USRE50203E1 - Airform for facilitating construction of a structure - Google Patents

Abstract

An airform that can be inflated, for example, for facilitating construction of a structure is provided. The airform may include a first portion, a second portion, or multiple other portions, and reinforcement. The first portion may, for example, be configured to be disposed in a first orientation, such as vertically or in a radial profile, when the airform is inflated. The second portion transitioning from the first portion may be configured, for example, to assume an alternate shape and profile, such as a radial shape and profile, when the airform is inflated. The reinforcement may, for example, be provided at a portion of the airform that defines a transition from the first portion to the second portion.

Description

BACKGROUND

1. Technical Field

In general, the subject matter contained herein relates to the field of monolithic dome structures or other permanent structures. More particularly, but not exclusively, the subject matter relates to air-inflated and air-supported forms (“airforms”) used for enabling construction of permanent monolithic dome structures.

2. Discussion of Related Field

Monolithic dome structures may be constructed using airforms. One end of an airform may be attached to a foundation, and thereafter the airform may be inflated. Sustained pressure within the inflated airform is maintained until a polyurethane layer is applied to the wall of the airform, a metal lattice is erected adjacent the polyurethane layer, concrete is applied to the metal lattice and polyurethane, and the polyurethane and concrete layers are permitted to cure, thus forming a self-supported shell structure.

Conventional airforms may extend superiorly in an oblique configuration from the foundation to define a shape that resembles a portion of a sphere. Headroom and/or other conventionally accessible and usable space (for human interaction and storage) at the structure's perimeter along the inside circumference of the airform, and therefore the eventual dome structure, may be adversely affected due to the oblique configuration, thereby negatively affecting the vertically-usable area of the structure. Thus, there is a need to provide a monolithic dome structure with increased usable space.

Further, due to the oblique configuration of the dome structures, it is difficult to install doors, windows, multiply-stacked domes, and other architectural features that are planar or otherwise shaped differently than conventional domes. Certain of such architectural features may be more easily provided if the dome structure has vertical walls. However, conventional domes that have been placed atop vertical walls are often formed of a different material and process as the dome structures. Employing different materials and processes between the dome, vertical support wall, doors, windows, and other features can cause long-term maintenance, water-tightness, or structural problems that might otherwise be avoided with a monolithic single-shell construction. Thus, there is a need to provide a monolithic dome structure that accommodates integrated architectural features having shapes and surfaces that vary from the shape of the dome structure.

Yet, when conventional airforms with transitions that vary from one shape to another (such as from a cylindrical vertical wall to a spherically-domed top) are placed under pressure, wrinkles are formed in the material of the airform along the transition portion between the two shapes. These wrinkles are similar to those seen along the circumference of a mylar birthday balloon. However, such wrinkles, if formed during the process of constructing a habitable structure, can cause suboptimal structural and/or aesthetic defects along any transition portion between two different shapes or surfaces of the structure. Thus, there is a need for a monolithic dome structure having varied shapes and/or surfaces without wrinkles, distortions, or other aberrations formed along transitions portions between such shapes and/or surfaces.

In light of the foregoing discussion, an improved airform and associated processes for facilitating construction of a structure enabling improved space utilization, varied shapes and/or surfaces, and/or no wrinkles, distortions, or other aberrations may be desired.

BRIEF DESCRIPTION OF THE DRAWINGS

Various embodiments of the present invention will now be discussed with reference to the appended drawings. It is appreciated that these drawings depict only typical embodiments of the invention and are therefore not to be considered limiting of its scope.

FIG.1A is a perspective view of an airform in which wrinkles are formed, at the connection of a dome and a vertical wall, as a result of air pressure within the airform;

FIG.1B is a perspective view of the airform ofFIG.1A to which reinforcement, such as a restrained compressive junction stiffener, is provided, and a wrinkle is still present in the airform;

FIG.1C is a perspective view of the airform ofFIG.1B in which the wrinkle has been removed by adjusting the reinforcement, such as by expanding or otherwise lengthening the restrained compressive junction stiffener;

FIG.1D is a perspective view of an alternative embodiment of an airform in which multiple transition portions are provided and reinforced between a cylindrical shape and a dome shape and between two different dome shapes;

