METHOD OF MANUFACTURING GLUE-LAMINATED WOOD STRUCTURAL MEMBER WITH SYNTHETIC FIBER REINFORCEMENT

Abstract: A method of manufacturing a glue-laminated structural wood member (10) for bearing a structural load (16) includes bonding together multiple elongate wood segments (12) and a synthetic fiber reinforcement (24, 30) with their lengths generally aligned with the length of the member. The synthetic fiber reinforcement includes multiple synthetic fiber strands (52, 54) held within a resin matrix (56).

Description: METHOD OF MANUFACTURING GLUE-LAMINATED WOOD STRUCTURAL MEMBER WITH SYNTHETIC FIBER REINFORCEMENT Technical Field The present invention relates to wood structural members and, in particular, to methods of manufacturing glue laminated wood structural members. Background of the Invention Beams, trusses, joists, and columns are the typical structural members that support the weight or loads of structures, including buildings and bridges. Structural members may be manufactured from a variety of materials, including steel, concrete, and wood, according to the structure design, environment, and cost. Wood structural members are now typically manufactured from multiple wood segments that are bonded together, such as in glue-laminated members, laminated veneer lumber, parallel strand lumber and I-beams. These manufactured wood structural members have replaced sawn lumber or timbers because the former have higher design limits resulting from better inspection and manufacturing controls. Wood is a desirable material for use in many structural members because of its various characteristics, including strength for a given weight, appearance, cyclic load response, and fire resistance. In any application, a load subjects a structural member to both compressive and tensile stresses, which correspond to the respective compacting and elongating forces induced by the load on opposite sides of the member. By convention, a neutral plane or axis extends between the portions of the member under compression and tension. The structural member must be capable of bearing the compressive and tensile stresses without excessive strain and particularly without ultimately failing. Reinforcement of wood structural members in regions subjected to tensile stresses are known. For example, U.S. Patent No. 5,026,593 of O'Brien describes the use of a thin flat aluminum strip to reinforce a laminated beam. The use of a synthetic tension reinforcement having multiple aramid fiber strands held within a resin matrix adhered to at least one of the wood segments in the tension portion of the structural member is described by the inventor of the present application i "Reinforced Glued-Laminated Wood Beams" presented at the 1988 International Conference on Timber Engineering. Despite prior descriptions of reinforced wood structural members, methods suitable for large scale manufacturing of structural wood members with synthetic reinforcement are not available. Some conventional methods of manufacturing structural wood members are unworkable with synthetic fiber reinforcements. Other conventional methods of manufacturing structural wood members would be inefficient and wasteful of relatively expensive synthetic fiber reinforcement. Summary of the Invention An object of the present invention is, therefore, to provide a method of manufacturing wood structural members with synthetic fiber reinforcement. Another object of this invention is to provide such a method that allows efficient application of synthetic reinforcement to wood structural members. A further object of this invention is to provid such a method that prevents waste of synthetic reinforcement. In a preferred embodiment, the present inventio includes a method of manufacturing glue laminated wood structural members in which multiple elongate wood segments and a synthetic fiber reinforcement are bonded together with their lengths generally aligned with the length of the member. The synthetic fiber reinforcement includes multiple synthetic fiber strands having a high modulus of elasticity in tension and/or compression held within a resin matrix. In another preferred embodiment of this invention, synthetic fiber reinforcement is formed with suitable characteristics to be wound onto reels or spools. As a result, arbitrary lengths of synthetic fiber reinforcement can be drawn and cut for use within glue laminated structural wood members of arbitrary length without waste. Similarly, synthetic fiber reinforcement is formed with a width that is matched to a finished width the wood members. Methods of applying synthetic fiber reinforcement