METHOD OF MANUFACTURING A SURFACE COMPOSITE REINFORCED MEMBER

Abstract: A surface composite reinforced member is manufac­ tured by, in order: applying a mixture of a reinforcing material and a solvent to the inner surface of a mold cavity of a casting mold; then drying the resulting layer of reinforcing material; then pouring a mass of molten metal into the mold cavity; and then solidifying this mass of molten metal under pressure. Thus the reinforcing material layer which has dried on the surface of the mold cavity is penetrated under pressure by the molten metal to form a composite reinforced surface portion of the resulting casting. Further, the mixture of reinforcing material and solvent may include an inorganic binder which is solidified by the drying process, so as to aid with the adherence of the reinforcing material to the wall of the mold cavity. The reinforcing material may be silicon carbide or silicon nitride whiskers, and the binder may be colloidal alumina or colloidal silica.

Description: METHOD OF MANUFACTURE FOR SURFACE COMPOSITE REINFORCED MEMBER BACKGROUND OF 1lIE INVENTION The present invention relates to a method of manufacture for a member which is partially reinforced by composite material, and more particularly to a method of manufacture for a member in which a portion proximate to the surface thereof, only, is reinforced by addition of reinforcing material, so as to be composed of composite material. Various types of composite materials are known in which small pieces, such as fibers, whiskers, or particles, of reinforcing material such as for example silicon carbide or silicon nitride are dispersed within a matrix of matrix metal such as for example aluminum alloy. These materials have great advantages over the original alloy or matrix metal with regard to certain characteristics such as strength and wear resistance, and more specifically with regard to tensile and bending strength, heat resistance, and wear and scuffing resistance; and accordingly many researches have been recently conducted with regard to the practicability of fabricating various automobile and aircraft parts from such composite materials. However, with regard to certain other characteristics such as wear on a cooperating member and cost and ease of machining and post finishing, the original alloy or matrix metal has advantages over the composite reinforced material, and accordingly in the case of some applications the desirability has been recognized of reinforcing only selected portions of metallic members with reinforcing material, the remaining portions being left as composed substantially of matrix metal without any composite reinforcement. For example, in the case of an engine piston, it is recognized that it is desirable to reinforce by the addition of fibers or the like the crown and side and skirt portions of the piston, which are the parts thereof which are most subject to high temperatures and pressures and thermal abrasion and also are most subject to wear by rubbing against mating surfaces, while on the other hand it is recognized that it is desirable to fabricate the remainder of the piston out of non reinforced metal only. In many cases, the parts of a member which are thus to be composite reinforced are surface parts thereof. Now, with regard to methods for fabricating a member with parts thereof reinforced by composite reinforcing material, there are various conventionally known methods such as diffusion joining, permeation, sintering, and high pressure casting. Of these methods, the high pressure casting method is the most sophisticated. In this method, as conventionally practiced, first a mass of the reinforcing material is shaped into a formed shape or block of the general configuration of the part of the member to be fabricated which is required to be reinforced by composite reinforcing material, and this formed shape of reinforcing material is placed within the mold cavity of a casting mold and is maintained by some means in an appropriate position therein. Then molten matrix metal is poured into said mold cavity so as to fill it, and is then pressurized to a high pressure by a mold plunger or the like within said mold cavity and is allowed to solidify therein while under said pressure, so that this applied pressure causes the molten matrix metal to penetrate into the interstices between the fibers or the particles of the reinforcing material formed shape, thus forming the portions of the finished member which correspond to the portions of the mold cavity which were occupied by the reinforcing material formed shape as composite reinforced portions, while leaving the remainder portions of the finished member which correspond to portions of the mold cavity which were not occupied by the reinforcing material formed shape as made only of matrix metal without any composite reinforcement. This high pressure casting method has the advantages that, even if the reinforcing material has poor wettability with regard to the matrix metal, very good bonding can be obtained between the reinforcing material and the matrix metal, and further that since no vacuum is employed no complicated and expensive equipment for creating a vacuum is required. However, the problem exists that it is necessary to form the reinforcing material into a formed shape before the casting process as explained above, and also that it is necessary to maintain this formed shape in a predetermined position in the mold cavity during the casting process, which can be very difficult. Especially in the particular case that it is desired to form certain portions of and proximate to the surface of the finished