ITBO20080754A1 - MODULAR BEAM DEVICE - Google Patents

MODULAR BEAM DEVICE Download PDF

Info

Publication number
ITBO20080754A1
ITBO20080754A1 IT000754A ITBO20080754A ITBO20080754A1 IT BO20080754 A1 ITBO20080754 A1 IT BO20080754A1 IT 000754 A IT000754 A IT 000754A IT BO20080754 A ITBO20080754 A IT BO20080754A IT BO20080754 A1 ITBO20080754 A1 IT BO20080754A1
Authority
IT
Italy
Prior art keywords
thickness
longitudinal
core
elements
wing
Prior art date
Application number
IT000754A
Other languages
Italian (it)
Inventor
Davide Ciceri
Original Assignee
Lynx S R L
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Lynx S R L filed Critical Lynx S R L
Priority to IT000754A priority Critical patent/ITBO20080754A1/en
Publication of ITBO20080754A1 publication Critical patent/ITBO20080754A1/en

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C3/06Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal with substantially solid, i.e. unapertured, web
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0408Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section
    • E04C2003/0413Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section being built up from several parts
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0408Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section
    • E04C2003/0413Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section being built up from several parts
    • E04C2003/0417Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section being built up from several parts demountable
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0426Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section
    • E04C2003/043Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section the hollow cross-section comprising at least one enclosed cavity
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0426Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section
    • E04C2003/0434Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section the open cross-section free of enclosed cavities
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0443Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by substantial shape of the cross-section
    • E04C2003/0452H- or I-shaped
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/04Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
    • E04C2003/0404Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
    • E04C2003/0443Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by substantial shape of the cross-section
    • E04C2003/0465Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by substantial shape of the cross-section square- or rectangular-shaped

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Air Bags (AREA)
  • Forging (AREA)
  • Thin Film Transistor (AREA)

Description

DISPOSITIVO A TRAVE MODULARE MODULAR BEAM DEVICE

DESCRIZIONE DELL'INVENZIONE DESCRIPTION OF THE INVENTION

La presente invenzione s'inquadra nel settore concernente le costruzioni e l’edilizia e si riferisce ad un dispositivo a trave modulare realizzabile con vari elementi per ottenere caratteristiche meccaniche diverse e particolarmente adatto alla realizzazione di strutture, anche prefabbricate, quali coperture mobili e telescopiche, vetrate, serre, giardini d’inverno, pensiline, tettoie ed in genere costruzioni, arredi ed elementi edili. The present invention is part of the construction and building sector and refers to a modular beam device that can be made with various elements to obtain different mechanical characteristics and is particularly suitable for the construction of structures, including prefabricated structures, such as mobile and telescopic covers, windows, greenhouses, winter gardens, canopies, canopies and buildings, furnishings and building elements in general.

Sono noti travi profilati, ad esempio in alluminio, aventi sezioni tubolati oppure a “T”, a “I” e destinati a realizzare costruzioni e strutture. Profiled beams are known, for example in aluminum, having tubular or "T", "I" -shaped sections and intended for building constructions and structures.

Uno svantaggio di tali dispositivi noti consiste nel fatto che ciascuno di essi ha proprie specifiche caratteristiche meccaniche e che pertanto devono essere realizzati con sezioni di varie forme e dimensioni per soddisfare tutte le possibili esigenze di utilizzo; ciò comporta elevati oneri di produzione, immagazzinamento, trasporto e di gestione. A disadvantage of these known devices consists in the fact that each of them has its own specific mechanical characteristics and that therefore they must be made with sections of various shapes and sizes to satisfy all the possible requirements of use; this entails high production, storage, transport and management costs.

Uno scopo della presente invenzione è quello di proporre un dispositivo a trave modulare realizzabile con varie caratteristiche meccaniche a partire da un ridotto numero di elementi componibili per minimizzare i costi di produzione, gestione immagazzinamento e trasporto. An object of the present invention is to propose a modular beam device which can be manufactured with various mechanical characteristics starting from a reduced number of modular elements in order to minimize the costs of production, management, storage and transport.