to wood laminae are also disclosed. Additional objects and advantages of this invention will be apparent from the following detailed description of preferred embodiments thereof which proceeds with reference to the accompanying drawings. Brief Description of the Drawings Fig. 1 is an elevation view of an exemplary glue laminated structural wood member having synthetic fiber reinforcement according to the present invention. Figs. 2A and 2B are perspective views of sections of respective synthetic tension and compression reinforcements with portions cut-away to show the alignments and orientations of fibers in the reinforcements. Fig. 3 is a perspective view of a pultrusion apparatus for producing an elongate synthetic reinforcement of the present invention. Detailed Description of Preferred Embodiments Fig. 1 shows a glue laminated wood structural member 10 having multiple wood laminae 12 that are bonded together and are preferably elongate boards. In this configuration, glue laminated wood member 10 is configured as a glue-laminated timber according to manufacturing standards 117-93 of the American Institute of Timber Construction (AITC) of Englewood, Colorado. A typical structural use of glue laminated wood member 10 is to extend as a beam over and bear a load along an otherwise open region. As a simplified, exemplary representation of such use, glue laminated wood member 10 is shown with its ends supported by a pair of blocks 14 and bearing a point load 16 midway between blocks 14. It will be appreciated, however, that glue laminated wood member 10 of the present invention could also bear loads distributed in other ways (e.g., cantilevered) or be used as a truss, joist, or column. Under the conditions represented in Fig. l, a lowermost lamina 20 is subjected to a substantially pure tensile stress, and an uppermost lamina 22 is subjected t a substantially pure compressive stress. To increase the tensile load-bearing capacity of glue laminated wood member 10, at least one layer of synthetic tension reinforcement 24 is adhered between lowermost lamina 20 and a next adjacent lamina 26 or, alternatively, to only an outer surface 28 of lowermost lamina 20. To increase the compressive load-bearing capacity of glue laminated wood member 10, at least one layer of synthetic compression reinforcement 30 is adhered between uppermost lamina 22 and a next adjacent lamina 32 or, alternatively to only the outer surface 34 of uppermost lamina 22. Synthetic reinforcements 24 and 30 are described below in greater detail. Synthetic tension reinforcement 24 and syntheti compression reinforcement 30 are generally centered about load 16 and preferably extend along about two-fifths to three-fifths the length of wood structural member 10, depending on load 16. A pair of wood spacers 35 are positioned at opposite ends of synthetic tension reinforcement 24 between laminae 20 and 26 to maintain a uniform separation therebetween. Similarly, a pair of wood spacers 35 are positioned at opposite ends of synthetic compression reinforcement 30 between laminae 22 and 32 to maintain a uniform separation therebetween. General aspects of the process for manufacturing of glue laminated structural wood member 10 are the same as the process for manufacturing conventional glue laminated structural wood members. With regard to the manufacture of conventional glue laminated structural wood members, wood laminae are carried by a conveyor through a glue spreader, which applies multiple thin streams of adhesive (e.g., resorcinol) along the length of each wood lamina on one of its major surfaces. Wood laminae are successively aligned with and set against other wood laminae in a stack that may be oriented horizontally or vertically. The wood laminae are arranged so that the adhesive on the major surface of one wood lamina engages the bare major surface of an adjacent wood lamina. After all the wood laminae are aligned with and set against each other, pressure in the range of about 125-250 psi is applied to the stack and the adhesive allowed to cure. As is known in the art, sufficient pressure is applied to establish consistent gluelines between adjacent wood laminae 12 of no more than 4 mils (0.10 mm) thick. The adhered stack of wood laminae 12 is then planed where the sides of all wood laminae 12 are exposed to form a conventional glue laminated structural wood member. In accordance with the present invention, various aspects of this conventional manufacturing process are modified to be compatible with the inclusion of synthetic fiber reinforcements 24 and 30 in wood member 10. In a first preferred