US20050108983A1 - Reinforced composite structural members and methods of making the same - Google Patents

Reinforced composite structural members and methods of making the same Download PDF

Info

Publication number
US20050108983A1
US20050108983A1 US10/856,920 US85692004A US2005108983A1 US 20050108983 A1 US20050108983 A1 US 20050108983A1 US 85692004 A US85692004 A US 85692004A US 2005108983 A1 US2005108983 A1 US 2005108983A1
Authority
US
United States
Prior art keywords
reinforcing member
resin
composite structural
structural member
recited
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US10/856,920
Inventor
Peter Simko
Carlos Almeida
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Composite Building Products International Inc
Carney Timber Co
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US10/856,920 priority Critical patent/US20050108983A1/en
Assigned to CARNEY TIMBER COMPANY reassignment CARNEY TIMBER COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ALMEIDA, CARLOS, SIMKO, PETER
Assigned to COMPOSITE BUILDING PRODUCTS INTERNATIONAL INC. reassignment COMPOSITE BUILDING PRODUCTS INTERNATIONAL INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SIMKO, PETER
Publication of US20050108983A1 publication Critical patent/US20050108983A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/28Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of materials not covered by groups E04C3/04 - E04C3/20
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/07Flat, e.g. panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/09Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels
    • B29C48/11Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels comprising two or more partially or fully enclosed cavities, e.g. honeycomb-shaped
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/15Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor incorporating preformed parts or layers, e.g. extrusion moulding around inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/30Extrusion nozzles or dies
    • B29C48/304Extrusion nozzles or dies specially adapted for bringing together components, e.g. melts within the die
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/30Extrusion nozzles or dies
    • B29C48/32Extrusion nozzles or dies with annular openings, e.g. for forming tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/88Thermal treatment of the stream of extruded material, e.g. cooling
    • B29C48/90Thermal treatment of the stream of extruded material, e.g. cooling with calibration or sizing, i.e. combined with fixing or setting of the final dimensions of the extruded article
    • B29C48/901Thermal treatment of the stream of extruded material, e.g. cooling with calibration or sizing, i.e. combined with fixing or setting of the final dimensions of the extruded article of hollow bodies
    • B29C48/903Thermal treatment of the stream of extruded material, e.g. cooling with calibration or sizing, i.e. combined with fixing or setting of the final dimensions of the extruded article of hollow bodies externally
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/88Thermal treatment of the stream of extruded material, e.g. cooling
    • B29C48/90Thermal treatment of the stream of extruded material, e.g. cooling with calibration or sizing, i.e. combined with fixing or setting of the final dimensions of the extruded article
    • B29C48/908Thermal treatment of the stream of extruded material, e.g. cooling with calibration or sizing, i.e. combined with fixing or setting of the final dimensions of the extruded article characterised by calibrator surface, e.g. structure or holes for lubrication, cooling or venting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/88Thermal treatment of the stream of extruded material, e.g. cooling
    • B29C48/911Cooling
    • B29C48/9115Cooling of hollow articles
    • B29C48/912Cooling of hollow articles of tubular films
    • B29C48/913Cooling of hollow articles of tubular films externally
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/88Thermal treatment of the stream of extruded material, e.g. cooling
    • B29C48/911Cooling
    • B29C48/9135Cooling of flat articles, e.g. using specially adapted supporting means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2024/00Articles with hollow walls
    • B29L2024/006Articles with hollow walls multi-channelled
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/60Multitubular or multicompartmented articles, e.g. honeycomb

