Construction, and method for creating same

Abstract

The invention relates to a construction, in particular a wall construction, floor construction, ceiling construction and / or roof construction of a building, said construction comprising: at least two shells that are spaced apart from one another; and an intermediate space which, apart from load-bearing and / or technical components, is substantially empty, and is delimited by the shells and enclosed therebetween. The construction contains: a composite construction-type component framework composed of one-dimensional and two-dimensional construction elements; and, if required, a hardening building material which, in a flowable or liquid state, is introduced into formworks / moulds specifically provided for this purpose, and thereby additionally forms a composite with the one-dimensional and two-dimensional construction elements of the component framework. The invention also relates to a method for manufacturing and processing starting materials and to a method for creating the construction in the different embodiments thereof.

Description

[0001] Construction and method of manufacturing the same

[0002] Description

[0003] Technical area

[0004] The invention relates to a structure, in particular a wall, floor, ceiling and / or roof structure of a building, comprising at least two spaced-apart shells and a space delimited by them and enclosed between them, which is essentially empty except for load-bearing and / or technical components. The structure includes a structural framework made of one- and two-dimensional structural elements in a composite construction and, if required, a hardening building material which is installed in a flowable or liquid state in specially provided formwork / casting molds and thus additionally creates a bond with the one- and two-dimensional structural elements of the structural framework. The invention further comprises a method for producing and processing starting materials and a method for producing the structure in its various embodiments.

[0005] State of the art

[0006] Current commercial practice in the construction sector can essentially be reduced to the implementation of two construction methods: solid construction versus skeleton construction. On the one hand, solid construction realizes the structural and room-enclosing functions using a single component (e.g., brick or concrete elements). On the other hand, skeleton construction uses systems consisting of a combination of post and beam elements and flat infills (timber-frame, post-and-beam, or drywall construction). The latter demonstrates the beginnings of composite technologies.

[0007] In light of the increased demands placed on the thermal performance of building components, particularly building envelopes, building systems have evolved primarily to enable the cost-effective integration of thermal insulation materials into the structure. Construction solutions that feature cavities for filling with thermal insulation materials or that allow the use of thermal insulation materials in sheet form are preferred. Recently, components designed for the active supply or removal of heat have also been used, allowing them to assume active thermal functions within a structure (e.g.,

[0008] Component temperature control).

[0009] Due to economic and sustainability considerations, it would be desirable to reduce the material consumption of the building materials used and increase cost efficiency, especially the productivity of the construction processes. This can hardly be improved with the approaches mentioned above. Existing construction solutions are implemented with a high proportion of manual labor, and a higher degree of digitalization is only being implemented industry-wide in the evaluation and planning of buildings.

[0010] Conventional composite technologies, which offer advantageous combinations of material properties (e.g., reinforced concrete, glued laminated timber, or laminated timber), have existed for some time and are widely used. However, they are still largely based on the aforementioned solid or skeleton construction methods. One example of a modern composite technology is the timber-concrete composite. This involves combining timber structures with concrete, particularly to achieve improved sound and vibration behavior of the components. However, the advantages of the specific material properties of wood and concrete are only partially realized in these solutions. In this context, concrete is primarily used as a bulk material and has little or no structural function.

[0011] In addition to the digitalization of evaluation and planning (BIM), the following digitalization approaches can be identified in the construction sector. On the one hand, concrete is being used in 3D printing processes, primarily for wall constructions. On the other hand, bar and panel joinery has established itself as a digitalization approach in timber construction. In this process, timber components in the form of bars or panels are prefabricated automatically. 1 . On-site assembly is still predominantly carried out manually.

[0012] Proposals for novel composite technologies, particularly using rod- or plate-shaped components, exist, but are based on the aforementioned solid or skeleton construction or a limited combination of material properties. See, for example, EP3453809A1.

[0013] DE202005007886U1, EP1745899A2, DE10230323A1, EP3577286A1, FR865513A,

[0014] W02023208510A1, EP2409821A1, DE10202497A1, JPH10338991A, EP3336274A1,

[0015] W02008028925A1, W00003850A1, RU2322545C2, US2022213684A1, DE29816002U1, US2017247883A1, US2020385976A1, USD941496S, IL58894A, US5058345A, CN212613356U

[0016] Description of the invention

[0017] The present invention is based on the object of providing a structure that can be manufactured using a cost-effective construction method and preferably also offers different design options with regard to the supply and removal of heat. Furthermore, a method for producing such a structure is also to be provided, which, in preferred embodiments, is as automated as possible and, if necessary, computer-aided or computer-implemented.

[0018] 1See, for example, Rogeau et al. “AN INTEGRATED DESIGN TOOL FOR TIMBER PLATE STRUCTURES TO GENERATE JOINTS GEOMETRY, FABRICATION TOOLPATH, AND ROBOT TRAJECTORIES” in Automation in Construction 130 (2021). Such a preferred aspect may, in certain embodiments, also consist in specifying an improved design for controlling the supply and removal of heat through the structure or for controlling thermal radiation and the temperature inside and / or outside a building. This is achieved in particular by decentralizing the heating and cooling function by means of miniaturized heating and cooling units distributed over the entire surface of the structure and positioned at suitable locations.

[0019] The invention further aims to provide a construction or method in which the construction costs of buildings can be massively reduced by digitizing the manufacturing process, thus improving sustainability and energy efficiency in the construction sector.

[0020] In a preferred aspect of the invention, the structure comprises a component framework using composite technology, which constitutes the basic structure of a building, and, if required, a hardening building material, which is installed in a loose, flowable, or liquid state into cavities required for the design or specially provided formwork / casting molds and then hardens. The structure can further comprise building or supply technology elements, which perform the thermal insulation as well as the heating and cooling function of the building, in particular also by means of thermal radiation. Furthermore, in a specific embodiment, the invention comprises a method for producing and processing starting materials for the structure. Finally, the invention comprises a method for producing the structure in its various embodiments.

[0021] The construction, which is preferably designed as a surface load-bearing structure, in particular a wall, floor, ceiling and / or roof construction and / or a cantilevered construction such as canopies, balconies or fire walls of a building or any structure, comprises in its general embodiment at least two spaced-apart shells which delimit and enclose between them a space which is essentially empty with the exception of load-bearing and / or technical components. On the one hand, the construction advantageously includes a prefabricated component framework which consists of a composite of one- and two-dimensional construction elements (such as a timber construction composite element made of bars and panels). On the other hand, the construction includes, if required, a hardening building material (e.g.Concrete, which is installed in a loose, flowable, or liquid state into cavities or specially designed formwork / casting molds, then hardens, thus creating a bond with the one- and two-dimensional structural elements of the component framework. Among other things, the material properties of the one- and two-dimensional structural elements are combined with the hardening building material in a novel way.

[0022] In the event that the one- or two-dimensional structural elements of the component framework consist of a porous, open-pored material (e.g. wood), an independent aspect of the invention comprises the prior setting of the one- or two-dimensional structural elements with a setting material in the form of a working mixture (e.g. mortar or synthetic resin). The setting material, in a flowable or liquid state, penetrates into the pores in the surface area of ​​the one- or two-dimensional structural elements and closes them during subsequent hardening. This creates a pore-closed surface layer filled with hardened setting material in the porous, open-pored, one- or two-dimensional structural elements. This has the advantage that the one- or two-dimensional structural elements can be exposed to increased structural static-dynamic forces and that they are protected from subsequent influences such as, for example,Moisture, fungal infestation, etc. When porous, open-pored, one- or two-dimensional structural elements are made of wood, the pore-sealed surface layer, filled with hardened filler material, prevents swelling during subsequent installation of the hardening building material, which subsequently hardens and thus also creates a bond with the one- or two-dimensional structural elements. This enables or increases the mutual connection, fastening, sealing, and / or anchoring, and thus the bond between the one- or two-dimensional structural elements and the hardening building material.

[0023] One possible embodiment of the structure comprises technical components such as building or supply technology elements, which in particular comprise heating and / or cooling circuits and / or circuits with secondary medium, or their miniaturized heating and / or cooling units, distributed as required across the entire building or structure surface, positioned at suitable locations, and integrated into the structure. Due to their material construction, the at least two spaced-apart shells provide the system with heat capacity and serve as heating and / or cooling surfaces. In turn, they can act as evaporators and / or condensers of the heating and / or cooling circuits. Furthermore, the building or supply technology consists of photovoltaic (PV) and / or battery storage elements as well as commercially available components for controlling them.The miniaturized heating and / or cooling units can be combined directly with a PV and / or battery storage unit and operated directly using renewable energy.

[0024] The general embodiment of the manufacturing process for the structure comprises several process steps, which are carried out as automated as possible and, if necessary, computer-aided or computer-implemented. These include, on the one hand, the production of the starting materials in the form of dry or working mixtures of the filling material or the hardening building material, or in the form of one- or two-dimensional structural elements of the component framework with various embodiments and materializations, in particular with a porous, open-pore material (e.g., wood). Furthermore, the process steps of the manufacturing process include the filling of the one- or two-dimensional structural elements with a filling material or the shaping of the starting materials, in particular the one- or two-dimensional structural elements of the component framework.On the other hand, the method steps of the manufacturing method comprise the assembly or joining of the one- or two-dimensional construction elements to form a component framework in various embodiments. Furthermore, the method steps of the manufacturing method comprise the assembly or joining of the component frameworks, which are designed as construction modules, modular building blocks, construction elements or components if required, and further, if required, the incorporation of the hardening building material into design-specific cavities or specially provided formwork / casting molds. Finally, the method steps of the manufacturing method comprise the assembly or joining of the component frameworks, or if required the construction modules, modular building blocks, construction elements or components and, if required, the incorporation of the hardening building material to form a construction according to the invention. The manufacturing method for the construction can be used in particular in prefabrication and pre- or post-production processes.Final assembly steps can be divided, whereby the process steps described above can be combined or carried out separately depending on the requirements and applications.

[0025] The field of application of the invention includes immobile structures, buildings, towers, bridges or facilities in any climate zone. On the other hand, the field of application also includes mobile structures such as all types of vehicles or means of transport (cars, trucks, mobile homes, coaches, trains, ships, aircraft) or mobile buildings and facilities. Furthermore, the invention can also be used for extraterrestrial structures (space travel) such as space transport systems, orbital habitats (space stations) or surface habitats (lunar or planetary bases). A special field of application of additional embodiments of the invention are heating and / or cooling applications using thermal radiation in outdoor areas, such as cantilevered canopies or freestanding structures such as bus shelters in public transport.

[0026] A fundamental innovation of the invention lies in a substantial reduction in the use of building materials (e.g., wood, concrete) while simultaneously achieving cost efficiency at all stages of the construction process (evaluation, planning, execution, prefabrication, final assembly, operation, and demolition). It begins with the approach of a novel composite technology that combines one- and two-dimensional structural elements into a building framework and, if necessary, can be expanded to include a composite with a hardening building material. This enables the combination of new materials, in particular the mutual coordination of specific material properties (e.g., a composite of concrete and beech dowels, whereby the concrete is used in a novel way as a two-dimensional structural element, which, by means of a multitude of beech dowels, forms a one-dimensional structural composite with the structural structure).Sustainability and cost-effectiveness are achieved primarily through innovative composite technology and a high degree of automation in the manufacture of the structure.

[0027] The individual components of the invention in detail

[0028] The construction

[0029] The structure advantageously fulfills several objectives simultaneously. In addition to the conventional structural function and protection against weather and climate, the structure should advantageously manage, on the one hand, sound, vibration, or thermal insulation (in its device aspect) and, on the other hand, active heat transport (implemented as an independent process aspect) by supplying and removing heat to thermally compensate for thermal transmission losses. Furthermore, in an independent aspect of the invention, the structure is intended to create thermal comfort within a building or between rooms, which is also achieved through the interaction of its device aspect and its process aspect by means of thermal radiation.

[0030] The structure should incorporate thermal capacity as well as design-related sound, vibration, and heat transmission dampeners. This is most easily achieved with a multi-shell construction, such as a general composite construction (e.g., wood-wood composite), a hybrid construction, or, more specifically, a wood-concrete composite construction. The shell, which contains thermal capacity, is structurally separated as far as possible from the components that dampen sound, vibration, or heat transmission. This multi-shell construction has the additional advantage of providing good moisture resistance. The structural and dynamic challenges resulting from the multi-shell construction are to ensure the bond between the at least two spaced-apart shells of the structure and to ensure that they are statically and dynamically spaced.To meet the above-mentioned requirements in a cost-effective construction method, a multi-shell composite construction method is proposed. This is advantageously realized using a structural framework that statically and dynamically spaced at least two spaced-apart shells and forms the basic structure of the building or structure.

[0031] In its general embodiment, the structural framework comprises formwork, as two-dimensional structural elements and structural components of the structure, and spacers, as one-dimensional structural elements and structural components of the structure, which, in a composite construction, statically and dynamically space the at least two spaced-apart shells. The structural framework can at least partially or completely form the space delimited by and enclosed between the at least two spaced-apart shells and / or at least one of the at least two spaced-apart shells.

[0032] If necessary, at least one of the at least two spaced-apart shells can be formed, at least partially or completely, with a hardening building material. This material is installed in a loose, flowable, or liquid state into at least one design-specific cavity or formwork as a shaping formwork / casting mold and / or, if necessary, at least one additional and / or independent, temporary formwork / casting mold. After a certain period of time, it then solidifies and hardens, providing the system with additional heat capacity through its materialization. We refer to this as the shell building material below. In this sense, the formwork as shaping formwork / casting mold can also be referred to as lost formwork.

[0033] Construction: The general embodiment of the construction, in particular a wall, floor, support, pillar, ceiling and / or roof construction and / or a cantilevered construction such as canopies, balconies or fire walls of a building or structure, which is preferably designed as a surface load-bearing structure, comprises at least two shells spaced apart from one another, which delimit and enclose between them a space that is essentially empty with the exception of load-bearing and / or technical components. The at least two shells spaced apart from one another comprise a shell facing the outside of the building or structure and a shell facing the inside of the building or structure or, in particular in the case of interior spaces of a building or structure, a shell facing one interior space and a shell facing the other interior space.generally with respect to the cross-section of the structure, a shell facing one space outside the structure and a shell facing the other space outside the structure.

[0034] An extended embodiment of the structure comprises, if required, a shell, partial, or complete structure and / or is designed in the form of building modules, modular building blocks, building elements, or components, which in turn may, if required, comprise shell, partial, or complete building modules, shell, partial, or complete modular building blocks, shell, partial, or complete building elements, or shell, partial, or complete components. Their borders and / or boundary surfaces, or if present, their formwork, parallel to a wall, floor, ceiling, or roof surface, have anchoring and / or sealing forms that serve for mutual connection, fastening, sealing, and / or anchoring.

[0035] Structural extensions: An extended embodiment of the structure includes, if necessary, structural extensions, whereby the structure is adjacent to a structural extension and is at least partially delimited by it. These can include conventional wall, floor, ceiling, and / or roof cladding or interior or exterior cladding. Furthermore, structural extensions can include embodiments of the structure in the foundation or support area. In this case, for example, at least two of the at least two spaced-apart shells in the foundation or support area are structurally connected to one another and serve to structurally stiffen the structure. This can be achieved, for example, using shell material and reinforcements, or using specially manufactured solid or welded parts. In addition, the structural extensions can also be designed as a finger system.These engage finger-like into the structure and are connected, fastened, sealed, and / or anchored to it. Additionally, the extended design of the structure, particularly the structural extensions, can include technical components if required.

[0036] Component framework: The structure includes at least one component framework of a preferred embodiment, which comprises a composite of one- and two-dimensional construction elements and, if required, a shell material which is incorporated in loose, flowable, or liquid form into at least one of the at least two spaced-apart shells by at least partially or completely defining said shell by means of at least one shaping formwork and / or, if necessary, forming said shell by means of an additional and / or independent, temporary formwork / casting mold. The at least one shaping formwork preferably consists of a two-dimensional construction element such as a formwork, in particular a permanent formwork. The component framework can be manufactured using steel, wood, dry-cast, mixed-cast, hybrid, and / or composite construction methods and / or an additive process (3D printing), plastic injection molding, or pressed materials.

[0037] An extended embodiment of the component scaffolding comprises, if required, a raw, partial, or complete component scaffold and / or is designed in the form of building modules, modular building blocks, building elements, or components, whereby these in turn can, if required, comprise raw, partial, or complete building modules, raw, partial, or complete modular building blocks, raw, partial, or complete building elements, or raw, partial, or complete components. Their borders and / or boundary surfaces, or if present, their formwork, parallel to a wall, floor, ceiling, or roof surface, have anchoring and / or sealing forms that serve for mutual connection, fastening, sealing, and / or anchoring. In addition, the extended embodiment of the component scaffolding can, if required, comprise structural extensions.

[0038] Formwork: Formwork, as two-dimensional structural elements and load-bearing components of the structure, can comprise panels, discs, boards, sheets, textiles, nonwovens, or films of various shapes, thicknesses, and strengths, and can include materials such as wood, metal, plastic, composite materials, fiber materials (metal, plastic, wood, stone, glass), or a combination and / or a composite thereof. Special mention should be made of formwork manufactured using an additive process (3D printing), plastic injection molding, pressed materials, or a porous, open-pore material and / or a sound, vibration, and / or thermal insulation material. If the formwork is made of a porous, open-pore material and / or a sound, vibration, and / or thermal insulation material, it can additionally include a waterproofing layer and / or a closed-pore layer in its surface area.Furthermore, they can be filled with a filling material (e.g., synthetic resin, concrete, mortar). The flowable or liquid working mixture of the filling material penetrates the pores in the surface area of ​​these formworks and closes and seals them as the filling material subsequently hardens. This provides additional stiffening and / or prevents swelling upon subsequent contact with moisture, water, or flowable or liquid building materials such as formwork material or mortar, or provides additional protection against moisture or fungal infestation.

[0039] Lost formwork: Formwork, as two-dimensional structural elements and load-bearing components of the structure, can be used in a general embodiment as mentioned above as formwork / casting mold for the shell construction material. With suitable materialization and processing of the formwork, a mechanical, chemical, or mechanical-chemical bond between the formwork and the shell construction material can be created and utilized for the structural statics and dynamics, particularly in the case of permanent formwork made of a porous, open-pore material (e.g., wood), if this penetrates the pores in at least part of the surface area of ​​the permanent formwork in the form of a working mixture and, upon subsequent curing, creates an improved bond with the permanent formwork.An extended embodiment of permanent formwork, as two-dimensional structural elements and load-bearing components of the structure, includes formwork provided with at least one anchoring feature (e.g., dovetail cutout) and / or at least one sealing feature (e.g., rebate) to improve the bond with a shell construction material. Particularly in the case of permanent formwork made of wood, it can be left uncut on the side facing the shell construction material to improve the bond with the shell construction material.

[0040] Individual formwork: In a further embodiment, the formwork, as two-dimensional structural elements and structural components of the structure, can completely form at least one of the at least two spaced-apart shells of the structure, whereby these formworks are referred to as individual formworks. An extended embodiment of individual formwork, as two-dimensional structural elements and structural components of the structure, includes formwork, particularly in the case where it consists of a multi-layer solid wood panel (e.g., a 3-layer solid wood panel), whose layer structure is coordinated and aligned with the one-dimensional structural elements and structural components of the structure, such as spacers.The mutual connection, fastening, sealing and / or anchoring is carried out by means of a blind hole and the layer structure of the 3-layer solid wood panel is manufactured and coordinated in such a way that the thickness of the cover sheet corresponds to the distance from the cover sheet surface to the penetration depth of the blind hole and its wood fiber direction is aligned parallel to the longitudinal axis of the composite component, and the thickness of the remaining transverse or longitudinal layers or their wood fiber directions, which are located within the area of ​​the blind hole, are aligned in the longitudinal or transverse direction according to the structural forces incurred, in particular in such a way that the coordinated, controlled and / or process-induced diversion of the structural forces incurred corresponds to the coordinated, controlled and / or process-induced layer structure or the orientation of the wood fibers.

[0041] Stabilization formwork: The formwork, as two-dimensional construction elements and structural components of the structure, can in a further embodiment be arranged in at least one intermediate space delimited by at least two spaced-apart shells and enclosed between them and can be used for stabilization and / or as a connection, fastening, sealing and / or anchoring of the one-dimensional construction elements and structural components of the structure, such as spacers.In particular, such that a first spacer is anchored in a first shell adjacent to the intermediate space and / or in further structural components and does not touch a second shell adjacent to the intermediate space, and at least one spacer is anchored in a second shell adjacent to the intermediate space and / or in further structural components and does not touch the first shell adjacent to the intermediate space, in particular in such a way as to achieve increased sound, vibration, or thermal insulation within the structure. Sound, vibration, and / or thermal insulation formwork: In a further embodiment, the formwork, as two-dimensional structural elements and structural components of the structure, can be arranged in at least one intermediate space delimited by at least two spaced-apart shells and enclosed between them, and serve to provide sound, vibration, or thermal insulation for the structure.

