WO2006071814A2 - Elements et kit de reparation de dommages structurels - Google Patents

Elements et kit de reparation de dommages structurels Download PDF

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Publication number
WO2006071814A2
WO2006071814A2 PCT/US2005/046923 US2005046923W WO2006071814A2 WO 2006071814 A2 WO2006071814 A2 WO 2006071814A2 US 2005046923 W US2005046923 W US 2005046923W WO 2006071814 A2 WO2006071814 A2 WO 2006071814A2
Authority
WO
WIPO (PCT)
Prior art keywords
adhesive
hollow
repaired
grooves
blade
Prior art date
Application number
PCT/US2005/046923
Other languages
English (en)
Other versions
WO2006071814A3 (fr
WO2006071814B1 (fr
Inventor
Wesley Scott Wilbur
David Kip Wilbur
Original Assignee
Scoda America, Inc.
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 Scoda America, Inc. filed Critical Scoda America, Inc.
Priority to EA200701350A priority Critical patent/EA200701350A1/ru
Priority to CA002593863A priority patent/CA2593863A1/fr
Priority to EP05855476A priority patent/EP1828501A2/fr
Publication of WO2006071814A2 publication Critical patent/WO2006071814A2/fr
Publication of WO2006071814A3 publication Critical patent/WO2006071814A3/fr
Publication of WO2006071814B1 publication Critical patent/WO2006071814B1/fr

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Classifications

    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B60/00—Details or accessories of golf clubs, bats, rackets or the like
    • A63B60/42—Devices for measuring, verifying, correcting or customising the inherent characteristics of golf clubs, bats, rackets or the like, e.g. measuring the maximum torque a batting shaft can withstand
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B59/00—Bats, rackets, or the like, not covered by groups A63B49/00 - A63B57/00
    • A63B59/70—Bats, rackets, or the like, not covered by groups A63B49/00 - A63B57/00 with bent or angled lower parts for hitting a ball on the ground, on an ice-covered surface, or in the air, e.g. for hockey or hurling
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B60/00—Details or accessories of golf clubs, bats, rackets or the like
    • A63B60/06—Handles
    • A63B60/16—Caps; Ferrules
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B2102/00—Application of clubs, bats, rackets or the like to the sporting activity ; particular sports involving the use of balls and clubs, bats, rackets, or the like
    • A63B2102/24—Ice hockey
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B2209/00—Characteristics of used materials
    • A63B2209/02—Characteristics of used materials with reinforcing fibres, e.g. carbon, polyamide fibres

