ES2329853A1 - Component for support structure - Google Patents

Component for support structure Download PDF

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Publication number
ES2329853A1
ES2329853A1 ES200600376A ES200600376A ES2329853A1 ES 2329853 A1 ES2329853 A1 ES 2329853A1 ES 200600376 A ES200600376 A ES 200600376A ES 200600376 A ES200600376 A ES 200600376A ES 2329853 A1 ES2329853 A1 ES 2329853A1
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Prior art keywords
wings
component according
pair
parallel
prominences
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Granted
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ES200600376A
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Spanish (es)
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ES2329853B1 (en
Inventor
Bruno Nicoletti
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Metal Work SpA
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Metal Work SpA
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Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00—Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/74—Removable non-load-bearing partitions; Partitions with a free upper edge
    • E04B2/7407—Removable non-load-bearing partitions; Partitions with a free upper edge assembled using frames with infill panels or coverings only; made-up of panels and a support structure incorporating posts
    • E04B2/7453—Removable non-load-bearing partitions; Partitions with a free upper edge assembled using frames with infill panels or coverings only; made-up of panels and a support structure incorporating posts with panels and support posts, extending from floor to ceiling
    • E04B2/7455—Glazing details
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00—Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/74—Removable non-load-bearing partitions; Partitions with a free upper edge
    • E04B2/76—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal
    • E04B2/78—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal characterised by special cross-section of the frame members as far as important for securing wall panels to a framework with or without the help of cover-strips
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00—Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/74—Removable non-load-bearing partitions; Partitions with a free upper edge
    • E04B2/76—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal
    • E04B2/78—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal characterised by special cross-section of the frame members as far as important for securing wall panels to a framework with or without the help of cover-strips
    • E04B2/7809—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal characterised by special cross-section of the frame members as far as important for securing wall panels to a framework with or without the help of cover-strips of single or multiple tubular form
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00—Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/74—Removable non-load-bearing partitions; Partitions with a free upper edge
    • E04B2/76—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal
    • E04B2/78—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal characterised by special cross-section of the frame members as far as important for securing wall panels to a framework with or without the help of cover-strips
    • E04B2/7809—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal characterised by special cross-section of the frame members as far as important for securing wall panels to a framework with or without the help of cover-strips of single or multiple tubular form
    • E04B2/7818—Removable non-load-bearing partitions; Partitions with a free upper edge with framework or posts of metal characterised by special cross-section of the frame members as far as important for securing wall panels to a framework with or without the help of cover-strips of single or multiple tubular form of substantially rectangular form
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00—Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/07—Reinforcing elements of material other than metal, e.g. of glass, of plastics, or not exclusively made of metal
    • E04C5/073—Discrete reinforcing elements, e.g. fibres

Abstract

In a component for supporting structures, a central body with a passing axial hole has on a front external wall and a rear external wall a first front seat and a first rear seat, accessible from outside and symmetrical with a first longitudinal symmetry plane of the body. Other external walls of the central body, namely a right external wall and a left external wall, have respectively a second right seat and a second left seat, accessible from the outside and symmetrical with respect to a second longitudinal symmetry plane extending at right angles to the first longitudinal symmetry plane of the central body.

Description

Componente para estructuras portantes.Component for bearing structures.

La presente invención se enmarca dentro del sector técnico relativo a la realización de estructuras portantes.The present invention is framed within the technical sector related to the realization of structures carriers

En el caso específico, la presente invención se refiere a un componente para estructuras portantes.In the specific case, the present invention will be refers to a component for bearing structures.

Son conocidos componentes para estructuras portantes constituidos por un perfil, con sección inscrita en un perfil cuadrangular, que forman en correspondencia con las superficies propias exteriores respectivas acanaladuras con sección trapezoidal (en forma de cola de milano). Estos perfiles tienen habitualmente acanaladuras iguales entre ellas, y pueden por lo tanto ser poco versátiles en el caso de que se necesiten acoplamientos especiales entre elementos de la estructura o dispositivos asociados a esta última.Components for structures are known supporters consisting of a profile, with a section inscribed in a quadrangular profile, which form in correspondence with the respective own external surfaces grooves with section trapezoidal (in the form of dovetail). These profiles have usually the same grooves between them, and they can therefore both be little versatile in case they are needed special couplings between elements of the structure or devices associated with the latter.

