Patent Publication Number: US-6909185-B1

Title: Composite material including copper and cuprous oxide and application thereof

Description:
TECHNICAL FIELD 
     The present invention relates to a composite material with low thermal expansivity and high thermal conductivity, to a process for production thereof, and to applications thereof such as semiconductor devices. 
     BACKGROUND ART 
     Power electronics include a technique which deals having a with power electronic devices to convert and a control electric power and energy, power electronic devices used in on-off mode, and a power conversion system as its application technique. 
     Conversion of electric power calls for a variety of power semiconductors with switching capability. These semiconductors in practical use include rectifier diodes (with a pn Junction for current flow in only one direction), and thyristors, bipolar transistors, and MOSFETs (with a combination of pn junctions). Recently developed ones include insulated gate bipolar transistors (IGBT) and gate turn-off thyristors (GTO) which perform switching in response to gate signals. 
     These power semiconductors, evolve heat when energized. They tend to evolve more heat with increased capacity and speed. To protect them from deterioration and a reduced life due to the effects of heat they should be provided with a radiator which prevents temperature rise in the temperature device itself and in the vicinity thereof. A common material used for radiators is copper, which is inexpensive and has a high thermal conductivity (393 W/m). Unfortunately, copper is not suitable for the radiator of power semiconductor devices because it has a high thermal expansivity of 17×10 −6 /° C. and hence it does not solder well with silicon, whose thermal expansivity is 4.2×10 −6 /C. One way to address this problem is to make the radiator from molybdenum or tungsten which has thermal expansivity close to that of silicon or to interpose one of these materials between the radiator and the semiconductor element. 
     Power semiconductor elements are contrasted with electronic semiconductor elements. The latter are exemplified by integrated circuits (IC) consisting of electronic circuits integrally formed on a single semiconductor chip. They are classified into memory, logic, microprocessors, etc. according to their functions. A problem involved with recent electronic semiconductor elements is heat evolution, which increases as the degree of integration increases and the speed of operation increases. To make things worse, electronic semiconductor elements are contained individually in hermetic packages for isolation from the atmosphere to prevent failure and deterioration. Various types of packages including ceramic packages (in which each semiconductor element is fixed to ceramics through die bonding) and plastics packages (which are sealed with plastics) are in widespread use. A new development to meet requirements for high reliability and high speed operation is the multi-chip module (MCM) equipped with a plurality of semiconductor elements on a single substrate. 
     A plastics package is constructed such that the semiconductor element therein has its terminals connected to the lead frame through bonding wires and the entire assembly is sealed with plastics. Recent improvements made to cope with increasing heat evolution involve packages in which the lead frame functions to dissipate heat or which are provided with a radiator for heat dissipation. The lead frame or radiator for heat dissipation is usually made of copper having a high thermal conductivity. Unfortunately, malfunction can be anticipated because of the difference the thermal expansivity between copper and silicon. 
     By contrast, ceramics packages are constructed such that a semiconductor element is placed on a ceramic substrate having wiring printed thereon and the entire assembly is sealed with a metal or ceramics cap. The ceramic substrate is backed with a Cu—Mo or Cu—W composite material or a kovar alloy, which functions as a radiator. Ceramic materials with low thermal expansivity, high thermal conductivity, and good workability are required at a low production cost. 
     An MCM consists of a metal or ceramic substrate having thin film wiring formed thereon, a plurality of semiconductor elements (in the form of a bare chip) mounted thereon, a ceramic package containing the elements, and a sealing lid. The package is provided with a radiator or fin if it needs heat dissipation. The metal substrate is made of copper or aluminum. This device has the advantage of a high thermal conductivity, but also the disadvantage of a high thermal expansivity, which leads to poor matching with the semiconductor element. Therefore, the substrate of MCMs for high reliability is made of silicon or aluminum nitride (AIN). The radiator, which is bonded to the ceramic package, should be made of a material which has high thermal conductivity and also has low thermal expansivity for good matching with the package material. 
     As mentioned above, all semiconductor devices evolve heat during operation and are subject to malfunction if heat is accumulated. Therefore, they need a radiator with good thermal conductivity for heat dissipation. The radiator, which is bonded to the semiconductor element directly or indirectly through an insulating layer, calls for not only a high thermal conductivity, but also a low thermal expansivity for good matching with the semiconductor element. 
     Prevailing semiconductor elements are based on the use of Si or GaAS, which have a coefficient of thermal expansion of 2.6×10 −6  to 3.6×10 −6 /° C. and 5.7×10 −6  to 6.9×10 −6 /° C., respectively. Among known materials comparable to them in thermal expansivity are AlN, SiC, Mo, W, and Cu—W. When used alone for radiators, they do not permit their heat transfer coefficient and thermal conductivity to be controlled as desired. They are poor in workability and high in production cost. A Cu—Mo sintered alloy is proposed in Japanese Patent Laid-open No. Hei 8-78578. A Cu—W—Ni sintered alloy is proposed in Japanese Patent Laid-open No. Hei 9-181220. A Cu—SiC sintered alloy is proposed in Japanese Patent Laid-open No. Hei 9-209058. An Al—SiC composite material is proposed in Japanese Patent Laid-open No. Hei 9-15773. These conventional composite materials permit their heat transfer coefficient and thermal conductivity to be controlled over a broad range if the ratio of their constituents is changed. However, they are poor in plastic workability and hence they present when used in making thin plate and need many manufacturing steps. 
     It is an object of the present invention to provide a composite material having a low thermal expansivity, a high thermal conductivity, and good plastic workability, a semiconductor device made with said composite material, a radiator for said semiconductor device, an electrostatic attractor, and a dielectric plate for said electrostatic attractor. 
     SUMMARY OF INVENTION 
     The first aspect of the present invention resides in a composite material composed the metal and inorganic particles having a smaller coefficient of thermal expansion than said metal, characterized in that said inorganic particles are dispersed in such a way that 95% or more of them (in terms of their area in cross-section) form aggregates of complex configuration joined together. 
     The second aspect of the present invention resides in a composite material composed of metal and inorganic particles having a smaller coefficient of thermal expansion than said metal, characterized in that said inorganic particles are individually present such that there 100 or less particles in a sectional area of 100 μm square, with the remainder being dispersed in the form of aggregates of complex configuration joined together. 
     The third aspect of the present invention resides in a composite material composed of metal and inorganic particles having a smaller coefficient of thermal expansion than said metal, characterized in that said inorganic particles have a Vickers hardness of 300 or less. The fourth aspect of the present invention resides in a composite material composed of metal and inorganic particles having a smaller coefficient of thermal expansion than said metal, said composite material having a coefficient of thermal expansion which increases by 0.025-0.035 ppm/° C. on average per W/m·K at 20° C. in the range of 20-105° C. 
     The fifth aspect of the present invention resides in a composite material composed of metal and inorganic particles having a smaller coefficient of thermal expansion than said metal, characterized in that said inorganic particles are dispersed in the form of aggregates joined together, said aggregates being elongated in the direction of plastic working. 
     The sixth aspect of the present invention resides in a composite material composed of copper and copper oxide particles, characterized in that said copper oxide particles are dispersed in such a way that 95% or more of them (in terms of their area in cross-section) form aggregates of complex configuration joined together. 
     The seventh aspect of the present invention resides in a radiator plate for a semiconductor device which is made of said composite material. 
     The eighth aspect of the present invention resides in a radiator plate for a semiconductor device which has a nickel plating layer thereon. 
     The ninth aspect of the present invention resides in a semiconductor device which comprises a plurality of insulating substrates and a plurality of semiconductor elements mounted on each of said insulating substrates, each of said insulating substrates having said radiator plate directly joined to said insulating substrate through a conductive layer formed on the upper and lower surfaces of said insulating substrate. 
     The tenth aspect of the present invention resides in a semiconductor device which comprises an insulating substrate with a radiator plate and a semiconductor element mounted on said insulating substrate, wherein said radiator plate is the one defined in the seventh or eighth aspect. 
     The eleventh aspect of the present invention resides in a semiconductor device which comprises a semiconductor element mounted on a radiator plate, a lead frame joined to said radiator plate, and metal wiring to electrically connect said lead frame with said semiconductor element, said semiconductor element being sealed with plastics, wherein said radiator plate is the one defined in the seventh or eighth aspect. 
