Abstract:
A printed circuit board composed of an epoxy impregnated nonwoven web substrate laminated to electrically conductive sheets is presented. The printed circuit board is flexible in the sense that it can be bent to any desired multiplanar shape and will retain that shape after installation as required by electronic interconnection systems. The printed circuit board also has improved thermal properties achieved through the addition of up to 70% by weight of low coefficient of thermal expansion (CTE) particulate fillers and/or the use of thermally stable reinforcement fibers in the non-woven web.

Description:
CROSS REFERENCE TO RELATED APPLICATION 
     This is a continuation-in-part Application of U.S. application Ser. No. 319,488 filed Mar. 6, 1989, and now abandoned. 
    
    
     BACKGROUND OF THE INVENTION 
     This invention relates to the field of printed circuit boards. More particularly, this invention relates to printed circuit boards having a fiber reinforced substrate which can be processed in a manner similar to rigid printed circuit board or hardboards but thereafter are bendable to retain multiplanar shapes. 
     The process for manufacturing a rigid printed circuit board or hardboard is well known in the art. The hardboard is produced in a panel form with the particular circuitry being etched, plated, screened or stamped thereon. Rigid printed circuit board of this type must necessarily only be used for single-plane hardboard applications since any bending would result in cracking and/or breaking. 
     In order to connect single-plane hardboards to other hardboards within the electronic device, expensive multiboard interconnections must be utilized. These interconnectors add both to parts costs and labor costs as well as increasing the complexity of a given installation. Multiplane circuitry can be achieved by: 
     1. Combinations of two or more rigid board segments interconnected by flexible jumper cables. 
     2. The mother-daughter board arrangement, using edge card connectors and, 
     3. Building a flexible circuit which is then selectively stiffened in sections which are designed for component mounting. 
     The above-discussed well known problems of building multiplanar circuits with both conventional rigid and flexible circuit boards have been overcome and alleviated by a novel bendable, shape retaining circuit board material described in U.S. Ser. No. 778,603 filed Sept. 20, 1985, which is assigned to the assignee hereof, all of the contents of which are incorporated herein by reference. This material is commercially available from Rogers Corporation, Rogers, Connecticut under the trademark BEND/flex. The circuit board material of prior U.S. Ser. No. 778,603 is made utilizing conventional hardboard processes. The circuit board is produced in sheet form, and can be converted into a printed circuit by using conventional hardboard processing techniques including component mounting. Thereafter, the unique properties of the prior material allow the printed circuit board to be formed into a predetermined three dimensional shape and thereafter mounted into electronic equipment. The formed printed circuit board will not crack and has sufficient stiffness to retain its shape after installation. 
     The manufacturing process of the circuit material of U.S. Ser. No. 778,603 includes forming a nonwoven web substrate of polyester and glass fibers, impregnating and saturating the web with an epoxy solution, and thereafter drying the web to drive off any solvent. The dry, tacky web is then laminated on one or both sides with sheets of copper to form a sheet of printed circuit board material. As with hardboard material, the sheet can be etched, punched, drilled or blanked out to form any desired circuit configuration and finally, the circuit with the mounted components can be formed or bent into a multiplanar configuration. 
     An important feature of the circuit material of U.S. Ser. No. 778,603 is its bendability and shape retention at room temperature. This key feature is achieved by carefully selecting the epoxy resin to exhibit a glass transition temperature (Tg) at or near room temperature. The Tg is typically in the range of 10-60° C. and preferably about 40-50° C. This glass transition is broad and spreads over 20-30° C. In addition to the epoxy matrix and nonwoven fabric web of glass and polyester fibers, the commercial bendable composite also includes flame retardant fillers. 
     As stated, the formable/bendable circuit material described above can be used to solve the problem of multiplane interconnections at a relatively lower cost than conventional techniques. In concept, portions of the bendable board function as the rigid segments while other portions of the same board function as the &#34;flexible&#34; interconnections in a multiplane configuration. 
