US20030226319A1 - Geodesic dome assemby joint - Google Patents

Geodesic dome assemby joint Download PDF

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Publication number
US20030226319A1
US20030226319A1 US10/163,906 US16390602A US2003226319A1 US 20030226319 A1 US20030226319 A1 US 20030226319A1 US 16390602 A US16390602 A US 16390602A US 2003226319 A1 US2003226319 A1 US 2003226319A1
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Prior art keywords
tubes
joint
struts
washers
assembly
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US10/163,906
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Ashton Richards
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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
    • E04B1/32Arched structures; Vaulted structures; Folded structures
    • E04B1/3211Structures with a vertical rotation axis or the like, e.g. semi-spherical 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
    • 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
    • E04B2001/193Struts specially adapted therefor of essentially circular cross section with flattened connecting parts, e.g. ends
    • 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
    • E04B2001/1963Screw connections with axis at an angle, e.g. perpendicular, 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
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B2001/1957Details of connections between nodes and struts
    • E04B2001/1966Formlocking connections other than screw connections
    • 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
    • E04B1/32Arched structures; Vaulted structures; Folded structures
    • E04B2001/3235Arched structures; Vaulted structures; Folded structures having a grid frame
    • E04B2001/3241Frame connection details
    • E04B2001/3247Nodes
    • 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
    • E04B1/32Arched structures; Vaulted structures; Folded structures
    • E04B2001/3294Arched structures; Vaulted structures; Folded structures with a faceted surface

