EP0097659A1 - Structure tridimensionelle monolithique en metal deploye applicable notamment comme armature d'un panneau de construction immobiliere. - Google Patents
Structure tridimensionelle monolithique en metal deploye applicable notamment comme armature d'un panneau de construction immobiliere.Info
- Publication number
- EP0097659A1 EP0097659A1 EP83900042A EP83900042A EP0097659A1 EP 0097659 A1 EP0097659 A1 EP 0097659A1 EP 83900042 A EP83900042 A EP 83900042A EP 83900042 A EP83900042 A EP 83900042A EP 0097659 A1 EP0097659 A1 EP 0097659A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- legs
- members
- rank
- cutting
- frame
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C5/00—Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
- E04C5/01—Reinforcing elements of metal, e.g. with non-structural coatings
- E04C5/06—Reinforcing elements of metal, e.g. with non-structural coatings of high bending resistance, i.e. of essentially three-dimensional extent, e.g. lattice girders
- E04C5/0636—Three-dimensional reinforcing mats composed of reinforcing elements laying in two or more parallel planes and connected by separate reinforcing parts
Definitions
- the present invention relates to a panel and more specifically the internal metal frame which it comprises, intended for building construction.
- These panels are the backbone and the facing ia 5 construction and can then be used to make the * interior and exterior walls, floors, ceilings and roofs.
- the metal frame of these known panels is made up of two metal lattices parallel to one another and kept at constant separation by separate metal elements for bracing and joining by welding, stapling, hooking, binding, etc .; the lattices under consideration are constituted by sufficiently large metallic wires 15 and welded together in the form of meshes or else by wire mesh.
- the present invention aims to remedy this major drawback which prevents any exploitation of said panels economically.
- the frame of the panel is only a frame in "expanded metal" according to a three-dimensional structure having on the surface members * parallel to each other and at the heart of inclined legs connecting these members.
- the invention resides:
- connection nodes in that the legs connecting the members extend between them and separated from them by interrupted cutting lines defining the edges of said members, while the two ends of each member remain integral for one of a member of even rank and for the other of a member of odd rank, forming connection nodes, - and in that the distribution of the connection nodes when the metal is flat and not deployed is different from the distribution of these nodes in projection on this plane when the metal is' deployed in three-dimensional structure, by the fact that during deployment, the members of even rank must be moved parallel to themselves in an oblique direction so as not to away only the odd-numbered frames relative to the plane defined by the ribs of even rank, but also tilt • manner concomitant jambs.
- each node of a member of an even rank couples the neighboring ends of two legs, extending respectively on both sides of the member considered and in the same direction, the directions reversing for the legs of the two consecutive members of even rank; each knot of a member of odd rank couples the ends. adjacent to two legs and extending respectively on both sides of the member considered and in opposite directions, the directions being reversed for the homologous legs of two consecutive members of odd rank.
- the connecting joints are arranged on the plane metal not of éployé, -according lines perpendicular to the ribs and during deployment, if les.noeuds of odd-numbered frames are immobilized longitudinally LEMENT , on the other hand the nodes of each member of even rank are moved longidutinally sometimes in one direction, for a member of even rank considered, and sometimes in the opposite direction, for the two members of even rank consecutive thereto, so that the legs incline opposing for two consecutive frames of even rank.
- each coupling node is formed by the part of the corresponding member- on which end the two legs which are coupled to it, this part being included between the four contiguous points of interruption of the two lines of interrupted cutting of this member, two opposite points in diagonal being connected by cutting bias to the edges of d- cutting of the jambs located on either side of the frame considered.
- each panel thus being formed, at the time of their installation in extension of each other and in contact by their extreme edges defined by the end members even on one side and odd on the opposite side, the members of each panel cooperate with bars regularly spaced transverse ends whose ends are fixed, in particular by force hooking, on the frames of the two adjoining panels.
- FIG. 1 is a partial plan view showing a first embodiment of the metal not deployed but precut according to the invention.
- Figure 2 is a plan view similar to Figure 1 showing the start of deployment and to distinguish the various components of the frame or frame of the panels of the invention.
- FIG. 3 is a partial perspective illustrating this framework or reinforcement deployed from the precut metal according to FIGS. 1 and 2.
- FIG. 4 is a partial section taken on the line IV-IV of FIG. 3,
- FIG. 5 is a partial plan view elementary similar to Figure 1, but showing on a larger scale two successive nodes of the metal before deployment.