     The twelfth aspect of the present invention resides in a semiconductor device which comprises a semiconductor element mounted on a radiator plate, a lead frame joined to said radiator plate, and metal wiring to electrically connect said lead frame with said semiconductor element, said semiconductor element being sealed with plastics and said radiator plate being open at the side opposite to the side to which said semiconductor element is joined, wherein said radiator plate is the one defined in the seventh or eighth aspect. 
     The thirteenth aspect of the present invention resides in a semiconductor device which comprises a semiconductor element mounted on a radiator plate, pins for connection with external wiring, a ceramics multilayer wiring substrate having at its center an open space to hold said semiconductor element, and metal wiring to electrically connect said semiconductor element with the terminals of the substrate, said radiator plate and said substrate being joined to each other such that said semiconductor element is installed in said space, and said substrate being joined to a lid such that said semiconductor element is isolated from the atmosphere, wherein said radiator plate is the one defined in the seventh or eighth aspect. 
     The fourteenth aspect of the present invention resides in a semiconductor device which comprises a semiconductor element mounted on a radiator plate, terminals for connection with external wiring, a ceramics multilayer wiring substrate having at its center a recess to hold said semiconductor element, and metal wiring to electrically connect said semiconductor element with the terminals of the substrate, said radiator plate and the recess of said substrate being joined to each other such that said semiconductor element is installed in said recess, and said substrate being joined to a lid such that said semiconductor element is isolated from the atmosphere, wherein said radiator plate is the one defined in the seventh or eighth aspect. 
     The fifteenth aspect of the present invention resides in a semiconductor device which comprises a radiator plate, a semiconductor element joined onto said radiator plate with a thermally conductive resin, a lead frame joined to a ceramics insulating substrate, and a TAB to electrically connect said semiconductor element with the lead frame, said radiator plate and said substrate being joined to each other such that said semiconductor element is isolated from the atmosphere, and said semiconductor element and said insulating substrate being separated by a thermally conductive elastic resin interposed between them, wherein said radiator plate is the one defined in the seventh or eighth aspect. 
     The sixteenth aspect of the present invention resides in a semiconductor device which comprises a first radiator plate, a semiconductor element joined to said radiator plate with metal, a second radiator plate joined to a grounding plate, said first radiator plate being mounted on the grounding plate of the radiator plate, and a TAB electrically connected to the terminals of said semiconductor element, said semiconductor element being sealed with plastics, wherein said radiator plate is the one defined in the seventh or eighth aspect. 
     The seventeenth aspect of the present invention resides in a dielectric plate for electrostatic attractors which is made of the composite material defined in any of the first to sixth aspects mentioned above. 
     The eighteenth aspect of the present invention resides in an electrostatic attractor which comprises an electrode layer and a dielectric plate bonded to said electrode layer, said dielectric producing an electrostatic attractive force upon application of a voltage to said electrode layer such that an object is fixed onto the surface of said dielectric plate, wherein said dielectric plate is the one defined in the seventeenth aspect. 
     The composite material according to the present invention is composed of metal and inorganic particles. The metal includes Au, Ag, Cu, and Al, among which Cu is the most desirable because of its high melting point and high strength. The inorganic particles should preferably be those which are comparatively soft and stable after sintering and have an average coefficient of thermal expansion equal to or smaller than 5.0×10 −6 /° C., preferably equal to or smaller than 3.5×10 −6 /° C., in the range of 20-150° C., and also have a Vickers hardness of 300 or less. (They are different from conventional ones, such as SiC and Al 2 O 3 , which greatly differ in hardness from the matrix metal.) Such soft inorganic particles provide good plastic workability (either hot or cold) after sintering. Rollability makes it possible to produce a comparatively thin plate in a short processing time. The resulting composite material has a high strength because of the inorganic particles dispersed therein. Conceivable examples of the inorganic particles include copper oxide, tin oxide, lead oxide, and nickel oxide. Of these examples, copper oxide is preferable because it has the smallest coefficient of thermal expansion. 
     The composite material of the present invention should preferably be reinforced with hard, fine ceramics particles, such as SIC and, Al 2 O 3 , having a Vickers hardness of 1000 or more and an average particle diameter of 3 μm or less, in an amount of 5 volt or less. 
     The radiator plate and dielectric plate according to the present invention may be obtained in its final shape by sintering, optional rolling, and plastic working (such as pressing). 
     The composite material according to the present invention should preferably be a copper (Cu) alloy containing cuprous oxide (Cu 2 O) in an amount of 20-80 volt, with the Cu phase and the Cu 2 O phase forming the dispersing structure. The composite material should preferably have a coefficient of thermal expansion of 5×10 −6  to 14×10 −6 /° C. and a thermal conductivity of 30-325 W/m·K in the range of room temperature to 300° C. 
     The copper-cuprous oxide composite material should preferably contain cuprous oxide (Cu 2 O) in an amount of 20-80 volt, with the remainder being copper (Cu). The Cu 2 O phase and the Cu phase should have an oriented structure. The composite material should preferably have a coefficient of thermal expansion of 5×10 −6  to 14×10 −6 /° C. and a thermal conductivity of 30-325 W/m·K in the range of room temperature to 300° C. The thermal conductivity in the direction of orientation should be greater than twice that in the direction perpendicular to the direction of orientation. 
     The composite material according to the present invention is produced by the steps of mixing copper powder and cuprous oxide powder, pressing the mixed powder, sintering the pressed form at 800-1050° C., and performing cold or hot plastic working. (Copper powder is an example of said metal and cuprous oxide powder is an example of said inorganic particles.) 
     The copper composite material according to the present invention is produced from a mixed powder of cupric oxide (CuO) and copper (Cu) containing inevitable impurities. The amount of cupric oxide is 10.8-48.8 vol %. The production process consists of steps of press-forming the mixed powder, sintering the pressed form at 800-1050° C., thereby solidifying the pressed form and forming Cu 2 O by reaction between CuO and Cu, hot or cold pressing (for plastic working), and annealing. 
     The copper composite material of the present invention is composed of Cu and Cu 2 O, the former having a high coefficient of thermal expansion of 17.6×10 −6 /° C. and a thermal conductivity as high as 391 W/m·K, the latter having a low coefficient of thermal expansion of 2.7×10 −6 /° C. and a thermal conductivity of 12 W/m·K. It is formed into a radiator plate for semiconductor devices by sintering. The sintered body is composed of Cu and Cu 2 O in an amount of 20-80 vol %. It has a coefficient of thermal expansion of 5×10 −6  to 14×10 −6 /° C. and a thermal conductivity of 30-325 W/m·K in the range of room temperature to 300° C. With Cu 2 O in an amount of 20% or more, the composite material has a high coefficient of thermal conductivity required of the radiator plate. With Cu 2 O in an amount of 80% or less, the composite material has sufficient thermal conductivity and structural strength. 
     The composite material according to the present invention is obtained basically by powder metallurgy. The copper composite material is obtained from Cu powder and Cu 2 O powder or CuO powder. These powders (as raw materials) are mixed in a prescribed ratio, the mixed powder is cold-pressed in a mold, and the resulting preform is sintered. If necessary, the sintered body undergoes hot or cold plastic working. 
     The mixing of raw material powders is accomplished by using a V-mixer, pot mill, or mechanical alloying. The particle size of the raw material powders affect the press molding performance and the dispersibility of Cu 2 O after sintering. Therefore, the Cu powder should have a particle diameter of 100 μm or less, and the Cu 2 O and CuO powder should have a particle diameter of 10 μm or less, preferably 1-2 μm. 
     The mixed powder undergoes cold pressing in a mold under a pressure of 400-1000 kg/cm 2 . The pressure should preferably be increased in proportion to the Cu 2 O content. 
     The preform of the mixed powder in sintered is an argon atmosphere under normal pressure or sintered by HIP or hot pressing under pressure. Sintering should be carried out at 800-1050° C. for about 3 hours. The sintering temperature should be increased in proportion to the Cu 2 O content. The sintering temperature varies depending on the kind of the matrix metal. In the case of copper, the sintered body will have a low density if the sintering temperature is 800° C. or less. In addition, sintering at a temperature of 1050° C. or more brings about a eutectic reaction between Cu and Cu 2 O, which would result in partial melting. Therefore, an adequate sintering temperature ranges from 900° C. to 1000° C. 
     The copper composite material according to the present invention is composed of Cu and Cu 2 O, which have a low hardness. Therefore, it is capable of cold or hot working, such as rolling and forging, which is carried out after sintering, if necessary. Working leads to anisotropic thermal conductivity, which contributes to strength or some applications which need heat conduction in a specific direction. 
     According to the present invention, the raw material powder may be CuO. This CuO powder is mixed with Cu powder and the mixed powder is press-formed. The resulting preform is sintered so that Cu is oxidized. Thus, there is obtained a sintered body which is composed of a matrix of Cu and a dispersed phase of Cu 2 O. CuO coexisting with Cu transforms into Cu 2 O (which is thermally stable) at high temperatures according to equation (1) below.
 