El objeto de la presente invención es proponer un componente para estructuras portantes que permita un ensamblaje rápido de la estructura, confiriéndole, al mismo tiempo, elevadas características de robustez y rigidez, de modo que tenga una versatilidad mayor respecto a los componentes con perfiles conocidos.The object of the present invention is to propose a component for bearing structures that allows assembly fast structure, conferring at the same time high robustness and stiffness characteristics, so that you have a greater versatility compared to components with profiles known.

Otro objeto de la presente invención consiste en proponer un componente para estructuras portantes que tenga dos caras contrapuestas iguales entre sí, y las restantes caras, también éstas iguales entre sí, pero conformadas de modo distinto a las primeras.Another object of the present invention consists in propose a component for bearing structures that has two opposite faces equal to each other, and the remaining faces, also these equal to each other, but shaped differently from the first.

A esto se le añade la intención de proponer un componente para estructuras portantes, extremadamente fiable, con un coste moderado, que pueda asegurar un fácil ensamblaje del mismo a elementos asociados y/o dispositivos.To this is added the intention of proposing a component for supporting structures, extremely reliable, with a moderate cost, which can ensure easy assembly of the same at associated elements and / or devices.

Los objetos anteriormente indicados se obtienen de acuerdo con el contenido de las reivindicaciones.The aforementioned objects are obtained according to the content of the claims.

Las características de la invención serán señaladas a continuación donde se describe una forma de realización preferida, pero no exclusiva, y una relativa variación en su realización, con referencia a los dibujos adjuntos en los que:The characteristics of the invention will be indicated below where an embodiment is described preferred, but not exclusive, and a relative variation in its realization, with reference to the attached drawings in which:

- las figuras 1, 2 ilustran esquemáticamente otras tantas vistas en planta del componente propuesto para estructuras portantes y de su variante de realización;- Figures 1, 2 schematically illustrate many other plan views of the proposed component for supporting structures and their variant embodiment;

- las figuras 3, 4, 5 representan de modo esquemático, otras tantas vistas en planta del componente al que hace referencia la figura 2, en disposición ensamblada a elementos asociados.- Figures 3, 4, 5 represent so schematic, many other plan views of the component to which referenced in figure 2, in assembled arrangement to elements Associates

Con referencia a las figuras 1 y 2 conviene indicar con 100 el componente propuesto para estructuras portantes constituido por un cuerpo central 2, de sección sustancialmente rectangular, con predominante desarrollo longitudinal y en el que se dispone un agujero pasante axial 1.With reference to figures 1 and 2, it is convenient indicate with 100 the proposed component for bearing structures constituted by a central body 2, of substantially section rectangular, with predominantly longitudinal development and in which it has an axial through hole 1.

Tal cuerpo central 2 está provisto en correspondencia con las paredes externas, respectivamente anterior 3 y posterior 4, de correspondientes asientos primarios, anterior 3A y posterior 4A, accesibles desde el exterior y simétricos respecto a un primer plano longitudinal L del mismo cuerpo 2. Este último forma además, en correspondencia con las restantes paredes externas, respectivamente (haciendo referencia a las figuras 1, 2) derecha 5 e izquierda 6, los correspondientes asientos secundarios, derecho 5A e izquierdo 6A, accesibles desde el exterior y simétricos respecto a un segundo plano longitudinal T, ortogonal al primero L, del propio cuerpo 2.Such central body 2 is provided in correspondence with the external walls, respectively previous 3 and later 4, of corresponding primary seats, previous 3A and later 4A, accessible from the outside and symmetrical with respect to a longitudinal first plane L of the same body 2. The latter also, in correspondence with the remaining external walls, respectively (referring to figures 1, 2) right 5 e left 6, the corresponding secondary seats, right 5A and left 6A, accessible from the outside and symmetrical with respect to a longitudinal second plane T, orthogonal to the first L, of the own body 2.

En particular, el asiento primario anterior 3A está definido por una porción 31, de la pared externa anterior 3, paralela al primer plano longitudinal L en cooperación con el primer par de prominencias 30 que se extienden hacia el exterior respecto al cuerpo central 2 y plegadas la una hacia la otra.In particular, the front primary seat 3A it is defined by a portion 31, of the anterior external wall 3, parallel to the longitudinal longitudinal plane L in cooperation with the first pair of prominences 30 extending outward with respect to the central body 2 and folded towards each other.

El asiento primario posterior 4A está definido por una porción 41, de la pared externa posterior 4, paralela al primer plano longitudinal L en cooperación con un segundo par de prominencias 40 que se extienden hacia el exterior respecto al cuerpo central 2 y plegadas la una hacia la otra.The rear primary seat 4A is defined by a portion 41, of the rear outer wall 4, parallel to the longitudinal foreground L in cooperation with a second pair of prominences 40 that extend outward from the central body 2 and folded towards each other.

