Modular Inflatable Dome Structure

1. Field of the Invention

This invention relates to modular cell structures which can be air supported and reinforced and subsequently stabilized to form a rigid structure or may be originally constructed as a rigid structure.

2. Description of the Prior Art

Dome structures are known in the prior art and are commonly seen in use for athletic arenas, auditoriums and other facilities. Quite often these domes are air inflated. These structures are typically very complex and require a precise design before construction. During construction, the process is very exact and must be performed by a skilled person with an ability to read the detailed instructions. Further, because of the specific design requirements of each individual structure, the costs are relatively high. The present invention overcomes these difficulties by providing a structure easily constructed and relatively inexpensive due to the uniformity of its component parts.

Various proposals have been made in the past for the construction of domed inflatable structures.

Further, the normally existing inflatable system requires a constant supply of air pressure internally within the dome by utilizing large mechanical blowers and other mechanical devices to sustain this structural configuration during usage. It is an object of the invention to overcome this requirement. The normal existing systems also use cable suspension systems to maintain their dome shape. It is an object of this invention to provide a dome structure which does not require a series of cable suspensions to maintain its dome shape.

The modular dome structure comprises a plurality of uniform Y joints and uniform length members. The Y joints preferably have branches forming angles of 120.degree., 120.degree. and 108.degree., and are uniform in the sense that all Y joints in a given structure are identical in configuration (and preferably in dimensions also), although they may differ in space orientation. The Y joints are inter-connected using the uniform length members. Each branch of the Y joint is provided with a means for attaching the members to the Y joints which may consist of a female groove in each branch and a mating male device with a notch or a single ring fitted to mate with the groove. The member material is attached to the Y joint branch by fitting it between the female groove on the branch and the mating device with seals on the grooves.

In accordance with another aspect of the invention, the members of the modular dome structure may be constructed so that they are inflatable. The Y joint branches are provided with valves to control flow rate into each member. After inflation, the inflatable members may be stabilized by vulcanization, hardening through the use of an internal osmostic catalytic reagent, injection or coating.

In accordance with another aspect of the present invention, the modular dome structure is enclosed, using modular panels for covering three panels of the structure. The modular panels consists of two hexagonal and one pentagonal structural covering.

During the construction of conventional dome structures, a vast amount of scaffolding and form work is normally required. Due to modular and inflatable constructions of the present invention, scaffolding becomes secondary in importance, and should result in substantial cost saving in construction.

For a more complete understanding of the present invention and for further advantages and objects thereof, reference is now made to the following description taken in conjunction with the accompanying drawings, in which:

FIG. 1 is a perspective view of a Y joint incorporating the present invention;

FIG. 2 is a detail of a device for attaching the members to the Y joints;

FIG. 3 is a view of a basic structure for a modular dome construction using a pentagonal apex;

FIG. 4 is a view of a basic pentagonal structure with an accompanying circular foundation;

FIG. 5 is a view of a basic pentagonal structure with a pentagonal foundation;

FIG. 6 shows a six panel pentagonal apex structure using the features of the present invention;

FIG. 7 shows an eleven panel structure using a basic pentagonal apex structure;

FIG. 8 shows a sixteen panel pentagonal apex structure using the features of the present invention;

FIG. 9 is a view of a basic structure for a modular dome construction using a hexagonal apex;

FIG. 10 shows a seven panel hexagonal apex structure using the features of the present invention;

FIG. 11 shows a sixteen panel hexagonal apex structure using features of the present invention; and

FIG. 12 shows a modular panel for use with the present invention.

FIG. 13 shows a screwing type end coupling;

FIG. 14 shows members other than tubular type;

FIG. 15 shows a truss member which is a framed structure.

Referring now to FIG. 1, a Y joint 10 is shown with branches 12a, 12b and 12c making space angles of 120.degree., 108.degree. and 120.degree.; thus the Y joints are not planar, but are three-dimensional. Each branch of the Y joint 10 is provided with a female groove 14a, 14b and 14c. Each end of the branches 12a, 12b and 12c are provided with tapered ends 16a, 16b and 16c. In the preferred embodiment, members 18 (FIG. 3) are used which are inflatable by air or gas injection. Each member is of equal length and for purposes of ease of construction and mass production, will be equal in size, thickness and other characteristics, except at special corners and locations where special considerations are required. Control valves 20a, 20b and 20c are incorporated into each branch 12a, 12b and 12c of the Y joint 10 to regulate flow during construction.

Where the members consist of some type of membrane material such as rubber, a sealing device 22 such as that shown in FIG. 2 can be used to attach the member to the Y joint 10. The sealing device 22 is tapered out at its end 24 to engage with the tapered ends 16a, 16b and 16c. The interior of the sealing device 22 has a male notch 26 which mateably engages with the female grooves 14a, 14b and 14c.

Referring now to FIG. 3, a basic pentagonal apex structure can be constructed consisting of 10 members and 10 Y joints. Each member 18 interconnects Y joints 10. To construct the pentagonal apex, the space angle of 108.degree. is used as an interior angle.

The base of the pentagonal apex structure can be supported by a ring connecting the bottom five joints as shown in FIG. 4. This foundation could also be a pentagonal grade beam system as shown in FIG. 5 or a mat or spread footings. This basic structure will have a ceiling height of approximately one-half the length of each member and will form a partial dome. The number of members and joints may be increased in order to increase the height of the dome.