[0042] Spacers: Spacers, as one-dimensional structural elements and load-bearing components of the structure, can include sleeves, anchoring, solid or hollow bars, dowels, bolts, profile bars or commercially available means of sealing and fastening technology as well as different shapes, thicknesses and strengths and include materials such as wood, metal, plastic, composite materials, fiber materials (metal, plastic, wood, stone, glass), a combination and / or a composite thereof. Special mention should be made of spacers manufactured using an additive process (3D printing), from plastic injection molding, from pressed materials or from a porous, open-pore material and / or from a sound, vibration and / or thermal insulation material. In the event that the spacers are made of a porous, open-pore material (e.g.If the spacers consist of a material such as wood) and / or a sound, vibration and / or thermal insulation material, they can also include a sealing layer and / or a closed-pore layer in their surface area. Furthermore, they can be mixed with a filling material (e.g. synthetic resin, concrete, mortar). The flowable or liquid working mixture of the filling material penetrates into the pores in the surface area of ​​these spacers and closes and seals them when the filling material subsequently hardens. This serves to provide additional stiffening and / or to prevent swelling upon later contact with moisture, water or flowable or liquid building materials such as formwork material or mortar or to provide additional protection against moisture or fungal infestation.

[0043] The spacers, as one-dimensional structural elements and structural components of the structure, generally serve to provide structural static-dynamic spacing between the formwork, and as two-dimensional structural elements and structural components of the structure, and in particular, to provide structural static-dynamic spacing between the at least two spaced-apart shells of the structure. The spacers can be arranged vertically or inclined at an angle other than 90° to a formwork, to a surface bordering a shell, or to a surface bordering a gap of a shell adjacent to a gap. Furthermore, the spacers can be distributed in a large number.

[0044] Spacer bars: The spacers, as one-dimensional construction elements and structural components of the structure, can in a general embodiment be arranged in at least one intermediate space delimited and enclosed by at least two spaced-apart shells and can be used to space the structural components such as formwork and / or reinforcements, and / or in particular for the structural static-dynamic spacing of at least two spaced-apart shells of the structure. We call these spacers spacer bars. On the one hand, the spacer bars can be installed in at least one formwork adjacent to the intermediate space and / or in other structural components by means of a screw, press, glue and / or adhesive connection, in particular by means of a drilled, threaded, dovetail, rebate, groove or notch connection, general one-in or one-out connection.Milled out sections or connected, fastened, sealed and / or anchored using commercially available sealing and fastening technology. In addition, the spacer bars can be connected, fastened, sealed and / or anchored in at least one formwork adjacent to the gap using special sealing and fastening technology or anchoring aids such as press, drilling, threading, thread-cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread. In the event that the spacer bars protrude into the shell material, they can, if required, be connected, fastened, sealed and / or anchored in the shell material of at least one of the at least two spaced-apart shells and / or other load-bearing structure components, such as formwork. This can be done, for example, using anchoring forms attached to the end area of ​​the spacer, such asGrooves, notches or millings etc. or anchoring aids can be achieved.

[0045] In the event that the spacers protrude into the shell construction material, an extended embodiment of the spacers, with suitable materialization and processing, comprises a mechanical, chemical or mechanical-chemical bond between the spacers and the shell construction material, which can be exploited for the structural statics and dynamics, in particular in the event that the spacer consists of a porous, open-pore material (e.g. wood) and the shell construction material in the form of a working mixture penetrates into the pores in at least part of the surface area of ​​the spacer and, upon its subsequent curing, brings about an improved bond with the same.

[0046] Shell spacers: The spacers, as one-dimensional structural elements and structural components of the structure, can be arranged in another embodiment in at least one of at least two spaced-apart shells and used to space the structural components, such as formwork and / or reinforcement. We refer to these spacers as shell spacers. The anchoring of the shell spacers in the formwork and / or other structural components that at least partially or completely delimit the at least two spaced-apart shells can be achieved by screwing, pressing, gluing, and / or adhesive bonding, in particular by means of drilling, threading, dovetail, rebate, groove, or notch connections, general milling or recessing, or with commercially available sealing and fastening means.In addition, the shell spacers can be anchored in the formwork that at least partially or completely delimits the at least two spaced-apart shells by means of special sealing and fastening technology or anchoring aids, such as press, drilling, threading, thread-cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread.Shell construction material: If required, the construction can comprise a hardening building material, the shell construction material, which is incorporated in the form of a loose, flowable or liquid working mixture into at least one of the at least two spaced-apart shells, at least partially or completely, by at least partially or completely defining the shell by means of at least one form-giving formwork and / or, if necessary, formed by means of an additional and / or independent, temporary formwork / casting mold. After being incorporated into the design-related cavities or into the formwork as a form-giving formwork / casting mold and, if necessary, into an additional and / or independent, temporary formwork / casting mold, the shell construction material subsequently solidifies and hardens after a certain period of time and thus develops its strength. The shell construction material can be concrete or a concrete-like building material. On the other hand, it can be, for example:also include a hardening powder, pellets, dust, sand or other loose, flowable or liquid materials as well as materials that are in different physical states of aggregation, which after installation in the formwork as a shaping formwork / casting mold and, if necessary, an additional and / or independent, temporary formwork / casting mold, subsequently solidify and harden after a certain period of time and thus develop a sufficiently high strength.

[0047] In a specific embodiment, the working mix of the shell building material comprises cement, aggregates, a liquid such as water and, if required, other substances such as chemicals to influence and adjust the viscosity and / or the curing behavior (in particular substances and / or chemicals which enable, support or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes). The nature or quality properties of the cement and / or aggregates such as the particle or grain size, the particle or grain geometry and / or their proportional distributions (e.g. particle or grain size distribution, distribution densities or distribution sums) in the dry mix orthe working mixture is adapted to a function or effect according to the invention, in particular to the coordinated, controlled and / or process-induced dissipation of structural forces by means of its connection with one- and / or two-dimensional construction elements and structural components of the construction, in particular in such a way that the mechanical, chemical or mechanical-chemical connection between the hardened and solidified shell building material and the one- and / or two-dimensional construction elements and structural components of the construction enables the improved dissipation of structural forces.

[0048] Filling material: If the one- and / or two-dimensional structural elements and load-bearing components of the structure are made of a porous, open-pore material (e.g., wood), the structure may, if necessary, include a hardening filling material whose working mixture, in a flowable or liquid form, penetrates the pores in at least part of the surface area of ​​the one- and / or two-dimensional structural elements and seals them upon subsequent hardening. The filling material can be, for example, an impregnation, a synthetic resin, concrete, or mortar, whose working mixture is flowable or liquid and which subsequently solidifies and hardens after a certain period of time.

[0049] In a specific embodiment, the working mixture of the setting material, in particular a mortar, comprises cement, aggregates, a liquid such as water and, if required, further substances such as chemicals to influence and adjust the viscosity and / or the curing behavior (in particular substances and / or chemicals which enable, support or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes). The nature or quality properties of the cement and / or aggregates, such as the particle or grain size, the particle or grain geometry and / or their proportional distributions (e.g. particle or grain size distribution, distribution densities or distribution sums) in the dry mix orthe working mixture is adapted to a function or effect according to the invention, in particular to the coordinated, controlled and / or process-induced displacement or penetration of the same into the pores in at least part of the surface area of ​​the porous, open-pored, one- and / or two-dimensional construction elements and supporting structure components of the construction.

[0050] Reinforcement: If necessary, the structure includes reinforcements, which in turn provide additional strength to the shell material and / or structural components such as formwork. This can include materials such as wood, metal, plastic, composite materials, fiber materials (metal, plastic, wood, stone, glass), or a combination and / or composite of these, and can be in the form of rods, bars, grids, meshes, textiles, nonwovens, or fibers. Of particular note are reinforcements manufactured using an additive process (3D printing), plastic injection molding, or molded materials.

[0051] Technical components: If necessary, the design and / or design extensions can include technical components. These include, on the one hand, building or

[0052] Supply engineering elements that, with the aid of a control process and suitable heat transfer media such as a refrigerant and / or a secondary medium, manage the controlled supply and removal of heat into and from the structure and / or its extensions. This is achieved via heating and / or cooling circuits and / or circuits with secondary media, or their miniaturized heating and / or cooling units, integrated directly into the structure and / or its extensions.

[0053] The function of the heat processed and transported via the building or supply technology elements is i. to actively compensate for thermal transmission losses due to the reduced thermal insulation of the structure and / or the structural extensions and ii. to process the heating and / or cooling function via component temperature control using thermal radiation in the interior and / or exterior of the building or structure and thus to ensure thermal comfort for the users and / or residents.

[0054] The surface of the structure and / or the structure extensions facing the interior serves as a heat radiation surface for heating and / or cooling by means of heat radiation in the interior of the building or structure and the surface of the structure and / or the structure extensions facing the exterior serves as a heat radiation surface for heating and / or cooling by means of heat radiation in the exterior of the building or structure.

[0055] On the other hand, the technical components integrated into the structure and / or the structure extensions comprise measurement and / or control technology elements, which carry out the execution of the thermal function of the structure and / or the structure extensions in their process aspect, as specified by a control method provided according to an independent aspect of the invention. They record measured variables such as temperature, pressure, humidity, and physical measured variables of thermal radiation at all designated locations, in particular in the exterior and / or interior of the building or structure, on the exterior and / or interior surfaces of the structure and / or the structure extensions and / or within the structure and / or the structure extensions, and process them in the form of signals as input information of a thermally relevant state variable for the control method.Furthermore, the measurement and / or control technology elements process, transmit and regulate the control commands specified by the control process and passed on to the respective devices and units of the building or supply technology and provide feedback of the system states to the control system.

[0056] Extraterrestrial structure: An optional embodiment of all general, extended, or specific embodiments of a basic, partial, or complete component framework or a basic, partial, or complete structure described above includes their design for extraterrestrial applications such as space transportation systems (space travel), surface habitats (lunar or planetary bases), or orbital habitats (space stations). Extraterrestrial structures are exposed to an extreme environment with challenges that are fundamentally different from those on Earth. They are subject to a number of significant structural and functional requirements, particularly those for protection against cosmic radiation.In the event that the one- and / or two-dimensional structural elements and structural components of the structure are made of a porous, open-pored material, the extraterrestrial structure can comprise a hardening filling material whose working mixture, in flowable or liquid form, penetrates the pores in at least part of the surface area of ​​the one- and / or two-dimensional structural elements and seals them upon subsequent hardening. This serves to shield and protect the porous, open-pored one- or two-dimensional structural elements and structural components of the structure from cosmic radiation and can reduce their material degradation due to the effects of cosmic radiation.

[0057] The manufacturing process

[0058] The method for producing the construction according to the invention comprises several process steps, which are carried out as automated as possible and, if necessary, computer-aided or computer-implemented. These include, on the one hand, the production of the starting materials in the form of dry or working mixes of the filling material or the hardening building material (shell building material) or in the form of one- or two-dimensional structural elements of the component framework with various materializations, preferably with a porous, open-pore material (e.g., wood). Furthermore, the process steps of the manufacturing process include the filling of the one- and / or two-dimensional structural elements with a filling material or the shaping of the starting materials, in particular the one- or two-dimensional structural elements of the component framework.On the other hand, the process steps of the manufacturing process include the assembly or joining of the one- and two-dimensional construction elements to form a component framework in various embodiments. Furthermore, the process steps of the manufacturing process include the assembly or joining of the component frameworks to form building modules, modular building blocks, building elements or components and, if required, the incorporation of a hardening building material such as a shell building material into design-related cavities or specially provided formwork / casting molds. Finally, the process steps of the manufacturing process include the assembly or joining of the building modules, modular building blocks, building elements or components and, if required, the partial or complete incorporation of a hardening building material such as a shell building material to form a structure, in particular a wall, floor, ceiling and / or roof structure and / or a cantilevered structure such asCanopies, balconies, or firewalls of a building or any structure, comprising at least two spaced-apart shells that delimit and enclose a space that is essentially empty except for structural and / or technical components. The manufacturing process of the structure can be divided, in particular, into prefabrication and pre- and / or final assembly steps. Depending on the requirements and applications, the process steps described above can be combined or carried out separately as prefabrication and pre- and / or final assembly steps.

[0059] Production of setting material: An embodiment of the method for producing a dry mix for a setting material, in particular a dry mix for a mortar, comprising cement, aggregates and, if required, further substances such as chemicals for influencing and adjusting the viscosity and / or the curing behavior (in particular substances and / or chemicals which enable, support or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes) and a working mix of a setting material, in particular a working mix of a mortar, comprising the dry mix of the mortar and a liquid, such as water, and, if required, further substances such asChemicals for influencing and adjusting the viscosity and / or curing behavior (in particular substances and / or chemicals which enable, support or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes) generally comprise the proportional preparation and proportional mixing of the starting materials for the dry mortar mix and the production of a proportionally adjusted working mixture of the mortar for the placement of porous, open-pore structural components of the structure with the same. If necessary, the process can be divided into individual process steps. In particular, the proportional composition, the nature and / or the quality properties of the dry mortar mix are adjusted to an inventive function or effect of the working mixture of the mortar.

[0060] In this case, a function or effect according to the invention of a working mixture of the setting material, in particular a function or effect according to the invention of a working mixture of the mortar, comprises the coordinated, controlled and / or process-induced setting or penetration of the same into the pores in at least a part of the surface area of ​​a porous, open-pore structural component of the construction, wherein the particle or grain size, the particle or grain geometry and / or their proportional distributions 2 (e.g. particle or grain size distribution, distribution densities or distribution sums) of the starting materials in the working mixture on the pore size, pore geometry and / or on their proportional distributions 3(cumulative or relative pore volume distribution as a function of the pore radius) in at least part of the surface area of ​​the porous, open-pored structural component, in particular such that the particle or grain size and / or the particle or grain geometry of the starting materials in the working mixture is smaller than or equal to the pore size or pore geometry in at least part of the surface area of ​​the porous, open-pored structural component, in the respective band of the corresponding distributions and in particular such that the coordinated, controlled and / or process-induced penetration of the working mixture into the pores in at least part of the surface area of ​​the porous, open-pored structural component takes place in a uniformly distributed manner and, during the solidification and curing of the working mixture of the filling material, in particular the working mixture of the mortar, the surface area of ​​the porous,open-pore structural component is evenly stiffened, sealed and closed.

[0061] The process steps for preparing the starting materials for a dry mix of the setting material, in particular a dry mix of the mortar, comprise the crushing, grinding, sieving and / or squeezing of the cement and / or at least one aggregate in order to achieve a degree of fineness or grinding, particle or grain size, particle or grain geometry and / or distribution (e.g. particle or grain size distribution, distribution densities or distribution sums) that is tailored to an inventive function or effect of the working mixture of the mortar.

[0062] 2 In case the backfill material includes cement and aggregates, see e.g. https: / / www.sympatec.com / de / applikationen / partikelgroessenanalyse-zement /

[0063] 3In the event that the porous, open-pored material consists of beech wood, see e.g. Vitas et al "Porosity and Pore Size Distribution of Native and Delignified Beech Wood Determined by Mercury Intrusion Porosimetry" in Materials 12, 416 (2019) Process steps for producing a dry mix of the mortar include the proportional mixing and blending of the prepared cement with at least one prepared aggregate and, if required, other substances such as chemicals to influence and adjust the viscosity and / or the curing behavior (in particular substances and / or chemicals which enable, support or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes).The process steps described above can be carried out by manual work, automated machines or a combination thereof, thus producing a dry mix of the filling material, in particular a dry mix of the mortar.

[0064] The process steps for producing a working mix of the filling material, in particular a working mix of the mortar, comprise the proportional mixing and blending of the dry mortar mix with a liquid, such as water, and, if necessary, other substances such as chemicals to influence and adjust the viscosity and / or curing behavior (in particular substances and / or chemicals that enable, support, or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes). The process steps described above can be carried out manually, using automated machines, or a combination thereof, thus producing a working mix of the filling material, in particular a working mix of the mortar.

[0065] Production of shell building material: An embodiment of the method for producing a dry mix for a shell building material comprising cement, aggregates and, if required, further substances such as chemicals for influencing and adjusting the viscosity and / or the curing behavior (in particular substances and / or chemicals which enable, support or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes) and a working mixture of a shell building material, comprising the dry mix of the shell building material and a liquid, such as water, and, if required, further substances such asChemicals for influencing and adjusting viscosity and / or curing behavior (in particular substances and / or chemicals that enable, support, or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes) generally comprise the proportional preparation and proportional mixing of the starting materials for the dry mix of the shell construction material and the production of a proportionally adjusted working mix of the shell construction material. If necessary, the process can be divided into individual process steps. In particular, the proportional composition, the nature, and / or the quality properties of the dry mix of the shell construction material are tailored to an inventive function or effect of the working mix of the shell construction material.

[0066] In this case, a function or effect according to the invention of a working mixture of the shell building material comprises the coordinated, controlled and / or process-induced reduction or prevention of the release of moisture, water or shell building material liquid into the pores in at least part of the surface area of ​​a porous, open-pore structural component of the construction, wherein the particle or grain size, the particle or grain geometry and / or their proportional distributions 4 (e.g. particle or grain size distribution, distribution densities or distribution sums) of the starting materials in the working mixture on the pore size, pore geometry and / or on their proportional distributions 5(cumulative or relative pore volume distribution as a function of the pore radius) in at least part of the surface area of ​​the porous, open-pored structural component, in particular such that the water retention capacity with respect to the particle or grain size and / or the particle or grain geometry of the starting materials in the working mixture is increased and is matched to the pore size or pore geometry in at least part of the surface area of ​​the porous, open-pored structural component, in the respective band of the corresponding distributions and in particular such that the coordinated, controlled and / or process-induced reduction or prevention of the release of moisture, water or shell building material liquid of the working mixture into the pores in at least part of the surface area of ​​the porous,open-pored structural component is evenly distributed and, during the solidification and curing of the working mixture of the shell building material, the surface area of ​​the porous, open-pored structural component is evenly protected from moisture ingress, water ingress or shell building material liquid ingress.

[0067] The process steps for preparing the starting materials for a dry mix of the shell building material comprise breaking, grinding, sieving and / or crushing the cement and / or at least one aggregate in order to achieve a degree of fineness or grinding, particle or grain size, particle or grain geometry and / or distribution (e.g. particle or grain size distribution, distribution densities or distribution sums) tailored to an inventive function or effect of the working mixture of the shell building material. The process steps for producing a dry mix of the shell building material comprise the proportional mixing and blending of the prepared cement with at least one prepared aggregate and, if required, other substances such as, for example,Chemicals for influencing and adjusting viscosity and / or curing behavior (particularly substances and / or chemicals that enable, support, or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes). The process steps described above can be carried out manually, using automated machines, or a combination of the two, resulting in a dry mix of the shell construction material.

[0068] The process steps for producing a working mixture of the shell building material include the proportional mixing and blending of the dry mixture of the shell building material with a liquid, such as water, and if necessary, other substances such as chemicals to influence and adjust the viscosity and / or the curing behavior (in particular substances and / or

[0069] 4In case the backfill material includes cement and aggregates, see e.g. https: / / www.sympatec.com / de / applikationen / partikelgroessenanalyse-zement /

[0070] 5 For the porous, open-pore material made of beechwood, see, for example, Vitas et al. "Porosity and Pore Size Distribution of Native and Delignified Beech Wood Determined by Mercury Intrusion Porosimetry" in Materials 12, 416 (2019). Chemicals that enable, support, or accelerate the incorporation of water into the material structure in self-compacting (SCC) mortars or concretes can be used. The process steps described above can be carried out manually, using automated machines, or a combination of the two, resulting in a working mixture of the shell construction material.

[0071] Manufacturing spacers: One embodiment of the method for manufacturing one-dimensional structural elements and load-bearing components of the structure, such as spacers made of wood, in particular in the form of sleeves, rods, dowels or bolts, generally comprises the preparation and processing of various starting materials such as wooden boards or planks and, if required, other substances and / or materials. In particular, material geometry, material thicknesses and dimensions as well as any other material properties of the various starting materials determine the quality properties of the one-dimensional structural elements, which are coordinated and optimized for their use for at least part of the structure, in particular for the inventive function or effect of the composite with a two-dimensional structural element and load-bearing component of the structure, such as

[0072] Formwork made of wood (so-called wood-wood composite) or on the inventive function or effect of the composite with a shell building material (so-called wood-concrete composite).