2Cu+CuO→Cu+Cu 2 O  (1) 
 
A certain length of time is required before an equilibrium is reached in the reaction represented by the equation (1). About 3 hours will be sufficient if the sintering temperature is 900° C.
 
     Cu 2 O particles in the sintered body should be as fine as possible because their particle diameter affects the density, strength, and plastic workability of the composite material. The particle diameter is greatly affected by the mixing method. The larger the mixing energy, the less the coagulation of powder particles. Thus, fine Cu 2 O particles are obtained after sintering. 
     According to the present invention, the particle size of the Cu 2 O phase is established as follows depending on the mixing machine employed. 50 vol % or more of particles should have a particle diameter of 50 μm or less if a V-mixer is used (with small mixing energy), a particle diameter of 50 μm or less if a pot mill containing steel balls is used, and a particle diameter of 10 μm or less if mechanical alloying (with the largest mixing energy) is employed, with the remainder having a particle diameter of 50-200 μm. With a particle diameter of 200 μm or more, the resulting composite material has a high porosity and hence is poor in plastic workability. With a content of Cu 2 O phase in excess of 50 vol %, the resulting composite material is low in thermal conductivity and uneven in characteristic properties and hence it is inadequate for use as the radiator plate for semiconductor devices. A preferred structure is one which is composed of a Cu phase and a Cu 2 O phase (50 μm or less) uniformly dispersed therein. Cu 2 O particles have an extremely irregular shape and are joined together before sintering; their particle diameter before sintering can be observed with a high magnification. The Cu 2 O phase should preferably 10 μm or less. 
    
