ITBO20080754A1 - MODULAR BEAM DEVICE - Google Patents
MODULAR BEAM DEVICE Download PDFInfo
- 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
Links
- 238000004026 adhesive bonding Methods 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 claims description 3
- 229920000647 polyepoxide Polymers 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 238000009435 building construction Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C3/06—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal with substantially solid, i.e. unapertured, web
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0408—Joists; 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
- E04C2003/0413—Joists; 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0408—Joists; 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
- E04C2003/0413—Joists; 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
- E04C2003/0417—Joists; 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0426—Joists; 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
- E04C2003/043—Joists; 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0426—Joists; 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
- E04C2003/0434—Joists; 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0443—Joists; 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
- E04C2003/0452—H- or I-shaped
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0443—Joists; 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
- E04C2003/0465—Joists; 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)
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 |
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IT (1) | ITBO20080754A1 (en) |
Citations (6)
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 |
-
2008
- 2008-12-18 IT IT000754A patent/ITBO20080754A1/en unknown
Patent Citations (6)
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 |
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