JP2013083003A - Hardening treatment method of liner surface part of cast iron cylinder block for internal combustion engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a hardening treatment method of a liner surface part of a cast iron cylinder block as an engine component.SOLUTION: In the hardening method of the liner surface part of the cast iron cylinder block for an internal combustion engine, an absorbent 10 in which graphite powder is diluted with a solvent such as a thinner is coated on a coating film of the liner surface part 26 of an inner wall of the dried cylinder block 25 and MC-based carbide is sintered during laser or electron beam irradiation. By promoting the diffusion of metal powders on a cast iron base material, an alloy layer 22 is formed on the liner surface part 26 of the inner wall of the cylinder block 25.

Description

  The present invention relates to a method for curing a liner surface portion of a cast iron cylinder block, which is a part that requires wear resistance, such as a transportation machine field or a machine structure field, such as an engine or a driving component.

  In recent years, fuel properties of low quality oil have deteriorated due to heavy crude oil, increased demand for light oil, changes in petroleum refining methods, etc., due to hard particles, sulfur content, fuel residue, etc. contained in fuel Internal combustion engine components are subject to wear. In order to cope with such a situation, for example, as a technique for improving the wear resistance of an integral FCD (dug tile cast iron) engine part mainly used in a diesel engine, a ring groove portion is hardened by using a laser. Laser hardening technology (for example, refer to Patent Document 1), induction hardening technology (for example, refer to Patent Document 2), chrome plating processing technology, and the like are known and widely applied.

JP-A 61-149424 Japanese Patent Laid-Open No. 7-119831

  However, the hardness of the hardened portion applied by the laser hardening technique or the induction hardening technique is only about 600 Hv to 800 Hv. Further, the structure of the quenched portion is not completely uniform, and a structure such as martensite, bainite, and retained austenite is mixed, resulting in a large variation in hardness. Further, the engine combustion temperature is easily transmitted to the top ring groove, and when the temperature is about 150 ° C. or higher, the quenched structure is tempered, and the hardness is reduced by about 100 Hv to 200 Hv. Furthermore, when the material of the engine component is easily corroded cast iron, the engine component is corroded by sulfur or the like contained in the combustion gas. For the above reasons, engine parts are worn by long-term use. Especially in engine parts for internal combustion engines, if the upper and lower gaps become larger due to wear, the engine parts must be replaced when a certain amount of wear is reached. There is a cost. Also, laser quenching cannot be performed very deeply because many fine cracks are generated when the quenching depth is about 300 μm or more. On the other hand, induction hardening is possible up to a quenching depth of about 800 μm, but the heat treatment distortion is large and post-processing such as grinding is required.

  Further, in the surface hardening in the chrome plating process, the hardness of the plated portion is about 800 Hv to 1000 Hv and the wear resistance is excellent, but it is very expensive. Moreover, since hexavalent chromium is included in the plating treatment liquid, it is not preferable in view of the influence on the environment. Accordingly, the present invention has been made in view of the above circumstances, and an object of the present invention is to propose a surface hardening method for improving the life of a component by coating the surface of an engine component with an alloy layer having excellent wear resistance. .

  The problem to be solved by the present invention is as described above. Next, means for solving the problem will be described.

  In claim 1, a coating film is formed by applying a mixture of metal powder, binder and solvent to the liner surface portion (26) which becomes the piston sliding portion of the cast iron cylinder block (25) for the internal combustion engine. The coating film is dried, and the coating film is irradiated with a laser or an electron beam to sinter and diffuse the metal powder, thereby generating MC-based carbides in the cylinder block (25), and In a method of curing a liner surface portion of a cast iron cylinder block for an internal combustion engine in which carbide is joined to a cast iron base material, graphite is coated on the liner surface portion (26) of the inner wall of the dried cylinder block (25). An absorbent (10) obtained by diluting the powder with a solvent such as thinner is applied and coated, and upon irradiation with the laser or electron beam, the MC carbide is sintered, and the metal powder is cast. By promoting the diffusion of the base material, the liner surface portion of the inner wall of the cylinder block (25) to (26) and forms an alloy layer (22).