FIG.1E is a perspective view of an alternative embodiment of an airform in which multiple transition portions are provided and reinforced between windows frames, a door frame, a hallway or connection portion between one or more monolithic structures, a cylinder, and a dome;

FIG.2A is a perspective view of a reinforcement member;

FIG.2B is a perspective view illustrating engagement between two reinforcement members of the type illustrated inFIG.2A;

FIG.2C is a perspective view of an alternative embodiment of a reinforcement member;

FIG.2D is a partial cross sectional view (A-A) of the engagement illustrated inFIG.2B;

FIG.2E is a perspective view illustrating engagement between two reinforcement members, each having a non-threaded protrusion;

FIG.2F is a cross sectional view (B-B) of the engagement illustrated inFIG.2E;

FIG.3A is a perspective view of a loop, which has a hook and loop type mechanism, adaptable with an airform;

FIG.3B is the loop ofFIG.3A in which loop of the mechanism is separated from the hook of the mechanism;

FIG.3C is a perspective view of a loop, which has a zip fastening mechanism, adaptable with an airform;

FIG.4 is a perspective view of an airform adapted with a reinforcement member which is inflatable;

FIG.5A is a top view of an airform defining a continuous airtight loop or pocket which is inflatable;

FIG.5B is a perspective sectional view along line A-A of the airform ofFIG.5A;

FIG.5C is a detailed perspective sectional view of the pocket provided in the airform ofFIG.5B;

FIG.6A is a top view of an airform having multiple layers of flexible sheets provided along a perimeter of a transition portion;

FIG.6B is a perspective sectional view taken along line A-A of the airform ofFIG.6A;

FIG.7A is a perspective sectional view illustrating an airform with one or more reinforcement members along an inner circumference of the airform;

FIG.7B is a perspective sectional view illustrating several layers of a monolithic structure formed within the airform ofFIG.7A;

FIG.7C is an enlarged cutout view of the layers illustrated inFIG.7B;

FIG.8A is a perspective view of an airform resembling a pyramid;

FIG.8B is a perspective view of an airform resembling a cube; and

FIG.8C is a perspective view of an airform resembling a pyramid disposed over a cube.

DETAILED DESCRIPTION

The present disclosure relates to an airform that can be inflated for facilitating construction of a structure, such as a monolithic structure, including without limitation a monolithic dome structure, or any other shaped structure.

The following description illustrates principles, which may be applied in various ways to provide many different alternative embodiments. This description is not meant to limit the inventive concepts in the appended claims. The principles, structures, elements, techniques, and methods disclosed herein may be adapted for use in other situations where undesirable wrinkles occurring in inflatable structures, such as airforms, are desired to be removed.

While exemplary embodiments of the present technology have been shown and described in detail below, it will be clear to the person skilled in the art that changes and modifications may be made without departing from its scope. As such, that which is set forth in the following description and accompanying drawings is offered by way of illustration only and not as a limitation. In addition, one of ordinary skill in the art will appreciate upon reading and understanding this disclosure that other variations for the technology described herein can be included within the scope of the present technology.

Referring toFIG.1A, anairform100 for enabling construction of one or multiple monolithic dome structures may be provided. Theairform100 may be inflatable and reinforced, and upon inflation and reinforcement, theairform100 may resemble the size and shape of the monolithic dome structure that may be constructed as per a template defined by theairform100.

Theairform100 may have an open end towards its inferior side or inferior end. The open end of theairform100 may be attached or otherwise engaged to a foundation. The open end may be engaged to the foundation such that a substantially airtight engagement may be formed along a perimeter or periphery of the open end. Theairform100 may be equipped with a mechanism to engage theairform100 with an inflating device. The inflating device may pump air into theairform100, to inflate theairform100 to achieve a desired shape. In addition to inflating theairform100, the inflating device may facilitate in retention of requisite pressure inside theairform100 such that the airform retains the desired shape. Theairform100 may provide access to the inside or enclosed area of theinflated airform100 to construction personnel such that, when personnel ingress or egress theairform100, the pressure inside theinflated airform100 is not lost substantially. Such access may be enabled by providing dual doors in theairform100, in which there may a corridor in between the doors. The construction personnel may open and enter a first door, and thereupon close the first door, and subsequently open and enter a second door, and then close the second door. The corridor between the doors may also be inflated.