Definitions

  • This invention relates to reinforced composite structural members and methods of making the same.
  • Structural members such as beams and joists made from composite materials are known.
  • the composite material may be made, for example, from a mixture of (1) a natural fiber and (2) a resin.
  • the natural fiber may be wood fiber, or another type of natural fibrous material, available in various processed forms such as flakes, strands, particles and chips.
  • the term “resin” refers to a polymer having an indefinite and high molecular weight, and a characteristic softening or melting range, exhibiting a tendency to flow when heated and subjected to stress.
  • a composite mixture of wood fibers and resins is often referred to as “composite wood”. Examples of composite wood materials are described in U.S. Pat. No. 3,888,810 to Shinomura, the contents of which are hereby incorporated by reference.
  • Structural members such as joists, beams and sections of decking or walkways, can be formed from composite wood materials by extrusion and pultrusion techniques. Examples of some techniques that can be employed are disclosed in U.S. Pat. No. 5,783,125 to Bastone et al., U.S. Pat. No. 5,096,406 to Brooks et al., U.S. Pat. No. 5,096,645 to Fink and U.S. Pat. No. 5,234,652 to Woodhams et al., the contents of all of which are hereby incorporated by reference.
  • the present invention discloses a reinforced composite structural member having a continuous reinforcing member embedded therein.
  • a reinforced composite structural member comprising:
  • the reinforced composite structural member may be formed by extrusion.
  • the physical characteristic comprises an increased bondable outer surface in comparison to a reinforcing member of a substantially similar shape and size having a substantially smooth outer surface.
  • the reinforcing member may comprise, for example, a strip.
  • the strip may have a plurality of flow-through apertures provided along its length.
  • the flow-through apertures may be adapted to allow the composite material to flow therein and solidify, thereby providing an increased bondable surface area and helping to secure the reinforcing member within the extruded composite structural member.
  • the reinforcing member may also comprise a braided cable or tow which provides a sufficiently coarse outer surface for facilitating secure bonding within the composite mixture.
  • the coarse outer surface may provide an increased bondable surface area to secure the reinforcing member within the extruded composite structural member.
  • the reinforcing member may be delivered in a flexible format, allowing a sufficiently long length of the reinforcing member to be supplied, for example, on a supply reel in order to make a continuous extrusion run possible.
  • the outer surface of the reinforcing member may be heated just as the reinforcing member is introduced into the extrusion apparatus. Bonding between the reinforcing member and the composite mixture preferably occurs immediately adjacent the extrusion apparatus outlet.
  • Suitably sized and shaped guide channels may be used to guide the reinforcing member and properly align the reinforcing member for embedding in the extruded composite structure.
  • the reinforcing member may be treated with a suitable resin that is the same as, or compatible with, a suitable resin used in the composite mixture.
  • suitable resins may comprise, for example, low density polyethylene (LDPE), high density polyethylene (HDPE), polypropylene, PVC, or another polymeric material, such as those referred to in U.S. Pat. No. 5,783,125 to Bastone et al., the contents of which are also hereby incorporated by reference, or in U.S. Pat. No. 6,015,611 referred to above.
  • Suitable resin bonding pairs for the reinforcing member and the composite mixture include, for example, LDPE and LDPE, HDPE and HDPE, polypropylene and polypropylene. Although bonding pairs may be chosen from the same type, this is not strictly necessary. Certain thermoplastic materials may bond to other such materials not of the same type.
  • a method of forming a reinforced composite structural member comprising:
  • FIG. 1 is a schematic block diagram of an exemplary processing line for processing a composite structural member.
  • FIG. 2 a is a detailed perspective view of an extrusion apparatus for practicing the method in accordance with an exemplary embodiment of the invention.
  • FIG. 2 b is the extrusion apparatus of FIG. 2 a showing an extruded segment of a reinforced composite structural member made in accordance with an exemplary embodiment of the invention.
  • FIG. 2 c is a cross-sectional view of the extrusion apparatus of FIGS. 2 a and 2 b showing paths for introducing reinforcing members.
  • FIG. 2 d is a detail of a portion of the extrusion apparatus of FIG. 2 c.
  • FIG. 3 a is a cross-sectional view of the reinforced composite structural member formed by the extrusion apparatus of FIGS. 2 a to 2 d.
  • FIG. 3 b is a cross-sectional view of another embodiment of a reinforced composite structural member which may be formed in a substantially similar extrusion apparatus.
  • the processing line 100 includes an extruder 110 having a mouth 112 for receiving raw materials.
  • the raw materials may be provided, for example, in a pelletized or granular form suitable for storage and transportation.
  • Machines located upstream from the extruder 110 which may form such pelletized or granular raw materials are not shown, but will be familiar to those skilled in the art. Such upstream machines possibly may be located at a completely different location, such as at a supplier's premises.
  • an extrusion apparatus 115 Attached to an end of the extruder 110 is an extrusion apparatus 115 .
  • An extrusion screw 210 (see FIG. 2 c ) is provided within the extruder 110 to apply suitable pressure on a composite mixture 111 formed from the raw materials therein.
  • the raw materials fed into mouth 112 may comprise, for example, any suitable combination of a resin (or resins) and natural fibers (e.g. wood fiber materials).
  • a suitable ratio for a mixture of HDPE to wood fiber material may be in the range of approximately 50:50 by weight, to 35:65 by weight.
  • a composite mixture 111 may be formed which has a suitable viscosity for extrusion through the extrusion apparatus 115 .
  • a suitable pressure is preferably in the order of 2000 PSI+400 PSI, and a suitable melting temperature is preferably in the order of between 150°-190° C.
  • Various other ranges of pressure and temperature may be used for different combinations of resins and natural fiber materials.
  • FIG. 1 shows an extruded composite structural member 118 emerging from the extrusion apparatus 115 .
  • the extruded composite structural member 118 may then undergo further processing.
  • the processing line 100 may further include a calibration/cooling machine 120 which receives the extruded composite structural member 118 from the extrusion apparatus 115 .
  • the calibration/cooling machine 120 may be used, for example, to maintain the form of the extruded composite structural member 118 as the structural member 118 cools down and solidifies. Once cooled and solidified, the extruded composite structural member 118 may emerge from the calibration/cooling machine 120 and be pulled by a puller 122 .
  • the puller 122 may be provided with belts 124 , 126 mounted on rollers which grip the composite structural member 118 from opposite sides. The extruded composite structural member 118 may then emerge from the puller 122 and continue on to a finishing and cutting machine (not shown) further down the processing line 100 .
  • the extrusion apparatus 115 includes a first opening 132 a for receiving, along a path A, a first reinforcing member 130 a therein. Shown in a hidden view is a second opening 132 b located on an opposite side of the extrusion apparatus 115 . The second opening 132 b receives, along a path B, a second reinforcing member 130 b therein.
  • the description of the opening 132 a and reinforcing member 130 a should be understood to apply equally to opening 132 b and reinforcing member 130 b , in a corresponding manner.
  • the reinforcing member 130 a may be in the form of a flexible strip or tape.
  • the reinforcing member 130 a may be provided with a plurality of flow-through apertures 133 along the length of the reinforcing member 130 a .
  • the flow-through apertures 133 are exaggerated in size for the purposes of illustration. As will be explained in detail below, these flow-through apertures 133 are adapted to allow the composite mixture 111 to flow and to solidify therein. This will help to secure the reinforcing member 132 a within the extruded composite structural member 118 .
  • the plurality of flow-through apertures 133 increases the area of the bondable outer surface of the reinforcing member 130 a (in comparison to a reinforcing member of a substantially similar shape and size not having said flow-through apertures 133 ). Also, the flow-through apertures 133 may provide a “peg-in-hole” anchoring effect, to secure the reinforcing member in the composite structural member a lengthwise direction.
  • the flow-through apertures 133 may be provided at regular or random intervals, and in a variety of shapes, sizes, and patterns.
  • the flow-through apertures 133 should be sufficiently large to permit the composite mixture 111 to flow through into them, but should not be so numerous, or placed so close together as to render the reinforcing member 130 a ineffective for bearing a significant tensile load.