     While well suited for its intended purposes, the circuit material of U.S. Ser. No. 778,603 does suffer from several problems related to its thermal properties including a perceived need for both improved plated through hole reliability and improved heat resistance. The circuit material of U.S. Ser. No. 778,603 has a coefficient of thermal expansion (CTE) in the Z-direction above the glass transition temperature of about 300-400ppm/°C. which limits the plated through hole reliability of the laminate in double clad circuit applications. 
     Also, the circuit material of U.S. Ser. No. 778,603 is comprised of polyester fibers which melt near standard solder reflow temperatures (250-260° C.) This may cause the prior art bendable circuit material to suffer from surface blistering and bulk structural fusion of the fibers&#39; network during solder reflow processing. 
     SUMMARY OF THE INVENTION 
     The above-discussed and other problems and deficiencies of the prior art are overcome or alleviated by the improved bendable and shape retaining circuit board material of the present invention. In accordance with the present invention, the circuit material of U.S. Ser. No. 778,603 is modified to contain up to 70% by weight of low CTE fillers and/or an additional weight fraction of higher melting point fiber reinforcement to improve the overall thermal properties of the material. As a result, the prior art problem of limited plated through hole reliability due to low CTE in the Z axis is improved by filling the circuit substrate (comprised of a non-woven web impregnated with epoxy) with low CTE particles such as glass spheres, silica or milled microglass fibers in a preferred filling range of about 20-50% by weight. 
     In addition, the prior art problem of limited heat resistance at solder reflow temperatures is alleviated by replacing the polyester component in the non-woven fabric web with a more thermally stable fiber such as an aromatic polyamide, a polyacrylonitrile or a similar polymeric fiber. The resultant circuit material will then easily withstand temperatures typical to the solder reflow process without deleterious effects. 
     The above-discussed and other features and advantages of the present invention will be appreciated and understood by those of ordinary skill in the art from the following detailed description and drawings. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     Referring now to the drawings, wherein like elements are numbered alike in the several FIGURES: 
     FIG. 1 is a graph showing a thermal cycling test for prior art bendable, shape retaining circuit board material; 
     FIG. 2 is a graph showing a thermal cycling test for circuit board material in accordance with a first embodiment of the present invention; and 
     FIG. 3 is a graph showing a thermal cycling test for circuit board material in accordance with a second embodiment of the present invention; and 
     FIG. 4 is an averaged comparison graph of the test data of FIGS. 1, 2 and 3. 
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENT 
     The circuit board of prior U.S Ser. No. 778,603 includes a fiber reinforced substrate laminated between one or more electrically conductive sheets. The substrate is made of a nonwoven blend of polyester and glass fibers forming a fabric web. This nonwoven web is thereafter saturated with an epoxy resin thus forming a polymer impregnated nonwoven web. 
     More particularly, the commercial laminate of U.S. Ser. No. 778,603 (sold under the trademark BEND/flex) is composed of an epoxy matrix, flame retardant compounds, and a nonwoven fabric reinforcement laminated with copper on one or both sides. The nonwoven reinforcement is composed of E glass staple fibers (0-100 weight %, 10-30 weight % preferred) with the balance of the nonwoven web composed of polyethylene terephthalate staple fibers such as Hoechst Celanese TREVIRA or DuPont DACRON fibers. The prior art composite contains 5-75 weight % nonwoven (20-40 weight % preferred) with the balance of the composite composed of a crosslinked epoxy resin and flame retardant compounds. 
     The flame retardant compounds used in the prior art are brominated organic compounds which comprise 5-50 weight % (20-30 weight % preferred) of the epoxy resin portion of the composite (including the weight of the fillers). The brominated organic compounds have good electrical properties and exhibit good thermal stability. The brominated fillers may be either solid or liquid. Decabromo-diphenyl oxide, pentabromo-diphenyl oxide, bis (2,3 dibromopropyl ether) of tetrabromobesphenol A, monofunctional brominated glycidyl ether, brominated imides such as ethylene bis tetrabromophthalimide and brominated di functional epoxy compounds are typical examples of this class of flame retardant chemicals. The flame retardant system is more effective if a synergistic antimony compound is also included as a filler. The quantity of the synergistic compound (such as antimony trioxide or antimony pentoxide) should be such that the molar ratio of bromine to antimony is between 1:1 and 5:1 (2:1-3:1 preferred). 
