US20140227467A1 - Hollow Wall Composite Tube - Google Patents
Hollow Wall Composite Tube Download PDFInfo
- Publication number
- US20140227467A1 US20140227467A1 US13/763,661 US201313763661A US2014227467A1 US 20140227467 A1 US20140227467 A1 US 20140227467A1 US 201313763661 A US201313763661 A US 201313763661A US 2014227467 A1 US2014227467 A1 US 2014227467A1
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- US
- United States
- Prior art keywords
- core
- tube
- providing
- fabric
- hollow
- 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
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 23
- 239000004744 fabric Substances 0.000 claims description 23
- 239000000470 constituent Substances 0.000 claims description 17
- 239000004593 Epoxy Substances 0.000 claims description 9
- 239000011159 matrix material Substances 0.000 claims 2
- 239000012783 reinforcing fiber Substances 0.000 claims 2
- 230000003014 reinforcing effect Effects 0.000 claims 1
- 239000011162 core material Substances 0.000 description 21
- 239000000835 fiber Substances 0.000 description 11
- 229920000049 Carbon (fiber) Polymers 0.000 description 5
- 239000004917 carbon fiber Substances 0.000 description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 230000003247 decreasing effect Effects 0.000 description 3
- 238000009730 filament winding Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- 229920006328 Styrofoam Polymers 0.000 description 1
- 229920006231 aramid fiber Polymers 0.000 description 1
- 210000000988 bone and bone Anatomy 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000002195 soluble material Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000008261 styrofoam Substances 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B1/00—Layered products having a non-planar shape
- B32B1/08—Tubular products
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B53/00—Golf clubs
- A63B53/10—Non-metallic shafts
-
- 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
-
- 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
-
- 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
- A63C—SKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
- A63C11/00—Accessories for skiing or snowboarding
- A63C11/22—Ski-sticks
- A63C11/227—Details; Structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2307/00—Use of elements other than metals as reinforcement
- B29K2307/04—Carbon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2023/00—Tubular articles
- B29L2023/22—Tubes or pipes, i.e. rigid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2024/00—Articles with hollow walls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/52—Sports equipment ; Games; Articles for amusement; Toys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2363/00—Epoxy resins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2597/00—Tubular articles, e.g. hoses, pipes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/1362—Textile, fabric, cloth, or pile containing [e.g., web, net, woven, knitted, mesh, nonwoven, matted, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/1369—Fiber or fibers wound around each other or into a self-sustaining shape [e.g., yarn, braid, fibers shaped around a core, etc.]
Definitions
- the present invention relates to products made from composite tubing and, more particularly, to tubular items in which strength and weight are at a premium. Golf club shafts, tennis rackets, ski poles, hockey sticks, fishing rods, and arrows are some examples.
- the invention also relates to lightweight structural members used in aerospace, sailboats, automobiles, and bicycles.
- Composite tubing is used because of its high strength-to-weight ratio. When more strength is desired in a composite tube, options are limited. Material can be upgraded, and wall thickness can be increased. When less weight is desired, wall thickness can be decreased, or holes can be added through the wall. Also a standard composite tube is configured exactly like a tubular bell. Having a single, solid wall like a bell creates maximum vibration after striking an object or flexural release. It also transmits vibration most efficiently to the human hand and adjacent bone structure, or in the case of an assembly, to the connecting components.
- Changing material can increase strength, but within narrow limits. Changing material can increase cost.
- a one piece composite tube having a hollow wall.
- the outside and inside diameters, and ends of the tube may have standard surfaces and shapes suitable for bonding or fastening.
- FIG. 1 is a section view of a hollow wall composite tube
- FIG. 2 is a perspective view of a flexible, shaped core, spiral wrapped with fiber or fabric, then spiral wrapped around a removable mandrel;
- FIG. 3 is a perspective view of a finished hollow wall composite tube with the hollow wall on one end exposed in detail.
- FIG. 1 is a section view of a hollow wall composite tube in accordance with the invention.
- the section view in FIG. 1 is cut parallel to the axis of the tube.
- the hollow 4 shown is arched for strength, like an architectural arch.
- the shape of the hollow 4 can be tuned to optimize performance in a given application. For example, if the tube is to be used as a golf club shaft, subject to severe side loads, the arch shaped hollow 4 strengthens the wall against collapse.