  • the possibility of nails or screws being driven through the reinforcing member 130 a should be taken into account in determining the pattern and size of the flow-through apertures 133 .
  • Suitable materials for the reinforcing member 130 a may include, for example, carbon composites, steel, aluminum, and other metal, glass and polymer based materials.
  • the material chosen for the reinforcing member 130 a can be selected to provide a desired tensile strength, but can also accommodate a nail, screw or other fastener that may be driven into the reinforced composite structural member 118 .
  • the material selected should also provide sufficient tensile strength, even if flow-through apertures 133 are provided.
  • the material can be selected to allow the reinforcing member 130 a to be sufficiently flexible such that a sufficiently long length of the reinforcing member 130 a may be provided on a supply reel (not shown). This will facilitate a sufficiently long, continuous run through the extruder 110 to form the extruded composite structural member 118 .
  • the reinforcing member may take another form that can be accommodated within the profile of the extruded composite structural member 118 .
  • the reinforcing member 130 a ( FIG. 3 b ) may be made of fibers braided into the form of a cable or tow.
  • the braided cable or tow may provide a coarse or uneven outer surface.
  • Such a coarse or uneven outer surface will provide an increased bondable outer surface on said reinforcing member 130 a , in comparison to a reinforcing member of a substantially similar shape and size having a substantially smooth outer surface. Furthermore, such a coarse or uneven outer surface will provide greater frictional force between the reinforcing member 130 a and the composite mixture 111 .
  • the cable or tow also provides a greater cross-sectional area for bearing tensile strength.
  • the extrusion apparatus 115 includes an extrusion outlet 117 suitably shaped to form a desired cross-sectional profile of the extruded composite structural member 118 .
  • an extrusion outlet 117 suitably shaped to form a desired cross-sectional profile of the extruded composite structural member 118 .
  • a plurality of channel shaping elements 134 a - 134 d may be suitably positioned within the extrusion outlet 117 .
  • the channel shaping elements 134 a - 134 d may be suspended at the mouth of outlet 117 by suitably placed braces or webs (not shown) further within the extrusion outlet 117 .
  • braces or webs should have a minimal profile, in the direction of flow of the composite mixture 111 , so as to minimize any disruption of flow of the composite mixture 111 into extrusion outlet 117 .
  • FIG. 2 b shown is another view of the extrusion apparatus 115 of FIG. 2 a .
  • a segment of the extruded composite structural member 118 has emerged from the extrusion outlet 117 .
  • Channels 206 a - 206 d have been formed by the channel shaping elements 134 a - 134 d , respectively.
  • the reinforcing members 130 a and 130 b have passed through the extrusion outlet 117 to become embedded within the extruded composite structural member 118 .
  • the general direction of flow of the emerging extruded composite structural member 118 is indicated by arrow C.
  • the extrusion apparatus 115 of FIGS. 2 a and 2 b , and a segment of the extruded composite structural member 118 are shown in a cross-sectional view.
  • the first reinforcing member 130 a follows a path through opening 132 a into extrusion apparatus 115 and then in between the channel shaping element 134 a and an extrusion apparatus wall 131 a .
  • reinforcing member 130 b follows a path through opening 132 b into extrusion apparatus 115 , and then in between the channel shaping element 134 d and extrusion apparatus wall 131 b.
  • an extrusion screw 210 provides the necessary pressure on composite mixture 111 to extrude the mixture 111 through the extrusion outlet 117 .
  • the composite mixture 111 should have a suitable viscosity, and sufficient momentum in the general direction of arrow C, such that the reinforcing members 130 a and 130 b are pulled into and through the extrusion apparatus 115 .
  • the openings 132 a , 132 b of the extrusion apparatus 115 may lead into suitably configured guide channels 212 a , 212 b which may guide the reinforcing members 130 a , 130 b into the extrusion apparatus 115 , near the extrusion outlet 117 , for bonding to the composite mixture 111 .
  • the guide channel 212 a is appropriately sized and shaped to allow reinforcing member 130 a to pass through the extrusion apparatus 115 and be aligned for accurate placement within the extruded composite member 118 .
  • guide channel 212 b is appropriately sized and positioned to allow reinforcing member 130 b to pass through the extrusion apparatus 115 and be aligned for accurate placement within the extruded composite member 118 .
  • the size, shape and length of the guide channels 212 a , 212 b will be determined by the outer dimensions of the reinforcing member 130 a , 130 b and also by the intended placement location in the profile of the extruded composite member 118 .
  • the guide channel 212 b may be provided with a lining 213 .
  • the lining may provide guide channel 212 b with different properties.
  • the lining 213 may provide a degree of thermal regulation, allowing the reinforcing member 130 b to be regulated substantially independently of the composite mixture 111 .
  • the lining 213 may provide a sufficiently smooth and hard surface which provides a sufficiently smooth entry for reinforcing members 130 a , 130 b which may have a coarse or uneven outer surface.
  • a suitable temperature gauge 214 may be employed to monitor the temperature of the guide channel 212 b for more accurate process control, although care should be taken in unobtrusively placing the gauge 214 so as not to hinder movement of the reinforcing member 130 b.
  • a heating element 215 may be provided along the guide channel 212 b in order to preheat the surface of the reinforcing member 130 b prior to its exit from the guide channel 212 b.
  • the reinforcing member 130 b may be guided into the opening 132 b by a pair of opposing rollers 220 a and 220 b .
  • the rollers 220 a , 220 b may be made of a suitably strong and heat resistant material, such as tungsten carbide or ceramic, for example.
  • the direction of rotation of each roller 220 a and 220 b is indicated by arrow D and arrow E, respectively.
  • the rollers 220 a and 220 b may be initially used in a driving manner to assist in threading the reinforcing member 130 b into the guide channel 212 b and through the extrusion apparatus 115 .
  • the rollers 220 a , 220 b may then become suitably biased against such rotation to regulate tension on the reinforcing member 130 b as it is pulled into the extrusion apparatus 113 .
  • the two functions, driving and tensioning may be performed by two separate sets of rollers.
  • appropriate tensioning of the reinforcing member fiber 103 b may help to impart a desired strength characteristic in the finished product.
  • the rate of introduction of reinforcing member 130 b into the extrusion apparatus 115 will be determined by the rate of formation of the extruded composite structural member 118 through the extrusion apparatus 115 . Consequently, the rate of introduction of the reinforcing member 130 b should be carefully matched with the rate of formation of the extruded composite structural member 118 in order to obtain substantially uniform product characteristics along substantially the entire length formed in a processing run.
  • the composite mixture 111 flows into a funnel shaped entrance to gap 225 . Sufficient pressure is present in this region such that the composite mixture 111 flows around and makes substantial contact with the reinforcing member 130 b as it emerges from the guide channel 212 b . Any flow-through apertures 133 provided on the reinforcing member 130 b are filled by the composite mixture 111 .
  • the reinforcing member 130 b may be coated or treated with a resin, selected to be compatible with the resin used in the composite mixture 111 , such that a solid bond may be formed between the reinforcing member 130 b and the composite mixture 111 .
  • preparation of the composite mixture 111 and preparation of the reinforcing member 130 b for bonding can proceed substantially independently, up to the point that reinforcing member 130 b is extruded together with composite mixture 111 through the extrusion apparatus 115 .
  • FIGS. 3 a and 3 b shown are cross-sectional views of an extruded composite structural member 118 formed by the method and apparatus shown and described above.
  • the reinforcing members 130 a and 130 b are placed within the composite structural member 118 and bonded to the surrounding composite material to provide assistance in bearing tensile forces under a load A or a load B, as the case may be.
  • such flow-through apertures 133 may be filled in by the composite mixture. This may help to keep to reinforcing member 130 a , 130 b firmly in position within the composite matrix.
  • the reinforcing members 130 a , 130 b may comprise braided cables or tows having a coarse outer surface. As explained earlier, such a coarse surface may provide an effectively greater surface area for bonding to the surrounding composite mixture 111 , and may also provide a greater frictional force between the reinforcing members 130 a , 130 b and the surrounding matrix of the extruded composite structural member 118 . Also, the braided cable or tow shape provides a greater cross-sectional area for bearing tensile stresses.