Altro scopo è quello di proporre un dispositivo a trave modulare che sia utilizzabile anche come traversa orizzontale, montante verticale, elemento inclinato, etc. Ulteriore scopo è di proporre un dispositivo che di gradevole aspetto ed utilizzabile anche in vista. Another purpose is to propose a modular beam device that can also be used as a horizontal crosspiece, vertical upright, inclined element, etc. A further object is to propose a device which has a pleasant appearance and can also be used in sight.

Le caratteristiche dell'invenzione sono nel seguito evidenziate con particolare riferimento agli uniti disegni nei quali: The characteristics of the invention are highlighted below with particular reference to the accompanying drawings in which:

- la figura 1 illustra una vista in sezione trasversale di un elemento ad ala del dispositivo a trave modulare oggetto della presente invenzione; Figure 1 illustrates a cross-sectional view of a wing element of the modular beam device object of the present invention;

- la figura 2 illustra una vista in sezione trasversale di due elementi ad ala di figura 1 reciprocamente fissati da un primo elemento ad anima realizzando una forma del dispositivo a trave; Figure 2 illustrates a cross-sectional view of two wing elements of Figure 1 mutually fixed by a first core element, making a shape of the beam device;

- la figura 3 illustra una vista in sezione trasversale di due elementi ad ala di figura 1 reciprocamente fissati da un secondo elemento ad anima realizzando una ulteriore forma del dispositivo a trave; figure 3 shows a cross-sectional view of two wing elements of figure 1 mutually fixed by a second core element, realizing a further shape of the beam device;

- la figura 4 illustra una vista in sezione trasversale di due elementi ad ala di figura 1 reciprocamente fissati dal primo elemento ad anima di figura 2 e da due mezzi ad anima laterali realizzando un’altra forma del dispositivo a trave. - Figure 4 illustrates a cross-sectional view of two wing elements of Figure 1 mutually fixed by the first core element of Figure 2 and by two lateral core means realizing another shape of the beam device.

Con riferimento alle figure 1 e 2, con 1 viene indicato il dispositivo a trave modulare oggetto della presente invenzione. With reference to Figures 1 and 2, 1 indicates the modular beam device object of the present invention.

Il dispositivo 1 può essere costituito da uno o preferibilmente due elementi ad ala 2 fissati, preferibilmente tramite mezzi d’incollaggio a resina epossidica, ad uno o più elementi ad anima 7, 8, 9, 10 che, eventualmente, interconnettono i due elementi ad ala 2. Gli elementi ad anima fissati all’elemento od elementi ad ala 2 possono essere di vario numero tipo e dimensioni per conferire al dispositivo a trave diverse caratteristiche meccaniche. The device 1 can be constituted by one or preferably two wing elements 2 fixed, preferably by means of epoxy resin gluing means, to one or more core elements 7, 8, 9, 10 which, possibly, interconnect the two elements to wing 2. The core elements fixed to the wing element or elements 2 can be of various number, type and size to give the beam device different mechanical characteristics.

L’elemento ad ala 2 comprende un corpo 3 di forma prismatica allungata recante una nervatura centrale longitudinale e due nervature laterali longitudinali. The wing element 2 comprises an elongated prismatic body 3 bearing a longitudinal central rib and two longitudinal lateral ribs.

La nervatura centrale presenta una sede centrale e longitudinale 4; ciascuna nervatura laterale presenta una rispettiva sede laterale e longitudinale 5, 6. The central rib has a central and longitudinal seat 4; each lateral rib has a respective lateral and longitudinal seat 5, 6.

Tali sedi 4, 5, 6 sono previste per l’alloggiamento e fissaggio di uno o più elementi ad anima 7, 8, 9, 10 fissabili in esse tramite i mezzi d’incollaggio o, in alternativa od in aggiunta, tramite mezzi meccanici, ad esempio a vite, o mezzi di saldatura, quali punti o cordoni di saldatura. These seats 4, 5, 6 are provided for housing and fixing one or more core elements 7, 8, 9, 10 which can be fixed in them by means of gluing means or, alternatively or in addition, by mechanical means, for example screw, or welding means, such as points or weld seams.