- FIG. 6 is a partial elementary perspective similar to FIG. 3, but showing in another orientation the two extreme nodes of the same jamb linked to two members,
- FIG. 7 and 8 are views similar to Figures 1 and 3 respectively and illustrating a second embodiment of the frame or reinforcement of the panels of the invention, the metal being for Figure 7, pre-cut and not deployed , for Figure 8, deployed in three-dimensional structure
- - Figures 9 to 12 are views similar to Figures 1, 2, 3 and 5 respectively, 'relating to a third embodiment, the metal being for Figure 9, precut and not deployed, for FIG. 10, in primed deployment, for FIG. 11, deployed in three-dimensional structure ” and for FIG. 12, shown diagrammatically flat for five successive nodes,
- FIG. 13 is a view similar to Figure 4 showing the assembly of several panels together to form a wall
- - Figure 14 is an elevation taken along arrow F of Figure 13.
- the panel of the invention comprises a frame 1 of expanded metal, a layer 2 of filling material, such as synthetic foam and surface coverings 3, 4 in mortar, plaster or other. Layer 2 is trapped at the heart of reinforcement 1 and coats the components of
- the metal sheet 5 ( Figures 1, -2.and 5 or 7) intended for the manufacture of the frame 1 is preferably made of steel and it is precut to generate, during its deployment, the three-dimensional structure of reinforcement 1 shown in Figure 3 or Figure 8 or 11.
- the sheet 3 has members parallel to each other and spaced from each other; these members are designated by the general reference 6 and are distinguished from each other by an index; it is important to note right now that the odd rank members 6.1, 6.3, 6.5, 6.7 ..., 6.2n + l are intended to define one of the faces of the reinforcement, while the members of even rank 6.2 , 6.4, 6.6., .. 6.2n are intended to define the opposite face of said frame. .
- the frames 6 are separated from each other, whatever their rank, * by solid parts of the sheet 5 intended to constitute jambs ; between the consecutive members 6.1 and 6.2, 6.3 and 6.4, 6.5 and 6.6 ..., the legs 7 extend one; the other and in the same way, between the members 6.2 and 6.3, 6.4 and 6.5, 6.6 and 6.7 ..., the legs 8 also extend one, the other.
- the legs 7 and 8 associated with the same frame 6 are paired two by two in the sense that the neighboring ends of the same set of legs 7 and 8 are made integral with each other and with the corresponding frame to form a connecting node 9 ;
- each frame is defined by two cutting lines interrupted 10. 11, the interruptions of which allow solid parts to remain which precisely constitute the aforementioned link nodes.
- said cutting lines 10 and 11 allow the members 6 to be separated from the legs 7 and 8; so that the separation of these is complete outside the nodes 9, cutting bias 12 and 13 connect, without destroying the nodes considered * , the cutting line 10 of a member to the cutting line 11 of the member neighbor ; in addition, it is also interesting to note that each of the cutting biases 12 and 13 separates a node 9.2n of even rank. from a node 9.2n + 1 of odd rank; at the same time, the cutting bias 12 separates the legs 7 from each other so that during deployment, these legs tilt in one direction, while the cutting bias
- FIG. 5 illustrates the breakdown in detail and therefore makes it possible to specify the connections between the constituent elements of the framework. So the interrupted cutting line 10 of member 6.2 ends, with respect to node 9.2, at two interrupting points 14, 15 and in the same way, interrupted cutting line 11 of this member 6.2 ends, for node 9.2 / at two breakpoints 16, 17 * . The same points 14 to 17 are found for the node 9.3 homologous to the previous 9.2 and aligned with the latter on an oblique line 18 having with respect to the members 6 a slope a_ defined in what follows. Points 14 and 17 of each node are diagonally opposite.
- point 14 of node 9.2 is linked to point 17 of node 9.1 which prefers it, by a cutting bias 12 separating two legs 7 from one another and, similarly, point 17 of this node 9.2 is linked to point 14 of node 9.3 which follows it. by a cutting bias 13 separating two legs 8 from one another.
- each node is also diagonally opposite. ; they mark the end of the separation of the jambs relative to the members.
- the cutting of the sheet 5 being thus achieved, it is clear that the members 6 are separated from each other over most of their length but that they are however connected to each other by legs 7 and 8 leading to connecting nodes 9, the legs 7 being directed in the direction opposite to that of the legs 8.