     The epoxy resin portion of the prior art composite is formed by reacting a multifunctional epoxy, a monofunctional epoxy and an anhydride or diacid. Typical multifunctional epoxies are glycidyl ethers of phenolic novolacs, glycidyl ethers of tetra phenylol ethane, or triglycidyl ethers of tris(hydroxy phenyl) methane and its isomers or oligomers. 
     Examples of monofunctional epoxies are aromatic or aliphatic glycidyl ethers and dibromo-phenyl glycidyl ether, all of which will function to lower the composite Tg. Room temperature bendability may also be achieved by including aliphatic diglycidyl ethers in the formulation. Typical anhydrides which may be used are: dodecenyl succinic, hexahydrophthalic, NADIC methyl, phthalic, succinic, tetrahydrophthalic, chlorendic, polyazelaic, polyadipic, and polysebasic anhydrides. The corresponding diacids of the aforementioned anhydrides may also be used. The anhydride to epoxy ratio is also important and may be varied from 0.5:1 to 1.5:1. The preferred range of anhydride to epoxy ratio is between 0.6:1 and 0.8:1. This preferred range results in optimum electrical and mechanical properties of the composite. 
     The prior art bendable laminate composite as described hereinabove suffers from two deficiencies. First, plated through hole (PTH) reliability is limited due to the high Z-axis (thickness) thermal expansion coefficient (CTE) of the composite above Tg (25-50° C.). The CTE of the composite above Tg is 300-400 PPM/° C. This high CTE limits the double sided applications which require plated through holes. The second problem is the potential melting and blistering of the polyester fibers during solder reflow or wave solder operations especially when the molten solder is above the recommended temperature. The melting and fusion of the polyester fibers results in embrittlement of the composite and lower PTH reliability. 
     In accordance with a first embodiment of the present invention, the problem of high Z-axis CTE is alleviated by adding low CTE inorganic particles or fibers to the resin formulation. As a result of the inorganic filler, the CTE in the Z direction of the overall composite material will be about 100-300 ppm/°C. Examples of inorganic low CTE particles include, but are not limited to clays or mineral fillers such as wollastonite, diatomaceous earth, mica, beta-eucryptite, silica, glass beads or spheres, milled glass fibers, milled mineral fibers, quartz fibers or particles, alumina fibers or particles, and calcium sulfate fibers. In order to obtain maximum benefit in CTE while maintaining processability of the composite, the loading levels (weight % of the resin fraction of the composite including the filler) of the fillers should be in the range of 20-70% (40-50% preferred). The use of coupling agents such as 3-aminopropyl-triethoxysilane or 3-glicidyloxpropyl-trimethoxysilane may be used to: (a) modify the mechanical properties of the composite (depending on whether the coupling agent is reactive or inert), (b) decrease moisture absorption, (c) improve dimensional stability. 
     In accordance with a second embodiment of the present invention, the potential problem of melting polyester fibers is overcome by replacing these low temperature (T m  =255° C.) fibers with organic fibers which have a higher thermal stability (preferably higher than 260° C.) Examples of higher thermal stability fibers include, but are not limited to aromatic polyamide (NOMEX, KEVLAR); phenolic, poly(acrylonitrile), polyester (KODEL), poly(phenylene sulfide), fluoropolymer (TEFLON), and other liquid crystalline or rigid rod type polymeric fibers. 
     As in the prior art laminate, the Tg of the epoxy is maintained at or near room temperature so that the Tg is in the range of 10-60° C.; and spreads over a range of 20-30° C. Also, it may be desirable to employ a catalyst/accelerator to facilitate in forming the composite circuit laminate. 
     Turning now to FIGS. 1-4, thermal cycling test data for the three materials set forth in Table 1 is graphically depicted (FIG. 4 is an averaged comparison of the data of FIGS. 1, 2 and 3). The thermal cycling test was conducted on a circuit board having a daisy chain pattern stringing sixty (60) holes with temperature cycling between 20° C. and 260° C. 
     