embodiment, synthetic fiber reinforcements 24 and 30 are carried through a conventional glue spreader (not shown) , which applies multiple thin streams of adhesive (e.g., resorcinol) along the length of each reinforcement 24 or 30 on one of its major surfaces. Adhesion between wood laminae 12 and reinforcements 24 or 30 can be relatively poor when using a nonepoxy adhesive such as resorcinol applied in the conventional manner. Adhesion is improved, however, when the adhesive is spread to generally completely cover the major surfaces of synthetic fiber reinforcements 24 and 30. It will be appreciated that such spreading of the adhesive can be accomplished by spreading the adhesive applied to one of the major surfaces of synthetic fiber reinforcements 24 and 30 or by spreading the adhesive applied to one of the major surfaces of a wood lamina to be applied to one of synthetic fiber reinforcements 24 and 30. The spreading of adhesive may be accomplished, for example, by manually spreading the adhesive before synthetic fiber reinforcements 24 and 30 and adjacent wood laminae 12 are engaged or by engaging them and sliding them against each other before the adhesive sets. In another preferred embodiment, synthetic fiber reinforcements 24 and 30 are manufactured with respective widths 42 and 44 (Figs. 2A and 2B) that are matched to the finished width of wood member 10 (extending into the plane of Fig. 1) and are therefore less than the widths of wood laminae 12 used to form wood member 10. The original widths of wood laminae 12 used to form wood member 10 can vary so long as they are greater than the finished width of wood member 10. As a result, planing of synthetic fiber reinforcements 24 and 30 is avoided, which prevents waste of the relatively expensive reinforcement materials. Moreover, synthetic fiber reinforcements 24 and 30 sometimes would not provide a smooth, finished surface when planed, so avoiding the planing of synthetic fiber reinforcements 24 and 30 helps provide wood member 10 with a smooth, finished surface. During manufacture of wood member 10, different wood laminae 12 and synthetic fiber reinforcements 24 and 30 are successively aligned with and set against each other in a stack that may be oriented horizontally or vertically. Alignment of the wood laminae in a conventional glue laminated structural wood member is typically achieved by aligning the sides of adjacent wood laminae. A consequence of widths 42 and 44 of synthetic fiber reinforcements 24 and 30 being less than the original widths of wood laminae 12 is that synthetic fiber reinforcements 24 and 30 cannot be aligned with wood laminae 12 by conventional methods. In accordance with the present invention, therefore, manufacture of glue laminated structural wood member 10 includes mechanically securing synthetic fiber reinforcements 24 and 30 to adjacent wood laminae 12 prior to the curing of the adhesive. For example, glue laminated structural wood member 10 may be manufactured by positioning wood laminae 12 and synthetic fiber reinforcements 24 and 30 in a horizontal stack (i.e., glue laminated structural wood member 10 being positioned on its side) . Synthetic fiber reinforcements 24 and 30 are secured with small nails (e.g., pin nails that are air- driven) to wood lamina 12 to which the reinforcements are being adhered and the nails left in wood member 10 as additional laminae are applied. As another example, glue laminated structural wood member 10 may be manufactured by positioning wood laminae 12 and synthetic fiber reinforcements 24 and 30 in a vertical stack (i.e., glue laminated structural wood member 10 being positioned upright) . Synthetic fiber reinforcements 24 and 30 are secured to wood lamina 12 to which reinforcements 24 and 30 are being adhered with plastic or metal straps or bands encircling their widths and being closed under tension. After the adhesive cures to hold synthetic fiber reinforcements 24 and 30 to their adjacent wood laminae 12, the portions of the straps or bands extending from the sides of wood member 10 are cut and removed and the portions within wood member 10 remain there. Figs. 2A and 2B are enlarged perspective views of one layer each of preferred synthetic tension reinforcement 24 and preferred synthetic compression reinforcement 30, respectively. Tension reinforcement 24 and compression reinforcement 30 have large numbers of synthetic fibers 52 and 54 that are arranged parallel to one another, aligned with the length of reinforcements 24 and 30, and have relatively high moduli of elasticity in tension and compression, respectively. A resin material 