El asiento secundario derecho 5A está definido por una porción 51, de la pared externa derecha 5, paralela al segundo plano longitudinal T en cooperación con un primer par de alas 50, que se extienden hacia el exterior respecto al cuerpo central 2, definido por un ala anterior 50A y un ala posterior 50B paralelas entre sí.The right secondary seat 5A is defined by a portion 51, of the right outer wall 5, parallel to the longitudinal background T in cooperation with a first pair of wings 50, which extend outwardly relative to the body central 2, defined by a front wing 50A and a rear wing 50B parallel to each other.

El asiento secundario izquierdo 6A está definido por al menos una porción 61, de la pared externa izquierda 6, paralela al segundo plano longitudinal T en cooperación con un segundo par de alas 60, que se extienden hacia el exterior respecto al cuerpo central 2, definido por un ala anterior 60A y un ala posterior 60B paralelas entre sí.The left secondary seat 6A is defined by at least a portion 61, of the left outer wall 6, parallel to the longitudinal second plane T in cooperation with a second pair of wings 60, which extend outwardly with respect to to the central body 2, defined by an anterior wing 60A and a wing posterior 60B parallel to each other.

Las superficies externas (52, 62) de las alas posteriores (50B, 60B) resultan internas, en relación con el primer plano longitudinal L, respecto a las correspondientes superficies externas de las porciones (31, 41) de las paredes externas, anterior 3 y posterior 4.The outer surfaces (52, 62) of the wings later (50B, 60B) are internal, in relation to the first longitudinal plane L, with respect to the corresponding surfaces outer portions (31, 41) of the outer walls, previous 3 and later 4.

El componente 100 (ver figura 1) puede obtenerse mediante extrusión: en tal caso, cada uno de los extremos libres de las alas pertenecientes al primer 50 y al segundo 60 par de alas forman, por ejemplo, un escalón 55.Component 100 (see figure 1) can be obtained by extrusion: in this case, each of the free ends of the wings belonging to the first 50 and the second 60 pair of wings they form, for example, a step 55.

Según una variante de realización, ilustrada en la figura 2, el componente 100 puede realizarse mediante una chapa 80 plegada de modo que determine una duplicación del espesor del perfil del componente 100 en relación con las prominencias (30, 40) y con los pares de alas (50, 60), para conferir a tales elementos una mayor rigidez.According to a variant embodiment, illustrated in Figure 2, the component 100 can be realized by means of a sheet 80 folded so as to determine a doubling of the thickness of the Profile of component 100 in relation to prominences (30, 40) and with the pairs of wings (50, 60), to confer on such elements greater rigidity

El extremo libre de cada una de las alas pertenecientes al primer 50 y al segundo 60 par de alas, forma un redondeamiento 56.The free end of each of the wings belonging to the first 50 and the second 60 pair of wings, forms a rounding 56.

En la figura 3 está representado el componente 100 de la figura 2, en disposición de ensamblaje con elementos asociados. Más concretamente, el asiento primario posterior 4A, cooperando con medios de soporte conocidos, permite la sujeción de un panel divisorio, por ejemplo una lámina de cristal 11.In figure 3 the component is represented 100 of Figure 2, in assembly arrangement with elements Associates More specifically, the rear primary seat 4A, cooperating with known support means, allows the clamping of a dividing panel, for example a glass sheet 11.

En la figura 4 está representado el mismo componente 100 de la figura 2, en disposición de ensamblaje con otros elementos asociados. En concreto, el asiento primario posterior 4A, cooperando con medios de enlace conocidos, permite la sujeción de un par de láminas de cristal 11A.In figure 4 the same is represented component 100 of Figure 2, in assembly arrangement with Other associated elements. Specifically, the primary seat subsequent 4A, cooperating with known link means, allows the holding a pair of 11A glass sheets.

En la figura 5 están representados tres componentes, respectivamente primero 100A, segundo 100B, y tercero 100C, cada uno análogo al ilustrado en la figura 2, en disposición de ensamblaje con elementos asociados. El asiento primario posterior 4A del primer componente 100A, permite el enganche a este último de un elemento estructural terminal 85.In figure 5 three are represented components, respectively first 100A, second 100B, and third 100C, each analogous to that illustrated in Figure 2, in arrangement of assembly with associated elements. The rear primary seat 4A of the first component 100A, allows the attachment to the latter of a terminal structural element 85.