- the members of odd rank 6.2n + 1 deviate from the above-mentioned reference plane to define another plane parallel to it, the two planes considered being in fact those of the faces of the reinforcement 1; at the same time as these members of odd rank move apart (as well from the reference plane / as from projection on this reference plane. members • of even rank) the legs tilt.
- the slope has oblique lines 18 of the homologous nodes 9 with respect to the members 6 is established in relation to the loss of length in projection on a member of the legs when they tilt in the space; with such a slope, the homologous nodes are aligned perpendicular to the members when the metal is deployed as can be seen from FIG. 3.
- the homologous nodes 9 of the sheet 5 can be aligned on lines perpendicular to the members 6; in this case, it is obvious then that, when the metal is deployed in three-dimensional structure, said homologous nodes are located on oblique lines whose slope depends as before on the loss of length in projection on a frame of the legs when they bow.
- Figures 7 and 8 show a second embodiment of the three-dimensional structure which can be produced to form the frame 1 of the panel.
- this second form of realization it is a question of multiplying the number of jambs in order to increase the density of the latter between the frames and / or to increase the thickness of the reinforcement obtained by deployment.
- each solid part is separated by means of cutting into legs 5 aligned with each other and each adjoining the two contiguous members
- each solid part is divided, in the manner described below, in legs which g not only extend one another over a part of their length, but also extend side by side over another part of their length. between said contiguous members.
- each solid part separating two contiguous members is delimited by the abovementioned interrupted cutting lines 10 and 11 - moreover, another interrupted cutting line 19 extends between the two preceding ones.
- the connecting nodes 37 (of the frame 33 with the frame 6.1 ) and 37 (of the leg 34 with the same frame 6.1) are delimited by the points of interruption 26 of the line 11 as well as by the cutting bias 21; in a similar manner, the connecting nodes 39 (of the leg 33 with the.
- Figures 9 to 12 illustrate a third embodiment of the onolithic and three-dimensional frame 1.
- the members 6 are separated from each other by solid parts of the sheet 5 intended to constitute the legs 57, 58, 67 and 68 terminating on connecting nodes 59, 69, 79 and 89 of the members 6.1, 6.5, .. 6.4n + 1; 6.3, 6.7 ... 6. 4n + 3; 6.4, 6.8 ... 6.4n; 6.2, 6.6 .. ' . 6.4n + 2 respectively.
- the legs 57 extend above and to the right, while the legs 58 extend below and to the left, a leg 57 being combined with a leg 58 to lead to a node 59 of a member of odd rank 6.4n + l, such as member 5.5; the legs 67 extend above and to the left, while the legs 68 extend below and to the right, a leg 67 being combined with a leg 68 to terminate on a knot 69 of an em- bridle of odd rank 6.4n + 3, such as chord 6.3; the frames of odd rank 6.2n + l being alternately provided with nodes 59 with legs 57, 58 and nodes 69 with legs 67, 68.
- nodes 79 (6.4n members such as member 6.4) on which converge from the left upper 68 and lower legs 67.
- - of nodes 89 (members 6.4n + 2 such as member 6.2) on which converge from the right upper legs 58 and lower legs 67.
- each member 6 is delimited by
- each node 59.4n + 1 is delimited by cutting biases 52 and 53
- each node 69.4n + 3 is delimited by cutting biases 54 and 55, each node 79.
- n is delimited by cutting biases 52 and 55 common to neighboring nodes 59 and 69
- each node 89.4n + 2 is delimited by cutting biases 53 and 54 common to neighboring nodes 59 and 69.
- These cutting biases are oriented and distributed in a very particular way analyzed in this which follows with reference to FIG. 12.
- the metal sheet 5 is divided into narrow strips by the cutting lines 50 and 51 which are interrupted at points 50a_, 50b and respectively 51a, 51b aligned on fictitious lines 61a, 61b , these being perpendicular to the cutting lines 50, 51 and spaced apart in correspondence with the chosen size of the nodes (left half of FIG. 4).
- Four neighboring points 50a., 50b, 5la ⁇ and 5lb could be connected by fictitious diagonals 62 and 63.
- the aforementioned bands successively constitute the frame 6.1, the legs 58, the frame 6.2, the legs 67, the frame 6.3, the frames 68, the frame 6.4, the legs 57, the member 6.5, the legs 58, the member 6.6 and so on.
- the cutting bias 52 and 53 are parallel to the diagonal 69
- the cutting bias 54 and 55 are parallel to the conjugate diagonal 63; these biases are distributed so as to be successively parallel to each other by two and diverging from one another by two.