member as composite reinforced, which as explained above is often the case, the manufacture of such a formed shape of composite reinforcing material which in this case is required to be large and yet thin, and also the maintenance of this thin and extensive formed shape in place during the casting process, becomes very difficult. Especially, since in many cases as explained above the surface portions of the member to be fabricated are required to be composite reinforced in order to confer upon them improved heat and/or wearing resistance, in such a case, if a part of the presumably large yet rather delicate composite material formed shape should become distorted during the casting process so as to be moved even by a relatively small amount inwards from the side wall surface of the mold cavity, then this surface portion of the resulting member will lack composite reinforcement, and will accordingly be deficient with regard to heat and/or friction resistance, thus vitiating the object of composite reinforcement to a large extent. The thinner are the portions of the member to be fabricated that are required to be surface reinforced by composite material, the more aggravated does these problems of fabricating and emplacing the composite material formed shape in the casting mold become, and in the most severe cases it becomes extremely difficult to practice the high pressure casting method as conventionally performed as described above, in order to manufacture such a surface composite reinforced member. SUMMARY OF THE INVENTION Accordingly, it is the primary object of the present invention to provide a method of manufacturing such a surface composite reinforced member, which can avoid the above outlined difficulties. It is a further object of the present invention to provide a method of manufacturing a surface composite reinforced member, which utilizes the high pressure casting method, which can be easily and efficiently utilized, even when the portions of the member which are to be composite reinforced are quite thin and extensive surface portions. It is a further object of the present invention to provide a method of manufacturing a surface composite reinforced member, which, even when the portions of the member which are to be composite reinforced are quite thin and extensive surface portions, does not risk that such a formed shape of reinforcing material as described above should become displaced from its proper position proximate to the surface of the mold cavity of the mold during casting, and that thus in fact szme of the surface portions of the finished member which ought to be composite reinforced should not be. It is a further object of the present invention to provide a method of manufacturing a surface composite reinforced member, which utilizes the high pressure casting method, while avoiding the prior art requirement for forming the reinforcing material into a formed shape before casting. It is a further object of the present invention to provide a method of manufacturing a surface composite reinforced member, which utilizes the high pressure casting method, while avoiding the prior art requirement for maintaining said formed shape of reinforcing material in a predetermined position in the mold cavity of the mold during casting. It is a further object of the present invention to provide a method of manufacturing a surface composite reinforced member, in which the reinforcing material is positively and easily kept in its appropriate place during the casting process, without any difficult pre casting procedure. According to the most general aspect of the present invention, these and other objects are accomplished by a method of manufacture for a surface composite reinforced member, wherein in order: (a) a mixture of a reinforcing material and a solvent is applied to the inner surface of a mold cavity of a casting mold; (b) the resulting layer of reinforcing material is dried; (c) a mass of molten metal is poured into said mold cavity; and then (d) this mass of molten metal is solidified under pressure. According to such a method, the reinforcing material is made into a liquid like mixture by being mixed with the solvent (which may be water or alcohol or a mixture thereof), and then a layer of the reinforcing material is stuck or plastered on to the inner surface of the casting mold, against the portions thereof which are so positioned as to form the parts of the surface of the cast member which are intended to be composite reinforced by said reinforcing material intermingled with matrix metal. Then, after drying this reinforcing material layer, molten matrix metal into is poured the casting mold and is allowed to solidify under pressure. This pressurized molten matrix metal percolates into the interstices of the reinforcing material layer and forms together with said reinforcing material (which may be fibers, whiskers, particles, or the like) a composite reinforced material, the body of said composite reinforced material thus being located in just the part or parts of the cast member where it is required. This is accomplished without any need for forming the reinforcing material into a preformed shape before casting, and is practicable, even when and though the portions of the member which are to be composite reinforced are quite thin and extensive surface portions. Further, no risk is run of the reinforcing material which is to form the composite reinforcement of the reinforced parts of the finished member in combination with matrix metal becoming displaced from its desired position proximate to the surface of the mold cavity of the mold during casting, and that thus