56 surrounds and extends into the interstices between synthetic fibers 52 and 54 to maintain them in their arrangement and alignment. To facilitate their adhesion to wood laminae 12, reinforcements 24 and 30 are preferably manufactured and treated as described in U.S. patent application No. 08/037,580, filed March 24, 1993, now U.S. Patent No. 5,362,545. Accordingly, compression reinforcement 54 includes a synthetic fiber layer 58 that further enhances the adhesion of compression reinforcement 30. Also, the major surfaces of reinforcements 24 and 30 are abraded or "haired up" so that adjacent fibers 52 and 58 are broken and their ends 60 and 62 protrude from resin material 56, respectively. The parallel arrangement and longitudinal alignment of the fibers 52 and 54 provide synthetic tension reinforcement 24 and synthetic compression reinforcement 30 with maximal strength. Suitable for use as synthetic tension fibers 52 and synthetic fiber layer 58 are aramid fibers, which are commercially available from E.I. DuPont de Nemours & Co. of Delaware under the trademark "KEVLAR, " and high modulus polyethylene which is available under the trademark "SPECTRA" from Allied Fibers of Allied Signal, Petersberg, Virginia. A preferred grade of synthetic fibers 52 and layer 58 is an aramid fiber available as "KEVLAR 49." Synthetic fibers 52 preferably have a modulus of elasticity in tension that is relatively high. For example, synthetic fibers 52 of Kevlar have a modulus of elasticity in tension of about 18 x 10 psi (124,000 MPa) . Synthetic tension reinforcement 24 comprising about 60 percent synthetic fibers 52 to 40 percent resin material 56 (by volume) has a modulus of elasticity in tension of about 11 x 10 6 psi (75,900 MPa). Suitable for use as synthetic compression fibers 54 are commercially available carbon fibers, which have a modulus of elasticity in compression in the range of about 34 x 10 6 to 36 x 10 6 psi (234,000-248,000 MPa). Synthetic compression reinforcement 30 comprising about 60 percent synthetic fibers 54 to 40 percent resin material 56 (by volume) has a modulus of elasticity in compression in the range of about 18 x 10 6 to 19 x 10 6 psi (124,000-131,000 MPa) . Resin material 56 used in fabrication of both reinforcement 24 and reinforcement 30 is preferably an epoxy resin, but could alternatively be other resins such as polyester, vinyl ester, phenolic resins, polyimides, or polystyrylpyridine (PSP) or thermoplastic resins such as polyethylene terephthalate (PET) and nylon-66. To minimize waste and to simplify handling and use, synthetic fiber reinforcements 24 and 30 are formed so as to be wound onto a reel so that arbitrary lengths can be drawn and cut for use within wood members 10 of arbitrary length 64. A major factor that allows synthetic fiber reinforcements 24 and 30 to be wound onto reels of workable diameters (e.g., in the range of about 39 to 72 inches (99-183 cm) ) is that they are formed with relatively small thicknesses of 0.010 to 0.250 inch (0.25- 6.4 cm) . Another major benefit of such relatively thin synthetic reinforcements 24 and 30 is that substantially arbitrary amounts of strength enhancement can be obtained by using multiple layers of such synthetic reinforcements 24 and 30, such as at the locations shown in Fig. l. In practice, single layers of such relatively thin synthetic reinforcements 24 and 30 would typically provide less tha optimal strength enhancement of wood member 10. However, the prevention of waste and simplified handling provided by reeling synthetic reinforcements 24 and 30, together with the relatively fine variability of strength enhancement by multiplication of reinforcement layers, make such relatively thin synthetic reinforcements 24 and 30 particularly useful for the efficient manufacture of wood member 10. Other factors that allow synthetic fiber reinforcements 24 and 30 to be wound onto reels are the fibers 52 and 54 and resin material that are used, as described above. These materials allow synthetic fiber reinforcements 24 and 30 to be cut in arbitrary lengths with commonly available tools, preferably a carbide tippe saw, a high speed steel-tipped saw, or a diamond wheel. In contrast, conventional manufacturing methods for reinforced structural wood members employ reinforcing panels of full thickness and fixed lengths that typically undergo some trimming to fit, thereby wasting relatively large amounts of expensive reinforcing material. Synthetic fiber reinforcements 24 and 30 are preferably fabricated by pultrusion, which is a continuou manufacturing process for producing lengths of fiber