Theairform100 may include afirst portion102, a second portion104 and at least one reinforcement retainer, such asloops108. Thefirst portion102 of theinflated airform100 may be of cylindrical shape, another dome shape, a singly- or multiply-curved surface around a principal axis, a window, a door, a hallway, an interconnecting structure, and/or any other varied shape or surface. The second portion104 or a superior end of theinflated airform100 may be a radial shape, such as a shape that resembles a portion of a sphere, oval, or quasi-sphere with an irregular, increasing, or decreasing radius of curvature, and may be disposed distally from the foundation when theairform100 is inflated. The second portion104 may alternatively or additionally be of cylindrical shape, another dome shape, a singly- or multiply-curved surface around a principal axis, a window, a door, a hallway, an interconnecting structure, and/or any other varied shape or surface. Thefirst portion102 may transition into the second portion104 at atransition portion106, such that the cylindrical shape transits into the radially-shaped portion. The shape of theairform100 may be based on the desired shape of the monolithic dome structure. Thefirst portion102 of theairform100 may be predominantly vertical when inflated.

Thetransition portion106 may define a curved or smooth transition, as opposed to a sharp transition, when theairform100 is inflated but not reinforced. Further, striations, dimples orwrinkles105 may be formed in thetransition portion106, thefirst portion102 and/or the second portion104. It may be desirable to have a sharp transition from thefirst portion102 to the second portion104, or a transition that defines a sharp or hard angle. Such a transition may facilitate inclusion of doors and windows in the monolithic dome structures, and may also define ample headroom even at the perimeter of theairform100, and therefore the eventual structure. Further, removal of thewrinkles105 may be desired since in certain construction processes theairform100 is retained as an outer shell of the final structure, and wrinkles may be aesthetically unpleasant. Furthermore, even if theairform100 were to be removed after construction, the wrinkles may appear on the outer surface of the structure. Additionally, adjustments may have to be made while spraying concrete ifsuch wrinkles105 are present in theairform100.

Reinforcement may be provided at thetransition portion106 or the portion of theairform100 that may be desired to be thetransition portion106. The reinforcement may segregate theairform100 into thefirst portion102 and the second portion104. The reinforcement may enable defining a transition portion that may have a sharp transition from thefirst portion102 to the second portion104, or a transition that defines a sharp or hard angle. Further, the reinforcement may enable disposing thefirst portion102 vertically or perpendicularly to the foundation, such that ample headroom may be defined even at the perimeter of theairform100. Furthermore, the reinforcement may enable elimination or removal ofunwanted wrinkles105 from theairform100.

Referring toFIGS.1A-2B, theloops108 may be provided along thetransition portion106. Theloops108 may be engaged to thetransition portion106 by techniques such as heat welding, sewing, adhesive, mechanical connection, or other means of attachment. Theloops108 may enable providingreinforcement200 to theairform100 at thetransition portion106. Theloops108 may be provided at predetermined gaps or intervals along the perimeter of thetransition portion106. Theloops108 may be configured such thatreinforcement members201 may be passed through theloops108. Theloops108 may be made of the same or a different material as theairform100.

Thereinforcement200 may be formed of a plurality ofreinforcement members201. A plurality ofreinforcement members201 may be joined together to form thereinforcement200. Referring toFIGS.2A-2B, eachreinforcement member201 may have a curved longitudinal axis. The curvature of the axis may depend on the curvature and shape of theairform100 or thetransition portion106. Further, the number ofreinforcement members201 used to form thereinforcement200 may depend on the length of the circumference or perimeter of thetransition portion106.

Thereinforcement member201 may include one or more mating, locking, or engagement mechanisms at afirst end201a and a second end201b that may enable engagement with anotherreinforcement member201 at each of itsends201a,201b. Thereinforcement members201 may be engaged or arranged to form a closed loop. At thefirst end201a a slot or aperture or bore202 may be provided. At the second end201b aprotrusion204 may be provided. Thebore202 of afirst reinforcement member201 may be configured to receive theprotrusion204 of asecond reinforcement member201. Theprotrusion204 may include threading defined on the external surface of theprotrusion204. Anut206 may be engaged to theprotrusion204. Adjustment of thenut206 may enable controlling the extent of insertion of theprotrusion204 into thebore202. Hence, adjustment of one or moresuch nuts206 may enable alteration of the length of the perimeter of thereinforcement200. Increasing the perimeter may result in stretching or tensioning of thefirst portion102 and the second portion104, which may in turn result in stretching the transition portion and thereby removal ofwrinkles105. Awrinkle105 may be removed by manipulating one ormore reinforcement members201 proximal to thewrinkle105. Referring toFIG.2D, a cross sectional view of the engagement of the threadedprotrusion204 with thenut206 is illustrated.

