvements in fuel economy.
According to a further aspect of the present invention, a skirt portion and a pin boss portion of the piston are covered with the plasma oxide film. Accordingly, the degree of friction can be reduced. When the piston is utilized for an engine, friction loss on the part of the engine can be decreased and this in turn leads to an improvement in the level of consumption of fuel by the engine.
The principles, preferred embodiment and mode of operation of the present invention have been described in the foregoing specification. However, the invention which is intended to be protected is not to be construed as limited to the particular embodiments disclosed. Further, the embodiments described herein are to be regarded as illustrative rather than restrictive. Variations and changes may be made by others, and equivalents employed, without departing from the spirit of the present invention. Accordingly, it is expressly intended that all such variations, changes and equivalents which fall within the spirit and scope of the present invention as defined in the claims, be embraced thereby.
Number | Date | Country | Kind |
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2004-332127 | Nov 2004 | JP | national |
The present application is a Continuation of U.S. application Ser. No. 11/271,942 filed on Nov. 14, 2005. Priority is claimed based on U.S. application Ser. No. 11/271,942 filed on Nov. 14, 2005, which claims priority to Japanese Patent Application 2004-332127, filed on Nov. 16, 2004, all of which is hereby incorporated by reference.
Number | Date | Country | |
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Parent | 11271942 | Nov 2005 | US |
Child | 12155293 | US |