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US20230250628A1 - Hub and strut in a reticulated frame - Google Patents

Hub and strut in a reticulated frame Download PDF

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Publication number
US20230250628A1
US20230250628A1 US17/665,155 US202217665155A US2023250628A1 US 20230250628 A1 US20230250628 A1 US 20230250628A1 US 202217665155 A US202217665155 A US 202217665155A US 2023250628 A1 US2023250628 A1 US 2023250628A1
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Prior art keywords
hub
struts
joints
hubs
frame structure
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Abandoned
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US17/665,155
Inventor
Alexis Rochas
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Oasys Technologies Inc
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Oasys Technologies Inc
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Priority to US17/665,155 priority Critical patent/US20230250628A1/en
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Abandoned legal-status Critical Current

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    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/38Connections for building structures in general
    • E04B1/58Connections for building structures in general of bar-shaped building elements
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B1/1903Connecting nodes specially adapted therefor
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B1/1903Connecting nodes specially adapted therefor
    • E04B2001/1921Connecting nodes specially adapted therefor with connecting nodes having radial connecting stubs
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B2001/1924Struts specially adapted therefor
    • E04B2001/1927Struts specially adapted therefor of essentially circular cross section
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B2001/1957Details of connections between nodes and struts
    • E04B2001/196Screw connections with axis parallel to the main axis of the strut
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/38Connections for building structures in general
    • E04B1/58Connections for building structures in general of bar-shaped building elements
    • E04B2001/5887Connections for building structures in general of bar-shaped building elements using connectors with sockets