in fact some of the surface portions of the finished member which ought to be composite reinforced should not be. Further, the prior art requirement for maintaining the formed shape of reinforcing material in a predetermined position in the mold cavity of the mold during casting is avoided, because the reinforcing material is merely attached to the side surfaces of the casting mold, thus allowing the reinforcing material to be positively and easily kept in its appropriate place during the casting process, without any difficult pre casting procedure. Further, any difficult pre casting forming requirement for the reinforcing material is avoided. This means, as a whole, that the process of manufacture of the surface composite reinforced member can be accomplished cheaply and efficently, without the use of any vacuum equipment or the like; and because the high pressure casting method is used it is possible to thus form a surface composite reinforced member of arbitrary shape while providing very good bonding characteristics between the matrix material and the reinforcing material. Further, according to a more particular aspect of the present invention, these and other objects are more particularly and concretely accomplished by a method of the type described above, wherein further said mixture includes an inorganic binder which is solidified by the drying of step (b). According to such a method, the layer of reinforcing material stuck or plastered on to the inner surface of the casting mold may be further caused to be well and strongly stuck onto said inner surface, by adding this inorganic binder to the mixture of the solvent and the reinforcing material, before applying the layer of reinforcing material to the inner surface of the casting mold in step (a). Thus, in step (b) when the layer of reinforcing material is dried, the inorganic binder, which is solidified by this drying, helps with the adhesion of said reinforcing material layer. Further, according to another more particular aspect of the present invention, these and other objects are more particularly and concretely accomplished by such a method as described above, in the particular cases that one or more of the materials used are: for the reinforcing material, silicon carbide whiskers or silicon nitride whiskers, or short alumina silica type fibers, metallic fibers, or pitch carbon, whiskers of potassium titanate, etc.; for the matrix metal, aluminum alloy; and for the inorganic binder, if one is used, colloidal alumina or colloidal silica or waterglass. According to such a method, particularly good results are obtained. Further, according to a yet more particular aspect of the present invention, these and other objects are more particularly and concretely accomplished by a method of either of the two types specified above, wherein said application of said mixture of said reinforcing material and said solvent to the inner surface of said mold cavity of said casting mold in step (a) is performed by using a brush; or alternatively wherein said application of said mixture of said reinforcing material and said solvent to the inner surface of said mold cavity of said casting mold in step (a) is performed by spraying. According to such methods, either of which may be advantageously employed depending upon the type of solvent used, the type of inorganic binder used if any, and the type of reinforcing material used, the layer of reinforcing material may be quickly and easily yet accurately applied. BRIEF DESCRIPTION OF THE DRAWINGS The present invention will now be shown and described with reference to several preferred embodiments thereof, and with reference to the illustrative drawings. It should be clearly understood, however, that the description of the embodiments, and the drawings, are all of them given purely for the purposes of explanation and exemplification only, and are none of them intended to be limitative of the scope of the present invention in any way, since the scope of the present invention is to be defined solely by the legitimate and proper scope of the appended claims. In the drawings, like parts and features are denoted by like reference symbols in the various figures thereof, and: Fig. 1 is a schematic axial longitudinal sectional view through a lower part of an apparatus which is being used in the practice of a first preferred embodiment of the method of manufacture for a surface composite reinforced member according to the present invention, said member be ing an engine piston, showing the apparatus during the practice of a first stage of said method in which reinforcing material is being applied to the inner side surface of a mold cavity; Fig. 2 is a schematic axial longitudinal sectional view of both the lower and upper parts of the same apparatus as shown in Fig. 1, showing the apparatus during the practice of a second stage of said first embodiment of this method, in which matrix metal is being pressurized in said mold cavity; ; Fig. 3 is a schematic axial longitudinal sectional view through part of an apparatus which is being used in the practice of a second preferred embodiment of the method of manufacture for a surface composite reinforced member according to the present invention, said member being a vehicle wheel, showing the apparatus during the practice of the first stage of said method in which reinforcing material is being applied to selected side surfaces of certain mold members of said apparatus which are currently separated; and Fig. 4 is a schematic axial longitudinal sectional view of the same apparatus as shown in Fig. 3, showing the apparatus during the practice of the second stage