    
     
       BRIEF DESCRIPTION OF DRAWINGS 
         FIG. 1  is an optical photomicrograph showing the microstructure of the sintered body (composed of Cu and 55 vol % of Cu 2 O) in Example 1 (sample No. 4) of the present invention. 
         FIG. 2  is an optical photomicrograph showing the microstructure of the sintered body (composed of Cu and 55 vol % of Cu 2 O) in Example 2 of the present invention. 
         FIG. 3  is an optical photomicrograph showing the microstructure of the sintered body (composed of Cu and 40 vol % of Cu 2 O) in Example 3 of the present invention. 
         FIG. 4  is an optical photomicrograph showing the microstructure of the forged material (composed of Cu and 55 vol % Of Cu 2 O) in Example 4 of the present invention, the microstructure being that of a plane parallel to the direction of elongation by forging. 
         FIG. 5  is an optical photomicrograph showing the microstructure of the sintered body (composed of Cu and 32.2 volt of CuO) in Example 5 (sample No. 14) of the present invention. 
         FIG. 6  is a graph showing the relation between thermal expansivity and thermal conductivity. 
         FIG. 7  is a plan view showing the IGBT module in Example 6 of the present invention. 
         FIG. 8  is a sectional view of the IGBT in Example 6 of the present invention. 
         FIGS. 9A  to  9 D are schematic diagrams showing the steps of production of the IGBT module in Example 6. 
         FIG. 10  is a graph showing the amount of warpage of the base in each step of producing the IGBT module in Example 6 of the present invention. 
         FIG. 11  is a plan view and side and end sectional views showing a power conversion apparatus equipped with the IGBT module in Example 6 of the present invention. 
         FIGS. 12A and 12B  are graphs showing the amount of warpage in a power conversion equipment which is not yet equipped with the IGBT module in Example 6 of the present invention. 
         FIGS. 13A and 13B  are graphs showing the amount of warpage in a power conversion equipment which has been equipped with the IGBT module in Example 6 of the present invention. 
         FIG. 14  is a sectional view showing the plastic package with a built-in radiator plate in Example 7 of the present invention. 
         FIG. 15  is a sectional view showing the plastic package with an exposed radiator plate in Example 7 of the present invention. 
         FIG. 16  is a sectional view showing the package in Example 8 of the present invention. 
         FIG. 17  is a sectional view showing the ceramics package with radiator fins in Example 8 of the present invention. 
         FIG. 18  is a sectional view of the semiconductor device in Example 9 of the present invention. 
         FIG. 19  is a sectional view of the semiconductor device in Example 9 of the present invention. 
         FIG. 20  is a sectional view of an MCM in Example 10 of the present invention. 
         FIG. 21  is a sectional view of the electrostatic attractor pertaining to the present invention. 
     
    
    
     BEST MODE FOR CARRYING OUT THE INVENTION 
     EXAMPLE 1 
     Raw material powders used in this example are electrolytic copper powder (with a particle diameter of 75 μm or less) and Cu 2 O powder (with a particle diameter of 1-2 μm and a purity of 3N). They were mixed in a ratio shown in Table 1. The resulting mixture (1400 g) was thoroughly mixed for more than 10 hours in a dry pot mill containing steel balls. The resulting mixed powder was placed in a mold, 150 mm in diameter, and cold-pressed under a pressure of 400-1000 kg/cm 2  depending on the Cu 2 O content. Thus, there were obtained preforms measuring 150 mm in diameter and 17-19 mm in height. The preforms were sintered in an argon atmosphere. The resulting sintered bodies were chemically analyzed, examined for structure, and measured for thermal expansivity, thermal conductivity, and Vickers hardness. Incidentally, sintering was carried out for 3 hours at 900-1000° C. depending on the Cu 2 O content. The thermal expansivity was measured in the range of room temperature to 300° C. by using an apparatus for TMA (Thermal Mechanical Analysis). The thermal conductivity was measured by a laser flash method. The results are shown in Table 1. The sintered body (sample No. 4) has the microstructure as shown in FIG.  1 . 
     The results of chemical analysis indicated that the composition of the sintered body agrees with the ratio of mixing. It is apparent from Table 1 that the thermal expansivity and thermal conductivity vary over a broad range depending on the ratio of Cu and Cu 2 O. Therefore, it was possible to produce the sintered body with thermal characteristics required of a radiator plate. 
     
       
         
           
               
               
               
               
               
             
               
                   
                 TABLE 1 
               
             
            
               
                   
                   
               
               
                   
                 Composition 
                   
                 Coefficient of 
                 Thermal 
               
               
                   
                 (vol %) 
                   
                 thermal expansion 
                 conductivity 
               
            
           
           
               
               
               
               
               
            
               
                 No. 
                 Cu 
                 Cu 2 O 
                 (×10 −6 /° C.) 
                 (W/m · K) 
               
               
                   
               
            
           
           
               
               
               
               
               
            
               
                 1 
                 20 
                 80 
                 5.5 
                 41 
               
               
                 2 
                 30 
                 70 
                 7.0 
                 63 
               
               
                 3 
                 40 
                 60 
                 8.4 
                 93 
               
               
                 4 
                 45 
                 55 
                 9.3 
                 116 
               
               
                 5 
                 50 
                 50 
                 10.1 
                 138 
               
               
                 6 
                 60 
                 40 
                 10.8 
                 183 
               
               
                 7 
                 70 
                 30 
                 12.9 
                 229 
               
               
                 8 
                 80 
                 20 
                 13.8 
                 280 
               
               
                   
               
            
           
         
       
     
