A METHOD AND AN APPARATUS FOR MANUFACTURING AN ARTICLE OF A COMPOSITE MATERIAL, AN ARTICLE, DISC BRAKE, A COMMUTATOR AND A COMMUTATOR BRUSH MADE BY THE METHOD

Abstract: A method of fabricating articles of manufacture of a composite material by curing a curable matrix-forming binder in a compound material under simultaneous application of pressure and ultrasonic energy; an apparatus to be used in carrying out the method, and articles of manufacture fabricated according to the method. Articles according to the invention are useful in a multitude of applications, particularly in applications where the article must retain its shape and properties when subjected to temperatures above the melting point of usual thermoplastic materials, e.g. above 1000 DEG C. The method provides dense, thermally stable, and coherent articles of manufacture of composite materials having a desired high density. Forming and curing times are typically 10 times shorter than conventional methods, e.g. for brake pads of the order of about 3 - 5 seconds.

Description: A method and an apparatus for manufacturing an article of a composite material, an article, disc brake, a commutator and a commutator brush made by the method. 1. BACKGROUND OF THE INVENTION Field of the Invention The invention relates to a method of fabricating an artic- le of manufacture of a composite material by providing a compound material; producing a preform by forming and com¬ pacting the compound material; producing the article by curing a curable matrix-forming binder; and optionally post-curing the matrix in the article; an apparatus to be used in carrying out the method, and articles of manufac¬ ture fabricated by the method. Articles of manufacture of composite materials according to the present invention are useful in a multitude of ap- plications particularly where in use the article must re¬ tain its shape and properties when subjected to temperatu¬ res above the melting point of usual thermoplastic materi¬ als, e.g. above 1000 °C. Typical examples of articles in¬ clude friction pads, commutators, rubber parts, heat shields, electrical insulations, connectors, machinery parts, and magnets and bearings. Prior Art Disclosure GB Patent Application No. 2 012 204 discloses a composite friction assembly comprising at least one friction member and a support member, said friction member being formed from a mixture of a thermosettable phenol-aldehyde resin and filler material by heating a mould to a temperature of the resin, usually between about 160 °C and about 180 °C, and exerting on the mixture a pressure, normally between about 30,000 psi and about 50,000 psi in a time between about 2 second and 10 second. EP Patent Application No. 0352363 discloses an acrylic containing friction element manufactured by compressing a mixture comprising a thermosetting organic binder, a fi¬ brous reinforcing material, and an effective amount of fi- brillated acrylic polymer fibers to form a preform; pres¬ sing the preform at elevated temperatures; treating the pressed material at a temperature sufficient to effect cu¬ ring and then forming a friction element such as disc bra¬ kes, friction pads, clutch linings from the cured materi¬ al. The pressure to form the preform is in the range from 2000 to 5000 psi (140-350 kg/cm 2 ), and the curing of the preform is accomplished by heating to a temperature in the range from 350 to 600 °F (175-315 °C) for about 15 min., whereafter the preform is post-baked for several hours. A disadvantage of these processes is that the compaction of the compound material has to be carried out at pressu¬ res as high as 200-500 kg/cm 2 , or more, for a satisfactory flow and compaction of the moulding material to occur which requires costly tooling and press equipment. Further, for economically short forming and curing times, the cure of the curable matrix binder has to proceed at an elevated curing temperature typically in the range from about 135 "C to about 250 °C, or more, to ensure that the curing temperature has been reached in all parts of the article. Otherwise, if lower curing temperatures are ap¬ plied, long forming and curing times are required which limits the production rate. The curing time depend on the nature of the curable matrix binder and the dimensions of the article. For large artic¬ les, such as friction elements for brake pads, the curing time can be from about 15 min. to about 75 min., or more, before sufficient mechanical stability is obtained, and the article can be removed from the mould and transferred to an oven for post-cure. Another disadvantage of these processes is that the hea¬ ting is provided by conductive transfer of heat from the mould into the compound material the homogeneity of which heat transfer is difficult to control and results in a non-uniform polymerisation of the curable matrix-forming binder. This deficiency of conductive heat transfer into moulds has been recognized, and methods of providing a homoge- neous and accelerated transfer of energy into the compound material have been disclosed. EP Patent Application No. 0 347 299 