EP1192016B1 - Method for assembling at least two component metal elements for producing a structure - Google Patents

Method for assembling at least two component metal elements for producing a structure Download PDF

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Publication number
EP1192016B1
EP1192016B1 EP00945472A EP00945472A EP1192016B1 EP 1192016 B1 EP1192016 B1 EP 1192016B1 EP 00945472 A EP00945472 A EP 00945472A EP 00945472 A EP00945472 A EP 00945472A EP 1192016 B1 EP1192016 B1 EP 1192016B1
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EP
European Patent Office
Prior art keywords
parts
hem
section
metal
assembly process
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.)
Expired - Lifetime
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EP00945472A
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German (de)
French (fr)
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EP1192016A1 (en
Inventor
Richard Kergen
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ArcelorMittal Liege Upstream SA
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Cockerill Sambre SA
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Priority to EP00945472A priority Critical patent/EP1192016B1/en
Publication of EP1192016A1 publication Critical patent/EP1192016A1/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D39/00Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
    • B21D39/02Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of sheet metal by folding, e.g. connecting edges of a sheet to form a cylinder
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49936Surface interlocking
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49938Radially expanding part in cavity, aperture, or hollow body
    • Y10T29/49941Peripheral edge joining of abutting plates
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/49Member deformed in situ
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/49Member deformed in situ
    • Y10T403/4966Deformation occurs simultaneously with assembly
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/49Member deformed in situ
    • Y10T403/4991Both members deformed

Definitions

  • the present invention relates to a method of assembling at least two metallic elements in order to create a structure, at least one of the two elements with a very high yield strength and its application to realize (beam) structures of complex form from simple elements, not requiring no significant deformations.
  • the objective is to significantly reduce the weight of structures by using as little metal as possible.
  • These structures, the chassis of motor vehicle for example are obtained by often complex parts assembled by stamping.
  • steels In order to reduce the thickness of the metal used to build these structures while retaining their mechanical properties, steels must be used with high mechanical characteristics. of the grades of low alloy carbon steels with high mechanical characteristics, but often associated to a capacity for shaping by deformation very limited, are available today.
  • the steels affected by this patent application have a yield strength located between 400 and 1500 MPa. These steels are produced by mass steel processes known per se, which allow to offer steels whose cost price is close to that of conventional carbon steels. The interest then lies in the fact that one can obtain significant reduction in structure. However, due to their low formatting capacity and sometimes poor weldability, these steels pose specific implementation problems, and in particular assembly.
  • the elements constitutive of the same structure often have complex shapes obtained by stamping processes involving significant deformations and therefore incompatible with poor formatting capabilities of these steels.
  • Document US-A-3 854 185 proposes, in the same area of application, a process for forming a joint structural between two rigid elements, one presenting on one side a flange with one projecting end and the other an essentially circular groove.
  • the flange enters the throat while deforming. More precisely, the assembly is done by joining of the flange with the groove, the flange forming a winding in said throat.
  • Document DE-C-385 642 proposes a machine for the assembly by crimping of two sheet metal elements to form a hollow body.
  • Document FR-A-2 321 962 proposes a process assembly by crimping a zinc element and a lead element to solve problems in the field of building cover.
  • the present invention aims to provide a method of assembling at least two metallic elements or component parts of which at least one of the two is made of steel with a very high limit of elasticity associated with a weak capacity of setting shape in order to make shaped structural parts complex, from simpler parts achievable at using formatting operations basically of folding type, not involving significant deformations in the plane of the sheet, and therefore compatible with steels with high mechanical characteristics.
  • At least one of the elements is made of preferably in steel with yield strength greater than 400 MPa or in an aluminum alloy with a yield strength greater than 200 MPa.
  • the ratio of the radius of the hem to the sum of the thicknesses of the different elements that we want to assemble along the junction section is between 2 and 10.
  • the ratio of the difference between the radius of hem and outermost metal thickness with the innermost metal thickness is, advantageously greater than 2.
  • the process is also characterized by the fact that the junction is not necessarily straight but may have local curvature, the radius of curvature preferably being greater than five radii hem exteriors.
  • the assembly method according to the invention is further characterized by the fact that after the operation of hem crimping, blocking said hem vis-à-vis the sliding of its elements along the section of junction, is obtained by gluing, indentation or nesting.
  • the present invention also relates to the product obtained by the assembly process described above, which is defined in claim 9.
  • the product is in the form of a double-core "I" beam, obtained by assembling four components connected by four hems the along the junction section of the four elements taken two by two.
  • the product results from the assembly of two elements by two hems so as to form a section closed, at least one of the two elements having a "U" section.
  • the process of the invention therefore allows to obtain structural parts of complex shape to from sheet metal materials presenting, on the one hand, a high to very high elastic limit, and on the other hand, a limited forming capacity. This last is not binding at the level of operations preparatory to the assembly process, such as the folding, involving little deformation in the plane of the sheet. This process thus makes it possible to obtain pieces of geometry equivalent to that obtained by stamping.
  • hem assembly is compatible with low formability of these steels, the working radius being several times the thickness, which is not the case for Simple crimping for example.
  • Another advantage of the invention lies in the fact that the assembly process or crimping by purely mechanical hem allows you to get rid of possible weldability problems of high steels mechanical characteristics.
  • An additional advantage of the invention is to propose a process for the production of pieces of reinforced structure, especially in industry automobile.
  • Figures 1 describe a structure carried out in a conventional manner having a geometry in "U”.
  • Figures 2 show the elements simple constituents in order to create the same kind of structure as that shown in FIGS. 1 according to the assembly method of the present invention.
  • Figures 3 show a tool allowing the realization of a structure as described in Figure 2.
  • Figure 4 shows variants assembly orientation for a U-shaped structure.
  • Figures 5 show a shape more complex execution of a structure with a closed section obtained by the assembly process of the present invention.
  • Figure 6 shows the tool used to make a closed structure as shown in Figures 5.
  • Figure 7 shows another form execution of a structure having the form of a double-core "I" beam.
  • Figure 8 shows the tool for realization and assembly of an "I" beam with core double.
  • FIG. 9 represents a part of the type shield crosspiece.
  • FIG. 10 represents a part of the type middle foot.
  • Figure 11 represents a part presenting tabs at the ends to facilitate assembly.
  • Figures 12 illustrate the principle of blocking of the relative sliding of the core with respect to the sole in hem assembly, by interlocking using a cut of alternating slots.
  • Figures 12a and 12b present the two sheets just before production hem.
  • the idea behind the invention is to decompose a structure element of complex shape, usually achieved by shaping operations by stamping not very compatible with high steels mechanical characteristics, in simple sub-elements, performed using folding type forming operations, and hemmed together.
  • Figure 1 shows the usual mode of production of a "U" shaped part. classically this type of part is obtained by stamping from a flat sheet as shown schematically in Figure la. As part steels with very high yield strength, stamping of such a room poses severe problems of control of the elastic return: the shape obtained deviates appreciably of the ideal shape as shown in Figure 1b. of the critical problems due to low formability of this type occur, for example when the height of the "U” section varies significantly as shown in figure 1c or when the height of the section remains constant, the curvature of the "U” beam varies locally so sensitive (Figure 1d).
  • Parts 1, 2 and 3 can be obtained by folding or lifting the edge. These bet techniques in shape only involve small deformations in the sheet plane and are compatible with steels with very high yield strength with low capacity forming.
  • Figure 3 shows a typical tool allowing the realization of this type of part using of a press.
  • the side elements 1 or 2 and the bottom 3 are prepared for hemming as shown in 5. These parts produced using press operations are presented in the tool described in Figure 3.
  • the left half-view shows the closed tool, before the hem
  • the right half view presents the tool when the hem is finished.
  • Elements 7, 7 'and 9 are supported on the upper slide of the press by means of springs not shown and whose crushing stroke is greater than the stroke of tools 8, 8 'forming the hem.
  • the springs are compressed and press, by through parts 7 and 9, parts 1, 2 and 3 against part 10 which follows their shape and rests on the press table.
  • the press slide ends its course the element 8 'which is directly to it bound forms the hem as shown on the right side of Figure 3.
  • Parts 1, 2 and 3 are not necessarily all high-limit steel elasticity: for example, depending on the function of the part, only part 3 can be made of very high limit steel of elasticity, steel parts 1 and 2 having a better formability and better weldability, making it easy to assemble the part to the rest of the structure with assembly processes such as spot welding.
  • the process allows also to adapt thicknesses to requirements structural parts: the three parts 1, 2 and 3 may have different thicknesses, the process hem assembly accepting thicknesses significantly different, with a ratio greater than of them.
  • the method also makes it possible to carry out closed sections as shown in Figure 5.
  • the part 11 can be obtained by simple folding, a variation of the closed section being obtained by varying the height of the folded edges. Exhibit 12 which closes the section is even simpler in shape.
  • the part 11 can also be produced by deep drawing of steel with lower yield strength, less than 400 MPa for example, part 12 being in very high yield strength steel and playing the role of reinforcement.
  • Element 15 holds parts 10 and 11 against the 17-17 'element which rests on the lower table of the press.
  • closed structure is based on the assembly of parts by four hems.
  • a typical section corresponding to this application is shown in Figure 7. Parts 22, 22 'are assembled by hem with the parts 21 and 21'.
  • Figure 8 presents a tool allowing hem this section to the hurry.
  • Exhibits 21 and 22 are prepared for the hem formation as shown in 23: they received a preform which initiates the hem.
  • the pieces are then placed in the tooling which is composed of the elements mobile 20 and 20 ', 19 and 19'. These elements are first apart, horizontally for 20 and 20 ', vertically for 19 and 19 '.
  • parts 22 and 22 'are deposited on elements 20 and 20 'and maintained in the same way. All type 18 tools (18 ', 18 '', 18 '') are then in the position indicated for the tool 18.
  • the tools 18 are then moved, successively or simultaneously to form the hem and find in the position indicated by 18 ', 18' ', 18' ''.
  • This type of tool can be mounted on a press, elements 19, 18 and 18 'being implemented by the slide upper of the press: 19 is mounted on springs and its stroke is limited by a stop not shown. The element 19 'rests on the press table and is therefore fixed, the 18 '' and 18 '' tools being activated by the slide bottom of the press.
  • This type of assembly method by press tool makes it possible to produce shapes whose section is not constant: the distance between the pieces 21 and 21 'as well as the distance between parts 22 and 22' may vary.
  • FIGS. 8 to 10 Potential applications concern different types of automotive structural parts like cockpit reinforcement parts (shield cross member), feet midpoints, spar elements, engine cradle. Some of these applications are illustrated in FIGS. 8 to 10.
  • the technique allows for complex shaped structures with steels having a very low ductility taking advantage of the productivity of the hem assembly process and the reinforcement it brings to the structure. It also helps to spare at the ends of the pieces of the metal tabs making it easy to assemble these parts to the rest of the automotive structure (Figure 11).
  • the hem assembly guarantees a very good keeping metals in the plane perpendicular to the axis of hem.
  • We can easily remedy this disadvantage for example by interposing an adhesive between the two sheets of metal at the hem, in performing local fusion welds or preferably by locally crushing the hem with a press comprising for example a punch in the shape of "V" terminated by a rounding and a flat anvil.
  • a press comprising for example a punch in the shape of "V" terminated by a rounding and a flat anvil.
  • This operation can be carried out with the press very productive: a tool can be designed to achieve simultaneously the indentations, the indentation step being on the order of 5 to 10 times the outside diameter of hem.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Manufacturing Of Electrical Connectors (AREA)
  • Electric Connection Of Electric Components To Printed Circuits (AREA)
  • Connection Of Plates (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Control Of Motors That Do Not Use Commutators (AREA)
  • Ceramic Products (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

The invention concerns a method for assembling at least two simple sheet metal elements (1, 2, 3,; 11, 12, 21, 21', 22, 22') for producing a structural part with open section, preferably U-shaped, or closed section, at least one of the metal elements having a high or very high yield strength and low deformability. The invention is characterised in that the metal elements are formed by at least a folding process; the metal elements are arranged relative to each other along a junction section; the metal elements are assembled by a crimped lap-joint (4) along the junction section of said elements.

Description

Objet de l'inventionSubject of the invention

La présente invention se rapporte à un procédé d'assemblage d'au moins deux éléments métalliques en vue de créer une structure, au moins un des deux éléments présentant une très haute limite d'élasticité et à son application pour réaliser des structures (de poutre) de forme complexe à partir d'éléments simples, ne demandant pas de déformations importantes.The present invention relates to a method of assembling at least two metallic elements in order to create a structure, at least one of the two elements with a very high yield strength and its application to realize (beam) structures of complex form from simple elements, not requiring no significant deformations.

Arrière-plan technologique et état de la techniqueTechnological background and state of the art

Dans le domaine de la construction mécanique et en particulier de l'automobile, l'objectif est de réduire sensiblement le poids des structures en utilisant le moins de métal possible. Ces structures, les châssis de véhicule automobile par exemple, sont obtenues par assemblage de pièces souvent complexes, réalisées par emboutissage.In the field of mechanical engineering and in particular of the automobile, the objective is to significantly reduce the weight of structures by using as little metal as possible. These structures, the chassis of motor vehicle for example are obtained by often complex parts assembled by stamping.

Afin de réduire l'épaisseur du métal utilisé pour réaliser ces structures tout en conservant leurs propriétés mécaniques, il faut utiliser des aciers présentant des caractéristiques mécaniques élevées. Des nuances d'aciers au carbone faiblement alliés présentant de hautes caractéristiques mécaniques, mais souvent associées à une capacité de mise en forme par déformation très limitée, sont aujourd'hui disponibles. In order to reduce the thickness of the metal used to build these structures while retaining their mechanical properties, steels must be used with high mechanical characteristics. of the grades of low alloy carbon steels with high mechanical characteristics, but often associated to a capacity for shaping by deformation very limited, are available today.

Pour fixer les idées, nous ferons la distinction, dans la suite de la description, entre ces aciers sur base de leur limite d'élasticité (LE) :

  • aciers doux : LE < 250 MPa ;
  • aciers à haute limite d'élasticité (HLE) : 250 MPa < LE < 600 MPa ;
  • aciers à très haute limite d'élasticité (THLE) : 600 MPa < LE < 1000 MPa ;
  • aciers à ultra-haute limite d'élasticité (UHLE) : 1000 MPa < LE < 1500 MPa.
To fix the ideas, we will make the distinction, in the following description, between these steels on the basis of their elastic limit (LE):
  • mild steels: LE <250 MPa;
  • high yield strength steels (HLE): 250 MPa <LE <600 MPa;
  • steels with very high yield strength (THLE): 600 MPa <LE <1000 MPa;
  • ultra-high yield strength steels (UHLE): 1000 MPa <LE <1500 MPa.

Typiquement, les aciers concernés par cette demande de brevet, présentent une limite d'élasticité située entre 400 et 1500 MPa. Ces aciers sont produits par des procédés sidérurgiques de masse connus en soi, qui permettent de proposer des aciers dont le prix de revient est voisin de celui des aciers au carbone classiques. L'intérêt réside alors dans le fait que l'on peut obtenir un allégement non négligeable de la structure. Cependant, de par leur faible capacité de mise en forme et de par une soudabilité parfois médiocre, ces aciers posent des problèmes spécifiques de mise en oeuvre, et en particulier d'assemblage.Typically, the steels affected by this patent application, have a yield strength located between 400 and 1500 MPa. These steels are produced by mass steel processes known per se, which allow to offer steels whose cost price is close to that of conventional carbon steels. The interest then lies in the fact that one can obtain significant reduction in structure. However, due to their low formatting capacity and sometimes poor weldability, these steels pose specific implementation problems, and in particular assembly.

Plus particulièrement, les éléments constitutifs d'une même structure présentent souvent des formes complexes obtenues par des procédés d'emboutissage impliquant des déformations importantes et donc incompatibles avec les faibles capacités de mise en forme de ces aciers.More specifically, the elements constitutive of the same structure often have complex shapes obtained by stamping processes involving significant deformations and therefore incompatible with poor formatting capabilities of these steels.

Le procédé de sertissage mécanique par ourlet ou similaire est bien connu, par exemple pour l'assemblage d'éléments tels que des échelles, en menuiserie métallique. Ainsi, le document US-A-4 356 888 décrit un joint structurel de deux éléments, réalisés de préférence en métal malléable et déformable, tel que l'aluminium. Selon une forme d'exécution particulière, le premier élément présente une languette allongée et une languette courte. Ces deux languettes définissent une cavité apte à recevoir le second élément au niveau d'une patte recourbée sur un support tel qu'un fil. Lorsque les deux éléments sont pressés l'un contre l'autre, en utilisant un outil adéquat, les languettes et la patte se déforment et s'interpénètrent. La languette allongée forme au moins partiellement une boucle circulaire autour de la patte, rendant alors impossible tout descellement ultérieur.The mechanical hem crimping process or the like is well known, for example for assembly items such as ladders, in metal carpentry. Thus, document US-A-4 356 888 describes a seal structural of two elements, preferably made of malleable and deformable metal, such as aluminum. according to a particular form of execution, the first element has an elongated tongue and a short tongue. These two tabs define a cavity capable of receiving the second element at the level of a curved leg on a support such as a wire. When the two elements are pressed together, using a suitable tool, the tabs and the tab deform and interpenetrate. The elongated tongue forms at least partially a circular loop around the tab, then making any subsequent loosening impossible.

Le document US-A-3 854 185 propose, dans le même domaine d'application, un procédé pour former un joint structurel entre deux éléments rigides, l'un présentant sur une face une bride avec une extrémité saillante et l'autre une gorge essentiellement circulaire. En appliquant les deux pièces avec suffisamment de force l'une contre l'autre, la bride pénètre dans la gorge en se déformant. Plus précisément, l'assemblage se fait par solidarisation de la bride avec la gorge, le bride formant un enroulement dans ladite gorge.Document US-A-3 854 185 proposes, in the same area of application, a process for forming a joint structural between two rigid elements, one presenting on one side a flange with one projecting end and the other an essentially circular groove. By applying the two pieces with enough force one against the other, the flange enters the throat while deforming. More precisely, the assembly is done by joining of the flange with the groove, the flange forming a winding in said throat.

Le document DE-C-385 642 propose une machine pour l'assemblage par sertissage de deux éléments de tôle pour former un corps creux.Document DE-C-385 642 proposes a machine for the assembly by crimping of two sheet metal elements to form a hollow body.

Le document FR-A-2 321 962 propose un procédé d'assemblage par sertissage d'un élément de zinc et d'un élément de plomb en vue de résoudre les problèmes d'étanchéité qui se présentent dans la domaine de la couverture de bâtiment.Document FR-A-2 321 962 proposes a process assembly by crimping a zinc element and a lead element to solve problems in the field of building cover.

Buts de l'inventionAims of the invention

La présente invention vise à proposer un procédé d'assemblage d'au moins deux éléments métalliques ou pièces constitutives dont au moins un des deux est réalisé dans un acier présentant une très haute limite d'élasticité associée à une faible capacité de mise en forme en vue de réaliser des pièces de structure de forme complexe, à partir de pièces plus simples réalisables à l'aide d'opérations de mise en forme essentiellement de type pliage, n'impliquant pas de déformations importantes dans le plan de la tôle, et donc compatibles avec les aciers à hautes caractéristiques mécaniques.The present invention aims to provide a method of assembling at least two metallic elements or component parts of which at least one of the two is made of steel with a very high limit of elasticity associated with a weak capacity of setting shape in order to make shaped structural parts complex, from simpler parts achievable at using formatting operations basically of folding type, not involving significant deformations in the plane of the sheet, and therefore compatible with steels with high mechanical characteristics.

En effet, au sein d'une famille d'alliage donnée, par exemple les aciers, ou encore les alliages d'aluminium, plus la limite d'élasticité est élevée, plus la ductilité est réduite. Le niveau de limite d'élasticité associé à cette faible capacité de mise en forme dépend de la famille d'alliage considérée ; ainsi pour les aciers cette limite peut être située de 600 à 800 MPa selon la nuance considérée. Au delà de cette limite, les aciers ne peuvent que très difficilement être mis en forme par emboutissage : des déformations dans le plan de la tôle en traction large ou en expansion vont rapidement conduire à la rupture. Le retour élastique rend également très difficile le respect de la géométrie de la pièce. Par contre ces aciers gardent une capacité de déformation par pliage. Toutefois le rayon limite de pliage étant de plusieurs fois l'épaisseur, l'assemblage par sertissage est pratiquement impossible.Indeed, within an alloy family given, for example steels, or alloys aluminum, the higher the elastic limit, the more ductility is reduced. The yield strength level associated with this low formatting capacity depends on the alloy family considered; so for steels this limit can be located from 600 to 800 MPa depending on the nuance considered. Beyond this limit, steels do not can be very difficult to be shaped by stamping: deformations in the plane of the sheet in wide or expanding traction will quickly lead to breaking. The elastic return also makes it very difficult to respect the geometry of the part. Through against these steels keep a capacity of deformation by folding. However, the bending limit radius is several times the thickness, the assembly by crimping is practically impossible.

Ces aciers présentent cependant un potentiel intéressant d'amélioration des structures métalliques et en particulier des structure automobiles. Ils permettent de réduire le poids à performances égales ou encore d'améliorer les performances à poids égal.However, these steels have potential interesting improvement of metallic structures and in particular of automobile structures. They allow to reduce weight for equal performance or improve performance at equal weight.

Il est donc déterminant de pouvoir réaliser des pièces de formes complexes à partir de ces métaux à hautes caractéristiques mécaniques, ce qui est l'objet de la présente invention. It is therefore crucial to be able to carry out parts of complex shapes from these metals to high mechanical properties, which is the subject of the present invention.

Principaux éléments caractéristiques de l'inventionMain characteristic features of the invention

La présente invention se rapporte à un procédé d'assemblage d'au moins deux éléments métalliques simples en feuille, en vue de créer une pièce de structure de section ouverte, de préférence en forme de "U", ou fermée, au moins un desdits éléments métalliques présentant une haute ou très haute limite d'élasticité LE supérieur a 250 MPa et une faible capacité de déformation, caractérisé en ce que :

  • les éléments métalliques sont mis en forme par au moins un procédé de pliage ;
  • les éléments métalliques sont disposés l'un par rapport à l'autre suivant une section de jonction ;
  • les éléments métalliques sont assemblés par sertissage par ourlet (4) le long de la section de jonction desdits éléments.
The present invention relates to a method of assembling at least two simple metal elements in sheet form, in order to create a structural part of open section, preferably in the shape of a "U", or closed, at least one of said metallic elements having a high or very high elastic limit LE greater than 250 MPa and a low deformation capacity, characterized in that:
  • the metal elements are shaped by at least one folding process;
  • the metal elements are arranged relative to each other along a joining section;
  • the metal elements are assembled by hemming (4) along the joining section of said elements.

Au moins un des éléments est réalisé de préférence dans un acier présentant une limite d'élasticité supérieur à 400 MPa ou dans un alliage d'aluminium avec une limite d'élasticité supérieure à 200 MPa.At least one of the elements is made of preferably in steel with yield strength greater than 400 MPa or in an aluminum alloy with a yield strength greater than 200 MPa.

Avantageusement, le rapport du rayon de l'ourlet à la somme des épaisseurs des différents éléments que l'on désire assembler le long de la section de jonction est compris entre 2 et 10.Advantageously, the ratio of the radius of the hem to the sum of the thicknesses of the different elements that we want to assemble along the junction section is between 2 and 10.

De plus, le rapport de la différence entre le rayon de l'ourlet et l'épaisseur du métal le plus extérieur avec l'épaisseur du métal le plus intérieur est, avantageusement supérieur à 2.In addition, the ratio of the difference between the radius of hem and outermost metal thickness with the innermost metal thickness is, advantageously greater than 2.

La nature ou l'épaisseur des différents éléments peut ne pas être identique pour tous les éléments.The nature or thickness of the different elements may not be the same for all elements.

Le procédé est également caractérisé par le fait que la jonction n'est pas nécessairement rectiligne mais peut présenter une courbure locale, le rayon de courbure étant de préférence supérieur à cinq rayons extérieurs d'ourlet.The process is also characterized by the fact that the junction is not necessarily straight but may have local curvature, the radius of curvature preferably being greater than five radii hem exteriors.

Le procédé d'assemblage selon l'invention se caractérise en outre par le fait qu'après l'opération de sertissage par ourlet, un blocage dudit ourlet vis-à-vis du glissement de ses éléments le long de la section de jonction, est obtenu par collage, indentation ou imbrication.The assembly method according to the invention is further characterized by the fact that after the operation of hem crimping, blocking said hem vis-à-vis the sliding of its elements along the section of junction, is obtained by gluing, indentation or nesting.

La présente invention concerne également le produit obtenu par le procédé d'assemblage décrit ci-dessus, lequel est défini dans la revendication 9.The present invention also relates to the product obtained by the assembly process described above, which is defined in claim 9.

Sous une première forme préférée de l'invention, le produit se présente sous la forme d'une poutre en "I" à âme double, obtenue par l'assemblage de quatre éléments constitutifs reliés par quatre ourlets le long de la section de jonction des quatre éléments pris deux à deux.In a first preferred form of the invention, the product is in the form of a double-core "I" beam, obtained by assembling four components connected by four hems the along the junction section of the four elements taken two by two.

Sous une deuxième forme préférée de l'invention, le produit résulte de l'assemblage de deux éléments par deux ourlets de façon à former une section fermée, un des deux éléments au moins présentant une section en "U".In a second preferred form of the invention, the product results from the assembly of two elements by two hems so as to form a section closed, at least one of the two elements having a "U" section.

Le procédé de l'invention permet donc d'obtenir des pièces de structure de forme complexe à partir de matériaux métalliques en feuille présentant, d'une part, une limite d'élasticité élevée à très élevée, et d'autre part, une capacité de formage limitée. Cette dernière n'est pas contraignante au niveau d'opérations préparatoires au processus d'assemblage, telles que le pliage, impliquant peu de déformation dans le plan de la tôle. Ce procédé permet ainsi d'obtenir des pièces de géométrie équivalente à celle obtenue par emboutissage. De plus, l'assemblage par ourlet est compatible avec la faible formabilité de ces aciers, le rayon de travail valant plusieurs fois l'épaisseur, ce qui n'est pas le cas du sertissage simple par exemple.The process of the invention therefore allows to obtain structural parts of complex shape to from sheet metal materials presenting, on the one hand, a high to very high elastic limit, and on the other hand, a limited forming capacity. This last is not binding at the level of operations preparatory to the assembly process, such as the folding, involving little deformation in the plane of the sheet. This process thus makes it possible to obtain pieces of geometry equivalent to that obtained by stamping. Of plus, hem assembly is compatible with low formability of these steels, the working radius being several times the thickness, which is not the case for Simple crimping for example.

Un autre avantage de l'invention réside dans le fait que le procédé d'assemblage ou sertissage par ourlet, purement mécanique, permet de s'affranchir des problèmes de soudabilité éventuels des aciers à hautes caractéristiques mécaniques.Another advantage of the invention lies in the fact that the assembly process or crimping by purely mechanical hem allows you to get rid of possible weldability problems of high steels mechanical characteristics.

Un avantage complémentaire de l'invention est de proposer un procédé pour la réalisation de pièces de structure renforcées, en particulier dans l'industrie automobile.An additional advantage of the invention is to propose a process for the production of pieces of reinforced structure, especially in industry automobile.

Enfin, le procédé de l'invention, qui utilise une simple presse pour l'assemblage, est un procédé bon marché.Finally, the method of the invention, which uses a simple press for assembly is a good process market.

Brève description des dessinsBrief description of the drawings

Les figures 1 décrivent une structure réalisée de manière classique présentant une géométrie en "U".Figures 1 describe a structure carried out in a conventional manner having a geometry in "U".

Les figures 2 représentent les éléments constitutifs simples en vue de créer le même genre de structure que celle représentée aux figures 1 selon le procédé d'assemblage de la présente invention.Figures 2 show the elements simple constituents in order to create the same kind of structure as that shown in FIGS. 1 according to the assembly method of the present invention.

Les figures 3 représentent un outil permettant la réalisation d'une structure telle que décrite à la figure 2.Figures 3 show a tool allowing the realization of a structure as described in Figure 2.

La figure 4 représente des variantes d'orientation d'assemblage pour une structure en U.Figure 4 shows variants assembly orientation for a U-shaped structure.

Les figures 5 représentent une forme d'exécution plus complexe d'une structure possédant une section fermée et obtenue selon le procédé d'assemblage de la présente invention. Figures 5 show a shape more complex execution of a structure with a closed section obtained by the assembly process of the present invention.

La figure 6 représente l'outil mis en oeuvre pour réaliser une structure fermée telle que représentée aux figures 5.Figure 6 shows the tool used to make a closed structure as shown in Figures 5.

La figure 7 représente une autre forme d'exécution d'une structure présentant la forme d'une poutre en "I" à âme double.Figure 7 shows another form execution of a structure having the form of a double-core "I" beam.

La figure 8 représente l'outil permettant la réalisation et l'assemblage d'une poutre en "I" à âme double.Figure 8 shows the tool for realization and assembly of an "I" beam with core double.

La figure 9 représente une pièce de type traverse de bouclier.FIG. 9 represents a part of the type shield crosspiece.

La figure 10 représente une pièce de type pied milieu.FIG. 10 represents a part of the type middle foot.

La figure 11 représente une pièce présentant des languettes aux extrémités pour faciliter l'assemblage.Figure 11 represents a part presenting tabs at the ends to facilitate assembly.

Les figures 12 illustrent le principe de blocage du glissement relatif de l'âme par rapport à la semelle dans l'assemblage par ourlet, par imbrication à l'aide d'une découpe de créneaux alternés. Les figures 12a et 12b présentent les deux tôles juste avant la réalisation de l'ourlet.Figures 12 illustrate the principle of blocking of the relative sliding of the core with respect to the sole in hem assembly, by interlocking using a cut of alternating slots. Figures 12a and 12b present the two sheets just before production hem.

Description détaillée de plusieurs formes d'exécution de l'inventionDetailed description of several embodiments of the invention

L'idée à la base de l'invention est de décomposer un élément de structure de forme complexe, réalisé habituellement par des opérations de mise à forme par emboutissage peu compatibles avec des aciers à hautes caractéristiques mécaniques, en sous-éléments simples, réalisés à l'aide d'opérations de formage de type pliage, et assemblés par ourlet.The idea behind the invention is to decompose a structure element of complex shape, usually achieved by shaping operations by stamping not very compatible with high steels mechanical characteristics, in simple sub-elements, performed using folding type forming operations, and hemmed together.

La présente invention sera décrite plus en détails à l'aide des figures annexées.The present invention will be described in more detail details using the attached figures.

La figure 1 présente le mode habituel de réalisation d'une pièce de géométrie en "U". Classiquement ce type de pièce est obtenu par emboutissage à partir d'une tôle plane comme schématisé à la figure la. Dans le cadre d'aciers à très haute limite d'élasticité, l'emboutissage d'une telle pièce pose des problèmes sévères de maítrise du retour élastique : la forme obtenue s'écarte sensiblement de la forme idéale comme présenté à la figure 1b. Des problèmes critiques dus à la faible formabilité de ce type d'acier surviennent, par exemple lorsque la hauteur de la section en "U" varie sensiblement comme indiqué à la figure 1c ou lorsque la hauteur de la section restant constante, la courbure de la poutre en "U" varie localement de façon sensible (figure 1d).Figure 1 shows the usual mode of production of a "U" shaped part. classically this type of part is obtained by stamping from a flat sheet as shown schematically in Figure la. As part steels with very high yield strength, stamping of such a room poses severe problems of control of the elastic return: the shape obtained deviates appreciably of the ideal shape as shown in Figure 1b. of the critical problems due to low formability of this type occur, for example when the height of the "U" section varies significantly as shown in figure 1c or when the height of the section remains constant, the curvature of the "U" beam varies locally so sensitive (Figure 1d).

Le principe selon la présente invention proposé pour réaliser ce type de pièce est illustré aux figures 2. La pièce est décomposée en éléments simples, les côtés 1 et 2, le fond 3 qui sont assemblés par un ourlet 4.The principle according to the present invention proposed to make this type of part is illustrated in figures 2. The part is broken down into simple elements, the sides 1 and 2, the bottom 3 which are joined by a hem 4.

Les pièces 1, 2 et 3 peuvent être obtenues par pliage ou par relevage de bord. Ces techniques de mise en forme n'impliquent que de faibles déformations dans le plan de la tôle et sont compatibles avec des aciers à très haute limite d'élasticité présentant une faible capacité de formage.Parts 1, 2 and 3 can be obtained by folding or lifting the edge. These bet techniques in shape only involve small deformations in the sheet plane and are compatible with steels with very high yield strength with low capacity forming.

La figure 3 présente un outil typique permettant la réalisation de ce type de pièce à l'aide d'une presse. Les éléments latéraux 1 ou 2 et le fond 3 sont préparés pour la formation de l'ourlet comme indiqué en 5. Ces pièces réalisées à l'aide d'opération de presses simples sont présentées dans l'outil décrit à la figure 3.Figure 3 shows a typical tool allowing the realization of this type of part using of a press. The side elements 1 or 2 and the bottom 3 are prepared for hemming as shown in 5. These parts produced using press operations are presented in the tool described in Figure 3.

La demi-vue de gauche présente l'outil fermé, avant la réalisation de l'ourlet, la demi-vue de droite présente l'outil une fois l'ourlet terminé. Les éléments 7, 7' et 9 prennent appui sur le coulisseau supérieur de la presse par l'intermédiaire de ressorts non représentés et dont la course d'écrasement est supérieure à la course des outils 8, 8' formant l'ourlet. Dans la situation présentée à la figure 3, les ressorts sont comprimés et pressent, par l'intermédiaire des pièces 7 et 9, les pièces 1, 2 et 3 contre la pièce 10 qui épouse leur forme et repose sur la table de la presse. Lorsque le coulisseau de la presse achève sa course, l'élément 8' qui lui est directement relié forme l'ourlet comme indiqué dans la partie droite de la figure 3.The left half-view shows the closed tool, before the hem, the right half view presents the tool when the hem is finished. Elements 7, 7 'and 9 are supported on the upper slide of the press by means of springs not shown and whose crushing stroke is greater than the stroke of tools 8, 8 'forming the hem. In the situation presented in FIG. 3, the springs are compressed and press, by through parts 7 and 9, parts 1, 2 and 3 against part 10 which follows their shape and rests on the press table. When the press slide ends its course, the element 8 'which is directly to it bound forms the hem as shown on the right side of Figure 3.

Les pièces 1, 2 et 3 ne sont pas nécessairement toutes en acier à haute limite d'élasticité : par exemple, selon la fonction de la pièce, seule la pièce 3 peut être en acier à très haute limite d'élasticité, les pièces 1 et 2 en acier présentant une meilleure capacité de mise à forme et une meilleure soudabilité, ce qui permet d'assembler facilement la pièce au reste de la structure avec des procédés d'assemblage tels que la soudure par points. Le procédé permet également d'adapter les épaisseurs aux exigences structurales de la pièce : les trois pièces 1, 2 et 3 peuvent présenter des épaisseurs différentes, le procédé d'assemblage par ourlet acceptant des épaisseurs sensiblement différentes, dont le rapport est supérieur à deux.Parts 1, 2 and 3 are not necessarily all high-limit steel elasticity: for example, depending on the function of the part, only part 3 can be made of very high limit steel of elasticity, steel parts 1 and 2 having a better formability and better weldability, making it easy to assemble the part to the rest of the structure with assembly processes such as spot welding. The process allows also to adapt thicknesses to requirements structural parts: the three parts 1, 2 and 3 may have different thicknesses, the process hem assembly accepting thicknesses significantly different, with a ratio greater than of them.

Des variantes d'orientation de l'ourlage sont présentées à la figure 4.Variations of hemming orientation are shown in Figure 4.

Le procédé permet également de réaliser des sections fermées comme indiqué à la figure 5. Selon la figure 5, la pièce 11 peut être obtenue par simple pliage, une variation de la section fermée étant obtenue en variant la hauteur des bords pliés. La pièce 12 qui ferme la section est de forme encore plus simple. Comme variante de ce cas, la pièce 11 peut également être réalisée par emboutissage d'un acier à plus basse limite d'élasticité, inférieure à 400 MPa par exemple, la pièce 12 étant en acier à très haute limite d'élasticité et jouant le rôle de renfort.The method also makes it possible to carry out closed sections as shown in Figure 5. According to the FIG. 5, the part 11 can be obtained by simple folding, a variation of the closed section being obtained by varying the height of the folded edges. Exhibit 12 which closes the section is even simpler in shape. As a variant of in this case, the part 11 can also be produced by deep drawing of steel with lower yield strength, less than 400 MPa for example, part 12 being in very high yield strength steel and playing the role of reinforcement.

Un outillage typique permettant de réaliser ce type de pièce est présenté à la figure 6. Le principe est proche de celui décrit à la figure 3. Les éléments 14, 14' et 15 prennent appui sur le coulisseau supérieur de la presse par l'intermédiaire de ressorts non représentés.A typical tool allowing to realize this type of part is presented in figure 6. The principle is close to that described in FIG. 3. Elements 14, 14 'and 15 are supported on the upper slide of the press by means of springs not shown.

L'élément 15 maintient les pièces 10 et 11 contre l'élément 17-17' qui repose sur la table inférieure de la presse.Element 15 holds parts 10 and 11 against the 17-17 'element which rests on the lower table of the press.

Dans la partie gauche de la figure, la situation avant la formation de l'ourlet est représentée : le coulisseau de la presse a amené les éléments 14 et 15 en contact, les ressorts étant légèrement comprimés. La vue de droite présente la situation à la fin de la formation de l'ourlet : le coulisseau de la presse a poursuivi sa course et l'élément 16', qui lui est directement relié, a formé l'ourlet.In the left part of the figure, the situation before hem formation is shown: the press slide brought elements 14 and 15 into contact, the springs being slightly compressed. The view of right presents the situation at the end of the formation of the hem: the press slide continued to run and the element 16 ', which is directly connected to it, has formed hem.

Un autre mode possible de réalisation de structure fermée est basé sur l'assemblage des pièces par quatre ourlets. Une section typique correspondant à cette application est présentée à la figure 7. Les pièces 22, 22' sont assemblées par ourlet avec les pièces 21 et 21'.Another possible embodiment of closed structure is based on the assembly of parts by four hems. A typical section corresponding to this application is shown in Figure 7. Parts 22, 22 'are assembled by hem with the parts 21 and 21'.

La figure 8 présente un outillage permettant de réaliser l'assemblage par ourlet de cette section à la presse. Les pièces 21 et 22 sont préparées en vue de la formation de l'ourlet comme indiqué en 23 : elles ont reçu une préforme qui amorce l'ourlet. Les pièces sont alors placées dans l'outillage qui est composé des éléments mobiles 20 et 20', 19 et 19'. Ces éléments sont d'abord écartés, horizontalement pour 20 et 20', verticalement pour 19 et 19'. Les pièces 21 et 21' sont déposées sur 19 et 19' respectivement et maintenues par des moyens non représentés, un système magnétique par exemple. De même, les pièces 22 et 22' sont déposées sur les éléments 20 et 20' et maintenues de même. Tous les outils de type 18 (18', 18'', 18''') sont alors dans la position indiquée pour l'outil 18. Les outils 18 sont alors déplacés, successivement ou simultanément pour former l'ourlet et se trouver dans la position indiquée par 18', 18'', 18'''. Ce type d'outillage peut être monté sur une presse, les éléments 19, 18 et 18' étant mis en oeuvre par le coulisseau supérieur de la presse : 19 est monté sur ressorts et sa course est limitée par une butée non représentée. L'élément 19' repose sur la table de la presse et est donc fixe, les outils 18'' et 18''' étant mise en action par le coulisseau inférieur de la presse. Ce type de mode d'assemblage par outil de presse permet de réaliser des formes dont la section n'est pas constante : la distance entre les pièces 21 et 21' ainsi que la distance entre les pièces 22 et 22' peuvent varier.Figure 8 presents a tool allowing hem this section to the hurry. Exhibits 21 and 22 are prepared for the hem formation as shown in 23: they received a preform which initiates the hem. The pieces are then placed in the tooling which is composed of the elements mobile 20 and 20 ', 19 and 19'. These elements are first apart, horizontally for 20 and 20 ', vertically for 19 and 19 '. The pieces 21 and 21 'are deposited on 19 and 19' respectively and maintained by means not shown, a magnetic system for example. Likewise, parts 22 and 22 'are deposited on elements 20 and 20 'and maintained in the same way. All type 18 tools (18 ', 18 '', 18 '') are then in the position indicated for the tool 18. The tools 18 are then moved, successively or simultaneously to form the hem and find in the position indicated by 18 ', 18' ', 18' ''. This type of tool can be mounted on a press, elements 19, 18 and 18 'being implemented by the slide upper of the press: 19 is mounted on springs and its stroke is limited by a stop not shown. The element 19 'rests on the press table and is therefore fixed, the 18 '' and 18 '' tools being activated by the slide bottom of the press. This type of assembly method by press tool makes it possible to produce shapes whose section is not constant: the distance between the pieces 21 and 21 'as well as the distance between parts 22 and 22' may vary.

Les applications potentielles concernent différents types de pièces de structure automobile comme pièces de renfort d'habitacle (traverse bouclier), pieds milieux, éléments de longeron, berceau moteur. Certaines de ces applications sont illustrées aux figures 8 à 10.Potential applications concern different types of automotive structural parts like cockpit reinforcement parts (shield cross member), feet midpoints, spar elements, engine cradle. Some of these applications are illustrated in FIGS. 8 to 10.

La technique permet de réaliser des structures de forme complexe avec des aciers présentant une très faible ductilité en profitant de la productivité du procédé d'assemblage par ourlet et du renforcement qu'il apporte à la structure. Elle permet également de ménager aux extrémités des pièces des languettes de métal permettant d'assembler facilement ces pièces au reste de la structure automobile (figure 11).The technique allows for complex shaped structures with steels having a very low ductility taking advantage of the productivity of the hem assembly process and the reinforcement it brings to the structure. It also helps to spare at the ends of the pieces of the metal tabs making it easy to assemble these parts to the rest of the automotive structure (Figure 11).

L'assemblage par ourlet garantit un très bon maintien des métaux dans le plan perpendiculaire à l'axe de l'ourlet. Toutefois, il existe un risque non négligeable de glissement des éléments assemblés dans l'axe de l'ourlet ou du moins dans la direction longitudinale, si l'ourlet n'est pas rectiligne. On peut facilement remédier à cet inconvénient, par exemple en interposant une colle entre les deux feuilles de métal au niveau de l'ourlet, en réalisant des soudures par fusion locale ou encore de préférence en écrasant localement l'ourlet avec un outil de presse comprenant par exemple un poinçon en forme de "V" terminé par un arrondi et une enclume plane. Cette opération peut être réalisée à la presse de façon très productive : un outillage peut être conçu pour réaliser simultanément les indentations, le pas d'indentation étant de l'ordre de 5 à 10 fois le diamètre extérieur de l'ourlet.The hem assembly guarantees a very good keeping metals in the plane perpendicular to the axis of hem. However, there is a significant risk of sliding of the assembled elements in the axis of the hem or at least in the longitudinal direction, if the hem is not not straight. We can easily remedy this disadvantage, for example by interposing an adhesive between the two sheets of metal at the hem, in performing local fusion welds or preferably by locally crushing the hem with a press comprising for example a punch in the shape of "V" terminated by a rounding and a flat anvil. This operation can be carried out with the press very productive: a tool can be designed to achieve simultaneously the indentations, the indentation step being on the order of 5 to 10 times the outside diameter of hem.

On peut également procéder à des découpes dentelées alternées dans les deux feuilles de métal, dans la zone à assembler par ourlet, de manière à garantir un blocage longitudinal (figures 12). Ces découpes sont pratiquées lors des étapes de fabrication à la presse de ces pièces. Les dents 20 présentent une hauteur inférieure à la circonférence de l'ourlet, par exemple le tiers de cette circonférence. La largeur des dents 20 est légèrement inférieure à celle des intervalles 21 entre les dents. Lors de l'assemblage des deux feuilles de métal par ourlet, les dents de la tôle se trouvant la plus proche de l'axe de l'ourlet s'imbriquent dans l'espace entre les dents de la feuille de métal extérieure réalisant ainsi un blocage selon l'axe de l'ourlet.You can also make cuts serrated alternating in the two sheets of metal, in the area to be hemmed together, so as to guarantee longitudinal locking (Figures 12). These cuts are practiced during the manufacturing steps in the press of these parts. The teeth 20 have a lower height around the hem, for example a third of this circumference. The width of the teeth 20 is slightly less than that of the intervals 21 between the teeth. then of joining the two sheets of metal by hem, the sheet metal teeth closest to the axis of the hem fit into the space between the teeth of the exterior metal sheet thereby blocking along the axis of the hem.

Claims (13)