Definitions

  • This invention relates to geodesic dome and space frame structure joint and assembly systems.
  • Tubular elements or pipes have advantages over other structural forms because of the load-transmitting qualities inherent in their circular cross section and their efficient strength-weight ratio.
  • the failure to employ them extensively in geodesic domes and trusses and truss-like structures was due to the lack of suitable connectors or coupling members for easily and efficiently joining their ends.
  • a current disadvantage of many geodesic domes and space frame structures presently in use is the high cost of connectors used to interconnect chord and strut members at each node and the high labor cost associated with the assembly of complicated structural systems.
  • the prior art A. E. Fentiman U.S. Pat. No. 2,964,147, Dec. 13, 1960 is a patent where the ends of tubes have been flattened in order to form a plane that can be received by a slotted connector.
  • the flattened ends of the tubes are sandwiched inside the slot and held in place by a bolt that passes simultaneously through the hole in the slotted connector and the holes in the individual flattened portion of the angled tubes sandwiched to the top of the slotted connector.
  • the prior art Fentiman U.S. Pat. No. 2,931,467 utilizes a similar system of flattened tube ends having their movement restricted by a slotted connector. Again, the design has only a few components uses only one bolt as a fastener but looses a portion or this cost advantage in the manufacturing of the a unique non pre-existing slotted connector.
  • FIGS. 1 , 2 , 5 , 6 are designs where the ends of tubes have been flattened in order to form planes that are sandwiched together by numerous bolts.
  • the design gains a cost advantage by using pre-existing components in conjunction with modified pre-existing components but looses much of this advantage as a result of the numerous bolts that add material cost and labor cost during assembly.
  • This invention relates to a joint for connecting the ends of tubes for the purpose of assembling a geodesic dome or truss structure.
  • the tube ends are modified to form top and bottom hooks which face away from each other.
  • the hooked ends facilitate the attachment of the tubes to one another by loosely gripping a common top and bottom washer.
  • the inner washers are used as tension rings for restricting the movement of the tubes.
  • To stiffen the structure the hooks are pressed down into flattened position by the outer top and bottom washers that are sandwiched by a single nut and bolt assembly
  • the invention uses tubular elements or pipes which have advantages over other structural forms because of the load-transmitting qualities inherent in their circular cross section and their efficient strength-weight ratio.
  • the failure to employ them extensively in geodesic domes and truss-like structures was due to the lack of suitable connectors or coupling members for easily and efficiently joining their ends.
  • the advantage of the invention is that it reduces the cost of geodesic domes and space frame structures by reducing the material and fabrication cost of connectors used to attach strut members at each node.
  • a further advantage of the invention is the reduction of high labor cost associated with the assembly of complicated structural systems.
  • the invention combines the novel use of a pre-existing component; the washer, with the modification and transformation of another pre-existing component; the tube, in such a way as to minimize the cost of the system by minimizing the following items which affect cost:
  • the invention gains an economic advantage through a simple fabrication process of modifying pre-existing readily available tubes.
  • the means by which the tubes are modified: flattening, cutting, and bending are fast, simple, and inexpensive to execute in any machine shop.
  • the invention maintains an economic advantage by using a preexisting readily available washer for a novel function as a tension ring.
  • FIG. 2. Shows a side elevation view
  • FIG. 3. Shows a top perspective view
  • FIG. 4. Shows the plan view with a portion of the outer washer and head of the bolt cut away to reveal the inside of the assembly
  • FIG. 5 Shows a section through the assembly
  • FIG. 6. Shows an exploded top perspective view
  • FIG. 7 Shows a side view and a plan view of the end of the strut before the strut tips are bent into their final position.
  • FIG. 10 Shows a sequence of partial sections describing the means by which the the dome joint is manipulated to facilitate assembly.
  • FIG. 1 A basic assembled embodiment of the dome joint is shown in the following figures: (FIG. 1, FIG. 2, FIG. 3, FIG. 5).
  • the struts 4 are sandwiched between the inner washers 3 in a radiating pattern.
  • the Bolt 1 and nut 5 transfer pressure to the top and bottom outer washers 2 which in turn apply pressure to the strut tips 4 A. pressing them flat against the outward facing surfaces of the inner washers 3 .
  • FIG. 1. Shows a bottom perspective view after the bolt 1 is tightened and the dome joint is completely assembled.
  • FIG. 2. Shows an elevation view with the struts 4 sandwiched and restrained by the tension rings 3 .
  • FIG. 10 illustrates the process and mechanism by which the tubes are brought together. And are initially held in place.
  • the shape of the hooked ends of the tubes facilitate the assembly of the joint.
  • the tube ends are brought close enough together so that inner bottom washer can be placed in a position over the bottom hooks.
  • the hooked ends of the tubes grip the inside surface of the hole in the washer.
  • the bottom inner washer holds the tubes loosely in position allowing the adjustments to the angle between the tubes to facilitate the positioning of the top washer over the top hooks at the tube ends.
  • FIG. 4. Shows an exploded top perspective view with the struts 4 radiating from the dome joint with the tips of the struts bent into their final position.
  • the bent strut tips 4 in their final position form hooks that are restrained by the inner washers 3 that act as tension rings.
  • the tension rings 3 restrict the movement of the struts 4 away from the center of the dome joint.
  • the angled edges of the struts 4 act as abutments resisting their movement towards the center of the joint and maintain the angular relationships between the struts.
  • Tubular elements or pipes have advantages over other structural forms because of the load-transmitting qualities inherent in their circular cross section geometry resulting in a superior strength-weight ratio.
  • the failure to use them extensively in the construction of geodesic domes and trusses and truss-like structures was due to the lack of suitable connectors or coupling members for easily and efficiently joining their ends at a common point.
  • a current disadvantage of many geodesic domes and space frame structures presently in use is high labor cost associated with the assembly of complicated structural systems.

Abstract

An improved joint for connecting the ends of tubes for the purpose of assembling a geodesic dome or truss structure (FIG. 6). The tube ends form top and bottom hooks (A4) which face away from each other. The hooked ends (A4) facilitate the attachment of adjacent tubes to the unifying joint by gripping a common top and bottom washer (3). The inner washers (3) are used as tension rings for restricting the movement of the tubes by which they are hooked. The structure is stiffened when the hooks are pressed down into a flattened position by the outer top and bottom washers (2). The outer top and bottom washers are sandwiched by a single nut and bolt assembly (1,5). As the nut and bolt assembly (1,5) is tightened pressure is applied to the outer washers which press the booked ends (4A) of the tubes backwards into a flattened position. The initial condition of the joint is loose to allow adjustments of the positioning of the tubes within the structure. The final state of the joint after the nut and bolt assembly is tightened is stiff completing the structure assembly as a ridged structural frame (FIG. 9).

