US20040031208A1 - Inflatable structure - Google Patents
Inflatable structure Download PDFInfo
- Publication number
- US20040031208A1 US20040031208A1 US10/643,247 US64324703A US2004031208A1 US 20040031208 A1 US20040031208 A1 US 20040031208A1 US 64324703 A US64324703 A US 64324703A US 2004031208 A1 US2004031208 A1 US 2004031208A1
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- United States
- Prior art keywords
- legs
- leg
- structural elements
- apical
- tetrahedron
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- Abandoned
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- 239000004744 fabric Substances 0.000 claims abstract description 17
- 230000000295 complement effect Effects 0.000 claims abstract description 3
- 229920003023 plastic Polymers 0.000 claims description 2
- 239000004033 plastic Substances 0.000 claims description 2
- 239000002759 woven fabric Substances 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 abstract description 11
- 229920000728 polyester Polymers 0.000 abstract description 5
- 238000005452 bending Methods 0.000 abstract description 2
- 238000005755 formation reaction Methods 0.000 description 10
- 239000012530 fluid Substances 0.000 description 4
- 239000011295 pitch Substances 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000013011 mating Effects 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000004800 polyvinyl chloride Substances 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000003319 supportive effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H15/00—Tents or canopies, in general
- E04H15/20—Tents or canopies, in general inflatable, e.g. shaped, strengthened or supported by fluid pressure
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H15/00—Tents or canopies, in general
- E04H15/20—Tents or canopies, in general inflatable, e.g. shaped, strengthened or supported by fluid pressure
- E04H2015/201—Tents or canopies, in general inflatable, e.g. shaped, strengthened or supported by fluid pressure with inflatable tubular framework, with or without tent cover
Definitions
- This invention relates to an inflatable structure.
- inflatable structures such as inflatable boats, inflatable life rafts and the like are manufactured from airtight fabrics.
- These fabrics conventionally consist of a polyvinyl chloride (PVC) fabric reinforced with woven polyester.
- PVC polyvinyl chloride
- the fabric is cut and welded, either with the use of heat welding or with adhesives, to obtain the desired shapes.
- Frame structures as typically utilised in a tent or canopy utilise structural intersections that are typically too complex and difficult to manufacture with the current state of art in inflatable tube manufacturing.
- a structure comprising at least three structural units each consisting of three inflatable legs, two of which constitute support legs and the third constituting an apical leg, each leg having a free end and an inner end, the inner ends of the three legs being joined at a centrepoint, the legs being arranged to define a tetrahedron with the three legs lying on three adjacent edges of the tetrahedron and with adjacent pairs of legs lying in planes of three sides of the tetrahedron, and the free ends of the legs define the fourth side of the tetrahedron; wherein the free ends of the units are closed and wherein the units are arranged each with one leg joined to corresponding legs of the other units at ajoint position.
- each leg of each unit are preferably of the same length although two of the legs are of the same length and the third leg is of a different length.
- each leg is straight.
- Each leg preferably comprises a plastic reinforced by a woven fabric. The warp of the fabric is conveniently aligned with the tube axis.
- a connector unit is conveniently provided at the free end of at least one of the legs whereby it may be connected to a similar leg of another structural unit.
- the structural element of the invention will yield, in combination with similar structural elements, a variety of geodesic structures.
- the apical legs of the structural elements may be secured to the apical legs of adjacent, similar structural elements.
- the support legs of the structural elements may be secured to the support legs of adjacent, similar structural elements.
- each structural element may be provided with mating connector formations to permit easy connection and disconnection to the apical legs of adjacent structural elements.
- the support legs of each structural element may be provided with mating connector formations to permit easy connection and disconnection to the support legs of adjacent structural elements.
- the connector constitutes the mating track and slider formations that can be inter engaged with one another to connect the structural elements together.
- each structural element is geometrically shaped along the natural complimentary lines along the intersecting surfaces of the adjacent structural element.
- the connectors are fixed along their relative axial angles.
- FIG. 1 is a diagrammatic isometric view of a tetrahedral structural element according to this invention.
- FIG. 2 is a diagrammatic plan view of a simple inflatable structure made up of four of the structural elements of FIG. 1.
- FIG. 3 is a diagrammatic end elevation of the structure of FIG. 2.
- FIG. 4 is a diagrammatic plan view on the point of connection of the structural elements in the structure of FIGS. 2 and 3.
- FIG. 5 is a diagrammatic sectional side elevation illustrating a novel lighting arrangement for structures according to the invention.
- FIGS. 6,7 and 8 are diagrammatic plan view, end elevation and side elevation respectively of a structure that combines the structural element of FIG. 1 with a number similar and dissimilar units to provide a more complex geodesic dome structure than that illustrated in FIGS. 2 and 3.