- FIG. 2 is a perspective view showing constituent tube 7 being wound onto a removable mandrel 5 . Also shown is constituent tube 7 being produced by spiral wrapping core 6 with tow (filaments) or fabric 8 prior to being wound on mandrel 5 . Tuning of the hollow 4 shape can be accomplished by changing the shape of core 6 .
- An elongated oval core 6 will produce an elongated oval hollow 4 after curing in a manner well known to those skilled in the art, and core 6 is removed by dissolving or melting.
- a round or rectangular cross section core 6 wrapped with fabric or filaments to form constituent tube 7
- Material used for making the core 6 may be wax, styrofoam, or otherwise meltable or soluble materials. After curing, the core can be melted or dissolved, with the helically traversing hollow providing a path for the core to drain out, leaving hollow 4 empty.
- core 6 is tubing, it can be pressurized and the mold and mandrel 5 can hold the constituent tube 7 supported by the core 6 , in a restrained position during epoxy cure, and the finish cured hollow 4 will have a shape corresponding to the mold and mandrel 5 .
- Mandrels are commonly used for the “layup” of composite fiber fabric, or filament winding of composite fiber in the manufacture of composite tubes. Typically carbon fiber filaments (called “tow”) or carbon fiber fabric is used, though other fibers and fabrics are also used.
- tow or fabric is wrapped on the mandrel already “wetted out” (called a “prepreg”) or encapsulated later, by injecting epoxy into the mold used to encapsulate the fibers and/or fabric.
- prepreg mandrel already “wetted out”
- these mandrels are tapered and coated with mold release or wax to facilitate easy removal.
- the mandrel forms the internal diameter of the tube, and typically a mold forms the outer diameter of the tube.
- Mandrels can be made from hardened steel or other metal and re-used.
- the present invention may have a ribbed interior on its inner diameter, in the form of a shallow helical groove if constituent tube 7 is crowned. This is due to the helical track formed by constituent tube 7 having been spirally wound on mandrel 5 . If the hollow 4 is crowned or arched as shown in FIG. 1 , there will be a small valley where the crowned winds of constituent tube 7 are tangent to each other. If the small valley on the internal diameter of the finished tube is “unfilled” and thus the internal diameter has ribs, then mandrel 5 extraction can be facilitated by rotating it, unscrewing it from the finished product. Leaving the internal surface unfilled and thus helically ribbed creates a slightly lighter structure without affecting aerodynamics if the shaft is to be swung through the air as with a golf shaft.
- the ribbed inner diameter of the tube to be produced may be filled between the crowned tops of the winds with fill, or just epoxy. This would produce a smooth inner diameter in the finished tube.
- the mandrel 5 can be extracted by pulling it straight out axially after curing in a manner well known to those skilled in the art.
- a narrow strip or strips of fiber or fabric can be wound on mandrel 5 before the constituent tube is wound onto mandrel 5 .
- This can produce a smoother inside diameter.
- Constituent tube 7 would necessarily be wound such that the crowned portion (if the preferred shape of hollow 4 is crowned) lies between the fill. So fill, consisting of stitching or fiber or fabric or any combination thereof, bridges the valley between the winds, and strengthens the area that would be prone to stress concentration. If core 6 is not pressurized with fluid or air, the winds of constituent tube 7 can be stitched together with carbon fiber thread, aramid fiber thread, or other suitable thread.
- This stitching can be done while constituent tube 7 is wound on the mandrel 5 or in combination with a strip or strip of tow or fabric 8 to fill the small unfilled area between the ribs, in accordance with provisional patent applications 61/656,010 and 61/671,700, referenced herein under “Related Applications”.
- the fiber content of the finished composite tube will be greater, resulting in higher strength.
- fill can be added in the helically traversing valley on the outer diameter of the pre-molded tube that would be formed by using a crowned core 6 inside constituent tube 7 .
- outer diameter can be accomplished by wrapping, in a manner well known to those skilled in the art, with carbon fiber fabric or filament winding or any combination, forming an outer sleeve.
- inner diameter can be accomplished by wrapping the mandrel 5 with fabric or fiber before the constituent tube 7 is deposited on it, forming an inner sleeve.