Definitions

  • the field of this invention relates to reticulated frame structures and space frames, and particularly to a novel hub capable of joining structural frame elements of such structures.
  • a reticulated frame is often referred to as a space frame because it is capable of covering large spaces with little interior support. It is typically a lightweight rigid structure having interlocking struts connected to hubs in a geometric pattern similar to a bridge truss. Like the well-known truss, such frames are strong because of the inherent rigidity of triangular beam arrangements where flexing loads and bending moments are transmitted as tension and compression vectors along the length of the beams. Such frames are common in building construction such as large roof spans in modern commercial and industrial buildings. Notable examples are the Stansted airport terminal in London, the Bank of China Tower, the Louvre Museum Pyramid, the Rogers Centre in Toronto, Ontario, and McCormick Place Lakeside Center in Chicago, Ill., USA.
  • the prior art does not teach a frame structure whereby frame elements converge to transfer loads to and from a common point at a hub thereby avoiding rotational moments in the hub.
  • the invention teaches structure and methods whereby beam loads are transferred axially to hubs. This approach is beneficial in its ability to enable a direct load transfer between load bearing members mutually terminated within a common hub.
  • the presently described hub is an essential joining element in the construction and operation of frames of the type described and shown.
  • the hub is a one piece monolithic element functional as a node within a frame structure.
  • a hub may be a terminal point within a frame structure, or it may join two or more struts of the frame.
  • the longitudinal axes of all struts which are joined to a single common hub pass through a common point. This avoids the possibility of force moments on, or within, the hub, important for passing tensile and compressive forces along the frame without unwanted stress being applied to the frame and without generating bending or shear forces on the struts or hubs.
  • the axis of each strut is coaxial with a radius of a theoretical sphere of the hub body and may be selectively positioned within a range of angular positions all the while remaining co-radial with the theoretical sphere. Of course, this accounts for the benefit described in the preceding.
  • each of the fasteners may have a threaded stud or a threaded entry and may be rotatable about its radially aligned axis thereby providing a simple and quick means for securely attaching one end of a strut to the fastener wherein the strut may be adapted for threadedly engaging the fastener.
  • each one of the hubs may be rotatable enabling any position within a solid angle having a cone outer surface defined by the angular range of the possible extreme positions of the fastener.
  • FIG. 1 is a perspective view of a frame structure of the invention
  • FIG. 3 is a perspective view of the hub of FIG. 2 ;
  • FIG. 4 is an elevation view thereof
  • FIG. 5 is a further elevation view thereof
  • FIG. 6 is an expanded partial section view of a strut-connector-hub of the invention.
  • FIG. 7 illustrates FIG. 6 with strut-connector-hub joined
  • FIG. 8 is a perspective view of a hub interconnected with struts of the invention.
  • a frame structure (frame 5 ) is shown in FIG. 1 and comprises a plurality of struts 50 engaged with a plurality of hubs 10 making up a structure which may be quite large and may have a desired overall shape or appearance.
  • frame 5 may have panels and similar structure attached and incorporated therewith forming walls, floors and other useful building features.
  • the designer or architect of frame 5 will consider the topography of the surface on which frame 5 is to be supported as well as loads due to wind and other natural forces including potential surface movements, and also bearing loads, and stress and strain factors within frame 5 due to its own weight and to possible loads and external forces. These considerations are well-known in structural engineering practice and can be calculated using standard methods.
  • hubs 10 within frame 5 are the elements to which all struts 50 attach and are therefore the “glue” which holds frame 5 together in its desired configuration.
  • Struts 50 may be made of metal, polymer materials, resins, nanotubes, fiber reinforced composites, and other engineering materials and may be solid beams or hollow with circular, rectangular or other cross sectional shapes; see FIG. 8 .
  • Each of the two opposite ends 52 of each strut 50 may be engaged with a hub joint 10 A, 10 B, or 10 C which are best shown in FIGS. 2 through 5 .
  • hub joints shall be designated by “ 10 x ” which shall mean one or more than one such hub joints.
  • Each one of hubs 10 comprises a monolithic body with at least two, but possibly more than two, integral hub joints 10 x .
  • hubs 10 be able to accommodate (receive and connect with) struts 50 arriving from a wide range of directions. This permits the total number of components (struts, hubs) to be minimized, thus minimizing costs. This, in turn, requires that hub joints 10 x have the largest number and greatest range of possible angular positions on hubs 10 .
  • length L as shown in FIG.
  • each one of hub joints 10 x is adapted, in a manner to be described, for engaging an end 52 of one of struts 50 as shown in FIGS. 6 and 7 .
  • Axes of each one of hub joints 10 x mutually converge on a common point 14 as shown in FIG. 2 .
  • hub joints 10 x are preferably positioned such that axes 12 all converge on common point 14 . Therefore, force moments on hubs 10 are avoided which assures that hubs 10 do not tend to rotate which could damage the components as well as frame 5 itself.
  • At least one of hub joints 10 x may be a tubular projection of the monolithic body of hub 10 .
  • Struts 50 may be of disparate sizes and hub joints 10 x may likewise be of disparate sizes corresponding to the sizes of struts 50 , see, for instance, FIG. 2 .
  • Hubs 10 are preferably fabricated by 3D printing methods and may be made of hard polymers or metals. They can also be produced by processes such as molding, machining and stamping. Struts 50 may be linear in form with two opposing ends 52 wherein each of these ends 52 may be joined with one of hub joints 10 x by a tubular sleeve 20 as shown in FIGS. 6 and 7 .
  • tubular sleeves 20 may be fastened to one of hub joints 10 x by an axially oriented fastener such as bolt 30 and to strut 50 by a transaxially oriented fastener 40 and nut 42 .
  • an axially oriented fastener such as bolt 30
  • strut 50 by a transaxially oriented fastener 40 and nut 42 .
  • a method of producing frame 5 may include engaging a plurality of struts 50 with a plurality of hubs 10 in a manner shown in FIGS. 6 and 7 .
  • each of hubs 10 may be a monolithic body having plural hub joints 10 x and adapting each one of hub joints 10 x for engaging an end 52 of one of struts 50 by using a tubular sleeve 20 .
  • Hub joints 10 x may be positioned so that axes 12 are mutually convergent on point 14 as shown in FIG. 2 .
  • the method may include producing hub joints 10 x as tubular projections integral to the monolithic body of hub 10 .
  • the struts 50 of frame 5 may be produced in sizes, of materials, and of cross-sectional design as required by their load carrying functions.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

A plurality of hubs are joined to frame struts thereby forming a space frame structure, wherein the hubs have monolithic bodies with protruding joints adapted for receiving and joining with the frame struts using tubular sleeves. Axes of the joints are aligned to converge at a common point to avoid rotational moment forces on the hubs. The hubs are preferably fabricated by a 3D printing method in a structural material. In a method of the invention, the struts, joint diameters and joint lengths are sized and positioned to avoid interference between adjacent struts.