Il corpo 3 dell’almeno un elemento ad ala 2 è pressoché piano e le sedi 4, 5, 6 longitudinali sono perpendicolari al piano geometrico definito da tale corpo 3. The body 3 of the at least one wing element 2 is almost flat and the longitudinal seats 4, 5, 6 are perpendicular to the geometric plane defined by this body 3.

Ciascun elemento ad anima 7, 8, 9, 10 è approssimativamente a forma di nastro piano o piastra allungata e, nella condizione di fissaggio nell’almeno una sede 4, 5, 6, è perpendicolare a detto corpo 3. Each core element 7, 8, 9, 10 is approximately in the shape of a flat ribbon or elongated plate and, in the condition of fixing in the at least one seat 4, 5, 6, is perpendicular to said body 3.

Ciascuna sede longitudinale centrale 4 dell’elemento ad ala 2 comprende una prima scanalatura 20 longitudinale, con sezione trasversale rettangolare, avente un rispettivo spessore e destinata ad ospitare un elemento ad anima spesso 8, avente il medesimo spessore o leggermente meno spesso, come illustrato in figura 3. Each central longitudinal seat 4 of the wing element 2 comprises a first longitudinal groove 20, with a rectangular cross section, having a respective thickness and intended to house a thick core element 8, having the same or slightly less thick thickness, as illustrated in figure 3.

Il fondo della prima scanalatura 20 longitudinale reca centralmente una seconda scanalatura 21 longitudinale, con sezione trasversale rettangolare, avente uno spessore minore di quello della prima scanalatura 20. The bottom of the first longitudinal groove 20 centrally bears a second longitudinal groove 21, with a rectangular cross-section, having a thickness less than that of the first groove 20.

Tale seconda scanalatura 21 longitudinale è destinata ad ospitare un elemento ad anima sottile 7 di corrispondente spessore, come illustrato, ad esempio, in figura 2. Il dispositivo 1 comprende inoltre due mezzi a spessore 22, 23 longitudinali, ciascuno avente spessore pressoché pari alla metà della differenza tra lo spessore della prima scanalatura 20 e lo spessore dell’elemento ad anima sottile 7. Detti mezzi a spessore 22, 23 sono destinati ad essere fissati, tramite resina epossidica o simili, nella prima scanalatura 20, ai lati dell’elemento ad anima sottile 7. This second longitudinal groove 21 is intended to house a thin core element 7 of corresponding thickness, as shown, for example, in Figure 2. The device 1 also comprises two longitudinal means 22, 23, each having a thickness almost equal to half the difference between the thickness of the first groove 20 and the thickness of the thin-core element 7. Said thickness means 22, 23 are intended to be fixed, by means of epoxy resin or the like, in the first groove 20, to the sides of the thin soul 7.

Il dispositivo comprende una pluralità di mezzi ad anima sottili 7 e spessi 8 aventi diverse larghezze per realizzare una pluralità di diverse travi, ciascuna con proprie specifiche meccaniche. The device comprises a plurality of thin 7 and thick 8 core means having different widths to make a plurality of different beams, each with its own mechanical specifications.

Le due sedi longitudinali laterali 5, 6 sono destinate al fissaggio di rispettivi elementi ad anima laterali 9, 10 come illustrato in figura 4. The two lateral longitudinal seats 5, 6 are intended for fixing respective lateral core elements 9, 10 as illustrated in figure 4.

gli elementi ad ala 2 e ad anima 7, 8, 9, 10 sono preferibilmente in alluminio o sue legne e sono preferibilmente verniciati, plastificati od anodizzati. the wing elements 2 and the core elements 7, 8, 9, 10 are preferably made of aluminum or its wood and are preferably painted, plasticized or anodized.