reinforced plastic parts. Generally, pultrusion involves pulling flexible reinforcing fibers through a liquid resi bath and then through a heated die where the reinforced plastic is shaped and the resin is cured. Pultruded part typically have longitudinally aligned fibers for axial strength and obliquely aligned fibers for transverse strength. In accordance with the present invention, however, preferred reinforcements 24 and 30 are manufactured with substantially all respective fibers 52 and 54 in a parallel arrangement and longitudinal alignment to provide maximal strength. In some circumstances, such as to enhance shear resistance in reinforcements 24 and 30, less than substantially all of respective fibers 52 and 54 would be in a parallel arrangement and longitudinal alignment. Fig. 3 shows a preferred pultrusion apparatus 68 for fabricating synthetic fiber reinforcements 24 and 30. Multiple bobbins 70 carry synthetic fiber rovings 72. As is known in the art, filaments are grouped together into strands or fibers, which may be grouped together into twisted strands to form yarn, or untwisted strands to form rovings. Rovings 72 are fed through openings 76 in an alignment card 74 that aligns that rovings 72 and prevents them from entangling. Openings 76 are typically gasketed with a low friction material, such as a ceramic or plastic, to minimize abrasion of or resistance to rovings 72. Rovings 72 pass from card 74 to a first comb 78 that gathers them and arranges them parallel to one another. Rovings 72 then pass over a tensioning mandrel 80, under a second alignment comb 82, and through close- fitting eyelets 85 directly into a resin bath 84 where rovings 72 are thoroughly wetted with resin material. Passing rovings 72 into resin bath 84 through eyelets 85 minimizes the waste of rovings 72 whenever pultrusion apparatus 68 is stoppped. Resin-wetted rovings 72 are gathered by a forming die 86 and pass through a heated die 88 that cures the resin material and shape rovings 72 into reinforcements 24 and 30. Multiple drive rollers 92 pull the reinforcements 24 and 30 and rovings 72 through pultrusion apparatus 68 at a preferred rate of 3-5 feet/minute (0.9-1.5 m/minute) . Pultrusion apparatus 68 is capable of forming synthetic reinforcements 24 and 30 without longitudinal cracks or faults extending through and with cross- sectional void ratios of no more than 5 percent. Cross- sectional void ratios refer to the percentage of a cross- sectional area of synthetic reinforcements 24 and 30 between respective fibers 52 and 54, typically occupied by resin material, and is measured by scanning electron microscopy. The absence of faults and the low void ratios assure that synthetic reinforcements 24 and 30 are of maximal strength and integrity. The preferred resin materials, as described above and applied to rovings 72, have a glass transition temperature within a range of 250-300 °F. Glass transitio is an indicator of resin flexibility and is characterized as the temperature at which the resin loses its hardness or brittleness, becomes more flexible, and takes on rubbery or leathery properties. A glass transition temperature within the preferred range is desirable because it provides a minimal fire resistance temperature. The preferred cure rate of the resin material, which is the amount of material that cures from a monomer structure to a polymer structure, is 78 to 82 percent. It has been determined that synthetic reinforcements 24 and 30 with cure rates within this range have higher shear stress bearing capabilities at interfaces with both synthetic reinforcements and wood laminae. Preferably, a fiber tension force in the range of about three to eight pounds is applied to rovings 72 during the resin cure. The fiber tension force may be applied as a back pressure by tensioning mandrel 80 in combination with combs 78 and 82 or by the use of friction bobbins 70, wherein rotational friction of the bobbins may be adjusted to provide the desired back pressure on rovings 72. Such tension in the fibers assists in maintaining their parallel arrangement and alignment in reinforcements 24 and 30. Also, by curing the resin material while the fibers are under tension, reinforcements 24 and 30 have greater rigidity and therefore decrease deflection of wood member 10 upon loading. It will be obvious to those having skill in the art that many changes may be made to the details of the above-described embodiment of this invention without departing from the underlying principles thereof. The scope of the present invention should be determined, therefore, only by the following claims.