discloses the use of capacitative microwave heating at pressures from 50 to 200 bars in moulding glass-filled unsaturated polyester resin- bonded composites; and German Laid Open Patent Application No. 29 06 842 discloses the use of capacitative high fre¬ quency microwave heating with a frequency of 2450 MHz for moulding of thermosetting materials. Both these methods are not suitable for composite materials containing signi¬ ficant amounts of metals. Further, they involve electrical shielding which is impractical to handle, and the appara¬ tus is complicated. EP Patent Application No. 0 093 655 discloses a method of fabricating an organo-metallic composite material compri¬ sing a mixture of a thermosetting resin, a metallic pow¬ der, and additives intended to confer certain properties to the final product by simultaneously application of in- duction heating and pressure, said pressure ensuring a good electrical conductivity of the composite material. This method requires a high content of electric conducting material having an appreciable hysteresis loss. GB Patent Applications Nos. 2 106 823 and 2 135 412 dis- close a method of resistive heating and sintering of me¬ tallic friction materials including a method of producing a friction assembly of friction material to a support mem¬ ber using resistive heating. This method requires a suffi¬ ciently high proportion of electrically conducting materi- al. Besides the disadvantages mentioned these processes have a high probability of providing articles having void forma¬ tions and non-uniform distribution of material components, particularly when the compound material comprises particu- late materials of different sizes and densities and/or comprises one- or more constituents in very low concentra¬ tions. Alternative methods of heating by application of ultra¬ sonic energy have been disclosed. US Patent No. 4487 728 discloses a method of producing mouldings of specific thermoplastic materials in a multi- cavity mould using ultrasonic vibration. Sintered blanks are obtained which are capable of further thermo-forming to the required shape. US Patent No. 4 548 771 discloses a method of vulcanizing conventional rubber materials comprising 75 % by volume of base elastomer, thus exclusively elastomeric in nature, and less than 25 % by volume of filler material by initi¬ ally applying ultrasonic energy at a maximum intensity of 31 W/cm 2 and asymptotically reducing the intensity to 40- 45 % of its initial value in the course of 3-5 min. there¬ by avoiding degradation of the elastomer due to exposure to excessive heat. Nothing is disclosed or suggested about curing composite materials containing a curable matrix- forming binder in less than 5 to 50 % by volume. Methods of producing friction products by a two-step pro¬ cedure comprising preheating of frictional material by ap¬ plying ultrasonic vibrations onto the material; and then applying pressure to the preheated material have been dis¬ closed. WPI Ace. No. 83-26393K/11 publishes an abstract of Japane¬ se Patent Application No. 58 020 413 (Australian Patent Application No. 86289-82) disclosing a method of moulding a friction material comprising providing a back metal on a support bed; filling particles of a friction material in the moulding cavity formed between a die and the support bed; melting the particles by heating using ultrasonic vi¬ bration; then transferring the die and support bed, the particles and the back metal to a pressing process wherein the particles are moulded so that the moulded friction ma¬ terial is welded to the back metal. WPI Ace. No. 84-265815/43 publishes an abstract of Japane¬ se Patent Application No. 59 023 804 disclosing a method of producing a friction product for brakes comprising pre¬ heating a frictional powder containing inorganic, organic and/or metallic fibres, friction adjuster, filter, and or¬ ganic coupler, and hot press-forming the powder. WPI Ace. No. 85-046916/08 publishes an abstract of Japane¬ se Patent Application No. 60 004 536 disclosing a method of moulding a frictional member comprising placing a back metal treated with an adhesive on the bottom of a mould; charging a powdered frictional material onto the back me- tal; preheating the frictional material by applying ultra¬ sonic vibrations onto the powdered frictional material; and applying a high pressure to the frictional material either by means of the vibration horn of the ultrasonic vibrator, or a hot press, thereby obtaining that moisture and gasses are removed from the frictional material during preheating; venting is not required in the subsequent sta¬ ge of moulding under application of high pressure to the frictional material; and moulding can be done in a short time period. Patent Abstract of Japan Vol. 11, No. 1 (M-550) publishes an abstract of Japanese Patent Application No. 61 181 630 disclosing the use of ultrasonic energy in friction hea¬ ting of sinterable powders. Materials are vibrated until their melting point is reached at which stage they sinter together at the points of contact. The method is aimed specifically at the manufacture of porous materials which do not contain a polymeric binder. An ultrasonic wave forming method comprising simultaneous application of ultrasonic wave oscillation and forming un¬ der pressure to the friction material is mentioned. How¬ ever, this application teaches away from a method of fra- bricating an article of manufacture by a one-step process applying ultrasonic heating and pressure simultaneously, because increasing pressure allegedly results in a retar¬ dation of the speed of the ultrasonic wave oscillations. 