     The photomicrograph (×300) shown in  FIG. 1  indicates the microstructure in which Cu 2 O particles are 50 μm or less and the Cu 2 O phase is uniformly dispersed in the Cu phase. (The Cu 2 O particles coagulate in the mixing step and slightly grow in the sintering step.) In the photomicrograph, the white part represents the Cu phase and the black part represents the Cu 2 O phase. 
     It is noted from  FIG. 1  that Cu 2 O particles disperse in an irregular insert, accounting for 99% or more of the sectional area. 
     The Cu phase and the Cu 2 O phase have a hardness (Hv) of 210-230 and 75-80, respectively. The resulting sintered body has good machinability (latheing and drilling) and can be readily shaped as desired. 
     EXAMPLE 2 
     The same procedure as in Example 1 was repeated except that mixing was carried out by using a V-mixer. There was obtained a sintered body composed of Cu and 55 volt of Cu 2 O. This sintered body was examined for microstructure, thermal expansivity, and thermal conductivity in the same way as in Example 1. 
       FIG. 2  is a photomicrograph (×300) of the sintered body composed of Cu and 55 volt of Cu 2 O. It is apparent from the photomicrograph that the microstructure contains Cu 2 O particles greatly varying in size. Large Cu 2 O particles are formed by coagulation during mixing in the V-mixer. The sintered body in this example is almost comparable in thermal expansivity and thermal conductivity to that of the same composition in which the Cu 2 O phase is uniformly dispersed in the Cu phase. However, the measured values vary from one position to another. It is noted that Cu 2 O particles are dispersed mostly in an irregular pattern as in  FIG. 1 , but they are in larger aggregates than those in FIG.  1 . 
     EXAMPLE 3 
     Raw material powders used in this example are electrolytic copper powder (with a particle diameter of 74 μm or less) and CuO powder (with a particle diameter of 1-2 μm and a purity of 3N). They were mixed to establish a composition of Cu and 22.4 volt of CuO. The resulting mixture (300 g) was thoroughly mixed by mechanical alloying for 25 hours in a planetary ball mill (120 mm in diameter) containing steel balls (8 mm in diameter). The resulting mixed powder was placed in a mold, 80 mm in diameter, and cold-pressed under a pressure of 1000 kg/cm 2 . Thus, there was obtained a preform. The preform was sintered in an argon atmosphere at 800° C. for 2 hours. The resulting sintered body was examined for structure, thermal expansivity, and thermal conductivity in the same way as in Example 1. It was also tested by X-ray diffractometry. 
       FIG. 3  is a photomicrograph (×1000) of the microstructure of the sintered body. It is apparent from the photomicrograph that Cu 2 O particles are finer than those in Examples 1 and 2 and Cu 2 O particles of 10 μm or less are uniformly dispersed. The fine microstructure is desirable for improvement in strength and cold rollability. It is noted that 95% or more of Cu 2 O particles are dispersed in an irregular pattern as in  FIG. 1 , but some of them are present in the form of spherical particles (about 20 particles in an area of 100 μm square). 
     The sintered body was tested by X-ray diffractometry to identify oxides contained therein. The diffraction peak is due to Cu 2 O only. This suggests that CuO has completely transformed into Cu 2 O during sintering. The results of chemical analysis indicate that the sintered body is composed of Cu and 40 volt of Cu 2 O as intended. 
     The sintered body was found to have the same thermal expansivity and thermal conductivity as those of the sinter body of the same composition in Example 5 mentioned later. 
     EXAMPLE 4 
     Raw material powders used in this example are the same those used in Example 1. They were mixed to establish a composition of Cu and 55 volt of Cu 2 O. The resulting mixture (550 g) was thoroughly mixed in a V-mixer. The resulting mixed powder was placed in a mold, 80 mm in diameter, and cold-pressed under a pressure of 600 kg/cm 2 . Thus, there was obtained a preform measuring 80 mm by 22 mm. The preform was sintered in an argon atmosphere at 975° C. for 3 hours. The resulting sintered body was heated to 800° C. and forged (with a forging ratio of 1.8) using a 200-ton press. Forging was followed by tempering and annealing at 500° C. The resulting product was examined for structure, thermal expansivity, and thermal conductivity in the same way as in Example 1. 
     The forged product was found to be satisfactory except for slight edge cracking. The copper composite material of the present invention is superior in plastic workability. 
       FIG. 4  is a photomicrograph (×300) of the microstructure of the forged product. It is noted that both the Cu phase and the Cu 2 O phase are deformed and oriented in the forging direction; however, there are no defects such as cracking. It is also noted that 95% or more of Cu 2 O particles are dispersed in the form of irregular particles joined together. They are elongated by plastic working. 
     The sintered body and forged product were measured for thermal conductivity by the laser flash method (Table 2). The sintered body does not show the anisotropism in thermal conductivity. However, the forged product shows the anisotropism in thermal conductivity. The thermal conductivity in the L direction in which the Cu phase and Cu 2 O phase are oriented is greater than twice that in the C direction (forging direction) perpendicular to the L direction. The thermal expansivity in the range from room temperature to 300° C. is almost free from anisotropism; it was identical with that in Example 1. 
     
       
         
           
               
               
               
             
               
                   
                 TABLE 2 
               
             
            
               
                   
                   
               
               
                   
                 Thermal conductivity 
                   
               
               
                   
                 (W/m · K) 
               
            
           
           
               
               
               
            
               
                   
                 L direction 
                 C direction 
               
               
                   
                   
               
            
           
           
               
               
               
               
            
               
                   
                 Sintered body 
                 111 
                 106 
               
               
                   
                 Forged product 
                 152 
                 67 
               
               
                   
                   
               
            
           
         
       
     
     EXAMPLE 5 
     Raw material powders used in this example are electrolytic copper powder (with a particle diameter of 74 μm or less) and CuO powder (with a particle diameter of 1-2 μm and a purity of 3N). They were mixed in a ratio shown in Table 3. The resulting mixture (1400 g) was thoroughly mixed for more than 10 hours in a dry pot mill containing steel balls. The resulting mixed powder was placed in a mold, 150 mm in diameter, and cold-pressed under a pressure of 400-1000 kg/cm 2  depending on the CuO content. Thus, there were obtained preforms, which were subsequently sintered in an argon atmosphere. The resulting sintered bodies were chemically analyzed, examined for structure, and measured for thermal expansivity, and thermal conductivity. They were also tested by X-ray diffractometry to identify oxides therein. Incidentally, sintering was carried out for 3 hours at 900-1000° C. depending on the CuO content. The thermal expansivity was measured in the range of room temperature to 300° C. by using an apparatus for TMA (Thermal Mechanical Analysis). The thermal conductivity was measured by laser flash method. The results are shown in Table 3. 
     