Claims: Claims 1. A method of packaging a synthetic fiber reinforcement to minimize waste and simplify handling during its use as a component in the fabrication of a laminated wood member, comprising: forming a layer of synthetic fiber reinforcement material having a length and a thickness and including a plurality of synthetic fiber strands encased within a resin matrix, the thickness of the layer being sufficiently small that the layer is flexible along its length; and forming a roll of the layer of synthetic fiber reinforcement material so that an arbitrary length of the layer can be later unrolled and cut for use in the fabrication of a laminated wood member of a desired length. 2. The method of claim 1 in which the forming of the roll comprises winding the layer of the synthetic fiber reinforcement material onto a reel having an inside diameter that is much greater than the thickness of the layer. 3. The method of claim l in which the layer of synthetic fiber reinforcement material includes multiple synthetic fiber layers encased within the resin matrix. 4. A roll of synthetic reinforcement material packaged in accordance with the method of claim 1. 5. A package of synthetic fiber reinforcement material for use as a component in the fabrication of a laminated wood member, comprising: a layer of synthetic fiber reinforcement material having a thickness and including a plurality of synthetic fiber strands encased within a resin matrix, the layer being wound in a roll having a diameter that is much greater than the thickness of the layer. 6. The package of synthetic fiber reinforcement material of claim 5 in which the layer of synthetic fiber reinforcement material includes multiple synthetic fiber layers encased within the resin matrix. 7. The package of synthetic fiber reinforcement material of claim 5 in which the layer of synthetic fiber material has a length and substantially all of the synthetic fiber strands are aligned parallel to one another along the length of the layer to maximize its strength. 8. The package of synthetic fiber reinforcement material of claim 5 in which the layer of synthetic fiber material has a length and a selected proportion of the synthetic fiber strands is aligned in nonparallel relationship to the length of the layer to enhance its shear strength properties. 9. The method of claim 5 in which the fiber strands are selected from a group consisting essentially of carbon, aramid, and high modulus polyethylene. 10. In a method of manufacturing a laminated wood structural member for bearing a structural load, the laminated wood structural member having a longitudinal axis and a finished width upon completion of manufacture, the improvement comprising: bonding plural elongate wood laminae together with their lengths generally aligned with the longitudinal axis of the laminated wood structural member, each of the wood laminae having a laminae width greater than the finished width; bonding a synthetic reinforcement having plural tension fiber strands held within a resin matrix to at least one of the wood laminae of the structural member, the synthetic reinforcement having a reinforcement width matched to that of the finished width; and reducing the wood laminae to the finished width. 11. The method of claim 10 in which the bonding of the synthetic reinforcement is preceded by mechanically securing the synthetic reinforcement to one of the wood laminae. 12. The method of claim 11 in which the synthetic reinforcement and the one of the wood laminae are oriented horizontally and the synthetic reinforcement is mechanically secured by nails driven into the one σf the wood laminae. 13. The method of claim 11 in which the synthetic reinforcement and the one of the wood laminae are oriented vertically and the synthetic reinforcement is mechanically secured by a strap-like member under tension encircling the width of the one of the wood laminae. 14. The method of claim 10 in which the laminated wood structural member includes multiple synthetic reinforcements each of which having two major surfaces, the major surfaces of any one of the synthetic reinforcements not contacting a major surface of any other of the synthetic reinforcements. 15. The method of claim 14 in which the synthetic reinforcements have lengths and the structural member has a length, the lengths of multiple ones of the synthetic reinforcements being less than the length of the structural member. 16. The method claim 14 in which one of the synthetic reinforcements includes multiple layers of fiber strands held within the resin matrix. 17. The method of claim 14 in which the fiber strands are selected from a group consisting essentially of carbon, aramid, and high modulus polyethylene. 18. The method of claim 14 in which the bonding of a synthetic reinforcement to at least one of the wood laminae is accomplished by applying an adhesive. 19. The method of claim 18 in which the adhesive is of a nonepoxy type. 20. The method of claim 10 in which the laminated wood structural member is of a structural composite lumber type. 21. The method of claim 20 in which the structural composite lumber members are selected from a group consisting essentially of laminated veneer wood, parallel strand wood, and I-beam. 22. The method of claim 10 in which the resin matrix is a thermoset resin. 23. The method of claim 10 in which the resin matrix is a thermoplastic resin. 