- FIG. 2 an end portion of constituent tube 7 is shown extended into the foreground, containing core 6 . In the finished product, this extended portion would not be present. Both ends would be cut perpendicular to the tube axis like a standard tube cut to length.
- the present invention's wound construction is in accordance with provisional patent applications 61/656,010 , 61/606,186, and 61/671,700, referenced herein under “Related Applications”, specifically FIG. 1 of each of the three listed provisional applications.
- FIG. 1 and FIG. 2 show a random length of the invention.
- FIG. 3 shows the invention configured as a golf shaft, mandrel 5 having been removed and core 6 melted or dissolved out or bonded in.
- the tube would be about 46 inches long.
- the gripped end would be approximately 5 ⁇ 8′′ diameter for an adult golf club, tapering smaller toward the clubhead end in the foreground.
- the mandrel can be removed and the core liquified and drained out (or in the opposite order), or in the case of a bonded in core, pressure is turned off to the core. Then the mold is opened, and the finished tube removed from the mold.
- the mold may be opened anytime after full cure, but for dimensional stability, it is usually preferable to open it as the last operation.
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- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Physical Education & Sports Medicine (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Golf Clubs (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
A one piece composite tube having a hollow wall structure. The outside and inside of the tube have a standard surface and shape for bonding or fastening. The hollow wall reduces vibration and allows consistent flexure and torsion. The shape of the hollow wall may be tuned to maintain light weight and optimize strength for a given application.
Description
- The present application is a continuation-in-part application of U.S. provisional patent application, Ser. No. 61/606,186, filed Mar. 2, 2012, by Robert Burch Fraidenburgh, Woodside, Calif., included by reference herein and for which benefit of the priority date is hereby claimed.
- The present application is a continuation-in-part application of U.S. provisional patent application, Ser. No. 61/656,010, filed Jun. 6, 2012, by Robert Burch Fraidenburgh, Woodside, Calif., included by reference herein and for which benefit of the priority date is hereby claimed.
- The present application is a continuation-in-part application of U..S provisional patent application, Ser. No. 61/671,700, filed Jul. 14, 2012, by Robert Burch Fraidenburgh, Woodside, Calif., included by reference herein and for which benefit of the priority date is hereby claimed.
- The present invention relates to products made from composite tubing and, more particularly, to tubular items in which strength and weight are at a premium. Golf club shafts, tennis rackets, ski poles, hockey sticks, fishing rods, and arrows are some examples. The invention also relates to lightweight structural members used in aerospace, sailboats, automobiles, and bicycles.
- Composite tubing is used because of its high strength-to-weight ratio. When more strength is desired in a composite tube, options are limited. Material can be upgraded, and wall thickness can be increased. When less weight is desired, wall thickness can be decreased, or holes can be added through the wall. Also a standard composite tube is configured exactly like a tubular bell. Having a single, solid wall like a bell creates maximum vibration after striking an object or flexural release. It also transmits vibration most efficiently to the human hand and adjacent bone structure, or in the case of an assembly, to the connecting components.
- Other solutions have involved substituting higher modulus fiber (generally carbon fiber), wrapping with filament or fabric at varying angles to create biased plies, using higher stiffness epoxy to increase strength, and decreasing wall thickness to decrease weight.
- Decreasing wall thickness to reduce weight can have catastrophic results. A single unsupported wall is subject to distortion, vibration, buckling, even cracking and splitting. Increasing strength by thickening the wall adds weight.
- Changing material can increase strength, but within narrow limits. Changing material can increase cost.
- In accordance with the present invention, there is provided a one piece composite tube having a hollow wall. The outside and inside diameters, and ends of the tube may have standard surfaces and shapes suitable for bonding or fastening.
- It would be advantageous to provide a composite tube having a hollow wall for light weight and strength.
- It would also be advantageous to provide a composite tube resistant to vibration, while maintaining light weight.
- It would also be advantageous to provide a composite tube resistant to distortion when flexed, loaded, or subjected to torque.
- A complete understanding of the present invention may be obtained by reference to the accompanying drawings, when considered in conjunction with the subsequent, detailed description, in which:
-
FIG. 1 is a section view of a hollow wall composite tube; -
FIG. 2 is a perspective view of a flexible, shaped core, spiral wrapped with fiber or fabric, then spiral wrapped around a removable mandrel; and -
FIG. 3 is a perspective view of a finished hollow wall composite tube with the hollow wall on one end exposed in detail. - For purposes of clarity and brevity, like elements and components will bear the same designations and numbering throughout the Figures.
-
FIG. 1 is a section view of a hollow wall composite tube in accordance with the invention. The section view inFIG. 1 is cut parallel to the axis of the tube. The hollow 4 shown is arched for strength, like an architectural arch. The shape of the hollow 4 can be tuned to optimize performance in a given application. For example, if the tube is to be used as a golf club shaft, subject to severe side loads, the arch shapedhollow 4 strengthens the wall against collapse. -
FIG. 2 is a perspective view showingconstituent tube 7 being wound onto aremovable mandrel 5. Also shown isconstituent tube 7 being produced by spiral wrappingcore 6 with tow (filaments) orfabric 8 prior to being wound onmandrel 5. Tuning of the hollow 4 shape can be accomplished by changing the shape ofcore 6. An elongatedoval core 6 will produce an elongatedoval hollow 4 after curing in a manner well known to those skilled in the art, andcore 6 is removed by dissolving or melting. Likewise a round or rectangular cross section core 6 (wrapped with fabric or filaments to form constituent tube 7) can produce a round or rectangular shaped hollow 4. Material used for making thecore 6 may be wax, styrofoam, or otherwise meltable or soluble materials. After curing, the core can be melted or dissolved, with the helically traversing hollow providing a path for the core to drain out, leaving hollow 4 empty. - If
core 6 is tubing, it can be pressurized and the mold andmandrel 5 can hold theconstituent tube 7 supported by thecore 6, in a restrained position during epoxy cure, and the finish cured hollow 4 will have a shape corresponding to the mold andmandrel 5. - Mandrels are commonly used for the “layup” of composite fiber fabric, or filament winding of composite fiber in the manufacture of composite tubes. Typically carbon fiber filaments (called “tow”) or carbon fiber fabric is used, though other fibers and fabrics are also used. In a common method of producing composite tubing, tow or fabric is wrapped on the mandrel already “wetted out” (called a “prepreg”) or encapsulated later, by injecting epoxy into the mold used to encapsulate the fibers and/or fabric. In the manufacture of golf shafts these mandrels are tapered and coated with mold release or wax to facilitate easy removal. The mandrel forms the internal diameter of the tube, and typically a mold forms the outer diameter of the tube. Mandrels can be made from hardened steel or other metal and re-used. The present invention may have a ribbed interior on its inner diameter, in the form of a shallow helical groove if
constituent tube 7 is crowned. This is due to the helical track formed byconstituent tube 7 having been spirally wound onmandrel 5. If the hollow 4 is crowned or arched as shown inFIG. 1 , there will be a small valley where the crowned winds ofconstituent tube 7 are tangent to each other. If the small valley on the internal diameter of the finished tube is “unfilled” and thus the internal diameter has ribs, thenmandrel 5 extraction can be facilitated by rotating it, unscrewing it from the finished product. Leaving the internal surface unfilled and thus helically ribbed creates a slightly lighter structure without affecting aerodynamics if the shaft is to be swung through the air as with a golf shaft. - Or the ribbed inner diameter of the tube to be produced may be filled between the crowned tops of the winds with fill, or just epoxy. This would produce a smooth inner diameter in the finished tube. In this case the
mandrel 5 can be extracted by pulling it straight out axially after curing in a manner well known to those skilled in the art. - To strengthen and fill between the crowned areas of the
constituent tube 7, a narrow strip or strips of fiber or fabric can be wound onmandrel 5 before the constituent tube is wound ontomandrel 5. This can produce a smoother inside diameter.Constituent tube 7 would necessarily be wound such that the crowned portion (if the preferred shape of hollow 4 is crowned) lies between the fill. So fill, consisting of stitching or fiber or fabric or any combination thereof, bridges the valley between the winds, and strengthens the area that would be prone to stress concentration. Ifcore 6 is not pressurized with fluid or air, the winds ofconstituent tube 7 can be stitched together with carbon fiber thread, aramid fiber thread, or other suitable thread. This stitching can be done whileconstituent tube 7 is wound on themandrel 5 or in combination with a strip or strip of tow orfabric 8 to fill the small unfilled area between the ribs, in accordance with provisional patent applications 61/656,010 and 61/671,700, referenced herein under “Related Applications”. - If the unfilled area on the outer diameter is filled by strips of fabric or stitching, or both, the fiber content of the finished composite tube will be greater, resulting in higher strength. Likewise fill can be added in the helically traversing valley on the outer diameter of the pre-molded tube that would be formed by using a crowned
core 6 insideconstituent tube 7. - Further strengthening of the outer diameter can be accomplished by wrapping, in a manner well known to those skilled in the art, with carbon fiber fabric or filament winding or any combination, forming an outer sleeve. Likewise strengthening of the inner diameter can be accomplished by wrapping the
mandrel 5 with fabric or fiber before theconstituent tube 7 is deposited on it, forming an inner sleeve. - In
FIG. 2 , an end portion ofconstituent tube 7 is shown extended into the foreground, containingcore 6. In the finished product, this extended portion would not be present. Both ends would be cut perpendicular to the tube axis like a standard tube cut to length. The present invention's wound construction is in accordance with provisional patent applications 61/656,010 , 61/606,186, and 61/671,700, referenced herein under “Related Applications”, specifically FIG. 1 of each of the three listed provisional applications. - Both
FIG. 1 andFIG. 2 show a random length of the invention. -
FIG. 3 shows the invention configured as a golf shaft,mandrel 5 having been removed andcore 6 melted or dissolved out or bonded in. In the case of many golf shafts, the tube would be about 46 inches long. The gripped end would be approximately ⅝″ diameter for an adult golf club, tapering smaller toward the clubhead end in the foreground. - Thus having suitable epoxy, tow and/or fabric, core material, a mandrel and a mold, those skilled in the art can wind the tow or fabric on a shaped core, wind that wrapped core around a mandrel, and clamp the assembly in a mold, the fiber having been pre-impregnated or to be encapsulated by epoxy injection while in the mold.
- After epoxy cure, the mandrel can be removed and the core liquified and drained out (or in the opposite order), or in the case of a bonded in core, pressure is turned off to the core. Then the mold is opened, and the finished tube removed from the mold. The mold may be opened anytime after full cure, but for dimensional stability, it is usually preferable to open it as the last operation.
- Since other modifications and changes varied to fit particular operating requirements and environments will be apparent to those skilled in the art, the invention is not considered limited to the example chosen for purposes of disclosure, and covers all changes and modifications which do not constitute departures from the true spirit and scope of this invention.
- Having thus described the invention, what is desired to be protected by Letters Patent is presented in the subsequently appended claims.
Claims (5)
1. A hollow wall composite tube for improving performance in sports shafts and lightweight structural members, comprising:
means for providing an adjustable shape on which to wind or braid filaments or fabric;
means for providing a reinforcing fiber matrix for saturation with epoxy, spirally wrapped or braided to said means for providing an adjustable shape on which to wind filaments or fabric;
means for reducing weight, reinforcing, providing a path for the core to be evacuated, conformally wrapped around said means for providing an adjustable shape on which to wind or braid filaments or fabric;
2. The hollow wall composite tube in accordance with claim 1 , wherein said means for providing an adjustable shape on which to wind or braid filaments or fabric comprises a flexible core.
3. The hollow wall composite tube in accordance with claim 1 , wherein said means for reducing weight, providing a path for the core to be evacuated comprises an adjustable shape hollow.
4. The hollow wall composite tube in accordance with claim 1 , wherein said means for forming the wall of the invention comprises a constituent tube.
5. A hollow wall composite tube for improving performance in sports shafts and lightweight structural members, comprising:
a flexible core, for providing an adjustable shape on which to wind or braid filaments or fabric;
tow or fabric, for providing a reinforcing fiber matrix for saturation with epoxy, spirally wrapped or braided on said core;
an adjustable shape hollow, for reducing weight, providing a path for the core to be evacuated, tightly conformed to said core; and
a constituent tube, for forming the wall of the invention.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/763,661 US20140227467A1 (en) | 2013-02-09 | 2013-02-09 | Hollow Wall Composite Tube |
| US14/480,421 US9802365B2 (en) | 2012-03-02 | 2014-09-08 | Hollow wall composite tube, methods of production and uses thereof |
| US15/796,820 US20180117858A1 (en) | 2012-03-02 | 2017-10-29 | Hollow wall composite tube, methods of production and uses thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/763,661 US20140227467A1 (en) | 2013-02-09 | 2013-02-09 | Hollow Wall Composite Tube |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/480,421 Continuation US9802365B2 (en) | 2012-03-02 | 2014-09-08 | Hollow wall composite tube, methods of production and uses thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20140227467A1 true US20140227467A1 (en) | 2014-08-14 |
Family
ID=51297619
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US13/763,661 Abandoned US20140227467A1 (en) | 2012-03-02 | 2013-02-09 | Hollow Wall Composite Tube |
| US14/480,421 Expired - Fee Related US9802365B2 (en) | 2012-03-02 | 2014-09-08 | Hollow wall composite tube, methods of production and uses thereof |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/480,421 Expired - Fee Related US9802365B2 (en) | 2012-03-02 | 2014-09-08 | Hollow wall composite tube, methods of production and uses thereof |
Country Status (1)
| Country | Link |
|---|---|
| US (2) | US20140227467A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200061872A1 (en) * | 2018-08-23 | 2020-02-27 | Marshal Industrial Corp. | Method of manufacturing a carbon fiber wheel rim |
| CN111137433A (en) * | 2018-11-02 | 2020-05-12 | 波音公司 | Composite structure composed of coiled tubular braid |
| US20220274355A1 (en) * | 2019-06-21 | 2022-09-01 | Marshal Industrial Corp. | Method of manufacturing a composite rim |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11213995B2 (en) | 2018-11-02 | 2022-01-04 | The Boeing Company | Composite structures constructed of wound tubular braiding |
| US11345099B2 (en) * | 2018-11-02 | 2022-05-31 | The Boeing Company | Composite structures constructed of wound tubular braiding |
| US11896880B2 (en) | 2020-07-10 | 2024-02-13 | Karsten Manufacturing Corporation | Ultra high stiffness putter shaft |
| US11649042B2 (en) | 2020-07-14 | 2023-05-16 | Lockheed Martin Corporation | Collapsible spar mandrel |
| JP7779128B2 (en) * | 2021-12-20 | 2025-12-03 | 住友ゴム工業株式会社 | Shaft and manufacturing method thereof |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0298376A (en) * | 1988-10-04 | 1990-04-10 | Ryobi Ltd | Shaft for golf club and manufacture thereof |
| US5968621A (en) * | 1996-01-16 | 1999-10-19 | Shimano, Inc. | Tubular member |
| US5988612A (en) * | 1997-08-07 | 1999-11-23 | Bertelson; Peter C. | Composite helical springs and process of manufacture |
-
2013
- 2013-02-09 US US13/763,661 patent/US20140227467A1/en not_active Abandoned
-
2014
- 2014-09-08 US US14/480,421 patent/US9802365B2/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200061872A1 (en) * | 2018-08-23 | 2020-02-27 | Marshal Industrial Corp. | Method of manufacturing a carbon fiber wheel rim |
| US10792843B2 (en) * | 2018-08-23 | 2020-10-06 | Marshal Industrial Corp. | Method of manufacturing a carbon fiber wheel rim |
| CN111137433A (en) * | 2018-11-02 | 2020-05-12 | 波音公司 | Composite structure composed of coiled tubular braid |
| US20220274355A1 (en) * | 2019-06-21 | 2022-09-01 | Marshal Industrial Corp. | Method of manufacturing a composite rim |
| US11813809B2 (en) * | 2019-06-21 | 2023-11-14 | Marshal Industrial Corp. | Method of manufacturing a composite rim |
Also Published As
| Publication number | Publication date |
|---|---|
| US9802365B2 (en) | 2017-10-31 |
| US20140377490A1 (en) | 2014-12-25 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STCB | Information on status: application discontinuation |
Free format text: EXPRESSLY ABANDONED -- DURING EXAMINATION |