Entre el primero 100A y el segundo 100B componente, hay un par de paneles 11C vinculados a los propios componentes (100A, 100B) mediante piezas de fijación conocidas.Between the first 100A and the second 100B component, there are a couple of 11C panels linked to the own components (100A, 100B) by known fixing parts.

El asiento primario anterior 3A del segundo componente 100B y el asiento primario posterior 4A del tercer componente 100C, en cooperación con medios de retención conocidos, permiten el bloqueo entre tales componentes (100B, 100C) de un elemento angular.The previous primary seat 3A of the second component 100B and the rear primary seat 4A of the third component 100C, in cooperation with known retention means, allow blocking between such components (100B, 100C) of a angular element.

El asiento primario anterior 3A del tercer componente 100C, cooperando con medios de soporte conocidos, permite la sujeción de un panel divisorio 11B.The primary primary seat 3A of the third 100C component, cooperating with known support means, allows the fastening of a partition panel 11B.

Ventajosamente, el componente propuesto permite un ensamblaje rápido de la estructura portante, confiriéndole al mismo tiempo elevadas características de robustez y rigidez.Advantageously, the proposed component allows a quick assembly of the supporting structure, giving the At the same time high characteristics of robustness and rigidity.

El componente descrito con anterioridad, al estar caracterizado por caras contrapuestas iguales dos a dos y que forman los respectivos asientos, puede ser notablemente versátil en el caso de que se necesiten acoplamientos especiales entre dos o más elementos de la estructura, o se necesite bloquear amoviblemente elementos y/o dispositivos asociados a la estructura, por ejemplo utilizando los asientos secundarios (5, 6).The component described above, at be characterized by opposing faces equal two to two and that form the respective seats, can be remarkably versatile in the case that special couplings are needed between two or more elements of the structure, or block needs to be locked removably elements and / or devices associated with the structure, for example using the secondary seats (5, 6).

Tal versatilidad tiene su reflejo positivo en los tiempos de ensamblaje de la estructura, que son reducidos, confiriendo a esta última, al mismo tiempo, elevadas características de robustez y rigidez.Such versatility has its positive reflection on the assembly times of the structure, which are reduced, conferring to the latter, at the same time, high robustness and stiffness characteristics.

A partir de lo expuesto anteriormente, es evidente que el componente descrito asegura elevados niveles de fiabilidad en cualquier condición de ensamblaje.From the above, it is It is clear that the described component ensures high levels of reliability in any assembly condition.

Hay que subrayar además que el componente es extremadamente fiable y tiene un coste moderado.It should also be stressed that the component is Extremely reliable and has a moderate cost.

La invención en cuestión ha sido obviamente descrita en referencia a los dibujos adjuntos, a mero título de ejemplo, y no limitativo, y es evidente, por lo tanto, que sobre ésta se pueden realizar todas las modificaciones o variaciones que estén comprendidas en el ámbito definido por las reivindicaciones siguientes.The invention in question has obviously been described in reference to the attached drawings, by way of example, and not limiting, and it is clear, therefore, that about this one can make all the modifications or variations that are within the scope defined by the claims following.

Claims (17)