- - node 69 is defined by two parallel biases 54 and 55 tilting from left upwards to right downwards to connect legs 67 and 68 to frame 6.3 beyond the breakpoints 50a and 5lb of the cutting lines 50 and 51 which separate this frame 6.3 from said legs 67 and 68 extending on either side in extension,
- the node 79 is defined by two biases 55 and 52 converging to the right on the frame 6.4 and diverging to the left on two legs 68 and 57 framing this frame which is separated by the lines 50 and 51 to the points 50a_ and 51a.
- the node 59 is defined by two parallel biases 52 and 53 tilting from left to bottom to the right at the top to connect the legs 58 and 57 to the frame ' 6.5 beyond the points of interruption 51a * and 50b of cutting lines. 51 and 50 which separate this frame 6.5 from said legs 58 and 57 extending on either side in extension.
- transverse bars 42 are placed at different regularly spaced levels. These bars are nothing special except that hooks 43 and 44 are formed by the ends of each. The forming of the hooks is effected by force and is intended to join the extreme member of a panel with the extreme member adjacent to the adjoining panel; thus, a real crossover of all the panels is obtained and at the same time ensures the intense connection of the extreme members which are close to the edges in contact with said panels.
- the material constituting the coverings 3 and 4 is then sprayed continuously and there is then no continuous solution.
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Revetment (AREA)
- Body Structure For Vehicles (AREA)
- Rod-Shaped Construction Members (AREA)
- Laminated Bodies (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT83900042T ATE27023T1 (de) | 1981-12-17 | 1982-12-17 | Dreidimensionale monolithische aus gestrecktem metall bestehende struktur, insbesondere als bewehrung einer bauplatte. |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8123618 | 1981-12-17 | ||
FR8123618A FR2518611B1 (fr) | 1981-12-17 | 1981-12-17 | Panneau prefabrique pour constructions immobilieres |
FR8214293A FR2531989B2 (fr) | 1982-08-18 | 1982-08-18 | Panneau prefabrique pour constructions immobilieres |
FR8214293 | 1982-08-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0097659A1 true EP0097659A1 (fr) | 1984-01-11 |
EP0097659B1 EP0097659B1 (fr) | 1987-05-06 |
Family
ID=26222671
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP83900042A Expired EP0097659B1 (fr) | 1981-12-17 | 1982-12-17 | Structure tridimensionelle monolithique en metal deploye applicable notamment comme armature d'un panneau de construction immobiliere |
Country Status (7)
Country | Link |
---|---|
US (1) | US4559752A (fr) |
EP (1) | EP0097659B1 (fr) |
JP (1) | JPS58502102A (fr) |
BR (1) | BR8208022A (fr) |
DE (1) | DE3276248D1 (fr) |
OA (1) | OA07523A (fr) |
WO (1) | WO1983002129A1 (fr) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2644494A1 (fr) * | 1989-03-14 | 1990-09-21 | Prodecid | Element structural en materiau composite, utilisable notamment a la realisation de couvertures ou de bardages d'edifices |
FR2708969B1 (fr) * | 1993-08-13 | 1995-11-03 | Vicat | Procédé de réalisation d'ouvrages de génie civil et ouvrage obtenu. |
CH690188A5 (de) * | 1994-05-04 | 2000-05-31 | Walter Zeller | Armierungsgitter für Mauerwerkfugen. |
GB2299112B (en) * | 1995-03-23 | 1999-04-21 | Rom Limited | Improvements in and relating to tunnel linings |
US5826539A (en) * | 1996-07-12 | 1998-10-27 | Bloedorn; Dan A. | Expanded mesh bird feeder |
US6226942B1 (en) | 1999-02-09 | 2001-05-08 | Pete J. Bonin | Building construction panels and method thereof |
US6370835B1 (en) | 1999-06-15 | 2002-04-16 | Robust Building Systems, Inc. | Method and apparatus for low cost housing construction |
DE10259307A1 (de) * | 2002-12-18 | 2004-07-08 | Protektorwerk Florenz Maisch Gmbh & Co Kg | Flächiges Metallelement und Profilelement |