  According to a second aspect of the present invention, in the method of hardening a liner surface portion of a cast iron cylinder block for an internal combustion engine according to the first aspect, the metal powder is a vanadium powder, a tungsten powder, or a chromium powder. .

  As effects of the present invention, the following effects can be obtained.

According to the present invention, a high hardness alloy layer can be easily formed on the liner surface portion (26) of the cast iron cylinder block (25) for an internal combustion engine.
This makes it possible to prevent aggressive wear due to combustion residues such as carbon.

The figure which shows the manufacturing process which concerns on an example of a piston in engine parts. The model figure similarly applied to the piston of a partial cross section.

The principal part expanded sectional view of FIG. The principal part sectional drawing which shows an example of a cylinder head made from cast iron typically.

The Z section enlarged view of FIG. The figure which shows the liner surface part of the cylinder block made from cast iron of this invention.

  Next, embodiments of the invention will be described. First, the process which applied the surface hardening method of a metal member to manufacture of the cast iron piston for internal combustion engines is demonstrated using FIG.1, FIG.2 and FIG.3.

<Casting and machining process>
After casting the cast iron melt into the mold and casting the piston 1 made of FCD (dug tile cast iron), the piston ring groove is cut to form the ring grooves 3 and 4.

<Formulation / application process>
First, a predetermined amount of several kinds of metal powder is weighed and blended. Next, the alloy powder is mixed using a ball mill or the like so that the metal powder is evenly dispersed. A predetermined amount of a solvent is added to the alloy powder and further mixed to uniformly disperse the alloy powder and the solvent. Then, the binder is added therein and stirred sufficiently so that the whole becomes a uniform mixture. Next, a mixture obtained by mixing the alloy powder, resin, and solvent obtained as described above is applied to the ring groove portions 3 and 4 by using an injection nozzle (not shown). At the time of application, the piston 1 is rotated at a constant speed to form a uniform powder alloy layer (thickness: 200 to 400 μm). After forming the powder alloy layer, the solvent is sufficiently dried by leaving it at room temperature. As said metal powder, it is preferable to use the metal which produces | generates very hard carbide | carbonized_material (MC type carbide), such as Cr, V, W, Mo, Ti, for example, but as a metal which forms other hard alloys, alumina , TiN, TiO2, CrN, zirconia, SiC, TiC or the like may be used to form the powder alloy layer.

  The resin is preferably a phthalic acid resin or alkyd resin that can be cured at room temperature, but is not particularly limited thereto. As the solvent, thinner, toluene, xylene or alcohols such as methanol, ethanol, and propanol can be used, and may be appropriately selected in consideration of drying speed and safety.

  In addition, as an example, the process of adding a binder later to the mixture of metal powder and solvent as described above is given as an example, but as a process of adding and blending metal powder in the mixture of solvent and binder It doesn't matter. In order to obtain the effects of the present invention, the thickness of the powder alloy layer is preferably about 200 to 400 μm, but is not particularly limited thereto. In addition, not only a mixture of a plurality of kinds of metal powders, but also a single metal powder may be used. In order to accelerate solvent drying, the object to be coated may be placed in a drying furnace or the like to shorten the drying time.

<Absorbent application process>
On the powder alloy layer, the laser absorbent 10 is applied using an injection nozzle so as to have a film thickness of about 5 μm to 15 μm according to the laser wavelength. When applying, the piston 1 is rotated at a constant speed so as to form a uniform film. After the coating is formed, the solvent is sufficiently dried by leaving it at room temperature. In this embodiment, a graphite film is formed on the powder alloy layer using a laser absorbent 10 obtained by diluting graphite powder with a solvent such as thinner. However, the present invention is not limited to this. You may apply | coat the coating agent etc. which were made into the main components as an absorber. The diluent solvent may be thinner, toluene, xylene, or alcohols such as methanol, ethanol, propanol, etc., and may be appropriately selected in consideration of drying speed and safety.