Description

    BACKGROUND
  • 1. Field of Invention [0001]
  • This invention relates to geodesic dome and space frame structure joint and assembly systems. [0002]
  • 2. Description of Prior Art [0003]
  • Tubular elements or pipes have advantages over other structural forms because of the load-transmitting qualities inherent in their circular cross section and their efficient strength-weight ratio. In the past the failure to employ them extensively in geodesic domes and trusses and truss-like structures was due to the lack of suitable connectors or coupling members for easily and efficiently joining their ends. [0004]
  • A current disadvantage of many geodesic domes and space frame structures presently in use is the high cost of connectors used to interconnect chord and strut members at each node and the high labor cost associated with the assembly of complicated structural systems. [0005]
  • Several current designs shown in the prior art attempt to solve the problems of joining tubes by flattening the ends of the tubes and restraining their movement with an attachment assembly. The first group gains an economic advantage through simple fabrication but loose that advantage in material and labor cost because multiple fasteners are required to complete the assembly. The second group gains economic advantage by reducing the number of fasteners to a minimum but looses this advantage by implementing non pre-existing components that are unique in form and require expensive manufacturing techniques to fabricate. [0006]
  • The prior art Johnson, Jr. U.S. Pat. No. 4,322,176, Mar. 30, 1982 is a patent where the ends of tubes have been formed in order to interlock into a housing with two opposite converging walls. The illustrations show flattened ends of tubes sandwiched together on top of the housings restraining the formed tubes. The sandwiched tubes and the restrained tubes are all held in place by a singular bolt. The bolt simultaneously passes through the housings and through holes in the individual flattened portion of the tubes. The design increases the number of different components and cost by having two different systems for restraining the tubes requiring two different shapes of formed tube ends. Manufacturing the housing; a non pre-existing component, further increases cost. [0007]
  • The prior art A. E. Fentiman U.S. Pat. No. 2,964,147, Dec. 13, 1960 is a patent where the ends of tubes have been flattened in order to form a plane that can be received by a slotted connector. The flattened ends of the tubes are sandwiched inside the slot and held in place by a bolt that passes simultaneously through the hole in the slotted connector and the holes in the individual flattened portion of the angled tubes sandwiched to the top of the slotted connector. The prior art Fentiman U.S. Pat. No. 2,931,467 utilizes a similar system of flattened tube ends having their movement restricted by a slotted connector. Again, the design has only a few components uses only one bolt as a fastener but looses a portion or this cost advantage in the manufacturing of the a unique non pre-existing slotted connector. [0008]
  • The prior art Codd U.S. Pat. No. 4,622,795 Nov. 18, 1986 FIGS. [0009] 1,2,3,4,5,6 and Codd U.S. Pat. No. 4,704,836 Nov. 10, 1987 FIGS. 1,2,5,6 Are designs where the ends of tubes have been flattened in order to form planes that are sandwiched together by numerous bolts. The design gains a cost advantage by using pre-existing components in conjunction with modified pre-existing components but looses much of this advantage as a result of the numerous bolts that add material cost and labor cost during assembly.
  • Several current designs shown in the prior art attempt to solve the problems of joining tubes by attaching the tubes to a tension ring in order to restrict their movement. The first group gains an economic advantage through simple fabrication but loose that advantage in material and labor cost because multiple fasteners are used to complete the assembly. The second group gains economic advantage by reducing the number of fasteners to a minimum but looses some of this advantage by implementing non pre-existing components that are unique in form and require expensive manufacturing techniques to fabricate. [0010]
  • The prior art Woods U.S. Pat. No. 3,486,278 and Birkemeier U.S. Pat. No. 3,635,509 both use components whose movement are restricted by a tension ring. The restricted components act as a connector between the tension ring and the struts. The restricted components are bolted to the struts. Each individual assembly for each end of a strut uses 2 or more bolts to complete the connection adding material cost and most importantly labor cost during assembly. [0011]
  • The prior art Braccini U.S. Pat. No. 3,323,820 and Littlefield U.S. Pat. No. 4,194,851 both use hubs to restrict the movement of the struts. The upper and lower halves of the hubs clamp the restricted struts. The hubs are neither a pre-existing item used in a new way nor a pre-existing item modified for a new use. The manufacture of these hubs are expensive especially when the specifications of the hub change to accommodate the various geometries of different projects. [0012]