Definitions

  • Objects comprised of or coated with fiberglass, carbon fiber, wood, etc. may develop or incur surface fractures or through-fractures.
  • Surface fractures are typically breaks, cracks, splits, etc., that occur or develop in the surface of an object, but do not extend entirely through the wall of an object (i.e. , a hockey stick (shaft, hozel, or blade), a boat hull, etc.).
  • Through-fractures are those breaks, cracks, splits, etc. that extend entirely through the wall of an object.
  • hollow formed objects typically do not provide similar strength and support as compared to the same objects which are made of the same materials, but are solid in design and not hollow.
  • hollow formed objects offer many advantages over solid formed objects including, but not limited to, hollow formed objects typically use less overall material and therefore are lighter in weight, more maneuverable and easier to transport. Additionally, because less material is used in the construction of hollow objects, these hollow objects typically cost less money to produce.
  • the present invention comprises external structural damage repair elements and may comprise a structural damage repair kit including an adhesive or molding agent (hereinafter referred to as "adhesive"), reinforcing members and one or more sleeves.
  • adhesive an adhesive or molding agent
  • reinforcing members and one or more sleeves.
  • these elements restore and/or enhance the structural integrity of fractured objects, reduce any potential shear points, typically cost much less than conventional repair kits, and are much less labor intensive than conventional repair kits and methods.
  • the structural damage repair elements of the present invention may be used with any type of fracture and are not limited to just surface fractures or through- fractures.
  • One aspect of the present invention includes a structural strength enhancing insert comprising one or more layers of reinforcing fabric. An adhesive is disposed between each layer of reinforcing fabric and the layers are subsequently compressed together to form a structural strength enhancing member.
  • Another aspect of the present invention includes a method of repairing an object using a structural damage repair kit including providing one or more structural strength enhancing members and an adhesive.
  • the object shaped to a desired shape. Grooves are created in the area of the object to be repaired and one or more structural strength enhancing members are inserted into each of the grooves.
  • An adhesive is applied to the object adjacent the structural enhancing members and excess adhesive is removed from the object.
  • Yet another aspect of the present invention includes a method of repairing a hollow object.
  • the method includes removing a damaged portion of the hollow object and inserting a foam plug into the hollow object. Also, a plurality of reinforcing members are inserted into the hollow object. An adhesive is applied over the reinforcing members.
  • Another aspect of the present invention includes a method of repairing a hollow object, including providing an object with a first hollow portion and a second hollow portion, the first hollow portion having a first end.
  • a plug is inserted into the first end of the first hollow portion and a plurality of reinforcing members are inserted into the first hollow portion, adjacent the plug.
  • the reinforcing members are positioned so that the reinforcing members extend beyond the first end of the first hollow object.
  • the second hollow portion is placed over the reinforcing members to abut the first hollow portion, and adhesive is inserted into the second hollow portion into contact with the reinforcing members.
  • a method of repairing an object using a structural damage repair kit including providing one or more structural strength enhancing members, and an adhesive.
  • the object is shaped to a desired shape and grooves are created in the area of the object to be repaired.
  • One or more structural strength enhancing members are inserted into each of the grooves and adhesive is applied to the object adjacent the structural enhancing members. In addition, excess adhesive is removed from the object.
  • FIG. 1 is an elevational view of a hockey stick upon which an embodiment of the present invention could be incorporated;
  • FIG. 2 is a partial exploded perspective view of a broken shaft of a hockey stick
  • FIG. 3 is a partial exploded perspective view of a broken shaft with locking channels
  • FIG. 4 is a partial exploded perspective view of a broken shaft with a foam plug
  • FIG. 5 is a partial exploded perspective view of a broken shaft with rods
  • Fig. 5A is a perspective view of a rod
  • Fig. 6 is a partial exploded perspective view of a reconnected broken shaft with rods
  • Fig. 7 is a partial exploded perspective view of a reconnected broken shaft with adhesive on the rods
  • Fig. 7 A is a partial exploded perspective view of a shaft with a sleeve around the shaft
  • Fig. 8 is an enlarged exploded perspective view of a solid shaft with external wafers on four sides
  • Fig. 9 is an enlarged exploded perspective view of a solid shaft with external wafers on two sides;
  • Fig. 10 is a partial perspective view of a broken hockey stick blade
  • Fig. 11 is a side elevational view of a radius restorer
  • Fig. 12 is a front elevational view of the radius restorer of Fig. 11 with a portion of a hockey stick blade;
  • Fig. 13 is a side elevational view of a clamp, radius restorer and hockey stick blade;
  • Fig. 14 is a partial perspective view of a partially repaired hockey stick blade
  • FIG. 15 is a perspective view of a jig with a hockey blade
  • Fig. 16 is a perspective view of a broken hockey stick blade with grooves and wafers
  • Fig. 16A is a cross-sectional view of a channel arrangement
  • Fig. 16B is a cross-sectional view of another channel arrangement
  • Fig. 16C is an enlarged cross-sectional view of blade with wafers protruding out of grooves
  • Fig. 16D is an enlarged cross-sectional view of a blade with sanded wafers
  • Fig. 17 A is a perspective view of a wafer
  • Fig. 17B is a perspective view of another wafer
  • Fig. 17C is a perspective view of yet another wafer
  • Fig. 18 is a cross-sectional view of hockey stick blade
  • Fig. 19 is a cross-sectional view of hockey stick blade
  • Fig. 20 is a cross-sectional view of wafer arrangement in a hockey stick blade
  • Fig. 21 is a side elevational view of a groove cutting tool
  • Fig. 22 is a partial perspective view of a hockey stick blade with grooves
  • Fig. 23 is a partial perspective view of a hockey stick blade with grooves and rods;
  • Fig. 24 is a partial perspective view of a hockey stick blade with grooves filled with rods and adhesive;
  • Fig. 25 is a partial perspective view of a partially repaired and sanded hockey stick blade;