US8365489B1 (en) | 2003-03-07 | 2013-02-05 | Bond Building Systems, Inc. | Building system and method of constructing a multi-walled structure |
US8006451B2 (en) * | 2003-03-07 | 2011-08-30 | Art Bond | Building system and method of constructing a multi-walled structure |
US7803466B2 (en) * | 2006-04-07 | 2010-09-28 | Dorsy Sean C | Expandable panel structures and methods of manufacturing the same |
US7803467B2 (en) * | 2006-04-07 | 2010-09-28 | Dorsy Sean C | Multi-tiered, expandable panel structures and methods of manufacturing the same |
US20090031661A1 (en) * | 2007-07-30 | 2009-02-05 | Khatchik Chris Khatchikian | Panels and a method of making |
ITNO20130004A1 (it) * | 2013-06-03 | 2014-12-04 | Mauro Sica | Sistema di pre-distanziamento collassabile particolarmente per gli elementi di un telaio strutturale |
US8904724B1 (en) * | 2013-12-20 | 2014-12-09 | Highland Technologies, LLC | Durable wall construction |
US8733047B1 (en) | 2013-12-20 | 2014-05-27 | Highland Technologies, LLC | Durable wall construction |
US8733048B1 (en) | 2013-12-20 | 2014-05-27 | Highland Technologies, LLC | Multi-story durable wall construction |
US9708816B2 (en) | 2014-05-30 | 2017-07-18 | Sacks Industrial Corporation | Stucco lath and method of manufacture |
US9752323B2 (en) | 2015-07-29 | 2017-09-05 | Sacks Industrial Corporation | Light-weight metal stud and method of manufacture |
US9797142B1 (en) | 2016-09-09 | 2017-10-24 | Sacks Industrial Corporation | Lath device, assembly and method |
JP7055465B2 (ja) | 2017-08-14 | 2022-04-18 | ストラクタ ワイヤー ユーエルシー | 可変長金属スタッド |
US11351593B2 (en) | 2018-09-14 | 2022-06-07 | Structa Wire Ulc | Expanded metal formed using rotary blades and rotary blades to form such |
US11352786B2 (en) * | 2019-08-19 | 2022-06-07 | WSP USA, Inc. | Constructing buildings with modular wall structure |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB114059A (en) * | 1917-04-18 | 1918-03-21 | Arthur Benham | Improvements in or relating to Reinforced Concrete. |
FR493868A (fr) * | 1917-12-13 | 1919-08-23 | Andrew Miller | Perfectionnement apporté au métal déployé ou s'y rattachant |
US3111204A (en) * | 1959-08-24 | 1963-11-19 | British Uralite Ltd | Structural element and a method of making a structural element |
US3111024A (en) * | 1960-08-11 | 1963-11-19 | Emmett F Sarver | Gas detecting apparatus |
US3825465A (en) * | 1972-03-24 | 1974-07-23 | R Stock | Three dimensional reticulated structure |
US3872636A (en) * | 1973-05-07 | 1975-03-25 | Pacenti Robert A | Light weight load bearing metal structural panel |
FR2265538A1 (en) * | 1974-03-27 | 1975-10-24 | Metal Deploye | Composite panels with metallic cores suitable for heating elements - readily fabricated for cladding and heating large structures |
LU77320A1 (fr) * | 1976-05-14 | 1977-08-24 | ||
US4336676A (en) * | 1977-12-05 | 1982-06-29 | Covington Brothers, Inc. | Composite structural panel with offset core |
DE2849520A1 (de) * | 1978-11-15 | 1980-05-29 | Fricker Frimeda Metall Draht | Verbindungsanker fuer eine mehrschichtenbauplatte |
-
1982
- 1982-12-17 EP EP83900042A patent/EP0097659B1/fr not_active Expired
- 1982-12-17 WO PCT/FR1982/000214 patent/WO1983002129A1/fr active IP Right Grant
- 1982-12-17 DE DE8383900042T patent/DE3276248D1/de not_active Expired
- 1982-12-17 BR BR8208022A patent/BR8208022A/pt not_active IP Right Cessation
- 1982-12-17 JP JP83500095A patent/JPS58502102A/ja active Pending
- 1982-12-17 US US06/530,593 patent/US4559752A/en not_active Expired - Lifetime
-
1983
- 1983-08-17 OA OA58090A patent/OA07523A/fr unknown
Non-Patent Citations (1)
Title |
---|
See references of WO8302129A1 * |
Also Published As
Publication number | Publication date |
---|---|
DE3276248D1 (en) | 1987-06-11 |
OA07523A (fr) | 1985-03-31 |
JPS58502102A (ja) | 1983-12-08 |
BR8208022A (pt) | 1983-11-08 |
WO1983002129A1 (fr) | 1983-06-23 |
EP0097659B1 (fr) | 1987-05-06 |
US4559752A (en) | 1985-12-24 |
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