  • SUMMARY
  • This invention relates to a joint for connecting the ends of tubes for the purpose of assembling a geodesic dome or truss structure. The tube ends are modified to form top and bottom hooks which face away from each other. The hooked ends facilitate the attachment of the tubes to one another by loosely gripping a common top and bottom washer. The inner washers are used as tension rings for restricting the movement of the tubes. To stiffen the structure the hooks are pressed down into flattened position by the outer top and bottom washers that are sandwiched by a single nut and bolt assembly [0013]
  • OBJECTS AND ADVANTAGES
  • The invention uses tubular elements or pipes which have advantages over other structural forms because of the load-transmitting qualities inherent in their circular cross section and their efficient strength-weight ratio. In the past the failure to employ them extensively in geodesic domes and truss-like structures was due to the lack of suitable connectors or coupling members for easily and efficiently joining their ends. [0014]
  • The advantage of the invention is that it reduces the cost of geodesic domes and space frame structures by reducing the material and fabrication cost of connectors used to attach strut members at each node. A further advantage of the invention is the reduction of high labor cost associated with the assembly of complicated structural systems. [0015]
  • The invention combines the novel use of a pre-existing component; the washer, with the modification and transformation of another pre-existing component; the tube, in such a way as to minimize the cost of the system by minimizing the following items which affect cost: [0016]
  • 1. total number of components in the joint [0017]
  • 2. number of unique components [0018]
  • 3. physical complexity of the components [0019]
  • 4. difficulty of fabricating the components [0020]
  • 5. complexity and time for assembly of the structure. [0021]
  • 6. number of workers required to assemble the structure [0022]
  • Using one system for attaching all the struts reduces the need for a variety of components. The need for many different components with different functions is further reduced by the consolidation of several functions into one component. The flattened angular shaped ends of each tube are bent to form around the tension ring. When the end of a strut is in its final position it becomes part of the restraining system for that strut and the adjacent struts. The angled edges of the flattened portions of the struts become abutments restraining the movement of the struts. The bolt while being tightened is being used as a tool for forming the bent ends of the struts into their final position. [0023]
  • The invention gains an economic advantage through a simple fabrication process of modifying pre-existing readily available tubes. The means by which the tubes are modified: flattening, cutting, and bending are fast, simple, and inexpensive to execute in any machine shop. The invention maintains an economic advantage by using a preexisting readily available washer for a novel function as a tension ring. [0024]
  • The cost advantage is maintained in minimum labor cost on the construction site because the action of tightening a single bolt per connector completes the coupling of the tubes with the tension ring during assembly. Flexibility within the lightly tightened joint allows the structure to be manipulated in order to sequentially attach tubes at adjacent joints. A sequential assembly requires a minimal amount of workers to execute which further reduces labor cost.[0025]
  • DRAWING FIGURES
  • FIG. 1. Shows a bottom perspective view of the joint [0026]
  • FIG. 2. Shows a side elevation view [0027]
  • FIG. 3. Shows a top perspective view [0028]
  • FIG. 4. Shows the plan view with a portion of the outer washer and head of the bolt cut away to reveal the inside of the assembly [0029]
  • FIG. 5. Shows a section through the assembly [0030]
  • FIG. 6. Shows an exploded top perspective view [0031]
  • FIG. 7. Shows a side view and a plan view of the end of the strut before the strut tips are bent into their final position. [0032]
  • FIG. 8. Shows a side view and a plan view of the end of the strut after the strut tips are bent into their final position. [0033]
  • FIG. 9 Shows an geodesic dome assembled with the dome joint. [0034]
  • FIG. 10 Shows a sequence of partial sections describing the means by which the the dome joint is manipulated to facilitate assembly.[0035]
  • REFRENCE NUMERALS IN DRAWINGS
  • [0036] 1. bolt
  • [0037] 2. top and bottom outer washers
  • [0038] 3. top and bottom inner washer tension rings
  • [0039] 4. tube
  • [0040] 4A. tube tip
  • [0041] 4B. angled abutment portion of the strut tip
  • [0042] 5. nut
  • DESCRIPTION