  • Fig. 26 is a partial perspective view of a hockey stick blade with fabric
  • Fig. 27 is a partial perspective view of a hockey stick blade with fabric and a sleeve;
  • Fig. 28 is a partial perspective view of a partially repaired hockey stick blade between flat supports;
  • Fig 29 is a partial perspective view of a partially repaired hockey stick blade covered with tape;
  • Fig. 30 is a partial cross-sectional view of the blade of Fig. 29 secured between clamps;
  • Fig. 31 is a partial perspective view of a repaired hockey stick blade
  • Fig. 32 is a partial perspective view of a damaged hockey stick blade missing the tip;
  • Fig. 33 is a partial perspective view of the blade of Fig. 32 with grooves and rods;
  • Fig. 34 is a partial perspective view of the blade of Fig. 32 with grooves and rods covered with adhesive;
  • Fig. 35 is a partial perspective view of the blade of Fig. 34 after being sanded;
  • Fig. 36 is a partial perspective view of the blade of Fig. 35 after sleeving and before curing of the adhesive;
  • Fig. 37 is a perspective view of a blade with straight wafers installed in the heel;
  • Fig. 38 is a perspective view of a blade with surface grooved wafers installed in the heel.
  • reference numeral 1 generally designates a hockey stick embodying the present invention.
  • the hockey stick 1 includes a shaft 2, hozel 3, and blade 4.
  • the shaft may have a solid or hollow construction and may be of varying lengths.
  • the hozel 3 and blade 4 may also be of varying sizes and angles.
  • Carbon-fiber rods 12 may be used to provide structural support to a hollow object 13 having first and second hollow portions 14, 15.
  • the second hollow portion has a top end 16a that may be uncovered or covered by a cap 16b, as shown in Fig. 2.
  • the carbon-fiber rods 12 are preferably hollow and approximately 3 to 6 inches in length.
  • the rods 12 have an open end 17 and a closed end 18, however, both ends may be closed.
  • the closed end 18 may be solid, but may be covered by glue, tape, a cap, etc.
  • the damaged portion 20 of the first and second hollow portions 14, 15 is cut off just above the damage 20 to remove any loose carbon-fiber strands, epoxy, laminate, etc.
  • the grooving bit 30 is used to create locking channels 21 (shown in Fig. 3) inside the first hollow portion 14 and the second hollow portion 15.
  • a plug/stopper 62 (see Fig. 4) is inserted into the first hollow portion 14 and forced to a predetermined position via the end 72 of the insertion tool 70 (shown in Fig. 11).
  • the end 72 of the insertion tool 70 has a length adequate to allow the rods 12 to rest approximately half-way inside the first hollow portion 14.
  • the rods 12 are inserted into the first hollow portion 14, with the open end 17 in contact with the plug/stopper 62.
  • the closed end 18 of the rods 12 protrudes outside of the first hollow portion 14.
  • the hollow portions 14, 15 are placed in a generally vertical orientation, if they are not already vertically oriented, and an adhesive 9 is poured into an end of the hollow object 13 and into contact with the rods 12.
  • small reinforcing shapes such as carbon fiber beads, mini rods, cylinders, cones, pyramids, microspheres, macrospheres, tiny hollow balls, tiny foam filled balls, etc. may also be poured into the end of the hollow object 13.
  • the closed end of the rods 12 prevents the adhesive 9 from filling the rods 12. It may be appropriate to gently shake the materials inside the hollow object 13 to settle all the materials.
  • the adhesive 9 is allowed to fill the gaps 25 between the rods 12 and cannot flow past the plug/stopper 62.
  • the structural damage repair method may be or also include a solid shaft repair system (see Figs. 8 and 9).
  • Wafers 100 may include specifically angled edge cuts 101. This allows two or more wafers 100 to fit together when angled edge cuts 101 are placed in contact with one another. It is also conceivable that these angled edge cuts 101 may lock or interlock with one another so as to be connected via means other than just to be in contact with one another.
  • through grooves 102 are created generally perpendicular to the fracture in the shaft 2. It is conceivable that these through grooves 102 may be positioned otherwise in relation to the fractures in the shaft 2, however, through grooves 102 must at least intersect the fracture in the shaft 2.
  • a chemical molding agent, wafers 100 and/or rods 12, and a sealant, discussed further below, may also be utilized in a manner substantially the same as previously discussed.
  • This shaft repair system may be utilized in hollow shafts or solid shafts.
  • a sleeve 200 may be used to repair the shaft 2, including at the hozel region of a hockey stick 1.
  • a carbon fiber sleeve 200 is used to externally around the shaft 2 to provide support at the break.
  • a sleeve 200 is then added over the epoxied area with approximately half of the sleeve 200 covering the first hollow portion 14 and half of the sleeve 200 covering the second hollow portion 15. Additional adhesive is then added to an outer portion of the sleeve 200 and allowed to cure. Once the adhesive has cured, it can be sanded and painted, or additional sleeves 200 can be added. It is also foreseen that fabric may be added to any side or sides to further aid in connecting the first and second hollow portions 14, 15.
  • the present invention includes a method for repairing structural damage to a flat or slightly curved object such as a hockey stick blade 4.
  • the repair can be accomplished by using an adhesive 9 (chemical molding agent), one or more rods 12 or wafers 100, one or more sleeves 200, and a brush 112.
  • the kit may also optionally include flexible flat supports 114, wrapping tape 103 and/or a sealant. The method of repairing a flat or curved item, such as a hockey stick blade 4, is described in further detail below.
  • any loose fibers or splinters 115 should be trimmed to get the parts to return to close proximity and original alignment.
  • a radius restorer 116 (shown in Fig. 11) is used to keep the parts in alignment during the curing time of the adhesive 9.
  • the radius restorer 116 includes two pins 117 that connect first and second clamping members 118, 119. The first clamping member 118 may be moved relative to the second clamping member 119 by sliding along the two pins 117.
  • the radius restorer 116 has contact portions 120 that are slightly curved. The slight curve of the contact portions 120 assists in obtaining and maintaining the desired blade radius/curve.