3. SUMMARY OF THE INVENTION Method of Fabrication It is the object of the present invention to provide a me¬ thod of fabricating a dense, and coherent article of manu¬ facture of desired high density. Further, it is the object of the present invention to pro¬ vide such a method wherein the article of manufacture has a reduced porosity and formation of voids. Also, it is the object of the present invention to provide such a method wherein the curable matrix-forming binder may be uniformly cured in a short time. It has previously been assumed that ultrasonic energy can- not be used to cure powdery materials containing a heat curable matrix-forming binder under pressure in an inte¬ grated heating and curing process because the ultrasonic energy cannot dissipate sufficiently in the powdery mate¬ rial to initiate and maintain the heat curing process. However, it has surprisingly been found that an excellent integrated compacting, heating and curing process can be obtained by proper selection of pressure and amplitude of the ultrasonic vibration. According to the invention, these objects is fulfilled by providing a method of fabricating an article of manufactu¬ re as defined in claim 1. By the above defined selection of the ultrasonic radiation proper dissipation of ultrasonic energy is ensured. The transferred ultrasonic energy is primarily transferred to particulate material particle oscillation energy, which subsequently is transformed to uniformly distributed heat. The desired high density is thus easily obtained by a com¬ pacting mechanism provided by the combined action of suit¬ ably adjusted external pressure and controlled inter par¬ ticle movements. The desired uniformity of the cured matrix material is en¬ sured by the uniform dissipation of the ultrasonic energy to heat, whereby a desired rapid increase in temperature can also be obtained. "Pressure and Ultrasonic Energy Dissipation" The pressure used in the method may vary within wide li¬ mits. Pressures from 10 to 200 kg/cm 2 are normally suita- ble. Higher pressures can be used, if necessary. Preferab¬ ly pressures from 60 to 120 kg/cm 2 , most preferably from 70 to 100 kg/cm 2 , are used if the ultrasonic energy is applied at a constant pressure. Otherwise, by applying a pressure profile and a constant a,plitude of the ultrasonic oscillations, the pressure is in the range from 5 to 60 kg/cm 2 , preferably from 10 to 40 kg/cm . The ultrasonic energy may vary within wide limits. Gene¬ rally a frequency above 18 kHz, preferably from 18 to 40 kHz, most preferably about 20 kHz is used. Particularly critical is the amplitude of the ultrasonic oscillation which should be suitably small depending on the pressure applied. Thus, besides providing a compacting pressure for compacting the powdery material, the applied pressure shall provide sufficient coupling between the ul¬ trasonic transducer and the material. Thus, a high pressu- re increases the probability for attenuating the oscilla¬ tions. Therefore, it turns out to be necessary to reduce the amplitude of the ultrasound oscillations rather than to increase the amplitude. This reduction can be obtained by use of an inverted sonic amplitude booster. In an alternative method of fabrication, simultaneous ap¬ plication of pressure and ultrasonic energy can be applied at a constant amplitude of the ultrasonic oscillations by applying pressure profile comprising applying an initial pressure of 10 kg/cm 2 and allowing the ultrasonic energy to dissipate for 2 to 5 seconds; allowing the pressure to rise at an even rate to 30 kg/cm 2 in the course of 3 to 5 seconds and ultrasound energy dissipation continued; dis¬ continuing the ultrasonic energy transfer; and imposing a dwell period of 2o to 30 seconds wherein the pressure is maintained at 30 kg/cm 2 while the mould is cooled. It is thus obtained that the method can be carried out at a much lower pressure. Compared to prior art techniques, the present invention provides articles of manufacture having a more uniform consistency, controlled porosity, and fewer voids. Another advantage of the process is the reduced curing time, form¬ ing and curing times often being more than 10 times shor- ter than conventional processes. Thus, typical forming ti¬ mes of brake pads according to the invention are 3-5 se¬ conds. Further, according to the invention, the method can be used to manufacture a composite article comprising at least one support element. In another preferred embodiment, the particulate material is comprising a reinforcing material, an electric conduc- tive