<Alloying process>
As shown in FIGS. 2 and 3, the ring grooves 3 and 4 are irradiated with a laser or an electron beam at an appropriate output and scanning speed to sinter or melt the powder alloy layer, and the ring grooves 3 and 4 are 150 μm to 350 μm. The alloy layer 20 having a thickness of about is formed. Examples of the laser include a CO2 laser, a YAG laser, and a semiconductor laser. It is also possible to use an electron beam having higher energy than the laser. Thus, by applying the laser absorbent (graphite coating) 10 in the previous step, the laser beam 8 is efficiently absorbed on the powder alloy layer, whereby the powder alloy layer is heated, and the powder alloy layer and the powder alloy are heated. Sintering and melting at the interface between the layer and the metal base material (cast iron base material) such as a piston, and diffusion to the base material are promoted to form a strong and wear-resistant alloy layer on the surface of the metal base material In addition, the alloy layer can be bonded to a metal base material (cast iron base material). In this embodiment, a member made of FCD (dug tile cast iron) is used as the metal base material, but it is not particularly limited to this, and an aluminum alloy or the like may be used.

<Finishing>
In the ring grooves 3 and 4 of the piston 1 manufactured by the above steps, the surface of the alloy layer 20 is ground as necessary. By such a process, a piston having an alloy layer in the ring groove portions 3 and 4 can be manufactured.

  Next, a specific example of manufacturing the piston 1 will be described. First, Mo (molybdenum) powder is weighed and added to toluene, which is a solvent, and mixed using a ball mill apparatus. Subsequently, a predetermined amount of phthalic acid resin is added and stirred so that the whole becomes a uniform mixture. Next, while rotating the FCD piston in the circumferential direction, the above mixture is uniformly applied to the concave portion of the ring groove portion 3 using an injection nozzle so that the film thickness becomes about 300 μm to form a powder alloy layer. After forming the powder alloy layer, the solvent is sufficiently dried by leaving it at room temperature. Next, the laser absorbent 10 (mixture of graphite and thinner) is applied onto the powder alloy layer using an injection nozzle so as to have a film thickness of about 10 μm. When applying, the piston is rotated in the circumferential direction at a constant speed so as to form a uniform film. After the coating is formed, the solvent is sufficiently dried by leaving it at room temperature. Then, as shown in FIGS. 2 and 3, when the ring groove portion 3 is irradiated with the laser beam 8 with a CO 2 laser and, for example, the alloy layer 20 is formed on the upper surface of the ring groove portion 3, the laser beam 8 is emitted from the condenser lens 5. Then, the piston 1 is rotated to form the alloy layer 20 around the entire groove while irradiating the upper surface with the incident angle α formed by the reflecting mirror 6. Subsequently, when the alloy layer 20 is formed on the lower surface of the ring groove 3, the piston 1 may be turned upside down and irradiated with the laser beam 8. However, the incident angle α of the laser beam 8 is changed for irradiation. May be. Here, in this embodiment, when forming the alloy layer 20 on both side surfaces of the ring groove portion 3 in particular, as shown in FIG. 2, the laser beam 8 has an incident angle α, and on the powder alloy layer of the groove. Since the corner portion 12 is masked and irradiated through the shielding plate 9 coated with the same graphite as the applied laser absorber 10, it is necessary to peel off the laser absorber 10 at the corner portion 12 and adjust its thickness. In addition, the alloy layer 20 can be formed only in the wear region 11, the corner portion 12 is not melted, and defects such as cracks due to melting can be prevented. In this way, a piston in which the alloy layer 20 was formed in the wear region 11 of the ring groove 3 was produced.

<Abrasion resistance evaluation method>
Under the same production conditions as in the above process, an alloy layer 20 is formed on a ductile cast iron test piece (30 × 100 (mm)), the surface hardness is measured with a Vickers hardness tester, and the wear resistance is evaluated. Went. As described above, in the test piece in which the alloy layer 20 was formed using the mixed powder of Mo (molybdenum) and C (carbon), the Vickers hardness was about 2000 Hv. It was confirmed that an alloy layer 20 having a hardness of about 6 times that of the base material, ductile cast iron (Vickers hardness: 300 Hv to 350 Hv), was obtained.