  • radius restorers 116 used in conjunction with a hand clamp 121 may be preferable, depending on how damaged the blade 4 is. If the curve is out of alignment after 24 hours, it is possible to readjust and reclamp for another two days. The adhesive is somewhat pliable for the first 48 hours and may be bent slightly. After 48 hours, however, this is no longer possible. On a completely broken off blade, it is imperative that the blade be reassembled with the proper "lay.” This may be accomplished by using a flat support form to ensure proper angulation or "lay.” The radius restorers 116 may be applied directly over flat supports 204 (see Fig. 28).
  • the adhesive may be applied to the structurally damaged area of the object to be repaired. Often, the adhesive is applied by troweling, brushing, or pouring the adhesive on the damaged area. Typically, the adhesive 9 has sufficient shape-retaining characteristics to allow a user to reshape the structurally damaged object to its original and/or desired shape. Typically, the adhesive will then harden and retain the original and/or desired shape of the object. Any adhesive may be used in this embodiment of the present invention.
  • the adhesive may be any adhesive agent, molding agent, shape- retaining compound, reinforcing agent, restructuring agent and/or restitution agent. Of course, the adhesive may also be any combination and/or derivation of any of the above.
  • the adhesive may include but is not limited to, epoxy, epoxy resin, epoxy for wet applications (i.e. , marine epoxy), multi-party epoxies, flex-epoxy, mercaptans, polyesters, urethanes, polyvinylchloride (PVC) cement, polyvinyl acetate, cellulose nitrate, polyvinyl butyral, polymethacrylates, methacrylates, polyvinyl alcohol, methylacry late/ethyl methacrylate, polyurea, etc. and any combinations or any derivations of any of the above including polymers and/or copolymers of any of the above, however, epoxy resin is typically preferred.
  • epoxy resin is typically preferred.
  • the adhesive 9 is applied to the object to be repaired, it is allowed to cure. Once the sealant has cured/dried, the remaining cured sealant is removed, typically by using a sanding device, however, any device may be used. By sanding off this excess sealant and adhesive 9, the surfaces of the object are smoothed.
  • the adhesive alone is insufficient to repair and/or restore the object to its original strength and/or increase the strength of the object. Accordingly, methods to enhance the strength of the repaired area are necessary. Specifically, reinforcement members and/or fabric and sleeving members are typically necessary to strengthen the object to be repaired.
  • grooves must first be made in the object to be repaired. Two methods have been developed for preparing the grooves. The first method involves use of a drill with a jig to assist in aligning and angling the grooves, and the second method involves using a grinding wheel attached to a drilling tool.
  • a jig 130 is optionally used as a guide to cut grooves 131 which are preferably staggered, or apertures in the object to be repaired.
  • Jig 130 may be made of any type of material, including, but not limited to, wood, metal, plastic, or any combinations or derivations thereof.
  • Jig 130 is typically a rectangular shape, however, it is conceivable that jig 130 may be any shape depending upon the shape and size of the object to be repaired.
  • the jig 130 has a center-line that is typically placed approximately perpendicular to the fracture of the object to be repaired. In the case of a pocket fracture, jig 130 may not be necessary.
  • grooves 131 are staggered relative to center-line 132. These staggered grooves 131 reduce creating a shear point and/or a shearline in the object to be repaired. That is to say, typically if all grooves 131 were the same length and had the same starting points and end points (i.e., non-staggered grooves), relative to center-line 132, and if the wafers 100 or rods 12 were positioned about parallel axes wherein their respective surfaces also positioned about parallel planes typically it is more likely that a shearing plane and/or shearline would be created at both the starting points and the end points of non-staggered grooves 131 between the non-staggered grooves 131 and the non-fractured and/or non-damaged material of the object to be repaired.
  • these staggered grooves 131 reduce these shearing planes and/or shearlines by having different groove starting points and end points than the groove 131 immediately adjacent to it such that these shearing planes and/or shearlines are virtually eliminated. As shown in Figs.
  • Jig 130 also includes clamp section(s) 136.
  • Clamp section(s) 136 are on either end of the substantially rectangularly-shaped jig 130.
  • clamp section(s) 136 may be any shape to accommodate the clamp(s) that may be used to clamp jig 130 to the object to be repaired.
  • clamp section(s) 136 of jig 130 may be modified to accommodate any other type of device utilized to secure jig 130 to the object to be repaired.
  • Guides 137 in jig 130 may be any length, including a length range of from about 1/2 inch to 72 inches, more typically from about 2 inches to about 48 inches, and most typically from about 3 inches to about 12 inches.
  • Guides 137 may be any width, including, but not limited to, 1/32 inch to about 2 inches, more typically from about
  • Guides 137 or apertures may be any shape and have any pattern within jig 130. Also, guides 137 in jig 130 may have a knurled cut or surface so that when a user uses a cutting device within jig 130 to create grooves 131, the resulting grooves 131 are knurled or they have the specific surface of the guides 137 in jig 130.
  • grooves 131 are cut in or on the object to be repaired. This cut may be made by any type of tool 138, however, typically a variable speed rotary saw or a DREMEL ® tool is preferred. While not necessary, it is preferred that the wafers 100 have a width of less than or equal to the thickness of the fractured area of the object to be repaired. While not necessary, it may be beneficial in repairs involving smaller narrow surfaces or surfaces having many angles to sleeve over the area to be repaired once the wafer 100 has been inserted into the object.
  • This sleeve process may involve covering the area with a portion of reinforcing fabric 11 and a chemical molding agent to aid in reinforcing the damaged area 20 and to further hold the wafer 100 in place during the chemical molding drying process, as will be further discussed below. This method is frequently used to create grooves for wafers 100.
  • a second method of making the grooves 131 does not involve use of a jig 130, in which case, a user manually staggers the grooves 131 keeping them relatively centered over the damaged area 20.
  • the grooves should be staggered so that between one-third and two-thirds of the groove is on one side of the break. This alternating alignment helps eliminate any shearing planes or lines that can be formed at the interface between the repaired and unrepaired areas.