of said second embodiment of this method, in which matrix metal is being pressurized in a mold cavity defined by the cooperation of said mold members when they are brought together. DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will now be described with reference to two preferred embodiments thereof, and with reference to the appended drawings. THE FIRST PREFERRED EMBODIMENT Fig. 1 shows in approximate axial longitudinal section the lower part of an apparatus 1 which is a casting device, and which was being used in the practice of the first stage of a first preferred embodiment of the method of manufacture for a surface composite reinforced member according to the present invention. In this figure, the reference numeral 2 denotes a substantially cylindrical mold cavity formed in a lower mold member 3 of the casting device 1. This mold cavity 2 was of an appropriate shape to define the outer surface of an engine piston which was to be manufactured. In fact, the diameter of the mold cavity 2 was 90 mm, and the depth thereof was 100 mm, in order to form a piston of substantially these dimensions for a four cylinder four stroke diesel engine of 2200 cc cylinder capacity, the crown, wall, and skirt surface portions of which were desired to be reinforced with fibers, so as to be composed of composite material. First, as the first stage in the first preferred embodiment, a mass of silicon carbide whiskers which were of fiber diameters 0.2 to 0.5 microns and fiber lengths 20 to 50 microns were added to an aqueous solution of 15% of colloidal silica, which was used as an inorganic binder. The volumetric concentration of the silicon carbide whiskers was about 30%. The liquid mixture was stirred until substantially homogenous, and then using a paintbrush a layer 6 of the mixture was painted on the inside wall surfaces and the bottom surface of the mold cavity 2 of the lower mold 3, this mixture layer 6 having a thickness of approximately 1.2 mm. At this time, the lower mold 3 was kept heated to a temperature of about 120 to 1500C. Then this liquid mixture was dried, so as to leave a layer 7 (see Fig. 2) of silicon carbide whiskers covered with and mixed with dried inorganic binder of colloidal silica (which of course solidified) stuck to the wall and bottom surfaces of the mold cavity 2. Next, as the second stage, as shown in Fig. 2 a mass 8 of molten aluminum alloy, of JIS standard AC8A, at 7400C, was poured into the mold cavity 2 of the lower mold 3, and then as shown in Fig. 2 an upper mold member 4 was pressed against the top surface of the lower mold 3, and an inner mold or male mold punch or former 5 was inserted downwards through a central hole in this upper mold member 4 and was pressed downwards into the mold cavity 2 by a pressure maintaining means such as a ram device not shown in the figure, so as to pressurize the molten aluminum alloy mass 8 in said mold cavity 2 to a pressure of approximately 2 1500 kg/cm . The outer surface of the male mold punch 5 was so shaped as to properly define the desired inner surface shape of the piston which was desired to be manufactured, and the proper amount of molten aluminum alloy 8 in the mold cavity 2 was used for the male mold punch 5 to enter into the mold cavity 2 for the correct distance to properly shape the piston. This pressure was maintained for approximately 120 seconds, until the molten aluminum alloy mass 8 had entirely solidified, and then the upper mold 4 and the male mold punch 5 were raised, and the formed piston preform was pushed out in tle upwards direction from the mold cavity 2 by means of a knock out pin 9 which was provided as extending through the bottom of the lower mold 3. Thus the crown and the side wall and the skirt surface portions of the resulting piston preform were formed of a reinforced material, produced by the molten aluminum alloy percolating between the interstices of the layer 7 of silicon carbide whiskers under pressure, and thus composed of silicon carbide whiskers disposed within a matrix of aluminum alloy. These portions were sectioned and observed under an electron microscope. It was observed that the silicon carbide whiskers lay in substantially random alignment in two dimensions, extending generally parallel to the contiguous surface, and the volumetric proportion of these reinforcing silicon carbide whiskers was approximately 12%. Further, from these reinforced portions of the piston preform test samples were cut, and the elasticity, thermal conductivity, thermal coefficient of expansion, and tensile strength of these test samples were measured, as a result of which it was found that the thermal conductivity and the thermal coefficient of expansion of these test samples were reduced as compared with those of test samples made of pure aluminum alloy of the same kind as the matrix metal, while the elasticity and the tensile strength of these test samples were increased, again as compared with those of said test samples made of pure aluminum alloy of the same kind as the matrix metal. Thus, it will be seen that according to this first preferred embodiment of the method of manufacture for a surface composite reinforced member according to the present invention it is possible to manufacture an engine piston which has good thermal properties such as high thermal insulating capability and low thermal expansion characteristic, as well as having good resistance to wear, high resistance to heat, high strength, and good elasticity, due to the surface reinforcement of the crown, wall, and skirt portions thereof. According to this method of fabrication of an engine piston as described above, a