Le figure da 2 a 4 illustrano travi realizzate con due elementi ad ala 2 reciprocamente connessi tramite uno o più elementi ad anima 7, 8, 9, 10 realizzando travi di tipo IPE o di tipo scatolare. In alternativa le travi possono essere realizzate con un solo elemento ad ala 2 connesso ad uno o più elementi ad anima 7, 8, 9, 10 per ottenere travi a “T” od a “Π”. Figures 2 to 4 illustrate beams made with two wing elements 2 mutually connected by one or more core elements 7, 8, 9, 10, making beams of the IPE type or of the box-like type. Alternatively, the beams can be made with a single wing element 2 connected to one or more core elements 7, 8, 9, 10 to obtain “T” or “Π” beams.

L’operatività prevede che il trave sia realizzato tramite il reciproco fissaggio degli elementi, in quantità, tipo e dimensioni variabili, per raggiungere le caratteristiche meccaniche, ad esempio di resistenza a flessione ed a torsione, richiesti dalla specifica applicazione. The operation requires that the beam is made through the mutual fastening of the elements, in varying quantities, types and sizes, to achieve the mechanical characteristics, such as resistance to bending and torsion, required by the specific application.

Un vantaggio della presente invenzione è di fornire un dispositivo a trave modulare realizzabile con varie caratteristiche meccaniche a partire da un ridotto numero di elementi componibili per minimizzare i costi di produzione, gestione immagazzinamento e logistici in genere. An advantage of the present invention is to provide a modular beam device which can be manufactured with various mechanical characteristics starting from a reduced number of modular elements to minimize production, storage management and logistics costs in general.

Altro vantaggio è quello di fornire un dispositivo a trave modulare che sia utilizzabile anche come traversa orizzontale, montante verticale, elemento inclinato, etc. Another advantage is that of providing a modular beam device that can also be used as a horizontal crosspiece, vertical upright, inclined element, etc.

Ulteriore vantaggio è di fornire un dispositivo utilizzabile anche in vista. A further advantage is to provide a device that can also be used in sight.

Claims (10)

