Transportable and rapidly deployable air supported structure systems and related methods are disclosed. The air supported structure systems include at least one transportable container. The systems also include a flexible outer membrane configured to couple to a base in a substantially air-tight manner. The systems further include at least one air handling mechanism contained within the at least one container configured to force air between the outer membrane and the base to form an enclosure therebetween via internal air pressure. The systems are configurable between a packaged state with the outer membrane contained within the at least one container, and a deployed state with the outer membrane being coupled to the base and the at least one air handling mechanism forming the enclosure via the internal air pressure. The at least one container may form a portion of the base and/or provide for ingress and egress with the enclosure.

Modular enclosures, structures, and components thereof are provided herein. A modular enclosure may include a plurality of enclosure panels and a dormer. A modular assembly may include first and second panels, an elongated structural reinforcing member, and a connector pin connecting the first and second panels. Another modular assembly may include a molded panel including an elongated channel, an elongated reinforcing member positioned in the channel, and at least one fastener configured to retain the elongated reinforcing member within the channel. The elongated reinforcing member may include pins to be retained within blind bores of the elongated channel.

A building system that includes a modular panel with side members, at least one of the side members having an associated coupling for hooked connection with a corresponding shaped fixture of an adjacent structure, the coupling and fixture being adapted to be held together by a locking device that, when engaged, acts to lock the structure and the side member together and, when disengaged, allows for play between the panel and structure in order to free the panel from the structure.

The invention relates to an assembly for incorporating into a solidified construction element, to a construction element comprising such an assembly, and to a method for producing said construction element. According to the invention, the assembly comprises an electronic system (1), said system (1) comprising a chip. It is characterised in that it also comprises a support part (2) provided with a positioning element (3) for said system (1) on one (4) of the so-called system-receiving faces thereof, and on the face (5) opposing said receiving face (4), a distinctive sign for locating the electronic system, which is visible from outside the construction element.

Methods for constructing and a building kit for use thereof are disclosed. The building kit includes a plurality of posts configured for embedding within square apertures of a foundation, wherein the posts have a cross-shaped cross-sectional shape, a plurality of cross-shaped cross-sectional shaped elongated members, a plurality of roof panels, wherein the roof panels include solar cells, and a plurality of wall panels having conforming shape to the cross-shaped cross-sectional shaped elongated members.

A shape-morphing space frame (SMSF) utilizing the linear bistable compliant crank-slider mechanism (LBCCSM). The frame's initial shape is constructed from a single-layer grid of flexures, rigid links and LBCCSMs. The grid is bent into the space frame's initial cylindrical shape, which can morph because of the inclusion of LBCCSMs in its structure. The design parameters include the frame's initial height, its tessellation pattern (including the unit cell bistable elements' placement), its initial diameter, and the resulting desired shape. The method used in placing the unit cell bistable elements considers the principle stress trajectories. Two different examples of shape-morphing space frames are presented herein, each starting from a cylindrical-shell space frame and morphing, one to a hyperbolic-shell space frame and the other to a spherical-shell space frame, both morphing by applying moments, which shear the cylindrical shell, and forces, which change the cylinder's radius using Poisson's effect.

The present invention provides a method for prefabricating, transporting, and rapidly assembling a portable, rigid, dome-shaped structure, with the structural integrity to enable the suspension of extensive hardware and supplies. Said structure would be shaped for acoustic purposes, extremely durable, and allow for extensive climate control. Said structure would be able to be fabricated in a wide range of sizes and shipped to remote locations.

Disclosed is a shelter having a base having base buses; a frame having curves and beams supporting the curves. Each end of the curves are attached to corresponding base bus; each curve is composed of curved elements, the curved element has means for connecting a curve to another curve with a beam. The shelter further has a cable, which cable is for tightening and supporting the frame. Additionally, there is a curved element, and a use of a shelter as a shelter for aircrafts or as a sports hall.

A mounting and stabilization system including a base portion and a mounting portion pivotally coupled to the base portion. The base portion and the mounting portion have a closed configuration where the base portion and the mounting portion are generally parallel with each other and an open configuration where the base portion and the mounting portion are generally perpendicular with each other. The system further includes a collapsible container positioned between the base portion and the mounting portion, where the collapsible container is adapted to expand and receive ballast therein when the base portion and the mounting portion are in the open configuration. The collapsible container is adapted to collapse between the base portion and the mounting portion when the base portion and the mounting portion are in the closed configuration.

A lightweight, compressible panel structure can include a collapsible portion that includes outer facing sections and inner core sections connected by hinge points and/or hinge assemblies. One or more longitudinal support structures can be included to hold the expandable panel structure in its expanded configuration. Methods and apparatus are described.