[0073] In this case, a function or effect according to the invention of a composite between porous, open-pored, one-dimensional construction elements and structural components of the construction and a shell construction material comprises the coordinated, controlled and / or process-induced dissipation of occurring structural forces by means of a mechanical, chemical or mechanical-chemical composite, in particular via the coordinated, controlled and / or process-induced penetration of the working mixture of the shell construction material into the pores in at least a part of the surface area of ​​the porous, open-pored structural component, wherein the particle or grain size, the particle or grain geometry and / or their proportional distributions (e.g. particle or grain size distribution, distribution densities or distribution sums) of the starting materials in the working mixture are influenced by the pore size,Pore ​​geometry and / or their proportional distributions (cumulative or relative pore volume distribution as a function of the pore radius) in at least part of the surface area of ​​the porous, open-pored structural component, in particular such that the particle or grain size and / or the particle or grain geometry of the starting materials in the working mixture is smaller than or equal to the pore size or pore geometry in at least part of the surface area of ​​the porous, open-pored structural component, in the respective band of the corresponding distributions, in particular such that the coordinated, controlled and / or process-induced penetration of the working mixture into the pores in at least part of the surface area of ​​the porous, open-pored structural component takes place in a uniformly distributed manner and during the solidification and curing of the working mixture of the shell building material, a mechanical,A chemical or mechanical-chemical bond is created between the porous, open-pore, one-dimensional structural elements and structural components of the structure and the shell material. Particularly in the case where the porous, open-pore, one-dimensional structural element and structural component of the structure is made of wood, the chemical components of the shell material can be coordinated, controlled, and / or induced by a process in such a way that a chemical bond with the chemical components of wood, such as cellulose or lignin, can also be achieved.

[0074] Furthermore, an embodiment of the method for producing one-dimensional structural elements and structural components of the structure, such as spacers, in particular in the form of sleeves, rods, dowels or bolts, can comprise additive manufacturing (3D printing), manufacturing by injection and / or die casting or by pressing or punching.

[0075] Formwork production: An embodiment of the method for producing two-dimensional construction elements and load-bearing components of the construction, such as formwork made of wood, in particular in the form of panels or boards, generally comprises the preparation and proportional joining and mutual fastening, pressing and / or gluing of various starting materials such as wood chips, wooden boards or wooden planks and, if required, other substances and / or materials.In particular, the degree of fineness, chip size, chip geometry, material thicknesses and material dimensions as well as any other material properties of the various starting materials determine the quality properties of the two-dimensional construction elements, which are coordinated and optimized for their use for at least part of the construction, in particular for the inventive function or effect of the composite with a one-dimensional construction element and load-bearing component of the construction, such as spacers made of wood (so-called wood-wood composite) or for the inventive function or effect of the composite with a shell building material (so-called wood-concrete composite).

[0076] In this case, the function or effect according to the invention of a composite between one- and two-dimensional structural elements and structural components of the structure comprises the coordinated, controlled, and / or process-induced dissipation of occurring structural forces by means of a special layered or ply structure of wood panels or wood boards, in particular via the coordinated, controlled, and / or process-induced alignment of the wood fibers in the direction of the occurring structural forces. For example, in a composite of a 3-layer solid wood panel as a two-dimensional structural element with a one-dimensional structural element, such as a spacer, the mutual connection, fastening, sealing, and / or anchoring is carried out by means of a blind hole, and the layered structure of the 3-layer solid wood panel is manufactured and coordinated accordingly.that the thickness of the cover sheet corresponds to the distance from the cover sheet surface to the penetration depth of the blind hole and its wood fiber direction is aligned parallel to the longitudinal axis of the composite component, and the thickness of the remaining transverse or longitudinal layers or their wood fiber directions, which are located within the area of ​​the blind hole, are aligned in the longitudinal or transverse direction according to the structural forces occurring, in particular such that the coordinated, controlled and / or process-induced dissipation of the structural forces occurring corresponds to the coordinated, controlled and / or process-induced layer structure or their alignment of the wood fibers. A function or effect according to the invention of a composite between porous, open-pore two-dimensional structural elements and structural components of the structure, such as wooden formwork, and a shell material, comprises the coordinated,controlled and / or process-induced dissipation of occurring structural forces by means of a mechanical, chemical or mechanical-chemical combination, in particular via the coordinated, controlled and / or process-induced penetration of the working mixture of the shell building material into the pores in at least part of the surface area of ​​the porous, open-pore structural component, wherein the particle or grain size, the particle or grain geometry and / or their proportional distributions (e.g. particle or grain size distribution, distribution densities or distribution sums) of the starting materials in the working mixture are coordinated with the pore size, pore geometry and / or their proportional distributions (cumulative or relative pore volume distribution as a function of the pore radius) in at least part of the surface area of ​​the porous, open-pore structural component, in particular in such a way thatthat the particle or grain size and / or the particle or grain geometry of the starting materials in the working mixture is smaller than or equal to the pore size or pore geometry in at least part of the surface area of ​​the porous, open-pored structural component, in the respective band of the corresponding distributions and in particular such that the coordinated, controlled and / or process-induced penetration of the working mixture into the pores in at least part of the surface area of ​​the porous, open-pored structural component is evenly distributed and, during the solidification and curing of the working mixture of the shell building material, a mechanical, chemical or mechano-chemical bond is formed between the porous, open-pored two-dimensional structural elements and structural components of the structure and a shell building material. In particular in the event that the porous,If the open-pore two-dimensional structural element and load-bearing component of the structure is made of wood, the chemical components of the shell material can be matched, controlled and / or induced by a process in such a way that a chemical bond with the chemical components of wood, such as cellulose or lignin, can also be achieved.

[0077] Furthermore, an embodiment of the method for producing two-dimensional construction elements and structural components of the construction, such as formwork, in particular in the form of plates or panels, can comprise additive manufacturing (3D printing), manufacturing by injection molding and / or die casting or by pressing or punching.

[0078] Manufacturing reinforcements, anchoring aids, and materials: One embodiment of the process for manufacturing reinforcements, anchoring aids, elastic filling materials, or materials for sound or impact sound insulation generally involves the preparation and processing of various starting materials, such as iron or plastic materials and, if necessary, additional substances and / or materials. In particular, the material geometry, thicknesses, and dimensions, as well as any other material properties of the various starting materials, determine the quality characteristics of the reinforcements, anchoring aids, elastic filling materials, or materials for sound or impact sound insulation, which are tailored and optimized for use in at least one part of the structure.Furthermore, an embodiment of the method for producing reinforcements, anchoring aids, elastic filling materials or materials for sound or impact sound insulation can comprise additive manufacturing (3D printing), manufacturing by injection and / or die casting or by pressing or punching.

[0079] The above-mentioned processes for the production of filling materials, shell construction materials, one- and two-dimensional construction elements, reinforcements, anchoring aids, elastic filling materials and / or materials for sound or impact sound insulation are preferably carried out by means of automated processing or process steps, in particular their execution by means of a control method according to the invention (see below).

[0080] Processing of structural components: An embodiment of the method for processing one-dimensional structural elements and structural components of the construction, such as spacers, in particular in the form of sleeves, rods, dowels or bolts and / or two-dimensional structural elements and structural components of the construction, such as formwork, in particular in the form of panels or plates, generally comprises a shaping processing step with regard to its border and / or geometric shape and / or the attachment of anchoring forms and / or sealing forms by means of preferably automated processing or method steps, in particular their execution by means of a control method according to the invention, such as the computer-aided or computer-implemented numerical control of automated processing machines (e.g. CNC machines).The processing steps are procedurally coordinated, controlled and / or optimized for the use of the one- and two-dimensional structural components within at least one part of the construction, in particular for the inventive function or effect of their combination with one another and, if necessary, for an inventive function or effect of their combination, individually or together, with a shell building material.

[0081] Installing structural components: A further embodiment of the method for processing one-dimensional structural elements and structural components of the construction, such as spacers consisting of a porous, open-pored material such as wood, in particular in the form of sleeves, rods, dowels or bolts and / or two-dimensional structural elements and structural components of the construction, such as formwork consisting of a porous, open-pored material such as wood, in particular in the form of panels or plates, comprises installing the same with a working mixture of a installing material, such as installing the same with a working mixture of a mortar according to the invention.The working mixture of the filling material penetrates into the pores of at least part of the surface area of ​​the porous, open-pored one- and / or two-dimensional structural element in a manner coordinated, controlled and / or process-induced according to the invention by means of preferably automated processing or process steps, in particular their execution by means of a control method according to the invention, such as, for example, the computer-aided or computer-implemented numerical control of automated processing machines. The processing steps are process-coordinated, controlled and / or optimized for the use of the one- and two-dimensional structural components consisting of a porous, open-pored material, such as, for example,Wood, within at least one part of the construction, in particular to the inventive function or effect of their combination with one another and, if necessary, to an inventive function or effect of their combination, individually or together, with a shell building material.

[0082] Assembly of structural components: A further embodiment of the method for processing one-dimensional structural elements and structural components of the structure, such as spacers, in particular in the form of sleeves, rods, dowels or bolts and / or two-dimensional structural elements and structural components of the structure, such as formwork, in particular in the form of panels or plates, comprises the assembly of anchoring aids, sealing aids, technical components, construction-specific materials such as elastic filling materials or sound or impact sound insulation and / or reinforcements in or on the same by means of preferably automated assembly or process steps, in particular their execution by means of a control method according to the invention such as the computer-aided or computer-implemented numerical control of automated assembly machines (e.g. assembly robots).The assembly steps are procedurally coordinated, controlled and / or optimized for the use of the one- and two-dimensional structural components within at least one part of the construction, in particular for the inventive function or effect of their combination with one another and, if necessary, for an inventive function or effect of their combination, individually or together, with a shell building material.

[0083] Freezing out structural components: A further embodiment of the method for processing one-dimensional structural elements and structural components of the structure, such as spacers consisting of a porous, open-pored material such as wood, in particular in the form of sleeves, rods, dowels or bolts and / or two-dimensional structural elements and structural components of the structure, such as formwork consisting of a porous, open-pored material such as wood, in particular in the form of panels or plates, comprises freezing them out with, for example, water. The one- and / or two-dimensional structural elements are exposed to water for a period of time coordinated with the method, for exampleby displacing, whereby water in the liquid phase penetrates into the pores in at least a portion of the surface area of ​​the porous, open-pore one- and / or two-dimensional structural element in a coordinated, controlled, and / or process-induced manner by means of preferably automated processing or process steps, in particular their execution by means of a control method according to the invention, such as, for example, the computer-aided or computer-implemented numerical control of automated processing machines. Subsequently, the one- and / or two-dimensional structural elements are exposed to temperatures at or below the freezing point of water for a process-coordinated period of time.The water that has penetrated into the pores in at least part of the surface area of ​​the porous, open-pored one- and / or two-dimensional structural element freezes and causes them to swell or break open in a randomly distributed manner, thereby causing an intended increase in porosity or the number of open-pored pores. During the subsequent, process-coordinated drying phase of the one- and / or two-dimensional structural elements, the pores in at least part of the surface area remain increasingly swollen or broken open, which can be used for further process steps or functions or effects according to the invention, in particular for subsequent setting of the one- and / or two-dimensional structural elements with a working mixture of a setting material, such as the setting of the same with a working mixture of a mortar according to the invention.The processing steps are process-relatedly coordinated, controlled and / or optimized for the use of the one- and two-dimensional structural components consisting of a porous, open-pore material such as wood, within at least one part of the construction, in particular for the inventive function or effect of their combination with one another and, if necessary, for an inventive function or effect of their combination, individually or together, with a shell building material.

[0084] Formwork processing: A specific embodiment of the method for processing two-dimensional construction elements and load-bearing components of the structure, such as formwork, in particular in the form of panels or slabs, preferably comprises automated processing or method steps, in particular their execution by means of a control method according to the invention, such as the computer-aided or computer-implemented numerical control of automated processing machines (e.g. CNC machines). A specific embodiment of the method comprises the processing of a plurality of hexagonally symmetrically arranged bores in the surface of a formwork based on a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, which are arranged obliquely at an angle of 45° to the surface of the formwork.

[0085] A further, specific embodiment of the method for processing two-dimensional structural elements and load-bearing components of the structure, such as formwork, in particular in the form of panels or slabs, preferably comprises automated processing or process steps, in particular their execution by means of a control method according to the invention, such as, for example, computer-aided or computer-implemented numerical control of automated processing machines (e.g., CNC machines). A further, specific embodiment of the method comprises the processing of at least one shaping step based on a hexagonal grid with respect to the border and / or geometric shape thereof and / or the application of anchoring and / or sealing forms based on a hexagonal grid to the same, such as, for example, notches, rebates, grooves, and / or ridges.

[0086] Processing reinforcements, anchoring aids and materials: One embodiment of the

[0087] A method for processing reinforcements, anchoring aids, elastic filling materials or materials for sound or impact sound insulation generally comprises a shaping processing step with regard to its border and / or geometric shape and / or the application of anchoring shapes and / or sealing shapes by means of preferably automated processing or method steps, in particular their execution by means of a control method according to the invention, such as, for example, the computer-aided or computer-implemented numerical control of automated processing machines (e.g., CNC machines).The processing steps are procedurally coordinated, controlled and / or optimized for the use of the reinforcements, anchoring aids, elastic filling materials or materials for sound or impact sound insulation within at least one part of the construction, in particular for the inventive function or effect of their combination with one- and / or two-dimensional construction elements and structural components of the construction and, if necessary, for an inventive function or effect of their combination, individually or together, with a shell building material.

[0088] Manufacturing of component scaffolding: An embodiment of the method for producing a raw, partial or complete component scaffolding, as a three-dimensional construction element of the construction according to the invention made of one- and two-dimensional construction elements in a composite construction, which can be made as required in the form of raw, partial or complete building modules, of raw, partial or complete modular building blocks, of raw, partial or complete building elements, of raw, partial or complete components and / or raw, partial or complete constructions of a construction, generally comprises shaping process steps such as the step-by-step, partial or complete introduction, assembly, joining, connecting, fastening, sealing and / or anchoring of the processed starting materials of the load-bearing components such as formwork, spacers, reinforcements, anchoring aids, sealing aids, technical components and / or other materials such aselastic filling materials or materials for sound or impact sound insulation, with, against and among each other by means of screw, press, glue and / or adhesive bonds, by means of anchoring and / or sealing forms such as drilled, threaded, dovetail, rebate, tongue, groove or notch connections, by means of anchoring and / or sealing aids such as press, drilled, threaded, thread-cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread and / or by means of general milling or countersinking or by means of commercially available means of sealing and fastening technology. The method steps described above can be carried out by means of preferably automated assembly or method steps, in particular their execution by means of a control method according to the invention such as the computer-aided or computer-implemented numerical control of automated assembly machines (e.g.Assembly robots), creating a connection, fastening, sealing, and / or anchoring between the one- and two-dimensional structural elements of the structure. Subsequently, if required, structural extensions and / or technical components can be mounted in and / or onto the basic, partial, or complete component framework. The process steps described above for producing a basic, partial, or complete component framework can be applied to all of the above-described embodiments of a basic, partial, or complete component framework.A special embodiment of the method for producing a raw, partial or complete component framework, as a three-dimensional construction element of the construction according to the invention made of one- and two-dimensional construction elements in a composite construction, which can be made as required in the form of raw, partial or complete building modules, of raw, partial or complete modular building blocks, of raw, partial or complete building elements, of raw, partial or complete components and / or raw, partial or complete constructions of a construction, comprises automated assembly or process steps, in particular their execution by means of a control method according to the invention, such as, for example, preferably the computer-aided or computer-implemented numerical control of the process steps, in particular the computer-aided or computer-implemented numerical control of an automated assembly machine (e.g.Assembly robots) for assembling the starting materials in the form of one- or two-dimensional construction elements such as formwork or spacers. A specific embodiment comprises the insertion and installation of a plurality of spacers into the hexagonally symmetrically arranged bores previously made in a formwork, in particular designed as formwork-penetrating bores or as blind bores, in a predetermined, final position, based on a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, which are arranged obliquely at an angle of 45° to the surface of the formwork.

[0089] Adhesive bond: An extended embodiment of the method for producing a raw, partial, or complete structural component, as a three-dimensional structural element of the construction according to the invention made of one- and two-dimensional structural elements in a composite construction, comprises an extended form of connection, fastening, sealing, and / or anchoring between the one- and two-dimensional structural elements of the construction in the event that the one- or two-dimensional structural elements of the structural component are made of a porous, open-pore material, such as wood. In this case, the one- or two-dimensional structural elements are filled with a filling material in the form of a working mixture (e.g., mortar or synthetic resin). The filling material penetrates, in a flowable or liquid state, into the pores in at least part of the surface area of ​​the one- or two-dimensional structural elements.During the subsequent gradual, partial, or complete insertion, assembly, joining, connecting, fastening, sealing, and / or anchoring of the one- and two-dimensional structural elements with, against, and among each other, they come into contact with each other, particularly the area that was previously filled with a filling material in the form of a working mixture. As the filling material subsequently hardens, an adhesive bond is created between the one- and two-dimensional structural elements of the structure.

[0090] Production of component framework: An embodiment of the method for producing a raw, partial or complete component framework, as a three-dimensional construction element of the construction according to the invention made of one- and two-dimensional construction elements in a composite construction, comprises shaping process steps such as, for example,the gradual, partial or complete assembly or joining of at least one raw, partial or complete component framework in the form of at least one raw, partial or complete building module, one raw, partial or complete modular building block, one raw, partial or complete building element and / or one raw, partial or complete component and / or the gradual or incremental and additive joining, connecting, fastening, sealing and / or anchoring of raw, partial or complete component frameworks in the form of raw, partial or complete building modules, of raw, partial or complete modular building blocks, of raw, partial or complete building elements and / or of raw, partial or complete components with, against and among each other by means of screwing, pressing, gluing and / or adhesive bonds, by means of anchoring and / or sealing forms such as e.g. B. Drilled, threaded, dovetail, rebate, tongue, groove or notch connections, using anchoring and / or sealing aids such as B.Pressing, drilling, threading, thread-cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread and / or by means of general milling or countersinking or by means of commercially available means of sealing and fastening technology. The method steps described above can be carried out by means of preferably automated assembly or method steps, in particular their execution by means of a control method according to the invention, such as the computer-aided or computer-implemented numerical control of automated assembly machines (e.g. assembly robots), thereby creating a connection, fastening, sealing and / or anchoring between individual raw, partial or complete component frameworks in the form of raw, partial or complete building modules, raw, partial or complete modular building blocks, raw, partial or complete building elements and / or raw, partial or complete components.Subsequently, if necessary, structural extensions and / or technical components can be mounted in and / or onto the basic, partial, or complete component scaffold. The process steps described above for manufacturing a basic, partial, or complete component scaffold can be applied to all of the above-described embodiments of a basic, partial, or complete component scaffold.

[0091] Production of a raw, partial or complete construction (dry): One embodiment of the process for producing a raw, partial or complete construction generally includes shaping process steps such as, for example,the gradual, partial or complete assembly or joining of at least one raw, partial or complete component framework, which, if required, is designed in the form of at least one raw, partial or complete construction module, one raw, partial or complete modular building block, one raw, partial or complete building element and / or one raw, partial or complete component and / or the gradual or incremental and additive joining, connecting, fastening, sealing and / or anchoring of raw, partial or complete component frameworks, which, if required, are designed in the form of raw, partial or complete construction modules, of raw, partial or complete modular building blocks, of raw, partial or complete building elements and / or of raw, partial or complete components and are connected to, against and among each other by means of screw, press, glue and / or adhesive bonds, by means of anchoring and / or sealing forms such as e.g.Drilled, threaded, dovetail, rebate, tongue, groove or notch connections, by means of anchoring and / or sealing aids such as press, drill, thread, thread-cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread and / or by means of general milling or countersinking or by means of commercially available means of sealing and fastening technology. The method steps described above can be carried out by means of preferably automated assembly or method steps, in particular their execution by means of a control method according to the invention such as the computer-aided or computer-implemented numerical control of automated assembly machines (e.g.Assembly robots) to create a connection, fastening, sealing and / or anchoring between individual raw, partial or complete component scaffolds, which, if required, are designed in the form of raw, partial or complete construction modules, raw, partial or complete modular building blocks, raw, partial or complete construction elements and / or raw, partial or complete components. Subsequently, if required, construction extensions and / or technical components can be mounted in and / or onto the raw, partial or complete component scaffold. The method steps described above for producing a raw, partial or complete component scaffold can be used for all of the above-described embodiments of a raw, partial or complete component scaffold.