- the inflatable structure of the invention is more of a construction system than a simple structure.
- the system relies on the use of an inflatable polyhedral structural element as its basic unit of construction. By combining such a structural element with similar structural elements or with similarly polyhedral structural elements, a large variety of structures can be created as will be illustrated below.
- the structural element 10 illustrated in FIG. 1 has an essentially tetrahedral shape.
- a tetrahedron being a polyhedron with four triangular sides, the structural element is made of three inflatable relatively narrow tubes 10 . 1 , 10 . 2 , 10 . 3 , each lying on an edge of the tetrahedron.
- Three of the triangular sides of the tetrahedron are constituted by the triangular planes included between the three legs and the fourth triangular side is constituted by the plane defined by the free ends of the legs.
- the structural element constitutes an inverted Y shaped support element.
- the legs 10 . 1 and 10 . 2 lie on the inverted arms of the Y and constitute support legs.
- the remaining leg 10 . 3 defines the stern of the Y, which is angled relatively to the legs 10 . 1 , 10 . 2 to define a support beam in structures to be erected with the use of the structural element 10 .
- the tubes making up the legs 10 . 1 , 10 . 2 , 10 . 3 of the structural support element are made from airtight PVC fabric reinforced with woven polyester.
- the woven polyester reinforcing fabric is arranged with the warp thereof aligned longitudinally with the principal axis of each of the tubular legs 10 . 1 , 10 . 2 , and 10 . 3 . This gives the tubes a high resistance to bending.
- the polyester reinforcing fabric may be arranged on the bias (with the warp at an angle to the tube axis) to a greater or lesser degree, depending on the curvature that will be permitted.
- the airtight fabric is double welded along the length of each tube.
- the fabric is welded along axially extending seams with a separate strip of fabric welded internally along each of the seams to provide enhanced sealing.
- each leg 10 . 1 , 10 . 2 and 10 . 3 are interconnected at their inner ends 10 a across a joint 12 through which the pressurising fluid can flow freely during inflation and deflation of the structural element 10 .
- the closed end of each legs 10 . 1 , 10 . 2 and 10 . 3 is geometrically shaped along the natural complimentary lines along the intersecting surfaces of the adjacent structural element.
- the structural element 10 is inflated and deflated by means of an inflation valve (illustrated diagrammatically at 14 ).
- the inflatable tubes are airtight and once it is filled with compressed gas to the desired pressure and sealed off, will maintain its rigidity and support strength without any further addition of compressed air.
- pressurising fluid would be compressed air obtained from a blower or compressor, or from a pressurised gas canister, but alternative pressurising fluids such as motor vehicle exhaust gas could also be used, provided the appropriate inflation fittings are used.
- the structural element 10 of the invention can be combined into relatively complex structures that, because of the tetrahedral shape of the unit 10 , will have the characteristics of geodesic domes.
- the simple structure 100 illustrated in FIGS. 2 and 3 provides an example of the structure building capabilities of the basic structural element 10 .
- the apical legs 10 . 3 of the units 10 are connected to one another at the apex 102 of the structure 100 by means of connectors that will be described below. At the connection there are preferably valves leading into support legs 10 . 2 and 10 . 2 near their lower closed ends. The valves of adjacent legs are connected by means of short hoses during inflation so that the entire structure can be inflated from a single inflation valve 14 .
- the support legs 10 . 1 and 10 . 2 of the structural elements 10 extend down to the ground and are connected to one another by means of connectors that will be described below.
- the structure 100 may now be clad with a fabric cover (not shown).
- the structure 100 is clad with a fabric cover and fastened to a groundsheet, it is completely free standing and needs no pegs or anchor ropes to keep it stable. Very little experience or knowledge is now required to pitch the tent. The energy that pitches the tent is supplied by the compressed gas and the whole process is done in a fraction of the normal time. There is also no assembly needed to pitch the tent. The unit only needs to be unfolded and inflated to pitch the tent. The same applies when putting the tent down. The valves in the tubes are opened to let the compressed gas out and the whole structure collapses. It is then folded as a unit in the normal way. There is thus no poles or other structural elements to account for.
- the structure 100 provides a high degree of wind resistance but, if required, the structure can be pegged to the ground.
- the structure 100 is erected using four separate structural elements 10 that are connected to one another.
- FIG. 4 illustrates two of the metal connectors 15 that are used to interconnect the structural element ends 10 . 4 of the structural elements 10 (the free ends of the legs 10 . 1 , 10 . 2 and 10 . 3 of the structural elements 10 ).
- the ends 10 . 4 of the structural elements 10 are shaped complementary to permit interconnection of the structural elements along the axial angle of the completed structure.