composite reinforced material mass was located in just the part or parts of the cast piston preform member where it is required, without any need for forming the silicon carbide whiskers into a preformed shape before casting. This is practicable, even when the portions of the piston preform member which are to be composite reinforced are quite thin and extensive surface portions, such as surface portions very close to its crown and side wall and skirt portions. Further, no risk is run of the silicon carbide whisker reinforcing mass becoming displaced from its desired position during casting. Further, there is no requirement for maintaining any formed shape of the silicon carbide whisker mass in a predetermined position in the mold cavity of the mold 3 during casting, because these whiskers are merely attached to the side surfaces 2 of the casting mold 3. The silicon carbide whiskers are positively and easily kept in their appropriate place during the casting process, without any difficult pre casting procedure. Thus, as a whole, the process of manufacture of the surface composite reinforced piston preform member is accomplished cheaply and efficently, without the use of any vacuum equipment or the like; and because the high pressure casting method is used it is possible to thus form a surface composite reinforced piston preform member in any arbitrary shape. Further, the layer 7 of silicon carbide whiskers is very well and strongly stuck onto said inner surface of the cavity of the mold 3, by adding the colloidal silica inorganic binder to the mixture of the silicon carbide whiskers and the water, before applying the layer of silicon carbide whiskers to the side surfaces of the casting mold cavity. Thus, when the layer of silicon carbide whisker reinforcing material is dried, the colloidal silica inorganic binder, which is solidified by this drying, helps with the adhesion of said reinforcing silicon carbide whisker layer. THE SECOND PREFERRED EMBODIMENT Figs. 3 and 4 broadly show, in a similar fashion to Figs. 1 and 2 respectively, the practice of a second preferred embodiment of the method of manufacture for a surface composite reinforced member according to the present invention. In Fig. 3 there is shown a part of a axial longitudinal section of an apparatus 11 which is a casting device, and which was being used in the practice of the first stage of this second preferred embodiment. In fact, this figure shows only the left hand part of the longitudinal section of the casting device, which is rotationally symmetrical about an axis 16. This casting device 11 comprises: a lower mold member 13 through the center of which there is provided a pressurizing punch 18, which also serves as a knock out pin as will be seen shortly; an upper mold member 14 which can be brought vertically downwards towards said lower mold member 13 or vertically upwards away therefrom, as desired; and a plurality of side mold members 15, only one of which can be seen in the figure and which are provided in plurality all around the upper and lower mold members 13 and 14, each of which can be brought horizontally towards the axis 16 or away therefrom, as desired. In Fig. 3, the upper mold member 14 is shown as raised away from the lower mold member 13, and the side mold member 15 is shown as brought away from the axis 16 and away from the lower and upper mold members 13 and 14, so as to open the casting mold 11 up. On the other hand, in Fig. 4, the upper mold member 14 is shown as lowered down towards the lower mold member 13, and the side mold member 15 is shown as approached towards the axis 16 and towards the lower and upper mold members 13 and 14 as are also in fact all the other side mold members which cannot be seen in the figure, so as to close up the casting mold 11; and in this position the upper and lower mold members 13 and 14 and the plurality of side mold members 15 defined a mold cavity 12 of an appropriate shape to define the outer surface of a vehicle wheel which was to be manufactured, certain surface rim portions of which were desired to be reinforced with fibers, so as to be composed of composite material. First, as the first stage in the second preferred embodiment, a mass of silicon nitride whiskers which were of average fiber diameter 1.3 microns and average fiber length 180 microns were added to an aqueous solution of 10% of colloidal alumina, which was used as an inorganic binder. The volumetric concentration of the silicon nitride whiskers was about 25%. The liquid mixture was stirred until substantially homogenous, and then using a paintbrush a layer 20 of the mixture was painted on the inside surfaces of the side mold portions 15 and the outer or wheel rim defining portions of the lower and upper mold portions 13 and 14, this mixture layer 20 having a thickness of approximately 2.0 mm. At this time, the mold portions 13, 14, and 15 were kept heated to a temperature of about 1200C. Then this liquid mixture was dried, so as to leave a layer 21 (see Fig. 4) of silicon nitride whiskers covered with and mixed with dried inorganic binder of colloidal alumina stuck to the various wall surfaces of the mold portions 13, 14, and 15. Next, as the second stage, the casting device 11 was partially closed up by the plurality of side mold portions 15 being all moved horizontally so as to be approached towards the central axis 16 of the apparatus, so that as shown in Fig. 4 by the cooperation of all these members a mold cavity 12 circularly symmetrical around the axis 16 of the shape of the vehicle wheel which was desired to be formed was defined, with the above mentioned layer 21 of silicon nitride