Description

    PRIOR PATENT INFORMATION RELATIVE TO THE INVENTION
  • Application 61/503,323 filed Jun. 30, 2011; application Ser. No. 13/540,449 filed Jul. 2, 2012 and issued as U.S. Pat. No. 8,820,025B1 on Sep. 2, 2014. The prior patent discloses a similar invention to that which is disclosed herein. The inventor is common to both.
  • FIELD OF THE DISCLOSURE OF THE INVENTION
  • The field of this invention relates to reticulated frame structures and space frames, and particularly to a novel hub capable of joining structural frame elements of such structures.
  • BACKGROUND AND PRIOR ART OF THE INVENTION
  • A reticulated frame is often referred to as a space frame because it is capable of covering large spaces with little interior support. It is typically a lightweight rigid structure having interlocking struts connected to hubs in a geometric pattern similar to a bridge truss. Like the well-known truss, such frames are strong because of the inherent rigidity of triangular beam arrangements where flexing loads and bending moments are transmitted as tension and compression vectors along the length of the beams. Such frames are common in building construction such as large roof spans in modern commercial and industrial buildings. Notable examples are the Stansted airport terminal in London, the Bank of China Tower, the Louvre Museum Pyramid, the Rogers Centre in Toronto, Ontario, and McCormick Place Lakeside Center in Chicago, Ill., USA. Large portable stages and lighting gantries are frequently built from such frames with octet trusses which are the structures of choice for holding signs above roads and in stadiums. The following documents have cited my prior patent U.S. Pat. No. 8,820,025B1 and are considered prior art in this application: US20150059263A1 and US9212479B1 to Devrim Pacaci, entitled “Supporting Framework Having Connection Hubs;” US20-150101645A1 to Garden Right, LLC, entitled “Dome Flubs, Dome Assembly Kits, and Dome Assembly Methods” CN106592762A to
    Figure US20230250628A1-20230810-P00001
    entitled Space assembling type bolt-column joint;“. CN106760235A to
    Figure US20230250628A1-20230810-P00002
    Figure US20230250628A1-20230810-P00003
    Figure US20230250628A1-20230810-P00004
    entitled Kind Of Multidirectional Adjustable Curved Surface Lighting Roof Grid System;” US20170167516A1 to Paul H. Mason, entitled “Strut Connector;”. US9731773B2 to Caterpillar Inc. entitled “-Node For A Space Frame;”. DE102016010883A1 to Technische Universitätm Chemnitz Variable, entitled “Connection Element,” CN110578370A to
    Figure US20230250628A1-20230810-P00005
    Figure US20230250628A1-20230810-P00006
    entitled “Bolt Ball For Steel Structure Connection;”. US20200109549A1 to Manuel Fernando and Bethencourt Cravid entitled “Lattice Structure”; and CNI 11042318A to
    Figure US20230250628A1-20230810-P00007
    , entitled “Single-Layer Aluminum Alloy Latticed Shell Box Type Modular Assembly Joint And Construction Process Thereof.”
  • SUMMARY OF THE INVENTION
  • It should be recognized that the prior art does not teach a frame structure whereby frame elements converge to transfer loads to and from a common point at a hub thereby avoiding rotational moments in the hub. The invention teaches structure and methods whereby beam loads are transferred axially to hubs. This approach is beneficial in its ability to enable a direct load transfer between load bearing members mutually terminated within a common hub. The presently described hub is an essential joining element in the construction and operation of frames of the type described and shown. Uniquely, the hub is a one piece monolithic element functional as a node within a frame structure. In practice, a hub may be a terminal point within a frame structure, or it may join two or more struts of the frame. In one aspect of the presently described apparatus, the longitudinal axes of all struts which are joined to a single common hub pass through a common point. This avoids the possibility of force moments on, or within, the hub, important for passing tensile and compressive forces along the frame without unwanted stress being applied to the frame and without generating bending or shear forces on the struts or hubs. In another aspect of the invention, the axis of each strut is coaxial with a radius of a theoretical sphere of the hub body and may be selectively positioned within a range of angular positions all the while remaining co-radial with the theoretical sphere. Of course, this accounts for the benefit described in the preceding. In another aspect of the invention, the angular range of positions of each one of the struts relative to their connected hubs may be between 45° and 90°. In another aspect of the invention, each of the fasteners may have a threaded stud or a threaded entry and may be rotatable about its radially aligned axis thereby providing a simple and quick means for securely attaching one end of a strut to the fastener wherein the strut may be adapted for threadedly engaging the fastener. In another aspect of the invention, each one of the hubs may be rotatable enabling any position within a solid angle having a cone outer surface defined by the angular range of the possible extreme positions of the fastener. The details of one or more embodiments of these concepts are set forth herein and other features, objects, and advantages of these concepts will be apparent to those of skill in the art from this writing and drawings, and from the claims.
  • DESCRIPTION OF THE DRAWINGS OF THE INVENTION
  • Embodiments of the invention are illustrated only as examples in the drawing figures accompanying this written description. Alpha-numerical call-outs are used to identify elements of the invention, wherein the same call-out refers to the same element as it may appear in various views of the figures.
  • FIG. 1 is a perspective view of a frame structure of the invention;
  • FIG. 2 is a section view of a hub thereof;
  • FIG. 3 is a perspective view of the hub of FIG. 2 ;
  • FIG. 4 is an elevation view thereof;
  • FIG. 5 is a further elevation view thereof;
  • FIG. 6 is an expanded partial section view of a strut-connector-hub of the invention;
  • FIG. 7 illustrates FIG. 6 with strut-connector-hub joined; and
  • FIG. 8 is a perspective view of a hub interconnected with struts of the invention.
  • DETAILED DESCRIPTION OF THE INVENTION
  • In an embodiment of the invention, a frame structure (frame 5) is shown in FIG. 1 and comprises a plurality of struts 50 engaged with a plurality of hubs 10 making up a structure which may be quite large and may have a desired overall shape or appearance. Although not described here, frame 5 may have panels and similar structure attached and incorporated therewith forming walls, floors and other useful building features. The designer or architect of frame 5 will consider the topography of the surface on which frame 5 is to be supported as well as loads due to wind and other natural forces including potential surface movements, and also bearing loads, and stress and strain factors within frame 5 due to its own weight and to possible loads and external forces. These considerations are well-known in structural engineering practice and can be calculated using standard methods. As will be understood, hubs 10 within frame 5 are the elements to which all struts 50 attach and are therefore the “glue” which holds frame 5 together in its desired configuration. Struts 50 may be made of metal, polymer materials, resins, nanotubes, fiber reinforced composites, and other engineering materials and may be solid beams or hollow with circular, rectangular or other cross sectional shapes; see FIG. 8 . Each of the two opposite ends 52 of each strut 50 may be engaged with a hub joint 10A, 10B, or 10C which are best shown in FIGS. 2 through 5 . In this description further reference to hub joints shall be designated by “10 x” which shall mean one or more than one such hub joints. Each one of hubs 10 comprises a monolithic body with at least two, but possibly more than two, integral hub joints 10 x. In order to provide maximum flexibility in placement of struts 50 within frame 5, it is desirable that hubs 10 be able to accommodate (receive and connect with) struts 50 arriving from a wide range of directions. This permits the total number of components (struts, hubs) to be minimized, thus minimizing costs. This, in turn, requires that hub joints 10 x have the largest number and greatest range of possible angular positions on hubs 10. In order to accommodate struts 50 that are near or adjacent to one another at any hub 10, it is necessary to use length L, as shown in FIG. 2 , as a design parameter and as a means of providing strut-to-strut clearance at any given hub 10. Further, it should be understood that by using a minimum possible length L for all hub joints 10 x, hub manufacturing time and material usage, and overall weight and cost of frame 5 are minimized. This can be of significant commercial benefit. Now, referring to FIGS. 2-5 , we see in FIG. 2 that in hub 10 the direction of each hub joint 10 x is defined by its vector 12. That being the case, then it is obvious that each two adjacent vectors 12 define a plane in 3-space and if the sizes of struts 50, hardware elements 40, 42 and sleeve 20 (see FIGS. 6 and 7 ) are known, the minimal length L to afford clearance between adjacent struts 50 may be determined by graphical or algebraic methods in order to assure adjacency clearance. Each one of hub joints 10 x is adapted, in a manner to be described, for engaging an end 52 of one of struts 50 as shown in FIGS. 6 and 7 . Axes of each one of hub joints 10 x mutually converge on a common point 14 as shown in FIG. 2 . With respect to each hub 10, its hub joints 10 x are preferably positioned such that axes 12 all converge on common point 14. Therefore, force moments on hubs 10 are avoided which assures that hubs 10 do not tend to rotate which could damage the components as well as frame 5 itself. At least one of hub joints 10 x may be a tubular projection of the monolithic body of hub 10. Struts 50 may be of disparate sizes and hub joints 10 x may likewise be of disparate sizes corresponding to the sizes of struts 50, see, for instance, FIG. 2 . Hubs 10 are preferably fabricated by 3D printing methods and may be made of hard polymers or metals. They can also be produced by processes such as molding, machining and stamping. Struts 50 may be linear in form with two opposing ends 52 wherein each of these ends 52 may be joined with one of hub joints 10 x by a tubular sleeve 20 as shown in FIGS. 6 and 7 . As shown tubular sleeves 20 may be fastened to one of hub joints 10 x by an axially oriented fastener such as bolt 30 and to strut 50 by a transaxially oriented fastener 40 and nut 42. This is considered to be a novel arrangement but it will be possible for those of skill in the mechanical arts to arrange different attachment schemes. In an embodiment of the invention, a method of producing frame 5 may include engaging a plurality of struts 50 with a plurality of hubs 10 in a manner shown in FIGS. 6 and 7 . This may involve forming each of hubs 10 as a monolithic body having plural hub joints 10 x and adapting each one of hub joints 10 x for engaging an end 52 of one of struts 50 by using a tubular sleeve 20. Hub joints 10 x may be positioned so that axes 12 are mutually convergent on point 14 as shown in FIG. 2 . The method may include producing hub joints 10 x as tubular projections integral to the monolithic body of hub 10. The struts 50 of frame 5 may be produced in sizes, of materials, and of cross-sectional design as required by their load carrying functions.
  • Embodiments of the subject apparatus and method of this invention have been described herein. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and understanding of this disclosure. Accordingly, other embodiments and approaches are within the scope of the following claims.

Claims (19)

What is claimed is:
1. A frame structure comprising:
a plurality of struts engaged with a plurality of hubs;
each of said hubs comprising a monolithic body with at least two integral hub joints integrally formed with said monolithic body; wherein each one of said hub joints is adapted for engaging an end of one of said struts; and wherein axes of said hub joints mutually converge.
2. The frame structure of claim 1 wherein at least one of said hub joints is an integral tubular projection extensive from said monolithic body.
3. The frame structure of claim 1 wherein said struts are of disparate sizes.
4. The frame structure of claim 3 wherein said hub joints are of disparate sizes corresponding to said disparate sizes of said struts.
5. The frame structure of claim 1 wherein at least one of said hubs is a product of a 3D printing method.
6. The frame structure of claim 1 wherein said end of said one of said struts is joined with one of said hub joints by a tubular sleeve.
7. The frame structure of claim 6 wherein said tubular sleeve is fastened to said one of said hub joints by an axially oriented fastener and to said strut by a transaxially oriented fastener.
8. A hub for integration into a frame structure said hub comprising:
a monolithic body with at least two integral hub joints;
wherein each one of said hub joints is adapted for engaging an end of a strut of said frame structure;
and wherein axes of said hub joints mutually converge.
9. The hub of claim 8 Wherein at least one of said hub joints is a tubular projection relative to said monolithic body.
10. The hub of claim 9 wherein said hub joints are of disparate sizes.
11. The hub of claim 10 wherein said hub is a product of a 3D printing method.
12. A method of producing a frame structure wherein said method comprises:
engaging a plurality of struts with a plurality of hubs;
forming each one of said hubs into a monolithic body having at least two integral hub joints;
adapting each one of said hub joints for engaging an end of one of said struts; and
positioning said hub joints wherein axes of said hub joints mutually converge.
13. The method of claim 12 wherein said hub joints are produced as tubular projections of said monolithic body and said tubular projections are minimized in length.
14. The method of claim 13 wherein said struts are produced with disparate sizes.
15. The method of claim 14 wherein said hub joints are produced with disparate sizes corresponding to said disparate sizes of said struts.
16. The method of claim 12 wherein at least one of said hubs is produced by a 3D printing method.
17. The method of claim 12 wherein a tubular sleeve is positioned for joining said end of said one of said struts with said one of said hub joints.
18. The method of claim 17 wherein an axially oriented fastener is positioned for joining said tubular sleeve to said one of said hub joints.
19. The method of claim 17 wherein a transaxially oriented fastener is positioned for joining said tubular sleeve to said one of said struts.
US17/665,155 2022-02-04 2022-02-04 Hub and strut in a reticulated frame Abandoned US20230250628A1 (en)

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