  • A basic assembled embodiment of the dome joint is shown in the following figures: (FIG. 1, FIG. 2, FIG. 3, FIG. 5). The [0043] struts 4 are sandwiched between the inner washers 3 in a radiating pattern. The Bolt 1 and nut 5 transfer pressure to the top and bottom outer washers 2 which in turn apply pressure to the strut tips 4A. pressing them flat against the outward facing surfaces of the inner washers 3. (FIG. 1.) Shows a bottom perspective view after the bolt 1 is tightened and the dome joint is completely assembled. (FIG. 2.) Shows an elevation view with the struts 4 sandwiched and restrained by the tension rings 3. (FIG. 3.) Shows a top perspective view with the struts 4 radiating from the dome joint. (FIG. 4.) Shows an exploded top perspective view with the struts 4 radiating from the dome joint with the tips of the struts 4A. bent into their final position. The bent strut tips 4 in their final position form hooks that are restrained by the inner washers 3 that act as tension rings. The tension rings 3 restrict the movement of the struts 4 away from the center of the dome joint. The angled edges of the struts 4 act as abutments 4B. resisting their movement towards the center of the joint and maintain the angular relationships between the struts.
  • Operations [0044]
  • The manner of assembling the dome joint is shown in the following figures: (FIG. 1, FIG. 2, FIG. 3, FIG. 5, FIG. 10). [0045]
  • FIG. 10 illustrates the process and mechanism by which the tubes are brought together. And are initially held in place. The shape of the hooked ends of the tubes facilitate the assembly of the joint. The tube ends are brought close enough together so that inner bottom washer can be placed in a position over the bottom hooks. The hooked ends of the tubes grip the inside surface of the hole in the washer. The bottom inner washer holds the tubes loosely in position allowing the adjustments to the angle between the tubes to facilitate the positioning of the top washer over the top hooks at the tube ends. [0046]
  • The second step of assembly is the sandwiching of the [0047] struts 4 between the inner washers 3 in a radiating pattern. The top and bottom outer washers 2 are placed in position and the bolt 1 and nut 5 are lightly tightened allowing flexibility within the structure. Flexibility within the joint allows for a sequentially assembly of the adjacent joints. Finally when all the tubes and joints are in place the bolts 1 and nuts 5 are further tightened to transfer pressure to the top and bottom outer washers 2 which in turn apply pressure to the strut tips 4 bending them backwards and flattening them against the outside surface of the inner washers 3. (FIG. 1.) Shows a bottom perspective view after the bolt 1 is tightened and the dome joint is completely assembled. (FIG. 2.) Shows an elevation view with the struts 4 sandwiched and restrained by the tension rings 3. (FIG. 3.) Shows a top perspective view with the struts 4 radiating from the dome joint.
  • (FIG. 4.) Shows an exploded top perspective view with the [0048] struts 4 radiating from the dome joint with the tips of the struts bent into their final position. The bent strut tips 4 in their final position form hooks that are restrained by the inner washers 3 that act as tension rings. The tension rings 3 restrict the movement of the struts 4 away from the center of the dome joint. The angled edges of the struts 4 act as abutments resisting their movement towards the center of the joint and maintain the angular relationships between the struts.
  • CONCLUSIONS, RAMIFICATIONS, SCOPE
  • Tubular elements or pipes have advantages over other structural forms because of the load-transmitting qualities inherent in their circular cross section geometry resulting in a superior strength-weight ratio. In the past the failure to use them extensively in the construction of geodesic domes and trusses and truss-like structures was due to the lack of suitable connectors or coupling members for easily and efficiently joining their ends at a common point. [0049]
  • In order to make the structural advantages of the tube more accessible for the use in domes and truss structures the simplest means by which a tube can be modified flattening, cutting, and bending were exploited in order to interlock the tubes with washers used as tension rings. The dome joint combines the novel use of a pre-existing inexpensive mass-produced component; the washer; with the simple modification of tubes, in such a way as to minimize the cost of the manufacture of the structural system. [0050]
  • A current disadvantage of many geodesic domes and space frame structures presently in use is high labor cost associated with the assembly of complicated structural systems. [0051]
  • The use of only one bolt per joint reduces the complexity and reduces the time needed for assembly of a structural dome or truss resulting in lower labor cost. The flexible nature of the joint before it is tightened allows the structure to be assembled sequentially which requires a minimal number of workers further lowering labor cost. [0052]
  • A geodesic dome and space frame structure joint and assembly systems.[0053]