24. A laminated wood structural load-bearing member having a longitudinal axis, comprising: multiple wood laminae of which each lamina has two major surfaces, the wood laminae having lengths generally aligned with the longitudinal axis; and multiple synthetic reinforcemt nt panels each of which having two major surfaces, at least one major surface of each reinforcement panel being secured by nonepoxy bonding to a major surface of one of the wood laminae. 25. The member of claim 24 in which more than one of the multiple reinforcement panels are positioned between the wood laminae such that the two major surfaces of each of the reinforcement panels are secured to major surfaces of the laminae. 26. The member of claim 24 in which the nonepoxy bonding is achieved by a nonepoxy adhesive. 27. The member of claim 26 in which the nonepoxy adhesive includes resorcinol. 28. The member of claim 24 constructed such that its laminae are of a structural composite lumber type. 29. The member of claim 28 in which the structural composite lumber member is selected from a group consisting essentially of laminated veneer wood, parallel strand wood, and I-beam. 30. A method of manufacturing a reinforced, laminated wood structural member for bearing a structural load, comprising: providing a wood lamina having a major surface and a reinforcement having a major surface; spreading an adhesive over a major surface of one of the wood lamina and the reinforcement to generally completely cover the major surface over which the adhesive is spread; and adhering the wood lamina to the reinforcement by contacting the adhesive-covered major surface to the nonadhesive-covered major surface. 31. The method of claim 30 in which the reinforcement includes multiple synthetic fiber strands encased within a resin matrix. 32. The method of claim 31 in which the reinforcement has a length and substantially all of the synthetic fiber strands are aligned parallel to one another along the length of the reinforcement to maximize its strength. 33. The method of claim 31 in which the reinforcement has a length and a selected proportion of the synthetic fiber strands is aligned in nonparallel relationship to the length of the reinforcement to enhance its shear strength properties. 34. The method of claim 31 in which the resin matrix is a thermoset resin. 35. The method of claim 31 in which the resin matrix is a thermoplastic resin. AMENDED CLAIMS [received by the International Bureau on 3 January 1995 (03.01.95); original claims 10,14,18 and 20 amended; new claims 35-41 added; remaining claims unchanged (δ pages)] reinforcement material includes multiple synthetic fiber layers encased within the resin matrix. 7. The package of synthetic fiber reinforcement material of claim 5 in which the layer of synthetic fiber 5 material has a length and substantially all of the synthetic fiber strands are aligned parallel to one another along the length of the layer to maximize its strength. 8. The package of synthetic fiber reinforcement 10 material of claim 5 in which the layer of synthetic fiber material has a length and a selected proportion of the synthetic fiber strands is aligned in nonparallel relationship to the length of the layer to enhance its shear strength properties. 15 9. The method of claim 5 in which the fiber strands are selected from a group consisting essentially of carbon, aramid, and high modulus polyethylene. 10. In a method of manufacturing a wood structural member for bearing a structural load, the wood 20 structural member having a longitudinal axis and a finished width upon completion of manufacture, the improvement comprising: providing elongate wood laminae having lengths extending along the longitudinal axis of the wood 25 structural member and one of the laminae having a width greater than the finished width; providing a synthetic reinforcement having plural tension fiber strands held within a resin matrix; arranging the wood laminae and the synthetic 30 reinforcement so that the synthetic reinforcement is positioned adjacent to the wood laminae; bonding the wood laminae and the synthetic reinforcement together; and reducing the wood structural member to the finished width. 11. The method of claim 10 in which the bondin of the synthetic reinforcement is preceded by mechanicall securing the synthetic reinforcement to one of the wood laminae. 12. The method of claim 11 in which the synthetic reinforcement and the one of the wood laminae are oriented horizontally and the synthetic reinforcement is mechanically secured by nails driven into the one of the wood laminae. 13. The method of claim 11 in which the synthetic reinforcement and the one of the wood laminae are oriented vertically and the synthetic reinforcement is mechanically secured by a strap-like member under tension encircling the width of the one of the wood laminae. 14. The method of claim 10 in which the wood structural member includes multiple synthetic reinforcements each having two major surfaces, the major surfaces of any one of the synthetic reinforcements not contacting a major surface of any other of the synthetic reinforcements. 15. The method of claim 14 in which the synthetic reinforcements have lengths and the structural member has a length, the lengths of multiple ones of the synthetic reinforcements being less than the length of th structural member. 