RIVENDICAZIONI 1) Dispositivo a trave modulare caratterizzato dal fatto di comprendere almeno un elemento ad ala (2) dotato di un corpo (3) di forma prismatica allungata recante almeno una sede (4, 5, 6) longitudinale per almeno un elemento ad anima (7, 8, 9, 10) fissabile in essa tramite mezzi d’incollaggio, mezzi di saldatura o mezzi meccanici. CLAIMS 1) Modular beam device characterized in that it comprises at least one wing element (2) equipped with an elongated prismatic body (3) bearing at least one longitudinal seat (4, 5, 6) for at least one core element (7 , 8, 9, 10) which can be fixed therein by means of gluing means, welding means or mechanical means. 2) Dispositivo secondo la rivendicazione 1 caratterizzato dal fatto che il corpo (3) dell’almeno un elemento ad ala (2) è pressoché piano e che la almeno una sede (4, 5, 6) longitudinale è perpendicolare al piano geometrico definito da tale corpo (3); l’almeno un elemento ad anima (7, 8, 9, 10), è approssimativamente a forma di nastro piano o piastra allungata e, nella condizione di fissaggio nell’almeno una sede (4, 5, 6), è perpendicolare a detto corpo (3). 2) Device according to claim 1 characterized in that the body (3) of the at least one wing element (2) is almost flat and that the at least one longitudinal seat (4, 5, 6) is perpendicular to the geometric plane defined by this body (3); the at least one core element (7, 8, 9, 10), is approximately in the shape of a flat ribbon or elongated plate and, in the condition of fastening in the at least one seat (4, 5, 6), is perpendicular to said body (3). 3) Dispositivo secondo la rivendicazione 2 caratterizzato dal fatto che ciascun elemento ad ala (2) comprende almeno una sede longitudinale centrale (4). 3) Device according to claim 2 characterized in that each wing element (2) comprises at least one central longitudinal seat (4). 4) Dispositivo secondo la rivendicazione 2 oppure la rivendicazione 3 caratterizzato dal fatto che ciascun elemento ad ala (2) comprende due sedi longitudinali laterali (5, 6). 4) Device according to claim 2 or claim 3 characterized in that each wing element (2) comprises two lateral longitudinal seats (5, 6). 5) Dispositivo secondo la rivendicazione 3 caratterizzato dal fatto che la sede longitudinale centrale (4) ha una prima scanalatura (20) longitudinale avente un rispettivo spessore e destinata ad ospitare un elemento ad anima spesso (8) di corrispondente spessore ed il cui fondo reca centralmente una seconda scanalatura (21) longitudinale avente uno spessore minore di quello della prima scanalatura (20) e destinata ad ospitare un elemento ad anima sottile (7) di corrispondente spessore, il dispositivo (1) comprendendo inoltre almeno due mezzi a spessore (22, 23) longitudinali, ciascuno avente spessore pressoché pari alla metà della differenza tra lo spessore della prima scanalatura (20) e lo spessore dell’elemento ad anima sottile (7); tali mezzi a spessore (22, 23) essendo destinati ad essere fissati nella prima scanalatura (20) ai lati dell’elemento ad anima sottile (7). 5) Device according to claim 3 characterized by the fact that the central longitudinal seat (4) has a first longitudinal groove (20) having a respective thickness and intended to house a thick core element (8) of corresponding thickness and whose bottom bears centrally a second longitudinal groove (21) having a thickness less than that of the first groove (20) and intended to house a thin core element (7) of corresponding thickness, the device (1) further comprising at least two thickness means (22 , 23) longitudinal, each having a thickness almost equal to half the difference between the thickness of the first groove (20) and the thickness of the thin core element (7); such thickness means (22, 23) being intended to be fixed in the first groove (20) on the sides of the thin core element (7). 6) Dispositivo secondo la rivendicazione 5 caratterizzato dal fatto di comprendere una pluralità di mezzi ad anima sottili (7) e spessi (8) aventi diverse larghezze. 6) Device according to claim 5 characterized in that it comprises a plurality of thin (7) and thick (8) core means having different widths. 7) Dispositivo secondo la rivendicazione 4 caratterizzato dal fatto che le due sedi longitudinali laterali (5, 6) sono destinate al fissaggio di rispettivi elementi ad anima laterali (9, 10). 7) Device according to claim 4 characterized by the fact that the two lateral longitudinal seats (5, 6) are intended for the fixing of respective lateral core elements (9, 10). 8) Dispositivo secondo una qualsiasi delle rivendicazioni precedenti caratterizzato dal fatto che gli elementi ad ala (2) e ad anima (7, 8, 9, 10) sono preferibilmente in alluminio o sue legne e sono preferibilmente verniciati, plastificati od anodizzati. 8) Device according to any one of the preceding claims, characterized by the fact that the wing elements (2) and the core elements (7, 8, 9, 10) are preferably made of aluminum or its woods and are preferably painted, plasticized or anodized. 9) Dispositivo secondo una qualsiasi delle rivendicazioni precedenti caratterizzato dal fatto di comprendere due elementi ad ala (2) reciprocamente connessi tramite uno o più elementi ad anima (7, 8, 9, 10). 9) Device according to any one of the preceding claims, characterized in that it comprises two wing elements (2) mutually connected by means of one or more core elements (7, 8, 9, 10). 10) Dispositivo secondo le rivendicazioni precedenti caratterizzato dal fatto che gli elementi ad anima (7, 8, 9, 10) sono fissati nelle rispettive sedi (4, 5, 6) longitudinali tramite mezzi d’incollaggio preferibilmente di tipo a resina epossidica.10) Device according to the previous claims characterized by the fact that the core elements (7, 8, 9, 10) are fixed in the respective longitudinal seats (4, 5, 6) by means of gluing preferably of the epoxy resin type.
IT000754A 2008-12-18 2008-12-18 MODULAR BEAM DEVICE ITBO20080754A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
IT000754A ITBO20080754A1 (en) 2008-12-18 2008-12-18 MODULAR BEAM DEVICE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT000754A ITBO20080754A1 (en) 2008-12-18 2008-12-18 MODULAR BEAM DEVICE