The basic pentagonal structure may be expanded by the addition of members and joints. Where a pentagonal apex is used, an initial secondary row of hexagonal structures will be constructed as shown in FIG. 6. The structure of FIG. 6 consists of six panels made by the modular construction of 25 members and 20 joints. This system raises the height of the ceiling to 1.26 times the length of each member.

An eleven panel pentagonal apex structure as shown in FIG. 7 can be constructed by the further addition of 15 members and 10 joints. This correspondingly raises the ceiling height to 2.03 times the length of each member. Referring to FIG. 8, the further addition of joints and members to a total of 55 members and 40 joints creates a sixteen panel semispherical dome.

Referring now to FIG. 9, a basic hexagonal apex structure is shown. This basic structure consists of 12 members and 12 joints. Each member 18 interconnects Y joints 10 to form interior angles of 120.degree.. This basic unit has a ceiling height of approximately 0.6 times the member length. A secondary row is composed of alternate hexagonal and pentagonal structures as shown in FIG. 10. This seven panel structure is constructed from 27 members and 21 joints. To achieve the semispherical dome as discussed above for the hexagonal apex structure, 54 members and 39 joints are necessary to form the sixteen panel sphere. Of these sixteen panels, ten will be hexagonal and six pentagonal as shown in FIG. 11.

In the preferred embodiment, a member is an inflatable balloon with an original length of 4 to 5 feet. If a rubber material is used for the member material, the member is capable of stretching to as much as 3 to 7 times its original length or approximately 20 feet. Therefore, 20 foot members result, and an area of approximately 7200 square feet can be covered using the modular dome construction of this invention. As the member length is increased, proportionately larger areas are covered. For very large member sizes, truss members can be used to achieve structural safety.

Unlike the conventional triangular combinations which rely on pin connected triangular formations for their stability, the present invention finds its stability in the rigid Y joints, in addition to any rigidity of each member. Once the inflatable structure is constructed, the members may be stabilized by various means. One method of stabilization is by injection of filler material 28 shown in FIG. 2, e.g. air-entrained foam rubber, polystyrene, EPDM, polyurethane latex foam or reactive gas, such as sulphic gas which vulcanizes the rubber membrane and stabilizes the member membrane walls. Further, for moment-resisting composite members, the coating 11 (FIG. 2) utilized outside the inflatable member or the filler 28 used inside the inflatable member can be such a material that it hardens after reaction with the injected gas. If membranes are sufficiently porous, impervious outside coating 11, e.g. Portland Cement or sprayable polyurethane can be used. Butyl rubber and isobutene-isoprene rubber (IIR) are known to have low permeability characteristics to gases and perform favorably to sunlight. Such material can be used without additional treatment where there is no danger of deflation due to accidental puncture or damage to the modular members 18.

Therefore, three methods of stabilization are acceptable with the preferred embodiment. First, after vulcanizing the rubber member material, proper and adequate curing and hardening of the member material sufficient to withstand an exterior load will make it unnecessary to have additional means of protecting each member 18. A second technique involves the injection of air-entrained lightweight material 28 which gains strength as it hardens. Material injected could be either sufficient to fill the full void to form a solid member or partially fill the void in order to form a hollow member. Finally, a third method involves the use of a protective coating 11 on the outside of the member membrane. Many materials could be used such as synthetic rubber material and also non-synthetic inorganic cementing material such as cement, grout, mortar or concrete. Further, combinations of the above three methods may be desirable when different processes act catalytically to strengthen the member membrane without significant increase in cost.

As shown in FIG. 12, a modular panel system is also used to construct the shell for the modular dome structure. The modular panel 60 consists of two hexagonal panels and one adjoining pentagonal panel. As shown in FIG. 12, the modular panel can be constructed from a flat piece of material by making a cut or fold at 62 to obtain the proper angles of 120.degree., 120.degree. and 108.degree.. The fold removes an angle of 12.degree.. Different arrangements in the modular panels can be used to obtain coverage of the modular shell structure including the use of a skylight. Looking at FIG. 7, the use of five modular panels would provide overlapped layer coverage of the hexagonal panels leaving the remaining pentagonal apex structure as the skylight. In FIG. 6, coverage may be obtained with any number of modular panels and a multiple pentagonal apex structure. If as many as five modular panels are used to obtain a two-ply secondary row, the pentagonal apex structure results in a five-ply covering. Particularly suitable panel materials are the teflon coated canvas developed by Owens-Corning Fiberglass Corporation and E. I. du Pont De Nemours & Company. This shell structural covering further acts to provide additional structural strength.

The shell panel system is a self-supporting structure in its entirety. The overlapping feature of the panel system makes it especially suited for reinforcement where needed. Additionally, the panel system can be reinforced either from insIde or suspended in its entirety from connecting joints from the outside.

Referring now to FIGS. 13, 14 and 15, where members 18 are rigid and consist of non-inflatable material, the special considerations required in inflatable members become unnecessary. Under those circumstances, ordinary screw-in type end coupling, shown by FIG. 13 can be engaged. Alternately, angular or built-up members may be used as shown in FIG. 14. For large span distance between joints 10, it becomes necessary to use trussed members as shown in FIG. 15.

Although the preferred embodiment of the invention has been illustrated in the accompanying drawings and described in the foregoing detailed description, it will be understood that the invention is not limited to the embodiments disclosed, but is capable of numerous rearrangements, modifications and substitution of parts and elements without departing from the spirit of the invention.