Claims (7)

1. A means by which tubular struts attach to a tension ring.
2. Said tubular strut with hooked ends for griping said tension ring in a loose manner allowing flexure of the struts.
3. Said tubular strut with hooked ends for griping said tension ring in a tight manner restricting the flexure and movement of the struts.
4. A means to deform said strut to complete the attachment to a tension ring.
5. A nut and bolt assembly tightened to apply pressure to and bend said strut angled tips to form top and bottom hooks for the purpose of griping said tension ring.
6. A means of restricting the movement of said tubular struts.
7. A washer used as a common tension resistant juncture for resisting the movement of said tubular struts.
US10/163,906 2002-06-06 2002-06-06 Geodesic dome assemby joint Abandoned US20030226319A1 (en)

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US20080209821A1 (en) * 2004-08-10 2008-09-04 Abdessatar Nefzi Method for Producing Triangular Elements Designed for the Manufacture of Structures and Resulting Triangular Elements
US20090049763A1 (en) * 2007-08-21 2009-02-26 Joseph Timothy Blundell C.O.R.E. - Continuous Omnidirectional Radian Energy geodesic hubs/structures
DE202008014225U1 (en) 2008-07-08 2009-03-12 Domesworld Gmbh Geodesic dome
KR101134699B1 (en) 2009-07-10 2012-04-13 한덕전 Multiple Axle Coupling Joint and Arch Type House structure Using the Same
US20150233342A1 (en) * 2014-02-19 2015-08-20 General Electric Company Wind turbine dome and method of assembly
CN105888066A (en) * 2016-04-22 2016-08-24 浙江财经大学 Multi-section type bamboo dome structure
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US9541109B2 (en) * 2013-02-25 2017-01-10 Xiaoping Sun Dome structure
CN106759896A (en) * 2017-01-25 2017-05-31 哈尔滨工业大学 A kind of aluminum joints of use self-locking screw assembly space structure
US20170167516A1 (en) * 2015-12-09 2017-06-15 Paul H. Mason Strut Connector
WO2017180078A1 (en) 2016-04-14 2017-10-19 360Art.Pro, Llc Coupling connector and geodome frame made therewith
US20170305471A1 (en) * 2015-03-11 2017-10-26 Caterpillar Inc. Node for a space frame
US9903107B1 (en) * 2016-12-16 2018-02-27 Linda K. Albright Beam connector
US20190154079A1 (en) * 2017-11-21 2019-05-23 Robert Shapiro Geodesic Framework Hub with Strut Holding Mechanism Movable Between Full-Hold and Partial-Hold Positions
USD855446S1 (en) * 2017-07-03 2019-08-06 Superpod Pty. Ltd Bracket for five point stand
US20190390454A1 (en) * 2018-06-25 2019-12-26 Anthony Martin Kalenak Method of attaching a membrane to a tubular framework and an integrated system using this method to build geodesic domes
US20200109549A1 (en) * 2017-03-30 2020-04-09 Manuel Fernando BETHENCOURT CRAVID Lattice structure
US20220025652A1 (en) * 2020-07-21 2022-01-27 Axis Lighting Inc. Ceiling panel assembly
US11486129B1 (en) * 2020-07-07 2022-11-01 Michael E. Garvey Geodesic frame connector system and method

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2658776A (en) * 1950-03-14 1953-11-10 Burr C Wilcox Structural rod joint
US2682235A (en) * 1951-12-12 1954-06-29 Fuller Richard Buckminster Building construction
US3323820A (en) * 1965-04-19 1967-06-06 Whittaker Corp Space frame structures
US3959937A (en) * 1974-06-17 1976-06-01 Leonard Spunt Modular dome structure
US4244152A (en) * 1978-12-19 1981-01-13 Pittsburgh-Des Moines Steel Company Joint for geodesic dome
US4296585A (en) * 1978-05-30 1981-10-27 Dante Bini Permanent weather covers
US4322176A (en) * 1980-05-14 1982-03-30 Lajet Energy Company Tubular beam joint
US4480418A (en) * 1981-07-14 1984-11-06 Ettore Ventrella Modular system for space grid structures
US4622795A (en) * 1983-08-23 1986-11-18 Tulserate Limited Space frames
US4704836A (en) * 1984-05-31 1987-11-10 Tulserate Limited Space frames
US5996288A (en) * 1997-10-20 1999-12-07 Aiken; Ernest G Geodesic domes and improved joints therefor
US6321502B1 (en) * 1999-06-16 2001-11-27 Geometrica, Inc. Method of making connector hub
US6378265B1 (en) * 1999-03-01 2002-04-30 Matias Konstandt Space frame construction assembly