material, or both. Also, if even higher production rates are required, the article can be partly cured in the apparatus and trans¬ ferred to post-curing by a conventional heating. "Curable Matrix-Forming Binder" According to the invention any curable binder producing cross linked or three dimensional structures may be used as the matrix-forming binder. The matrix-forming binder include condensation-type ther¬ mosetting polymers including condensation polymers of formaldehyde combined with phenol, urea, melanin, or re- sorcinol; diallyl phthalate, and diallyl isophthalate; polyester resins including addition-type unsaturated poly¬ ester and condensation resins obtained from the reaction of polyols and multifunctional carboxylic acids such as adipic or terephtalic acids; vinyl esters ; epoxy polymers including diglycidyl ether of bisphenol A, epoxy-novolak resins obtained from the reaction of epi- chlorohydrin and a phenolic-novolak resin cured conven¬ tionally by addition of amines or anhydrides; polyamide-imide polymers; polyimide polymers; polyurethanes including the polymerisation products of polyols and di-iso cyanates such as trimethylol propane and toluene diisocyanate; and heat resistant silicone polymers including phenyl-methyl or methyl hydroxy-functional silanol products which are brought to react with phenolic resins, epoxy resins, po- lyester resins or other resinsous materials containing hydroxy1 groups. "Particulate Material" According to the invention any particulate material may be used including mineral particles, e.g. calcium carbonate, metaloxides, baryte, silica (sand), clay, glass spheres, graphite, carbon black, or coke powder; reinforcement materials such as heat resistant man-made fibers including mineral fibers, aromatic polyamide fi¬ bers, novolak fibers, glass fibers, carbon fibers, sponge iron, dendritic copper, and crushed magnetic neodynium boron iron; heat resistant minerals with elongated crystal form and an aspect ratio greater than 3 including wollastonite, atta- pulgite, and sepiolite; and heat resistant crystals with a micaceous form including muscovite, phlogopite, lepidolite, biotite, and micaceous haematite. Also, organic particles or fibers may be used, e.g. saw dust and textile fibres, and particularly graphitized carbon fibers, conductive fillers, including conductive carbon black, conductive polymers, including polyethylene oxide, or electronically conductive polymers, including polyacetylene. "Other Additives" According to the invention additives may be added such as antioxidants, antistatics, colorants, coupling agents, flame redardants, foaming agents, heat stabilizers, impact modifiers, lubricants, curing agents (initiators, accele- rators, and catalysts), plasticizers, preservatives, and processing aids (mould release agents, antiblocking agents, emulsifiers, viscosity depressants), rock wool, etc. Apparatus of Production A further object of the present invention is to provide an apparatus of production to be used in carrying out the me- thod of fabricating an article of manufacture of a compo¬ site material according to the invention having at a high rate of production, a uniform quality and a low cost com¬ pared to conventional production apparatus. This object is fulfilled by providing an apparatus as defined in claim 7. Article of Manufacture A still further object of the present invention is to pro¬ vide an article of manufacture comprising a dense, ther¬ mally stable, and coherent composite material of desired high density. Examples of such articles are disc-brake pads, hard magnet elements, soft iron articles, woven glass fiber pads, heat resistant electrical insulating articles, etc. This object is fulfilled by providing an article of manu- facture as defined in claim 8. Definition of Expressions Within the present context the expression a "particulate material" is intended to designate a material in a fluid form of powder, preferably a dry powder. A powdery mate- rial may comprise materials in form of powder, fibers (reinforcements), laminars, particulates (fillers), etc. These materials may include reinforced composite materi¬ als. Within the present context the expression "compound mate¬ rial" designates an admixture of a curable matrix-forming binder with at least one particulate material and option¬ ally other additives including fillers, softeners, plasti- cizers, reinforcements, catalysts, pigments, or dyes. Within the present context, the expression "composite ma¬ terial" designates a combination of two or more distinct materials comprising a particulate material and a matrix which materials differ in form or composition on a macro- scale. The constituents of the composite material retain their identities, i.e. they do not dissolve or merge com¬ pletely into one another, although they act in concert. Normally, the components can be identified and exhibit an interface between one another. Within the present context, the expression "matrix" de¬ signates an essentially homogeneous coherent phase in a composite material in which the particulate materials of the composite is embedded. Within the present context, the expression "a curable ma¬ trix-forming binder" is a precursor for the matrix which is transformed to an essentially homogenoeus coherent phase of cured binder in the composite material during the fabrication of said composite material. Within the present context, the expression "cure" designa¬ tes the irreversible change of the properties of a thermo- setting resin by chemical reaction. 