       
         
           
               
               
               
               
               
             
               
                   
                 TABLE 3 
               
             
            
               
                   
                   
               
               
                   
                 Powder 
                 Composition 
                 Coefficient 
                 Thermal 
               
               
                   
                 composition 
                 of sintered 
                 of thermal 
                 conductiv- 
               
               
                   
                 (vol %) 
                 body (vol %) 
                 expansion 
                 ity 
               
            
           
           
               
               
               
               
               
               
               
            
               
                 No. 
                 Cu 
                 CuO 
                 Cu 
                 Cu 2 O 
                 (×10 −6 /° C.) 
                 (W/m · K) 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
            
               
                 11 
                 51.2 
                 48.8 
                 20 
                 80 
                 5.6 
                 55 
               
               
                 12 
                 58.1 
                 41.9 
                 30 
                 70 
                 7.0 
                 80 
               
               
                 13 
                 64.9 
                 35.1 
                 40 
                 60 
                 8.5 
                 105 
               
               
                 14 
                 67.8 
                 32.2 
                 45 
                 55 
                 9.1 
                 129 
               
               
                 15 
                 71.4 
                 28.6 
                 50 
                 50 
                 9.7 
                 149 
               
               
                 16 
                 77.6 
                 22.4 
                 60 
                 40 
                 10.6 
                 185 
               
               
                 17 
                 83.5 
                 16.5 
                 70 
                 30 
                 12.7 
                 228 
               
               
                 18 
                 89.2 
                 10.8 
                 80 
                 20 
                 13.5 
                 282 
               
               
                   
               
            
           
         
       
     
     The sintered body was examined by X-ray diffractometry to identify oxides therein. The diffraction peak is due to Cu 2 O only. This suggests that CuO has completely transformed into Cu 2 O during sintering. 
     The microstructure of sample No. 14 is shown in FIG.  5 . The photomicrograph (×300) indicates that the structure is identical with that of the same composition in Example 1. The Cu 2 O phase is composed of Cu 2 O (which has formed from Cu and CuO by oxidation) and Cu 2 O (which has formed from CuO by decomposition). The Cu 2 O particles are identical with those in Example 1. 
     It is apparent from Table 3 that the sintered body is not so greatly different in thermal expansivity from that produced from Cu 2 O powder. However, it is higher in thermal conductivity when its Cu 2 O content exceeds 50 volt. This is because the sintered body has a higher density when it is made of CuO powder. 
       FIG. 6  is a graph showing the relation between the thermal conductivity (x) and the coefficient of thermal expansion (y) which are shown in Table 3. The plotted points lie between two lines represented by y=0.031x+4.65 and y=0.031x+5.95. The coefficient of thermal expansion on average should be 0.025-0.035 ppm/° C. per W/m·K at 20° C. in the range of 20-250° C. 
     EXAMPLE 6 
     This example demonstrates an application of the copper composite material of the present invention. This application is a radiator plate for an IGBT (Insulated Gate Bipolar Transistor) which in one of the known power semiconductor elements. 
       FIG. 7  is a plan view showing the inside of the module consisting of 24 IGBT elements.  FIG. 8  is a sectional view of the module of one IGBT. Four IGBT elements  101  and two diode elements  102  are connected to an AlN substrate  103  with solder  201 . The AIN substrate  103  consists of two sheets of copper foil  202  and  203  and an AIN plate  204  bonded together with silver solder (not shown). On the AlN substrate  103  there are formed regions for the emitter wiring  104 , the collector wiring  105 , and the gate wiring  106 . The IGBT element  101  and the diode element  102  are soldered to the collector wiring  105 . Each element is connected to the emitter wiring  104  through the metal wire  107 . And, on the region of the gate wiring  106  there is arranged the resistance element  108 , and the gate pad of the IGBT element  101  is connected to the resistance element  108  through the metal wire  107 . Six AlN substrates  103 , each carrying semiconductor elements, are bonded to the radiator plate  109  with solder  205 . The radiator plate  109 , having a Ni-plated surface, is made of the Cu—Cu 2 O composite material described in Examples 1 to 5. The AlN substrate  103  is connected to the terminal  206  through the solder  209 . The terminal  206  and the plastic case  207  together form the base block  208 . The case  207  is bonded to the radiator plate  109  with a silicone rubber adhesive  210 . The terminals from the case block  208  are connected to each AlN substrate at two emitter terminals  110 , two emitter sense terminals  111 , two collector terminals  112 , and one gate terminal  113 . Then, silicone gel  212  is injected through the case lid  211  (having a resin injection port) so that the terminals are entirely covered. Subsequently, thermosetting epoxy resin  213  is poured to cover the entire surface. Thus, the module is completed. The radiator plate  109  is attached to the aluminum support by eight bolts passing through eight bolt holes  114 . The bolt holes  114  are made by machining. In addition, the case  207  is joined by another eight bolts (joined by the adhesive  210 ) passing through eight bolt holes  115 . 
     Table 4 shows a comparison in thermal expansivity and thermal conductivity between commonly used base materials and the Cu composite material (with 30 volt Cu 2 O) according to the present invention. It is noted that the semiconductor element with the Cu—Cu 2 O base material has a lower coefficient of thermal expansion than the module with the commonly used Cu base material. The solder  209  joining together the AlN substrate  103  and the base  109  is improved in reliability. The Mo or Al—SiC base used to improve the reliability of the solder  106  in a severe environment has a lower coefficient of thermal expansion than the Cu—Cu 2 O base. However, it also has a small thermal conductivity, which leads to a high heat resistance of the module. The module with the Cu—Cu 2 O base according to the present invention has a heat fatigue life which is more than five times that of a module with a Cu base and also has 0.8 times the heat resistance of a module with the Mo base of a same thickness. 
     
       
         
           
               
               
               
               
             
               
                 TABLE 4 
               
               
                   
               
               
                   
                 Coefficient of 
                   
                   
               
               
                   
                 thermal 
                 Thermal 
               
               
                   
                 expansion 
                 conductivity 
               
               
                 Material 
                 (ppm/° C.) 
                 (W/m · K) 
                 Remarks 
               
               
                   
               
             
            
               
                   
               
            
           
           
               
               
               
               
            
               
                 Cu—Cu 2 O (30 vol %) 
                 13.5 
                 230 
                 Present invention 
               
               
                 Cu 
                 17 
                 390 
                 Prior art 
               
               
                 Mo 
                 5 
                 140 
               
               
                 Al—SiC 
                 8 
                 160 
               
               
                   
               
            
           
         
       
     