  • the damaged areas 20 on the backside of the blade 4 can be marked with a silver or white marker.
  • the top and bottom groove lines should be drawn first, about a 1 A" (10mm) from the edge of the blade 4. The next two lines should each be evenly spaced between the top and bottom.
  • the lines cross the damaged area.
  • the damaged area crosses each line at point approximately within the middle one-third of the line. If the break runs diagonally across the blade 4, the grooves 131 will need to be staggered to accommodate the diagonal break. If the damaged area 20 runs down the blade 4 a long distance, it is sometimes desirable to grind a line of grooves 131 one after another down the blade 4 and then stagger each line of grooves 131 under it. This creates a continuous area of reinforcement that still accommodates the curve of the blade 4. As shown in Fig. 21, a drill 150 having a grinding wheel 152 can be used to create the grooves 131 in the surface of the object. The grooves 131 should be cut with a 3/16" x 2" grinding wheel 152.
  • the grooves 131 are only cut partially into the blade 4, as depicted in Fig. 36. However, if the grooves 131 penetrate the blade 4 creating holes through the blade 4, adhesive can be used to fill the holes. This method of making grooves is generally used when rods are to be used.
  • rods are used for grooves that only partially penetrate the object to be repaired.
  • wafers are used in grooves that fully penetrate the object to be repaired.
  • each of the grooves 131 is fitted with an appropriate sized rod 12.
  • the rods 12 are used in a similar manner described in relation to the shaft repair above.
  • the ends of the rods may also be dual angle cut, rounded, square cut, cone-shaped, or cut on a curve.
  • the rods are frequently solid, rather than hollow.
  • the rods are generally comprised of carbon fiber, but may be constructed from any suitable material, including, but not limited to fiberglass, KEVLAR ® , carbon fiber, wood, plastic, metal, etc.; however, typically carbon fiber is preferred.
  • the rods 12 generally have a diameter that is slightly less then the width of the grooves 131.
  • the rods 12 may also have a diameter that is substantially smaller so that more than one rod 12 can be inserted into a single groove 131.
  • the rods in the grooves should stagger over the break and between one-third and two-thirds of the length of the rods should be on one side of the break. Also, typically the repair grooves 131 for the rods 12 are not created in the front side. Because of the curve of the blade 4, this would cause the middle of the rods 12 to lay shallowest over the break.
  • the grooves 131 are filled with an adhesive 9 (Fig. 23) to aid in completely sealing the grooves 131 when the rods 12 are placed in the grooves 131.
  • the adhesive used herein may be any type of an adhesive, however, an epoxy resin is preferred. After the adhesive has been properly mixed, the adhesive mixture should be spread into the grooves 131. The grooves 131 need not be filled completely. The grooves 131 should be filled approximately half way, but the bottom of the grooves 131 should be completely covered with no bubbles or gaps.
  • the rods 12 should be oriented so that the cut angle is at the bottom of the groove 131. After the rods 12 have been inserted in the proper position, the entire repair area should be smeared with adhesive. All gaps around the rods 12 and in the grooves 131 should be filled. The rods 12 should not be allowed to move much during this process. If the rods 12 move too much, bubbles will be formed in the adhesive, thereby reducing the repair strength.
  • the blade 4 should be stored undisturbed in a warm dry place. The blade 4 should be stored at an angle so that gravity pulls the rods 12 and adhesive deeper into the grooves 131. With a thicker adhesive, storing the blade 4 at an angle may not be necessary.
  • rods 12 may be coated with an adhesive, of one of the types previously mentioned.
  • the rods 12 are then inserted into the staggered grooves 131. Wafers
  • reinforcement wafers 100 as previously shown in Figs. 8 and 9, comprised of compressed materials may be used in conjunction with, or instead of, the rods 12. More specifically, the wafers 100 are typically comprised of layers of reinforcing fabric having an adhesive substance in between the layers which are then compressed together. Any type of adhesive may be used, including, but not limited to epoxy, epoxy resin, epoxy for wet applications (i.e.
  • the material layers may be the following types of materials, including, but not limited to fiberglass, KEVLAR ® , carbon fiber, wood, plastic, metal, etc.
  • the wafers 100 may be made from any combinations or derivations of the above-mentioned material layers compressed together.
  • the wafers 100 may be made of any number of layers of these materials within the range of from about 1-20 layers, more typically from about 4-12 layers, and most preferably from about 4-8 layers of the above-mentioned materials.
  • the wafers 100 may optionally be knurled as shown in Figs. 17A-17B.
  • a knurled surface typically will hold or retain more sealant thereby creating a stronger bond between the wafers 100, the sealant and the object to be repaired. Additionally, a knurled surface typically offers more resistance to movement once placed in the object to be repaired. Any type of knurled surface is acceptable, including, but not limited to, checker grooved surface (see Fig. 17A), lateral grooved surface, longitudinal grooved surface (see Fig. 17B), diamond grooved surface, or any other type of knurled surface or any combinations or derivations of the above type of knurled surfaces.
  • the knurled surface may include a combination of any of these types of above-noted surfaces.
  • the edges of the wafers 100 may be any configuration to better fit into the grooves 131, including, but not limited to rounded edges, square edges, etc., however, typically rounded edges are preferred. It is also conceivable that the grooves 131 in which the inserts are placed may have a knurled cut to create a better fit between the wafer 100 and the groove 131.
  • These wafers 100 may be sized to any shape. However, they will typically be sized to the shape of the corresponding groove 131 in which the wafers 100 are to be placed.
  • the wafers 100 may be any width, any thickness and/or length. Unlike the rods
  • the wafers 100 should protrude through both ends of the blade.
  • the width, thickness and length ranges will vary depending upon the shape of the grooves 131 cut into the object to be repaired.
  • the grooves 131 cut into the object to be repaired may vary depending upon the size of the fracture within the object to be repaired.