Referring to,FIGS.2E and2F some of thereinforcement members201 may not have threaded protrusions; rather theprotrusion204 may be non-threaded or may have a plain surface (alternatively and/or additionally, theprotrusion204 may include an irregular, geared, notched, keyed, starred, or other surface). Thenon-threaded protrusion204 may be received by thebore202 of anadjacent reinforcement member201. An interference fit or friction fit may be established between thebore202 and thenon-threaded protrusion204.

Theprotrusion204 may define one or more diametrically extending bores. Alternatively or additionally, a diametrically extending bore may be formed in theprotrusion204. Further, a stop may be inserted through the bore after the position of thenut206 is finalized. Such an arrangement may prevent movement of thenut206 away from the finalized position when the structure is placed under pressure.

Referring toFIGS.1D and1E,multiple transition portions106 may be defined.Reinforcement200 may be provided at each of thetransition portions106. Thetransition portions106 may be concentric (FIG.1D), irregular (FIG.1E), and/or intermittent (FIG.1E). Each of thetransition portions106 may define a same angle of transition. Alternatively, at least one of thetransition portions106 may define an angle of transition that may differ from angle(s) of transition defined at the remaining transition portion(s)106.FIG.1D shows twoconcentric transitions portions106 forming a transition from a vertical cylindrical wall of afirst portion102 to a radial sphere or quasi-sphere of a first dome of a second portion104, and forming a transition from the second portion104 to a smaller and taller radial or quasi-sphere of a second dome of a third portion110.FIG.1E shows anairform100 in whichmultiple transition portions106 are provided and reinforced between at least threewindows frames112, adoor frame114, a hallway orconnection portion116 between one or more monolithic structures, a cylinder orfirst portion102, and a dome or second portion104.

Referring toFIG.2C, asingle reinforcement member210 may form the requisite reinforcement. Thereinforcement member210 may be flexible in nature. Thereinforcement member210 may define a circular configuration. Ends of thereinforcement member210 may be engaged with each other to define a closed loop. One or more mating, locking, or engagement mechanisms may be provided, such as those described previously, which can be manipulated to alter the length of the perimeter of thereinforcement member210.

FIGS.3A-3C illustrate multiple embodiments of loops capable of being opened for insertion of a reinforcement member into the loop, closed around a reinforcement member, and re-opened for removal and/or reclamation of the reinforcement member. Various loop, sleeve or other retention or retainer members may be used to connect transition portions of the airform with a variety of one or more reinforcement members. For example, U.S. Pat. Nos. 6,192,633, 5,893,238, 6,722,084, 4,901,481, 4,031,674, 4,665,935, 7,954,504, 5,628,336, 7,128,078, and 8,615,966 illustrate a variety of tent structures with inflatable or structural members interfacing with sleeves. The elements, principles, structures, techniques, and methods of the aforementioned patents may be combined in any manner with any of the elements, principles, structures, techniques, and methods of the present invention disclosed herein. All of the subject matter and disclosure of the aforementioned patents is incorporated herein by reference in its entirety.

Referring toFIGS.3A-3B, at least one reinforcement retainer, such asloops302, may be provided for receiving reinforcement. Theloops302 may hang from thetransition portion106. One ormore loops302 may include a hook and loop type fastener such that loops can be selectively formed by operating the hook and loop type fastener. A hook mechanism may be provided on or towards a first edge of theloop302 and a loop mechanism may be provided on or towards a second edge, opposite the first edge, of theloop302. Upon engaging the hook and loop mechanism, theloop302 may be formed, which may be configured to receive the reinforcement. The formation of theloop302 may facilitate selective usage of theloops302 based on requirements of the user. Theloops302 may be formed based on user requirements to form theloops302 to enable reception of the reinforcement. In an embodiment, some of the loops may be fastened to theairform100 by adopting hook and loop mechanisms. The position of such loops relative to the airform may be altered based on user requirements.