1. Componente para estructuras portantes, caracterizado porque está formado por un cuerpo central 2, con predominante desarrollo longitudinal en el que se dispone un agujero pasante axial 1, provisto, en correspondencia con las paredes externas, respectivamente anterior 3 y posterior 4, de correspondientes asientos primarios, anterior 3A y posterior 4A, accesibles desde el exterior y simétricos respecto a un primer plano longitudinal L del mismo cuerpo 2; con este último forma además, en correspondencia con las restantes paredes externas, respectivamente derecha 5 e izquierda 6, los correspondientes asientos secundarios, derecho 5A e izquierdo 6A, accesibles desde el exterior y simétricos respecto a un segundo plano longitudinal T, ortogonal al primero L, del propio cuerpo 2.1. Component for bearing structures, characterized in that it is formed by a central body 2, with a predominantly longitudinal development in which an axial through hole 1 is provided, corresponding, in correspondence with the external walls, respectively anterior 3 and posterior 4, of corresponding primary seats, front 3A and rear 4A, accessible from the outside and symmetrical with respect to a longitudinal first plane L of the same body 2; with the latter also, in correspondence with the remaining external walls, respectively right 5 and left 6, the corresponding secondary seats, right 5A and left 6A, accessible from the outside and symmetrical with respect to a second longitudinal plane T, orthogonal to the first L , of the body itself 2. 2. Componente según la reivindicación 1, caracterizado porque el citado asiento primario anterior 3A está definido por al menos una porción 31, de la mencionada pared externa anterior 3, paralela a dicho primer plano longitudinal L en cooperación con un primer par de prominencias 30 que se extienden hacia el exterior respecto a dicho cuerpo central 2; y porque el citado asiento primario posterior 4A está definido por al menos una porción 41, de la mencionada pared externa posterior 4, paralela a dicho primer plano longitudinal L en cooperación con un segundo par de prominencias 40 que se extienden hacia el exterior respecto a dicho cuerpo central 2.2. Component according to claim 1, characterized in that said said primary primary seat 3A is defined by at least a portion 31, of said anterior external wall 3, parallel to said first longitudinal plane L in cooperation with a first pair of prominences 30 which they extend outwardly with respect to said central body 2; and because said rear primary seat 4A is defined by at least a portion 41, of said rear exterior wall 4, parallel to said first longitudinal plane L in cooperation with a second pair of prominences 40 extending outwardly with respect to said central body 2. 3. Componente según la reivindicación 1, caracterizado porque el citado asiento secundario derecho 5A está definido por al menos una porción 51, de la mencionada pared externa derecha 5, paralela a dicho segundo plano longitudinal T en cooperación con un primer par de alas 50 que se extienden hacia el exterior respecto a dicho cuerpo central 2; y porque el citado asiento secundario izquierdo 6A está definido por al menos una porción 61, de la mencionada pared externa izquierda 6, paralela a dicho segundo plano longitudinal T en cooperación con un segundo par de alas 60 que se extienden hacia el exterior respecto a dicho cuerpo central 2.3. Component according to claim 1, characterized in that said right secondary seat 5A is defined by at least a portion 51, of said right outer wall 5, parallel to said second longitudinal plane T in cooperation with a first pair of wings 50 which they extend outwardly with respect to said central body 2; and because said left secondary seat 6A is defined by at least a portion 61, of said left outer wall 6, parallel to said second longitudinal plane T in cooperation with a second pair of wings 60 extending outwardly with respect to said central body 2. 4. Componente según la reivindicación 3, caracterizado porque el citado primer par de alas 50 está definido por un ala anterior 50A y por un ala posterior 50B.4. Component according to claim 3, characterized in that said first pair of wings 50 is defined by a front wing 50A and a rear wing 50B. 5. Componente según la reivindicación 3, caracterizado porque el citado segundo par de alas 60 está definido por un ala anterior 60A y por un ala posterior 60B.5. Component according to claim 3, characterized in that said second pair of wings 60 is defined by a front wing 60A and a rear wing 60B. 6. Componente según las reivindicaciones 2 y 3, caracterizado porque las superficies externas (52, 62) de las alas posteriores (50B, 60B) pertenecientes a dicho primer 50 y segundo 60 par de alas resultan internas, en relación con dicho primer plano longitudinal L, respecto a las correspondientes superficies externas de dichas porciones (31, 41) de las mencionadas paredes externas, anterior 3 y posterior 4.6. Component according to claims 2 and 3, characterized in that the external surfaces (52, 62) of the rear wings (50B, 60B) belonging to said first 50 and second 60 pairs of wings are internal, in relation to said first longitudinal plane L, with respect to the corresponding external surfaces of said portions (31, 41) of said external walls, anterior 3 and posterior 4. 7. Componente según la reivindicación 1, caracterizado porque las alas (50A, 50B) que constituyen el primer par de alas 50 son entre ellas paralelas.7. Component according to claim 1, characterized in that the wings (50A, 50B) constituting the first pair of wings 50 are parallel to each other. 8. Componente según la reivindicación 1, caracterizado porque las alas (60A, 60B) que constituyen el segundo par de alas 60 son entre ellas paralelas.8. Component according to claim 1, characterized in that the wings (60A, 60B) constituting the second pair of wings 60 are parallel to each other. 9. Componente según la reivindicación 1, caracterizado porque las citadas porciones (51, 61) de las mencionadas paredes externas, derecha 5 e izquierda 6, son paralelas a dicho segundo plano longitudinal T.9. Component according to claim 1, characterized in that said portions (51, 61) of said external walls, right 5 and left 6, are parallel to said second longitudinal plane T. 10. Componente según la reivindicación 1, caracterizado porque las citadas porciones (31, 41) de las mencionadas paredes externas, anterior 3 y posterior 4, son paralelas a dicho primer plano longitudinal L.10. Component according to claim 1, characterized in that said portions (31, 41) of said external walls, anterior 3 and posterior 4, are parallel to said first longitudinal plane L. 11. Componente según la reivindicación 1, caracterizado por ser obtenido por extrusión.11. Component according to claim 1, characterized in that it is obtained by extrusion. 12. Componente según las reivindicaciones 3 y 11, caracterizado por formar un escalón 55 dispuesto en el extremo libre de cada una de las alas pertenecientes a los citados primer 50 y segundo 60 par de alas.12. Component according to claims 3 and 11, characterized by forming a step 55 disposed at the free end of each of the wings belonging to said first 50 and second 60 pair of wings. 13. Componente según las reivindicaciones 2 y 3, caracterizado por estar formado por una chapa plegada, de modo que duplica el espesor del perfil de dicho componente 100 en las citadas prominencias (30, 40) y en los citados pares de alas (50, 60).13. Component according to claims 2 and 3, characterized in that it is formed by a folded sheet, such that it doubles the thickness of the profile of said component 100 in said prominences (30, 40) and in said pairs of wings (50, 60). 14. Componente según la reivindicación 13, caracterizado por formar un redondeamiento 56 en el extremo libre de cada una de las alas pertenecientes a dichos primer 50 y segundo 60 pares de alas.14. Component according to claim 13, characterized by forming a rounding 56 at the free end of each of the wings belonging to said first 50 and second 60 pairs of wings. 15. Componente según la reivindicación 2, caracterizado porque las prominencias que constituyen dicho primer par de prominencias 30 están plegadas la una hacia la otra.15. Component according to claim 2, characterized in that the prominences constituting said first pair of prominences 30 are folded towards each other. 16. Componente según la reivindicación 2, caracterizado porque las prominencias que constituyen dicho segundo par de prominencias 40 están plegadas la una hacia la otra.16. Component according to claim 2, characterized in that the prominences constituting said second pair of prominences 40 are folded towards each other. 17. Componente según la reivindicación 1, caracterizado porque el citado cuerpo central 2 tiene una sección sustancialmente rectangular.17. Component according to claim 1, characterized in that said central body 2 has a substantially rectangular section.
ES200600376A 2005-02-17 2006-02-17 COMPONENT FOR CARRIER STRUCTURES. Expired - Fee Related ES2329853B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT000074A ITBO20050074A1 (en) 2005-02-17 2005-02-17 COMPONENT FOR BEARING STRUCTURES
ITBO05A0074 2005-02-17

