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US20140227467A1 - Hollow Wall Composite Tube - Google Patents

Hollow Wall Composite Tube Download PDF

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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
Application number
US13/763,661
Inventor
Robert Burch Fraidenburgh
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Individual
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 US13/763,661 priority Critical patent/US20140227467A1/en
Publication of US20140227467A1 publication Critical patent/US20140227467A1/en
Priority to US14/480,421 priority patent/US9802365B2/en
Priority to US15/796,820 priority patent/US20180117858A1/en
Abandoned legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00Layered products having a non-planar shape
    • B32B1/08Tubular products
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63BAPPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B53/00Golf clubs
    • A63B53/10Non-metallic shafts
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63BAPPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B60/00Details or accessories of golf clubs, bats, rackets or the like
    • A63B60/06Handles
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63BAPPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B2209/00Characteristics of used materials
    • A63B2209/02Characteristics of used materials with reinforcing fibres, e.g. carbon, polyamide fibres
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63BAPPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B59/00Bats, rackets, or the like, not covered by groups A63B49/00 - A63B57/00
    • A63B59/70Bats, 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
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63CSKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
    • A63C11/00Accessories for skiing or snowboarding
    • A63C11/22Ski-sticks
    • A63C11/227Details; Structure
    • 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
    • B29K2063/00Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
    • 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
    • B29K2307/00Use of elements other than metals as reinforcement
    • B29K2307/04Carbon
    • 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
    • B29L2023/00Tubular articles
    • B29L2023/22Tubes or pipes, i.e. rigid
    • 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
    • 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
    • B29L2031/52Sports equipment ; Games; Articles for amusement; Toys
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2363/00Epoxy resins
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2597/00Tubular articles, e.g. hoses, pipes
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]
    • Y10T428/1352Polymer or resin containing [i.e., natural or synthetic]
    • Y10T428/1362Textile, fabric, cloth, or pile containing [e.g., web, net, woven, knitted, mesh, nonwoven, matted, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]
    • Y10T428/1352Polymer or resin containing [i.e., natural or synthetic]
    • Y10T428/1369Fiber 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

    RELATED APPLICATIONS
  • 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.
  • FIELD OF THE INVENTION
  • 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.
  • BACKGROUND OF THE INVENTION
  • 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.
  • SUMMARY OF THE INVENTION
  • 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.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • 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.
  • DESCRIPTION OF THE PREFERRED EMBODIMENT
  • 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. 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 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.
  • If 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. 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 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.
  • 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 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”.
  • 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 inside constituent 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 the constituent tube 7 is deposited on it, forming an inner sleeve.
  • In 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.
  • Both 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. 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)

What is claimed is:
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.
US13/763,661 2012-03-02 2013-02-09 Hollow Wall Composite Tube Abandoned US20140227467A1 (en)

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

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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

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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

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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

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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

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