<Analytical method of alloy layer>
As a result of analyzing the interface part between the alloy layer 20 and the test piece which is a cast iron base material using EDX (energy dispersive X-ray fluorescence analyzer), Mo (molybdenum) is distributed in a gradient manner. I confirmed. That is, it was confirmed that the alloy layer 20 was joined to the cast iron base material. It was also confirmed that Mo was combined with C using an X-ray diffractometer to produce MoC (molybdenum carbide), which is an example of a ceramic alloy having a high hardness and a high melting point.

  By such a process, that is, the metal powder, the binder and the solvent are mixed, and the mixture is uniformly applied to the surface of the metal base material to form a coating film (powder alloy layer). Alternatively, the surface hardening method of the present invention in which the alloy layer 20 is formed on the surface of the metal base material by irradiating an electron beam to sinter, melt, and diffuse, and the alloy layer 20 is joined to the metal base material. By applying to the manufacture of members, for example, MC type carbides such as MoC and VC are finely and uniformly dispersed on the ring groove surface portion of an FCD piston, and a high-hardness alloy layer having a hardness of about 1000 to 3000 Hv is formed. It can be formed easily. As a result, the wear resistance or heat resistance is drastically improved, and aggressive wear due to combustion residues such as carbon can be prevented. Further, even when an expensive metal alloy is used, since only necessary portions are used, the amount used is extremely small and economical.

  In the case of steel materials, the hardness is reduced by tempering at 150 ° C. or higher. However, special carbides such as the above-mentioned MoC have a high melting point and are difficult to agglomerate and coarsen even at high temperatures. Therefore, a decrease in the hardness of the ring groove surface due to the temperature increase of the piston ring groove portions 3 and 4 during engine operation is prevented.

  Furthermore, corrosion such as sulfur can be prevented by forming on the surface a ceramic alloy as described above that is more resistant to corrosion than steel materials.

  In addition, the induction hardening of the conventional method requires tempering and grinding after quenching. On the other hand, in the present invention, after the ring groove portion 3 is cut, the alloy layer 20 having a thickness of 100 μm to 300 μm is uniformly formed on the surface thereof, so that the tempering can be omitted and the post-processing can be eliminated. Can be reduced.

  Next, an example in which the metal member surface hardening method is applied to a cast iron cylinder head for an internal combustion engine will be described with reference to FIGS.

  The cylinder head 15 was produced under the same production conditions as described above except that a mixed powder of V (vanadium) and C was used as the metal powder. As shown in FIG. 5, an intake valve 16 and an exhaust valve 17 are supported on the cast iron cylinder head 15 via a valve stem 18 so as to be slidable in the vertical direction. Based on the manufacturing method of the present invention, an alloy layer 21 having a film thickness of 150 μm to 350 μm was formed on the valve seat portion 19 serving as a sliding portion of the cylinder head 15. It was confirmed that V was distributed in an inclined manner and VC (vanadium carbide) was generated at the interface portion between the alloy layer 21 and the cylinder head 15 as the cast iron base material. VC is known as a ceramic alloy (Vickers hardness: about 2500 to 2800 Hv) having high hardness, wear resistance and heat resistance like MoC described above, and is very effective in improving the wear resistance of sliding parts. It is. That is, as described above, the metal powder is heated and melted by the laser beam 8 to promote sintering and diffusion in the alloy layer 21 and at the interface portion between the alloy layer 21 and the cylinder head 15 that is the base material, thereby providing a valve seat. The valve seat integrated cylinder head 15 having the wear-resistant alloy layer 21 on the surface of the portion 19 can be manufactured.

  According to the cast iron cylinder head 15 manufactured by the above process, the valve seat portion 19 and the cast iron base material (cylinder head 11) can be integrated, so that the cylinder head 11 which is a cast iron base material. And the bonding strength at the boundary between the alloy layer 21 and the alloy layer 21 can be improved. That is, the bonding strength can be increased as compared with the conventional valve seat fitting type cast iron cylinder head.