4. BRIEF DESCRIPTION OF DRAWINGS Fig. 1 shows a sectional sketch of a disc brake pad manu¬ factured by the method according to the invention, and Fig. 2 shows a distribution of shear strengths of disc brake pads fabricated according to the invention and com¬ pared to conventionally produced disc brake pads. 5. DETAILED DESCRIPTION Apparatus of Production Referring to Fig. 1, an ultrasonic compacting and curing apparatus 10 comprises an electric oscillator 11 generat¬ ing electric oscillations in the range 18 to 200 kHz; an ultrasound generating unit 120 comprising a piezo-electric crystal converting electrical oscillations to mechanical oscillations, an inverted sonic amplitude booster 121 am- plifying/attenuating the amplitude of the mechanical os¬ cillation and generating a desired oscillation pattern, i.e. a distribution of maxima, minima, and nodal points of the oscillations, and a sonotrode or horn 122 designed and shaped to transfer maximum ultrasound energy to a disc brake pad 150,151,152 being moulded and cured; a mould or die 130 having movable parts and enclosing a die cavity 131; and a pressure generating device 140 applying a static predetermined pressure on the die 130 and sub¬ sequently the backing plate 152 of the disc brake pad being moulded and cured. A specific apparatus comprises an electric oscillator 1300 P supplied by Branson Sonic Power A/S, Kastrup, Denmark. "Booster and Sonotrode" Generally, the ultrasound energy transfer from the sono¬ trode 122 to the compound material depends on the ampli- tude and frequncy of the ultrasound oscillations and on the pressure by which the energy is transferred to the ma¬ terial. However, in order to be able to apply sufficient energy at the beginning of the moulding operations without complete¬ ly attenuating the oscillations, the combination of ampli¬ tude of the ultrasound oscillation and the applied pressu¬ re must be optimized. Thus, it is advisable to reduce the amplitude of the oscillations by inverting the booster when a high moulding pressure is applied. Alternatively, especially for materials with a well-estab¬ lished plastic flow when heated to the plastic stage, it can be necessary to reduce the pressure in order to main- tain ultrasound energy dissipation at the required level. Thus, in designing a proper ultrasonic compacting and cu¬ ring apparatus for the manufacturing of a given article, the sonotrode 122 is shaped according to the article and further designed to transfer maximum ultrasound energy of the desired frequency and amplitude depending on the mate¬ rial to be moulded and cured and depending on the pressure applied. Then the booster 121 is designed to meet the re¬ quirements of the sonotrode 122 and a given conventional ultrasound converter 120. Further, in optimizing the ultrasound energy transfer to the material, particularly composite materials comprising a plurality of components, the frequency, amplitude and pressure can be varied during the manufacturing process. 6. EXAMPLES EXAMPLE 1 Preparation of a Non-Asbestos Disc Brake Pad A non-asbestos disc brake pad, e.g. 150,151,152 as illu¬ strated in Fig. 1, has been prepared according to the in¬ vention by co-compacting a non-asbestos friction material 150 of formulation (A) (see below) with an adhesive-pro¬ moting underlayer 151 of the composition (B) and com¬ pacting said material and layer to a steel backing plate (152) followed by curing the combined friction material, underlayer and backing plate by simultaneously applying a constant pressure of 150 kg/cm 2 and ultrasonic energy dissipation of 165 kW/kg (3.3 kW per 20 g compound mate¬ rial) using an inverted Black 1:2.5 Booster supplied from Branson Sonics Power A/S, Kastrup, Denmark. A^ Friction material formulation of the following composition by volume: Artificial mineral fibres: 16.2 % Novolak phenolic matrix-forming binder: 14.8 % Powdered nitrile elastomer: 8.2 % Barytes: 10.5 % Granulated electrode graphite: 5.5 % Hematite: 6.0 % Muscovite mica: 16.0 % Calcium silicate: 10.0 % Petroleum coke: 6.0 % Lead sulphide: 6.8 % B. Adhesion-promoting underlayer of the following composition by volume: Novolak phenolic matrix-forming binder: 25 % Powdered nitrile rubber: 12 % Rockwool lapinus 4164 fibre: 63 % 30 g of the formulation A and 10 g of the underlayer B were transferred to a 16 cm 2 die cavity of an ultrasonic compacting and curing apparatus as shown in Fig.l. A steel backing plate 152 was inserted between the under¬ layer B of the compacted layered structure of friction ma¬ terial A and adhesion-promoting underlayer B into the die cavity 131 by removing the platten 141 of the pressure ge¬ nerating device 140 