The present invention is in the field of modular structures, assembled by way of fastening or attached means, whose purpose is to be used as base support structures for various applications, particularly connecting systems involving plastic or aluminum containers, recipients, bottles or vessels. Particularly, the invention comprises an omnidirectional construction system that includes connectors and terminals to be attached to containers with threaded openings or flat openings and container bases, to which various types of connectors may be attached to.

A joint connector comprising a hub, two registration caps, a bolt assembly or similar means of connecting the components, and at least two wing pairs. The joint connector is adaptable and thus is capable of creating a variety of different joint networks. Joint connectors can be arranged to connect panel frames and panels for regularly faceted structures and asymmetrical or irregularly shaped structures.

A space frame is provided having a first set of nodes located along a first surface and a second set of nodes located along a second surface, and a unitary cell. The second surface non-intersecting the first surface. The unitary cell comprises at least four continuous web elements and extending in three dimensions. The unitary cell spans at least two nodes of the first set of nodes and at least two nodes of the second set of nodes.

A novel system and related methods for sequentially deploying, in automated or semi-automated fashion, a strip of a plurality of truss bays with integral solar panels from a moving carrier onto a surface being traversed, resulting in a long, contiguous truss structure laid upon on the surface. The solar panels are angled at a predetermined orientation for solar operation at the deployment location. The carrier is easily and quickly reloaded with another set of truss bays for repeated deployment of a series of strips of solar truss structures in a solar array. The solar array thus is constructed in substantially less time and with substantially less labor that conventional support racking in the filed using prior art piece-wise assembly operations.

A strut-and-node truss design that is applicable to all space frame structure designs can be made with using robotic (semi-autonomous and/or fully autonomous) or telerobotic assembly/joining. Nodes can include a 2-dimensional weld path in an effort to reduce the complexity of having to weld in 3-dimensions. Furthermore, each strut to node connection can be concentrated in a small area where each weld can be performed robotically from a fixed position that only requires the robotic weld head to swivel in a small operating window to reach each joint.

A triangular pyramidal supporting structure, which has the shape of a tetrahedron made up of elements to form a primary plane, and sloping elements (projecting slopingly upwards from the primary plane and meeting in a junction point. The joining of the elements of the tetrahedron is governed by imaginary lines that are determined by the primary plane. Further, a system has at least four tetrahedrons, and a method for providing the tetrahedron and the system are described.

A space frame is provided having a first set of nodes located along a first surface and a second set of nodes located along a second surface, and a unitary cell. The second surface non-intersecting the first surface. The unitary cell comprises at least four continuous web elements and extending in three dimensions. The unitary cell spans at least two nodes of the first set of nodes and at least two nodes of the second set of nodes.

An assembly for integrating an elongate structural member is provided. The elongate structural member includes a first end portion, a second end portion, and an elongate mid-portion that extends between the first and the second end portions. The first end portion is within a first plane and the second end portion within a second plane, and the first and the second planes are offset and parallel to each other. The elongate mid-portion is sloped between the first and the second planes. each of the first and the second end portions defining therein a polygonal hole. Multiple elongate structural members may be used to assemble a lattice structure.

A lattice structure comprising a series of connecting rings or half-rings on which a series of orienting elements are secured. The orienting elements being equipped with holes and a slot in which the connecting rings or half-rings are disposed, as well as comprising profiles that are solidly connected using joining elements that extend through holes in the profiles.

A lattice structure comprising a series of connecting rings or half-rings on which a series of orienting elements are secured. The orienting elements being equipped with holes and a slot in which the connecting rings or half-rings are disposed, as well as comprising profiles that are solidly connected using joining elements that extend through holes in the profiles.