                       TABLE 1______________________________________                  NUMBER OF CYCLESFIG.  MATERIAL         TO FAILURE______________________________________1     Prior Art        422     NOMEX Reinforcement                  52 in non-woven web3     NOMEX reinforcement                  73 and 40% by weight silica______________________________________ 
    
     As is clear from a comparison of FIGS. 1, 2, 3 and 4, the bendable laminates with NOMEX high temperature fibers significantly improve PTH reliability relative to laminates with polyester non-woven webs. Moreover, the addition of silica (FIG. 3) further improves the performance of the composite which contains the NOMEX non-woven web. In fact, the combination of NOMEX and silica about doubles the reliability of PTH relative to the prior art bendable circuit board of U.S. Ser. No. 678,603. 
     The following are non-limiting examples of several embodiments of the present invention; all of which were found, subsequent to lamination and curing to be bendable and shape retaining at or near room temperature. 
     EXAMPLE 1 
     A mixture of 396g of hexahydrophthalic anhydride, 402g of polyazelaic polyanhydride, and 2020g of a polyfunctional glycidyl ether of phenolic novolac (average functionality of 3.6) were blended at l40° C. for 20-30 minutes. Once a homogenous mixture was obtained, 940g of tetrabromo bisphenol A, 560g of antimony trioxide (Sb 2  O 3 ), l500g of large (50 percentile 5 micron) particle size hydrated aluminum silicate and 1310g of small (50 percentile 0.8 micron) particle size hydrated aluminum silicate were stirred into the mixture of epoxy and anhydrides. 
     A fiber mixture (2850 grams) containing 40 weight % poly(ethylene terephthalate) (PET) 6 denier x 2&#34; long and 60 weight % 3 denier x 2.0&#34; long PET staple fibers (such as Dacron polyester from DuPont) were blended together on a fiber blender and formed into a nonwoven fabric web. The nonwoven webs could be varied in weight from 2 to 24 ounces/ft 2  depending on the thickness of the composite laminate desired. 
     The composite laminate was formed by coating a nonwoven web with the hot resin mixture using a two roll coater. The resin content of the composite was controlled by the distance between the two rolls. Resin to fiber ratio was further controlled by adding a second dry nonwoven web of desired weight. The impregnated nonwoven web was B-staged at 90° C. followed by lamination to 1 ounce/ft 2  electrodeposited copper. The lamination was carried out at 100-500 psi and 220° C. The resulting composite contained 21-34% polyester fiber by weight with the balance of the composite composed of epoxy, flame retardant fillers and clays (hydrated aluminum silicates). 
     EXAMPLE 2 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________PAPA                770Polyfunctional glycidyl ether               800of phenolic novolac (averagefunctionality = 2.2)Diglycidyl ether of tetra-               300bromo bisphenol ADibromophenyl glycidyl ether               431Antimony trioxide   333Glass microspheres, 2560(60 micron maximum size)Nonwoven fabric of2 denier poly (M-phenylene               1560isothalamide) (e.g., NOMEX) fibersH glass fibers      670______________________________________ 
    
     The above components were blended in a similar manner to the components for Example 1. The resulting mixture of fillers, epoxies, anhydride and silane was used to saturate the nonwoven web. The saturated nonwoven web was laminated to electrodeposited 1 ounce/ft 2  copper using similar conditions to Example 1. This process was repeated in the following Examples 3-10. 
     EXAMPLE 3 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________Polyadipic polyanhydride (PADA)               330Triglycidyl ether of               416para-amino phenolDibromophenyl glycidyl ether               300Decabromo diphenyl oxide               150Antimony trioxide   260Silica (maximum particle               1470size = 60 microns)Nonwoven fabric of  3203 denier PET fibers______________________________________ 
    
     EXAMPLE 4 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________Azelaic Acid        340Polyfunctional glycidyl ether               720of phenolic novolac (averagefunctionality = 3.6)Dibromo phenyl glycidyl ether               640Antimony trioxide   240Silica (10 micron maximum size)               1900Nonwoven fabric of3 denier acrylic fibers               410H glass fibers      285______________________________________ 
    
     EXAMPLE 5 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________PAPA                195Polyfunctional glycidyl ether of               247phenolic novolac (averagefunctionality = 3.6)Dibromo phenyl glycidyl ether               109Decabromo diphenyl oxide                54Antimony trioxide   190Glass microspheres (44 micron               435maximum size)Nonwoven fabric of2 denier NOMEX fibers               168H glass fibers       42______________________________________ 
    
     EXAMPLE 6 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________Polysebacic polyanhydride (PSPA)               206Diglycidyl ether of bisphenol A               250Dibromo phenyl glycidyl ether               110Antimony trioxide    95Glass microspheres (60 micron               675maximum size)Nonwoven fabric of  3806 denier poly-1,4 cyclohexylene-dimethylene terephthalate (PCDT)______________________________________ 
    
     EXAMPLE 7 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________PAPA                195Diglycidyl ether of bisphenol A               258O-cresyl glycidyl ether                65Decabromo diphenyl oxide               108Antimony trioxide   165Silica (30 micron maximum size)               6753-glycidyl oxypropyl trimethoxysilane                8Nonwoven fabric of3 denier acrylic fibers               400H glass fibers      100______________________________________ 
    