  • these wafers 100 may have tongue and grooved ends or edges, or some other type of interlocking, overlapping or other type of connection so that multiple wafers 100 may be used to fill larger grooved areas or to custom fit a series of wafers 100 into a grooved area. Any type of interlocking, overlapping or adjacent connection may be used.
  • jig 130 is placed adjacent to the object to be repaired. More specifically, jig 130 is positioned to create the desired grooves 131 or apertures, whether angled or not. Additionally, a jig having a wafer angulation configuration may be used with the wafers 100 (see Figs. 18 and 19). Referring to Fig. 18, the wafers 100 are configured at angles to create more reinforcement than if the wafers 100 were positioned along parallel axes and parallel surfaces to one another. Typically, as shown in Fig. 18, "A" represents the inside, or typically the puck-receiving portion of the hockey stick blade 4. Referring to Fig. 18, a greater surface area reinforcement is achieved by using the wafer angulation configuration. As seen in Fig.
  • the surface area reinforcement and strength withstanding capabilities can be described as follows: (B > A), (C > D) and (E>F).
  • the typical shearlines in this wafer angulation configuration are not similar to conventional shearlines.
  • the wafers 100 reinforce where conventional shearlines would be and reduce the likelihood of creating shearlines due to impact distribution.
  • staggered wafer 100 configuration may also be employed.
  • these wafers 100 used in the wafer angulation configuration may be independent of one another when used in a repair, may be connected to one another as described above and may be made of the materials as described above.
  • Fig. 20 shows one example of the wafer angulation configuration.
  • These wafers 100 are placed at approximately a 45 ° angle relative to the flat face of the hockey stick blade 4. While any angle may be used, typically a 30° or a 45° angle are preferred and provide an increased resistance to fracturing.
  • a custom length wafer 100 is required, it should be fashioned by cutting or sanding. It is important that the wafers 100 are organized relative to the position of each wafer 100 in the blade 4. Specifically, after the proper sized wafers 100 have been removed from the grooves 131, they should be placed in order (on a bench, for example) relative to their location in the blade 4. This is of particular importance if multiple wafers 100 are being used in an extended groove 131, as explained below.
  • an adhesive or sealant of the type previously discussed, is applied to the surface of the object (see Fig. 24). While this adhesive 9 is still wet, a small brush may be used to brush and smooth the surface of the sealant on the object. This smoothes the adhesive coated surface, distributes the sealant over the area to be repaired, and eliminates any voids (i.e., air pockets) in the adhesive-coated surface. The adhesive is allowed to cure for approximately 24 hours. After curing, the excess adhesive and wafer 100 material is removed from the surface of the object. This may be done by any means, including, but not limited to, a mechanical removal process (i.e. , sanding, scrapping, chiseling, etc.) or any type of a chemical process (i.e. , using a solvent or other type of chemical removal liquid and/or process). Sanding
  • holding the rods 12 or wafers 100 in the blade 4 is preferably sanded to smooth rough edges and to conform the repaired area to the general shape of the blade 4.
  • the sanding method best suited for sanding repair entails use of any angle drill 150 (die grinder) and small 2" (50mm) sanding disks. Grit can run from 36 to 100, depending on preference and precision. The bigger grit requires a delicate touch, but does scarify (i.e., rough up) the surface well. A shop vac or some type of dust collection system should be operated near the sanding disk to keep flying dust to a minimum.
  • the original stick 1 surface serves as a guide as to how much material should be removed.
  • the areas over the rod 12/wafer 100 inserts should be sanded until the outlines of the grooves 131 that were cut in the blade 4 can be clearly seen.
  • the blade 4 should be sanded at least 1" (40mm) past the area to be sleeved.
  • the area to be sleeved and that should be sanded should extend 1 inch past the rods 12/wafers 100 that extend furthest from the break.
  • the sleeved area should extend two inches (50mm) past the rods 12/wafers 100 toward the tip. This helps the blade 4 to flex more naturally and prevents wear on the repaired area.
  • the ends of the rods 12/wafers 100 create a shearing plane for future breakage.
  • the sleeved area should extend slightly up the hozel 3 if possible. This is a prime breakage area and with this preventative maintenance completed, the end-user will have a more durable repair.
  • edges of the blade 4 should be sanded very carefully. Because these surfaces are narrow, they can be notched or gouged quickly. Smooth long passes should be made on these areas. Hidden damage to the blade 4 that was previously overlooked may be visible at this time. These areas can usually be reinforced and repaired in the sleeving process. One of the most typical types of damage that shows up is a split along the bottom edge of the blade 4. When the blade 4 is sleeved, adhesive should be rubbed into this crack and then reinforced with carbon fiber tape. The bottom edge should usually be reinforced with tape as part of the final sleeving process. If further reconstruction is necessary, it is appropriate to do so before any sleeving takes place.
  • a sleeve 200 and/or separate piece of fabric are added over the repaired area to enhance strength and durability.
  • a sleeve and a fabric are used.
  • the structural strength enhancing sleeves 200 and fabrics 202 are generally comprised of woven materials. More specifically, the sleeves 200 and fabrics 202 (see Figs. 26 and 27) are typically comprised of one or more layers of woven fabric.
  • the sleeves 200 may be the same or similar length, but may be different lengths depending on the repair and geometry of the object being repaired.
  • An adhesive substance can be used to adhere the sleeve 200 to the damaged object and to hold the object together.
  • any type of adhesive may be used, including, but not limited to epoxy, epoxy resin, epoxy for wet applications (i.e., marine epoxy), multi-party epoxies, flex-epoxy, mercaptans, polyesters, urethanes, polyvinylchloride (PVC) cement, polyvinyl acetate, cellulose nitrate, polyvinyl butyral, polymethacrylates, methacrylates, polyvinyl alcohol, methylacrylate/ethyl methacrylate, polyurea, etc., and any combinations or any derivations of any of the above including polymers and/or copolymers of any of the above.
  • a bis- A based epoxy is preferred.