- Each such leg end 10 . 4 is finished off with a flat end weld 13 that is double welded and inserted between the flat strips of metal making up the connectors 15 .
- Each structural element 10 is provided, at its leg ends 10 . 4 with a connector 15 that comprises a slider 16 and track formation 18 , the slider 16 being adapted to slide into the track 18 of an adjacent connector 15 .
- the slider and track formations 16 , 18 are dimensioned to provide a secure friction fit once interconnected.
- the connectors are fixed along their relative axial angles at the vertex of the polyhedron.
- the utilisation of the connector 15 on each tube end has the advantage that two or more tube ends can be interconnected in a very strong and stable bond alleviating the need for a complex welded joint.
- the entire connector 15 is riveted together with blind rivets. This has the advantage that the connector formations 16 , 18 can be removed to permit reopening of the tube ends and the servicing of the tubes.
- the structure 100 illustrated in FIGS. 2 and 3 are a relatively simple structure that utilises only the basic structural element 10 illustrated in FIG. 1.
- the basic structural unit 10 can be used in conjunction with similar yet slightly more complex structural elements to provide more complex structures as is illustrated in FIGS. 6, 7 and 8 .
- the structure 200 shown in these drawings utilises three of the basic structural elements 10 at each of its short ends.
- the apex and long sides of the structure 200 are defined by a pair of opposed structural elements 204 , each of which incorporates a pair of support legs 204 . 1 and a pair of apical legs 204 . 2 that extend upwardly towards an apical beam 206 that defines the apex of the structure 200 .
- the apical legs 10 . 3 of the elements 10 at each end of the structure 200 are connected to the ends of the beam 206 by means as described above.
- the structural element 10 will yield, in combination with similar structural elements, a variety of geodesic structures.
- the apical legs of the structural elements may be secured to the apical legs of adjacent, similar structural elements.
- the support legs of the structural elements may be secured to the support legs of adjacent, similar structural elements.
- the basic structural elements 10 may be flanked by a slightly modified structural element, each of which differs from the basic structural element 10 only in the fact that it has an asymmetrical tetrahedral shape.
- the structures of the invention being inflatable, lend themselves to novel uses.
- the structure could be internally lit using light fittings 20 fitted to the insides of the tubes making up the structural elements.
- the fabric of the tubes and the structure as a whole will be chosen for translucency to enhance the lighting effect.
- the structures need not be confined to land. Being inflatable, the structures will float on water to provide a novel staging facility for events and advertising.
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- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Tents Or Canopies (AREA)
- Materials For Medical Uses (AREA)
Abstract
This invention comprises an inflatable structure that is constructed by combining polyhedron structural elements to form more complex geodesic structures. The structural elements are constructed out of straight inflatable tubes, in which the warp of the polyester reinforced fabric is aligned with the principal tube axis, giving it high resistance to bending. The complementary leg ends are connected at the vertices with connectors that comprise a slider and track formation, fixed along the axial angle at the end of each leg. Each leg end is shaped along the natural complimentary lines along the intersecting surfaces of the adjacent structural element. Once assembled, in combination with a fabric cover and groundsheet, the tent is stable and completely freestanding.
Description
- This application is a continuation-in-part of co-pending International Application No. PCT/ZA01/00175, filed on Nov. 14, 2001 and claims priority of South African Application No. 2000/6289, filed Nov. 14, 2000.
- This invention relates to an inflatable structure.
- DESCRIPTION OF THE PRIOR ART
- The applicant is the patentee in respect of South African Patent No. 97/5569—Inflatable tent frame—which describes a frame comprising at least three tubular legs each constituting a separately sealed chamber that is capable of being inflated with a fluid such as air or gas to constitute a frame structure for a tent or canopy.
- Conventionally, inflatable structures such as inflatable boats, inflatable life rafts and the like are manufactured from airtight fabrics. These fabrics conventionally consist of a polyvinyl chloride (PVC) fabric reinforced with woven polyester. The fabric is cut and welded, either with the use of heat welding or with adhesives, to obtain the desired shapes.
- However, tubes that are relatively long and narrow tend to distort, particularly if they are unsupported. Thus for example to endeavour to deal with this problem large numbers of inflatable tubes are used in an arrangement as shown in French Patent No. 2697045 (A. S. Semmel). This is complex and expensive.
- This kind of problem normally does not arise with inflatable water craft since these craft utilise relatively short, large diameter tubes and normally include rigid or semi-rigid structures to which the tubes are attached.