[0092] Connection: An extended embodiment of the method for producing a shell, partial, or complete structure comprises an extended embodiment of a connection, fastening, sealing, and / or anchoring between individual shell, partial, or complete building modules, individual shell, partial, or complete modular building blocks, individual shell, partial, or complete building elements, individual shell, partial, or complete components, and / or individual shell, partial, or complete structures. These are provided on the front and / or longitudinal sides with a mutually overlapping fold and / or with a mutually sliding and interlocking profile and provided with mutually corresponding reinforcements.Following assembly or joining, connecting, fastening, sealing and / or anchoring thereof, a shell material or a conventional mortar / concrete in the form of a working mixture is introduced into at least one design-related cavity of the connection and sealing point and the mutually overlapping fold. During subsequent solidification and curing of the shell material, an expanded embodiment of a connection, fastening, sealing and / or anchoring is created between individual raw, partial or complete building modules, individual raw, partial or complete modular building blocks, individual raw, partial or complete building elements, individual raw, partial or complete components and / or individual raw, partial or complete structures, which in particular provides reinforcement in the second axis (biaxial reinforcement).

[0093] Manufacturing of a raw, partial or complete structure (wet): An embodiment of the method for manufacturing a raw, partial or complete structure, which can be carried out as required in the form of raw, partial or complete building modules, raw, partial or complete modular building blocks, raw, partial or complete building elements, raw, partial or complete components and / or raw, partial or complete structures of a structure, generally comprises shaping process steps such as the step-by-step, partial or complete assembly or joining of at least one raw, partial or complete component framework and / or the step-by-step or incremental and additive joining, connecting, fastening, sealing and / or anchoring of raw, partial or complete component frameworks with, against and among each other by means of screw, press, glue and / or adhesive bonds, by means of anchoring and / or sealing forms such asDrilled, threaded, dovetail, rebate, tongue, groove or notch connections, by means of anchoring and / or sealing aids such as press, drilled, threaded, thread-cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread and / or by means of general milling or recesses or by means of commercially available means of sealing and fastening technology and, if necessary, the partial or complete installation of a hardening shell building material which is introduced in the form of a working mix, i.e. in loose, liquid or flowable form, into at least one formwork as a shaping formwork / casting mold and, if necessary, into at least one additional and / or independent, temporary formwork / casting mold.The method steps described above can be carried out by means of preferably automated assembly or process steps, in particular their execution by means of a control method according to the invention, such as, for example, computer-aided or computer-implemented numerical control of automated assembly machines (e.g., assembly robots), thereby creating a connection, fastening, sealing, and / or anchoring between the one- and two-dimensional structural elements of the structure, between individual raw, partial, or entire component frameworks, and / or, if necessary, between the one- and two-dimensional structural elements of the structure in the hardening shell material. Subsequently, if necessary, structural extensions and / or technical components can be mounted in and / or onto the raw, partial, or entire structure.The method steps described above for producing a raw, partial or complete construction can be used for all embodiments of a raw, partial or complete construction described above.

[0094] Manufacturing of a raw, partial or complete construction: One embodiment of the process for manufacturing a raw, partial or complete construction generally includes shaping process steps such as, for example,the gradual, partial or complete assembly or joining of at least one raw, partial or complete component framework, which, if required, is designed in the form of at least one raw, partial or complete construction module, one raw, partial or complete modular building block, one raw, partial or complete building element and / or one raw, partial or complete component and / or the gradual or incremental and additive joining, connecting, fastening, sealing and / or anchoring of raw, partial or complete component frameworks, which, if required, are designed in the form of raw, partial or complete construction modules, of raw, partial or complete modular building blocks, of raw, partial or complete building elements and / or of raw, partial or complete components, with, against and among each other by means of screw, press, glue and / or adhesive bonds, by means of anchoring and / or sealing forms such as e.g.Drilled, threaded, dovetail, rebate, tongue, groove or notch connections, by means of anchoring and / or sealing aids such as press, drilled, threaded, thread-cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread and / or by means of general milling or recesses or by means of commercially available means of sealing and fastening technology and, if necessary, the partial or complete installation of a hardening shell building material which is introduced in the form of a working mix, i.e. in loose, liquid or flowable form, into at least one formwork as a shaping formwork / casting mold and, if necessary, into at least one additional and / or independent, temporary formwork / casting mold.The method steps described above can be carried out by means of preferably automated assembly or process steps, in particular their execution by means of a control method according to the invention, such as computer-aided or computer-implemented numerical control of automated assembly machines (e.g. assembly robots), whereby a connection, fastening, sealing and / or anchoring is created between individual raw, partial or complete component frameworks in the form of raw, partial or complete building modules, raw, partial or complete modular building blocks, raw, partial or complete building elements and / or raw, partial or complete components and / or, if required, the one- and two-dimensional construction elements of the construction in the hardening shell building material. Subsequently, if required, construction extensions and / or technical components can be mounted in and / or onto the raw, partial or complete construction.The method steps described above for producing a raw, partial or complete construction can be used for all embodiments of a raw, partial or complete construction described above.

[0095] Manufacturing construction: One embodiment of the method for manufacturing a construction generally comprises shaping process steps such as the step-by-step, partial or complete assembly or joining of at least one raw or partial construction and / or the step-by-step or incremental and additive joining, connecting, fastening, sealing and / or anchoring of raw or partial constructions with, against and among each other by means of screw, press, glue and / or adhesive bonds, by means of anchoring and / or sealing forms such as drilled, threaded, dovetail, rebate, tongue, groove or notch connections, by means of anchoring and / or sealing aids such as press, drill, thread, thread cutting and / or screw sleeves and / or screw-in nuts and / or sleeves with an external and / or internal thread and / or by means of general insertion or insertionMilling or by means of commercially available means of sealing and fastening technology and, if required, the partial or complete installation of a hardening shell building material, which is introduced in the form of a working mixture, i.e. in loose, liquid or flowable form, into at least one formwork as a shaping formwork / casting mold and, if necessary, into at least one additional and / or independent, temporary formwork / casting mold. The method steps described above can be carried out by means of preferably automated assembly or method steps, in particular their execution by means of a control method according to the invention, such as, for example, the computer-aided or computer-implemented numerical control of automated assembly machines (e.g.Assembly robots) are used to create a connection, fastening, sealing, and / or anchoring between individual shell or partial structures and / or, if necessary, the one- and two-dimensional structural elements of the structure in the hardening shell material. Subsequently, if necessary, structural extensions and / or technical components can be mounted in and / or onto the shell or partial structure. The process steps for producing a structure described above can be applied to all of the above-described embodiments of a structure.Assembly cage: An optional embodiment of the method for producing a raw, partial or complete component scaffold or a raw, partial or complete construction comprises the deployment and use of an assembly cage, which serves as an assembly template for the shaping insertion, assembly, joining, connecting, fastening, sealing and / or anchoring of the processed starting materials of the structural components such as formwork, spacers, reinforcements, anchoring aids, sealing aids, technical components and / or other materials such as elastic filling materials or materials for sound or impact sound insulation, of the raw or partial component scaffold or the raw or partial construction in relation to the border and / or internal or external geometric shape of a raw, partial or complete component scaffold or a raw, partial or complete construction.In this process, individual machined starting materials of the structural components to be assembled, individual raw or partial component scaffolds or individual raw or partial constructions are introduced into the assembly cage for the shaping assembly step and fixed by means of the same in order to maintain their final position and / or spacing for the further process steps.

[0096] Auxiliary assembly tool: An optional embodiment of the method for producing a raw, partial or complete component scaffold or a raw, partial or complete construction comprises the deployment and use of an auxiliary assembly tool which serves as an assembly jig for the shaping insertion, assembly, joining, connecting, fastening, sealing and / or anchoring of the processed starting materials of the structural components such as formwork, spacers, reinforcements, anchoring aids, sealing aids, technical components and / or other materials such as elastic filling materials or materials for sound or impact sound insulation, of the raw or partial component scaffold or the raw or partial constructions with regard to the spacing of the two-dimensional construction elements of the construction such as formwork.The assembly tool is inserted into a designated opening in at least one two-dimensional structural element. By means of a finite rotational movement of the assembly tool, the at least one two-dimensional structural element is brought into a predetermined position, spacing, or distance with the aid of an assembly mold, and positioned and fixed there in order to maintain its final position and / or spacing for the subsequent process steps.

[0097] Extraterrestrial Manufacturing Construction: An optional embodiment of all the above-described general or extended embodiments of the method for manufacturing a raw, partial or complete component framework or a raw, partial or complete construction comprises their implementation for extraterrestrial applications such as space transport systems (space travel), surface habitats (lunar or planetary bases) or orbital habitats (space stations), in particular by means of preferably automated assembly or process steps, in particular their implementation by means of a control method according to the invention, such as the computer-aided or computer-implemented numerical control of automated assembly machines (e.g. assembly robots). The control method

[0098] The control method comprises the process-engineering control of the manufacturing process of the structure, in particular the control of the process steps for manufacturing, processing, and / or assembling the starting materials and / or the control of the process steps for manufacturing the structure in its various embodiments. In its general embodiment, the control method comprises reading input information (input), processing the input information, and creating output information (output), which is preferably implemented in the form of an input-processing-output architecture (IPO).

[0099] The input information may include real-time signals, measured variables, and / or system-internal or system-external processed information of a value, in particular a material-specific or design-specific value, or input information of a machine-specific relevant state variable. Additionally, the input information may include stored information or information from publicly accessible sources relevant to the manufacture of the design, as well as information in the form of forecasts and predictions relevant to the manufacture of the design.Examples include: material-specific values ​​such as material type, material condition, and / or material properties (particle or grain size, particle or grain geometry, their distributions, chip size, chip geometry, degree of fineness, grinding degree, material geometry, material thicknesses, material dimensions), or construction-specific values ​​(designs, type of construction, shape and dimensions, materialization). Further examples include information on building use, building standards, building requirements, interior layouts and arrangements such as room and floor layouts, as well as specific physical or psychological needs and preferences of users and / or residents.

[0100] Processing the input information includes reading, comparing, calculating, and / or deriving a value from at least one piece of input information and converting, preparing, and / or creating at least one value in the form of at least one piece of output information. These can include instructions for initiating or implementing process steps or rule-based control commands that trigger the process-related functions or effects of the process steps using control technology.

[0101] In its general embodiment, the control method comprises reading, comparing, calculating and / or deriving a value from at least one piece of input information and converting, processing and / or creating a value in the form of at least one piece of output information which, by means of control or regulation technology, regulates and controls the individual process steps, in particular the process steps for producing, processing and / or assembling the starting materials and / or the process steps for producing the construction in its various embodiments. On the one hand, the control method can be designed centrally, i.e. implemented by means of a central control unit which centrally reads in, compares, calculates, prepares and processes the required input information and then summarizes, prepares or creates the output information either individually or in groups.On the other hand, the control process can be designed in a decentralized manner and consist of several independent control processes, i.e. it can be implemented by means of decentralized control units, in which each individual control unit reads in, compares, calculates, prepares and processes the required input information and then summarizes, prepares or creates the output information either individually or in groups.

[0102] A general embodiment of the control method comprises the process-engineering control of the manufacturing process of the structure, in particular the process-engineering control of the process steps for producing the starting materials in the form of dry or working mixtures such as, for example, filling materials or shell construction materials, in the form of one- or two-dimensional construction elements such as, for example, formwork or spacers and / or in the form of anchoring aids, sealing aids, construction-specific materials such as, for example, elastic filling materials or sound or impact sound insulation and / or reinforcements.

[0103] A further embodiment of the control method comprises the process-engineering control of the manufacturing process of the construction, in particular the process-engineering control of the process steps for processing the starting materials in the form of one- or two-dimensional construction elements such as formwork or spacers.

[0104] A further embodiment of the control method comprises the process-engineering control of the manufacturing process of a component framework, in particular the process-engineering control of the process steps for manufacturing a raw, partial or complete component framework, which, if required, can be designed in the form of raw, partial or complete building modules, raw, partial or complete modular building blocks, raw, partial or complete building elements and / or raw, partial or complete components.

[0105] A further embodiment of the control method comprises the process-engineering control of the manufacturing process of a construction, in particular the process-engineering control of the process steps for manufacturing a raw, partial or complete construction, which, if required, can be carried out in the form of raw, partial or complete construction modules, raw, partial or complete modular building blocks, raw, partial or complete construction elements and / or raw, partial or complete components.

[0106] An extended embodiment of the control method, which is designed either centrally or decentrally, comprises the process control, in particular the computer-aided or computer-implemented numerical control of the process steps for producing, processing and / or assembling the starting materials and / or the computer-aided or computer-implemented numerical control of the process steps for producing the construction in its various embodiments, in particular the computer-aided or computer-implemented numerical control of an automated processing machine (e.g. CNC machine) and / or an automated assembly machine (e.g. assembly robot).The extended control method is based on a computer program (software) that reads, compares, calculates, and / or processes at least one piece of input information, converts it into at least one suitable data format, and prepares or creates at least one piece of output information from it. These can include instructions for initiating or implementing process steps or rule-based control commands that trigger the process-engineering functions or effects of the process steps using control technology, in particular the computer-aided or computer-implemented numerical control of automated processing machines (e.g., CNC machines) and / or automated assembly machines (e.g., assembly robots).

[0107] A specific embodiment of the computer-aided or computer-implemented control method comprises a computer-implemented tool (software tool) in the form of a computer program for the evaluation, planning, manufacture, processing, prefabrication, assembly, and / or execution of a shell, partial, or complete structure. Possible input information includes information and / or data on the type, shape / dimensions, location, materialization, costs, use / construction standard, user preferences, and / or requirements of a shell, partial, or complete structure, which are fed to the computer program for processing via a user interface (HMI).The calculation and / or processing steps of the computer-implemented tool (software tool) include processing the input information, such as reading, comparing, calculating, and / or deriving a value from it, and converting, preparing, and / or creating a value in the form of output information. This can include, for example, the divisions and sizes of the components, the size / number of hexagonal grids, the arrangement / number of spacers, system parameters, and / or dimensions of the components and / or the one- and / or two-dimensional design elements of the basic, partial, or complete construction.

[0108] A specific embodiment of the computer-aided control method comprises the computer-aided or computer-implemented numerical control of the process steps, in particular the computer-aided or computer-implemented numerical control of an automated processing machine (e.g., CNC machine) for processing the starting materials in the form of one- or two-dimensional construction elements such as formwork or spacers. A specific embodiment of the computer-aided control method comprises the creation of a plurality of hexagonally symmetrically arranged bores in the surface of a formwork based on a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, which are arranged obliquely at an angle of 45° to the surface of the formwork.

[0109] A further specific embodiment of the computer-aided control method comprises the computer-aided or computer-implemented numerical control of the process steps, in particular the computer-aided or computer-implemented numerical control of an automated processing machine (e.g., a CNC machine) for processing the starting materials in the form of one- or two-dimensional construction elements such as formwork or spacers. A further specific embodiment of the computer-aided control method comprises at least one shaping processing step based on a hexagonal grid with respect to the border and / or geometric shape of a formwork and / or the application of hexagonally symmetrical anchoring and / or sealing forms based on a hexagonal grid to the formwork, such as notches, folds, grooves, and / or ridges.

[0110] A further, special embodiment of the computer-aided control method comprises the computer-aided or computer-implemented numerical control of the method steps, in particular the computer-aided or computer-implemented numerical control of an automated assembly machine (e.g. assembly robot) for assembling the starting materials in the form of one- or two-dimensional construction elements such as formwork or spacers.A specific embodiment of the computer-aided control method comprises the insertion and installation of a plurality of spacers into the hexagonally symmetrically arranged bores previously made in a formwork, in particular designed as formwork-penetrating bores or as blind bores, in a predetermined, final position, on the basis of a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, which are arranged obliquely at an angle of 45° to the surface of the formwork.

[0111] An optional embodiment of the computer-aided control method consists in executing it as an intelligent, computer-aided control method in the form of an intelligent computer program. The intelligent computer program reads, compares, calculates, processes, and / or creates additional input information in the form of model and / or comparison calculations executed internally or externally within the system. Furthermore, the intelligent computer program can be equipped with and / or networked with artificial intelligence (AI) algorithms, in particular with algorithms for statistical or reinforced learning. The intelligent computer program reads, compares, calculates, and / or processes the input information specified by the intelligent measurement and / or control system, converts it into suitable data formats, and creates and prepares output information from it.These may include instructions for initiating or implementing process steps or rule-based control commands that trigger the process-engineering functions or effects of the process steps by means of control or regulation technology, in particular the computer-aided or computer-implemented numerical control of automated processing machines (e.g. CNC machines) and / or automated assembly machines (e.g. assembly robots).

[0112] An optional embodiment of the intelligent, computer-aided control method consists in executing the process steps for manufacturing, relocating, processing, or assembling the starting materials of the construction, as well as the process steps for manufacturing component frameworks and constructions in various embodiments, using artificial intelligence (AI) algorithms, in particular using algorithms for statistical or reinforced learning. These algorithms are trained on a selection of general, existing process steps for manufacturing, relocating, processing, or assembling the starting materials of the construction, as well as on a selection of general, existing process steps for manufacturing component frameworks and constructions in various embodiments (AI system training) and subsequently fine-tuned on a selection of construction-specific process steps (AI system fine-tuning).The automated processing or assembly machines carry out the individual process steps using artificial intelligence (AI) algorithms, in particular algorithms for statistical or reinforced learning.

[0113] An optional embodiment of all of the above-described general, extended special or optional embodiments of the control method for the process-engineering control of the process steps for producing, processing and / or assembling the starting materials and / or the process-engineering control of the process steps for producing the construction in its various embodiments comprises their implementation for extraterrestrial applications such as space transport systems (space travel), surface habitats (lunar or planetary bases) or orbital habitats (space stations), in particular their implementation by means of computer-aided or computer-implemented numerical controls of automated processing machines (e.g. CNC machines) and / or automated assembly machines (e.g. assembly robots).

[0114] Short description of the drawings

[0115] Fig. 1 is a partially sectioned, perspective view of an embodiment of a partial construction in the form of a ceiling element

[0116] Fig. 2a - 2l schematic cross-sectional representations of a construction comprising at least two spaced-apart shells and a space defined by them and enclosed between them according to various embodiments of the invention

[0117] Fig. 3a, b schematic cross-sectional representations of a construction comprising a construction extension according to further embodiments of the invention

[0118] Fig. 3c, d, e, f schematic cross-sectional views of a construction comprising a heating and / or cooling circuit according to further embodiments of the invention

[0119] Fig. 4a - 4k schematic cross-sectional representations of a construction comprising at least two spaced-apart shells and a space defined by them and enclosed between them according to various embodiments of the invention

[0120] Fig. 5a, b schematic cross-sectional representations of a construction comprising a construction extension according to further embodiments of the invention

[0121] Fig. 5c, d, e, f schematic cross-sectional representations of a construction comprising a heating and / or cooling circuit according to further embodiments of the invention Fig. 6a1 - a6 schematic cross-sectional representations of a connection, fastening, sealing or anchoring according to various embodiments of the invention

[0122] Fig. 7a, b schematic cross-sectional representations of a connection, fastening, sealing or anchoring according to various embodiments of the invention

[0123] Fig. 7 c, d schematic cross-sectional representations of various embodiments of the invention

[0124] Fig. 8a1 - b2 schematic cross-sectional representations of structural components according to various embodiments of the invention

[0125] Fig. 9a, b schematic cross-sectional views of an anchoring, connecting and sealing point according to a further embodiment of the invention

[0126] Fig. 10a1 - a4 schematic cross-sectional representations of connecting and sealing forms according to a further embodiment of the invention

[0127] Fig. 11 a1 - a3 schematic representations of an assembly auxiliary tool according to a further embodiment of the invention

[0128] Fig. 12a, b, c, d schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0129] Fig. 13a, b, c, d schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0130] Fig. 14a, b, c, d schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0131] Fig. 15a, b, c, d schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0132] Fig.16a, b, c schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0133] Fig. 17a, b schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0134] Fig. 18a, b schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0135] Fig. 19 is a schematic diagram illustrating a method for manufacturing the construction according to another embodiment of the invention

[0136] Fig. 20a, b schematic representations to illustrate a method for producing the construction according to further embodiments of the invention

[0137] Fig. 21 is a schematic diagram illustrating a method for manufacturing the construction according to another embodiment of the invention

[0138] Fig. 22 is a schematic diagram illustrating a method for manufacturing the construction according to another embodiment of the invention

[0139] Fig. 23 is a schematic diagram illustrating a method for producing the construction according to a further embodiment of the invention. Fig. 24 is a schematic diagram illustrating a method for producing the construction according to a further embodiment of the invention.

[0140] Way to implement the invention

[0141] Fig.1 shows a partially sectioned, perspective view of a partial construction (11), as an embodiment of the construction (11) according to the invention, in the form of a component (54).

[0142] Fig. 2a - 1 show schematic cross-sectional representations of a floor, ceiling, and / or roof structure as exemplary embodiments of the structure (11) according to the invention, which includes at least one component framework (12) of a preferred embodiment, comprising a composite of one- and two-dimensional structural elements and load-bearing components of the structure (11), and, if necessary, a shell construction material (13). In particular, the exemplary embodiments shown can be expanded as desired by a reflection at the center plane of the space delimited by the at least two spaced-apart shells and enclosed between them.

[0143] Fig. 2a and 2b show schematic cross-sectional representations of a structure (11) with at least two spaced-apart shells (14a, 14b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) which contains a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b). These spacers are anchored in at least one shell (14a, 14b) adjacent to the gap (16) and / or in other structural components, such as formwork (1), and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14a, 14b) adjacent to the gap.The component framework (12) further comprises at least one formwork (1) which is arranged in at least one of the at least two spaced-apart shells (14a, 14b) and at least partially delimits said shells laterally. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b). Fig. 2a additionally shows shell spacers (3) which are arranged in at least one of the at least two spaced-apart shells (14b) and anchored in at least one formwork (1). At least one of the at least two spaced-apart shells (14a, 14b) further comprises at least one reinforcement (2).The structure (11) also comprises a shell material (13) which at least partially fills at least one of the at least two spaced-apart shells (14a, 14b), at least partially adjoins at least one formwork (1), and at least partially adjoins the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b). Figs. 2c and 2d show schematic cross-sectional representations of a structure (11) with at least two spaced-apart shells (14, 15) and an intermediate space (16) delimited by and enclosed between them.The structure (11) comprises, on the one hand, a component framework (12) which contains a plurality of intermediate space spacers (4) arranged in the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14, 15). These spacers are anchored in at least one shell (14, 15) adjacent to the intermediate space (16) and / or in further structural components, such as formwork, and are arranged at an angle other than 90° to the surface defining the intermediate space of a shell (14, 15) adjacent to the intermediate space. Furthermore, the component framework (12) contains at least one formwork (1) which completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (1), and therefore the intermediate space spacers (4) are anchored in at least one single formwork. Fig.2d additionally includes at least one formwork (1) arranged in at least one of the at least two spaced-apart shells (14) and at least partially laterally delimiting said shells. In addition, the component framework (12) includes at least one formwork (17) arranged in the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14, 15). At least one of the at least two spaced-apart shells (14) further includes at least one reinforcement (2). The structure (11) further comprises a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially borders the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14, 15).

[0144] Fig. 2e shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14, 15a, 15b) and spaces (16a, 16b) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of spacer supports (4) arranged in the spaces (16a, 16b) delimited by the at least two spaced-apart shells (14, 15a, 15b) and enclosed between them. The spacer supports (4) are anchored in at least one shell (14, 15a, 15b) adjacent to the spaces (16a, 16b) and / or in other structural components, such as formwork, and are arranged at an angle other than 90° to the surface of a shell (14, 15a, 15b) adjacent to the spaces, which surface delimits the spaces.The component framework (12) further comprises at least two formworks (1, 17), which in turn completely form at least one of the at least two spaced-apart shells (15a, 15b) in that they are constructed using a single formwork (1, 17), and therefore the space spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the spaces (16a, 16b) delimited by and enclosed between the at least two spaced-apart shells (14, 15a, 15b). At least one of the at least two spaced-apart shells (14) further comprises at least one reinforcement (2).The construction (11) comprises, on the other hand, a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially adjoins at least one of the intermediate spaces (16a) delimited by the at least two spaced-apart shells (14, 15a, 15b) and enclosed between them.

[0145] Fig. 2f shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (15a, 15b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). These spacers are anchored in at least one shell (15a, 15b) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged at an angle other than 90° to the surface delimiting the gap of a shell (15a, 15b) adjacent to the gap.The component framework (12) further comprises at least one formwork (1) which completely forms at least one of the at least two spaced-apart shells (15a, 15b) by being constructed using a single formwork (1), and therefore the space spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). The construction (11) shown here does not comprise any shell building material (13).

[0146] Fig. 2g shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14, 15) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). These spacers are anchored in at least one shell (14, 15) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14, 15) adjacent to the gap.The component framework (12) further includes at least one formwork (1) that completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (1), and therefore the space spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) includes at least one formwork (17) that is arranged in the space (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15).The structure (11) also comprises a shell construction material (13) which at least partially fills at least one of the at least two spaced-apart shells (14), at least partially adjoins at least one formwork (1), and at least partially adjoins the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). The structure (11) additionally includes at least one formwork (1) which is arranged in at least one of the at least two spaced-apart shells (14), at least partially delimits it laterally, and has at least one anchoring form (60) which ensures at least one anchoring of the shell construction material (13) therein and can thus act as reinforcement for the shell construction material (13).

[0147] Fig. 2h shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (15a, 15b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). These spacers are anchored in at least one shell (15a, 15b) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (15a, 15b) adjacent to the gap.The component framework (12) further comprises at least two formworks (1, 17) which completely form at least one of the at least two spaced-apart shells (15a, 15b) by being constructed using a single formwork (1, 17), and therefore the spacer elements (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). The construction (11) shown here does not comprise any shell building material (13).

[0148] Fig. 2i shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (15a, 15b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). These spacers are anchored in at least one shell (15a, 15b) adjacent to the gap (16) and / or in other structural components, such as formwork (1, 17), and are arranged at an angle other than 90° to the surface delimiting the gap of a shell (15a, 15b) adjacent to the gap.The component framework (12) further comprises at least one formwork (17) which completely forms at least one of the at least two spaced-apart shells (15a, 15b) by being constructed using a single formwork (17), and therefore the gap spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least two formworks (1, 17) which are arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). The construction (11) shown here does not comprise any shell building material (13). Fig. 2j shows a schematic cross-sectional view of a construction (11) with at least two spaced-apart shells (14, 15) and a gap (16) delimited by and enclosed between them.The structure (11) comprises, on the one hand, a component framework (12) which contains a plurality of intermediate space spacers (4) arranged in the intermediate space (16) delimited by the at least two spaced-apart shells (14, 15) and enclosed therebetween. These spacers are anchored in at least one shell (14, 15) adjacent to the intermediate space (16) and / or in further structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface of a shell (14, 15) adjacent to the intermediate space, which surface delimits the intermediate space. Furthermore, the component framework (12) contains at least one formwork (17) which completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (17), and therefore the intermediate space spacers (4) are anchored in at least one single formwork.In addition, the component framework (12) includes at least one formwork (17) arranged in the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14, 15). At least one of the at least two spaced-apart shells (14) further includes at least one reinforcement (2). The structure (11) also comprises a shell construction material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially borders the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14, 15).

[0149] Fig. 2k shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14a, 14b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b). These spacers are anchored in at least one shell (14a, 14b) adjacent to the gap (16) and / or in other structural components, such as formwork (1, 17), and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14a, 14b) adjacent to the gap.The component framework (12) further comprises at least two formworks (1, 17) arranged in the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14a, 14b). At least one of the at least two spaced-apart shells (14a, 14b) further comprises at least one reinforcement (2). The structure (11) further comprises a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14a, 14b) and at least partially borders the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14a, 14b).

[0150] Fig. 2I corresponds to Fig. 2k, which shows a schematic cross-sectional view of a structure (11) with at least two shells (14a, 14b) spaced apart from one another and an intermediate space (16) delimited by them and enclosed between them, wherein at least one intermediate space spacer (4) is anchored in the first shell (14a) adjacent to the intermediate space (16) and / or further structural components, such as formwork (1, 17), and does not touch the second shell (14b) adjacent to the intermediate space (16), and at least one intermediate space spacer (4) is anchored in the second shell (14b) adjacent to the intermediate space (16) and / or further structural components, such as formwork (1, 17), and does not touch the first shell (14a) adjacent to the intermediate space (16). The formwork (1) shown here can also be referred to as stabilization formwork.

[0151] Fig. 3a - f show schematic cross-sectional representations of an extended floor, ceiling and / or roof construction, as embodiments of the construction according to the invention (11).

[0152] Fig. 3a shows a schematic cross-sectional view of an extended structure (11) which, on its side facing the upper floor (9), is adjacent to and bounded by a structural extension (18), such as a conventional floor structure. If the structure (11) is a roof structure, the structural extension (18) may include a conventional roof or exterior cladding.

[0153] Fig. 3b shows a schematic cross-sectional view of an extended structure (11) which, on its side facing the lower floor (10), is adjacent to and bounded by a structural extension (19), such as a conventional interior or ceiling cladding. If the structure (11) is a floor structure, the structural extension (19) may comprise a conventional floor foundation.

[0154] Fig. 3c shows a schematic cross-sectional view of an extended structure (11), which additionally comprises a heating and / or cooling circuit (22) and at least one miniaturized heating and / or cooling unit (23) positioned on its side facing the outdoor area (7), which is combined with a PV panel (56) for energy generation. The structure (11) contains fluid lines (21) which are connected to, sealed off from, and in fluid contact with at least one of the miniaturized heating and / or cooling units (23). These fluid lines are arranged from the side of the structure (11) facing the outdoor area (7) in such a way that they traverse said side and are connected to, sealed off from, and in fluid contact with at least one heat radiation panel (31) positioned on the side of the structure (11) facing the indoor area (8).

[0155] Fig. 3d corresponds to Fig. 3c, which shows a schematic cross-sectional view of an extended structure (11), wherein the latter adjoins and is delimited by a structure extension (18) on its side facing the outer region (7) and / or adjoins and is delimited by a structure extension (19) on its side facing the inner region (8), wherein the fluid lines (21) logically also traverse the structure extension (18) and / or the structure extension (19), since they are positioned between the structure (11) and at least one of the miniaturized heating and / or cooling units (23) and / or at least one heat radiation panel (31).

[0156] Fig. 3e shows a schematic cross-sectional view of an extended structure (11), which additionally comprises a heating and / or cooling circuit (22) and at least one miniaturized heating and / or cooling unit (23) positioned on its side facing the outdoor area (7), which is combined with a PV panel (56) for energy generation. The structure (11) contains fluid lines (21) which are connected to, sealed off from, and in fluid contact with at least one of the miniaturized heating and / or cooling units (23). These fluid lines, originating from the side of the structure (11) facing the outdoor area (7), are arranged in such a way that they are connected to, sealed off from, and in fluid contact with at least one plate heat exchanger (32) positioned within the structure (11).In addition, fluid lines (21) are arranged within the structure (11), which in turn are connected to at least one of the plate heat exchangers (32), sealed and in fluid contact and comprise at least one circulation pump (57) which serves to circulate a secondary medium.

[0157] Fig. 3f corresponds to Fig. 3e, which shows a schematic cross-sectional view of an extended structure (11), wherein the latter adjoins and is delimited by a structural extension (18) on its side facing the outer region (7) and / or adjoins and is delimited by a structural extension (19) on its side facing the inner region (8), wherein the fluid lines (21) logically also traverse the structural extension (18) since the latter is positioned between the structure (11) and at least one of the miniaturized heating and / or cooling units (23). In addition, fluid lines (21) are laid out within the structure (11) and the structural extension (19), which in turn are connected, sealed, and in fluid contact with at least one of the plate heat exchangers (32).

[0158] Fig. 4a-k show schematic cross-sectional representations of a wall construction, as exemplary embodiments of the construction (11) according to the invention, which includes at least one component framework (12) of a preferred embodiment, comprising a composite of one- and two-dimensional construction elements and load-bearing components of the construction (11), and, if required, a shell construction material (13). In particular, the exemplary embodiments shown can be expanded as desired by a reflection at the center plane of the space delimited by the at least two spaced-apart shells and enclosed between them.

[0159] Fig. 4a shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14a, 14b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) which contains a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b). These spacers are anchored in at least one shell (14a, 14b) adjacent to the gap (16) and / or in other structural components, such as formwork (1), and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14a, 14b) adjacent to the gap.The component scaffolding (12) further comprises at least one formwork (1) which is arranged in at least one of the at least two spaced-apart shells (14a, 14b) and at least partially delimits said shells laterally. In addition, the component scaffolding (12) comprises at least one formwork (17) which is arranged in the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b), as well as shell spacers (3) which are arranged in at least one of the at least two spaced-apart shells and anchored in at least one formwork (1). At least one of the at least two spaced-apart shells (14a, 14b) further comprises at least one reinforcement (2).The structure (11) also comprises a shell construction material (13) which at least partially fills at least one of the at least two spaced-apart shells (14a, 14b) and at least partially adjoins at least one formwork (1). The structure (11) additionally includes at least one formwork (1) which is arranged in at least one of the at least two spaced-apart shells (14a), at least partially delimits the shell laterally, and has at least one anchoring form (60) which ensures at least one anchoring of the shell construction material (13) therein and can thus act as reinforcement for the shell construction material (13).

[0160] Fig. 4b shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14, 15) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) which contains a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). These spacers are anchored in at least one shell (14, 15) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged obliquely at an angle other than 90° to the surface delimiting the gap of a shell (14, 15) adjacent to the gap.The component framework (12) further comprises at least one formwork (1) which completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (1), and therefore the gap spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). At least one of the at least two spaced-apart shells (14) further comprises at least one reinforcement (2). The structure (11) also comprises a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially borders at least one formwork (1).

[0161] Fig. 4c shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (15a, 15b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). These spacers are anchored in at least one shell (15a, 15b) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged at an angle other than 90° to the surface delimiting the gap of a shell (15a, 15b) adjacent to the gap.The component framework (12) further comprises at least one formwork (1) which completely forms at least one of the at least two spaced-apart shells (15a, 15b) by being constructed using a single formwork (1), and therefore the space spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). The construction (11) shown here does not comprise any shell building material (13).

[0162] Fig. 4d shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14, 15a, 15b) and spaces (16a, 16b) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of spacer supports (4) arranged in the spaces (16a, 16b) delimited by the at least two spaced-apart shells (14, 15a, 15b) and enclosed between them. The spacer supports (4) are anchored in at least one shell (14, 15a, 15b) adjacent to the spaces (16a, 16b) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface of a shell (14, 15a, 15b) adjacent to the spaces, which surface delimits the spaces.The component framework (12) further comprises at least two formworks (1, 17), which in turn completely form at least one of the at least two spaced-apart shells (15a, 15b) in that they are constructed using a single formwork (1, 17), and therefore the gap spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the spaces (16a, 16b) delimited by and enclosed between the at least two spaced-apart shells (14, 15a, 15b), as well as shell spacers (3) which are arranged in at least one of the at least two spaced-apart shells (14) and anchored in at least one formwork (1). At least one of the at least two spaced-apart shells (14) further comprises at least one reinforcement (2).The construction (11) comprises, on the other hand, a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially adjoins at least one formwork (1).

[0163] Fig. 4e shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14, 15) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). These spacers are anchored in at least one shell (14, 15) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14, 15) adjacent to the gap.The component framework (12) further comprises at least one formwork (1) which completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (1), and therefore the gap spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). At least one of the at least two spaced-apart shells (14) further comprises at least one reinforcement (2).The construction (11) comprises, on the other hand, a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially borders the intermediate space (16) delimited by the at least two spaced-apart shells (14, 15) and enclosed between them.

[0164] Fig. 4f shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14, 15) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). These spacers are anchored in at least one shell (14, 15) adjacent to the gap (16) and / or in other structural components, such as formwork (1, 17), and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14, 15) adjacent to the gap.The component framework (12) further comprises at least one formwork (17) which completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (17), and therefore the space spacers (4) are anchored at least in at least one single formwork. The component framework (12) further comprises at least two formworks (1, 17) which are arranged in the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15).

[0165] At least one of the at least two spaced-apart shells (14) further comprises at least one reinforcement (2). The structure (11) also comprises a shell construction material (13) that at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially borders the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14a, 14b).

[0166] Fig. 4g shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14a, 14b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b). These spacers are anchored in at least one shell (14a, 14b) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14a, 14b) adjacent to the gap.The component framework (12) further comprises at least one formwork (1) arranged in at least one of the at least two spaced-apart shells (14b) and at least partially laterally delimiting said shells. In addition, the component framework (12) comprises at least one formwork (17) arranged in the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14a, 14b). At least one of the at least two spaced-apart shells (14a, 14b) further comprises at least one reinforcement (2).The construction (11) comprises, on the other hand, a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14a, 14b), at least partially adjoins at least one formwork (1) and at least partially adjoins the intermediate space (16) delimited by the at least two spaced-apart shells (14a, 14b) and enclosed between them.

[0167] Fig. 4h shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14a, 14b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14a, 14b). These spacers are anchored in at least one shell (14a, 14b) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14a, 14b) adjacent to the gap.The component framework (12) further comprises at least two formworks (1, 17) which are arranged in the intermediate space (16) delimited by the at least two shells (14a, 14b) which are spaced apart from one another and enclosed between them, wherein at least one intermediate space spacer (4) is anchored in the first shell (14a) adjoining the intermediate space (16) and / or further load-bearing structure components, such as formworks (1, 17), and in the process does not touch the second shell (14b) adjoining the intermediate space (16), and at least one intermediate space spacer (4) is anchored in the second shell (14b) adjoining the intermediate space (16) and / or further load-bearing structure components, such as formworks (1, 17), and in the process does not touch the first shell (14a) adjoining the intermediate space (16).

[0168] At least one of the at least two spaced-apart shells (14a, 14b) further includes at least one reinforcement (2). The structure (11) also comprises a shell construction material (13) that at least partially fills at least one of the at least two spaced-apart shells (14a, 14b) and at least partially borders the intermediate space (16) defined by and enclosed between the at least two spaced-apart shells (14a, 14b). The formwork (1) shown here can also be referred to as stabilization formwork.

[0169] Fig. 4i shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (15a, 15b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). These spacers are anchored in at least one shell (15a, 15b) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (15a, 15b) adjacent to the gap.The component framework (12) further comprises at least two formworks (1, 17) which completely form at least one of the at least two spaced-apart shells (15a, 15b) by being constructed using a single formwork (1, 17), and therefore the spacer elements (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the intermediate space (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). The construction (11) shown here does not comprise any shell building material (13).

[0170] Fig. 4j shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (15a, 15b) and a gap (16) delimited by and enclosed between them. The structure (11) comprises a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (15a, 15b). These spacers are anchored in at least one shell (15a, 15b) adjacent to the gap (16) and / or in other structural components such as formwork (1, 17), and are arranged at an angle other than 90° to the surface delimiting the gap of a shell (15a, 15b) adjacent to the gap.The component framework (12) further comprises at least one formwork (17) which completely forms at least one of the at least two spaced-apart shells (15a, 15b) by being constructed using a single formwork (17), and therefore the space spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least two formworks (1, 17) which are arranged in the space (16) delimited by the at least two spaced-apart shells (15a, 15b) and enclosed between them. The construction (11) shown here does not comprise any shell building material (13).

[0171] Fig. 4k shows a schematic cross-sectional view of a structure (11) with at least two spaced-apart shells (14, 15) and a gap (16) delimited by and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) containing a plurality of gap spacers (4) arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). These spacers are anchored in at least one shell (14, 15) adjacent to the gap (16) and / or in other structural components, such as formwork, and are arranged in an inclined position at an angle other than 90° to the surface delimiting the gap of a shell (14, 15) adjacent to the gap.The component framework (12) further comprises at least one formwork (17) which completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (17), and therefore the gap spacers (4) are anchored at least in at least one single formwork. In addition, the component framework (12) comprises at least one formwork (17) which is arranged in the gap (16) delimited by and enclosed between the at least two spaced-apart shells (14, 15). At least one of the at least two spaced-apart shells (14) further comprises at least one reinforcement (2).The construction (11) comprises, on the other hand, a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially borders the intermediate space (16) delimited by the at least two spaced-apart shells (14, 15) and enclosed between them.

[0172] Fig. 5a - f show schematic cross-sectional views of an extended wall construction, as embodiments of the construction according to the invention (11).

[0173] Fig. 5a shows a schematic cross-sectional view of an extended construction (11) which, on its side facing the outside area (7), adjoins and is limited by a construction extension (18), such as a conventional external cladding.

[0174] Fig. 5b shows a schematic cross-sectional view of an extended construction (11) which, on its side facing the interior area (8), adjoins and is delimited by a construction extension (19), such as a conventional interior lining.

[0175] Fig. 5c shows a schematic cross-sectional view of an extended structure (11), which additionally comprises a heating and / or cooling circuit (22) and at least one miniaturized heating and / or cooling unit (23) positioned on its side facing the outdoor area (7), which is combined with a PV panel (56) for energy generation. The structure (11) contains fluid lines (21) which are connected, sealed, and in fluid contact with at least one of the miniaturized heating and / or cooling units (23). These fluid lines are arranged from the side of the structure (11) facing the outdoor area (7) in such a way that they traverse it and are connected, sealed, and in fluid contact with at least one heat radiation panel (31) positioned on the side of the structure (11) facing the indoor area (8). Fig. 5d corresponds to Fig.5c, which shows a schematic cross-sectional view of an extended structure (11), wherein the latter adjoins and is delimited by a structural extension (18) on its side facing the outer region (7) and / or adjoins and is delimited by a structural extension (19) on its side facing the inner region (8), wherein the fluid lines (21) logically also traverse the structural extension (18) and / or the structural extension (19), since they are positioned between the structure (11) and at least one of the miniaturized heating and / or cooling units (23) and / or at least one heat radiation panel (31).

[0176] Fig. 5e shows a schematic cross-sectional view of an extended structure (11), which additionally comprises a heating and / or cooling circuit (22) and at least one miniaturized heating and / or cooling unit (23) positioned on its side facing the outdoor area (7), which is combined with a PV panel (56) for energy generation. The structure (11) contains fluid lines (21) which are connected to, sealed off from, and in fluid contact with at least one of the miniaturized heating and / or cooling units (23). These fluid lines, originating from the side of the structure (11) facing the outdoor area (7), are arranged in such a way that they are connected to, sealed off from, and in fluid contact with at least one plate heat exchanger (32) positioned within the structure (11).In addition, fluid lines (21) are arranged within the structure (11), which in turn are connected to at least one of the plate heat exchangers (32), sealed and in fluid contact and comprise at least one circulation pump (57) which serves to circulate a secondary medium.

[0177] Fig. 5f corresponds to Fig. 5e, which shows a schematic cross-sectional view of an extended structure (11), wherein the latter adjoins and is delimited by a structural extension (18) on its side facing the outer region (7) and / or adjoins and is delimited by a structural extension (19) on its side facing the inner region (8), wherein the fluid lines (21) logically also traverse the structural extension (18) since the latter is positioned between the structure (11) and at least one of the miniaturized heating and / or cooling units (23). In addition, fluid lines (21) are laid out within the structure (11) and the structural extension (19), which in turn are connected, sealed, and in fluid contact with at least one of the plate heat exchangers (32).

[0178] Fig. 6 a1.) - a6.) show schematic cross-sectional representations, as embodiments of the construction (11) according to the invention, of a connection, fastening, sealing and / or anchoring of a load-bearing component such as shell and / or intermediate spacer (3, 4) in a shell building material (13), wherein said component is arranged at an angle other than 90° to the surface of the shell building material (13) delimiting the area of ​​the connection, fastening, sealing and / or anchoring.

[0179] Fig. 6 a1.) shows a connection, fastening, sealing and / or anchoring of a

[0180] A structural component such as a shell and / or intermediate spacer (3, 4) in a shell building material (13), wherein said component completely penetrates the formwork (1) delimiting the shell building material (13) and is connected, fastened, sealed and / or anchored in the shell building material (13) by means of an anchoring form (60).

[0181] Fig. 6 a2.) shows a connection, fastening, sealing and / or anchoring of a structural component such as a shell and / or intermediate spacer (3, 4) in a shell building material (13), wherein said component is connected, fastened, sealed and / or anchored in the shell building material (13) by means of an anchoring form (60) mounted therein.

[0182] Fig. 6 a3.) and a5.) shows a connection, fastening, sealing and / or anchoring of a structural component such as a shell and / or intermediate spacer (3, 4) in a shell building material (13), wherein said component completely penetrates the formwork (1) delimiting the shell building material (13) and is connected, fastened, sealed and / or anchored in the shell building material (13) by means of an anchoring aid (64), wherein the anchoring aid (64) has an anchoring shape (60). In addition, the anchoring aid (64) shown in Fig. 6 a5.) can be designed as a spring (e.g. spiral spring) so that it automatically straightens up again after the formwork (1) is stepped on.

[0183] Fig. 6 a4.) and a6.) shows a connection, fastening, sealing and / or anchoring of a structural component such as a shell and / or intermediate spacer (3, 4) in a shell building material (13), wherein said component is connected, fastened, sealed and / or anchored in the hardened shell building material (13) by means of an anchoring aid (64) mounted therein, wherein the anchoring aid (64) has an anchoring shape (60). In addition, the anchoring aid (64) shown in Fig. 6 a6.) can be designed as a spring (e.g. spiral spring) so that it automatically straightens itself after the formwork (1) is stepped on.

[0184] Fig. 7a shows a schematic cross-sectional representation, as an embodiment of the construction (11) according to the invention, of an indirect connection, fastening, sealing and / or anchoring of a one-dimensional structural component such as a shell and / or intermediate spacer (3, 4) with a shell building material (13), wherein the latter is arranged at an angle other than 90° to the surface of the shell building material (13) that delimits the area of ​​the connection, fastening, sealing and / or anchoring, is in turn connected, fastened, sealed and / or anchored in a two-dimensional structural component such as a formwork (1) and is connected, fastened, sealed and / or anchored to the shell building material (13) via the formwork (1) that is connected, fastened, sealed and / or anchored to the shell building material (13) by means of an anchoring form (60).

[0185] Fig. 7b. Fig. 7 b1.) shows a schematic cross-sectional representation, as an embodiment of the construction (11) according to the invention, of an indirect connection, fastening, sealing and / or anchoring of a reinforcement (2) to a two-dimensional structural component such as a formwork (1, 17). The reinforcement (2) is connected, fastened, sealed and / or anchored to a shell building material (13) and connected, fastened, sealed and / or anchored to the formwork (1, 17) via the shell building material (13) which is connected, fastened, sealed and / or anchored to the formwork (1, 17) by means of an anchoring form (60). Fig. 7 b2.) shows a schematic floor plan representation of the indirect connection, fastening, sealing and / or anchoring of a reinforcement (2) to a two-dimensional structural component such as a formwork (1, 17).

[0186] Fig. 7c. Fig. 7 c1.) shows a schematic cross-sectional representation, as an embodiment of the construction (11) according to the invention, of a layered or ply structure of a 3-layer solid wood panel, as a two-dimensional structural component such as a formwork (1). The connection of the same with a one-dimensional structural component, such as a spacer, is carried out by means of a blind hole as a mutual connection, fastening, sealing and / or anchoring, and the coordinated, controlled and / or process-induced layered or ply structure of the 3-layer solid wood panel is produced and coordinated such that the thickness of the cover sheet (1iii) corresponds to the distance from the cover sheet surface to the penetration depth of the blind hole and its wood fiber direction is aligned parallel to the longitudinal axis of the composite component or the component framework. The thickness of the remaining transverse or longitudinal layers (1i, 1ii) ortheir wood fiber directions, which are located within the area of ​​the blind hole, are aligned in the longitudinal or transverse direction according to the structural forces occurring, in particular such that the transverse layer (1 ii) shown here, or its wood fiber direction, is specifically arranged at a 45° orientation to the longitudinal axis of the composite component or the component framework, and the transverse layer (1i) shown here, or its wood fiber direction, is specifically arranged at a 45° orientation to the longitudinal axis of the composite component or the component framework, or its wood fiber direction, opposite to the transverse layer (1 ii). Fig. 7 c2.) shows a schematic floor plan representation of the layer or layer structure of a 3-layer solid wood panel, as a two-dimensional structural component such as a formwork (1 ).

[0187] Fig. 7d. Fig. 7 d1.) shows a schematic cross-sectional view of a support region (18) of a structure (11) which comprises at least two shells (14, 15) spaced apart from one another and a gap (16) delimited by them and enclosed between them. The structure (11) comprises, on the one hand, a component framework (12) which includes a plurality of gap spacers (4) arranged in the gap (16) delimited by the at least two spaced-apart shells (14, 15) and enclosed between them, which are anchored at least in at least one shell (14, 15) adjacent to the gap (16) and / or other supporting structure components, such as formwork, and are arranged obliquely at an angle other than 90° to the surface delimiting the gap of a shell (14a, 14b) adjacent to the gap.The component framework (12) further comprises at least one formwork (1) which is arranged in at least one of the at least two spaced-apart shells (14) and at least partially delimits said shell laterally, as well as at least one formwork (1) which completely forms at least one of the at least two spaced-apart shells (15) by being constructed using a single formwork (1) and therefore the intermediate spacers (4) are anchored at least in at least one single formwork. At least one of the at least two spaced-apart shells (14, 15) further comprises at least one reinforcement (2). The structure (11) also comprises a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells (14) and at least partially borders at least one formwork (1).The support area of ​​the structure (18) is at least partially made of a shell material (13) and reinforcements (2). In addition, the reinforcement (2), which is arranged within the individual formwork (1) and extends into the support area of ​​the structure (18), can be connected, fastened, sealed and / or anchored to the individual formwork (1) by means of an indirect connection, fastening, sealing and / or anchoring, as described and shown in Fig. 7b. Fig. 7 d2.) corresponds to Fig. 7 d1.) whereby the individual formwork (1) extends into the support area, is constructed therein by means of a finger system and is connected, fastened, sealed and / or anchored to at least one of at least two spaced-apart shells (14) by means of an additional construction extension (18).

[0188] Fig. 8 a1.) - b2.) show schematic cross-sectional representations of structural components, as embodiments of the construction according to the invention (11).

[0189] Fig. 8 a1.) shows a schematic cross-sectional view of a structural component such as a shell and / or intermediate spacer (3, 4), which consists of a porous, open-pore material (5), such as wood.

[0190] Fig. 8 a2.) shows a schematic cross-sectional view of a structural component such as a shell and / or intermediate spacer (3, 4), which consists of a porous, open-pored material (5), such as wood, and which is mixed with a filling material (6). This has penetrated into the pores in the surface area of ​​the porous, open-pored structural component (3, 4) in the form of a working mixture. The penetration depth can be determined and controlled by the length of time the porous, open-pored structural component (3, 4) is exposed to the filling material (6) in the form of a working mixture - the longer the exposure, the greater the penetration depth. If required, the structural component (3, 4) can be directly, i.e. while still wet (i.e.the filling material is still flowable or liquid and not yet hardened), for subsequent manufacturing or assembly steps or only after the filling material (6) has solidified and hardened.

[0191] Fig. 8 a3.) shows a schematic cross-sectional view of a structural component such as a shell and / or intermediate spacer (3, 4), which consists of a porous, open-pored material (5), such as wood, and which is filled with a filling material (6). The filling material (6) is already hardened, i.e. the pores in the surface area of ​​the porous, open-pored structural component (3, 4) are sealed and closed. In addition, the porous, open-pored structural component (3, 4) is embedded, in particular connected, fastened, sealed and / or anchored, in a shell material (13).The swelling effect of the porous, open-pored material (5) in the freshly installed shell building material (13) is reduced or prevented because the hardened filling material (6) has sealed and closed the pores in the surface area of ​​the porous, open-pored structural component (3, 4) and the latter can therefore no longer absorb moisture, such as water, released by the freshly installed shell building material (13).

[0192] Fig. 8 b1.) shows a schematic cross-sectional representation of a connection, fastening, sealing and / or anchoring of a structural component such as a shell and / or intermediate spacer (3, 4) consisting of a porous, open-pore material (5), such as wood, in a formwork (1, 17), also consisting of a porous, open-pore material (5), such as wood, wherein the structural component (3, 4) completely penetrates the formwork (1, 17) and is inclined to its surface, arranged at an angle other than 90°. In this case, the structural component (3, 4) in its end region and the bore in the formwork (1, 17) were previously filled with a setting material (6) and, while this material was still wet, in particular flowable or liquid and not yet hardened, the structural component (3, 4) was inserted into the bore in the formwork (1, 17) and mounted.Subsequently, the filling material (6) solidifies, hardens and creates an adhesive bond in the contact area of ​​the structural component (3, 4) with the formwork (1, 17) and thus a connection, fastening, sealing and / or anchoring.

[0193] Fig. 8 b2.) corresponds to Fig. 8 b1.), which is a schematic cross-sectional representation of a connection, fastening, sealing and / or anchoring of a structural component such as a shell and / or intermediate spacer (3, 4) consisting of a porous, open-pore material (5), such as wood, in a formwork (1, 17), also consisting of a porous, open-pore material (5), such as wood, wherein the structural component (3, 4) does not penetrate the formwork (1, 17).

[0194] Fig. 9a shows a schematic cross-sectional representation of a mutually sliding and interlocking profile (45) between two individual raw, partial or complete component frames (12) or raw, partial or complete structures (11), which, if required, are designed in the form of raw, partial or complete building modules (50), raw, partial or complete modular building blocks (52), raw, partial or complete building elements (54), and / or raw, partial or complete components (55), as an embodiment of the construction (11) according to the invention, comprising at least two spaced-apart shells (14a, 14b) and an intermediate space (16) delimited by them and enclosed between them. The individual raw, partial or complete component frames (12) or raw, partial or complete structures (11) contain load-bearing components such as, for example,Intermediate spacers (4) and / or reinforcements (2), wherein the structure (11) comprises a shell material (13) which at least partially fills at least one of the at least two spaced-apart shells (14a, 14b). As soon as the assembly parts, such as the individual raw, partial, or complete component frameworks (12) or raw, partial, or complete structures (11), are joined together during their assembly by means of the connecting and sealing point (40) with a mutually sliding and interlocking profile (45) and / or fold by means of a rectangular overlapping surface (41), a shell material (13) or a mortar is installed in the design-dependent cavity of the connecting and sealing point (40) and the fold by means of a rectangular overlapping surface (41), which then solidifies and hardens and in this way connects the two reinforcements (2) to one another in a force-fitting manner.This creates a connection, fastening, sealing and / or anchoring between individual raw, partial or complete component scaffolds (12) or raw, partial or complete structures (11), which can be used as reinforcement in the 2nd axis.

[0195] Fig. 9b corresponds to Fig. 9a with the difference that the structure (11) comprises, instead of the at least two spaced-apart shells (14a, 14b), at least two spaced-apart shells (15a, 15b) and an intermediate space (16) delimited by them and enclosed between them. The individual raw, partial or complete component frameworks (12) or raw, partial or complete structures (11) contain load-bearing components such as intermediate space spacers (4) and / or reinforcements (2), wherein the structure (11) comprises at least one formwork (1) which completely forms at least one of the at least two spaced-apart shells (15a, 15b) by being constructed using a single formwork (1), and therefore the intermediate space spacers (4) are anchored at least in at least one individual formwork.

[0196] Fig. 10 a1.) - a4.) show schematic cross-sectional representations, as embodiments of the construction (11) according to the invention, of a connection and sealing point (40) between individual, adjacent raw, partial or complete component scaffolds (12) or raw, partial or complete structures (11), which, if required, are designed in the form of raw, partial or complete building modules (50), raw, partial or complete modular building blocks (52), raw, partial or complete building elements (54), and / or raw, partial or complete components (55), or their formwork (1, 17). Fig. 10 a1.) shows a schematic cross-sectional representation of a connection and sealing point (40), designed by means of a mutually overlapping fold with a cross-section in rectangular shape (41), which is additionally supplemented with a sealing aid (65). Fig. 10 a2.) shows a schematic cross-sectional view of a connection and sealing point (40), implemented by means of a mutually overlapping fold with a cross-section in rectangular shape (41), which is additionally provided with a groove containing a sealing aid (65). Fig. 10 a3.) shows a schematic cross-sectional view of a connection and sealing point (40), implemented by means of a mutually overlapping fold with a cross-section in rectangular shape (41), which is additionally provided with a sealing shape (61) in the form of a groove and a ridge. Fig. 10 a4.) shows a schematic cross-sectional view of a connection and sealing point (40), implemented by means of a mutually overlapping fold with a cross-section in rectangular shape (41), which is additionally provided with a sealing shape (61) in the form of a sealing nub.The mutually overlapping folds with a cross-section in rectangular shape (41 ) in Fig. a1.) - a4.) can alternatively also be designed with a mutually overlapping fold with a cross-section of an inclined overlapping surface.

[0197] Fig. 11 a1 .) - a3.) show schematic representations of an auxiliary assembly tool (48) in different views. Fig. 10 a1.) shows a side view of the auxiliary assembly tool (48), which has at least one auxiliary assembly mold (49). Fig. 10 a2.) shows a plan view of the auxiliary assembly tool (48), which has at least one auxiliary assembly mold (49). To use it, the auxiliary assembly tool (48) is inserted into an opening provided for this purpose in at least one formwork (1, 17). By means of a finite rotary movement of the auxiliary assembly tool (48) in the specified direction, the auxiliary assembly molds (49) are used to position, fix and space the at least one formwork (1, 17) at a specific distance. Fig. 10 a3.) shows a side view of the auxiliary assembly tool (48). The assembly auxiliary tool (48) is inserted into an opening provided for this purpose in at least one formwork (1, 17).By means of a finite rotary movement of the auxiliary assembly tool (48), the positioning, fixing and spacing of the at least one formwork (1, 17) at a specific distance is effected by means of the auxiliary assembly forms (49).

[0198] Fig. 12a - d show schematically in the form of simple flow diagrams, as embodiments of the production method according to the invention, a sequence for producing a material mixture in the form of a dry mixture or in the form of a working mixture, which can preferably be carried out with a control method according to the invention.

[0199] Fig. 12a shows schematically, in the form of a simple flow diagram, a process for producing a dry mix for a filling material (6), such as a dry mix for a mortar. The process step (1201) comprises the proportional preparation and proportional mixing of various starting materials, such as cement, aggregates and, if required, other substances and / or materials. In particular, the fineness or grinding degree, grain size, grain geometry and any other material properties of the various starting materials determine the quality properties of the dry mix for a filling material (6), which, mixed and prepared with a liquid, such as water, is coordinated and optimized for an inventive function and effect of the working mixture of the filling material (6) in conjunction with a porous, open-pore material, such asWood, as a starting material for structural components for at least part of the structure (11). This completes the process for producing a dry mix for a filling material (6).

[0200] Fig. 12b shows schematically, in the form of a simple flow diagram, a process for producing a working mixture of a setting material (6), such as a working mixture of a mortar. The process step (1202) comprises the proportional preparation and proportional mixing and blending of various starting materials, such as a liquid such as water, with a setting material (6) in the form of a dry mix or generally with cement, aggregates and, if required, other substances and / or materials. In particular, the degree of fineness, grain size, grain geometry, viscosity and any other material properties of the various starting materials determine the quality properties of the working mixture for a setting material (6), which is coordinated and optimized for an inventive function and effect of the working mixture of the setting material (6) in connection with a porous, open-pore material, such as, for example,Wood, as starting material for load-bearing components for at least part of the construction (11). This completes the process for producing a working mix for a filling material (6). Fig. 12c shows schematically, in the form of a simple flow diagram, a process for producing a dry mix for a shell building material (13), such as a dry mix for concrete. The process step (1203) comprises the proportional preparation and proportional mixing of various starting materials, such as cement, aggregates and, if required, other substances and / or materials. In particular, the fineness or grinding degree, grain size, grain geometry and any other material properties of the various starting materials determine the quality properties of the dry mix for a shell building material (13), which, when mixed and prepared with a liquid, such as,Water, is matched and optimized for the use of the shell building material (13) for at least one part within the structure (11), in particular for use in combination with one- and / or two-dimensional construction elements of the structure (11), such as formwork (1, 17) or spacers (3, 4). This completes the process for producing a dry mix for a shell building material (13).

[0201] Fig. 12d schematically shows, in the form of a simple flow diagram, a process for producing a working mix for a shell construction material (13), such as a working mix for concrete. Process step (1204) comprises the proportional preparation and mixing and blending of various starting materials, such as a liquid such as water, with a shell construction material (13) in the form of a dry mix or generally with cement, aggregates, and, if necessary, other substances and / or materials.In particular, the degree of fineness, grain size, grain geometry, viscosity, and any other material properties of the various starting materials determine the quality properties of the working mixture of the shell building material (13), which is tailored and optimized for the use of the shell building material (13) for at least one part within the structure (11), in particular for use in combination with one- and / or two-dimensional construction elements of the structure (11), such as formwork (1, 17) or spacers (3, 4). This completes the process for producing a working mixture for a shell building material (13).

[0202] Fig. 13a - d show schematically in the form of simple flow diagrams, as embodiments of the manufacturing method according to the invention, a sequence for producing starting materials of the construction (11) in the form of formwork (1, 17), spacers (3, 4), anchoring aids (64), sealing aids (65), materials (67, 68) and / or reinforcements (2), which can preferably be carried out using a control method according to the invention.

[0203] Fig. 13a schematically shows, in the form of a simple flow chart, a process for producing formwork (1, 17) in the form of panels or slabs as two-dimensional structural elements of the structure (11). Process step (1301) comprises the preparation and proportional assembly, mutual fastening, pressing, and / or gluing of various starting materials, such as wood chips, wooden boards, or wooden planks, and, if necessary, other substances and / or materials.In particular, the degree of fineness, chip size, chip geometry, material thicknesses and dimensions, as well as any other material properties of the various starting materials, determine the quality properties of the formwork (1, 17), which are matched and optimized for use as starting materials for at least one part of the structure (11), in particular for the inventive function and effect of the composite with a one-dimensional structural element of the structure (11), such as spacers (3, 4) (so-called wood-wood composite). This completes the process for producing formwork (1, 17) in the form of panels or plates as two-dimensional structural elements of the structure (11).