Referring toFIG.3C, at least one reinforcement retainer, such asloops304, may be provided for receiving reinforcement. One ormore loops304 may include a zip fastening mechanism such that the loops can be selectively formed by operating the zip fastening mechanism. Theloops304 may be selectively formed by operating the zip fastening mechanism. The zip fastening mechanism may be configured such that one end of theloop304 may include one row of the zip fastening mechanism and the other end of theloop304 may include another row with protruding teeth. The ends may be brought together and a slider of the zip fastening mechanism may be slid over the two rows, thereby interlocking the rows and forming theloop304. In an embodiment, a zip fastening mechanism may be used to fasten the loops to theairform100. The zip fastening mechanism may be configured such that, one row of the zip fastening mechanism with protruding teeth may be provided on theairform100 and the other row of the zip fastening mechanism with protruding teeth may be provided on theloops304. The slider of the zip fastening mechanism may be slid over the two rows, thereby interlocking the two rows and attaching theloop304 to theairform100.

Referring toFIG.4, aninflatable reinforcement member400 may be provided. Thereinforcement member400 may be a flexible pipe or tube whose ends may be engaged to define a closed loop. Thereinforcement member400 may include a valve402 which may be adapted with an inflating device to inflate thereinforcement member400. Thereinforcement member400 may be inflated using fluid, which may include liquid and/or gas. Wrinkles may be removed by manipulating or altering the pressure created by the fluid. The pressure created by the fluid may vary from the pressure at which the airform is retained. The pressure created by the fluid may be higher compared to the pressure at which the airform is retained.

Referring toFIGS.5A-5C, a single continuous airtight reinforcement retainer, such as aloop502, tube, or pocket, may be provided along the perimeter of atransition portion503 of anairform500. Theloop502 may include amechanism504, such as a valve, for connecting theloop502 to the inflating device. Theloop502 may be configured to be in inflated using fluid. Theinflated loop502 may function as the reinforcement to theairform500. Wrinkles may be removed by manipulating or altering the pressure created by the fluid. The pressure created by the fluid may vary from the pressure at which the airform is retained. In order to remove the wrinkles, the pressure created by the fluid may be higher compared to the pressure at which the airform is retained.

Referring toFIGS.6A-6B, areinforcement602 in the form of one or more (e.g., multiple) layers of flexible sheets may be provided in theairform600. The flexible sheets of material may be formed of any material compatible with theairform600, and such sheets may be heat welded, glued, sewn, hermetically sealed, or otherwise secured in an air-tight and water-tight connection to each other. Thereinforcement602 may be provided along the perimeter of atransition portion606 of theairform600. The multiple layers of flexible sheets provided along the perimeter of thetransition portion606 of theairform600 may increase the thickness and stiffness of the area along the perimeter of thetransition portion606. The flexible sheets may be made of the same or different material as theairform600 or its various portions. Various portions of theairform600 andtransition portion606 may have materials of different rigidity and strength in order to help provide structural stiffness to the airform and transition portion capable of minimizing or removing wrinkles or other surface aberrations. The multiple layers of flexible sheets reinforce the area around thetransition portion606, which may be prone to wrinkles Upon inflating theairform600, the presence ofreinforcement602 along the perimeter of thetransition portion606 restricts or limits the formation of wrinkles in theairform600.

The first portion and the second portion and any other multiple portions of the airform may be configured to define a singular or monolithic airform. The reinforcement may be removed from the airform after a solid structure is built along the airform, and the structure is capable of retaining the desired shape absent air pressure within the air form.

Referring toFIGS.7A through7C, theairform100 may include at least one reinforcement retainer, such asloops108, along the inner circumference of atransition portion106 on the inside surface of theairform100. Theloops108 may retain one ormore reinforcement members201 orreinforcement hangers201 on the inner surface of theairform100. Any portion of any inner surface of theairform100 may include any number of reinforcement retainers and/or reinforcement members. Thereinforcement200 described on the exterior surface of the airform in any or all of the various figures of this disclosure may be inverted, that is, placed on the interior surface instead of the exterior surface, of the airform. For example, thereinforcement200 shown and described on the exterior surface of the airform with reference toFIGS.1B,1D,1E,3A-3C,4, and8A-8C may be provided asreinforcement200 on the inner surface or interior of the airform at any location of the airform.

