WO2022246160A1 - Structures annulaires formées de matériaux composites et systèmes et procédés de formation de structures annulaires à partir de matériaux composites - Google Patents

Structures annulaires formées de matériaux composites et systèmes et procédés de formation de structures annulaires à partir de matériaux composites Download PDF

Info

Publication number
WO2022246160A1
WO2022246160A1 PCT/US2022/030197 US2022030197W WO2022246160A1 WO 2022246160 A1 WO2022246160 A1 WO 2022246160A1 US 2022030197 W US2022030197 W US 2022030197W WO 2022246160 A1 WO2022246160 A1 WO 2022246160A1
Authority
WO
WIPO (PCT)
Prior art keywords
component part
strip
mandrel
circumference
fiber reinforced
Prior art date
Application number
PCT/US2022/030197
Other languages
English (en)
Inventor
Ben BOSWORTH
Matt Giaraffa
Meghan BUCHOLZ
Ian Ramsay
Sam Nichols
Original Assignee
Guerrilla Industries LLC
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
Priority claimed from US17/748,965 external-priority patent/US20220371260A1/en
Application filed by Guerrilla Industries LLC filed Critical Guerrilla Industries LLC
Priority to EP22736409.8A priority Critical patent/EP4132774A1/fr
Publication of WO2022246160A1 publication Critical patent/WO2022246160A1/fr

Links

Classifications

    • 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
    • B29C70/32—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 on a rotating mould, former or core
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3091—Bicycles
    • 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
    • B29L2031/32—Wheels, pinions, pulleys, castors or rollers, Rims
    • B29L2031/322—Wheels, pinions, pulleys, castors or rollers, Rims made wholly of plastics

Definitions

  • the present disclosure provides annular structures formed from composite materials and systems and methods for forming annular structures from composite materials.
  • the annular structures can include, but are not limited to, bicycle wheel rims.
  • Composite materials have a variety of advantages as compared to alternate materials, such as steel, aluminum, or wood. For example, composite materials can be used to form structures having intricate shapes, allowing strength and aesthetics to be optimized. Composite materials have also been used to form annular structures, such as the rims of bicycle wheels. The potential strength to weight ratio of structures formed using carbon fiber composites is very high, and products formed from carbon fiber composites, commonly referred to as simply “carbon fiber”, are also popular with consumers.
  • composite structures are typically formed by laying multiple sheets of composite material in a mold. Each sheet includes fibers that are oriented along one or several directions or plies, and that generally extend from one edge of the sheet to another. More particularly, different layers of material, having the associated ply or plies oriented in a specific direction, are placed in a mold and set into a final form using a two-part epoxy. In addition to being time-consuming and labor-intensive, such techniques are prone to defects when used to form complex structures time efficiently.
  • composite structures have typically used thermoset materials that are relatively brittle and difficult to recycle.
  • structures can be formed relatively quickly and cheaply using injection molding.
  • the structures formed using such processes are typically quite weak.
  • the annular composite structures can include wheel rims formed from one or more sheets of fiber reinforced thermoplastic material. Each of the sheets can include one or more layers. The sheet or sheets are fused to form the completed annular structure.
  • Methods in accordance with embodiments of the present disclosure include providing a mandrel or mold.
  • a sheet or strip of fiber reinforced thermoplastic material is clamped or otherwise fixed to the mandrel, and the mandrel is turned, bending a portion of the strip about the mandrel.
  • the strip can be warmed before or as it is bent about the mandrel.
  • the mandrel can itself be heated.
  • the portion of the strip that has been bent about the mandrel can also be placed under pressure, for example by a shoe or rollers. The shoe or rollers can also be heated.
  • multiple strips of fiber reinforced thermoplastic or composite material can be used to form the annular structure.
  • an additional strip can be clamped to the mandrel such that it at least partially overlaps a strip previously bent about the mandrel. Overlapping portions of the multiple strips are then at least partially consolidated as the strips are placed on the mandrel. After all of the strips have been bent about the mandrel, a final step of heating and applying pressure can be performed to fuse the strips, or portions of a single strip, to one another. The now integral annular composite structure can then be removed from the mold, and any desired finishing steps can be performed.
  • Systems for forming annular structures can include a feed assembly, a preheating assembly, a mandrel, and a forming assembly that includes an external mold or forming surface.
  • the feed assembly is configured to receive a strip of fiber reinforced thermoplastic material, and to pass the strip of material past or through the preheating assembly, before introducing the strip of material to the mandrel.
  • the preheating assembly can include, for example, infrared heaters positioned on opposite sides of the strip of material.
  • the mandrel can include clamps that function to fix an end of a strip of fiber reinforced thermoplastic material to the mandrel.
  • the mandrel generally incorporates or forms an inner mold having a shape that mirrors the shape of the inner surfaces of the annular structure (i.e., the surfaces that generally face a center point of the completed structure).
  • each strip of fiber reinforced thermoplastic material contains multiple sheets or layers of fiber reinforced composite thermoplastic material.
  • Each sheet can have fibers oriented in different directions.
  • a first sheet can have relatively short fibers oriented randomly
  • a second sheet can include relatively long, unidirectional fibers oriented parallel to one another in a first direction
  • a third sheet can include relatively long unidirectional fibers oriented parallel to one another in a second direction that is at a selected angle relative to the fibers of the second sheet
  • a fourth sheet with fibers of different lengths and orientations can be used to be used.
  • Fig. 1 depicts a bicycle wheel incorporating an annular composite structure in accordance with embodiments of the present disclosure
  • Fig. 2 is a perspective view of an annular composite structure in accordance with embodiments of the present disclosure
  • Fig. 3 is a side view in elevation of an annular composite structure in accordance with embodiments of the present disclosure
  • Figs. 4A and 4B depict example cross-sections of an annular composite structure in accordance with embodiments of the present disclosure
  • Fig. 5A depicts a relationship between components of an annular composite structure in accordance with embodiments of the present disclosure in a side elevation view
  • Figs. 5B and 5C depict example relationships between components of an annular composite structure in accordance with embodiments of the present disclosure in cross sectional views;
  • Figs. 6A and 6B depict a component of an annular composite structure in accordance with embodiments of the present disclosure in side elevation and top plan views respectively;
  • Figs. 6C and 6D depict variants of a component of an annular composite structure in accordance with embodiments of the present disclosure in end elevation views;
  • Figs. 7A-7D are plan views depicting a system for forming annular composite structures in accordance with embodiments of the present disclosure
  • Figs. 8A-8D are cross-sectional views of portions of a system for forming annular composite in accordance with embodiments of the present disclosure
  • Fig. 9 depicts steps of forming an annular composite structure in accordance with embodiments of the present disclosure.
  • Fig. 10 is a flowchart depicting a method for forming an annular composite structure in accordance with embodiments of the present disclosure.
  • Fig. 1 depicts a bicycle wheel 100 that includes an example of an annular composite structure 104 formed from fiber reinforced thermoplastic material in accordance with embodiments of the present disclosure.
  • the annular composite structure 104 is a bicycle wheel rim 108.
  • the wheel 100 generally includes a hub 112 and spokes 116 interconnecting the rim 108 to the hub 112.
  • an annular composite structure 104 in accordance with embodiments of the present disclosure can include various other annular structures.
  • Figs. 2 and 3 are perspective and elevation views respectively of the annular composite structure 104 in the form of a bicycle wheel rim 108 in accordance with embodiments of the present disclosure.
  • the rim 108 can include spoke holes 204 and a valve hole 208.
  • Figs. 4A and 4B depict variants of the rim 108 in a cross section taken at section line 4-4’ in Fig. 2.
  • the rim 108 or structure 104 has an outer (or outward facing) circumferential surface 404 and an inner (or inward facing) circumferential surface 408.
  • the outer circumferential surface 404 can be dished in overall profile (in cross section), and can include a flat, dished, or otherwise profiled (in cross-section) central support section 406.
  • the inner circumferential surface 408 can have a profile that generally mirrors the profile of the outer circumferential surface 404.
  • the rim 108 can include a pair of flanges 412 for engaging the sides or the beads of a beaded tire (not shown) that extend from the central support section 406.
  • the structure 104 can be generally uniform in thickness, in which case the inner circumferential surface 408 can have a profile that generally mirrors the profile of the outer circumferential surface 404.
  • the structure 104 can feature areas or sections of varying thickness, forming shoulders, tapered elements, grooves, or the like.
  • at least some embodiments of the present disclosure can include enlarged or hook sections 416 proximate the edges of the flanges 412 (as shown in Fig. 4B) for engaging the beads of a mounted beaded or clincher tire.
  • Other embodiments can be configured as “hookless” rims 108, in which the flanges 412 have generally featureless tire engaging surfaces (as shown in Fig. 4A).
  • Still other embodiments can be formed without flanges 412 extending from the central support section 406, as in rims 108 configured for use with tubular tires, or rims configured for use with airless or non-pneumatic tires.
  • annular composite structure 104 can be formed from multiple component parts.
  • a single annular composite structure 104 can be formed from four component parts 504, labeled 504a-504d in the figures (note that the thickness of the individual component parts 504 relative to other dimensions of those parts have been exaggerated for illustration purposes).
  • Each component part 504 in this example is a strip of fiber reinforced thermoplastic material. The length of the component part or strip 504 is equal to or about equal to the circumference of the annular structure 104(where
  • each strip 504 join or butt against each other at a seam 508.
  • the different component parts 504 can be incorporated into the structure 104 such that their associated seams 508 are offset from one another.
  • four component parts 504 having a length that is about equal to the circumference of the annular structure 104 are combined to form a four layered structure 104.
  • the seams 508 are offset from one another by about 90 degrees.
  • each component part 504 can be fused to one or more of the other component parts 504, forming an integral composite structure
  • a single component part 504 can have a length that is different than a circumference of the annular structure
  • multiple component parts 504, each having a length that is less than a circumference of the annular structure 104, can be incorporated into that structure 104.
  • eight component parts that each have a length of about one-half the circumference of the annular structure 104 can be combined to form a four layered structure, and the seams can be offset from one another by about 45 degrees.
  • the annular structure can include one or more component parts 504 with a length that is greater than the circumference of the annular structure 104.
  • two component parts 504 each having a length that is twice that of the annular structure 104 can be combined to form a four layered structure 104, and their seams can be offset by 180 degrees.
  • a single component part 504 having a length that is two or more times the circumference of the annular structure 104 can be used, alone or in combination with other component parts 504, to form a multiple layered structure 104.
  • an annular structure can include component parts 504 of different lengths, such as one component part 504 having a length about equal to the circumference of the structure 104, and two component parts 504 having a length of about half the circumference of the structure 104, to form a two layered annular structure 104.
  • each component part 504 can have the same width, and that width can be equal or about equal to a width of the annular composite structure, or that is wide enough to span the entire width of the annular composite structure 104 after molding and fusing, as described elsewhere herein, to achieve the desired final shape of the composite structure 104, has been completed.
  • Fig. 5B each component part 504 can have the same width, and that width can be equal or about equal to a width of the annular composite structure, or that is wide enough to span the entire width of the annular composite structure 104 after molding and fusing, as described elsewhere herein, to achieve the desired final shape of the composite structure 104, has been completed.
  • Fig. 5B depict component parts 504 of a composite structure 104 in a transverse cross section
  • different component parts 504 can have different widths, and thus less than all of the component parts 504 have a width that is enough to span the entire width of the formed composite structure 104.
  • different component parts 504 can have different thicknesses.
  • different component parts can have different widths and/or thicknesses at different locations within the structure 104.
  • Figs. 6A and 6B depict an example component part 504 of an annular composite structure 104 in side elevation and top plan views respectively.
  • Figs. 6C and 6D depict variants of the example component part of Figs. 6A and 6B in end elevation views.
  • the length of each strip or component part 504 can be equal or about equal to the circumference of the annular composite structure 104. In accordance with other embodiments of the present disclosure, some or all of the strips or component parts 504 have a length that is greater or less than the circumference of the annular composite structure 104.
  • annular composite structure 104 can be formed using a single strip or component part 504 with a length that is greater than the circumference of the annular structure 104.
  • annular composite structure can include one or more strips or component parts 504 that wrap around the circumference of the annular structure 104 multiple (e.g. 2-5) times.
  • each strip or component part 504 can include a stack of multiple sheets or layers 604 of fiber reinforced thermoplastic material.
  • a component part 504 can include a single layer 604 of fiber reinforced thermoplastic material.
  • Each layer 604 can have a size that is equal or about equal to the finished size of the component part 504, as depicted in Figs. 6A and 6C.
  • a strip 504 can be formed from partially overlapping layers 604 having an individual size that is smaller than the component 504 incorporating the layers 604.
  • a component part 504 can be contoured in cross section by incorporating individual sheets 604 having different widths, as depicted in Fig. 6D.
  • different layers 604 within a component part 504 can have dimensions that vary along the length of the layer 604.
  • each layer 604 can itself include one or more layers or plies of fibers embedded in a thermoplastic material.
  • Different layers 604 within a component part 504 can have different fiber orientations and configurations.
  • one or more sheets 604 within a strip 504 can feature relatively long fibers that are parallel to one another (i.e.
  • one or more sheets 604 within a strip 504 can feature relatively long fibers that are parallel to one another and that are oriented at a nonzero angle relative to a longitudinal axis of the strip 504 in which the sheet 604 is incorporated.
  • a strip 504 can include at least some layers 604 with relatively long reinforcing fibers at a selected angle relative to other layers 604 within the same strip 504.
  • the layers 604 with relatively long fibers can have those fibers configured unidirectionally, such that the fibers 512 extend in the same general direction, but not necessarily parallel to one another.
  • Other layers 604 can include fibers of moderate length (e.g., greater than 10mm) that have varying angles relative to one another.
  • Still other layers 604 can have relatively short, randomly oriented fibers 512. More particularly, the fibers can be randomly oriented in at least a plane encompassing the edges of the layer when that layer 604 is in a flat configuration.
  • the fibers in a layer 604 incorporating randomly oriented fibers can be relatively short (e.g. less than 10 mm), and generally do not extend between opposite edges of the layer 604.
  • the fibers within a sheet 604 can be woven, with subsets of fibers at selected angles with respect to other subsets of fibers within the layer 604.
  • a strip 504 having four layers 604 is illustrated, it should be appreciated that a strip 504 can include any number of layers 604.
  • the strip 504 is formed as a planar or substantially planar panel from textile-like composite sheets or layers 604.
  • the individual sheets may or may not be flexible at room temperature.
  • Each of the composite sheets 604 may be in the form of a substantially continuous sheet, for example in the shape of a rectangle, that is trimmed to form edges and to size the respective sheet 604 for inclusion in the strip 504.
  • the sheets or layers 604 are then stacked with one another to form the layup of the composite strip 504, and then may be fused, to complete the strip 504.
  • some or all of the composite sheets 604 may be trimmed after being fused to one or more other composite sheets 604.
  • the fusing of multiple sheets 604 to form a composite strip 504 can be performed while the sheets are held under tension.
  • the layers 604 of a strip 504 are loosely stacked or only partially consolidated prior to winding the strip 504 about itself or other strips 504 of the structure 104.
  • Figs. 7A-7D and 8A-8D depict components of an apparatus or system 704 for manufacturing an annular composite structure 104 in accordance with embodiments of the present disclosure.
  • the apparatus 704 includes a mandrel 708.
  • One or more clamps or clamp assemblies 712 are provided as part of or attached to the mandrel 708.
  • clamp assemblies 712 or mounting points for a clamp assembly 712 are located at 90 degree intervals around the mandrel 708.
  • the system 704 additionally includes a forming assembly 716, for example configured as a shoe or roller assembly, adjacent the mandrel 708.
  • a feed assembly 720 is also adjacent to the mandrel 708, and extends through a preheating assembly 724.
  • the system 704 can further include a base structure or assembly 726 through which various components of the system 704 are interconnected, and which can house or mount other components of the system 704, such as control electronics, motors, power supplies, switches, operator interfaces, and the like.
  • the clamp 712 is operable to attach an end of a component part or strip 504 to the outer circumference of the mandrel 708 and against a molding surface 736.
  • the clamp 712 can include a jaw 728 and a releasable pressure mechanism 732 that can be operated to supply a force that clamps the end of the strip 504 between the jaw 728 and the outer circumference of the mandrel 708.
  • the pressure mechanism 732 can include a bolt or thumbscrew with a bearing surface that acts on the jaw 728, and threads that are received by a threaded hole formed in the mandrel 708.
  • the forming or molding surface 736 at or near the outer circumference of the mandrel 708 has a shape in the form (or the approximate form) of the surface at or near the inner circumference 408 of the annular composite structure 104.
  • the surface of the clamp 712 jaw 728 that bears on the strip 504 can have a shape in the form (or the approximate form) of the surface at or near the outer circumference 404 of the annular composite structure 104.
  • the molding surface 736 at or near the outer circumference of the mandrel 708 can include or be associated with a heater 738.
  • heating elements such as, but not limited to, electrical resistance heaters, conduits for heated fluids, or other mechanisms for providing heat to the molding surface 736, can be placed at or near the molding surface 736 of the mandrel 708.
  • a single or first strip 504a has a first surface that is held against the molding surface 736 at the outer circumference of the mandrel 708 by the jaw 728 of the clamp mechanism 712, which presses on a second surface of the strip 504a (e.g. as illustrated in Fig. 8A).
  • a subsequent or second strip 504b has a first surface that is held against the second surface of the first strip 504a by the jaw 728 of the clamp mechanism 712, which now presses on a second surface of the second strip 504b (e.g. as illustrated in Fig. 8C).
  • the first surface of the first strip 504a remains in position against the molding surface 736.
  • the clamp 712 used to secure the end of the first strip 504b may be the same as or different than the clamp 712 used to secure the end of subsequent strips 504.
  • a jaw 728 used to clamp the end of the first strip 504a can differ, for example in a size or contour of the contact surface of the jaw 728, from a jaw 728 used to clamp the end of a subsequent strip, for instance to accommodate dimensional differences resulting from the different number of layers.
  • the forming assembly 716 generally ensures that the first surface of the first strip 504a is in complete contact with the molding surface 736 of the mandrel 708.
  • the forming assembly 716 can be configured as a shoe or roller assembly that includes a forming surface 740 having a shape in the form (or the approximate form) of the surface at or near the outer circumference 404 of the annular composite structure 104. Like the molding surface 736 of the mandrel 708, the forming surface 740, can include or be associated with a heater 742. In addition, the forming assembly 716 can include or can be acted on by a press assembly 744. The press assembly 744 can be operated to selectively apply pressure to a portion of the strip 504 between the forming surface 740 of the forming assembly 716 and the molding surface 736 of the mandrel 708.
  • first surface of the first strip 504a is pressed against the molding surface 736 by the forming surface 740, which acts on the second surface of the first strip 504a (e.g. as illustrated in Fig. 8B).
  • a subsequent or second strip 504b has a first surface that is pressed against the second surface of the first strip 504a by the forming surface 740, which now presses on a second surface of the second strip 504b (e.g. as illustrated in Fig. 8D).
  • the first surface of the first strip 504a remains in position against the molding surface 736.
  • the forming surface 740 used with respect to the first strip 504a may be the same as or different than the forming surface 740 used with respect to subsequent strips 504.
  • a size or contour of the forming surface used with just the first strip 504a can be different than the forming surface 740 used with the first 504a and second 504b strips to accommodate dimensional differences resulting from the different number of layers.
  • the feed assembly 720 supports portions of the component part or strip 504 that are not held by the clamp 712 or that have not been pressed against the molding surface
  • the feed assembly 720 can include a number of clips or hangers that attach to and support the strip 504, and that are themselves supported and selectively moved by a chain running on a pair of sprockets.
  • the feed assembly 720 positions the component part 504 adjacent the preheating assembly 724, moves the component part 504 past the preheating assembly 724, and maintains tension on the component part 504 as the component part 504 is wound onto the mandrel 708.
  • the preheating assembly 724 can include a plurality of infrared heaters positioned on opposite sides of a strip 504 being carried by the feed assembly 720.
  • a first component part or strip 504a is being carried by the feed assembly 720, and has a first end fixed to the molding surface 736 of the mandrel 708 by a first clamp 712a.
  • the preheating assembly 724 by operating the preheating assembly 724 to warm the strip 504 to a processing temperature that is less than the melting point temperature of the thermoplastic material of the strip 504, the strip 504 can be made pliable.
  • Fig. 7B the mandrel 708 has been rotated in a clockwise direction (by about 45° in the figure), and the warmed component part 504 has been partially wound about the molding surface 736 of the mandrel 708.
  • the press assembly 744 has been operated to move the forming surface 740 of the forming assembly 716 into contact with the strip 504, and further to apply pressure to the strip 504. Additional heat can be applied to the portion of the strip 504 acted on by the forming assembly 716 by heaters in or associated with the forming assembly 716 and/or the mandrel 708.
  • the applied pressure in combination with the applied heat, causes the strip 504 to conform to the contours of the molding surface 736 of the mandrel 708 and the forming surface 740 of the forming assembly 716.
  • the process of rotating the mandrel 708, and forcing the strip 504 between the molding surface 736 in the forming surface 740 can continue until the first strip 504a is completely wound about the mandrel 708.
  • Fig. 7C the mandrel 708 is shown with the first strip 504a completely wound about the mandrel 708 such that the ends of the first strip 504a are adjacent one another, defining a seam 508.
  • the mandrel 708 is rotated in the clockwise direction by 270° relative to its position in Fig. 7A.
  • a first end of a second strip 504b is fixed to the mandrel 708 by a second clamp 712b.
  • the end of the second strip 504b is thus fixed to the mandrel 708 at a point that is offset by 90° from the point at which the end of the first strip 504a was fixed.
  • Fig. 7D the mandrel 708 has been rotated by a further 45° relative to its position in Fig. 7C, partially winding the second strip 504b about the mandrel 708.
  • the first surface of the second strip 504b in this example is being wound about the outer or second surface of the first strip 504a, which has itself been contoured by the molding 736 and forming 740 surfaces.
  • the forming assembly 716 has been operated to heat and press against the second surface of the second strip 504b, thereby forcing a portion of the second strip 504b between the first strip 504a, as contoured by the molding surface 736 of the mandrel 708, and the forming surface 740 of the forming assembly 716.
  • the first504a and second 504b strips are at least partially consolidated by the applied heat and pressure.
  • FIG. 9 An example sequence of operation of an example system 704 for manufacturing an annular composite structure 104, generally configured as illustrated in Figs. 7A-7D and 8A-8D, is depicted in Fig. 9.
  • a first end of a first strip 504a has been fixed to the mandrel 708 by the first clamp 712a.
  • the mandrel 708 is then rotated in a clockwise direction, in this example by 45 degrees, while tension is maintained on the strip 504a by the feed assembly 720.
  • a portion of the first strip 504a is then pressed between the molding surface 736 and the forming surface 740 by the forming assembly 716, as shown in C of Fig. 9.
  • the forming assembly 716 has again been moved away from the molding surface 736 of the mandrel 708, releasing the pressure on the first strip 504a, and the mandrel 708 has been still further rotated in a clockwise direction (here by 45 degrees).
  • a next portion of the first strip 504a is then pressed between the molding surface 736 and the forming surface 740 by the forming assembly 716, as shown in G of Fig. 9.
  • These processes continue until the first strip 504a has been completely wound about the mandrel 708 (see H and I of Fig. 9).
  • the length of the strips 504 are equal or about equal to the circumference of the annular composite structure 104, at least at the position of the individual strips 504 within the structure 104. Accordingly, when a strip 504 is completely wound about the mandrel, a seam 508 is formed between the ends of the strip 504.
  • the forming assembly 716 has been moved away from the molding surface 736 of the mandrel 708, and the mandrel 708 has been rotated in a counterclockwise direction (here by 135 degrees). More particularly, in this example, the mandrel 708 has been rotated in a counterclockwise direction by an amount that places a second clamp 712b in position to receive a first end of a second strip 504b. The second strip 504b is then attached to the second clamp 712b. In accordance with embodiments of the present disclosure, the rotation of the mandrel 708 places the seam 508 of the first strip 504a in a location different than the first end of the second strip 504b.
  • the seams 508 of the various strips 504 can be placed at different locations about the circumference of the annular composite structure 104.
  • the mandrel 708 is rotated in a counterclockwise direction to place the seam 508 of the first strip 504a in a location that will be overlaid by a portion in a first half of the second strip 504b, while minimizing the amount by which the mandrel 708 must be rotated.
  • the locations of the seams 508 can be offset from one another by, as examples, at least 10°, at least 45°, or at least 90°.
  • the process then proceeds, with the second strip 504b being placed or wound over the first strip 504a. This general process can then be continued until the required number of strips 504 have been wound about the mandrel 708.
  • the amounts by which the mandrel 708 is rotated in the various steps will depend at least in part in the relative dimensions of the components of the system 704 and the strips 504 applied in any particular implementation.
  • the forming assembly 716 when the forming assembly 716 is configured as a shoe type assembly, the forming surface 740 can be moved to simultaneously form some portion of the outer circumference of the annular structure 104.
  • the forming assembly 716 is configured as a roller assembly type assembly, the forming surface 740 can be engaged continuously, and the forming of the strip 504 can be performed as the mandrel 708 is rotated to draw the strip 504 between the molding surface 736 and the forming surface 740.
  • forming surface 740 of a forming assembly 716 configured as a roller assembly need not be withdrawn in order to rotate the mandrel 708, and can instead remain pressed against the second surface of the outer-most strip 504.
  • the forming assembly 716 can be changed, for example to present a forming surface 740 with a different contour, or can be repositioned, as additional strips 504 are added to the structure 104.
  • Fig. 10 is a flowchart illustrating aspects of a method for forming an annular composite structure 104 in accordance with embodiments of the present disclosure. Initially, at step 1004, a strip or component part 504 is formed.
  • Forming a strip 504 can include cutting the strip 504 from a larger sheet of fiber reinforced thermoplastic material. More particular, the length of a strip 504 can be sized such that it is equal to the circumference of the annular composite structure 104, at least at the intended location of that strip within the structure 104. In addition, the width of a strip 504 can be sized such to be about equal to the width of the annular composite structure after the strip has been formed into a final or approximately final shape. In accordance with other embodiments of the present disclosure, the length of a strip 504 can be less than or greater than the circumference of the annular composite structure, depending on different layup configurations.
  • the angle of the reinforcing fibers within a strip can be determined through the selection of the sheet of material from which a strip is cut, and/or from the way in which the strip 504 is cut from the larger sheet.
  • a strip 504 can include multiple layers 604 of fiber reinforced thermoplastic material.
  • a strip 504 can include multiple layers 604 of single or multiple layer fiber reinforced thermoplastic material.
  • one or more strips 504 can be supplied in a width and/or length that is suitable for inclusion in the annular composite structure 104 without any cutting.
  • a first end of a strip 504 is connected to the mandrel 708, for example provided as part of a system 704 as described herein.
  • This can include fixing the end of the strip 504 to the mandrel 708 using a clamp 712 carried by the mandrel 708.
  • the clamp 712 includes a jaw 728 that is contoured similarly to or the same as the forming surface 736 of the mandrel 708 and/or a contour of the annular composite structure 104 at a location occupied by the strip 504.
  • the strip 504 between the forming surface 736 of the mandrel 708 and the jaw 728.
  • the remainder of the strip 504 is then connected to the feed assembly 720 of the system 704 for manufacturing the annular composite structure 104 (step 1012).
  • Connecting the strip 504 to the feed assembly 720 can include clipping the strip to a chain or carrier along a longitudinal edge of the strip 504. Heating elements included in the preheating assembly
  • the preheating assembly 724 can then be activated (step 1016).
  • the preheating assembly 724 is operated to raise the temperature of a strip 504 carried by the feed assembly 720, thereby making the strip 504 more pliable.
  • heating elements in other components of the system 704 such as heating elements 738 incorporated into the mandrel 708, and heating elements 742 in or associated with a forming assembly 716, can be activated.
  • the mandrel 708 is rotated, thereby drawing the strip 504 around a portion of the outer circumference of the mandrel 708.
  • the feed assembly 720 maintains tension on the strip 504 as it is drawn around the mandrel 708, promoting tight engagement of the strip 504 with the molding surface 736 of the mandrel 708.
  • the forming assembly 716 is operated to press a portion of the strip 504 against the molding surface 736 of the mandrel 708 (step 1024).
  • the shoe assembly 716 is moved towards the molding surface 736 to apply pressure between the molding surface 736 and the forming surface 740 of the shoe assembly 716, and is then retracted to facilitate a subsequent rotation step or other step of the process.
  • the forming assembly 716 can be configured to continuously apply pressure as the strip 504 is drawn onto the mandrel 708.
  • the molding surface 736, the forming surface 740, or both the molding 736 and forming 740 surfaces can be heated (for example using heating elements 738 and 742) to raise the temperature of the strip 504 to at or less than the melting temperature of the thermoplastic material of the strip 504, making the strip 504 more pliable and thereby helping to ensure conformance of the strip 504 to the contours of the molding 736 and the forming 740 surfaces.
  • the heat and pressure applied by the forming assembly 716 can fuse or otherwise consolidate the strips 504 or strip 504 portions.
  • the mandrel 708 is rotated (step 1036).
  • rotating the mandrel 708 allows an end or the ends of the previously wound strip 504 to be adjacent an intermediate portion of the next strip 504, rather than an end of the next strip 504. That is, the locations of the ends of the strips 504 forming component parts of the annular composite structure 104 can be placed at different locations about the circumference of the structure 104.
  • the rotation of the mandrel 708 at step 1036 is in a direction opposite the direction used to wind the strips 504 about the mandrel 708.
  • Moving the mandrel 708 in the opposite direction to that used to wind the previous strip or strips 504 about the mandrel can reduce the amount of rotation required to place the seam of the previously applied strip 504 under a portion of the next strip 504.
  • the process can then return to step 1004, and a next strip for inclusion in the structure 104 can be formed (or selected from a set of previously formed strips 504).
  • a strip 504 can be the same or different than a previously wound strip 504 in its configuration, including in the number of layers and/or the orientation of reinforcing layers, or in its overall dimensions.
  • the process of winding, forming, and fusing can then continue until all of the strips 504 have been incorporated into the structure 104.
  • the strips 504 that have been wound about the mandrel 708 can be placed in a final mold and fused to one another (step 1040).
  • Final molding and fusing the strips or component parts 504 can include placing a multipart external mold over the strips 504, while the strips 504 remain in place against the forming surface 736 of the mandrel 708, and applying heat and pressure, forming a fused or integral annular composite structure 104.
  • fusing of the layers, whether those layers are formed from the same or different strips 504, can be performed simultaneously with the step winding of the strips 504 about the mandrel 708 under heat and pressure as described herein. In such embodiments, a final molding and fusing step can be eliminated.
  • the structure 104 can then be removed from the mold parts and/or mandrel, and final finishing steps can be performed (step 1044).
  • the final finishing steps can include drilling spoke holes and a valve hole, removing flash, adding labels and graphics, and the like.
  • the process of forming the annular composite structure 104 is then complete.
  • a strip 504 can have a length that is greater than the circumference of the annular composite structure 104.
  • a structure 104 can be formed from strips 504 that each have a length that is less than a circumference of the completed structure 104.
  • strips 504 having different lengths 504, widths, number and configuration of layers 604, or other differences can be incorporated into a composite structure 104.
  • a component part or strip 504 can be formed from one or more layers 604 of thermoplastic fiber reinforced material.
  • a layer 604 used to form a strip 504 can itself be formed from a piece of material having multiple layers or plies of reinforcing materials impregnated with a thermoplastic material.
  • a layer 604 can include a layer of unidirectional reinforcing fibers that are non-parallel to the sides of the strip 504, and a layer with a relatively sparse number of reinforcing fibers that are generally parallel to the sides of the strip 504.
  • Such a configuration provides a strip 504 that can withstand a relatively large amount of tension while it is wound about the mandrel 708, while at the same time allowing fibers oriented generally transverse to a plane of the structure 104 to be incorporated into that structure 104.
  • the technology encompasses:
  • An annular composite structure comprising: a first component part, wherein the first component part includes at least one layer of a fiber reinforced thermoplastic material, and wherein the first component part extends about at least a first portion of a circumference of the structure; and a second component part, wherein the second component part includes at least one layer of the fiber reinforced thermoplastic material, wherein the second component part extends about at least a second portion of the circumference of the structure, and wherein the first component part is fused to the second component part.
  • each component part includes multiple layers of the fiber reinforced thermoplastic material.
  • annular composite structure of any of (1) to (7) further comprising: a third component part, wherein the third component part includes at least one layer of a fiber reinforced thermoplastic material, and wherein the third component part extends about a portion of the circumference of the structure; and a fourth component part, wherein the fourth component part includes at least one layer of the fiber reinforced thermoplastic material, and wherein the fourth component part extends about a portion of the circumference of the structure, wherein the first component part extends about a portion of the circumference of the structure, wherein the second component part extends about a portion of the circumference of the structure, and wherein the first, second, third, and fourth component parts are fused to one another.
  • the technology encompasses:
  • a method of forming an annular composite structure comprising: winding a first strip of fiber reinforced thermoplastic material about a mandrel, wherein at least a portion of the first strip is in contact with a molding surface of the mandrel, and wherein a first end of the first strip is at a first location about the circumference of the mandrel; and winding a second strip of fiber reinforced thermoplastic material about the mandrel, wherein at least a portion of the first strip is between the second strip and the molding surface of the mandrel, and wherein a first end of the second strip is at a second location about the circumference of the mandrel.
  • the technology encompasses:
  • a system comprising: a mandrel, wherein the mandrel includes an outer circumference with a molding surface formed therein; a first clamp assembly; and a forming assembly, wherein the forming assembly includes a forming surface, wherein a first end of a first fiber reinforced thermoplastic component part is fixed to the mandrel by the first clamp assembly, and wherein a portion of the first fiber reinforced thermoplastic component part is pressed between the molding surface and the forming surface.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

La présente invention concerne des structures annulaires (104) formées en utilisant des matériaux composites et des systèmes et des procédés de formation de structures annulaires utilisant des matériaux composites. Les matériaux composites peuvent comprendre des matériaux thermoplastiques renforcés de fibres. Les structures annulaires comprennent de nombreuses pièces constitutives. Chaque pièce constitutive peut se présenter sous la forme d'une bande de matériau thermoplastique renforcé de fibres (504) qui s'étend autour de tout ou d'une portion d'une circonférence de la structure. Les extrémités (508) des pièces constitutives peuvent être étagées, de sorte qu'elles sont placées à différents emplacements autour de la circonférence de la structure. Des procédés de formation de structures composites annulaires comprennent l'enveloppement d'une ou plusieurs bandes de matériau thermoplastique renforcé de fibres ayant une ou plusieurs couches autour d'un mandrin, et la fusion des bandes pour former une structure annulaire intégrale.
PCT/US2022/030197 2021-05-20 2022-05-20 Structures annulaires formées de matériaux composites et systèmes et procédés de formation de structures annulaires à partir de matériaux composites WO2022246160A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP22736409.8A EP4132774A1 (fr) 2021-05-20 2022-05-20 Structures annulaires formées de matériaux composites et systèmes et procédés de formation de structures annulaires à partir de matériaux composites

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US202163191238P 2021-05-20 2021-05-20
US63/191,238 2021-05-20
US17/748,965 2022-05-19
US17/748,965 US20220371260A1 (en) 2021-05-20 2022-05-19 Annular structures formed from composite materials and systems and methods for forming annular structures from composite materials

Publications (1)

Publication Number Publication Date
WO2022246160A1 true WO2022246160A1 (fr) 2022-11-24

Family

ID=82361210

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2022/030197 WO2022246160A1 (fr) 2021-05-20 2022-05-20 Structures annulaires formées de matériaux composites et systèmes et procédés de formation de structures annulaires à partir de matériaux composites

Country Status (1)

Country Link
WO (1) WO2022246160A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023083841A1 (fr) * 2021-11-09 2023-05-19 Safran Aircraft Engines Procédé d'injection de résine et dispositif de maintien d'une texture fibreuse sur un mandrin d'imprégnation d'une machine d'enroulement

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004074010A2 (fr) * 2003-02-14 2004-09-02 Trek Bicycle Corporation Jante de roue de bicyclette composite legere presentant une bonne performance de freinage
EP1506882A1 (fr) * 2003-08-11 2005-02-16 Campagnolo Srl Jante composite de bicyclette et procédé de sa fabrication
DE102008028441A1 (de) * 2008-06-17 2009-12-31 Eads Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung eines ringförmigen Vorformlings aus Fasermaterialhalbzeug, sowie Verwendung derartiger Verfahren und Vorrichtungen
US20120264536A1 (en) * 2011-04-18 2012-10-18 Tatsuya Yashiki Golf club shaft

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004074010A2 (fr) * 2003-02-14 2004-09-02 Trek Bicycle Corporation Jante de roue de bicyclette composite legere presentant une bonne performance de freinage
EP1506882A1 (fr) * 2003-08-11 2005-02-16 Campagnolo Srl Jante composite de bicyclette et procédé de sa fabrication
DE102008028441A1 (de) * 2008-06-17 2009-12-31 Eads Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung eines ringförmigen Vorformlings aus Fasermaterialhalbzeug, sowie Verwendung derartiger Verfahren und Vorrichtungen
US20120264536A1 (en) * 2011-04-18 2012-10-18 Tatsuya Yashiki Golf club shaft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023083841A1 (fr) * 2021-11-09 2023-05-19 Safran Aircraft Engines Procédé d'injection de résine et dispositif de maintien d'une texture fibreuse sur un mandrin d'imprégnation d'une machine d'enroulement

Similar Documents

Publication Publication Date Title
EP1328409B1 (fr) Jante composite
US7513769B2 (en) Apparatus and methods for forming composite stiffeners and reinforcing structures
US6306235B1 (en) Spiral formed products and method of manufacture
US6524515B1 (en) Method of producing a vehicle steering wheel
US20080265657A1 (en) Method and apparatus for producing a rim
US8784592B2 (en) Method for manufacturing a core composite provided with cover layers on both sides
US20060073309A1 (en) Method for laying composite tape
US20020011047A1 (en) Contoured crushable composite structural members and methods for making the same
JPH09201908A (ja) 合成複合構造を形成するための方法
KR20120029438A (ko) 복합섬유 자전거 휠
KR20200043420A (ko) 복합 휠의 림 섬유 아키텍처
WO2022246160A1 (fr) Structures annulaires formées de matériaux composites et systèmes et procédés de formation de structures annulaires à partir de matériaux composites
US11142020B2 (en) Reinforced thermoplastic components and method of manufacture thereof
TW200900270A (en) Wheel, rim, and method of manufacturing a wheel
US20110014429A1 (en) Composite Member Defining a Contour Surface
EP2602082B1 (fr) Appareil et procédé de formation d'un composant creux
US20220371260A1 (en) Annular structures formed from composite materials and systems and methods for forming annular structures from composite materials
US20120000597A1 (en) Method of manufacturing composite parts
AU4987293A (en) Structural and other components, method of manufacture
US4878976A (en) Method for continuously manufacturing synthetic resin tube
KR101865775B1 (ko) 소재 성형장치
US5470414A (en) Method of making flat stock having a bearing surface and the flat stock made thereby
WO2006022788A1 (fr) Procede de formation d’un renfort pour roue elastique et renfort pour roue elastique
US20040227268A1 (en) Method of deforming a workpiece
JPH03166937A (ja) 軸状複合部材およびその製造方法

Legal Events

Date Code Title Description
ENP Entry into the national phase

Ref document number: 2022736409

Country of ref document: EP

Effective date: 20221110

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 22736409

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE