MODULAR CONSTRUCTION SYSTEM.
Patent Information
- Application Number
- MX2021010784
- Authority / Receiving Office
- MX · MX
- Patent Type
- Patents
- Current Assignee / Owner
- Filing Date
- 2021-09-07
- Publication Date
- 2026-02-25
- Estimated Expiration
- 2041-09-07
AI Technical Summary
Existing construction systems are limited in the number of geometries they can form due to the finite quantity, shape, and dimensions of their elements, and the union by friction results in inadequate structural resistance to static and dynamic forces.
A modular construction system where components have dimensions proportional to a reference element, allowing interchangeable modules to be coupled in various arrangements and orientations, with assembly holes and inserts ensuring structural integrity.
Enables the assembly of structures with diverse geometries and improved resistance to static and dynamic loads by using components with proportional dimensions and strategic hole placements.
Smart Images

Figure MX431861B0
Abstract
Description
MODULAR CONSTRUCTION SYSTEM. TECHNICAL FIELD OF THE INVENTION. The present invention belongs to the field of construction systems, which have a plurality of elements that are coupled to form a desired structure where said elements are associated by the proportions in their dimensions, which allows the exchange in the location or orientation of said components as required by the structure that is to be integrated. OBJECT OF THE INVENTION. The object of the present invention is to have a construction system comprising a series of interchangeable elements where all of them are related by different proportions in their dimensions, defined from the same reference element, which allows the construction of different geometric or geodesic figures with the same number of components and even the integration of modules that can be interconnected and interchanged randomly, thanks to the fact that the dimensions of the elements that make them up have a proportion relative to said reference element, regardless of their geometry, which allows the construction of various structures as desired. BACKGROUND. Construction systems are known that comprise modular elements to form structures from a number of interchangeable elements, such as the MULTIMODEL brand construction system, which is known from the website https: / / www.imaqinarium.mx / set-para-armarproyectos-de-bricolaje-multi-model-64-ocs-76382.htm, which teaches a construction system for the formation of 11 different structures from the assembly of panels and geodesic figures by screws. Document GB 1,060,200, dated March 1, 1967, describes a modular system for mosaics, comprising square modular elements. One face of each element has four pins, the spacing of which is equal to the diameter of the pins. Pins from other square modular elements can be inserted between these pins, creating a frictional connection. The opposite face of each modular element also features a cylindrical cavity of a specific diameter and depth equal to the length of the pins. ML / a / ZUZ l / U 1 U / O4 Other inventions of construction systems can be found in documents CN109069938A, EP0463281A1, GB2355672A, GB2502546A, US5938566A, US2013072086A1, US2013195547A1, US2015017377A1, US2018071651A1, US2020139259A, WO2018226499A1, WO2019109466A1. TECHNICAL PROBLEM TO BE SOLVED. Although construction systems using panels and prismatic bodies are known, these systems have a finite number of possible structural geometries, since the quantity, shape, and dimensions of their elements are geared towards constructing structures with predetermined forms. Furthermore, the stacking of elements in known construction systems limits the creation of internal spaces within the structures, and frictional joints also limit the structural resistance to static and dynamic stresses. BRIEF DESCRIPTION OF THE INVENTION. To solve the problem of the limitation of the number of geometries in the construction of structures due to dependence on the number of available elements, as well as to have an assembly with structural resistance capable of withstanding static and dynamic loads during its use, a construction system has been developed in which its components have a dimension that is proportional to a reference element, which allows the assembly of said elements to constitute interchangeable modules so that the geometries that can be developed only depend on the number of elements since their dimensions allow them to be coupled in different arrangements and in different orientations. The invention consists of establishing a reference piece with defined dimensional characteristics. From this reference piece, panels and other prismatic pieces are developed with dimensions proportional to said reference piece. This allows for the integration of modules with interchangeable elements, so that different structures can be obtained from the number of elements that make up the modules, in an indeterminate number and geometry. Assembly holes are located on the surface of the panels, and their placement is also related to the dimensions of the reference piece. The combination of the dimensions of each of the structural elements with the location of the assembly holes allows for the integration of modules with diverse configurations, so that shapes can be obtained as required during assembly. ML / a / ZUZ l / U 1 U / O4 structure, since its shape is defined by the user, with internal spaces that form tubular prismatic structures, which improves resistance to the stresses that occur at the time of its construction and use. BRIEF DESCRIPTION OF THE FIGURES. Figure 1 Shows the top front perspective view of a modular corner cube type cube. Figure 2 - Shows the lower rear perspective view of the corner cube. Figure 3 - Shows the schematic front view of the corner cube. Figure 4 - Shows the rear schematic view of the corner cube. Figure 5 - Shows the top front perspective view of a sliding cube-type modular cube. Figure 6 - Shows the lower rear perspective view of the sliding cube. Figure 7 - Shows the schematic front view of the sliding cube. Figure 8 - Shows the schematic side view of the sliding cube. Figure 9 - Shows the top front perspective view of a modular cross cube type cube. Figure 10 - Shows the lower rear perspective view of the cross cube. Figure 11.- Shows the schematic front view of the cross cube. Figure 12 - Shows the left side schematic view of the cross cube. Figure 13.- Shows the top front perspective view of a modular prism of the union prism type. Figure 14 - Shows the lower rear perspective view of the junction prism. Figure 15 - Shows the schematic front view of the prism union. Figure 16 - Shows the lower schematic view of the joining prism. Figure 17,- Shows the schematic side view of the joining prism. Figure 18.- Shows the upper left front perspective view of a multiple prism type modular prism. Figure 19,- Shows the lower left rear perspective view of the multiple prism. Figure 20,- Shows the lower right front schematic view of the multiple prism. Figure 21 A.- Shows the top schematic view of the multiple prism. Figure 21B.- Shows the schematic front view of the multiple prism. Figure 22,- Shows the rear schematic view of the joining prism. Figure 23.- Shows the left side schematic view of the multiple prism. Figure 24,- Shows the right side schematic view of the multiple prism. IVIA / a / ZUZ l / UIU / O4 Figure 25.- Shows a second schematic rear view of the multiple prism. Figure 26.- Shows a second front perspective view, top left, of the multiple prism. Figure 27 - Shows the front view of a quadrangular panel. Figure 27A.- Shows the side view of the quadrangular panel. Figure 28.- Shows the front view of a larger rectangular panel. Figure 29.- Shows the front view of a medium rectangular panel. Figure 30.- Shows the front view of a smaller rectangular panel. Figure 31.- Shows the front view of a triangular panel. Figure 32 - Shows the front view of a group of modular canes. Figure 33 - Shows the perspective view of a modular bearing bar. Figure 34 - Shows the front view of the modular bearing bar. Figure 35.- Shows the top view of the modular bearing bar. Figure 36.- Shows the side view of the modular bearing bar body. Figure 37 - Shows the perspective view of a group of interconnecting accessories. Figure 38 - Shows the perspective view of a group of joining elements. Figure 39.- Shows the top front perspective view of a modular polyhedron. Figure 40.- Shows the lower rear perspective view of the modular polyhedron. Figure 41.- Shows the top schematic view of the modular polyhedron. Figure 42 - Shows the front view of a textile canvas. Figure 43,- Shows the perspective view of an alternative structure built with the modular construction system of the present invention. Figure 44,- Shows the exploded perspective view of a second alternative structure built with the modular construction system of the present invention. Figure 45.- Shows the perspective view of a second alternative structure built with the modular construction system of the present invention. DETAILED DESCRIPTION OF THE INVENTION. The present modular construction system (01) comprises modular cubes (100), modular prisms (200), modular panels (300), modular rods (400), at least one modular bearing bar (500), and interconnecting accessories (600), as well as joining elements (700). ML / a / ZUZ l / U 1 U / O4 as an alternative, there are also modular polyhedra (800). Complementarily, there are textile canvases (900) for applications that will be described later. Modular cubes (100) are bodies made of a natural fiber material such as wood, or of a polymer or metallic material, with dimensions from which the dimensions of the other elements that make up the construction system are determined. In each modular cube (100), a constant distance is defined for each of its edges, determined by the variable “a”. Preferably, the edges and vertices of the modular cubes (100) are beveled to eliminate stress concentration points that could potentially damage their geometry from impact or cause injuries during handling.These modular cubes (100) are grouped into various categories based on their application in the modular construction system (01) of the present invention, such that there are corner cubes (110), sliding cubes (120), and cross cubes (130); all of them of the same dimension, that is, they have the same value of the variable "a" for the length of their edges in the same modular construction system (01). Each of the groups is identified primarily by the number and type of holes found in each of them, and, for practical purposes, they are of different colors. The manufacturing process for the modular cubes (100) is one of the known processes, such as machining, material injection, or blow molding. Each corner cube (110) comprises perforations that allow its assembly with modular panels (300) as well as receiving sections of modular rods (400) as shown in Figures 1 to 4. For this purpose, there is an end corner hole (111) centered on three adjacent faces of the corner cube body (110). Each end corner hole (111) has a diameter that allows the sliding projection of a distal end of a modular rod (400). Additionally, there is an insert corner hole (112) centered on the three remaining adjacent faces of the corner cube body (110). These inserts are also centered on the respective face of the corner cube body (110) where they are located and coaxially aligned with an end corner hole (111) on the opposite face.A corner insert (113) is housed and retained in each of said insert corner holes (112), with features that allow it to receive a joining element (700) for joining the elements that make up the modular construction system of the present invention. Both the end corner holes (111) and the corner holes of. IVIA / a / ¿U¿ l / UIU / O4 insert (112) are blind holes, so that there is a bottom wall in each hole. The group of corner cubes (110) are painted in a first color for easy identification. Each dowel cube (120), as shown in Figures 5 through 8, comprises perforations that allow its assembly with modular panels (300) and the receipt of modular rod sections (400). These dowel cubes (120) can also be slid along the length of the modular rods (400) by means of an end dowel hole (121) centered on two adjacent faces of the dowel cube body (120). Each end dowel hole (121) has a diameter that allows the sliding projection of a distal end of a modular rod (400). Additionally, an insert dowel hole (122) is centered on two adjacent faces of the corner cube body (120), aligned coaxially with an end dowel hole (121) on the opposite face.A pin insert (123) is housed in each of the insert pin holes (122), with features that allow it to receive a connecting element (700) for joining the elements that make up the modular construction system of the present invention. A rod pin hole (124) projects centrally along the entire length of the pin hub body (120), between the two remaining opposite faces of the pin hub body (120), perpendicular to the coaxial axes between the end pin holes (121) and the insert pin holes (122), to receive a modular rod (400). The rod pin hole (124) has a diameter that allows the pin hub (120) to move along the length of a modular rod (400). Both the end pin holes (121) and the insert pin holes (122) are blind holes. The group of pin cubes (120) are a second color for easy identification. Each cross cube (130), as shown in Figures 9 to 12, comprises perforations that allow its assembly with modular panels (300) and the reception of modular rod sections (400). For this purpose, an end cross hole (131) is centered on four opposite faces of the cross cube body (130). Each end cross hole (131) has a diameter that allows the sliding projection of a distal end of a modular rod (400). Additionally, an insert cross hole (132) is centered on the two remaining opposite faces of the cross cube body (130), where a cross insert (133) is rigidly housed and retained. These inserts are also centered on the respective face of the cross cube body (130) where they are located and are therefore coaxially aligned with each other. A cross insert (133) is housed in said cross insert bore ML / a / ZUZ l / U 1 U / O4 (132), with features that allow it to receive a joining element (700) for joining the elements that make up the modular construction system of the present invention. The coaxial alignment of the end cross holes (131) creates continuous passages through which it is possible to slide the length of the modular rods (400) in a pair of them aligned in such a way that the distal ends of two other modular rods (400) are housed in each of the remaining end cross holes (131) until they contact the initially installed modular rod (400). Alternatively, these end cross holes (131) are blind holes, so that each one has a bottom wall. The insert cross holes (132) are also blind holes, so that each one has a bottom wall.The group of cross cubes (130) are painted in a third color for easy identification. Each end corner hole (111), end pin hole (121), cane pin hole (124) and end cross hole (131) are of the same diameter to fit with the diameter of the modular canes (400) in a sliding manner. Each corner insert hole (112), pin insert hole (122) and cross insert hole (132) are of the same diameter and depth to receive the respective corner insert (113), pin insert (123), and cross insert (133). The modular prisms (200) are bodies made of a natural fiber material such as wood, or of a polymeric or metallic material, with dimensions defined based on the dimensions of the modular cubes (100) that make up the modular construction system (01), particularly the dimension defined for the variable “a” for the length of the edges of the modular cubes (100). In each of the modular prisms (200), a distance is defined for each of its edges, determined by a ratio related to the variable “a” of the modular cubes (100). Preferably, the vertices and edges of the modular prisms (200) are beveled to eliminate stress concentration points that could potentially damage their geometry due to impact or cause injuries during handling.These modular prisms (200) are grouped into different categories, based on their application in the modular construction system (01) of the present invention, such that there are joining prisms (210) and multiple prisms (220). Each of these groups is identified primarily by its geometry, the number and type of holes found in each of them, and also for other purposes. ML / a / ZUZ l / U 1 U / O4 practical, are of different colors. The manufacturing process of the modular prisms (200) is one of the known ones, such as machining, material injection or blow molding processes. Each joining prism (210) as shown in Figure 13 to Figure 17, has a rectangular prismatic body where a pair of opposite major joining faces (211) are defined; a pair of opposite middle joining faces (212) perpendicular to the major joining faces (211); and a pair of opposite minor joining faces (213) at the distal ends of the rectangular prismatic body, perpendicular to the major joining faces (211) as well as to the middle joining faces (212). There are perforations that allow the assembly of the joining prisms (210) with modular panels (300) and other components, of which there is a pair of insert joining holes (214) located transversely to the body of the joining prism (210), on one of the two larger joining faces (211), where a joining insert (215) is housed and rigidly retained, which are located adjacently on the longitudinal axis of the larger joining face (211) where they are found.The insert joint holes (214) are blind holes, so each one has a bottom wall. The group of joint prisms (210) are painted a fourth color for easy identification. Each of the edge types of the rectangular prismatic body of the union prism (210) is identified based on its characteristics to define the dimensional relationship with the modular cubes (100), so that there is a major union edge (210 a), a medium union edge (210b) and a minor union edge (210c). The dimension of the larger joining edge (210a) of the joining prism (210) is identified by the variable (iu), so that it is defined by the following proportion: i = 2a +e. The dimension of the middle joining edge (210b) of the joining prism (210) is identified by the variable (ju), so that it is defined by the following proportion: j = a. The dimension of the smaller joining edge (210c) of the joining prism (210) is identified by the variable (ku), so that it is defined by the following proportion: IVIA / a / ZUZ l / UIU / O4 The dimensions to define the area of the faces corresponding to each of the pair of larger joining faces (211), the pair of medium joining faces (212) and the pair of smaller joining faces (213), are defined by the following proportion: A of 211 = 2a2+ ae = i -j; Ade212 = a2+ e -= ik; a2 Ade213 = — = ik; 21where: A of 211,- area of each of the pair of larger joining faces (211): A of 212.- area of each of the pair of middle joining faces (212); A of 213.- area of each of the pair of smaller joining faces (213); a.- the length of the edge of the modular cubes (100); e.- thickness of the modular panels (300). The separation between the longitudinal axes of the rectangular insert holes (214), identified with the variable (I), is defined by the proportion: I = a + e; where: a.- the length of the edge of the modular cubes (100); e.- thickness of the modular panels (300). Similarly, the location of the longitudinal axes of the rectangular insert holes (214) with respect to the middle joining faces (212), identified with the variable (m), is defined by the proportion: am = 2 Similarly, the location of the longitudinal axes of the rectangular insert holes (214) with respect to the nearby smaller joining faces (213), identified with the variable (n), is defined by the proportion: IVIA / a / ¿U¿ l / UIU / O4 Each multiple prism (220) as shown in Figure 18 to Figure 26, has a body in the shape of a quadrangular prism, where a first pair of rectangular faces (221) opposite each other are defined; a second pair of rectangular faces (222) opposite each other and perpendicular to the first rectangular faces (221); and a pair of distal faces (223) opposite each other and perpendicular to the first rectangular faces (221) as well as to the second rectangular faces (222).In addition, there are perforations that allow the assembly of the multiple prisms (220) with modular panels (300), as well as receiving the distal ends of the modular rods (400) of which there is a first multiple insert hole (221a), a first multiple rod end hole (221b), a second multiple insert hole (221c), a third multiple insert hole (221d), a fourth multiple insert hole (222a), a fifth multiple insert hole (222b), a sixth multiple insert hole (222c), a seventh multiple insert hole (222d) and an eighth multiple insert hole (223a) in addition, a second multiple rod end hole (223b). The first multiple insert hole (221a) oriented transversely to the body of the multiple prism (220), located on one of the first two rectangular faces (221), in which a first multiple insert (224a) is housed and rigidly retained, with its longitudinal axis located on the longitudinal axis of the first rectangular face (221). Located adjacent to the same first rectangular face (221), is the first end rod hole (221b) oriented transversely to the body of the rectangular prism (210) to receive the distal free end of a modular rod (400), with its longitudinal axis located on the longitudinal axis of the first rectangular face (221) where it is located, parallel to the first multiple insert hole (221a). There is a second multiple insert hole (221c) oriented transversely to the body of the rectangular prism (210), located on the first opposite rectangular face (221), in which a second multiple insert (224c) is housed and rigidly retained, with its longitudinal axis located on the longitudinal axis of the first opposite rectangular face (221) where it is located and coaxial to the first multiple insert hole (221a). IVIA / a / ZUZ l / UIU / O4 There is a third multiple insert hole (221 d) oriented transversely to the body of the rectangular prism (210), located on the first opposite rectangular face (221), in which a third multiple insert (224d) is housed and rigidly retained, with its longitudinal axis located on the longitudinal axis of the first opposite rectangular face (221) where it is located, parallel to the second multiple insert hole (221c) and coaxial with the first end rod hole (221b). There is a fourth multiple insert hole (222a) oriented transversely to the body of the rectangular prism (210), located on a second rectangular face (221), in which a fourth multiple insert (224e) is housed and rigidly retained, with its longitudinal axis located on the longitudinal axis of the second rectangular face (222) where it is located, perpendicular to the coaxial axis between the first multiple insert hole (221a) and the second multiple insert hole (221c). There is a fifth multiple insert hole (222b) oriented transversely to the body of the rectangular prism (210), located on a second rectangular face (222), in which a fifth multiple insert (224f) is housed and rigidly retained, with its longitudinal axis located on the longitudinal axis of the second rectangular face (222) where it is located, parallel to the fourth multiple insert hole (222a), perpendicular to the coaxial axis between the first multiple rod end hole (221b) and the third multiple insert hole (221d). There is a sixth multiple insert hole (222c) oriented transversely to the body of the rectangular prism (210), located on a second opposite rectangular face (222), in which a sixth multiple insert (224g) is housed and rigidly retained, with its longitudinal axis located on the longitudinal axis of the second opposite rectangular face (222) where it is located, coaxial with the fourth multiple insert hole (222a), perpendicular to the coaxial axis between the first multiple insert hole (221a) and the second multiple insert hole (221c). A seventh multiple insert hole (222d) is oriented transversely to the body of the rectangular prism (210), located on a second opposite rectangular face (222), in which a seventh multiple insert (224h) is rigidly housed and retained, with its longitudinal axis located on the longitudinal axis of the second opposite rectangular face (222) where it is located, parallel to the axis of the sixth hole. IVIA / a / ZUZ l / UIU / O4 multiple insert (222c), coaxial with the fifth multiple insert drill (222b), perpendicular coaxial axis between the first multiple drill rod end (221b) with the third multiple insert drill (221 d). There is an eighth multiple insert hole (223a) oriented longitudinally to the body of the rectangular prism (210), located centrally on a distal face (222), in which an eighth multiple insert (224I) is housed and rigidly retained, with its longitudinal axis located on the longitudinal axis coaxial with the longitudinal axis of the quadrangular prismatic body of the multiple prism (220), perpendicular to the coaxial axis between the first multiple insert hole (221a) and the second multiple insert hole (221c), as well as with the coaxial axis between the fourth multiple insert hole (222a) and the sixth multiple insert hole (222c). Located coaxially with the eighth multiple insert hole (223a) and centered on the opposite distal face (223), is the second end rod hole (223b), oriented longitudinally to the body of the rectangular prism (210) to receive the distal free end of a modular rod (400), with its longitudinal axis located perpendicular to the coaxial axis between the end rod multiple hole (221b) and the third multiple insert hole (221d), as well as to the coaxial axis between the fifth multiple insert hole (222b) and the seventh multiple insert hole (222d). The first multiple insert hole (221a), the first end rod hole (221b), the second end rod hole (221c), the third insert hole (221d), the fourth insert hole (222a), the fifth insert hole (222b), the sixth insert hole (222c), the seventh insert hole (222d), the eighth insert hole (223a), and the second end rod hole (223b) are blind holes, so that each one has a bottom wall. The multiple prism group (220) is painted in a fifth color for easy identification. The dimension of the largest edge of the multiple prism (220) identified by the variable (o), is defined by the following proportion: o = 2a + e. The dimension of the smaller edge of the multiple prism (220) identified by the variable (p) is defined by the following proportion: ML / a / ZUZ l / U 1 U / O4 p = a. The second extreme rod drill (223b) projects to a depth equal to the distance for each of the edges determined by the variable “a”. The dimensions to define the area of each of the faces corresponding to each of the rectangular faces (221, 222) and the pair of distal faces (223), are defined by the following proportion: A of 221 = 2a2+ae = op; A of 223 = a2; where: A of 221 area of each of the rectangular faces (221, 222); A of 223.- area of each of the pair of multiple distal faces (223); a.- the length of the edge of the modular cubes (100); e.- thickness of the modular panels (300). The separation between the longitudinal axes of adjacent boreholes (221a - 221b, 221c - 221d, 222a 222b, 222c - 222d) identified with the variable (q) is defined by the proportion: q = a + e; where: a.- the length of the edge of the modular cubes (100); e.- thickness of the modular panels (300). Similarly, it turns out that the location of the longitudinal axes of the multiple insert holes (221a, 221b, 221c, 221d, 222a, 222b, 222c, 222d), with respect to the adjacent rectangular faces (221,222), identified with the variable (r) is defined by the proportion: ML / a / ZUZ l / U 1 U / O4 Similarly, the location of the longitudinal axes of the eighth multiple insert hole (223a) and the second end rod hole (223b) with respect to the adjacent rectangular faces (221, 222), identified with the variable (s), is defined by the proportion: a S = 2 Additionally, it turns out that the location of the longitudinal axes of the multiple insert holes (221a, 221b, 221c, 221d, 222a, 222b, 222c, 222d), with respect to the nearest multiple faces (223), identified with the variable (t) is defined by the proportion: Modular panels (300) are elements with sheet-like bodies made of a natural fiber material such as wood, or of a polymeric or metallic material, with dimensions defined based on the dimensions of the modular cubes (100) that make up the construction system, particularly the dimension defined for the variable “a” for the length of the edges of the modular cubes (100). Each modular panel (300) has a defined distance for each of its edges, determined by a proportion related to the variable “a” of the modular cubes (100). In addition, each panel has a constant thickness “e” across all groups of modular panels (300).These modular panels (300) are grouped into different categories based on their geometry, which relates to their application in the modular construction system (01) of the present invention. These categories include square panels (310), larger rectangular panels (320), medium rectangular panels (330), smaller rectangular panels (340), and triangular panels (350). The manufacturing process for the modular panels (300) is one of the known processes, such as machining, material injection, or thermoplastic molding. The square panels (310), as shown in Figure 27 and Figure 27A, have longitudinal edges spaced to accommodate a square matrix of N x N perforations (311), where the number of perforations (N) aligned in a column is an odd number. The number of perforations (N) machined into the square panel (311) depends on the application of the modular panels (300). The perimeter edges of the modular panels (300) are of a length that accommodates a certain number of panel perforations. The fact that ML / a / ZUZ l / UIU / O4 square panel (311) does not imply that all of them must be machined. The separation between the layout axes of each of the square panel perforations (311) is identified by the variable (uc), defined by the proportion: uc = a + e The length of the perimeter edges of the quadrangular panels (310) is identified by the variable (Ic), defined by the proportion: Ic = Na + ((N-1)e) The perforations of the quadrangular panel (311) located adjacent to the longitudinal edge of the quadrangular panel (310) have a distance from said edge identified by the variable (ve), determined by the following proportion: a vc = 2 These square panel perforations (311) are sized to allow the free passage of a fastening element (700), such as the threaded body of a fixing screw, such that the screw head is larger than the diameter of the square panel perforation (211) where it is installed. Alternatively, at least one of the square panel perforations (311) is a through-hole (312) with a diameter for the free passage of modular rods (400). The larger rectangular panels (320), as shown in Figure 28, have perimeter edges spaced to accommodate a rectangular array of N x (2 x N) perforations for the larger rectangular panel (321), where the number of perforations (N) aligned in longitudinal rows is an odd number. The number of machined perforations (N) for the larger rectangular panel (321) depends on the application of the modular panels (300). The fact that the perimeter edges of the modular panels (300) are of a length sufficient to accommodate a certain number of perforations for the larger rectangular panel (321) does not imply that all of them must be machined. The spacing between the centerlines of each perforation for the larger rectangular panel (321) is identified by the variable (umy), defined by the proportion: umy = a + e Ideally, the longitudinal edge of the larger rectangular panels (320) of the same modular construction system (01) is twice the length of the edges of the square panels (310) and the transverse edge of the larger rectangular panels (320) of the same modular construction system (01) is equal to the length of the edges of the square panels (310). The perforations of the larger rectangular panel (321) located adjacent to the longitudinal edge of the larger rectangular panel (320) have a distance from said edge identified by the variable (vmy), determined by the following proportion: vmy^ These larger rectangular panel perforations (321) are sized to allow the free passage of a fastening element (700), such as the threaded body of a fixing screw, such that the screw head is larger than the diameter of the larger rectangular panel perforation (321) where it is installed. Alternatively, at least one of the larger rectangular panel perforations (321) is a through-hole (322) with a diameter for the free passage of modular rods (400). The medium rectangular panels (330), as shown in Figure 29, have perimeter edges spaced to accommodate a rectangular array of N x ((N+1) / 2) perforations for the medium rectangular panel (331), where the number of perforations (N) aligned in transverse rows is an odd number. The number of perforations (N) for the medium rectangular panel (331) that are machined depends on the application of the modular panels (300). The fact that the perimeter edges of the modular panels (300) are of a length sufficient to accommodate a certain number of perforations for the medium rectangular panel (331) does not imply that all of them must be machined. The spacing between the centerlines of each perforation for the medium rectangular panel (331) is identified by the variable (umd), defined by the proportion: umd = a + e Ideally, the longitudinal edge of the medium rectangular panels (330) of the same modular construction system (01) is equal to the length of the edges of the square panels (310) and the transverse edge is of a shorter length that allows the presence of the number of rows defined by the length ratio for this group of panels mentioned above. ML / a / ZUZ l / U 1 U / O4 The perforations of the medium rectangular panel (331) located adjacent to the longitudinal edge of the medium rectangular panel (330) have a distance from said edge identified by the variable (vmd), determined by the following proportion: vmd = 2 These half-rectangular panel perforations (331) are sized to allow the free passage of a fastening element (700), such as the threaded body of a fixing screw, such that the screw head is larger than the diameter of the half-rectangular panel perforation (331) where it is installed. Alternatively, at least one of the half-rectangular panel perforations (331) is a through-rectangular panel perforation (332) with a diameter for the free passage of modular rods (400). The smaller rectangular panels (340), as shown in Figure 30, have perimeter edges spaced to accommodate a rectangular array of N x ((N-1) / 2) perforations of smaller rectangular panels (341), where the number of perforations (N) aligned in transverse rows is an odd number. The number of perforations (N) of smaller rectangular panels (341) that are machined depends on the application of the modular panels (300). The fact that the perimeter edges of the modular panels (300) are of a length sufficient to accommodate a certain number of perforations of smaller rectangular panels (341) does not imply that all of them must be machined. The spacing between the centerlines of each of the perforations of smaller rectangular panels (341) is identified by the variable (umn), defined by the proportion: umn = a + e Ideally, the longitudinal edge of the smaller rectangular panels (340) of the same modular construction system (01) is equal to the length of the edges of the square panels (310) and the transverse edge is of a length less than the length of the transverse edge of the medium rectangular panels (330), sufficient to allow the presence of the number of rows defined by the length ratio for this group of panels mentioned above. ML / a / ZUZ l / U 1 U / O4 The perforations of the smaller rectangular panel (341) located adjacent to the longitudinal edge of the smaller rectangular panel (340) have a distance from said edge identified by the variable (vmn), determined by the following proportion: a vmn =2 These smaller rectangular panel perforations (341) are sized to allow the free passage of a fastening element (700), such as the threaded body of a fixing screw, such that the screw head is larger than the diameter of the smaller rectangular panel perforation (341) where it is installed. Alternatively, at least one of the smaller rectangular panel perforations (341) is a through-hole (342) with a diameter for the free passage of modular rods (400). The triangular panels (350), as shown in Figure 31, are a sheet-like body, preferably an isosceles triangle, with perimeter edges spaced to accommodate a plurality of triangular panel perforations (351). At least one row of these perforations is aligned parallel to the perimeter edges, and the number of perforations (N) aligned in rows parallel to the perimeter edges of the sides of the triangular panel (350) is an odd number. The number of machined triangular panel perforations (N) (351) depends on the application of the modular panels (300). The fact that the perimeter edges of the modular panels (300) are of a length sufficient to accommodate a certain number of triangular panel perforations (351) does not imply that all of them must be machined.The separation between the tracing axes of each of the triangular panel perforations (351) is identified by the variable (ut), defined by the proportion: ut = a + e. Ideally, the edge of two of the sides of the triangular panels (350) of the same modular construction system (01) are perpendicular, with a length equal to the length of the edges of the quadrangular panels (310) and the diagonal edge is longer than the two adjacent edges, with a length that allows the presence of a row of a number of perforations of triangular panel (351). ML / a / ZUZ l / U 1 U / O4 The triangular panel perforations (351) located adjacent to the perimeter edge of the triangular panel (350) have a distance from said edge identified by the variable (vt), determined by the following proportion: , a Vt = 2 Because the dimension of the longest edge of the triangular panel (350) represents the base or hypotenuse of the triangular geometry of this panel and knowing that the number of perforations of the triangular panel (351) aligned with this edge is an odd number, there are holes aligned symmetrically with respect to one of them located in the plane perpendicular with respect to the vertex opposite to said hypotenuse, which represents a central perforation of hypotenuse (352), so the number of holes distributed symmetrically with respect to said central hole of hypotenuse (352) is an even number.In addition to the above, the plurality of triangular panel perforations (351) aligned to said hypotenuse edge maintain the separation “ut” defined by the aforementioned proportion, so that the location of this plurality of triangular panel perforations (351) has an alignment in a plane parallel to said hypotenuse, but a different alignment from the plurality of remaining triangular panel perforations (351) in the triangular panel (350) adjacent to a side edge. These triangular panel perforations (351) are sized to allow the free passage of a fastening element (700), such as the threaded body of a fixing screw, such that the screw head is larger than the diameter of the smaller rectangular panel perforation (341) where it is installed. Alternatively, at least one of the triangular panel perforations (351) is a through-hole triangular panel perforation (352) with a diameter for the free passage of modular rods (400). The modular rods (400), as shown in Figure 32, are ideally cylindrical, preferably solid, elements made of a natural fiber material such as wood, or of a polymer or metallic material. Their dimensions are defined based on the dimensions of the modular cubes (100) that comprise the same construction system, particularly the dimension defined for the variable “a” for the length of the edges of the modular cubes (100). However, to simplify the expression of proportions, the length of each modular rod is defined as a function of the number of perforations (N) for the quadrangular panel (310). These modular rods (400) are grouped into different categories based on their length, which is related to their application within the system. The modular construction (01) of the present invention comprises larger rods (410), medium rods (420), and smaller rods (430). The diameters of the modular rods (400) are of the same diameter, sufficient to allow them to slide into the end holes and the pin holes of the modular cubes (100) and the modular prisms (200), as well as the through holes of the modular panels (300). The larger sticks (410) have a length identified by the variable (Imy), determined by the proportion: lmy = 2Na+e(2N-1)-2a+ 2be; where: a.- is the length of the edges of the modular cubes (100); N.- is the number of rows and columns that can be machined in the quadrangular panels (310) of the same modular construction system (01); be.- is the depth of the end corner hole (111) of the corner cubes (110). Medium sticks (420) have a length identified by the variable (Imd), determined by the proportion: lmd= a(N-2)+e(2N-1)+2be; where: a.- is the length of the edges of the modular cubes (100); N.- is the number of rows and columns that can be machined in the quadrangular panels (310) of the same modular construction system (01); be.- is the depth of the end corner hole (111) of the corner cubes (110). The smaller sticks (430) have a length identified by the variable (Imn), determined by the proportion: Imn = a(N-3) / 2 + e(2N-1) / 2 + 2be; where: a.- is the length of the edges of the modular cubes (100); ML / a / ZUZ l / U 1 U / O4 N.- is the number of rows and columns that can be machined in the quadrangular panels (310) of the same modular construction system (01); be.- is the depth of the end corner hole (111) of the corner cubes (110). Each of the at least one modular bearing bar (500) as shown in Figure 33 to Figure 36, is a prismatic body of random cross-section, preferably rectangular cross-section, made of a natural fiber material such as wood or a polymeric material or a metallic material, with dimensions defined from the dimensions of the modular cubes (100) that make up the construction system, particularly the dimension defined for the variable “a” for the length of the edges of the modular cubes (100).Each modular bearing bar (500) comprises perforations that allow its assembly with modular panels (300) as well as receiving sections of modular rods (400). For this purpose, a rod bar hole (501) is centrally located, with an axis perpendicular to the faces of greater area and perpendicular to the axis of length of the modular bearing bar (500), and with a diameter that allows the body of the modular rods (400) to be slidably accommodated. The length of the modular bearing bar (500) of the same modular construction system (01) is identified by the variable (Ib), determined by the proportion: Ib = lc+2e+2Dr = (N -a + ((N-1) -e)) + 2e + 2Dr; = Na+(Ne - e) + 2e + 2Dr where le = Na + ((N-1)e) Dr.- is the diameter of the installation fitting, a caster or load bearing (510) The thickness of the modular bearing bar (500) of the same modular construction system (01) is identified by the variable (le), determined by the proportion: । Cl lc= 2 Furthermore, there is at least one pair of insert bar holes (502) located symmetrically and parallel to the longitudinal axis of the rod bar hole (501), with their longitudinal axes perpendicular to the longitudinal axis of the prismatic body of the bearing bar (500), where the separation between the insert bar holes (502) of each of the pairs is identified by the variable (wb), determined by the proportion: IVIA / a / ZUZ l / UIU / O4 wb = a + e The separation between the longitudinal axes of the most distant insert bar holes (502) is identified by the variable (sb), determined by the proportion: sb = (N-1) (a+e) The distance between the longitudinal axis of the rod bar hole (501) with respect to the nearest insert bar hole (502) of the pair of insert bar holes (502) of the same modular construction system (01), is identified by the variable (xb), determined by the proportion: xb= ((N-3) / 2) x (a+e). Furthermore, the separation of the insert bar holes (502) with respect to the center of a bearing fitting (510) is identified by the variable (zb), determined by the proportion: , a , , ,Drxzb = - + e + — 2v2 ' Each insert bar hole (502) is of the same diameter and depth, in which a bar insert (503) is rigidly housed and retained, with its longitudinal axis located on the longitudinal axis of the prismatic body of the modular bearing bar (500). Each of the insert bar holes (502) is located on the same longitudinal face of the largest area of the modular bearing bar (500). On the face opposite the location of the insert bar holes (502) are the load bearings (510), which are located close to the distal edges of the prismatic body of the modular insert bar (500), as shown in Figures 33 to 35, where the separation of the center of the fitting with respect to the distal edge of the prismatic body of the modular bearing bar is identified by the variable (sr), determined by the proportion: Dr sr= — 2 The interconnection fittings (600) are elements made of a polymeric material, with random geometries such as 90° elbows, 45° elbows, three-way T-shaped elbows, cross-shaped elbows, or cylindrical elbows as shown in Figure 37. These elements are hollow and their free ends are of a ML / a / ZUZ l / U 1 U / O4 geometry and dimension that allows the installation with sliding of the free ends of modular rods (400) of the modular construction system (01). The joining elements (700) are elements such as joining screws (710) with pulleys (720), also known as washers, as shown in Figure 38. These elements have characteristics that allow their installation with the various inserts in the components of this modular construction system (01) in such a way as to ensure the joining between the elements to build a structure. The modular polyhedra (800), as shown in Figures 39 to 41, comprise a pentagonal prism-shaped body made of a natural fiber material such as wood, a polymeric material, or a metallic material. Their dimensions are defined based on the dimensions of the modular cubes (100) that make up the same modular construction system (01), particularly the dimension defined for the variable “a” for the length of the edges of the modular cubes (100). Preferably, the vertices and edges of the modular polyhedra (800) are beveled to eliminate stress concentration points that could potentially damage their geometry due to impact or cause injuries during handling. They also have perforations that allow them to be assembled with modular panels (300) and to receive sections of modular rods (400).The body of each modular polyhedron (800) has a pair of major polyhedron faces identified by the variable (cmy) which are perpendicular to each other; a middle polyhedron face (cmd) located opposite the edge formed by the angle of the perpendicular major polyhedron faces (cmy); a pair of minor polyhedron faces identified by the variable (cmn) adjacent to the longitudinal edges of the middle polyhedron face (cmd) and perpendicular to the major polyhedron faces (cmy), in addition to a pair of distal faces at the distal ends of the prismatic body of each modular polyhedron (800) which are identified by the variable (cds), where the proportion of each of these faces is determined by the following proportions:. cmy = bmy x hp = a2en where: bmyBase of the largest face of the polyhedron = a; hp.- Height of the prismatic body of the polyhedron (800) = a ΜΛ / a / ZUZ l / U 1 U / O4 cmd = bmd x hp en donde bmd.- Base de la cara media de poliedro = ^φ2+ φ2cmn = φ hp There is a first polyhedral end hole (811), located centrally on the middle face (cmd), as shown in Figures 39 and 41, with its longitudinal axis aligned with the edge formed by the perpendicular larger faces (cmy). Additionally, there is a second polyhedral end hole (812), located centrally on one of the larger faces (cmy), as shown in Figures 40 and 41, with its longitudinal axis aligned with the opposite smaller face (cmn). Each of the polyhedral end holes (811, 812) has a diameter that allows the sliding projection of a distal end of a modular rod (400) and a depth that allows them to communicate with each other to form an open polyhedral channel (810).On the other hand, there is an insert polyhedral hole (820) located centrally on another larger face (cmy), with its longitudinal axis aligned perpendicularly to the axis of the second end polyhedral hole (812), so that its location with respect to the adjacent edges is defined by the variable (sbp), determined by the proportion:. sbp = í A polyhedral insert (821) is housed in said polyhedral insert bore (820), with characteristics that allow it to receive a joining element (700) for joining the elements that make up the modular construction system (01) of the present invention. The group of pin cubes (120) are of a sixth color for their identification at a glance. Each insert (113, 123, 133, 215, 224a, 224c, 224d, 224e, 224f, 224g, 224h, 224i, 503, 821) of each element of the modular construction system (01) of the present invention, is made of a material resistant to the stresses that occur when joining said elements together by coupling the respective joining element (700), for example, it is a conical body of a material such as a metal or a high-density polymer, which is rigidly installed in the respective insert hole in the components that require it and has a threaded central hole (not polished) that extends conveniently along the length of the conical body to receive the threaded end of a joining screw (710) for detachable coupling between elements of the modular construction system (01). ML / a / ZUZ l / U 1 U / O4 The textile panels (900) are made of a textile material known in the technique, with a rectangular geometry, and dimensions defined from the dimensions of the modular cubes (100) that make up the same modular construction system (01), particularly from the dimension defined for the variable “a” for the length of the edges of the modular cubes (100). The textile panel (900) has a base length identified by the variable (bl) defined on the distal edges of the rectangular body, determined by the proportion: bl = 2Na+e(2N-1)-2a where N.- is the number of rows and columns that can be machined in the quadrangular panels (310) of the same modular construction system (01). The length of the textile canvas (900) is identified by the variable (II), determined by the proportion: II = 4a + Imd + 6 Db where Imd = length of the medium sticks (420); Db = diameter of the stick. Parallel to the distal edges of the canvas base (bl) are tubular seams (920) forming rod passages (921), which are distributed along the length of the textile canvas (900) aligned in pairs symmetrically with respect to the longitudinal axis of the textile canvas (900), such that a modular rod (400) is freely accommodated in each coaxial pair of these tubular seams (920). The length of the seams is identified by the variable (lt), determined by the proportion: lt = a(N-2) + e(N-1) Ideally, the tubular seams (920) extend in such a way that they are spaced apart from each other at a separation distance along the length of the textile canvas (900) identified by the variable (TS) for the proper handling of the modular poles (400) when installing them on the tubular seams (920), determined by the ratio; TS = Imd -2be IVIA / a / ¿U¿ l / UIU / O4 These tubular seams (920) are generated in such a way that a pair of rod passages (921a) are located on one of the transverse edges. The length of the tubular seams (920) allows a separation between each of the pairs of cane passages (921) for the handling of the modular canes (400) and to facilitate the installation of interconnecting accessories (600) and to form a desired structure. The height of the cane passages (921) to allow the accommodation of the modular canes (400) of the same modular construction system (01) is identified by the variable (Ip) which, in an illustrative way, is determined by the proportion: lp= 1.5 Db. BEST WAY TO CARRY OUT THE INVENTION. The construction of a structure using the modular construction system (01) of the present invention allows for the interchangeable use of various elements when the constituent elements maintain the same dimensional proportions based on a common reference element, which, in the case of the present invention, is the edges of the modular cubes (100). Therefore, once the elements of the modular construction system (01) are available in a desired number of units, the modular cubes (100) or polyhedra (800) are assembled into the modular panels (300), such that the inserts housed in the insert holes of the components align with the panel perforations. This allows for the insertion of a joining screw (710) with its respective washer (720) and the tightening of the connection between these elements to ensure the structural components are joined.Similarly, the poles are projected through the holes designed for their passage and their free end is secured in one of the bodies that has a hole to receive said pole end. Due to the dimensional proportions of the components, it is possible to reposition the elements to modify the structure's configuration, as well as alter the structure by combining more interchangeable elements that maintain the same proportions, as described in this document. Therefore, the resulting structural configuration is random, according to the user's needs. The characteristics of the components, and specifically their dimensions determined from the edge lengths of a reference element, allow them to be interchanged to form various structures, as shown in Figures 43 through 45.
Claims
1. A modular construction system (01) comprising modular cubes (100) with perforations centered on their faces, grouped into categories, modular prisms (200) with perforations, modular panels (300) of the same thickness, each with a plurality of perforations, modular rods (400) and joining elements (700), wherein in each of the modular cubes (100) the same distance is defined for each of its edges, determined by the variable “a” and they have the same value of the variable “a” for the length of their edges in the same modular construction system (01), characterized in that: - the modular cubes (100) have dimensions defined by a variable (a) for the length of their edges, from which the dimensions of the rest of the elements that make up the construction system are determined;- the modular prisms (200) are of proportional dimensions based on the variable “a” of the length of the edges of the modular cubes (100); - the perforations in the modular prisms (200) have a location relative to the variable “a” of the length of the edges of the modular cubes (100); - the modular panels (300) are of proportional dimensions based on the variable “a” of the length of the edges of the modular cubes (100) together with the thickness (e) defined for the same modular panels (300) and the number of perforations of one of the modular panels (300); - the perforations in the modular prisms (200) have a location relative to the variable “a” of the length of the edges of the modular cubes (100) and with a spacing between them relative to the variable “a” of the length of the edges of the modular cubes (100) and to the thickness (e) defined for the same modular panels (300);- the length of the modular rods is a dimension proportional to the variable “a” of the length of the edges of the modular cubes (100), the number of holes defined for one of the modular panels (300) and the thickness (e) defined for said modular panels (300).; 2. The modular construction system (01) according to claim 1, further characterized in that the elements comprising the modular construction system (01) are bodies manufactured from a natural fiber material such as wood, or from a polymeric material, or from a metallic material. IVIA / a / ZUZ l / UIU / O4 3. The modular construction system (01) according to claim 1, further characterized in that the modular cubes (100) are grouped into various categories based on their application in the modular construction system (01).
4. The modular construction system (01) according to claim 1, further characterized in that the modular cubes (100) comprise groups of corner cubes (110), sliding cubes (120) and cross cubes (130).
5. The modular construction system (01) according to claim 1, further characterized in that among the modular cubes (100) there is defined a group of corner cubes (110) in which there is an end corner hole (111) on three adjacent faces of the corner cube body (110) and an insert corner hole (112) located on the three remaining adjacent faces of the corner cube body (110) and aligned coaxially with an end corner hole (111) on the face opposite its location.
6. The modular construction system (01) according to claim 1, further characterized in that between the modular cubes (100) there is defined a group of corner cubes (110) in which there are end corner holes (111) on three adjacent faces of the corner cube body (110), of a diameter that allows the sliding projection of a distal end of a modular rod (400) and insert corner holes (112) located on the three remaining adjacent faces of the corner cube body (110), where a corner insert (113) is housed and retained to receive a joining element (700).
7. The modular construction system (01) according to claim 1, further characterized in that between the modular cubes (100) there is defined a group of corner cubes (110) in which there are both end corner holes (111) and insert corner holes (112), which are blind holes.
8. The modular construction system (01) according to claim 1, further characterized in that between the modular cubes (100) there is defined a group of pin cubes (120) in which there are end pin holes (121) on two adjacent faces of the pin cube body IVIA / a / ¿U¿ l / UIU / O4 (120), insert pin holes (122) located on two adjacent faces, aligned coaxially with an end pin hole (121) on a face opposite its location and a rod pin hole (124) projects centrally along the entire length of the pin cube body (120), between the two remaining opposite faces of the pin cube body (120).
9. The modular construction system (01) according to claim 1, further characterized in that between the modular cubes (100) there is defined a group of pin cubes (120) in which there are end pin holes (121) on two adjacent faces of the pin cube body (120) of a diameter that allows the sliding projection of a distal end of a modular rod (400); insert pin holes (122) on two adjacent faces, aligned coaxially with an end pin hole (121) on a face opposite its location where a pin insert (123) is housed and retained to receive a joining element (700) and a rod pin hole (124) projecting between two remaining opposite faces of the pin hub body (120) to receive a modular rod (400), of a diameter that allows the pin hub (120) to move along the length of a modular rod (400).
10. The modular construction system (01) according to claim 1, further characterized in that between the modular cubes (100) there is defined a group of pin cubes (120) in which there are both end pin holes (121) and insert pin holes (122), which are blind holes.
11. The modular construction system (01) according to claim 1, further characterized in that among the modular cubes (100) there is defined a group of cross cubes (130) in which there is an end cross hole (131) coaxially aligned on four opposite faces of the cross cube body (130) and an insert cross hole (132) located on the two remaining opposite faces of the corner cube body (110) coaxially aligned.
12. The modular construction system (01) according to claim 1, further characterized in that between the modular cubes (100) there is defined a group of cross cubes (130) in which there is an end cross hole (131) of a diameter that allows the sliding projection of a distal end of a modular rod (400) and insert cross holes (132) where a cross insert (113) is housed and retained.
13. The modular construction system (01) according to claim 1, further characterized in that between the modular cubes (100) there is defined a group of cross cubes (130) in which there are both end cross holes (131) and insert cross holes (132), which are blind holes.
14. The modular construction system (01) according to claim 1, further characterized in that the modular prisms (200) are grouped into various categories based on their application in the modular construction system (01).
15. The modular construction system (01) according to claim 1, further characterized in that the modular prisms (200) comprise groups of joining prisms (210) and prisms and multiple prisms (220).
16. The modular construction system (01) according to claim 1, further characterized in that between the modular prisms (200) there is defined a group of joining prisms (210), each with a rectangular prismatic body.
17. The modular construction system (01) according to claim 1, further characterized in that between the modular prisms (200) there is defined a group of joining prisms (210), with a rectangular prismatic body, in which there is a pair of insert joining holes (214) located transversely to the body of the joining prism (210), on one of two larger joining faces (211), where a joining insert (215) is housed.
18. The modular construction system (01) according to claim 1, further characterized in that a group of connecting prisms (210) is defined between the modular prisms (200), with a rectangular prismatic body, in which a pair of insert joining holes (214) is located transversely to the body of the connecting prism (210), on one of two larger joining faces (211), where a joining insert (215) is housed and rigidly retained. ML / a / ZUZ l / UIU / O4 19. The modular construction system (01) according to claim 1, further characterized in that between the modular prisms (200) there is defined a group of multiple prisms (220), each with a body in the shape of a quadrangular prism.
20. The modular construction system (01) according to claim 1, further characterized in that between the modular prisms (200) there is defined a group of multiple prisms (220), each with a body in the form of a quadrangular prism with blind perforations that allow the assembly of the multiple prisms (220) with modular panels (300), as well as receiving the distal ends of the modular rods (400).
21. The modular construction system (01) according to claim 1, further characterized in that between the modular prisms (200) there is defined a group of multiple prisms (220), each with a body in the shape of a quadrangular prism with a first multiple insert hole (221a) housing a first multiple insert (224a); a first rod end multiple hole (221b) to receive the distal free end of a modular rod (400); a second multiple insert hole (221c) housing a second multiple insert (224c); a third multiple insert hole (221d) housing a third multiple insert (224d); a fourth multiple insert hole (222a) housing a fourth multiple insert (224e); a fifth multiple insert hole (222b) housing a fifth multiple insert (224f); a sixth multiple insert hole (222c) where a sixth multiple insert (224g) is housed;a seventh multiple insert bore (222d) housing a seventh multiple insert (224h); an eighth multiple insert bore (223a) housing an eighth multiple insert (224i); and a second cane end multiple bore (223b) for receiving the distal free end of a modular cane (400).
22. The modular construction system (01) according to claim 1, further characterized in that the modular panels (300) are grouped into different categories, based on their geometry.
23. The modular construction system (01) according to claim 1, further characterized in that the modular panels (300) comprise groups of square panels (310), larger rectangular panels (320), medium rectangular panels (330), smaller rectangular panels (340), and triangular panels (350). ML / a / ZUZ l / U 1 U / O4 24. The modular construction system (01) according to claim 1, further characterized in that the perforations of the square panel (311) are of a dimension to allow the free passage of a joining element (700).
25. The modular construction system (01) according to claim 1, further characterized in that at least one of the perforations in each panel of the modular panels (300) is a through panel perforation, of a diameter for the free passage of the modular rods (400).
26. The modular construction system (01) according to claim 1, further characterized in that the modular rods (400) are ideally cylindrical elements, preferably solid.
27. The modular construction system (01) according to claim 1, further characterized in that the modular poles (400) are grouped into different categories, based on their length, which is related to their application in the modular construction system (01), so that there are larger poles (410), medium poles (420) and smaller poles (430).
28. The modular construction system (01) according to claim 1, further characterized by at least one modular bearing bar (500).
29. The modular construction system (01) according to claim 1, further characterized by at least one modular bearing bar (500) with dimensions defined from the dimension defined for the variable “a” for the length of the edges of the modular cubes (100).
30. The modular construction system (01) according to claim 1, further characterized by at least one modular bearing bar (500), where each of them comprises perforations that allow its assembly with modular panels (300) as well as receiving sections of modular rods (400).
31. The modular construction system (01) according to claim 1, further characterized by at least one modular bearing bar (500), where each of them comprises IVIA / a / ZUZ l / UIU / O4 load bearings (510) close to its distal edges; a centrally located rod bar bore (501) of a diameter to accommodate the modular rods (400) in a sliding manner; at least one pair of insert rod bores (502) located symmetrically and parallel to the longitudinal axis of the rod bar bore (501); and further a rod insert (503) housed in each insert rod bore (502).
32. The modular construction system (01) according to claim 1, further characterized by interconnection accessories (600) of random geometries such as 90° elbows, 45° elbows, three-way T-shaped elbows, cross-shaped elbows, or cylindrical elbows 33. The modular construction system (01) according to claim 1, further characterized in that the joining elements (700) are elements such as joining screws (710) with pulleys (720).
34. The modular construction system (01) according to claim 1, further characterized by modular polyhedra (800) with a pentagonal prism-shaped body with dimensions defined from the dimension defined for the variable “a” for the length of the edges of the modular cubes (100) and with perforations with polyhedron inserts (821) that allow assembly with modular panels (300) and perforations to receive sections of modular rods (400).
35. The modular construction system (01) according to claim 1, further characterized by textile canvases (900) with dimensions defined from the dimension defined for the variable “a” for the length of the edges of the modular cubes (100) together with the thickness (e) defined for the same modular panels (300) and the number of perforations made in one of the modular panels (300).
36. The modular construction system (01) according to claim 1, further characterized by textile canvases (900) with tubular seams (920) to form cane passages (921), parallel to the distal edges of the canvas base (bl), which are distributed along the textile canvas (900) aligned in pairs symmetrically with respect to the longitudinal axis of the textile canvas (900), to freely accommodate a modular cane (400) in each coaxial pair of tubular seams (920).