The structure built as per the template of theairform100 may include several layers formed of different materials. Theairform100 may be inflated and reinforced to remove wrinkles or striations, if any. Upon inflation of theairform100, the construction process may be begun either from the inside of the inflated airform or from the outside of theinflated airform100, based on a chosen method of construction. If construction is carried out from the inside of theinflated airform100, theairform100 may form the outer layer of the structure. Alternatively, if construction is carried out from the outside of theinflated airform100, theairform100 may form the inside layer of the structure. The structure may include theairform100, a first layer of sprayedpolyurethane foam702,rebar hangers704 embedded in the first layer of polyurethane foam, a second layer ofpolyurethane foam706 as desired to embed and retain therebar hangers704 or otherwise provide additional insulation or structural support, steel, metal, or otherrigid reinforcement708 arranged as per design specification and concrete710 of desired thickness sprayed over thesteel reinforcement708.

The first layer ofpolyurethane foam702 may be sprayed onto to theinflated airform100, permittingrebar hangers704 to extend through the first layer ofpolyurethane foam702 from thereinforcement hangers201. Additional oralternative rebar hangers704 may be embedded in the first layer of sprayedpolyurethane foam702 at suitable positions. Therebar hangers704 facilitate in attaching the steel reinforcement to theairform100. The second layer ofpolyurethane foam704 may be sprayed onto the earlier layers, thereby embedding therebar hangers704. Upon embedding therebar hangers704,steel reinforcement708 may be arranged as per design specification, considering the doors, windows, vents and/or chimney, among others, to be provided in the structure.Concrete710 of desired thickness may be sprayed to complete the structure. Upon setting of the concrete710, the structure may be complete. Theairform100 may be retained under a suitable pressure until the concrete sets. Theairform100 may be separated from the structure and reused.

Other internal and/or external structures in addition to and/or instead ofrebar hangers704,steel reinforcements708, and/orconcrete710 may be used in conjunction with the structures, features, benefits, methods, steps, and processes of the present disclosure. For example, a furring strip or other internal and/or external structure may be placed along the internal and/or external vertical, horizontal, circumferential, spherical, quasi-spherical, irregular, and/or other surface(s) of the airform. The furring strip (of wood, PVC, or other penetrable and/or fixable material), or other structure, may then be used to anchor or otherwise affix auxiliary structures or materials (such ashangers704,steel reinforcements708, concrete710, siding, flashing, rain gutter, and/or other structures).

Referring toFIG.8A, anairform802 may be provided to resemble a pyramid.Reinforcement804 may be provided at one ormore transition portion806 so that the desired transition is achieved and/or wrinkles if any may be removed.

Similarly, referring toFIG.8B, anairform812 may be provided to resemble a cube.Reinforcement814 may be provided at one ormore transition portion816 so that the desired transition is achieved and/or wrinkles if any may be removed.

Likewise, referring toFIG.8C, anairform822 may be provided to resemble a pyramid disposed over a cube.Reinforcement824 may be provided at one ormore transition portion826 so that the desired transition is achieved and/or wrinkles if any may be removed. In light of this disclosure, other shapes may be contemplated, andFIGS.8A to8C are merely examples of a variety of curved or linear shapes, ellipses, etc. that may be employed.

FIGS.8A to8C includestraight reinforcements824 that may buckle at certain weak inflection points along the length of the reinforcement members and under the internal air pressure of a fully-inflated and pressurized airform. In other embodiments with straight sections, sigmoid sections, or other sections of reinforcement members that do not follow the natural profile and geometry of a fully-inflated and pressurized airform, such as the examples inFIGS.8A through8C, it may be preferable to further strengthen such reinforcement members. Reinforcement members may be strengthened by using stronger, more rigid materials (such as metal alloys or carbon fiber materials) to form the reinforcement members and/or by using additional structure on or surrounding each of the reinforcement members (such as increased diameter, straight or bent I-beam geometries, triangular or truss like geometries, supplemental sleeves, or other structures and geometries). By providing additional strength along at least a portion of each reinforcement member where such member is likely to bend, buckle, or otherwise deform when the airform changes shape under pressure, the airform is more likely to retain a desired shape influenced by the reinforcement members whenever such members are present and adequately strengthened.