     EXAMPLE 8 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________Polysebacic polyanhydride               206Glycidyl ether of   300tetraphenylol ethaneDibromo phenyl glycidyl ether               109Antimony trioxide    75Silica (60 micron maximum size)               5753-amino oxypropyl trimethoxysilane                10Nonwoven fabric of3 denier PET fibers 260H glass fibers      170______________________________________ 
    
     EXAMPLE 9 
     
         ______________________________________MATERIAL           PARTS BY WEIGHT______________________________________PAPA               123Polyfunctional glycidyl ether of              372brominated phenolic novolacp-t-butyl phenyl glycidyl ether               80Decabromo diphenyl oxide               54Antimony trioxide   55Glass microspheres 200(60 micron maximum size)Nonwoven fabric of 2802 denier NOMEX______________________________________ 
    
     EXAMPLE 10 
     
         ______________________________________MATERIAL            PARTS BY WEIGHT______________________________________PSPA                206Glycidyl ether of para-amino phenol               247O-cresyl glycidyl ether                65Tetrabromo bisphenol A               225Antimony trioxide   120Silica (30 micron maximum               375particle size)3 glycidyl oxypropyl trimethoxysilane                30Nonwoven fabric of2 denier NOMEX fibers               200H glass fibers      100______________________________________ 
    
     EXAMPLE 11 
     
         ______________________________________MATERIAL             PARTS BY WEIGHT______________________________________PAPA                 209Polyfunctional glycidyl ether of coupled                373bisphenol units (averagefunctionality = 8.0)Dibromo phenyl glycidyl ether                117Decabromo diphenyl oxide                 58Antimony trioxide    205Glass microballoons (60 micron                285maximum particle size)Nonwoven reinforcement of:2 denier Nomex fibers                218H glass fibers        55______________________________________ 
    
     EXAMPLE 12 
     
         ______________________________________MATERIAL           PARTS BY WEIGHT______________________________________PAPA               209Polyfunctional glycidyl ether              404of brominated phenolic novolacDibromo phenyl glycidyl ether              117Antimony trioxide  210Glass microspheres (60 micron              305maximum particle size)Nonwoven reinforcement of:3 denier PET fibers              240H glass fibers      60______________________________________ 
    
     EXAMPLE 13 
     
         ______________________________________MATERIAL           PARTS BY WEIGHT______________________________________PAPA               209Difunctional glycidyl ether of              188tetrabromobisphenol ADibromo phenyl glycidyl ether              117Antimony trioxide  205Silica             465Nonwoven reinforcement of:3 denier PET       320H glass fibers      80______________________________________ 
    
     EXAMPLE 14 
     
         ______________________________________MATERlAL           PARTS BY WEIGHT______________________________________Dodecenyl succinic anhydride              266Polyfunctional glycidyl ether of              178phenolic novolac (averagefunctionality of 3.6)Antimony trioxide   80Decabromo diphenyl oxide               35Silica             335Nonwoven reinforcement of:3 denier polyacrylonitrile              240H glass fibers      60______________________________________ 
    
     EXAMPLE 15 
     
         ______________________________________MATERIAL             PARTS BY WEIGHT______________________________________PAPA                 209Polyfunctional glycidyl ether of                265phenolic novolac (averagefunctionality of 3.6)Polyfunctional glycidyl ether of an                100aliphatic polyol with a glycidyl etherequivalent weight of approximately 640Antimony trioxide    105Glass microballoons (60 micron                215maximum particle size)Nowoven reinforcement of:2 denier Nomex       210H glass fibers       140______________________________________ 
    
     EXAMPLE 16 
     
         ______________________________________MATERIAL             PARTS BY WEIGHT______________________________________PAPA                 209Polyfunctional glycidyl ether of                265phenolic novolac (averagefunctionality of 3.6)Diglycidyl ether of dibromo neopenthyl                 91glycolAntimony trioxide    145Decabromodiphenyl oxide                 45Glass microspheres (35 micron                535maximum size)Nonwoven reinforcement of:3 denier PET         400H glass fibers       100______________________________________ 
    
     EXAMPLE 17 
     
         ______________________________________MATERIAL             PARTS BY WEIGHT______________________________________PAPA                 209Tetraglycidyl diamino diphenyl methane                162Dibromophenyl glycidyl ether                115Antimony trioxide    120Decabromo diphenyl oxide                 54Silica               260Nonwoven reinforcement of:2 denier Nomex       210H glass fibers       140______________________________________ 
    