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2658776A (en) * 1950-03-14 1953-11-10 Burr C Wilcox Structural rod joint
US2682235A (en) * 1951-12-12 1954-06-29 Fuller Richard Buckminster Building construction
US3323820A (en) * 1965-04-19 1967-06-06 Whittaker Corp Space frame structures
US3959937A (en) * 1974-06-17 1976-06-01 Leonard Spunt Modular dome structure
US4296585A (en) * 1978-05-30 1981-10-27 Dante Bini Permanent weather covers
US4244152A (en) * 1978-12-19 1981-01-13 Pittsburgh-Des Moines Steel Company Joint for geodesic dome
US4322176A (en) * 1980-05-14 1982-03-30 Lajet Energy Company Tubular beam joint
US4480418A (en) * 1981-07-14 1984-11-06 Ettore Ventrella Modular system for space grid structures
US4622795A (en) * 1983-08-23 1986-11-18 Tulserate Limited Space frames
US4704836A (en) * 1984-05-31 1987-11-10 Tulserate Limited Space frames
US5996288A (en) * 1997-10-20 1999-12-07 Aiken; Ernest G Geodesic domes and improved joints therefor
US6378265B1 (en) * 1999-03-01 2002-04-30 Matias Konstandt Space frame construction assembly
US6321502B1 (en) * 1999-06-16 2001-11-27 Geometrica, Inc. Method of making connector hub

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080209821A1 (en) * 2004-08-10 2008-09-04 Abdessatar Nefzi Method for Producing Triangular Elements Designed for the Manufacture of Structures and Resulting Triangular Elements
US7770338B2 (en) * 2004-08-10 2010-08-10 Abdessatar Nefzi Method for producing triangular elements designed for the manufacture of structures and resulting triangular elements
US20090049763A1 (en) * 2007-08-21 2009-02-26 Joseph Timothy Blundell C.O.R.E. - Continuous Omnidirectional Radian Energy geodesic hubs/structures
DE202008014225U1 (en) 2008-07-08 2009-03-12 Domesworld Gmbh Geodesic dome
DE102008053205A1 (en) 2008-07-08 2010-04-15 Domesworld Gmbh Geodetic dome, has connections for production of point storage including stud for drilling in latches, where stud is connected with plate and receiving borehole for stud in another gusset plate
KR101134699B1 (en) 2009-07-10 2012-04-13 한덕전 Multiple Axle Coupling Joint and Arch Type House structure Using the Same
US9541109B2 (en) * 2013-02-25 2017-01-10 Xiaoping Sun Dome structure
US20150233342A1 (en) * 2014-02-19 2015-08-20 General Electric Company Wind turbine dome and method of assembly
US9249776B2 (en) * 2014-02-19 2016-02-02 General Electric Company Wind turbine dome and method of assembly
US10569810B2 (en) * 2015-03-11 2020-02-25 Caterpillar Inc. Node for a space frame
US20170305471A1 (en) * 2015-03-11 2017-10-26 Caterpillar Inc. Node for a space frame
US20170167516A1 (en) * 2015-12-09 2017-06-15 Paul H. Mason Strut Connector
US9719243B2 (en) * 2015-12-09 2017-08-01 Paul H. Mason Strut connector
WO2017180078A1 (en) 2016-04-14 2017-10-19 360Art.Pro, Llc Coupling connector and geodome frame made therewith
CN105888066A (en) * 2016-04-22 2016-08-24 浙江财经大学 Multi-section type bamboo dome structure
CN105971119A (en) * 2016-04-22 2016-09-28 浙江财经大学 Manufacturing method for soil-covering bamboo component
US9903107B1 (en) * 2016-12-16 2018-02-27 Linda K. Albright Beam connector
CN106759896A (en) * 2017-01-25 2017-05-31 哈尔滨工业大学 A kind of aluminum joints of use self-locking screw assembly space structure
US20200109549A1 (en) * 2017-03-30 2020-04-09 Manuel Fernando BETHENCOURT CRAVID Lattice structure
US10822787B2 (en) * 2017-03-30 2020-11-03 Manuel Fernando BETHENCOURT CRAVID Lattice structure
USD855446S1 (en) * 2017-07-03 2019-08-06 Superpod Pty. Ltd Bracket for five point stand
US20190154079A1 (en) * 2017-11-21 2019-05-23 Robert Shapiro Geodesic Framework Hub with Strut Holding Mechanism Movable Between Full-Hold and Partial-Hold Positions
US20190390454A1 (en) * 2018-06-25 2019-12-26 Anthony Martin Kalenak Method of attaching a membrane to a tubular framework and an integrated system using this method to build geodesic domes
US11486129B1 (en) * 2020-07-07 2022-11-01 Michael E. Garvey Geodesic frame connector system and method
US20220025652A1 (en) * 2020-07-21 2022-01-27 Axis Lighting Inc. Ceiling panel assembly

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