In an embodiment, reinforcement may be provided for reinforcing the airform and thereby remove wrinkles that may be formed upon inflating the airform. The reinforcement provided may be such that shape of the reinforcement may facilitate collection of water which may drip down from the top of the structure. The reinforcement may function as a rain gutter around the structure and facilitate collection and disposal of rain water dripping from the roof of the structure.

The reinforcement members may be made of materials, such as steel, PVC pipes, wires, cables and rigid canvas, among other suitable materials. The airform may be made of material capable of withstanding inflation and/or providing protection against nature's elements.

In an embodiment, a design of a structure or a monolithic dome structure to be constructed may be finalized. An airform may be manufactured to complement the design of the structure. The airform may be manufactured by joining several sheets which may be joined using techniques such as heat welding. Foundation may be prepared for the structure. An inferior end of the airform may be engaged to the foundation. Subsequently, the airform may be inflated and a requisite pressure may be retained inside the airform. Reinforcement may be provided to the airform, and the reinforcement may be adjusted or manipulated such that wrinkles, striations, dimples or other surface aberrations, if any, formed on the airform are removed. The airform may be sprayed and other preparation steps may be carried out to ready the airform for rest of the construction steps. The construction steps may include spraying a polyurethane foam or other insulation against the inside surface of the airform and/or erection of steel or other reinforcement inside the airform or outside, depending on the chosen construction technique. Concrete of desired thickness may be sprayed over the steel reinforcement, insulation, and/or airform. Once the concrete structure is capable of retaining the desired shape, mechanisms that may be used to retain the airform at requisite pressure may be turned off. The airform may be left on the structure or may be reused.

Claims (26)

What is claimed is:

1. An inflatable airform that can be inflated for facilitating construction of a permanent structure, the airform for building construction, comprising:

a first portion comprising a first complete surface of revolution when the airform is inflated, wherein the first portion is configured to be disposed in a first shape and to form a first profile when the airform is inflated;

a second portion comprising a second complete surface of revolution when the airform is inflated, wherein the second portion is configured to be disposed in a second shape and to form a second profile when the airform is inflated;

wherein at least one of the following is present: the first complete surface of revolution is configured to be different than the second complete surface of revolution, the first shape is configured to be different than the second shape, or the first profile is configured to be different than the second profile, when the airform is inflated;

at least one transition portion comprising at least one portion of the airform that defines a transition from the first portion to the second portion when the airform is inflated, wherein the first portion and the second portion share at least one common radius of revolution at the transition when the airform is inflated;

at least one reinforcement comprising at least one reinforcement member provided located at the at least one transition portion, wherein the at least one reinforcement enables defining the defines a transition point from the first portion to the second portion and maintaining maintains the first shape and the second shape when the airform is inflated; and

at least one reinforcement retainer configured to retain the at least one reinforcement member at the at least one transition portion;

wherein the at least one reinforcement comprises a plurality of reinforcement members; and

wherein the airform is configured to facilitate the construction of a permanent structure.

2. The airform ofclaim 1, wherein the at least one reinforcement comprises a plurality of reinforcement members.

3. The airform of claim21, wherein the plurality of reinforcement members are configured to be engaged to each other to form a closed loop encircling the at least one transition portion, wherein the closed loop comprises a perimeter.

4. The airform ofclaim 3, wherein said engagement is the plurality of reinforcement members are configured to be manipulated to alter the length of the perimeter of the closed loop.

5. The airform ofclaim 1,

wherein the first portion further comprising a first at least one radius of curvature when the airform is inflated;

wherein the second portion further comprising a second at least one radius of curvature when the airform is inflated; and

wherein at least one radius of curvature of the second at least one radius of curvature is different than at least one radius of curvature of the first at least one radius of curvature at the at least one transition portion when the airform is inflated.

6. The airform ofclaim 1, further comprising at least one window and at least one door.

7. The airform ofclaim 1, further comprising a third portion configured to be disposed in a third shape when the airform is inflated, wherein the at least one transition portion further comprising at least one portion of the airform that defines a transition from the second portion to the third portion when the airform is inflated.