a few millimeters. Pressure was then applied to the back plate 152. On reach- 2 ing a pressure of 138 kg/cm , ultrasound of 20 kHz was ap- plied at a power of 3300 W for a period of 6 s and then switched off. The pressure was held for a further 6 s and then released. The finished disc pad was ejected from the mould by removing the die platten 141. The disc pad was then post-cured by conventional heat treatment in an air oven for 10 hours at 160 °C. In an alternative method of fabrication, simultaneous ap¬ plication of ultrasound energy and pressure was applied by an initial pressure being 10 kg/cm 2 and the ultrasound be¬ ing dissipated for 2 to 3 seconds whereafter the pressure is allowed to rise at an even rate to 30 kg/cm 2 in the course of 3 to 4 seconds and ultrasound energy dissipation continued, herafter the ultrasound energy transfer is dis- continued and a dwell period of 24 seconds is imposed wherein the pressure is maintained at 30 kg/cm 2 while the mould is cooled. Comparison of Disc Pads The prepared disc pads were compared to disc pads prepared from the same disc brake formulation (A), adhesion-promo¬ ting underlayer (B), and steel backing plate, but cured using conventional heating. In one batch B2, 17 dies brake pads were manufactured ac¬ cording to the invention were subjected to a shear strength, all falling at a shear strength above 50 kg/cm 2 as shown in Fig.2. The 17 disc brake pads had an average shear strength of about 67 kg/cm 2 with a range from 60 to 74 kg/cm 2 compared to the minimum acceptable shear strength of 50 kg/cm 2 . 100 conventionally heat-cured dies brake pads had all an average shear strength of about 60 kg/cm 2 and a signifi¬ cantly larger range from 40 to 80 kg/cm 2 . In another batch Bl, 57 disc brake pads manufactured ac¬ cording to the invention were subjected to a shear test, all failing at a shear strength above 50 kg/cm 2 as shown in Fig. 2. 57 disc brake pads had an average shear strength of about 60 kg/cm 2 with a range from 52 to 74 compared to the mini- mum acceptable shear strength of 50 kg/cm . Besides shorter manufacturing times of few seconds com¬ pared to minutes for conventional heat curing, the shear strength tests show that pressure and ultrasound-induced curing according to the invention provides a much stronger article, and a significantly improved homogeneous quality of production. Friction Tests Disc pads manufactured according to the invention were tested on a Friction Test Machine from Allied Signal GmbH, Reinbed, Germany capable of performing tests a constant rubbing speed according to the procedures adopted as an industrial standard in Europe. The test was carried out at 660 rpm at a constant torque of 120 Nm on a disc pad used in a frontwheel application on a 750cc motorcycle. Friction test results for normal pads (Test no. 8) and for pads prepared according to the invention (Test no. 188) are shown in Table 1. TABLE 1 Friction Test Results Test No. Material Av μ Min α Max (i Cold μ Fade u Wear Pad 1 Wear Pad 2 The results shows that the friction coefficient has been raised slightly, due to an improvement in frictional sta¬ bility in single brake applications, while the wear rate has not been changed. There is a marginal improvement in fading performance. EXAMPLE 2 Hard Magnet Elements Magnets were made of Neodynium boron magnetic material suspended in a Novolak phenolic matri -forming binder using the following procedure. 100 g of crushed metal al¬ loy material was intimately mixed with 10 g Novolak, and the mixture was placed in a cylindrical die cavity and subjected to a pressure of 200 kg/cm 2 and simultaneously ultrasound energy of 20 kHz and density 500 kj per kilo¬ gram weight of compound material. EXAMPLE 3 Soft Magnetic Core Article 100 g σarbonyl iron of a particle size of 6-8 μm was in- timately mixed with 50 g of a 30 % alcoholic solution of a bisphenyl epoxide. 2 g phthalic anhydride was added, and the mixture was dried to a powder. The mixture was cured in a mould shaping the material to the required form while the polymeric binder cross-linked sufficiently to maintain shape during the subsequent post-cure. This was carried out by subjecting the material to a pressure of 200 kg/cm 2 while simultaneously being subjected to ultrasound of 20 kHz for a total energy dose of 100 kJ per kilogram weight of compound material. The compressed article was post cured at 150 °C for 20 minutes. The cylindrical article was a magnet having a very low hysteresis loss. EXAMPLE 4 Pads of Woven Glass Fibers A pad of woven glass fibers was saturated with a liquid polyester polymer binder containing 10 % (w/w) calcium carbonate powder, 1 % benzoylperoxide and 1 % cobalt naph- thanate. The pad was cured for 5 seconds under a pressure of 120 kg/cm 2 and ultrasound of 20 kHz and a total energy dose of 50 kJ per kilogram weight of compound material. EXAMPLE 5 Heat Resistant Electrical Insulating Article A dough of 70 % amorphous silica based composite material and 30 % silicone polymer binder was transferred to a mould for an insulating cup and subjected to a pressure of 200 kg/cm 2 and ultrasound of 20 kHz and a total energy dose of 1000 kJ per kilogram weight of compound material. EXAMPLE 6 Commutator An electric motor commutator having an outer diameter of 20 mm, height 24 mm and internal bore of 10 mm was pre¬ pared from 13 g of a mixture containing 30 % by weight of phenolic resin as binder and 70 % by weight filler con¬ sisting of glassfibers and silica. The mixture was transferred to a 20 mm inner diameter mould and placed as a powder inside a commutator copper ring. The commutator was pressed at 160 kg/cm 2 and simul¬ taneously exposed to ultrasound at a frequency of 20 kHz in 7 seconds. The commutator was left for cooling for 25 seconds in the mould. Then post-cured at 180 °C for 8 hours. The commutators manufactured showed no internal porosity and step arbor tests of the material showed an expansion at break of 6 micrometers and an ultimate strength of 210 to 400 Kg with an average of 301 kg. The compression stregth was found to be significantly im- proved compared to conventionally processed commutators. In the axial direction the longitudinal breaking force for three commutator tubes was 7500 for all three. In the ra¬ dial direction the compression force at failure was 454, 504 and 468 kg. it is anticipated that the significantly improved physical properties is due to an improvement of the preferential orientation of the reinforcing fibers of the composite ma¬ terial when compacted using ultrasonic energy. The conventional process involves compression of preformed or granulated material which flows into the annulus of the die. During this flow process the reinforcing fibre tend to orientate longitudinally and parallel to the axis. This reduces the burst and compression stregth of the article. When these articles are compacted using ultrasound the en¬ hanced material flow in the loosely filled powdered mate¬ rial yields a compacted article where there is much less preferential orientation in the axial direction. As more fibre is orientated tangentially or circumferentially the step arbour test results are much more uniform at an im- proved level. Compression tests in the longitudinal and radial direction are improved and show a smaller distri¬ bution. EXAMPLE 7 Commutator Brush An electrical contacting brush for use in electrical mo- tors, having a length of 25 and a square cross sectional area of 1 cm 2 was manufactured from a compound material composed by volume as follows: Granulated Electrode Graphite 0-0.5 mm: 30 % Powdered Graphite Lonza KS6: 15 % Conductive Black Ketjen EC: 7 % Bronze Powder 90/10: 3 % Phenolic Resin J1311H: 32 % Sigrafil Carbon Fibre SF01MNT: 4 % Kynol Novolak Fibre KF0203: 3 % Kynol Novolak Fibre KF05BT: 3 % Powdered Cuprous Sulfide: 3 % The material was filled into a mould die with a sectional length of 25 mm and a sectional height of 10 mm so that the final dimensions were 25 x 10 x 10 mm. The plunger was dropped and pressure applied at 100 kg/cm 2 . Ultrasonic energy was applied for 2.3 s and the pressure was main¬ tained for a further 3 s before the brush was ejected from the mould. The finished item had an electrical resistivity of 0.128 Ohm cm.

Claims: P A T E N T C L A I M S : 1. A method of fabricating an article of manufacture of a composite material comprising the steps of: a) providing a compound material consisting of a mixture of: i) a curable matrix-forming binder, ii) at least one particulate material, and iii) optionally other additives; b) producing a preform by forming and compacting the com- pound material into a desired compact form; c) producing the article by curing the curable matrix- forming binder in said preform; and d ) optionally subjecting the matrix in the article produ¬ ced in step (c) to post-curing; wherein the amount of curable matrix-forming binder is in the range from 5 to 50 %, preferably from 15 to 45 %, particu¬ larly from 20 to 35 % by volume of the compacted compound material of the preform, and the compacting and curing processes in step (b) and (c) comprise: i) a compacting and heating phase wherein the compound ma¬ terial is subjected to pressure and ultrasonic energy dissipation, the pressure being larger than the inter¬ nal vapor pressure, and the amplitude of the ultrasonic radiation applied to the material is selected within a range allowing surmounting of the internal friction forces, a desired density being provided by the combined action of pressure and inter particle movements, and a uniform internal heating being essentially provided by inter particle friction, whereby a sufficient amount of ultrasonic energy is dissipated into heat to ensure formation of a coherent uncured matrix having a temperature at which the binder is ready to cure; ii) a subsequent incipient curing phase wherein the binder is cured to a desired degree by simultaneously apply¬ ing pressure and ultrasonic energy; and iii) optionally a subsequent dwell and consolidation phase wherein the binder is cured to a desired degree by applying pressure only; whereby the preform is cured to a degree to ensure safe handling and form stability of the article. 