- In the known inflatable tent technology it is very difficult to construct a frame that is fully free standing, unsupported by anchors and anchor ropes. Stability is normally achieved by utilising relatively large diameter tubes combined with an anchoring system, making the tent relatively heavy and expensive, limiting the application potential to relative small-specialised market sectors. The arrangement of tubes in tetrahedron formation is disclosed in British Patent No. 2090622. Here the ends of all three tubes engage the ground. There is no learning that these tubes can be connected together.
- Frame structures as typically utilised in a tent or canopy, utilise structural intersections that are typically too complex and difficult to manufacture with the current state of art in inflatable tube manufacturing.
- In conventional tent construction where the frame is constructed out of solid structural elements such as metal tubing or spring steel rods, a fair amount of labour and knowledge and time is needed to construct the tent. These tents, even in their simplest form still comprise different parts that need assembly. In U.S. Pat. No. 3,502,091 (Corbin) there is shown a tent supporting frame comprising a ridge struts which are hinged together and to side struts. In order for the frame to take up a support position, a complicated hub with an extendable rod therethrough is provided and cable system including lock means is provided to draw the ridge struts into the desired position.
- In U.S. Pat. No. 2,938,526 (Harrison III, et al) there is described an inflatable shelter including an arrangement of tubes some of which are arranged in tetrahedron formation wherein a cap portion is provided to which twelve inflatable struts are connected. Although this may seem to be theoretically possible, it is doubted whether this can be provided in practice. The cap portion is too complicated to be practically possible to manufacture. Furthermore, with the arrangement in this specification, ropes are required to connect the ends of the formations to permit the structure to be erected. In addition spoke-like tubes are provided between the formation leading to the cap portion. This will mean that webbing members on either side of each spoke-like tube will be inclined to one another making for a complex internal shape.
- It is an object of this invention to provide tubular structural elements that address these deficiencies and to provide structures that utilise such structural elements.
- According to this invention there is provided a structure comprising at least three structural units each consisting of three inflatable legs, two of which constitute support legs and the third constituting an apical leg, each leg having a free end and an inner end, the inner ends of the three legs being joined at a centrepoint, the legs being arranged to define a tetrahedron with the three legs lying on three adjacent edges of the tetrahedron and with adjacent pairs of legs lying in planes of three sides of the tetrahedron, and the free ends of the legs define the fourth side of the tetrahedron; wherein the free ends of the units are closed and wherein the units are arranged each with one leg joined to corresponding legs of the other units at ajoint position.
- The three legs of each unit are preferably of the same length although two of the legs are of the same length and the third leg is of a different length. Preferably each leg is straight. Each leg preferably comprises a plastic reinforced by a woven fabric. The warp of the fabric is conveniently aligned with the tube axis.
- A connector unit is conveniently provided at the free end of at least one of the legs whereby it may be connected to a similar leg of another structural unit.
- Being polyhedral, the structural element of the invention will yield, in combination with similar structural elements, a variety of geodesic structures. In such structures, the apical legs of the structural elements may be secured to the apical legs of adjacent, similar structural elements. In the same way the support legs of the structural elements may be secured to the support legs of adjacent, similar structural elements.
- The apical leg of each structural element may be provided with mating connector formations to permit easy connection and disconnection to the apical legs of adjacent structural elements. In the same way the support legs of each structural element may be provided with mating connector formations to permit easy connection and disconnection to the support legs of adjacent structural elements.
- In the preferred form of the invention, the connector constitutes the mating track and slider formations that can be inter engaged with one another to connect the structural elements together.
- The tube ends of each structural element is geometrically shaped along the natural complimentary lines along the intersecting surfaces of the adjacent structural element. The connectors are fixed along their relative axial angles.
- Connecting adjacent structural elements in this manner is simple yet it results in a very strong and supportive joint, utilising the inherent strength of the inflatable tube.
- Structural elements connected together into a composite structure in this way form a very stable inflated structure.
- FIG. 1 is a diagrammatic isometric view of a tetrahedral structural element according to this invention.
- FIG. 2 is a diagrammatic plan view of a simple inflatable structure made up of four of the structural elements of FIG. 1.
- FIG. 3 is a diagrammatic end elevation of the structure of FIG. 2.
- FIG. 4 is a diagrammatic plan view on the point of connection of the structural elements in the structure of FIGS. 2 and 3.
- FIG. 5 is a diagrammatic sectional side elevation illustrating a novel lighting arrangement for structures according to the invention.
- FIGS. 6,7 and 8 are diagrammatic plan view, end elevation and side elevation respectively of a structure that combines the structural element of FIG. 1 with a number similar and dissimilar units to provide a more complex geodesic dome structure than that illustrated in FIGS. 2 and 3.
- The inflatable structure of the invention is more of a construction system than a simple structure. The system relies on the use of an inflatable polyhedral structural element as its basic unit of construction. By combining such a structural element with similar structural elements or with similarly polyhedral structural elements, a large variety of structures can be created as will be illustrated below.