8. The airform ofclaim 1, wherein the at least one transition portion comprises a plurality of portions of the airform that define transition from the first portion to the second portion, wherein at least two of the plurality of portions of the airform are configured to be reinforced.

9. The airform ofclaim 1, wherein the first shape is cylindrical.

10. The airform ofclaim 1, wherein the second shape is doubly curved.

11. A method of preparing an airform that can be inflated for facilitating construction of a permanent structure, the method comprising:

inflating the airform ofclaim 1, such that the first portion of the airform is disposed in said the first profile, and the second portion of the airform assumes said the second profile, which the second profile is different to than the first profile, then;

manipulating the at least one reinforcement at the at least one transition portion to remove at least one surface aberration extending across the at least one transition portion.

12. The method ofclaim 11, wherein providing manipulating the at least one reinforcement comprises assembling a the plurality of reinforcement members along the at least one transition portion of the airform.

13. The method ofclaim 11, wherein manipulating the at least one reinforcement comprises altering a perimeter of the at least one reinforcement for removing the at least one surface aberration.

14. The method ofclaim 11, wherein manipulating the at least one reinforcement comprises altering a dimension of the at least one reinforcement at least proximal to the at least one surface aberration.

15. The method ofclaim 11, wherein the second shape is doubly curved.

16. An monolithic architectural structure, comprising:

a cement concrete layer;

a structural layer of metal adjoining the cement concrete layer;

insulation adjoining the structural layer of metal; and

the airform ofclaim 1 adjoining the insulation;

wherein the first portion of the airform is configured to be engaged to a foundation;

wherein the second portion of the airform is configured to be disposed distally from the foundation when the airform is inflated; and

wherein the at least one reinforcement is configured to be manipulated for removing one or more striations, if any, at the at least one transition portion, when the airform is inflated.

17. The monolithic architectural structure ofclaim 16, wherein,

the first portion extends perpendicularly from the foundation to the at least one reinforcement;

the second portion extends superiorly from the at least one reinforcement; and

the second shape is doubly curved.

18. The monolithic architectural structure ofclaim 17, wherein the at least one reinforcement comprises a rigid material and is configured to be operable for manipulating a the material under tension at the at least one transition portion.

19. The monolithic architectural structure ofclaim 16, wherein the at least one reinforcement comprises a plurality of reinforcement members are configured with ends that engage to define a closed loop, wherein engagement of the ends is configured to be manipulated to alter a dimension of the closed loop.

20. The airform ofclaim 7, wherein the third shape is doubly curved.

21. An architectural structure, comprising:

a concrete layer;

a structural layer comprising metal adjoining the concrete layer;

an airform integrally connected to the structural layer, the airform comprising:

a first portion having a first complete surface of revolution when the airform is inflated to form a first profile;

a second portion having a second complete surface of revolution when the airform is inflated to form a second profile, wherein the first and second profiles are different;

a plurality of reinforcement members located at a transition between the first and second portions, wherein the first and second portions share a common radius of revolution at the transition between the first and second portions; and

one or more retainers configured to retain the plurality of reinforcement members;

wherein the airform is configured so as to be capable of facilitating construction of a permanent structure, and the plurality of reinforcement members define the transition from the first portion to the second portion and maintain the first profile and the second profile when the airform is inflated.

22. The architectural structure ofclaim 21, further comprising insulation adjoining the structural layer.

23. The architectural structure ofclaim 21, further comprising a foundation operably connected to the first portion.

24. A method of preparing an architectural structure, comprising:

providing an airform configured so as to be capable of facilitating construction of a permanent structure, the airform comprising:

a first portion having a first complete surface of revolution when the airform is inflated to form a first profile;

a second portion having a second complete surface of revolution when the airform is inflated to form a second profile, wherein the first and second profiles are different;

a reinforcement member located at a transition between the first and second portions, wherein the first and second portions share a common radius of revolution at the transition between the first and second portions; and

one or more retainers configured to retain the reinforcement member; and

inflating the airform;

wherein the reinforcement member defines the transition from the first portion to the second portion and maintains a first shape and a second shape when the airform is inflated; and

wherein the method further comprises assembling a plurality of reinforcement members along the transition of the airform.

25. The method ofclaim 24, further comprising removing at least one surface aberration extending across the transition.

26. The method ofclaim 24, further comprising altering a perimeter of the reinforcement member.

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