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ES2329853A1 true ES2329853A1 (en) 2009-12-01
ES2329853B1 ES2329853B1 (en) 2010-09-16

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AU2002952991A0 (en) * 2002-11-29 2002-12-12 Somerville, Declan Garden extrusion
US9850656B2 (en) 2014-09-02 2017-12-26 Chung Jong Lee Construction panel assembly and construction method using same
FR3048442B1 (en) * 2016-03-01 2020-09-18 Benjamin Parzy PILLAR OR POST SUITABLE TO RECEIVE WALLS, PANELS OR SIMILAR, FOR EXAMPLE FOR FENCES, OR FOR FURNITURE

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EP0600545A1 (en) * 1992-12-01 1994-06-08 HYDRO ALUMINIUM SYSTEMS S.p.A. Set of metal sections suitable for constructing movable partition walls and related movable partition wall
WO2004083545A1 (en) * 2003-03-18 2004-09-30 Alprogetti S.R.L. System for fixing wall coverings to mullions

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FR2150257A1 (en) * 1971-08-23 1973-04-06 Royon Regis
FR2376927A1 (en) * 1977-01-06 1978-08-04 Diffusion Materiel Stockage H=section mullion for releasable mounting of glazed panels - has sub-flanges and houses clips retaining panel ends and masking strips
DE3532507A1 (en) * 1985-04-15 1987-03-19 Moeller Automation Gmbh Supporting profiles for mounting devices, supporting structures and conveyor belts
EP0600545A1 (en) * 1992-12-01 1994-06-08 HYDRO ALUMINIUM SYSTEMS S.p.A. Set of metal sections suitable for constructing movable partition walls and related movable partition wall
WO2004083545A1 (en) * 2003-03-18 2004-09-30 Alprogetti S.R.L. System for fixing wall coverings to mullions

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