  • the woven material 202 layers may be the following types of materials, including, but not limited to fiberglass, KEVLAR ® , carbon fiber, wood, plastic, metal, etc. , however, typically carbon fiber is preferred.
  • the sleeves 200 may be made of any number of layers of these materials 202 within the range of from about 1-4 layers, more typically from about 1-3 layers, and most preferably 2 layers.
  • the sleeves 200 may be any width and thickness. The width and thickness will vary depending upon the size and shape of the object to be repaired.
  • the sleeves 200 and the fabric 202 should be cut to length.
  • the length should be enough to cover up the hozel 3 slightly and at least half of the blade 4.
  • the sleeve 200 should extend 1" (40mm) past both ends of the reinforcing rods 12.
  • the shaft 2 should be clamped firmly in a vise to ease painting of the adhesive over the entire sanded repair area, including the bottom of the shaft 2.
  • the fabric 202 should be applied to the bottom of the repair area.
  • the fabric 202 should cover the bottom edge and wrap just slightly to the front side.
  • the majority of the fabric 202 should be on the backside of the blade 4.
  • the purpose of the fabric 202 is to double up the reinforcement near the puck impact zone.
  • adhesive can be painted over the fabric 202.
  • the adhesive should be rubbed into the fabric 202 from the middle out toward the ends until it appears smooth.
  • additional adhesive should be applied.
  • the additional adhesive enhances the wetting out of the sleeve 200 that goes over the fabric 202.
  • the sleeve 200 may be slid over the blade 4 and fabric 202. The sleeve 200 should then be stretched outward from the middle to shrink the sleeve's diameter and tighten the sleeve 200 onto the blade 4.
  • the sleeve 200 should be painted with adhesive outwardly from the middle toward the ends in a similar fashion to the fabric 202.
  • the sleeve 200 should be fully saturated and smooth. Once the sleeve 200 is fully saturated and smooth, additional adhesive should be applied to be sure that enough adhesive has been added to the entire sleeved area. Multiple sleeves 200 and fabric 202 may be applied to the damaged area to increase the durability of the damaged area after the repair is complete. Curing
  • An appropriate flat support 204 will have a height that is less than the height of the blade 4. This ensures that the blade 4 edges are not covered by the flat support 204 and instead are in contact with a molding tape 205 that will be wrapped around the blade 4 and flat supports 204. This facilitates additional compression to the edge of the blade 4.
  • the supports 204 are preferably made of a resilient but slightly flexible material, such as polypropylene.
  • the blade 4 and flat supports 204 are then completely wrapped in the silicone tape 210, preferably 1-1/2" wide "square" EXTREME ® brand tape (see Fig. 29).
  • the flat supports 204 are clamped to the blade 4 using any clamping means desired, such as by a standard commercially available clamp 121, and the adhesive 9 is allowed to cure.
  • holes 216 may be punched in the tape 210 after it has been thoroughly wrapped over the blade 4 and flat supports 204. This allows excess adhesive 9 to ooze from the blade 4 area. In addition, this area may be wrapped with two layers of tape 210 to prevent splitting.
  • clamps 121 are added to compress the repair securely within the blade 4. Ideally, the clamps 121 will squeeze the repair to a thin, light, and smooth construction. Any number of clamps 121 may be necessary. Once the clamps 121 are in position and securely tightened, the tape 210 may be punctured to release excess adhesive. Any punctures in the tape 210 should not exceed 1 A inch in distance along the top and bottom edges of the blade 4. Too many holes 216 may result in tearing of the tape 210.
  • the repair should be allowed to cure for two days at approximately
  • the tape 210 is cut and removed, and the flat supports 204 are removed by peeling them away from the object. After the tape 210 and flat supports are removed, raised edges of cured adhesive 9 on the repair will be visible. This material should be removed by an angle drill 150 equipped with small sanding disks. Any adhesive that has been squeezed out onto the non-repair area should also be ground away. If any paint is removed, it can be repainted at a later time.
  • the adhesive may be removed by any means, including, but not limited to, a mechanical removal process (i.e. , sanding, scrapping, chiseling, etc.) or any type of a chemical process (i.e. , using a solvent or other type of chemical removal liquid and/or process). Cuts should not be made on the flat supports 204, as any imperfections, nicks or cuts may show on future repair jobs.
  • a mechanical removal process i.e. , sanding, scrapping, chiseling, etc.
  • a chemical process i.e. , using a solvent or other type of chemical removal liquid and/or process
  • the lacquer is applied to the surface of the sleeve 200 and to the surface of the object.
  • the lacquer is then allowed time to cure or dry.
  • the lacquer may include any type of sealant, including, but not limited to, a lacquer, an adhesive, a water-sealant, a UV-resistant sealant, a moisture-resistant sealant, etc.
  • a lacquer sealant is typically preferred.
  • the sealant is allowed to cure for approximately 24 hours.
  • the resulting repaired object is returned to its original strength, if not stronger.
  • the repaired area 250 is generally the same size and shape as the original object (see Fig. 31).
  • the adhesive is allowed to harden and is later sanded to conform with the shape of the missing/broken off portion of the blade 4 (Fig. 34).
  • adhesive 9 and sleeve 200 are added to the portion 260 (Fig. 35).
  • Adhesive 9 is added to the sleeve 200 after the sleeve 200 covers the damaged area 20 to make sure full saturation of the sleeve 200 has occurred.
  • the blade 4 is then secured between two compression members 211 (Fig. 36) having an inner soft layer 212 and an outer hard layer 214.
  • the compression members 211 are placed around the sleeve 200, adhesive 9 and blade 4 and clamps 121 are applied to the outer hard layer 214.
  • any other external portion of a hockey stick blade 4 may be repaired. Referring to Figs. 37 and 38, a heel portion of a hockey stick blade 4 is damaged and is therefore reinforced using either straight wafers 100 (Fig. 37) or grooved surface wafers 100 (Fig. 38).
  • the above-noted structural damage repair method and system may be used on any type of damaged object, including, but not limited to, hockey sticks (including blades, hozel, and shafts), boat hulls, automobiles, or any other type of object.
  • the above-noted wafers 100 and the structural damage repair method and system restore and/or enhance the structural integrity of the repaired object resulting in less twisting and more strength of the repaired object.