     The above-mentioned effects broaden the range of selection the module structure and material. For example, in the example shown in  FIG. 7 , the Cu—Cu 2 O base has a higher thermal conductivity than the Mo base. In other words, it exhibits an improved heat diffusion. Therefore, the temperature difference between the end and the center of the semiconductor element is reduced during its operation. The semiconductor element can be made 1.2 times larger than the conventional module. As the result, a conventional structure with 30 units of IGBT is now replaced by a new structure with 24 units of IGBT. In this way, it is possible to reduce the module size. In addition, it is now possible to use an alumina substrate (as the insulating substrate) which is lower (by about 20%) in thermal conductivity than an AlN substrate. Alumina is superior in flexural strength to AlN, and hence it can be made into a larger substrate. The alumina plate has a higher coefficient of thermal expansion than the AlN plate, and it differs less in thermal expansion from the base material. This leads to reduction in the amount of warpage of the module itself. The alumina substrate can be made larger in size, and a larger substrate can hold more semiconductor elements. In other words, the aluminum substrate permits a reduction of the area for insulation in each substrate and a reduction of the area for insulation between substrates. This leads to a reduction in the module size. 
       FIGS. 9A  to  9 D are schematic diagrams showing the steps of producing the module according to the present invention. 
     ( FIG. 9A ) A Cu—Cu 2 O base  109  with a nickel-plated surface is made ready. It is nearly flat in its as-purchased state. 
     ( FIG. 9B ) To the base  109 , the AlN substrate  103  is bonded with solder  205 . The AlN substrate carries the semiconductor elements  101  bonded thereto with solder  102 . The base  109  warps while the solder is cooling because it differs in thermal expansivity from the assembly of the AlN substrate and the semiconductor elements. Thus, the reverse side of the module becomes concave. 
     ( FIG. 9C ) The case block  208  is assembled with a thermosetting adhesive. While the adhesive is cooling, the reverse side of the module becomes almost flat because the case has a higher coefficient of thermal expansion than the assembly  301  which has undergone soldering. 
     ( FIG. 9D ) The inside of the module is filled with the silicone gal  212  and the thermosetting epoxy resin  213 . The reverse side of the module becomes convex because the resin has a high coefficient of thermal expansion. 
       FIG. 10  is a graph showing the amount of warpage of the reverse side in each step. The plus value represents concave warpage and the minus value represents convex warpage. The module with the Cu—Cu 2 O base according to the present invention warps less (about one-third) than that with the conventional Mo base. The module with the Cu base has a warped concave reverse side (100 μm or more) after its completion because its reverse side warps concave in the step (b) due to its great difference in thermal expansivity from the AlN substrate (although the results are not shown). The module with the Cu—Cu 2 O base of the present invention has a small amount of warpage; therefore, the module can be made larger than before. Just as the amount of warpage is small in the assembling steps, so the amount of warpage is small due to the temperature change during operation. Therefore, the grease between the module and the cooling fin does not flow. 
       FIG. 11  shows an example of the power conversion apparatus to which the module of the present invention is applied. This example comprises a 2-level inverter. The power semiconductor device  501  is mounted on the aluminum heat sink  511  and is fixed by the tightening bolt  512 , with the heat dissipating grease  510  interposed between them. Usually, two modules  501  are arranged symmetrically so that they are connected by a single middle wiring  503  (point B). The collector wiring  502  and the emitter wiring  504  are supplied with source voltage  509  through the U, V, and W phases to which they are connected. The signal wire is constructed of each IGBT module  501 , the gate wiring  505 , the emitter auxiliary wiring  506 , and the collector auxiliary wiring  507 . A load is indicated by  508 . 
       FIGS. 12A and 12B  are graphs showing the amount of warpage of the module.  FIGS. 13A and 13B  are graphs showing the amount of warpage (grease thickness) on the module reverse side that was measured before and after the mounted module was tightened.  FIGS. 12A and 13A  represent the results in the present invention, and  FIGS. 12B and 13B  represent the results in the prior art technology. In the case of the module with the known conventional Al—SiC base, the amount of warpage (convex) in the reverse side about 100 μm. However, if the module is coated with grease and then tightened, the warpage is reversed (from convex to concave) because the surface is pushed by grease at the time of tightening. As a result, the thickness of the grease increases at the center and the contact resistance increases accordingly. By contrast, in the case of the Cu—Cu 2 O base according to the present invention, the amount of initial warpage is about 50 μm, but the thickness of grease at the center of the module remains about 50 μm after grease application and tightening. This is because the base is highly stiff. Thus, the amount of warpage is reduced by half from that of the conventional Al—SiC base. In addition, the grease thickness in the module becomes uniform. Deformation due to pushed grease at the time of mounting occurs in the case of the module with the Cu base which has lower stiffness than the Cu—Cu 2 O alloy base. This problem is solved by the Cu—Cu 2 O alloy of the present invention. 
     As shown in the figure, the Cu—Cu 2 O alloy base of the present invention has a lower thermal resistance and contact thermal resistance than the conventional Mo or Al—SiC base material applied to the high-reliability modules. Therefore, it permits the modules to be densely mounted as shown in FIG.  11 . In addition, the fact that the cooling fin has an improved cooling effect makes it possible to reduce the area and volume required for the mounting of the power conversion apparatus. The reduction of the grease thickness permits the cooling fin to remain flat, and this makes it possible to construct a power conversion apparatus with large-sized fins. In addition, it possible to eliminate the auxiliary cooling function such as forced air cooling. This leads to a size reduction and noise reduction. 
     EXAMPLE 7 
     In this example, the copper composite material of the present invention described in Examples 1 to 5 is applied to the plastic package containing an IC as shown in  FIGS. 14 and 15 .  FIG. 14  shows a package with a built-in radiator plate.  FIG. 15  shows a package with an exposed radiator plate. 
     The radiator plate is prepared from a Cu—Cu 2 O composite material, with the Cu 2 O content varied in the range of 20 vol % to 55 vol %. The resulting composite material has a coefficient of thermal expansion in the range of 9×10 −6  to 14×10 −6 /° C. at room temperature to 300° C. This coefficient of thermal expansion is close to that of the molding resin. The radiator plate was finally machined and nickel-plated. 
     The structure of the package will be described with reference to FIG.  14 . There is shown a nickel-plated radiator plate  33  which is made of the copper composite material of the present invention. There is shown the lead frame  31  which is bonded to the radiator plate  33  with the insulating polyimide tape  32 . There is shown an IC  34  which is soldered to the radiator plate  33 . There is shown an Au wire  35  which connects the Al electrode on the IC to the lead frame. These components, except for part of the lead frame, are sealed with the molding resin  36  which is composed mainly of epoxy resin, silica filler, and hardener. The package with an exposed radiator plate shown in  FIG. 15  differs from the package shown in  FIG. 14  in that the radiator plate  33  is exposed to the outside from the molding resin. 