  Next, the Example which applied the surface hardening method of the metal member to the liner surface part of the cast iron cylinder block for internal combustion engines is described using FIG.

  The cylinder block 25 was manufactured under the same manufacturing conditions as described above except that a mixed powder of W (tungsten) and C was used as the metal powder. As shown in FIG. 6, an alloy layer 22 having a film thickness of 150 μm to 350 μm was formed on the liner surface portion 26 serving as a sliding portion of the cast iron cylinder block 25 based on the manufacturing method of the present invention. W (tungsten) is distributed in an inclined manner and WC (tungsten carbide) is generated at the interface portion between the alloy layer 22 and the liner surface portion 26 of the cylinder block 25 which is a cast iron base material. It was confirmed. WC (tungsten carbide) is known as a ceramic alloy (Vickers hardness: about 2600-2800Hv) having high hardness, wear resistance and heat resistance, similar to the above-mentioned MoC and VC, and is extremely effective in improving wear resistance. It is effective. That is, as described above, the metal powder is heated and melted by the laser beam 8 to promote sintering and diffusion in the alloy layer 22 and at the interface portion between the alloy layer 22 and the liner surface portion 26 of the cylinder block 25 that is the base material. Thus, the cast iron cylinder block 25 having the wear-resistant alloy layer 22 on the liner surface portion 26 can be manufactured.

  In addition, although the method for forming an alloy layer having wear resistance and heat resistance on the metal member for an internal combustion engine has been described above, the alloy layer is similarly applied to the surface portion of the member that requires wear resistance for other purposes. It is also possible to improve wear resistance by forming.

DESCRIPTION OF SYMBOLS 1 Piston 3.4 Ring ring part 8 Laser beam 10 Laser absorber 15 Cylinder head 19 Valve seat part 20, 21, 22 Alloy layer 25 Cylinder block 26 Liner surface part

In claim 1, a coating film is formed by applying a mixture of metal powder, binder and solvent to the liner surface portion (26) which becomes the piston sliding portion of the cast iron cylinder block (25) for the internal combustion engine. The coating film is dried, and the coating film is irradiated with a laser or an electron beam to sinter and diffuse the metal powder, thereby generating MC-based carbides in the cylinder block (25), and carbides in hardening method of the liner surface portion of the cast iron cylinder block for an internal combustion engine to be bonded to the cast iron base material, on the coating of the liner surface portion of the inner wall (26) of the dried cylinder block (25), The metal powder is coated with an absorbent (10) obtained by diluting graphite powder with a solvent such as thinner, and the MC carbide is sintered at the time of irradiation with the laser or electron beam. By promoting the diffusion of the cast iron base material, the liner surface portion of the inner wall of the cylinder block (25) to (26) and forms an alloy layer (22).

Claims (2)

  A mixture of metal powder, binder and solvent is applied to the liner surface portion (26) which is the piston sliding portion of the cast iron cylinder block (25) for the internal combustion engine to form a coating film, and the coating film is dried. The coating film is irradiated with a laser or an electron beam to sinter and diffuse the metal powder, thereby generating MC-based carbides in the cylinder block (25), and using the MC-based carbides as a cast iron base material. In the method for curing a liner surface portion of a cast iron cylinder block for an internal combustion engine to be joined, graphite powder is used as a solvent such as thinner on the coating film on the liner surface portion (26) of the inner wall of the dried cylinder block (25). Applying and coating the absorbent diluted with (10), sintering the MC carbide during the laser or electron beam irradiation, and promoting the diffusion of the metal powder into the cast iron base material It makes the cylinder block (25) hardening method of the liner surface portion of the cast iron cylinder block for an internal combustion engine, characterized in that the liner surface portion (26) to form an alloy layer (22) of the inner wall of which.   The cast iron for an internal combustion engine according to claim 1, wherein the metal powder is a vanadium powder, a tungsten powder, or a chromium powder. Curing method for liner surface of cylinder block made of steel.

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