- The
structural element 10 illustrated in FIG. 1 has an essentially tetrahedral shape. A tetrahedron, being a polyhedron with four triangular sides, the structural element is made of three inflatable relatively narrow tubes 10.1, 10.2, 10.3, each lying on an edge of the tetrahedron. Three of the triangular sides of the tetrahedron are constituted by the triangular planes included between the three legs and the fourth triangular side is constituted by the plane defined by the free ends of the legs. - Seen differently, the structural element constitutes an inverted Y shaped support element.
- The legs 10.1 and 10.2 lie on the inverted arms of the Y and constitute support legs. The remaining leg 10.3 defines the stern of the Y, which is angled relatively to the legs 10.1, 10.2 to define a support beam in structures to be erected with the use of the
structural element 10. - The tubes making up the legs 10.1, 10.2, 10.3 of the structural support element are made from airtight PVC fabric reinforced with woven polyester.
- The woven polyester reinforcing fabric is arranged with the warp thereof aligned longitudinally with the principal axis of each of the tubular legs 10.1, 10.2, and 10.3. This gives the tubes a high resistance to bending.
- If it is desired to permit curvature of the tubes to provide a more dome shaped tetrahedron, the polyester reinforcing fabric may be arranged on the bias (with the warp at an angle to the tube axis) to a greater or lesser degree, depending on the curvature that will be permitted.
- The airtight fabric is double welded along the length of each tube. In practice, the fabric is welded along axially extending seams with a separate strip of fabric welded internally along each of the seams to provide enhanced sealing.
- The tubes making up the legs 10.1, 10.2 and 10.3 are interconnected at their inner ends 10 a across a joint 12 through which the pressurising fluid can flow freely during inflation and deflation of the
structural element 10. The closed end of each legs 10.1, 10.2 and 10.3 is geometrically shaped along the natural complimentary lines along the intersecting surfaces of the adjacent structural element. - The
structural element 10 is inflated and deflated by means of an inflation valve (illustrated diagrammatically at 14). The inflatable tubes are airtight and once it is filled with compressed gas to the desired pressure and sealed off, will maintain its rigidity and support strength without any further addition of compressed air. - The most convenient pressurising fluid would be compressed air obtained from a blower or compressor, or from a pressurised gas canister, but alternative pressurising fluids such as motor vehicle exhaust gas could also be used, provided the appropriate inflation fittings are used.
- The
structural element 10 of the invention can be combined into relatively complex structures that, because of the tetrahedral shape of theunit 10, will have the characteristics of geodesic domes. - The
simple structure 100 illustrated in FIGS. 2 and 3 provides an example of the structure building capabilities of the basicstructural element 10. - In the
structure 100, four of theunits 10 are interconnected to form a four-sided structural frame. - The apical legs 10.3 of the
units 10 are connected to one another at the apex 102 of thestructure 100 by means of connectors that will be described below. At the connection there are preferably valves leading into support legs 10.2 and 10.2 near their lower closed ends. The valves of adjacent legs are connected by means of short hoses during inflation so that the entire structure can be inflated from asingle inflation valve 14. - The support legs 10.1 and 10.2 of the
structural elements 10 extend down to the ground and are connected to one another by means of connectors that will be described below. - The
structure 100 may now be clad with a fabric cover (not shown). - Once the
structure 100 is clad with a fabric cover and fastened to a groundsheet, it is completely free standing and needs no pegs or anchor ropes to keep it stable. Very little experience or knowledge is now required to pitch the tent. The energy that pitches the tent is supplied by the compressed gas and the whole process is done in a fraction of the normal time. There is also no assembly needed to pitch the tent. The unit only needs to be unfolded and inflated to pitch the tent. The same applies when putting the tent down. The valves in the tubes are opened to let the compressed gas out and the whole structure collapses. It is then folded as a unit in the normal way. There is thus no poles or other structural elements to account for. - The
structure 100 provides a high degree of wind resistance but, if required, the structure can be pegged to the ground. - It will be seen that the
structure 100 is erected using four separatestructural elements 10 that are connected to one another. - FIG. 4 illustrates two of the
metal connectors 15 that are used to interconnect the structural element ends 10.4 of the structural elements 10 (the free ends of the legs 10.1, 10.2 and 10.3 of the structural elements 10). The ends 10.4 of thestructural elements 10 are shaped complementary to permit interconnection of the structural elements along the axial angle of the completed structure. Each such leg end 10.4 is finished off with aflat end weld 13 that is double welded and inserted between the flat strips of metal making up theconnectors 15. - Each
structural element 10 is provided, at its leg ends 10.4 with aconnector 15 that comprises aslider 16 andtrack formation 18, theslider 16 being adapted to slide into thetrack 18 of anadjacent connector 15. The slider and 16, 18 are dimensioned to provide a secure friction fit once interconnected. The connectors are fixed along their relative axial angles at the vertex of the polyhedron.track formations - The utilisation of the
connector 15 on each tube end has the advantage that two or more tube ends can be interconnected in a very strong and stable bond alleviating the need for a complex welded joint. - The
entire connector 15 is riveted together with blind rivets. This has the advantage that the 16, 18 can be removed to permit reopening of the tube ends and the servicing of the tubes.connector formations - In certain situations it might be appropriate to insert a gasket within the sealing arrangement constituted by the
connector 15 and the welded end of the tube in order to enhance the sealing effect. - The
structure 100 illustrated in FIGS. 2 and 3 are a relatively simple structure that utilises only the basicstructural element 10 illustrated in FIG. 1. However, the basicstructural unit 10 can be used in conjunction with similar yet slightly more complex structural elements to provide more complex structures as is illustrated in FIGS. 6, 7 and 8. - The
structure 200 shown in these drawings utilises three of the basicstructural elements 10 at each of its short ends. - The apex and long sides of the
structure 200 are defined by a pair of opposedstructural elements 204, each of which incorporates a pair of support legs 204.1 and a pair of apical legs 204.2 that extend upwardly towards anapical beam 206 that defines the apex of thestructure 200. The apical legs 10.3 of theelements 10 at each end of thestructure 200 are connected to the ends of thebeam 206 by means as described above. - It will be noted that polyhedral, the
structural element 10 will yield, in combination with similar structural elements, a variety of geodesic structures. In such structures, the apical legs of the structural elements may be secured to the apical legs of adjacent, similar structural elements. In the same way the support legs of the structural elements may be secured to the support legs of adjacent, similar structural elements. If desired the basicstructural elements 10 may be flanked by a slightly modified structural element, each of which differs from the basicstructural element 10 only in the fact that it has an asymmetrical tetrahedral shape. - The structures of the invention, being inflatable, lend themselves to novel uses. For instance, the structure could be internally lit using
light fittings 20 fitted to the insides of the tubes making up the structural elements. In this kind of an application, the fabric of the tubes and the structure as a whole will be chosen for translucency to enhance the lighting effect. - In addition, the structures need not be confined to land. Being inflatable, the structures will float on water to provide a novel staging facility for events and advertising.
- What has been described above are preferred aspects of the present invention. It is of course not possible to describe every conceivable combination of components or methodologies for purposes of describing the present invention, but one of ordinary skill in the art will recognize that many further combinations and permutations of the present invention are possible. Accordingly, the present invention is intended to embrace all such alterations, combinations, modifications, and variations that fall within the spirit and scope of the appended claims.
Claims (10)
1. A structure comprising:
at least three structural units, each of said at least three structural units consisting of three inflatable legs constituting two support legs and an apical leg,
each leg having a free end and an inner end, the inner ends of the three legs being joined at a centrepoint,
the legs being arranged to define a tetrahedron with the three legs lying on three adjacent edges of the tetrahedron and with adjacent pairs of legs lying in planes of three sides of the tetrahedron, and the free ends of the legs defining the fourth side of the tetrahedron;
wherein the apical legs of the units are joined to corresponding legs of the other units at ajoin position.
2. A structure as claimed in claim 1 wherein the three legs of each unit are of the same length.
3. A structure as claimed in claim 1 wherein two of the legs are of the same length and the third leg is of a different length.
4. A structure as claimed in claim 1 wherein each leg is straight.
5. A structure as claimed in claim 1 wherein each leg comprises a plastic reinforced by a woven fabric.
6. A structure as claimed in claim 5 wherein the warp of the fabric is aligned with the tube axis.
7. A structure as claimed in claim 1 wherein a connector unit is provided at the free end of at least one of the legs of each element.
8. A structure as claimed in claim 1 wherein the apical legs are all joined directly together.
9. A structure as claimed in claim 1 wherein some of the apical legs are connected to other legs through an intermediate beam.