Publications (1)

Publication Number Publication Date
ITBO20080754A1 true ITBO20080754A1 (en) 2010-06-19

Family

ID=40848422

Family Applications (1)

Application Number Title Priority Date Filing Date
IT000754A ITBO20080754A1 (en) 2008-12-18 2008-12-18 MODULAR BEAM DEVICE

Country Status (1)

Country Link
IT (1) ITBO20080754A1 (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3960637A (en) * 1973-07-23 1976-06-01 Ostrow Paul F Composite structural member
DE9116436U1 (en) * 1991-10-24 1992-10-08 Kitz, Hans Josef, 5216 Niederkassel Construction of profile bars and truss profiles
DE19622759A1 (en) * 1995-12-14 1997-06-19 Niemeier Ralf Metal profile
WO1999014451A1 (en) * 1997-09-16 1999-03-25 Tube Technology Pty. Ltd. Hollow flange section
GB2420606A (en) * 2004-11-30 2006-05-31 Boeing Co Joint assembly with self locating feature
DE102005048243A1 (en) * 2005-10-07 2007-04-19 Thyssenkrupp Steel Ag Profile element and uses of such a profile element

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3960637A (en) * 1973-07-23 1976-06-01 Ostrow Paul F Composite structural member
DE9116436U1 (en) * 1991-10-24 1992-10-08 Kitz, Hans Josef, 5216 Niederkassel Construction of profile bars and truss profiles
DE19622759A1 (en) * 1995-12-14 1997-06-19 Niemeier Ralf Metal profile
WO1999014451A1 (en) * 1997-09-16 1999-03-25 Tube Technology Pty. Ltd. Hollow flange section
GB2420606A (en) * 2004-11-30 2006-05-31 Boeing Co Joint assembly with self locating feature
DE102005048243A1 (en) * 2005-10-07 2007-04-19 Thyssenkrupp Steel Ag Profile element and uses of such a profile element

Similar Documents

Publication Publication Date Title
CN204266376U (en) A kind of liftable floor
KR102188023B1 (en) Carbon curtain wall
ITMI20070060U1 (en) MODULAR SHIP FOR COVERS OF LARGE AREAS
PL2065541T3 (en) Metal fence
ITMI20082244A1 (en) FENDER FOR STEEL BOATS WITH PVC SOUL
ITBO20080754A1 (en) MODULAR BEAM DEVICE
US20140374197A1 (en) Frame for a car of a passenger/freight elevator, and such a car and passenger/freight elevator
WO2009092890A3 (en) Prefabricated modular dry-floor element, method of producing such a modular element and dry floor comprising a plurality of modular elements
USD825783S1 (en) Architecture member
JP5641456B2 (en) Building material connection structure
CN104364451A (en) Prefabricated wall frame for construction and ceiling frame using same
CN207211357U (en) A kind of house civil structure
CN105946988A (en) Novel four-door fire fighting truck cab top cover assembly
JP4425143B2 (en) Modular building unit and assembly method
JP6783038B2 (en) Building structure
JP5629195B2 (en) building
KR102620147B1 (en) Advanced type assembly pillar
JP5117794B2 (en) Building
CN207633581U (en) A kind of light girder steel rod structure of Combined thin-walled
ITRM970152A1 (en) METALLIC STRUCTURE FOR TEMPORARY ARCHITECTURE
WO2004113633A3 (en) House set for a frame-panel unit-built building
KR20160095871A (en) Movable resort structure
JP6128382B2 (en) Bearing wall
KR20200000602U (en) A ridge of roof for a greenhouse
CN201190401Y (en) Outer cover plate aluminium alloy sections for column of decorative steel structure curtain wall