     The packages described above were examined for warpage and cracking at the joint between the radiator plate and the molding resin. It was found that there is no problem if the difference in the coefficient of thermal expansion between the radiator plate and the molding resin is 0.5×10 −6 /° C. or less. It was also found that the composite material has high thermal conductivity (200 W/m·K) if its Cu 2 O content is 20-35 vol %. 
     EXAMPLE 8 
     This example demonstrates an IC ceramics package which is provided with a radiator plate made of the copper composite material of the present invention explained in Examples 1 to 5.  FIGS. 16 and 17  are sectional views of the ceramics package. In  FIG. 16 , there is shown an IC  41  which is bonded to the nickel-plated radiator plate  42  with a polyimide resin. The radiator plate  42  is soldered to the package  43  of Al 2 O 3 . This package has copper wiring and is provided with pins  44  for connection to the circuit board. There is shown an aluminum wire  45  which connects the aluminum electrode on the IC to the package wiring. These components are sealed as follows. A weld ring  46  of kovar alloy is bonded to the package with silver solder. Then, the weld ring is welded to the lid  47  of kovar alloy by using a roller electrode.  FIG. 17  shows a ceramics package (the same one as shown in  FIG. 16 ) which is provided with radiator fins  48 . 
     EXAMPLE 9 
     This example demonstrates a package which is provided with a radiator plate made of the copper composite material of the present invention explained in Examples 1 to 5. This package is formed by a TAB (Tape Automated Bonding) technique.  FIGS. 18 and 19  are sectional views of the package. 
     In  FIG. 18 , there is shown an IC  51  which is bonded to the nickel-plated radiator plate  53  with a heat-conductive resin  52 . The IC has terminals at which the Au bump  54  is formed. The Au bump  54  is connected to the TAB  55 . The TAB  55  is connected to the lead frame  57  through the thin-film wiring  56 . The IC is sealed by the ceramics substrate  59 , the frame  60 , and the sealing glass  61 , with the silicone rubber  58  interposed therebetween. 
     The resin-sealed package is shown in FIG.  19 . The IC  65  is bonded to the nickel-plated radiator plate  67  of the present invention with the Au—Si alloy  66 . It is further bonded to the copper grounding plate  69  and the nickel-plated radiator plate  70  of the present invention with the heat-conductive resin  68 . On the other hand, the terminal of the IC is connected to the TAB  72  (including layers  72 A and  72 B) though the Au bump  71  and sealed with the resin  73 . The lead frame  57  and the radiator plate are partly exposed to the outside from the sealing resin. The TAB is fixed to the copper grounding plate with an epoxy-based silver paste  74 . 
     EXAMPLE 10 
     This example demonstrates an MCM having a radiator plate made of the copper composite material of the present invention as shown in  FIGS. 1  to  5 .  FIG. 20  is a sectional view of the MCM. The radiator plate  83  is formed from a sintered body (with or without rolling) by press working. 
     The IC  81  is connected through the Au wire  82  to the thin-film wiring  84  formed on the nickel-plated radiator plate  83  of the present invention. It is further connected through the Au wire to the wiring formed on the package  85  made of AlN. It is led to the external terminal  86 . The IC is sealed by the lid  87 , which is bonded, with the Au—Sn preform  88  interposed between the W metallized layers of the package. 
     EXAMPLE 11 
     This example demonstrates the electrostatic attractor equipped with the dielectric plate of the composite material of the present invention.  FIG. 21  is its sectional view. 
     As shown in  FIG. 21 , the electrostatic attractor is used as a chuck in the sputtering apparatus which processes the work  90  of conductor or semiconductor in a reduced pressure atmosphere in the vacuum chamber  95 . When a voltage (about 500V) is applied from the DC power supply  91  to the electrode  94  of the electrostatic attractor, an electrostatic attractive force occurs between the dielectric plate  92  and the work  90 . Thus, the work  90  is attracted toward the surface of the dielectric plate. In this example, the dielectric is formed from the composite material shown in Example 1 to 5. 
     In actual sputtering, the work  90  is mounted on the electrostatic attractor. Then, the vacuum chamber  95  is evacuated until the internal pressure decreases to about 1×10 −3  Pa by means of the vacuum pump connected to the exhaust vent  97 . The valve attached to the gas inlet  96  is opened to introduce the reaction gas (argon and the like) into the vacuum chamber  95  at a flow rate of about 10 sccm. The pressure in the vacuum chamber  95  is about 2×10 −2  Pa. 
     After that, a high-frequency power (about 4 kW at 13.56 MHz) is supplied to the electrode  94  of the electrostatic attractor, so that plasma is generated between the electrode  94  of the electrostatic attractor and another electrode (not shown). The voltage of the high-frequency power is 2 kV (V DC ) and 4 kV (V pp ). The matching box  98 , which is inserted between the electrode  94  of the electrostatic attractor and the high-frequency power source  93 , is designed for impedance matching with the vacuum chamber so that the high-frequency power is efficiently supplied to the plasma. 
     In actual operation of this sputtering apparatus, the temperature of the work  90  reached about 450° C. Nevertheless, the dielectric plate  92  of the electrostatic attractor remained unchanged without cracking (which gives rise to foreign matter). This means that the electrostatic attractor is effective in improving the reliability of working. 
     Incidentally, the electrostatic attractor will produce the same effect as mentioned above when it is applied to any apparatus which is designed to fabricate works of a conductor or semiconductor (such as silicon substrate) in a reduced pressure atmosphere. It may be used as a chuck for the chemical vapor deposition apparatus, physical vapor deposition apparatus, milling apparatus, etching apparatus, ion implantation apparatus, or the like. 
     The electrostatic attractor in this example permits the dielectric plate to have an improved heat resistance without impairing its dielectric breakdown strength. If the electrostatic attractor according to the present invention is used as a chuck for the apparatus for fabrication in a reduced pressure, it is possible to reduce the occurrence of foreign matter resulting from the cracking of the dielectric plate. 
     The composite material of the present invention has a low thermal expansivity, a high thermal conductivity, and a good plastic workability. Therefore, it permits mass production with reduced manufacturing steps. 
     The composite material of the present invention also has the mixed structure of a Cu phase (with extremely high thermal conductivity) and a Cu 2 O phase (with low thermal expansivity); therefore, it has the characteristics of both of them. The composite material of the present invention will have a low thermal expansivity and a high thermal conductivity if the Cu content and Cu 2 O content are adequately adjusted. The composite material of the present invention will find use as a radiator plate for semiconductor devices and a dielectric plate for an electrostatic attractor.