10. A structure as claimed in claim 1 wherein the outer ends of the legs are shaped complementary to permit interconnection of the structural elements along the axial angle of the completed structure.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ZA200006289 | 2000-11-14 | ||
| ZA2000/6289 | 2000-11-14 | ||
| PCT/ZA2001/000175 WO2002064917A1 (en) | 2000-11-14 | 2001-11-14 | Inflatable structure |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/ZA2001/000175 Continuation-In-Part WO2002064917A1 (en) | 2000-11-14 | 2001-11-14 | Inflatable structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20040031208A1 true US20040031208A1 (en) | 2004-02-19 |
Family
ID=25588963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/643,247 Abandoned US20040031208A1 (en) | 2000-11-14 | 2003-08-15 | Inflatable structure |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US20040031208A1 (en) |
| EP (1) | EP1346119B1 (en) |
| AT (1) | ATE317481T1 (en) |
| AU (1) | AU2002231380B2 (en) |
| CA (1) | CA2449262C (en) |
| DE (1) | DE60117171T2 (en) |
| WO (1) | WO2002064917A1 (en) |
| ZA (1) | ZA200206637B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080190472A1 (en) * | 2007-02-08 | 2008-08-14 | Jean-Marc Daniel Turcot | Inflatable structure for covering sport utility vehicles, boats and the like |
| US20090084043A1 (en) * | 2007-08-13 | 2009-04-02 | Drs Technical Services, Inc. | Air support structures and methods of erecting same |
| US10465376B1 (en) * | 2016-06-28 | 2019-11-05 | Charles Hoberman | Construction method for foldable polyhedral enclosures |
| US11141888B1 (en) * | 2012-09-14 | 2021-10-12 | Hrl Laboratories, Llc | Hollow polymer micro-truss structures containing pressurized fluids |
| WO2023064974A1 (en) * | 2021-10-18 | 2023-04-27 | Clinical Governance Australia Pty Ltd | Inflatable sports net |
| FR3152158A1 (en) * | 2023-08-18 | 2025-02-21 | Compagnie Generale Des Etablissements Michelin | Elongated element of inflatable revolution with foldable captive air. |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE202007015754U1 (en) * | 2007-11-09 | 2009-03-26 | Vector Foiltec Gmbh | Foil cushion arrangement |
| FR2963631B1 (en) * | 2010-08-03 | 2013-06-07 | Komex | SHELTER WITH INFLATABLE STRUCTURE |
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|---|---|---|---|---|
| US2938526A (en) * | 1958-06-02 | 1960-05-31 | Iii Richard Harrison | Inflatable shelter |
| US3221464A (en) * | 1961-03-17 | 1965-12-07 | Alvin E Miller | Tetrahelical structure |
| US3277479A (en) * | 1963-09-25 | 1966-10-04 | Jr Arthur D Struble | Passive communications satellite |
| US3502091A (en) * | 1968-09-12 | 1970-03-24 | Wendel V Goltermann | Tent supporting frame |
| US3913105A (en) * | 1971-04-05 | 1975-10-14 | Trw Inc | Collapsible self-erecting tubular frame structure and deployable electromagnetic reflector embodying same |
| US3994102A (en) * | 1974-05-06 | 1976-11-30 | Alley Friends | Inflatable element and system |
| US4120024A (en) * | 1976-10-18 | 1978-10-10 | Julian Borisovich Aizenberg | Lighting installation |
| US4723382A (en) * | 1986-08-15 | 1988-02-09 | Haresh Lalvani | Building structures based on polygonal members and icosahedral |
| US4807405A (en) * | 1987-08-20 | 1989-02-28 | Borgquist Ronald B | Geodesic inflatable structure, and methods of constructing and utilizing same |
| US4932169A (en) * | 1989-11-01 | 1990-06-12 | Robert Charbonneau | Inflatable structure |
| US5007212A (en) * | 1990-03-21 | 1991-04-16 | Monty Fritts | Inflatable shelter |
| US5311706A (en) * | 1991-07-19 | 1994-05-17 | Tracor Aerospace, Inc. | Inflatable truss frame |
| US5743049A (en) * | 1994-11-11 | 1998-04-28 | Festo Kg | Support structure for architectural systems |
| US5893237A (en) * | 1998-02-26 | 1999-04-13 | Ryon; Michael J. | Inflatable tent construction |
| US5987822A (en) * | 1997-09-18 | 1999-11-23 | Cyrk, Inc. | Inflatable tent |
| US6061969A (en) * | 1997-02-11 | 2000-05-16 | Leary; Jeremiah E. | Inflatable greenhouse |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2090622A (en) * | 1980-11-13 | 1982-07-14 | Williams Mervyn Ellis | Emergency tent |
| FR2697045B1 (en) * | 1992-10-19 | 1995-01-27 | Semmel Alain | Inflatable shelter with modular elements. |
-
2001
- 2001-11-14 EP EP01991641A patent/EP1346119B1/en not_active Expired - Lifetime
- 2001-11-14 WO PCT/ZA2001/000175 patent/WO2002064917A1/en not_active Ceased
- 2001-11-14 AU AU2002231380A patent/AU2002231380B2/en not_active Ceased
- 2001-11-14 DE DE60117171T patent/DE60117171T2/en not_active Expired - Fee Related
- 2001-11-14 AT AT01991641T patent/ATE317481T1/en not_active IP Right Cessation
- 2001-11-14 CA CA002449262A patent/CA2449262C/en not_active Expired - Fee Related
-
2002
- 2002-01-01 ZA ZA200206637A patent/ZA200206637B/en unknown
-
2003
- 2003-08-15 US US10/643,247 patent/US20040031208A1/en not_active Abandoned
Patent Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2938526A (en) * | 1958-06-02 | 1960-05-31 | Iii Richard Harrison | Inflatable shelter |
| US3221464A (en) * | 1961-03-17 | 1965-12-07 | Alvin E Miller | Tetrahelical structure |
| US3277479A (en) * | 1963-09-25 | 1966-10-04 | Jr Arthur D Struble | Passive communications satellite |
| US3502091A (en) * | 1968-09-12 | 1970-03-24 | Wendel V Goltermann | Tent supporting frame |
| US3913105A (en) * | 1971-04-05 | 1975-10-14 | Trw Inc | Collapsible self-erecting tubular frame structure and deployable electromagnetic reflector embodying same |
| US3994102A (en) * | 1974-05-06 | 1976-11-30 | Alley Friends | Inflatable element and system |
| US4120024A (en) * | 1976-10-18 | 1978-10-10 | Julian Borisovich Aizenberg | Lighting installation |
| US4723382A (en) * | 1986-08-15 | 1988-02-09 | Haresh Lalvani | Building structures based on polygonal members and icosahedral |
| US4807405A (en) * | 1987-08-20 | 1989-02-28 | Borgquist Ronald B | Geodesic inflatable structure, and methods of constructing and utilizing same |
| US4932169A (en) * | 1989-11-01 | 1990-06-12 | Robert Charbonneau | Inflatable structure |
| US5007212A (en) * | 1990-03-21 | 1991-04-16 | Monty Fritts | Inflatable shelter |
| US5311706A (en) * | 1991-07-19 | 1994-05-17 | Tracor Aerospace, Inc. | Inflatable truss frame |
| US5743049A (en) * | 1994-11-11 | 1998-04-28 | Festo Kg | Support structure for architectural systems |
| US6061969A (en) * | 1997-02-11 | 2000-05-16 | Leary; Jeremiah E. | Inflatable greenhouse |
| US5987822A (en) * | 1997-09-18 | 1999-11-23 | Cyrk, Inc. | Inflatable tent |
| US5893237A (en) * | 1998-02-26 | 1999-04-13 | Ryon; Michael J. | Inflatable tent construction |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080190472A1 (en) * | 2007-02-08 | 2008-08-14 | Jean-Marc Daniel Turcot | Inflatable structure for covering sport utility vehicles, boats and the like |
| US20090084043A1 (en) * | 2007-08-13 | 2009-04-02 | Drs Technical Services, Inc. | Air support structures and methods of erecting same |
| US11141888B1 (en) * | 2012-09-14 | 2021-10-12 | Hrl Laboratories, Llc | Hollow polymer micro-truss structures containing pressurized fluids |
| US10465376B1 (en) * | 2016-06-28 | 2019-11-05 | Charles Hoberman | Construction method for foldable polyhedral enclosures |
| WO2023064974A1 (en) * | 2021-10-18 | 2023-04-27 | Clinical Governance Australia Pty Ltd | Inflatable sports net |
| FR3152158A1 (en) * | 2023-08-18 | 2025-02-21 | Compagnie Generale Des Etablissements Michelin | Elongated element of inflatable revolution with foldable captive air. |
| WO2025040860A1 (en) * | 2023-08-18 | 2025-02-27 | Compagnie Generale Des Etablissements Michelin | Folding, rotationally symmetrical elongate element that is inflatable with captive air |
Also Published As
| Publication number | Publication date |
|---|---|
| AU2002231380B2 (en) | 2006-09-07 |
| ZA200206637B (en) | 2004-07-06 |
| WO2002064917A1 (en) | 2002-08-22 |
| EP1346119A1 (en) | 2003-09-24 |
| ATE317481T1 (en) | 2006-02-15 |
| CA2449262C (en) | 2008-03-18 |
| EP1346119B1 (en) | 2006-02-08 |
| CA2449262A1 (en) | 2002-08-22 |
| DE60117171T2 (en) | 2006-11-02 |
| DE60117171D1 (en) | 2006-04-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |
|
| AS | Assignment |
Owner name: WILKINS, THOMAS, NEVADA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:WILKINS, THOMAS;REEL/FRAME:034035/0968 Effective date: 20141010 |