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  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Physical Education & Sports Medicine (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Biophysics (AREA)
  • Adhesives Or Adhesive Processes (AREA)

Abstract

L'invention concerne des éléments de réparation de dommages structurels, notamment des pièces rapportées et un kit de réparation de dommages structurels. Les éléments de réparation de dommages structurels comprennent en général au moins deux couches de matériaux entre lesquelles est disposé un adhésif, lesdites couches étant ensuite compressées l'une contre l'autre. Le kit de réparation de dommages structurels comprend un agent de moulage chimique, un gabarit facultatif, un ou plusieurs éléments de réparation de dommages structurels et un agent d'étanchéité. Le kit de l'invention permet à la fois de réparer des objets allongés creux et solides, ainsi que des objets courbés relativement plats. Parmi les éléments de réparation de dommages structurels, on trouve des tiges, des plaquettes, et/ou des pièces rapportées saturées adhésives.
PCT/US2005/046923 2004-12-23 2005-12-23 Elements et kit de reparation de dommages structurels WO2006071814A2 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EA200701350A EA200701350A1 (ru) 2004-12-23 2005-12-23 Элементы и комплект для ремонта структурных повреждений
CA002593863A CA2593863A1 (fr) 2004-12-23 2005-12-23 Elements et kit de reparation de dommages structurels
EP05855476A EP1828501A2 (fr) 2004-12-23 2005-12-23 Elements et kit de reparation de dommages structurels

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US63864604P 2004-12-23 2004-12-23
US60/638,646 2004-12-23

Publications (3)

Publication Number Publication Date
WO2006071814A2 true WO2006071814A2 (fr) 2006-07-06
WO2006071814A3 WO2006071814A3 (fr) 2006-09-08
WO2006071814B1 WO2006071814B1 (fr) 2006-11-16

Family

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PCT/US2005/046923 WO2006071814A2 (fr) 2004-12-23 2005-12-23 Elements et kit de reparation de dommages structurels

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Country Link
EP (1) EP1828501A2 (fr)
CA (1) CA2593863A1 (fr)
EA (1) EA200701350A1 (fr)
WO (1) WO2006071814A2 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018031682A1 (fr) * 2016-08-12 2018-02-15 Bauer Hockey Inc. Matériaux à mémoire de forme pour structures d'âme et procédés de réparation de structures d'âme
US10688359B2 (en) 2016-08-12 2020-06-23 Bauer Hockey Ltd. Recovery materials for core constructs and methods for repairing core constructs
CN113889366A (zh) * 2021-09-17 2022-01-04 符成波 水利工程用空心锥体瓷套湿法生产线组

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5175973A (en) * 1988-06-14 1993-01-05 Team, Inc. Compression repair method and apparatus
US5326410A (en) * 1993-03-25 1994-07-05 Timber Products, Inc. Method for reinforcing structural supports and reinforced structural supports
US6742314B2 (en) * 2002-02-04 2004-06-01 Robert A. Young Working poles and method of repair

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5175973A (en) * 1988-06-14 1993-01-05 Team, Inc. Compression repair method and apparatus
US5326410A (en) * 1993-03-25 1994-07-05 Timber Products, Inc. Method for reinforcing structural supports and reinforced structural supports
US6742314B2 (en) * 2002-02-04 2004-06-01 Robert A. Young Working poles and method of repair

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018031682A1 (fr) * 2016-08-12 2018-02-15 Bauer Hockey Inc. Matériaux à mémoire de forme pour structures d'âme et procédés de réparation de structures d'âme
US10688359B2 (en) 2016-08-12 2020-06-23 Bauer Hockey Ltd. Recovery materials for core constructs and methods for repairing core constructs
US10729957B2 (en) 2016-08-12 2020-08-04 Bauer Hockey, Llc Recovery materials for core constructs and methods for repairing core constructs
US10737157B2 (en) 2016-08-12 2020-08-11 Bauer Hockey, Llc Recovery materials for core constructs and methods for repairing core constructs
US11389704B2 (en) 2016-08-12 2022-07-19 Bauer Hockey, Llc Recovery materials for core constructs and methods for repairing core constructs
CN113889366A (zh) * 2021-09-17 2022-01-04 符成波 水利工程用空心锥体瓷套湿法生产线组

Also Published As

Publication number Publication date
EA200701350A1 (ru) 2007-12-28
CA2593863A1 (fr) 2006-07-06
WO2006071814A3 (fr) 2006-09-08
WO2006071814B1 (fr) 2006-11-16
EP1828501A2 (fr) 2007-09-05

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