Abstract

There is disclosed a reinforced extruded composite structural member and a method of forming the same. The structural may member comprise a solidified composite mixture of a fibrous material and a resin, and a reinforcing member embedded therein. The reinforcing member may have a known tensile strength, and at least one physical characteristic adapted to promote bonding of the reinforcing member with the surrounding fibrous material.

Description

  • This application claims the benefit of U.S. Provisional Application No. 60/474,518 filed on May 30, 2003, the contents of which are incorporated by reference herein in their entirety.
  • FIELD OF THE INVENTION
  • This invention relates to reinforced composite structural members and methods of making the same.
  • BACKGROUND OF THE INVENTION
  • Structural members such as beams and joists made from composite materials are known. The composite material may be made, for example, from a mixture of (1) a natural fiber and (2) a resin. The natural fiber may be wood fiber, or another type of natural fibrous material, available in various processed forms such as flakes, strands, particles and chips. As used in this specification, the term “resin” refers to a polymer having an indefinite and high molecular weight, and a characteristic softening or melting range, exhibiting a tendency to flow when heated and subjected to stress. A composite mixture of wood fibers and resins is often referred to as “composite wood”. Examples of composite wood materials are described in U.S. Pat. No. 3,888,810 to Shinomura, the contents of which are hereby incorporated by reference.
  • Structural members, such as joists, beams and sections of decking or walkways, can be formed from composite wood materials by extrusion and pultrusion techniques. Examples of some techniques that can be employed are disclosed in U.S. Pat. No. 5,783,125 to Bastone et al., U.S. Pat. No. 5,096,406 to Brooks et al., U.S. Pat. No. 5,096,645 to Fink and U.S. Pat. No. 5,234,652 to Woodhams et al., the contents of all of which are hereby incorporated by reference.
  • There has, however, been a desire to improve the strength and performance characteristics of composite structural members, particularly for structural members such as beams and joists as referenced in U.S. Pat. No. 6,015,611 to Deaner et al., the contents of which is also hereby incorporated by reference.
  • Certain techniques for strengthening and reinforcing extruded structures are known, as described for example in U.S. Pat. No. 5,792,529 to May, and U.S. Pat. No. 3,993,726 to Moyer. However, the application of these techniques to composite materials made from natural fiber and resin may not be straightforward. For example, in comparison to pure thermoplastic and synthetic materials, the viscosity of a composite wood mixture prior to extrusion may be relatively high due to the presence of natural fibers, and therefore the composite wood mixture may not easily flow around and bond to a reinforcing member. Also, a relatively high-viscosity composite wood mixture may tend to misalign a flexible reinforcing member, having a detrimental effect on the structural properties of the embedded reinforcing member.
  • Therefore, there is a need for an improved method of forming a reinforced composite structural member, and in particular those composite structural members including natural fibers such as wood fibers.
  • SUMMARY OF THE INVENTION
  • The present invention discloses a reinforced composite structural member having a continuous reinforcing member embedded therein. In an aspect of the invention, there is provided a reinforced composite structural member, comprising:
      • a solidified composite mixture of a fibrous material and a resin;
      • a reinforcing member embedded therein, said reinforcing member having at least one physical characteristic for promoting bonding of said reinforcing member with said mixture of a fibrous material and a resin.
  • In an embodiment, the reinforced composite structural member may be formed by extrusion.
  • In an embodiment, the physical characteristic comprises an increased bondable outer surface in comparison to a reinforcing member of a substantially similar shape and size having a substantially smooth outer surface.
  • In an embodiment, the reinforcing member may comprise, for example, a strip. The strip may have a plurality of flow-through apertures provided along its length. The flow-through apertures may be adapted to allow the composite material to flow therein and solidify, thereby providing an increased bondable surface area and helping to secure the reinforcing member within the extruded composite structural member.
  • In another embodiment, the reinforcing member may also comprise a braided cable or tow which provides a sufficiently coarse outer surface for facilitating secure bonding within the composite mixture. The coarse outer surface may provide an increased bondable surface area to secure the reinforcing member within the extruded composite structural member.
  • The reinforcing member may be delivered in a flexible format, allowing a sufficiently long length of the reinforcing member to be supplied, for example, on a supply reel in order to make a continuous extrusion run possible.
  • The outer surface of the reinforcing member may be heated just as the reinforcing member is introduced into the extrusion apparatus. Bonding between the reinforcing member and the composite mixture preferably occurs immediately adjacent the extrusion apparatus outlet.
  • Suitably sized and shaped guide channels may be used to guide the reinforcing member and properly align the reinforcing member for embedding in the extruded composite structure.
  • The reinforcing member may be treated with a suitable resin that is the same as, or compatible with, a suitable resin used in the composite mixture. Suitable resins may comprise, for example, low density polyethylene (LDPE), high density polyethylene (HDPE), polypropylene, PVC, or another polymeric material, such as those referred to in U.S. Pat. No. 5,783,125 to Bastone et al., the contents of which are also hereby incorporated by reference, or in U.S. Pat. No. 6,015,611 referred to above.
  • Suitable resin bonding pairs for the reinforcing member and the composite mixture include, for example, LDPE and LDPE, HDPE and HDPE, polypropylene and polypropylene. Although bonding pairs may be chosen from the same type, this is not strictly necessary. Certain thermoplastic materials may bond to other such materials not of the same type.
  • In another aspect of the invention, there is provided a method of forming a reinforced composite structural member, comprising:
      • (i) providing a composite mixture comprising a fibrous material and a resin;
      • (ii) providing a length of a reinforcing member having at least one physical characteristic for promoting bonding of said reinforcing member with said composite mixture;
      • (i) embedding said reinforcing member into said composite mixture prior to forming said composite structural member.
  • These and other aspects of the invention will become apparent through the illustrative figures and accompanying description provided below.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • In the figures which illustrate example embodiments of the present invention:
  • FIG. 1 is a schematic block diagram of an exemplary processing line for processing a composite structural member.
  • FIG. 2 a is a detailed perspective view of an extrusion apparatus for practicing the method in accordance with an exemplary embodiment of the invention.
  • FIG. 2 b is the extrusion apparatus of FIG. 2 a showing an extruded segment of a reinforced composite structural member made in accordance with an exemplary embodiment of the invention.
  • FIG. 2 c is a cross-sectional view of the extrusion apparatus of FIGS. 2 a and 2 b showing paths for introducing reinforcing members.
  • FIG. 2 d is a detail of a portion of the extrusion apparatus of FIG. 2 c.
  • FIG. 3 a is a cross-sectional view of the reinforced composite structural member formed by the extrusion apparatus of FIGS. 2 a to 2 d.
  • FIG. 3 b is a cross-sectional view of another embodiment of a reinforced composite structural member which may be formed in a substantially similar extrusion apparatus.
  • DETAILED DESCRIPTION
  • Referring to FIG. 1, a portion of a processing line 100 for making an extruded product is shown. In this illustrative example, the processing line 100 includes an extruder 110 having a mouth 112 for receiving raw materials. The raw materials may be provided, for example, in a pelletized or granular form suitable for storage and transportation. Machines located upstream from the extruder 110 which may form such pelletized or granular raw materials are not shown, but will be familiar to those skilled in the art. Such upstream machines possibly may be located at a completely different location, such as at a supplier's premises.
  • Attached to an end of the extruder 110 is an extrusion apparatus 115. An extrusion screw 210 (see FIG. 2 c) is provided within the extruder 110 to apply suitable pressure on a composite mixture 111 formed from the raw materials therein.
  • The raw materials fed into mouth 112 may comprise, for example, any suitable combination of a resin (or resins) and natural fibers (e.g. wood fiber materials). In an embodiment, a suitable ratio for a mixture of HDPE to wood fiber material may be in the range of approximately 50:50 by weight, to 35:65 by weight.
  • In operation, with the application of an appropriate amount of heat, pressure and agitation within the extruder 110, a composite mixture 111 may be formed which has a suitable viscosity for extrusion through the extrusion apparatus 115. For example, for the mixture of HDPE and wood fiber described above, a suitable pressure is preferably in the order of 2000 PSI+400 PSI, and a suitable melting temperature is preferably in the order of between 150°-190° C. Various other ranges of pressure and temperature may be used for different combinations of resins and natural fiber materials.
  • FIG. 1 shows an extruded composite structural member 118 emerging from the extrusion apparatus 115. The extruded composite structural member 118 may then undergo further processing. For example, the processing line 100 may further include a calibration/cooling machine 120 which receives the extruded composite structural member 118 from the extrusion apparatus 115. The calibration/cooling machine 120 may be used, for example, to maintain the form of the extruded composite structural member 118 as the structural member 118 cools down and solidifies. Once cooled and solidified, the extruded composite structural member 118 may emerge from the calibration/cooling machine 120 and be pulled by a puller 122. The puller 122 may be provided with belts 124, 126 mounted on rollers which grip the composite structural member 118 from opposite sides. The extruded composite structural member 118 may then emerge from the puller 122 and continue on to a finishing and cutting machine (not shown) further down the processing line 100.
  • Referring to FIG. 2 a, shown is a perspective view of the extrusion apparatus 115 of FIG. 1. As shown, the extrusion apparatus 115 includes a first opening 132 a for receiving, along a path A, a first reinforcing member 130 a therein. Shown in a hidden view is a second opening 132 b located on an opposite side of the extrusion apparatus 115. The second opening 132 b receives, along a path B, a second reinforcing member 130 b therein. In the discussion below, the description of the opening 132 a and reinforcing member 130 a should be understood to apply equally to opening 132 b and reinforcing member 130 b, in a corresponding manner.
  • In an embodiment, the reinforcing member 130 a may be in the form of a flexible strip or tape. The reinforcing member 130 a may be provided with a plurality of flow-through apertures 133 along the length of the reinforcing member 130 a. In FIG. 2, the flow-through apertures 133 are exaggerated in size for the purposes of illustration. As will be explained in detail below, these flow-through apertures 133 are adapted to allow the composite mixture 111 to flow and to solidify therein. This will help to secure the reinforcing member 132 a within the extruded composite structural member 118. It will be understood that, generally, the plurality of flow-through apertures 133 increases the area of the bondable outer surface of the reinforcing member 130 a (in comparison to a reinforcing member of a substantially similar shape and size not having said flow-through apertures 133). Also, the flow-through apertures 133 may provide a “peg-in-hole” anchoring effect, to secure the reinforcing member in the composite structural member a lengthwise direction.
  • The flow-through apertures 133 may be provided at regular or random intervals, and in a variety of shapes, sizes, and patterns. The flow-through apertures 133 should be sufficiently large to permit the composite mixture 111 to flow through into them, but should not be so numerous, or placed so close together as to render the reinforcing member 130 a ineffective for bearing a significant tensile load. The possibility of nails or screws being driven through the reinforcing member 130 a should be taken into account in determining the pattern and size of the flow-through apertures 133.
  • Suitable materials for the reinforcing member 130 a may include, for example, carbon composites, steel, aluminum, and other metal, glass and polymer based materials. Generally speaking, the material chosen for the reinforcing member 130 a can be selected to provide a desired tensile strength, but can also accommodate a nail, screw or other fastener that may be driven into the reinforced composite structural member 118. The material selected should also provide sufficient tensile strength, even if flow-through apertures 133 are provided. Furthermore, the material can be selected to allow the reinforcing member 130 a to be sufficiently flexible such that a sufficiently long length of the reinforcing member 130 a may be provided on a supply reel (not shown). This will facilitate a sufficiently long, continuous run through the extruder 110 to form the extruded composite structural member 118.
  • In other embodiments, the reinforcing member may take another form that can be accommodated within the profile of the extruded composite structural member 118. For example, in one such embodiment, the reinforcing member 130 a (FIG. 3 b) may be made of fibers braided into the form of a cable or tow. Instead of a plurality of flow-through apertures 133, as shown in FIG. 2 a, the braided cable or tow may provide a coarse or uneven outer surface.
  • It will be understood that such a coarse or uneven outer surface will provide an increased bondable outer surface on said reinforcing member 130 a, in comparison to a reinforcing member of a substantially similar shape and size having a substantially smooth outer surface. Furthermore, such a coarse or uneven outer surface will provide greater frictional force between the reinforcing member 130 a and the composite mixture 111. The cable or tow also provides a greater cross-sectional area for bearing tensile strength.
  • Still referring to FIG. 2 a, the extrusion apparatus 115 includes an extrusion outlet 117 suitably shaped to form a desired cross-sectional profile of the extruded composite structural member 118. For example, in order to form a number of voids or channels within the profile of the extruded composite structural member 118, a plurality of channel shaping elements 134 a-134 d may be suitably positioned within the extrusion outlet 117. The channel shaping elements 134 a-134 d may be suspended at the mouth of outlet 117 by suitably placed braces or webs (not shown) further within the extrusion outlet 117. Preferably, such braces or webs should have a minimal profile, in the direction of flow of the composite mixture 111, so as to minimize any disruption of flow of the composite mixture 111 into extrusion outlet 117.
  • Now referring to FIG. 2 b, shown is another view of the extrusion apparatus 115 of FIG. 2 a. As shown in FIG. 2 b, a segment of the extruded composite structural member 118 has emerged from the extrusion outlet 117. Channels 206 a-206 d have been formed by the channel shaping elements 134 a-134 d, respectively. Furthermore, the reinforcing members 130 a and 130 b have passed through the extrusion outlet 117 to become embedded within the extruded composite structural member 118. The general direction of flow of the emerging extruded composite structural member 118 is indicated by arrow C.
  • Referring to FIG. 2 c, the extrusion apparatus 115 of FIGS. 2 a and 2 b, and a segment of the extruded composite structural member 118, are shown in a cross-sectional view. As shown, the first reinforcing member 130 a follows a path through opening 132 a into extrusion apparatus 115 and then in between the channel shaping element 134 a and an extrusion apparatus wall 131 a. Similarly, reinforcing member 130 b follows a path through opening 132 b into extrusion apparatus 115, and then in between the channel shaping element 134 d and extrusion apparatus wall 131 b.
  • Still referring to FIG. 2 c, an extrusion screw 210 provides the necessary pressure on composite mixture 111 to extrude the mixture 111 through the extrusion outlet 117. Within the extrusion apparatus 115, the composite mixture 111 should have a suitable viscosity, and sufficient momentum in the general direction of arrow C, such that the reinforcing members 130 a and 130 b are pulled into and through the extrusion apparatus 115.
  • In an embodiment, the openings 132 a, 132 b of the extrusion apparatus 115 may lead into suitably configured guide channels 212 a, 212 b which may guide the reinforcing members 130 a, 130 b into the extrusion apparatus 115, near the extrusion outlet 117, for bonding to the composite mixture 111. As shown in FIG. 2 c, the guide channel 212 a is appropriately sized and shaped to allow reinforcing member 130 a to pass through the extrusion apparatus 115 and be aligned for accurate placement within the extruded composite member 118. Similarly, guide channel 212 b is appropriately sized and positioned to allow reinforcing member 130 b to pass through the extrusion apparatus 115 and be aligned for accurate placement within the extruded composite member 118. The size, shape and length of the guide channels 212 a, 212 b will be determined by the outer dimensions of the reinforcing member 130 a, 130 b and also by the intended placement location in the profile of the extruded composite member 118.
  • Now referring to FIG. 2 d, and referring back to FIG. 2 c, in an embodiment, the guide channel 212 b may be provided with a lining 213. The lining may provide guide channel 212 b with different properties. For example, the lining 213 may provide a degree of thermal regulation, allowing the reinforcing member 130 b to be regulated substantially independently of the composite mixture 111. As another example, the lining 213 may provide a sufficiently smooth and hard surface which provides a sufficiently smooth entry for reinforcing members 130 a, 130 b which may have a coarse or uneven outer surface.
  • In an embodiment, a suitable temperature gauge 214 may be employed to monitor the temperature of the guide channel 212 b for more accurate process control, although care should be taken in unobtrusively placing the gauge 214 so as not to hinder movement of the reinforcing member 130 b.
  • If desired, a heating element 215 may be provided along the guide channel 212 b in order to preheat the surface of the reinforcing member 130 b prior to its exit from the guide channel 212 b.
  • There should not be any back-flow of the composite mixture 111 into guide channel 212 b, especially if the exit of the guide channel 212 b is suitably sized and shaped for the reinforcing member 130 b. Also, the movement of composite mixture 111 in the general direction of arrow C should minimize any such back-flow problems.
  • Still referring to FIG. 2 d, as shown, the reinforcing member 130 b may be guided into the opening 132 b by a pair of opposing rollers 220 a and 220 b. The rollers 220 a, 220 b may be made of a suitably strong and heat resistant material, such as tungsten carbide or ceramic, for example. The direction of rotation of each roller 220 a and 220 b is indicated by arrow D and arrow E, respectively. The rollers 220 a and 220 b may be initially used in a driving manner to assist in threading the reinforcing member 130 b into the guide channel 212 b and through the extrusion apparatus 115. Once the extrusion process is under way, however, the rollers 220 a, 220 b may then become suitably biased against such rotation to regulate tension on the reinforcing member 130 b as it is pulled into the extrusion apparatus 113. (In another embodiment, the two functions, driving and tensioning, may be performed by two separate sets of rollers.) Depending on the type of the material used, and the material's flexibility, appropriate tensioning of the reinforcing member fiber 103 b may help to impart a desired strength characteristic in the finished product.
  • The rate of introduction of reinforcing member 130 b into the extrusion apparatus 115 will be determined by the rate of formation of the extruded composite structural member 118 through the extrusion apparatus 115. Consequently, the rate of introduction of the reinforcing member 130 b should be carefully matched with the rate of formation of the extruded composite structural member 118 in order to obtain substantially uniform product characteristics along substantially the entire length formed in a processing run.
  • In the vicinity of the exit of guide channel 212 b, the composite mixture 111 flows into a funnel shaped entrance to gap 225. Sufficient pressure is present in this region such that the composite mixture 111 flows around and makes substantial contact with the reinforcing member 130 b as it emerges from the guide channel 212 b. Any flow-through apertures 133 provided on the reinforcing member 130 b are filled by the composite mixture 111.
  • In another embodiment, the reinforcing member 130 b may be coated or treated with a resin, selected to be compatible with the resin used in the composite mixture 111, such that a solid bond may be formed between the reinforcing member 130 b and the composite mixture 111. Advantageously, preparation of the composite mixture 111 and preparation of the reinforcing member 130 b for bonding can proceed substantially independently, up to the point that reinforcing member 130 b is extruded together with composite mixture 111 through the extrusion apparatus 115.
  • Referring to FIGS. 3 a and 3 b, shown are cross-sectional views of an extruded composite structural member 118 formed by the method and apparatus shown and described above. The reinforcing members 130 a and 130 b are placed within the composite structural member 118 and bonded to the surrounding composite material to provide assistance in bearing tensile forces under a load A or a load B, as the case may be.
  • As shown in FIG. 3 a, in the case of a reinforcing member 130 a, 130 b provided with flow through apertures, such flow-through apertures 133 may be filled in by the composite mixture. This may help to keep to reinforcing member 130 a, 130 b firmly in position within the composite matrix.
  • As shown in FIG. 3 b, in an alternative embodiment, the reinforcing members 130 a, 130 b may comprise braided cables or tows having a coarse outer surface. As explained earlier, such a coarse surface may provide an effectively greater surface area for bonding to the surrounding composite mixture 111, and may also provide a greater frictional force between the reinforcing members 130 a, 130 b and the surrounding matrix of the extruded composite structural member 118. Also, the braided cable or tow shape provides a greater cross-sectional area for bearing tensile stresses.
  • Still referring to FIGS. 3 a and 3 b, if the extruded composite structural member 118 is bearing load A on side 300 b, between two fixed supports (not shown) supporting side 300 a, then reinforcing member fiber 130 a will be in tension. Similarly, if load B is applied to side 300 a, say between two fixed supports (not shown) supporting side 300 b, then reinforcing member fiber 130 b will be in tension. By having the symmetrical arrangements shown, it will be understood that the extruded composite structural member 118 provides virtually the same structural loading characteristics regardless of which side, 300 a or 300 b, is bearing a load.
  • While certain illustrative embodiments of the present invention has been shown and described, various modifications will be apparent to those skilled in the art. For example, while an extrusion process has been described, it will be appreciated that various aspects of this invention may be adapted to pultrusion and injection molding techniques. As well, while the illustrative extruded composite structural member is shown and described as having a plurality of channels, it will be understood that the teachings of the present invention are equally applicable to strengthening an extruded composite structural member with just one channel, or without such channels (i.e. a member having a solid cross-section). Also, the shape of the internal channels may vary. While the extruded composite structural member is shown as having a generally rectangular shape, it will be understood that various other shapes may also be used. As well, while the reinforcing member is shown as being embedded substantially along the entire length of a composite structural member, it will be appreciated that only a portion of a length of a composite structural member may be reinforced in this manner, if appropriate to do so.
  • Therefore, the invention is defined in the following claims.

Claims (27)

1. A reinforced composite structural member, comprising:
a solidified composite mixture of a fibrous material and a resin;
a reinforcing member embedded therein, said reinforcing member having at least one physical characteristic for promoting bonding of said reinforcing member with said mixture of a fibrous material and a resin.
2. The reinforced composite structural member of claim 1, wherein said composite structural member is formed by extrusion.
3. The reinforced composite structural member of claim 1, wherein said physical characteristic comprises an increased bondable outer surface in comparison to a reinforcing member of a substantially similar shape and size having a substantially smooth outer surface.
4. The reinforced composite structural member recited in claim 1, wherein said physical characteristic comprises a plurality of flow-through apertures.
5. The reinforced composite structural member recited in claim 4, wherein said reinforcing member is in the form of a strip, and said flow-through apertures are provided along the entire length of said strip.
6. The reinforced composite structural member recited in claim 1, wherein said physical characteristic comprises a resin compatibly bondable with said resin in said composite mixture.
7. The reinforced composite structural member recited in claim 1, wherein said physical characteristic comprises a coarse outer surface.
8. The reinforced composite structural member recited in claim 7, wherein said reinforcing member is a braided cable having said coarse outer surface.
9. The reinforced composite structural member recited in claim 8, wherein said reinforcing member includes a resin compatibly bondable with said resin in said composite mixture.
10. The reinforced composite structural member recited in claim 1, wherein said fibrous material is a natural fiber.
11. The reinforced composite structural member recited in claim 1, wherein said fibrous material is wood fiber.
12. The reinforced composite structural member recited in claim 1, wherein said reinforcing member includes an anchoring feature to secure said reinforcing member in said composite structural member in a lengthwise direction.
13. A method of forming a reinforced composite structural member, comprising:
(i) providing a composite mixture comprising a fibrous material and a resin;
(ii) providing a length of a reinforcing member having at least one physical characteristic for promoting bonding of said reinforcing member with said composite mixture;
(iii) embedding said reinforcing member into said composite mixture prior to forming said composite structural member.
14. The method recited in claim 13, wherein (iii) is performed during extrusion of said composite mixture.
15. The method recited in claim 13, wherein said physical characteristic comprises an increased bondable outer surface in comparison to a reinforcing member of a substantially similar shape and size having a substantially smooth outer surface.
16. The method recited in claim 13, further comprising, prior to (iii), applying sufficient heat, pressure and agitation to said composite mixture to bring said resin to its melting point, and said composite mixture of said natural fiber and said resin to a flowing, extrudable state.
17. The method recited in claim 16, wherein said characteristic comprises providing on said reinforcing member a resin compatibly bondable with said resin in said composite mixture.
18. The method recited in claim 13, further comprising thermally regulating said reinforcing member strip independently of said composite mixture, up to the point of said embedding in (iii).
19. The method recited in claim 13, wherein in (ii) said providing a length of a reinforcing member with at least one physical characteristic for increasing the area of the bondable outer surface of said reinforcing member comprises providing a plurality of flow-through apertures on said reinforcing member.
20. The method recited in claim 19, further comprising providing on said reinforcing member a resin compatibly bondable with said resin in said composite mixture.
21. The method recited in claim 13, wherein in (ii) said providing a length of a reinforcing member with at least one physical characteristic for increasing the area of the bondable outer surface of said reinforcing member comprises providing a coarse outer surface.
22. The method recited in claim 21, further comprising providing on said reinforcing member a resin compatibly bondable with said resin in said composite mixture.
23. The method recited in claim 22, further comprising heating the outer surface of said reinforcing member as said reinforcing member is embedded in (iii).
24. The method recited in claim 13, wherein said reinforcing member is provided in a flexible format, allowing a sufficiently long length of said reinforcing member to be supplied on a reel.
25. The method recited in claim 14, further comprising providing guiding said reinforcing member into an extrusion apparatus and immediately adjacent to an extrusion apparatus outlet for proper alignment within said reinforced composite structural member.
26. The method recited in claim 13, wherein said fibrous material is a natural fiber.
27. The method recited in claim 13, wherein said fibrous material is wood fiber.
US10/856,920 2003-05-30 2004-05-28 Reinforced composite structural members and methods of making the same Abandoned US20050108983A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US10/856,920 US20050108983A1 (en) 2003-05-30 2004-05-28 Reinforced composite structural members and methods of making the same

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US47451803P 2003-05-30 2003-05-30
US10/856,920 US20050108983A1 (en) 2003-05-30 2004-05-28 Reinforced composite structural members and methods of making the same

Publications (1)

Publication Number Publication Date
US20050108983A1 true US20050108983A1 (en) 2005-05-26

Family

ID=34594501

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/856,920 Abandoned US20050108983A1 (en) 2003-05-30 2004-05-28 Reinforced composite structural members and methods of making the same

Country Status (1)

Country Link
US (1) US20050108983A1 (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070193199A1 (en) * 2004-08-02 2007-08-23 Tac Technologies, Llc Engineered structural members and methods for constructing same
US20080295453A1 (en) * 2004-08-02 2008-12-04 Tac Technologies, Llc Engineered structural members and methods for constructing same
US20100068451A1 (en) * 2008-09-17 2010-03-18 David Richard Graf Building panel with wood facing layer and composite substrate backing layer
US7721496B2 (en) 2004-08-02 2010-05-25 Tac Technologies, Llc Composite decking material and methods associated with the same
FR2955523A1 (en) * 2010-01-27 2011-07-29 Alphacan Sa EXTRUSION TOOLING FOR MANUFACTURING PLASTIC PROFILES WITH REINFORCEMENT ELEMENTS, METHOD OF IMPLEMENTATION AND PROFILES OBTAINED
US8065848B2 (en) 2007-09-18 2011-11-29 Tac Technologies, Llc Structural member
US8266856B2 (en) 2004-08-02 2012-09-18 Tac Technologies, Llc Reinforced structural member and frame structures
EP2650452A1 (en) * 2012-04-11 2013-10-16 Alphacan Composite material for boards for outdoor construction
US20140182241A1 (en) * 2012-12-27 2014-07-03 Jeong Moon Seo Support beam with a steel core frame
US9611692B1 (en) 2013-01-25 2017-04-04 Apollomarine Specialties, Inc. Rope ladder rung and method of manufacture
WO2018122200A1 (en) * 2017-01-02 2018-07-05 Sabic Global Technologies B.V. Solar roof forming element, roof, and method of manufacturing
US20210308965A1 (en) * 2017-04-26 2021-10-07 The Boeing Company Pultrusion systems that apply lengthwise curvature to composite parts
US11897177B2 (en) 2017-01-02 2024-02-13 Sabic Global Technologies B.V. Method for manufacturing a structural beam, structural beam, and building comprising such a beam

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3470598A (en) * 1964-04-29 1969-10-07 Viggo Berthelsen Method of making structural elements
US3888810A (en) * 1972-07-11 1975-06-10 Nippon Oil Co Ltd Thermoplastic resin composition including wood and fibrous materials
US3993726A (en) * 1974-01-16 1976-11-23 Hercules Incorporated Methods of making continuous length reinforced plastic articles
US4492063A (en) * 1981-04-15 1985-01-08 Schock & Co. Gmbh Extruded plastics material hollow profiled strip for window frames, window frames produced from this type of profiled strips and method for the production of a window frame of this type
US4965980A (en) * 1989-08-10 1990-10-30 Weston Leavens Deck bracket
US5096406A (en) * 1990-03-14 1992-03-17 Advanced Environmental Recycling Technologies, Inc. Extruder assembly for composite materials
US5096645A (en) * 1990-10-09 1992-03-17 Plastigage Corporation Method of forming reinforced thermoplastic members
US5234652A (en) * 1990-12-20 1993-08-10 Woodhams Raymond T Process for the continuous production of high modulus articles from high molecular weight plastics
US5759680A (en) * 1990-03-14 1998-06-02 Advanced Environmetal Recycling Technologies, Inc. Extruded composite profile
US5783125A (en) * 1993-04-05 1998-07-21 Crane Plastics Company Limited Partnership Reinforced extrusion products and method of making same
US5792529A (en) * 1994-12-21 1998-08-11 Intek Weatherseal Products, Inc. Reinforced plastic extrusion
US6015611A (en) * 1992-08-31 2000-01-18 Andersen Corporation Advanced polymer wood composite
US20040062915A1 (en) * 2002-10-01 2004-04-01 Pabedinskas Arunas Antanas Reinforced composite structural members

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3470598A (en) * 1964-04-29 1969-10-07 Viggo Berthelsen Method of making structural elements
US3888810A (en) * 1972-07-11 1975-06-10 Nippon Oil Co Ltd Thermoplastic resin composition including wood and fibrous materials
US3993726A (en) * 1974-01-16 1976-11-23 Hercules Incorporated Methods of making continuous length reinforced plastic articles
US4492063A (en) * 1981-04-15 1985-01-08 Schock & Co. Gmbh Extruded plastics material hollow profiled strip for window frames, window frames produced from this type of profiled strips and method for the production of a window frame of this type
US4965980A (en) * 1989-08-10 1990-10-30 Weston Leavens Deck bracket
US5759680A (en) * 1990-03-14 1998-06-02 Advanced Environmetal Recycling Technologies, Inc. Extruded composite profile
US5096406A (en) * 1990-03-14 1992-03-17 Advanced Environmental Recycling Technologies, Inc. Extruder assembly for composite materials
US5096645A (en) * 1990-10-09 1992-03-17 Plastigage Corporation Method of forming reinforced thermoplastic members
US5234652A (en) * 1990-12-20 1993-08-10 Woodhams Raymond T Process for the continuous production of high modulus articles from high molecular weight plastics
US6015611A (en) * 1992-08-31 2000-01-18 Andersen Corporation Advanced polymer wood composite
US5783125A (en) * 1993-04-05 1998-07-21 Crane Plastics Company Limited Partnership Reinforced extrusion products and method of making same
US5792529A (en) * 1994-12-21 1998-08-11 Intek Weatherseal Products, Inc. Reinforced plastic extrusion
US20040062915A1 (en) * 2002-10-01 2004-04-01 Pabedinskas Arunas Antanas Reinforced composite structural members

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8266856B2 (en) 2004-08-02 2012-09-18 Tac Technologies, Llc Reinforced structural member and frame structures
US20080295453A1 (en) * 2004-08-02 2008-12-04 Tac Technologies, Llc Engineered structural members and methods for constructing same
US8438808B2 (en) 2004-08-02 2013-05-14 Tac Technologies, Llc Reinforced structural member and frame structures
US20070193199A1 (en) * 2004-08-02 2007-08-23 Tac Technologies, Llc Engineered structural members and methods for constructing same
US7721496B2 (en) 2004-08-02 2010-05-25 Tac Technologies, Llc Composite decking material and methods associated with the same
US7882679B2 (en) 2004-08-02 2011-02-08 Tac Technologies, Llc Engineered structural members and methods for constructing same
US7930866B2 (en) 2004-08-02 2011-04-26 Tac Technologies, Llc Engineered structural members and methods for constructing same
US8938882B2 (en) 2004-08-02 2015-01-27 Tac Technologies, Llc Reinforced structural member and frame structures
US20070193212A1 (en) * 2004-08-02 2007-08-23 Tac Technologies, Llc Engineered structural members and methods for constructing same
US8065848B2 (en) 2007-09-18 2011-11-29 Tac Technologies, Llc Structural member
US20100068451A1 (en) * 2008-09-17 2010-03-18 David Richard Graf Building panel with wood facing layer and composite substrate backing layer
EP2528723B1 (en) 2010-01-27 2015-03-04 Alphacan Extrusion equipment for manufacturing plastic profile members and implementation method
WO2011092409A1 (en) * 2010-01-27 2011-08-04 Alphacan Extrusion equipment for manufacturing plastic profile members, implementation method, and resulting profile members
FR2955523A1 (en) * 2010-01-27 2011-07-29 Alphacan Sa EXTRUSION TOOLING FOR MANUFACTURING PLASTIC PROFILES WITH REINFORCEMENT ELEMENTS, METHOD OF IMPLEMENTATION AND PROFILES OBTAINED
FR2989303A1 (en) * 2012-04-11 2013-10-18 Alphacan Sa COMPOSITE MATERIAL FOR BOARDS INTENDED FOR OUTDOOR FITTING
EP2650452A1 (en) * 2012-04-11 2013-10-16 Alphacan Composite material for boards for outdoor construction
US20140182241A1 (en) * 2012-12-27 2014-07-03 Jeong Moon Seo Support beam with a steel core frame
US9611692B1 (en) 2013-01-25 2017-04-04 Apollomarine Specialties, Inc. Rope ladder rung and method of manufacture
WO2018122200A1 (en) * 2017-01-02 2018-07-05 Sabic Global Technologies B.V. Solar roof forming element, roof, and method of manufacturing
US11897177B2 (en) 2017-01-02 2024-02-13 Sabic Global Technologies B.V. Method for manufacturing a structural beam, structural beam, and building comprising such a beam
US20210308965A1 (en) * 2017-04-26 2021-10-07 The Boeing Company Pultrusion systems that apply lengthwise curvature to composite parts
US11772337B2 (en) * 2017-04-26 2023-10-03 The Boeing Company Pultrusion systems that apply lengthwise curvature to composite parts

Similar Documents

Publication Publication Date Title
JP6066435B2 (en) Die assembly and apparatus
US9409347B2 (en) Method for forming reinforced pultruded profiles
US8859089B2 (en) Reinforced hollow profiles
US10940625B2 (en) Method and apparatus for extrusion of thermoplastic handrail
US9919481B2 (en) Structural member formed from a solid lineal profile
US20050108983A1 (en) Reinforced composite structural members and methods of making the same
TWI549140B (en) Continuous fiber reinforced thermoplastic rods
US10350807B2 (en) Method and apparatus for extrusion of thermoplastic handrail
TW201308362A (en) Composite core for electrical transmission cables
CA2430638A1 (en) Reinforced composite structural members and methods of making the same
US20160201403A1 (en) Composite Sucker Rod Assemblies
TWI458621B (en) Method and apparatus for extrusion of thermoplastic handrail

Legal Events

Date Code Title Description
AS Assignment

Owner name: CARNEY TIMBER COMPANY, CANADA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SIMKO, PETER;ALMEIDA, CARLOS;REEL/FRAME:015430/0129

Effective date: 20040521

AS Assignment

Owner name: COMPOSITE BUILDING PRODUCTS INTERNATIONAL INC., CA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SIMKO, PETER;REEL/FRAME:016204/0990

Effective date: 20040910

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION