EP1779940A1 - Verfahren zum Hertsellen von metallischen geflechteten Strukturen sowie durch das Verfahren hergestellte Strukture - Google Patents

Verfahren zum Hertsellen von metallischen geflechteten Strukturen sowie durch das Verfahren hergestellte Strukture Download PDF

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Publication number
EP1779940A1
EP1779940A1 EP06301079A EP06301079A EP1779940A1 EP 1779940 A1 EP1779940 A1 EP 1779940A1 EP 06301079 A EP06301079 A EP 06301079A EP 06301079 A EP06301079 A EP 06301079A EP 1779940 A1 EP1779940 A1 EP 1779940A1
Authority
EP
European Patent Office
Prior art keywords
plate
strips
longitudinal
braided metal
plane
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
Application number
EP06301079A
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English (en)
French (fr)
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EP1779940B1 (de
Inventor
Gilbert Primet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Primet Ets
Original Assignee
Primet Ets
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Filing date
Publication date
Application filed by Primet Ets filed Critical Primet Ets
Publication of EP1779940A1 publication Critical patent/EP1779940A1/de
Application granted granted Critical
Publication of EP1779940B1 publication Critical patent/EP1779940B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D47/00—Making rigid structural elements or units, e.g. honeycomb structures
    • B21D47/005—Making gratings
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/08—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of metal, e.g. sheet metal

Definitions

  • the invention relates to the technical sector of metal braiding and, in particular, braided metal products.
  • These products may be, for example, plates, trays, panels, chairs, furniture.
  • FIGS. 1 and 2 show the implementation of the configuration of a braided grid. Beams of the metal strips (A - B) are alternately arranged, over and under, in perpendicular planes thereby providing an alternative overlap of the transverse strips with respect to the longitudinal strips.
  • the implementation of this method allows to obtain various forms of cutting and braiding, in visual aspects of different axial planes and in the context of a continuous manufacturing automation.
  • FIG. 6 shows an example of a plate (10) to be worked according to the invention.
  • This sheet metal plate is solid in dimensional characteristics established from manufacturing production considerations and mesh to achieve.
  • the plate is arranged with the formation of a plurality of holes (10a) according to a pre-established grid, these holes being of square, rectangular or other configuration, obtained using appropriate punches. whose profiles are complementary. The positioning of the holes and their shape are chosen according to the final appearance to be obtained from the braided plate.
  • the next step is to define strips to be shaped, from the dimensions, width and length of the plate to be worked and to proceed to the successive operations of stamping half-flesh, on the one hand for all bundles strips (C) located along the same longitudinal axis, and step by step with the desired offset.
  • the width of the bands worked, and thus shaped, depends on the shape of the mesh.
  • Mid-body stamping operations are done using a numerically controlled machine capable of performing the aforementioned operations.
  • the operation After executing a first line in a longitudinal plane, the operation continues with an axial offset, parallel to the first line (L1 - L2 ... LN), to form the entire useful surface of the plate in the longitudinal direction. Then the forming tools are rotated at 90 ° to make, by pressing halfway, complementary operations in the oblique direction, for example, transverse, line by line (La, Lb, Ln), to obtain a braiding complete along the axes (XX - YY) of the worked metal plate.
  • the numerically controlled machine executes the successive operations in a very short time after programming.
  • the braided metal plate according to the method of the invention, remains monoblock without interstice since there is no longer crossing zone and overlap bands.
  • the visual aspect of the finished product gives the braided appearance. Referring to FIG. 3, each of the faces of the braided plate has a mid-flesh stamping appearance.
  • the method, object of the invention finds multiple applications and, by way of example, not limited to, those cited relating to braided metal structures for furnishing, making furniture, displays, panels, and a way for any product having a substantially flat face to form support planes or sitting or decoration.
  • the resulting product can remain flat or be shaped by bending or otherwise. Depending on the applications, it can be framed.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Mechanical Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Wire Processing (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Metal Extraction Processes (AREA)
EP06301079A 2005-10-27 2006-10-23 Verfahren zum herstellen von metallischen geflechteten Strukturen sowie durch das Verfahren hergestellte Strukture Not-in-force EP1779940B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0553264A FR2892649B1 (fr) 2005-10-27 2005-10-27 Procede de fabrication de structures en metal tresse et les produits obtenus selon le procede

Publications (2)

Publication Number Publication Date
EP1779940A1 true EP1779940A1 (de) 2007-05-02
EP1779940B1 EP1779940B1 (de) 2008-01-02

Family

ID=36933428

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06301079A Not-in-force EP1779940B1 (de) 2005-10-27 2006-10-23 Verfahren zum herstellen von metallischen geflechteten Strukturen sowie durch das Verfahren hergestellte Strukture

Country Status (4)

Country Link
EP (1) EP1779940B1 (de)
AT (1) ATE382443T1 (de)
DE (1) DE602006000398D1 (de)
FR (1) FR2892649B1 (de)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR893207A (fr) * 1942-12-21 1944-06-02 Nouveau procédé de fabrication de grillage métallique et produit en résultant
DE4142260A1 (de) * 1991-12-20 1993-07-01 Sorst Ernst & Co Bauelement und vorrichtung zu dessen herstellung
EP0918581B1 (de) * 1996-08-10 2000-06-14 Federal-Mogul Technology Limited Hitzeschild
EP1457617A1 (de) * 2003-03-13 2004-09-15 Royal Packaging Industry van Leer N.V. Eine Verbindungsanordnung für eine Gitterstruktur

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR893207A (fr) * 1942-12-21 1944-06-02 Nouveau procédé de fabrication de grillage métallique et produit en résultant
DE4142260A1 (de) * 1991-12-20 1993-07-01 Sorst Ernst & Co Bauelement und vorrichtung zu dessen herstellung
EP0918581B1 (de) * 1996-08-10 2000-06-14 Federal-Mogul Technology Limited Hitzeschild
EP1457617A1 (de) * 2003-03-13 2004-09-15 Royal Packaging Industry van Leer N.V. Eine Verbindungsanordnung für eine Gitterstruktur

Also Published As

Publication number Publication date
FR2892649A1 (fr) 2007-05-04
EP1779940B1 (de) 2008-01-02
DE602006000398D1 (de) 2008-02-14
FR2892649B1 (fr) 2008-01-18
ATE382443T1 (de) 2008-01-15

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