  1. Process for assembling at least two simple sheet metal parts (1, 2, 3; 11, 12; 21, 21', 22, 22') in order to create a structural component of open cross section, which is preferably U-shaped, or of closed cross section, at least one of said metal parts having a high or very high elastic limit (EL of more than 250 MPa) and low deformability, characterised in that:
    the metal parts are formed by at least one bending process;
    the metal parts are arranged relative to each other in a junction section;
    the metal parts are assembled by crimping at the hem (4) along the junction section of said parts.
  2. Assembly process according to Claim 1, characterised in that at least one of the parts is made of steel and has an elastic limit of more than 400 MPa.
  3. Assembly process according to Claim 1, characterised in that at least one of the parts is made of aluminium alloy and has an elastic limit of more than 200 MPa.
  4. Assembly process according to any one of Claims 1 to 3, characterised in that the ratio of the radius of the hem (4) to the sum of the thicknesses of the various parts one wishes to assemble along the junction section is between 2 and 10.
  5. Assembly process according to any one of Claims 1 to 3, characterised in that the ratio of the difference between the radius of the hem (4) and the thickness of the outermost metal with the thickness of the innermost metal is more than 2.
  6. Assembly process according to any one of the preceding claims, characterised in that the nature or the thickness of the various parts is not identical for all.
  7. Assembly process according to any one of the preceding claims, characterised in that the junction is not rectilinear and has a local curvature, the radius of which is more than at least five times the external radius of the hem (4).
  8. Assembly process according to any one of the preceding claims, characterised in that, after said hem crimping, a blocking of said hem with respect to the sliding of the assembled parts along the junction section is achieved by bonding, indentation or imbrication.
  9. Product obtained by the assembly process described in any one of the preceding claims, characterised in that it has at least two simple sheet metal parts (1, 2, 3; 11, 12; 21, 21', 22, 22') in order to create a structural component of open cross section, which is preferably U-shaped, or of closed cross section, at least one of said metal part having a high or very high elastic limit (EL of more than 250 MPa) and low deformability, characterised in that the metal parts, which have been formed by at least one bending process and arranged relative to each other in a junction section, are assembled by means of a hem (4) along said junction section, said hem mechanically reinforcing the structure.
  10. Product according to Claim 9, characterised in that the ratio of the radius of the hem (4) to the sum of the thicknesses of the various parts that are assembled along the junction section is between 2 and 10.
  11. Product according to Claim 9 or 10, characterised in that the ratio of the difference between the radius of the hem (4) and the thickness of the outermost metal with the thickness of the innermost metal is more than 2.
  12. Product according to any one of Claims 9 to 11, characterised in that it is in the form of a two-web I-shaped girder obtained by assembling four constituent parts (21, 21', 22, 22') connected by means of four hems (4) along the junction section of the four parts taken in pairs.
  13. Product according to any one of Claims 9 to 11, characterised in that it results from the assembly of two parts (11, 12) by means of two hems (4) so as to form a closed cross section, at least one of the two parts having a U-shaped cross section.
EP00945472A 1999-07-05 2000-07-05 Method for assembling at least two component metal elements for producing a structure Expired - Lifetime EP1192016B1 (en)

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EP00945472A EP1192016B1 (en) 1999-07-05 2000-07-05 Method for assembling at least two component metal elements for producing a structure

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EP99202194A EP1066894A1 (en) 1999-07-05 1999-07-05 Method of assembling at least two metallic elements for creating a metallic structure
EP99202194 1999-07-05
PCT/BE2000/000080 WO2001002110A1 (en) 1999-07-05 2000-07-05 Method for assembling at least two component metal elements for producing a structure
EP00945472A EP1192016B1 (en) 1999-07-05 2000-07-05 Method for assembling at least two component metal elements for producing a structure

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EP1192016A1 EP1192016A1 (en) 2002-04-03
EP1192016B1 true EP1192016B1 (en) 2003-02-26

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EP99202194A Withdrawn EP1066894A1 (en) 1999-07-05 1999-07-05 Method of assembling at least two metallic elements for creating a metallic structure

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US (1) US6857812B1 (en)
EP (2) EP1066894A1 (en)
KR (1) KR20020043545A (en)
AT (1) ATE233139T1 (en)
AU (1) AU5956400A (en)
BR (1) BR0012356A (en)
CA (1) CA2373908A1 (en)
DE (1) DE60001502T2 (en)
WO (1) WO2001002110A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7628287B1 (en) * 2004-05-10 2009-12-08 Arnold William M Reusable container unit having spaced protective housings
DE102006029180A1 (en) * 2006-06-24 2007-12-27 Bayerische Motoren Werke Ag Production of a sheet metal part used in the production of doors and tailgates for vehicles comprises injecting an adhesive into the flange fold after flanging the ends of the flange fold
JP5927874B2 (en) * 2011-01-31 2016-06-01 株式会社リコー Sheet material punching device
JP6610777B2 (en) * 2016-04-20 2019-11-27 株式会社デンソー Heat exchanger and manufacturing method thereof

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DE385642C (en) * 1921-12-15 1923-11-27 Menuiserie Metallique Du Sud E Machine for joining two sheet metal parts to form a hollow body by folding
US2125692A (en) * 1932-04-27 1938-08-02 Budd Edward G Mfg Co Beam structure
US2054703A (en) * 1935-03-28 1936-09-15 Newport Culvert Company Pipe or tubing and manufacture of same
US2129624A (en) * 1936-12-04 1938-09-06 Rafter Machine Company Stud and rafter
US2818272A (en) * 1954-08-27 1957-12-31 Lay Ind Inc De Adjusting and locking device for relatively movable main and auxiliary trailer frames
US3151767A (en) * 1961-09-02 1964-10-06 Nakata Takehiko Container seam
US3716895A (en) * 1971-10-27 1973-02-20 Allied Chem Unitary seat belt buckle
US3854185A (en) * 1973-07-09 1974-12-17 R Reid Method of forming structural joints
FR2319439A1 (en) * 1975-07-31 1977-02-25 Gallay Sa PERFECTION OF THE TRIPLE CRIMPING PROCESS
FR2321962A1 (en) * 1975-08-25 1977-03-25 Mines Fond Zinc Vieille Connecting zinc and lead sheet by folding edges - to form watertight assembly for roofing construction
US4193247A (en) * 1978-02-06 1980-03-18 Amca International Corporation Panel mounting clip
US4190160A (en) * 1979-03-06 1980-02-26 The United States Of America As Represented By The United States Department Of Energy Accident resistant transport container
US4356888A (en) * 1980-09-15 1982-11-02 Steenberg Christen K Structural joint
US4554718A (en) * 1984-06-04 1985-11-26 Armstrong World Industries, Inc. Method of reinforcing a ceiling runner
US4982487A (en) * 1988-10-27 1991-01-08 Hughes Aircraft Company Metallic component cold roll/crimping tool
US5238146A (en) * 1992-02-18 1993-08-24 Van Leer Containers, Inc. Support device to facilitate emptying of containers
US5327631A (en) * 1992-06-29 1994-07-12 Lincavage George P Roll pin punch kit apparatus
US5351736A (en) * 1993-10-04 1994-10-04 The Dometic Corporation Roller tube for awning and method of forming
US5603153A (en) * 1995-04-28 1997-02-18 Radar Industries, Inc. Methodology for forming stamped sheet metal parts of complex configuration
US6041564A (en) * 1998-03-06 2000-03-28 Usg Interiors, Inc. Clinched double web grid tee

Also Published As

Publication number Publication date
BR0012356A (en) 2002-03-26
KR20020043545A (en) 2002-06-10
EP1192016A1 (en) 2002-04-03
US6857812B1 (en) 2005-02-22
DE60001502T2 (en) 2003-12-11
AU5956400A (en) 2001-01-22
ATE233139T1 (en) 2003-03-15
EP1066894A1 (en) 2001-01-10
CA2373908A1 (en) 2001-01-11
WO2001002110A1 (en) 2001-01-11
DE60001502D1 (en) 2003-04-03

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