[0204] Fig. 13b shows schematically, in the form of a simple flow chart, a process for producing spacers (3, 4) in the form of sleeves, rods, dowels or bolts as one-dimensional construction elements of the structure (11). The method step (1302) comprises the preparation and processing of various starting materials such as wooden boards or wooden planks and, if required, other substances and / or materials. In particular, the material geometry, material thicknesses and material dimensions as well as any other material properties of the various starting materials determine the quality properties of the spacers (3, 4), which are coordinated and optimized for use as starting materials for at least part of the structure (11), in particular for the inventive function and effect of the composite with a two-dimensional construction element of the structure (11), such as formwork (1, 17) (so-calledWood-wood composite) or to an inventive function and effect of the composite with a shell construction material (13) (so-called wood-concrete composite). This completes the process for producing spacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11).

[0205] Fig. 13c shows schematically, in the form of a simple flow diagram, a process for producing anchoring aids (64) and / or materials (67, 68). Method step (1303) comprises the preparation and processing of various starting materials, such as iron or plastic raw materials and, if required, further substances and / or materials. In particular, material geometry, material thicknesses and dimensions, as well as any further material properties of the various starting materials, determine the quality properties of the anchoring aids (64) and / or materials (67, 68), which are matched and optimized for use for at least one part within the structure (11), in particular for the inventive function and effect of the composite with one- and / or two-dimensional construction elements of the structure (11), such as, for example,Formwork (1, 17) or spacers (3, 4) or to an inventive function and effect of the composite with a formwork material (13). This completes the process for producing anchoring aids (64) and / or materials (67, 68).

[0206] Fig. 13d shows a schematic, simple flow chart-like process for producing reinforcements (2). Process step (1304) comprises the preparation and processing of various starting materials, such as iron or plastic raw materials and, if required, other substances and / or materials. In particular, material geometry, material thicknesses, and material dimensions, as well as any other material properties of the various starting materials, determine the quality properties of the reinforcements (2), which are matched and optimized for use for at least one part within the structure (11), in particular for the inventive function and effect of the composite with one- and / or two-dimensional construction elements of the structure (11), such as formwork (1, 17) or spacers (3, 4), or for an inventive function and effect of the composite with a shell material (13).This completes the process for producing reinforcements (2).

[0207] Fig. 14a-d schematically show, as exemplary embodiments of the manufacturing method according to the invention, in the form of simple flow diagrams, a sequence for processing starting materials of the structure (11) in the form of structural components such as formwork (1, 17), which can preferably be carried out using a control method according to the invention. In particular, by means of preferably automated processing or method steps, in particular their execution by means of a control method according to the invention, such as the computer-aided or computer-implemented numerical control of automated processing machines (e.g., CNC machines).The processing steps are process-relatedly coordinated, controlled and / or optimized for the use of the structural components within at least one part of the construction (11), in particular for the inventive function or effect of their connection with a one-dimensional construction element of the construction (11), such as spacers (3, 4).

[0208] Fig. 14a schematically shows, in the form of a simple flow chart, a process for processing structural components such as formwork (1, 17) in the form of panels or slabs as two-dimensional structural elements of the structure (11). Method step (1401) comprises processing the starting materials of the structural components in a shaping step with regard to their border and / or geometric shape and / or attaching anchoring forms (60) and / or sealing forms (61) to them. This completes the process for processing structural components such as formwork (1, 17).

[0209] Fig. 14b schematically shows, in the form of a simple flow chart, a process for processing structural components such as formwork (1, 17) in the form of panels or plates as two-dimensional construction elements of the structure (11). The first method step (1402) comprises processing the starting materials of the structural components in a shaping step with regard to their border and / or geometric shape and / or the attachment of anchoring forms (60) and / or sealing forms (61) to the same. A further method step (1403) comprises drilling holes in the starting materials of the structural components. This completes the process for processing structural components such as formwork (1, 17).

[0210] Fig. 14c shows schematically, in the form of a simple flow chart, a process for processing structural components such as formwork (1, 17) in the form of panels or plates as two-dimensional construction elements of the structure (11). The first method step (1404) comprises processing the starting materials of the structural components in a shaping process step with regard to their border and / or geometric shape and / or the attachment of anchoring forms (60) and / or sealing forms (61) to the same. A further method step (1405) comprises drilling holes in the starting materials of the structural components. A further method step (1406) comprises further processing the starting materials of the structural components and / or the further attachment of anchoring forms (60) and / or sealing forms (61) to the same. The process for processing structural components such asFormwork (1, 17) completed.

[0211] Fig. 14d schematically shows, in the form of a simple flow chart, a process for processing structural components such as formwork (1, 17) in the form of panels or slabs as two-dimensional structural elements of the structure (11). The first method step (1407) comprises processing the starting materials of the structural components in a shaping step with regard to their border and / or geometric shape and / or the attachment of anchoring forms (60) and / or sealing forms (61) to the same. A further method step (1408) comprises positioning and fixing the processed starting materials of the structural components in a predetermined position relative to one another, in particular at a predetermined distance or a predetermined distance parallel to one another in the slab or panel plane. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48).A further process step (1409) involves drilling holes in the starting materials of the structural components. This completes the process for processing structural components such as formwork (1, 17).

[0212] Fig. 15a-d schematically show, as exemplary embodiments of the manufacturing method according to the invention, a sequence for processing starting materials of the structure (11) in the form of supporting structure components such as spacers (3, 4), which can preferably be carried out using a control method according to the invention. In particular, by means of preferably automated processing or method steps, in particular their execution using a control method according to the invention, such as the computer-aided or computer-implemented numerical control of automated processing machines (e.g., CNC machines).The processing steps are process-relatedly coordinated, controlled and / or optimized for the use of the structural components within at least one part of the construction (11), in particular for the inventive function or effect of their connection with a two-dimensional construction element of the construction (11) such as formwork (1, 17).

[0213] Fig. 15a shows a schematic, simple flow chart representation of a process for machining structural components such as spacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11). Process step (1501) comprises machining the starting materials of the structural components in a shaping step with regard to their outline and / or geometric shape and / or attaching anchoring molds (60) and / or sealing molds (61) to the same. This completes the process for machining structural components such as spacers (3, 4). Fig. 15b shows a schematic, simple flow chart representation of a process for machining structural components such as spacers (3, 4).Spacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11), wherein the structural components consist of a porous, open-pored material such as wood. The first method step (1502) comprises processing the starting materials of the structural components in a shaping step with regard to their border and / or geometric shape and / or the attachment of anchoring forms (60) and / or sealing forms (61) to the same. A further method step (1503) comprises displacing the structural components in a displacing material (6) in the form of a working mixture or displacing the structural components with a displacing material (6) in the form of a working mixture. The displacing material (6) in the form of a working mixture penetrates into the pores in at least part of the surface area of ​​the structural component consisting of the porous, open-pored material.The penetration depth can be determined and controlled by the length of time the structural component is exposed to the filling material (6) in the form of a working mixture—the longer the exposure, the greater the penetration depth. Depending on the requirements, the processing of structural components such as spacers (3, 4) can be terminated while the filling material (6) in the form of a working mixture is still flowable or liquid and not yet hardened, or only after the filling material (6) in the form of a working mixture has solidified and hardened.

[0214] Fig. 15c schematically shows, in the form of a simple flow chart, a process for processing structural components such as spacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11). The first method step (1504) comprises processing the starting materials of the structural components in a shaping step with regard to their border and / or geometric shape and / or the attachment of anchoring forms (60) and / or sealing forms (61) to the same. A further method step (1505) comprises the installation of anchoring aids (64), sealing aids (65), technical components, and / or other materials in or on the structural components. This completes the process for processing structural components such as spacers (3, 4).

[0215] Fig. 15d shows schematically, in the form of a simple flow chart, a process for processing structural components such as spacers (3, 4) in the form of sleeves, rods, dowels or bolts as one-dimensional structural elements of the structure (11), wherein the structural components consist of a porous, open-pored material such as wood. The first method step (1506) comprises processing the starting materials of the structural components in a shaping step with regard to their border and / or geometric shape and / or the attachment of anchoring forms (60) and / or sealing forms (61) to the same. A further method step (1507) comprises displacing the structural components with water. The water penetrates into the pores in at least part of the surface area of ​​the structural components consisting of the porous, open-pored material.The penetration depth can be determined and controlled by the length of time the structural components are exposed to water—the longer the exposure, the greater the penetration depth. A further process step (1508) involves freezing the structural components. In this process, the structural components, which have been mixed with water in at least part of their surface area, are exposed to temperatures below the freezing point of water for a specific period of time so that the water that has penetrated the surface area of ​​the structural component freezes.The intention here is that the increase in volume of freezing water will cause as many pores in the porous, open-pored material as possible to break open, thus increasing the porosity or the number of open pores in the porous, open-pored material. The intention is that when the structural components are subsequently filled with a filling material (6) in the form of a working mixture, the absorption and penetration capacity of the filling material is improved. A further method step (1509) comprises thawing and drying out the structural components. The structural components to which at least part of their surface has been added with water are exposed for a specific period of time to temperatures above the freezing point of water so that the water that has penetrated into the surface area of ​​the structural components thaws and evaporates, i.e. the structural components are dried.A further method step (1510) comprises the disposition of the structural components with a filling material (6) in the form of a working mixture. In this process, the filling material (6) in the form of a working mixture penetrates into the pores in at least part of the surface area of ​​the structural component, consisting of the porous, open-pore material. The penetration depth can be determined and controlled by the length of time the structural component is exposed to the filling material (6) in the form of a working mixture—the longer the exposure, the greater the penetration depth. Depending on requirements, the process for processing structural components such as spacers (3, 4) can be terminated while the filling material (6) in the form of a working mixture is still flowable or liquid and not yet hardened, or only after the filling material (6) in the form of a working mixture has solidified and hardened.

[0216] Fig. 16a - c show schematically in the form of simple flow diagrams, as exemplary embodiments of the manufacturing method according to the invention, a sequence for producing a raw, partial or complete component framework (12) of a structure (11), which, if required, is designed in the form of raw, partial or complete building modules (50), raw, partial or complete modular building blocks (52), raw, partial or complete building elements (54), raw, partial or complete components (55) and / or raw, partial or complete structures of a structure (11), which can preferably be carried out using a control method according to the invention. This creates a connection, fastening, sealing and / or anchoring between a one-dimensional structural component such as, for example, spacers (3, 4) and a two-dimensional structural component such as, for example,Formwork (1, 17) and thus the inventive connection between one- and two-dimensional construction elements and load-bearing components of the construction (11).

[0217] Fig. 16a shows schematically, in the form of a simple flow diagram, a process for producing a raw, partial, or complete component framework (12) as a three-dimensional structural element of the structure (11) made from one- and two-dimensional structural elements in a composite construction. The first method step (1601) comprises the application or application of adhesive or setting material (6) in the form of a working mixture into bores previously made in the structural components, such as formwork (1, 17) in the form of panels or plates as two-dimensional structural elements of the structure (11). A further method step (1602) comprises the insertion and assembly of structural components, such as spacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11), into the bores of the structural components, such as formwork (1, 17), machined in the previous method step (1602).Formwork (1, 17). This completes the process for producing a raw, partial, or complete component framework (12).

[0218] Fig. 16b shows schematically, in the form of a simple flow diagram, a process for producing a raw, partial or complete component framework (12) as a three-dimensional structural element of the structure (11) made of one- and two-dimensional structural elements in a composite construction. The first method step (1603) comprises the positioning and fixing of a previously machined structural component, such as a formwork (1, 17) in the form of a panel or plate, as a two-dimensional structural element of the structure (11) in a predetermined position or location. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48). A further method step (1604) comprises the assembly of structural components, such asSpacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11) are inserted into the supporting structure component positioned and fixed in the preceding process step (1603). This completes the process for producing a raw, partial, or complete component framework (12).

[0219] Fig. 16c shows schematically, in the form of a simple flow chart, a process for producing a raw, partial or complete component framework (12) as a three-dimensional structural element of the structure (11) made of one- and two-dimensional structural elements in a composite construction. The first method step (1605) comprises the positioning and fixing of a previously machined structural component, such as a formwork (1, 17) in the form of a panel or plate, as a two-dimensional structural element of the structure (11) in a predetermined position or location. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48). A further method step (1606) comprises the assembly of structural components, such asSpacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11) are inserted into the structural component positioned and fixed in the preceding method step (1605). A further method step (1607) comprises the installation of anchoring aids (64), sealing aids (65), technical components, and / or other materials in or on the structural components. This completes the process for producing a raw, partial, or complete component framework (12).

[0220] Fig. 17a, b show schematically in the form of simple flow diagrams, as exemplary embodiments of the manufacturing method according to the invention, a sequence for producing a raw, partial or complete component framework (12) of a structure (11), which, if required, is designed in the form of raw, partial or complete building modules (50), raw, partial or complete modular building blocks (52), raw, partial or complete building elements (54), raw, partial or complete components (55) and / or raw, partial or complete structures of a structure (11), which can preferably be carried out using a control method according to the invention. This creates a connection, fastening, sealing and / or anchoring between a one-dimensional load-bearing component such as, for example, spacers (3, 4) and a two-dimensional load-bearing component such as, for example,Formwork (1, 17) and thus the inventive connection between one- and two-dimensional construction elements and load-bearing components of the construction (11).

[0221] Fig. 17a shows schematically, in the form of a simple flow diagram, a process for producing a raw, partial, or complete component framework (12) as a three-dimensional structural element of the structure (11) made of one- and two-dimensional structural elements in a composite construction. The first method step (1701) comprises the positioning and fixing of the previously processed structural components, such as formwork (1, 17) in the form of panels or plates as two-dimensional structural elements of the structure (11), in a predetermined position relative to one another, in particular at a predetermined distance or a predetermined distance parallel to one another, in the plate or panel plane. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48). A further method step (1702) comprises the assembly of structural components, such asSpacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11) are inserted into the supporting structure components positioned and fixed in the preceding method step (1701). This completes the process for producing a raw, partial, or complete component framework (12).

[0222] Fig. 17b shows schematically, in the form of a simple flow diagram, a process for producing a raw, partial, or complete component framework (12) as a three-dimensional structural element of the structure (11) made of one- and two-dimensional structural elements in a composite construction. The first method step (1703) comprises the positioning and fixing of the previously processed structural components, such as formwork (1, 17) in the form of panels or plates as two-dimensional structural elements of the structure (11), in a predetermined position relative to one another, in particular at a predetermined distance or a predetermined distance parallel to one another, in the plane of the panels or plates. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48). A further method step (1704) comprises the assembly of structural components, such asSpacers (3, 4) in the form of sleeves, rods, dowels, or bolts as one-dimensional structural elements of the structure (11) are inserted into the structural components positioned and fixed in the preceding method step (1703). A further method step (1705) comprises the installation of anchoring aids (64), sealing aids (65), technical components, and / or other materials in or on the structural components. This completes the process for producing a raw, partial, or complete component framework (12).

[0223] Fig. 18a schematically shows, in the form of a simple flow diagram, as an exemplary embodiment of the manufacturing method according to the invention, a sequence for producing a component framework (12) of a structure (11) in the form of a raw, partial, or complete construction module (50), raw, partial, or complete modular building block (52), raw, partial, or complete component element (54), raw, partial, or complete component (55), and / or a raw, partial, or complete structure of a structure (11), as a three-dimensional construction element of the structure (11) made of one- and two-dimensional construction elements in a composite construction, which can preferably be carried out using a control method according to the invention. The first method step (1801) comprises the assembly of at least one raw or partial component framework (12) and / or the stepwise or incremental and additive joining, fastening, and, if necessary, mutual sealing of raw or partial component frameworks (12).This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48). A further method step (1802) comprises reading, comparing, calculating and / or processing the actual value of the current production status of a component scaffold (12), which is present as input information in the form of a measured variable, with the target value of the production status of a component scaffold (12), which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is equal to the component scaffold value, the method for producing a component scaffold (12) is terminated. If the result of the comparison of the actual value with the target value is not equal to the component scaffold value, the first method step (1801) is executed again.

[0224] Fig. 18b schematically shows, in the form of a simple flow diagram, as an embodiment of the manufacturing method according to the invention, a sequence for producing a shell, partial, or complete structure (11), which can preferably be carried out using a control method according to the invention. The first method step (1803) comprises the installation of anchoring aids (64), sealing aids (65), technical components, and / or other materials in or on structural components. A further method step (1804) comprises the partial or complete incorporation of a shell building material (13), such as concrete in the form of a working mix, into at least one formwork as the shaping formwork / casting mold and, if necessary, into at least one additional and / or independent, temporary formwork / casting mold.A further method step (1805) comprises allowing the previously installed shell material (13) to harden until it has reached a sufficiently high strength. This creates a connection, fastening, sealing, and / or anchoring between the structural components and the shell material (13), thus forming a bond according to the invention between structural components of the structure (11) and a shell material (13). This completes the process for producing a shell, partial, or complete structure (11).

[0225] Fig. 19 shows schematically, in the form of a simple flow diagram, as an embodiment of the manufacturing method according to the invention, a sequence for producing a building element (54), component (55) or a shell, partial or complete construction (11), which can preferably be carried out using a control method according to the invention. The first method step (1901) comprises the production or assembly of at least one independent, temporary formwork as a shaping formwork / casting mold. A further method step (1902) comprises the assembly of reinforcements (2), anchoring aids (64), sealing aids (65), technical components and / or other materials in or on the at least one independent, temporary formwork as a shaping formwork / casting mold. A further method step (1903) comprises the partial or complete installation of a shell building material (13), such as, for example,Concrete in the form of a working mix into the at least one independent, temporary formwork as a shaping formwork / casting mold. A further method step (1904) comprises the assembly or insertion of at least one raw, partial, or complete component framework (12), raw or partial construction element (54), and / or raw or partial component (55) and / or the step-by-step or incremental and additive joining, fastening, and, if necessary, mutual sealing of raw, partial, or complete component frameworks (12), raw or partial construction elements (54), and / or raw or partial components (55) in the shell material (13), such as concrete. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48).A further method step (1905) comprises reading, comparing, calculating, and / or processing the actual value of the current production status of a component (54), part (55), or a raw, partial, or complete construction (11), which is present as input information in the form of a measured variable, with the target value of the production status of a component (54), part (55), or a raw, partial, or complete construction (11), which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is not equal to the value of the raw, partial, or complete component, raw, partial, or complete component, or raw, partial, or complete construction is fully assembled, the previous method step (1904) is executed again.If the result of the comparison of the actual value with the target value is equal to the value of the raw, partial or entire component, raw, partial or entire component, or raw, partial or entire construction is fully assembled, a further method step (1906) is initiated. This comprises allowing the previously installed shell material (13) to harden until it has reached a sufficiently high strength. A further method step (1907) comprises reading, comparing, calculating and / or processing the actual value of the current state of manufacture of a component (54), component (55) or a raw, partial or entire construction (11), which is present as input information in the form of a measured variable, with the target value of the state of manufacture of a component (54), component (55) or a raw, partial or entire construction (11), which is present as input information in the form of a stored or calculated value.If the result of the comparison of the actual value with the target value is not equal to the value of the component, part, or rough, partial, or entire construction, the first method step (1901) is executed again. If the result of the comparison of the actual value with the target value is equal to the value of the component, part, or rough, partial, or entire construction, the method for producing a component (54), component (55), or a rough, partial, or entire construction (11) is terminated.

[0226] Fig. 20a schematically shows, in the form of a simple flow diagram, as an exemplary embodiment of the manufacturing method according to the invention, a sequence for producing a component (55) or a raw, partial, or complete construction (11), which can preferably be carried out using a control method according to the invention. The first method step (2001) comprises the assembly of at least one raw, partial, or complete component framework (12) and / or at least one raw, partial, or complete component element (54) and / or the stepwise or incremental and additive joining, fastening, and, if necessary, mutual sealing of raw, partial, or complete component frameworks (12) and / or raw, partial, or complete components (54).A further method step (2002) comprises reading, comparing, calculating and / or processing the actual value of the current production status of a component (55) or a raw, partial or entire construction (11), which is present as input information in the form of a measured variable, with the target value of the production status of a component (55) or a raw, partial or entire construction (11), which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is equal to the value of the component or raw, partial or entire construction, the method for producing a component (55) or a raw, partial or entire construction (11) is ended. If the result of the comparison of the actual value with the target value is not equal to the value of the component or raw, partial or entire construction, the first method step (2001) is executed again.