whiskers all around the portion of said mold cavity 12 which defined the rim portion of said vehicle wheel. Then a mass 19 of molten aluminum alloy, of JIS standard AC4C, at 7300C, was poured through the gap between the upper mold member 14 (which was still in the raised position) and the side mold members 15 into the thus defined mold cavity 21, and then the casting mold device 11 was fully closed up by the upper mold portion 14 being lowered downwards towards the lower mold portion 13 and the side mold portions 15. Then the pressurizing punch 18 was pushed upwards through the central hole 17 in the lower mold member 13 by a pressure maintaining means such as a ram device not shown in the figure, so as to pressurize the molten aluminum alloy mass 19 in said mold cavity 12 to a pressure of approximately 1200 kg/cm2. The proper amount of molten aluminum alloy 19 in the mold cavity 12 was used for the mold punch 18 to enter into the hole 17 for the correct distance to properly shape the central portion of the wheel. This pressure was maintained for approximately 60 seconds, until the molten aluminum alloy mass 19 had entirely solidified, and then the upper mold portion 14 was raised and the side mold portions 15 were brought horizontally away from the lower mold portion 13, and the formed wheel was pushed out in the upwards direction from the lower mold 13 by means of the punch 18 being raised through the hole 17. Thus the rim portions of the resulting vehicle wheel were formed of a reinforced material, produced by the molten aluminum alloy percolating between the interstices of the layer 20 of silicon nitride whiskers under pressure, and thus composed of silicon nitride whiskers disposed within a matrix of aluminum alloy. These portions were sectioned and observed under an electron microscope. It was observed that the silicon nitride whiskers lay in a layer inwards from the surface of the wheel rim approximately 1.5 mm thick in substantially random alignment in two dimensions extending generally parallel to the contiguous surface, and by measuring the specific gravity of a sample portion of this layer it was determined that the volume proportion of these reinforcing silicon nitride whiskers was approximately 12%. Thus, it will be seen that according to this second preferred embodiment of the method of manufacture for a surface composite reinforced member according to the present invention it is possible easily and efficiently to manufacture a vehicle wheel in which the rim portions are reinforced with silicon nitride whiskers, and which thus has good resistance to wear, high resistance to heat, high strength, and good elasticity, while still being thin and light, due to the surface reinforcement of said rim portions thereof; and this is done without any requirement for a surface treatment such as the application of a coating to the surface of these wheel rim portions. Although the present invention has been shown and described with reference to several preferred embodiments thereof, and-in terms of the illustrative drawings, it should not be considered as limited thereby. Various possible modifications, omissions, and alterations could be conceived of by one skilled in the art to the form and the content of any particular embodiment, without departing from the scope of the present invention. For example, although in the shown two preferred embodiments the application of the mixture including the reinforcing material to the inside surfaces of the mold cavity was performed by using a brush, in an alternative embodiment spraying or the like could also be used. Therefore it is desired that the scope of the present invention, and of the protection sought to be granted by Letters Patent, should be defined not by any of the perhaps purely fortuitous details of the shown embodiments, or of the drawings, but solely by the scope of the appended claims, which follow.

Claims: WHAT IS CLAIMEI, IS: 1. A method of manufacture for a surface composite reinforced member, wherein in order: (a) a mixture of a reinforcing material and a solvent is applied to the inner surface of a mold cavity of a casting mold; (b) the resulting layer of reinforcing material is dried; (c) a mass of molten metal is poured into said mold cavity; and then (d) this mass of molten metal is solidified under pressure. 2. A method according to claim 1, wherein further said mixture includes an inorganic binder which is solidified by the drying of step (b). 3. A method according to claim 1 or 2, wherein said reinforcing material is silicon carbide whiskers. 4. A method according to claim 1 or 2, wherein said reinforcing material is silicon nitride whiskers. 5. A method according to claim 3, wherein said inorganic binder is colloidal silica. 6. A method according to claim 4, wherein said inorganic binder is colloidal alumina. 7. A method according to claim 3, wherein said molten metal is aluminum alloy. 8. A method according to claim 4, wherein said molten metal is aluminum alloy. 9. A method according to claim 1 or 2, wherein said application of said mixture of said reinforcing material and said solvent to the inner surface of said mold cavity of said casting mold in step (a) is performed by using a brush. 10. A method according to claim 1 or 2, wherein said application of said mixture of said reinforcing material and said solvent to the inner surface of said mold cavity of said casting mold in step (a) is performed by spraying.

Inventors: DONOMOTO, TADASHI, TANAKA, ATSUO, TATEMATSU, YOSHIAKI
Applicants: TOYOTA JIDOSHA KABUSHIKI KAISHA
Application year: 1983
Main classification: B22D19
IPC codes: B22D19, C22C47, B60B3, F02F3