16. The method claim 14 in which one of the synthetic reinforcements includes multiple layers of fibe strands held within the resin matrix. 17. The method of claim 14 in which the fiber strands are selected from a group consisting essentially of carbon, aramid, and high modulus polyethylene. 18. The method of claim 14 in which the bondin of a synthetic reinforcement to the wood laminae is accomplished by applying an adhesive. 19. The method of claim 18 in which the adhesive is of a nonepoxy type. 20. The method of claim 10 in which the wood structural member is of a structural composite lumber type. 21. The method of claim 20 in which the structural composite lumber members are selected from a group consisting essentially of laminated veneer wood, parallel strand wood, and I-beam. 22. The method of claim 10 in which the resin matrix is a thermoset resin. 23. The method of claim 10 in which the resin matrix is a thermoplastic resin. 24. A laminated wood structural load-bearing member having a longitudinal axis, comprising: multiple wood laminae of which each lamina has two major surfaces, the wood laminae having lengths generally aligned with the longitudinal axis; and multiple synthetic reinforcement panels each of which having two major surfaces, at least one major surface of each reinforcement panel being secured by nonepoxy bonding to a major surface of one of the wood laminae. 25. The member of claim 24 in which more than one of the multiple reinforcement panels are positioned between the wood laminae such that the two major surfaces of each of the reinforcement panels are secured to major surfaces of the laminae. 26. The member of claim 24 in which the nonepoxy bonding is achieved by a nonepoxy adhesive. 27. The member of claim 26 in which the nonepoxy adhesive includes resorcinol. 28. The member of claim 24 constructed such that its laminae are of a structural composite lumber type. 29. The member of claim 28 in which the structural composite lumber member is selected from a group consisting essentially of laminated veneer wood, parallel strand wood, and I-beam. 30. A method of manufacturing a reinforced, laminated wood structural member for bearing a structural load, comprising: providing a wood lamina having a major surface and a reinforcement having a major surface; spreading an adhesive over a major surface of one of the wood lamina and the reinforcement to generally completely cover the major surface over which the adhesiv is spread; and adhering the wood lamina to the reinforcement b contacting the adhesive-covered major surface to the nonadhesive-covered major surface. 31. The method of claim 30 in which the reinforcement includes multiple synthetic fiber strands encased within a resin matrix. 32. The method of claim 31 in which the reinforcement has a length and substantially all of the synthetic fiber strands are aligned parallel to one another along the length of the reinforcement to maximize its strength. 33. The method of claim 31 in which the reinforcement has a length and a selected proportion of the synthetic fiber strands is aligned in nonparallel relationship to the length of the reinforcement to enhanc its shear strength properties. 34. The method of claim 31 in which the resin matrix is a thermoset resin. 35. The method of claim 31 in which the resin matrix is a thermoplastic resin. 36. The method of claim 10 in which the synthetic reinforcement has a width that is slightly greater than the finished width of the wood structural member. 37. The method of claim 36 in which the width of the synthetic reinforcement is reduced to the finished width of the wood structural member. 38. The method of claim 10 in which the synthetic reinforcement has a width that corresponds to the finished width of the wood structural member. 39. In a method of manufacturing a wood structural member for bearing a structural load, the wood structural member having a longitudinal axis and a finished width upon completion of manufacture, the improvement comprising: providing elongate wood laminae having lengths extending along the longitudinal axis of the wood structural member and widths greater than the finished width; providing a synthetic reinforcement having plural tension fiber strands held within a resin matrix, the synthetic reinforcement having a width that closely corresponds to the finished width; arranging the wood laminae and the synthetic reinforcement so that the synthetic reinforcement is positioned adjacent to the wood laminae; bonding the wood laminae and the synthetic reinforcement together; and reducing the wood structural member to the finished width. 40. The method of claim 39 in which both the wood laminae and the synthetic reinforcement are reduced AMENDED SHEET(ARTICLE 10) to the finished width. 41. The method of claim 39 in which only the wood laminae is reduced to avoid reduction of the synthetic reinforcement width. 42. The method of claim 39 in which the wood structural member is of a structural composite lumber type. 43. The method of claim 42 in which the structural composite lumber members are selected from a group consisting essentially of laminated veneer wood, parallel strand wood, and I-beam.

Inventors: TINGLEY DANIEL A, TINGLEY, DANIEL, A.
Applicants: TINGLEY DANIEL A, TINGLEY, DANIEL, A.
Application year: 1995
Main classification: B32B5
IPC codes: B27D1, B27M3, B29C70, B32B5, B32B21, E04B1, E04C3