2. A method according to claim 1, c h a r a c t e r ¬ i z e d in that the applied pressure is kept constant with a value within the range from 10 to 200 kg/cm 2 , pre¬ ferable from 60 to 120 kg/cm 2 , particularly from 70 to 100 kg/cm 2 . 3. A method according to any of claims 1-2, c h a r a c t e r i z e d in that the ultrasound energy density per weight compound material under pressure is in the range from 33 to 16500 kJ/kg, preferable from 50 to 5000 kJ/kg, particularly from 100 to 800 kJ/kg. 4. A method according to any of claims 1-3, c h a r a c t e r i z e d in that the applied ultrasound energy dissipation rate is in the range from 33 to 660 kW/kg, preferable from 50 to 400 kW/kg, particularly from 66 to 165 kW/kg. 5. A method according to any of claims 1-4, c h a r a c t e r i z e d in that the ultrasonic energy has a frequency generally above 18 kHz, preferable from 18 to 40 kHz, particularly about 20 kHz. 6. A method according to claims 1-5, c h a r a c t e r i z e d in that the article is post- cured by thermal heating. 7. Apparatus to be used in a method of fabricating an article of manufacture of a composite material according to any of claims 1-6 comprising: a) an electric oscillator; b) an ultrasound generating device; c) a sonically tuned energy transfer system comprising a sonic amplitude booster and a sonotrode; d) a closed mould cavity; and e) a pressure generating device, c h a r a c t e r i z e d in that the sonic amplitude booster is an inverted sonic amplitude booster. 8. An article of manufacture of a composite material com¬ prising a matrix, at least one particulate material, and optionally other additives fabricated by a method accor- ding to claims 1-6. 9. An article according to claim 8, c h a r a c t e r ¬ i z e d in that it further comprises at least one support element. 10. An article according to claims 8-9, c h a r a c ¬ t e r i z e d in that the particulate material comprises a reinforcing material. 11. An article according to claim 10, c h a r a c - t e r i z e d in that the reinforcing material is selec¬ ted from a group consisting of heat resistant man-made fibers including mineral fibers, aromatic polyamide fibers, novolak fibers, glass fibers, carbon fibers, sponge iron, dendritic copper, and crushed magnetic neodynium boron iron; heat resistant minerals with elongated crystal form and an aspect ratio greater than 3 including wollastonite, atta- pulgite, and sepiolite; and heat resistant crystals with a micaceous form including muscovite, phlogopite, lepidolite, biotite, and micaceous haematite. 12. An article according to claims 8-11, c h a r a c ¬ t e r i z e d in that the particulate material is an electric conductive material. 13. An article according to claim 12, c h a r a c ¬ t e r i z e d in that the electric conductive material is selected from a group consisting of graphitized carbon fibers, conductive fillers, including conductive carbon black, conductive polymers, including polyethylene oxide, or electronically conductive polymers, including polyace- tylene. 14. An article according to claims 8-13, c h a r a c t e r i z e d in that the matrix is a hard, durable, and infusible thermoset polymer produced by curing a curable matrix-forming binder under influence of heat. 15. A method according to claims 8-14, c h a r a c ¬ t e r i z e d in that the matrix-forming binder is selected from a group consisting of a condensation-type thermosetting polymer including con¬ densation polymers of formaldehyde combined with phenol, urea, melanin, or resorcinol; diallyl phthalate, and di¬ allyl isophthalate; polyester resins including addition-type unsaturated poly¬ ester and condensation resins obtained from the reaction of polyols and multifunctional carboxylic acids such as adipic or terephtalic acids; vinyl esters ; epoxy polymers including diglycidyl ether of bisphenol A, epoxy-novolak resins obtained from the reaction of epi- chlorohydrin and a phenolic-novolak resin cured conven¬ tionally by addition of amines or anhydrides; polyamide-imide polymers; polyimide polymers; polyurethanes including the polymerisation products of polyols and di-iso cyanates such as trimethylol propane and toluene diisocyanate; and heat resistant silicone polymers including phenyl-methyl or methyl hydroxy-functional silanol products which are brought to react with phenolic resins, epoxy resins, polyester resins or other resinsous materials containing hydroxyl groups. 16. A disc brake comprising a layered structure of a friction material, an adhesion-promoting underlayer, and a steel backing plate fabricated according to claims 1-6. 17. A commutator comprising an electrical conducting material fabricated according to claims 1-6. 18. A commutator brush comprising an electrical conduc- ting material fabricated according to claims 1-6.

Inventors: LINDGAARD TORBEN, THOMAS DAVID MORGAN, LINDGAARD, TORBEN, THOMAS, DAVID, MORGAN
Applicants: OBTEC AS, OBTEC A/S
Application year: 1991
Main classification: H01R39
IPC codes: B29C35, B29C43, B29C67, B29C70, B29K103, B29L31, F16D65, F16D69, H01B1, H01F41, H01R39, H02K13