[0227] Fig. 20b schematically shows, in the form of a simple flow diagram, as an exemplary embodiment of the manufacturing method according to the invention, a sequence for producing a partial or complete construction (11), which can preferably be carried out using a control method according to the invention. The first method step (2003) comprises the assembly of at least one raw, partial, or complete component frame (12), a raw, partial, or complete component element (54), and / or a raw, partial, or complete component (55), and / or the stepwise or incremental and additive joining, fastening, and, if necessary, mutual sealing of raw, partial, or complete component frames (12), raw, partial, or complete components (54), and / or raw, partial, or complete components (55).A further method step (2004) comprises reading, comparing, calculating and / or processing the actual value of the current status of production of a partial or complete construction (11), which is present as input information in the form of a measured variable, with the target value of the status of production of a partial or complete construction (11), which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is not equal to the value of the raw or partial construction being fully assembled, the first method step (2003) is carried out again. If the result of the comparison of the actual value with the target value is equal to the value of the raw or partial construction being fully assembled, a further method step (2005) is initiated.This comprises the installation of reinforcements (2), anchoring aids (64), sealing aids (65), technical components and / or other materials in or on at least one structural component such as at least one formwork (1, 17) and / or at least one spacer (3, 4) and, if necessary, in or on at least one additional and / or independent, temporary formwork as a shaping formwork / casting mold. A further method step (2006) comprises the partial or complete installation of a shell building material (13), such as concrete in the form of a working mix, in at least one formwork as a shaping formwork / casting mold and, if necessary, in at least one additional and / or independent, temporary formwork / casting mold. A further method step (2007) comprises allowing the previously installed shell building material (13) to harden until it has reached a sufficiently high strength.This concludes the process for producing a partial or complete structure (11). Fig. 21 schematically shows, in the form of a simple flow chart, as an exemplary embodiment of the production method according to the invention, a process for producing a building element (54), component (55) or a shell, partial or complete structure (11), which can preferably be carried out using a control method according to the invention. The first process step (2101) comprises the production or assembly of at least one independent, temporary formwork as a shaping formwork / casting mold. A further process step (2102) comprises the assembly of reinforcements (2), anchoring aids (64), sealing aids (65), technical components and / or further materials in or on the at least one independent, temporary formwork as a shaping formwork / casting mold.A further method step (2103) comprises the assembly of at least one raw, partial, or complete component framework (12), a raw or partial component element (54), and / or a raw or partial component (55), and / or the stepwise or incremental and additive joining, fastening, and, if necessary, mutual sealing of raw, partial, or complete component frameworks (12), raw or partial component elements (54), and / or raw or partial components (55) in or on the at least one independent, temporary formwork as a shaping formwork / casting mold. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48).A further method step (2104) comprises reading, comparing, calculating, and / or processing the actual value of the current production status of a component (54), part (55), or a raw, partial, or entire construction (11), which is present as input information in the form of a measured variable, with the target value of the production status of a component (54), part (55), or a raw, partial, or entire construction (11), which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is not equal to the value of the raw, partial, or entire component, raw, partial, or entire component, or raw, partial, or entire construction is fully assembled, the previous method step (2103) is executed again.If the result of the comparison of the actual value with the target value is equal to the value of the raw, partial or complete structural element, raw, partial or complete component, or raw, partial or complete structure is fully assembled, a further method step (2105) is initiated. This comprises the partial or complete incorporation of a shell construction material (13), such as concrete in the form of a working mix, into the at least one independent, temporary formwork as the shaping formwork / casting mold and, if necessary, into at least one additional, independent, temporary formwork / casting mold. A further method step (2106) comprises allowing the previously installed shell construction material (13) to harden until it has reached a sufficiently high strength.A further method step (2107) comprises reading, comparing, calculating, and / or processing the actual value of the current manufacturing status of a component (54), part (55), or a raw, partial, or entire construction (11), which is present as input information in the form of a measured variable, with the target value of the manufacturing status of a component (54), part (55), or a raw, partial, or entire construction (11), which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is not equal to the value of the component, part, or raw, partial, or entire construction, the first method step (2101) is executed again.If the result of the comparison of the actual value with the target value is equal to the value of the component, part or raw, partial or complete construction, the method for producing a component (54), part (55) or a raw, partial or complete construction (11) is ended.

[0228] Fig. 22 schematically shows, in the form of a simple flowchart, as an embodiment of the computer program according to the invention, which is designed either centrally or decentrally, an architecture of a computer-implemented tool (software tool) in the form of an input-processing-output (IPO) structure for the evaluation, planning, manufacture, processing, prefabrication, assembly, and / or execution of a raw, partial, or complete construction (11). The input information (input) comprises values ​​of information and / or data on, for example, the type, shape / dimensions, location, materialization, costs, use / construction standard, user preferences, and / or requirements of a raw, partial, or complete construction (11), which are fed to the computer program for processing via a user interface (HMI).The calculation and / or processing steps of the computer-implemented tool (software tool) comprise reading, comparing, calculating and / or deriving a value of at least one piece of input information and converting, preparing and / or creating a value of at least one piece of output information, such as, for example, divisions of the components, sizes of the components, size / number of hexagonal grids, arrangements / number of spacers, system parameters and / or dimensions of the components and / or the one- and / or two-dimensional construction elements of the raw, partial or complete construction (11).At least one processing step comprises reading, comparing, calculating and / or deriving the actual value of the current processing status, which is present as information in the form of at least one result of at least one previous processing step, with the target value of the processing status, which is present as information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is not equal to the specified value, at least one of the previous processing steps is executed again. If the result of the comparison of the actual value with the target value is equal to the specified value, at least one subsequent method step is initiated. This comprises reading, comparing, calculating and / or deriving, for example, material expenditure, costs and / or CO2 balance of the raw, partial or entire construction (11).The results of the processing steps are prepared and provided as output information and include information and / or data for, for example, BIM (Building Information Modeling), evaluation, planning, manufacturing, processing, prefabrication, assembly, execution, material lists, verifications and / or cost structure of a shell, partial or complete construction (11).

[0229] Fig. 23 shows schematically in the form of a simple flow chart, as an embodiment of the control method according to the invention, which is designed either centrally or decentrally, a sequence for the computer-aided or computer-implemented numerical control of automated processing machines for processing starting materials of the structure (11) in the form of load-bearing structure components such as formwork (1, 17) and / or spacers (3, 4), which is computer-implemented on at least one automated processing machine (e.g. CNC machine) if necessary. The first method step (2301) comprises initializing the control method. A further method step (2302) comprises mounting and / or loading at least one processing tool into the automated processing machine. A further method step (2303) comprises moving to a processing position with at least one processing tool.A further method step (2304) comprises the computer-aided or computer-implemented, numerically controlled machining of a component in the form of a starting material of the structure (11) using at least one machining tool. A further method step (2305) comprises reading, comparing, calculating, and / or processing the actual value of the current machining status of the component, which is present as input information in the form of a measured variable, with the target value of the machining status of the component, which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is not equal to the machining complete value, the previous method step (2304) is executed again. If the result of the comparison of the actual value with the target value is equal to the machining complete value, a further method step (2306) is initiated.This comprises moving at least one machining tool away from the machining position. A further method step (2307) comprises reading, comparing, calculating and / or processing the actual value of the current machining status of the component, which is present as input information in the form of a measured variable, with the target value of the machining status of the component, which is present as input information in the form of a stored or calculated value. If the result of the comparison of the actual value with the target value is not equal to the machining value, method step 2302 is carried out again. If the result of the comparison of the actual value with the target value is equal to the machining value, the method for computer-aided or computer-implemented numerical control of automated machining machines for machining starting materials of the construction (11) in the form of load-bearing structure components, such as, for example,B. formwork (1, 17) and / or spacers (3, 4).

[0230] Fig. 24 shows schematically in the form of a simple flow chart, as an embodiment of the control method according to the invention, which is designed either centrally or decentrally, a sequence for the computer-aided or computer-implemented numerical control of automated assembly machines for the assembly of starting materials of the structure (11) in the form of load-bearing structure components such as formwork (1, 17) and / or spacers (3, 4), which is computer-implemented if necessary on at least one automated assembly machine (e.g. assembly robot). The first method step (2401) comprises the initialization of the control method. A further method step (2402) comprises the picking up and / or loading of at least one assembly part in the form of a starting material of the structure (11) by means of at least one assembly tool of the automated assembly machine.A further method step (2403) comprises moving to an assembly position with at least one assembly part using at least one assembly tool. A further method step (2404) comprises the computer-aided or computer-implemented, numerically controlled insertion and / or assembly of the assembly part using at least one assembly tool. This method step can also be carried out with the aid of an assembly cage (47) and / or an auxiliary assembly tool (48). A further method step (2405) comprises reading, comparing, calculating and / or processing the actual value of the current assembly status of the assembly part, which is present as input information in the form of a measured variable, with the target value of the assembly status of the assembly part, which is present as input information in the form of a stored or calculated value.If the result of the comparison of the actual value with the target value is not equal to the assembly part end position value, the previous method step (2404) is executed again. If the result of the comparison of the actual value with the target value is equal to the assembly part end position value, a further method step (2406) is initiated. This involves moving at least one assembly tool away from the assembly position. A further method step (2407) involves reading, comparing, calculating and / or processing the actual value of the current assembly status of the assembly parts, which is present as input information in the form of a measured variable, with the target value of the assembly status of the assembly parts, which is present as input information in the form of a stored or calculated value.If the result of the comparison of the actual value with the target value is not equal to the value of assembly parts fully assembled, method step 2402 is executed again. If the result of the comparison of the actual value with the target value is equal to the value of assembly parts fully assembled, the method for computer-aided or computer-implemented numerical control of automated assembly machines for the assembly of starting materials of the construction (11) in the form of load-bearing structure components such as formwork (1, 17) and / or spacers (3, 4) is terminated.This sequence of the control method can also be used for the computer-aided or computer-implemented, numerically controlled assembly of a component (55) or a raw, partial or complete construction (11), wherein the method steps comprise the computer-aided or computer-implemented, numerically controlled assembly of at least one assembly part in the form of a raw, partial or complete component framework (12) and / or at least one raw, partial or complete component element (54) and / or the computer-aided or computer-implemented, numerically controlled, step-by-step or incremental and additive joining, fastening and, if necessary, mutual sealing of raw, partial or complete component frameworks (12) and / or raw, partial or complete components (54).

[0231] List of reference symbols

[0232] 1 Formwork, two-dimensional construction element, in particular single, lost and / or stabilizing formwork

[0233] 2 Reinforcement

[0234] 3 Spacer, one-dimensional construction element, in particular shell spacer

[0235] 4 Spacer, one-dimensional construction element, in particular

[0236] Spacer

[0237] 5 Porous, open-pored material, such as wood

[0238] 6 Filling material, hardening, working mixture flowable or liquid, such as mortar, synthetic resin or impregnation

[0239] 7 Side facing the outside of the building or structure or, in particular, in the case of interior spaces, the side facing one interior space or, in general, with regard to the cross-section of the structure, the side facing a space outside the structure. Side facing the inside of the building or structure or, in particular, in the case of interior spaces, the side facing the other interior space or, in general, with regard to the cross-section of the structure, the side facing the other space outside the structure.

[0240] Side facing the upper floor or, in general terms of the cross-section of the structure, the side facing a room outside the structure

[0241] Side facing the lower floor or, in general terms with respect to the cross-section of the structure, the side facing the other room outside the structure, such as a shell, part or whole structure

[0242] Component scaffolding, such as raw, partial or complete component scaffolding

[0243] Shell building material, hardening, working mixture flowable or liquid, such as concrete 14a, 14b, ... Shell, at least one of at least two spaced-apart shells, made at least partially or completely by means of shell building material

[0244] 15a, 15b, ... shell, at least one of at least two spaced-apart shells, constructed by means of a single formwork

[0245] 16a, 16b, ... Intermediate space, bounded by at least two spaced-apart shells and enclosed between them

[0246] Formwork, two-dimensional construction element, in particular single, lost and / or stabilizing formwork, in particular made using sound, vibration and / or thermal insulation material, porous, open-pore material, material for absorbing moisture and / or material for absorbing or reflecting thermal radiation. Construction extension, such as conventional exterior cladding or right-handed foundation or support area.

[0247] Construction extension, such as conventional interior cladding or left-handed foundation or support area

[0248] Building or supply technology elements

[0249] Fluid lines

[0250] Heating and / or cooling circuit

[0251] Miniaturized heating and / or cooling unit

[0252] Refrigerant-air heat exchanger

[0253] compressor

[0254] 4-way valve

[0255] Evaporator or condenser

[0256] Filter / Dryer

[0257] capillary tube

[0258] fleece

[0259] Heat radiation panel plate heat exchanger

[0260] Measurement and / or control technology elements

[0261] Control unit

[0262] Sensor and / or input means Actuator and / or output means

[0263] Electrical line

[0264] Connection and sealing point

[0265] Fold, mutually overlapping, by means of a rectangular overlapping area

[0266] Fold, mutually overlapping, by means of an inclined overlapping surface (tongue and groove fold)

[0267] Fold, mutually overlapping, with click system

[0268] Fold, with groove and comb connection

[0269] Mutually sliding and interlocking profile

[0270] Sliding stop or sliding limitation

[0271] Mounting cage

[0272] Assembly tools, such as spacer tools

[0273] Assembly aids, such as centering surfaces

[0274] Construction module, such as raw, partial or complete construction module

[0275] Modular building block, such as a raw, partial or complete modular building block, extension of the border or boundary surface parallel to a wall, floor, ceiling or roof surface up to a size scale in the range of one square meter

[0276] Component, such as raw, partial or complete component

[0277] Component, such as raw, partial or complete component

[0278] PV panel

[0279] Circulation pump

[0280] Circuit with secondary medium

[0281] External fluid supply and / or discharge

[0282] Anchoring form, such as hole, thread, spiral, notch, milling, dovetail shape or mutually sliding and interlocking profile

[0283] Sealing shape, such as bore, thread, spiral, notch, milled recess, dovetail shape, mutually overlapping fold or nub, groove / comb and / or groove / tongue

[0284] Anchoring aid, such as screw, press, drill, thread, thread cutting or screw sleeve

[0285] Sealing aid, such as adhesive tape or expanding cord

[0286] Material such as elastic filling material

[0287] Material such as sound or impact sound insulation

Claims

Patent claims 1. A structure (11), in particular a shell, partial or complete structure, comprising at least two spaced-apart shells (14, 14a, 14b, 15, 15a, 15b) and a space (16, 16a, 16b) which is essentially empty except for structural and / or technical components, delimited by them and enclosed between them, wherein the structure includes a component framework (12) made of one- and two-dimensional structural elements in a composite construction, in particular a shell, partial or complete component framework, which structurally space the at least two spaced-apart shells, wherein the one-dimensional structural elements consist of structural components such as spacers (3, 4), in particular spacers made of wood, and the two-dimensional structural elements consist of structural components such as formwork (1, 17), in particular formwork made of wood, wherein the component framework includes a plurality of spacers,which are arranged in the space delimited by the at least two spaced-apart shells and enclosed between them, at least in at least one formwork adjacent to the space and / or at least in at least one formwork arranged in the space, by means of a press, glue or adhesive bond, by means of anchoring forms (60) or anchoring aids (64), in particular by means of drilled connections with hexagonally symmetrically arranged bores in the surface of the formwork, designed as formwork-penetrating bores or as blind bores, connected, fastened, sealed and / or anchored, and which are arranged in particular on the basis of a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, inclined at an angle of 45° to the surface of the formwork.

2. Construction according to claim 1, wherein the component framework at least partially forms the intermediate space delimited by the at least two spaced-apart shells and enclosed between them and / or at least one of the at least two spaced-apart shells.

3. Construction according to one of the preceding claims, characterized in particular by a wall, floor, ceiling and / or roof construction of a building or a structure, wherein the construction or the component framework can be designed in the form of a construction module (50), a modular building block (52), a building element (54) or a component (55).

4. Construction according to one of the preceding claims, characterized in that at least one of the at least two spaced-apart shells (14, 14a, 14b) comprises a shell building material (13), wherein the shell building material at least partially fills the shell and the plurality of in the space delimited by the at least two spaced-apart shells and between them The spacers arranged in the enclosed space preferably extend into the shell material and are connected, fastened, sealed and / or anchored in the same by means of anchoring forms or anchoring aids.

5. Construction according to one of the preceding claims, wherein the spacers and / or the formworks are filled with a setting material (6), in particular such that the working mixture of the setting material has penetrated into the pores in at least part of the surface area of ​​the spacers and / or the formworks and has closed and sealed them during the subsequent hardening of the working mixture of the setting material.

6. Method for displacing one- or two-dimensional structural components of a construction (11), in particular spacers (3, 4) consisting of wood or formwork (1, 17) consisting of wood, with a working mixture of a displacing material (6), in particular the coordinated, controlled and / or process-induced displacing of the working mixture into the pores in at least part of the surface area of ​​the spacers or the formwork.

7. A method for machining two-dimensional construction elements and structural components of a structure (11), such as formwork (1, 17), the method comprising shaping machining steps with regard to the border or geometric shape of the two-dimensional structural components, which are carried out by means of a computer-aided or computer-implemented numerical control of at least one automated processing machine (CNC machine), wherein in particular a plurality of hexagonally symmetrically arranged bores are made in the surface of the formwork, designed as formwork-penetrating bores or as blind bores, on the basis of a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, which are arranged obliquely, at an angle of 45° to the surface of the formwork.

8. A method for producing a component scaffold (12), in particular a component scaffold according to one of claims 1 - 5, wherein the manufacturing method comprises shaping method steps such as the gradual, partial or complete introduction, assembly, joining, connecting, fastening, sealing and / or anchoring of processed starting materials such as spacers (3, 4), as one-dimensional construction elements, and formwork (1, 17), as two-dimensional construction elements, to a component scaffold made from the same in a composite construction by means of a press, glue or adhesive bond, by means of anchoring forms (60), anchoring aids (64) or drilled connections, wherein the method steps in particular comprise the introduction and assembly of a plurality of one-dimensional structural components, such as spacers (4) in the in a two-dimensional structural component, such asa formwork (1, 17) previously provided, hexagonally symmetrically arranged, holes in the surface of the formwork,. executed as formwork-penetrating boreholes or as blind boreholes, which are arranged on the basis of a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, inclined, at an angle of 45° to the surface of the formwork.

9. A method for producing a construction (11), in particular a construction according to one of claims 1-5, wherein the manufacturing method comprises shaping process steps such as the gradual, partial or complete introduction, assembly, joining, connecting, fastening, sealing and / or anchoring of processed starting materials such as spacers (3, 4), as one-dimensional construction elements, and formwork (1, 17), as two-dimensional construction elements, to a component framework made of the same in a composite construction by means of press, glue or adhesive bonding, by means of anchoring forms (60), anchoring aids (64) or drilled connections, wherein the process steps in particular comprise the introduction and assembly of a plurality of one-dimensional structural components, such as spacers (4) into the previously attached in a two-dimensional structural component, such as a formwork (1, 17),hexagonally symmetrically arranged boreholes in the surface of the formwork, designed as formwork-penetrating boreholes or as blind boreholes, which are arranged on the basis of a hexagonal grid with at least one borehole circle and in hexagonally symmetrical orientations, inclined, at an angle of 45° to the surface of the formwork, wherein the construction, if required, comprises a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells and is introduced in the form of a working mixture into at least one formwork as a shaping formwork / casting mold and, if necessary, into at least one additional and / or independent, temporary formwork / casting mold,wherein the plurality of spacers arranged in the space delimited by the at least two spaced-apart shells and enclosed between them preferably extend into the shell building material and are connected, fastened, sealed and / or anchored therein by means of anchoring forms or anchoring aids.

10. A method for producing a construction (11), in particular a construction according to one of claims 1-5, wherein the manufacturing method comprises shaping process steps such as the step-by-step, partial or complete assembly or joining of at least one component framework and / or the step-by-step or incremental and additive joining, connecting, fastening, sealing and / or anchoring of component frameworks with, against and among each other by means of press, glue and / or adhesive bonds, by means of anchoring forms (60) and / or sealing forms (61) and / or by means of anchoring aids (64) and / or sealing aids (65), wherein the construction, if required, comprises a shell building material (13) which at least partially fills at least one of the at least two spaced-apart shells and is introduced in the form of a working mixture into at least one formwork as a shaping formwork / casting mold and, if required, into at least one additional and / or independent, temporary formwork / casting mold, wherein the plurality of spacers arranged in the space delimited by the at least two spaced-apart shells and enclosed between them preferably extend into the shell building material and are connected, fastened, sealed and / or anchored in the same by means of anchoring forms or anchoring aids.

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