     EXAMPLE 18 
     
         ______________________________________MATERIAL           PARTS BY WEIGHT______________________________________PAPA               100Diglycidyl ether of bisphenol A              100Antimony trioxide   50Decabromo diphenyl oxide               27Silica             175Nonwoven reinforcement of:2 denier Nomex     160H glass fibers      40______________________________________ 
    
     EXAMPLE 19 
     
         ______________________________________MATERIAL             PARTS BY WEIGHT______________________________________Azelaic acid         448Polyglycidyl ether of phenolic novolac                850(average functionality of 3.6)Decabromo diphenyl oxide                307Antimony trioxide    4813-glycidyl oxypropyl trimethoxysilane                 25Silica               800Nonwoven reinforcement of:3 denier PET         600H glass fibers       400______________________________________ 
    
     EXAMPLE 20 
     
         ______________________________________MATERIAL             PARTS BY WEIGHT______________________________________Azelaic acid         108Polyglycidyl ether of phenolic novolac                 34(average functionality of 3.6)Diglycidyl ether of bisphenol A                 72Antimony trioxide    140Decabromo diphenyl oxide                 75Glass microspheres   240Nonwoven reinforcement of:3 denier Nomex       160H glass fibers        40______________________________________ 
    
     All of the examples included a catalyst/accelerator for increasing the rate of reaction. However, such catalyst/accelerators are not required to make the circuit material composite of this invention. 
     In accordance with the present invention, the unique combination of components provides a printed circuit board which can be bent and formed into permanent multiplanar shape without cracking or creasing of the substrate or of the copper. The multiplanar bent circuit board will then retain its bent or formed shape when the forming forces are removed therefrom. In general, the bends should be curved (forming distinct radii) since sharp creases may break the copper and/or craze the substrate. The radius should be about 1/4 inch for a laminate of 0.015 substrate and 1 oz. copper, and should increase for thicker laminates. Significantly, the bending or forming can be done at room temperature. 
     The minimum bend radius (R) to dielectric thickness ratio (t) is dependent on the elongation of the laminated copper and the conductor width. Typically, the minimum value of R/t ranges from 5 to 10. For example, when a sample of the present invention having a 0.030&#34; thickness containing 100% of the original one ounce/ft 2  copper cladding on both sides is bent at a radius of 0.030&#34; to a bend angle of 50°; the retained angle is 60-80° several hours after the initial bend. The retained angle does not substantially change with time. For a variety of samples made with standard electrodeposited copper foil, cracks first appeared in the copper conductors at a bend ratio (R/t) of 5-8. No cracks or crazes were visible at 50X magnification in the dielectric at these bend ratios. 
     Thus, as in the prior art circuit material of U.S. Ser. No. 778,603, the forming or bending may be at room temperature, and it may be done manually or by machine. Once the circuit element is formed, it retains its shape, which is of crucial importance to the present invention. 
     Thus, the printed circuit board of the present invention is a formable or bendable circuit element which essentially combines some of the advantages of both rigid and flexible printed circuit board materials including: 
     (1) the ability to process in sheet form, which is useful to hardboard manufacturers who conventionally process in this manner; 
     (2) heavy components may be mounted on the relatively rigid structure without the use of extra stiffeners as are required with conventional flexible printed circuit boards, and may be used with automatic handling machines; 
     (3) like flexible printed circuit boards, the ability to conform to the shape of the space available and to bend circuitry around corners; and 
     (4) like hardboard, the ability to retain its shape after installation. 
     It will be appreciated that the present invention is not analogous to a B-staged material. Instead, the present invention may be bent or formed into a multiplanar shape after exposure to circuit processing thermal operations. Exposure to thermal processes such as hot air solder leveling, wave soldering or infrared solder reflow do not substantially change the bendability of the material. A printed circuit board of the present invention is capable of being bent to a bend ratio (R/t) of 10:1 without fracture of the copper conductors or cracking and/or crazing of the dielectric after several excursions to temperatures as high as 288° C.. 
     While preferred embodiments have been shown and described, various modifications and substitutions may be made thereto without departing from the spirit and scope of the invention. Accordingly, it is to be understood that the present invention has been described by way of illustrations and not limitation.