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EP1689939B2 - Girder for a support wall curtain - Google Patents

Girder for a support wall curtain Download PDF

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Publication number
EP1689939B2
EP1689939B2 EP04817205.0A EP04817205A EP1689939B2 EP 1689939 B2 EP1689939 B2 EP 1689939B2 EP 04817205 A EP04817205 A EP 04817205A EP 1689939 B2 EP1689939 B2 EP 1689939B2
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EP
European Patent Office
Prior art keywords
thickness
flange
web
flanges
extra material
Prior art date
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EP04817205.0A
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German (de)
French (fr)
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EP1689939B1 (en
EP1689939A1 (en
Inventor
Aloyse Hermes
Marc Widong
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ArcelorMittal Belval and Differdange SA
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ArcelorMittal Belval and Differdange SA
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Application filed by ArcelorMittal Belval and Differdange SA filed Critical ArcelorMittal Belval and Differdange SA
Priority to PL04817205T priority Critical patent/PL1689939T3/en
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Publication of EP1689939B1 publication Critical patent/EP1689939B1/en
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    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02DFOUNDATIONS; EXCAVATIONS; EMBANKMENTS; UNDERGROUND OR UNDERWATER STRUCTURES
    • E02D5/00Bulkheads, piles, or other structural elements specially adapted to foundation engineering
    • E02D5/02Sheet piles or sheet pile bulkheads
    • E02D5/03Prefabricated parts, e.g. composite sheet piles
    • E02D5/04Prefabricated parts, e.g. composite sheet piles made of steel
    • E02D5/08Locking forms; Edge joints; Pile crossings; Branch pieces
    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02DFOUNDATIONS; EXCAVATIONS; EMBANKMENTS; UNDERGROUND OR UNDERWATER STRUCTURES
    • E02D5/00Bulkheads, piles, or other structural elements specially adapted to foundation engineering
    • E02D5/02Sheet piles or sheet pile bulkheads
    • E02D5/03Prefabricated parts, e.g. composite sheet piles
    • E02D5/04Prefabricated parts, e.g. composite sheet piles made of steel

Definitions

  • the present invention relates to a beam for a retaining curtain and a retaining curtain comprising such beams.
  • Retaining curtains formed, either exclusively of beams or beams and sheet piles, have been known for a long time. They have the advantage of presenting very important resistance modules for an advantageous surface weight.
  • the connections between two beams or a beam and a sheet pile are made at the edges of the flanges of the beams.
  • HZ an integrated system for making retaining curtains.
  • This integrated system includes special beams, called HZ beams.
  • the edge of the wings of these beams HZ ends with a substantially triangular section bead, which is projecting relative to the outer surface of the wing. On this beaded wing edge, it is possible to slide a RH or RZ-type connection profile making it possible to connect another HZ beam or AZ sheet pile.
  • a connecting system for joists with thick wings is known from the document DE 583 471 . These are small joists, the height of the soul being equal to the width of the wing, which can be mounted in the retaining curtain with their soul either perpendicular or parallel to the axis of the curtain.
  • a wing of this beam has a groove rolled or machined along each longitudinal edge in the inner surface of the wing and a bearing rolled or machined in the side edge of the wing. The groove and the bearing make it possible to connect the ends of the wings of two adjacent beams by means of special connector profiles and to connect a wing of a first beam transversely between the two wings of a second beam. It is therefore a very special connection system, which was designed in 1927 for a particular implementation of low joists and which has probably never been successful.
  • a first type of lock member includes a "bent finger” and "an inch” defining a lock chamber.
  • a second type of lock member comprises a bead adapted to be received in the lock chamber.
  • a projection to which several functions are assigned.
  • a first function would be to increase the stability of a stack of beams.
  • the elongated beam on a wing rests indeed on said projection and on the lock element of said first type, which has substantially the same height as said projection.
  • a second function would be to form a support for a guide element when driving a beam into the ground.
  • a third function would be to balance the cross sections of the wings with respect to the soul.
  • said projection would increase the section module of the beam.
  • the rolling of such claws and projections is a difficult operation and almost impossible for a beam with wings having a thickness of more than 22 mm.
  • the practice should still show if this new connection system is proving itself on construction sites.
  • An object of the present invention is to provide a beam that can be easily laminated with a higher resistance module, without having to increase its height significantly, and whose Installation in retaining curtains can be done using various connection systems that have proven themselves on construction sites.
  • a beam for retaining curtain according to claims 1, 3 or 4.
  • the reinforcement of the wings by a material thickness, located on the opposite side to the core, allows to significantly increase the resistance module of the beam, without any notable increase in height.
  • the non-reinforced wing tips, whose thickness is comparable to the wing thickness of a conventional beam for retaining curtains, allow on the other hand to use almost all connection systems known for the integration of a beam in a retaining curtain.
  • the connecting means carried by the wingtips comprise a connecting bead.
  • a beam of this type can be easily integrated into a retaining wall using connecting elements comparable to the "RH” or “RZ” type connection profiles of the "HZ” system of PROFILARBED SA. that the maximum thickness of the thickness of material is preferably greater than the height of the bead, so that the bead is recessed relative to a bearing surface formed by the material thickness of the wing.
  • the wing bead must have a triangular section. However, it is not excluded to design connecting profiles requiring a connecting bead with another section.
  • At least one of the lower thickness wing tips has a corrugated longitudinal profile to directly form the connecting means.
  • a beam of this type can for example be easily integrated into a retaining curtain as described in the patent application. EP-A-0072118 .
  • the coupling means may also comprise a connecting section for a sheet pile which is welded end to end on a lateral face of one of the wing tips of smaller thickness.
  • a connecting section for a sheet pile can also be carried by a U-shaped section slid on one of the wing tips of lower thickness and fixed to this wing tip by means of two angular welds. This latter embodiment is not the subject of the claims.
  • the extra material thickness has a symmetry with respect to the median plane of the core.
  • the extra thickness of material on the wing is advantageously divided in two by a longitudinal groove extending above the core.
  • the ratio between the thickness of said wingtips and the thickness of the core is preferably between 1.0 and 1.7.
  • the ratio between the maximum thickness of the wing at the thickness of the material and the thickness of the wingtips is preferably between 1.5 and 4.0.
  • the ends of the garments will preferably have a thickness of between 10 mm and 25 mm. If the maximum thickness of a wing at the thickness of material is between 40 mm and 60 mm, it will most often be ensured that in a retaining wall the connections are arranged set back from the bearing surfaces. formed by the extra thicknesses of material.
  • the present invention is especially interesting for increasing the resistance modulus of a high beam, that is to say for which the ratio between the core height (H) and the wing width (B) is greater than 2, because it makes it possible to obtain a notable increase in its resistance modulus without any significant additional increase in its height.
  • a retaining wall according to claims 11 or 12 at least two beams according to the invention are connected at their wings with connecting profiles.
  • the thicknesses of material advantageously form bearing surfaces which define a support plane arranged in front of the connecting profiles (in other words, the connecting profiles are arranged set back with respect to the support plane defined by the extra thicknesses of wings material). A lierne can then bear directly on the bearing surfaces formed by the material thicknesses, without being hindered by the connecting profiles.
  • the Fig. 1 shows two beams 10, 10 'connected to each other.
  • a beam 10, 10 ' comprises a core 12, 12' and two wings 14, 16, 14 ', 16'.
  • the web 12, 12 ' supports the wings 14, 16, 14', 16 'so that the beam 10, 10' has a section in the form of a Roman numeral I, with a first plane of symmetry consisting of the median plane 11 of the core 12, 12 'and a second plane of symmetry 15 which is perpendicular to the median plane of the core 12, 12'.
  • the height H of the core 12, 12 ' is approximately twice the width B of the flange 14, 16, 14', 16 '.
  • the two beams are connected at their flanges 14, 16, 14 ', 16' using connection profiles 18 known per se, for example using HR fittings marketed by PROFILARBED S.A. (Luxembourg).
  • the wings 14, 16, 14 ', 16' comprise along each longitudinal edge a bead 20, 20 'of substantially triangular section.
  • the connecting section 18 is slid over these longitudinal edges of the wings 14, 16, 14 ', 16', so that the connecting beads 20 engage the lock chambers of the connectors 18. This method of connection is well known and is widely used for the construction of retaining curtains.
  • the broken lines 22, 22 ' represent the trace of the outer face of the wings of a conventional HZ beam produced by PROFILARBED SA (Luxembourg). It can be seen that in the new beams 10, 10 ', the two wings 14, 16, 14', 16 'are reinforced on the opposite side to the core by a material allowance 24, 26, 24', 26 'which starts only at a certain distance from the edges of the wing. At a certain distance d1 from the edge of the wing, the thickness of the wing gradually increases to reach a maximum value e * at a distance d2 from the edge (d1 ⁇ d2).
  • the thickness of the wing 14 then remains equal to e * up to a distance d2 from the opposite edge of the wing, and then decreases symmetrically with respect to the median plane of the core 12, 12 '.
  • the extra thicknesses of material 24, 26, 24 ', 26' thus leave wing tips 21, 21 'having substantially the same thickness e as the wings of a conventional HZ beam.
  • These ends of garlic 21 carry the connecting beads 20, respectively other connecting means (cf. Fig. 5 and 8 ).
  • the thickness e * is about twice the thickness e of the wingtips 21. In practice, this ratio can vary between 1.5 and 4.0.
  • a thickness e * of the order of 50 mm allows the extra thicknesses 24, 26, 24 ', 26' to define bearing surfaces 27, 29, 27 ', 29' located in front of the profiles. fitting 18.
  • a link 31 which bears on the bearing surfaces 29, 29 'without being hindered by the connecting sections 18 connecting the wings 26 and 26'.
  • the thickness e of garlic ends 21 is generally between 10 mm and 25 mm.
  • the ratio between the thickness of the ends of the garments 21 and the thickness of the core 12 is generally between 1.0 and 1.7.
  • the Fig. 2 shows how two pairs 30, 32 of these beams 10, 10 'can form with a pair 34 of sheet pile Z a mixed retaining wall.
  • Fittings profiles 36, 36 'adapted to connect the sheet piles 34 to the flanges of the beams 30, 32 are for example those marketed by PROFILARBED SA (Luxembourg) under the designation connection RZ-U, respectively RZ-D.
  • connection RZ-U connection marketed by PROFILARBED SA (Luxembourg) under the designation connection RZ-U, respectively RZ-D.
  • the Fig. 3 shows a schematic detail of a first execution of a wingtip of a beam.
  • the bead 20 has a height h which is smaller than the reinforced thickness e * of the flange 14.
  • the material allowance 24 begins with a ramp 40.
  • Fig. 4 the connections of the ramp 40 'and the bead 20 at the wing tip 21 are rounded, as is the connection of the ramp 40' to the bearing surface 27.
  • the Fig. 5 shows a wing tip 21 of a beam without connecting flange.
  • a connecting section 44 for a sheet pile is welded end to end on the lateral face of the wing tip 21. Note that the butt welding operation would be much more difficult if the wing tip 21 also had the thickness e *.
  • the Fig. 6 is a schematic detail showing the finishing of a connecting bead 20.
  • the connecting bead 20 At the outlet of the rolling mill, the connecting bead 20 has substantially the same height h * as the thickness e *.
  • a cutting torch 50 then gives the connecting bead 20 its final height h which is smaller than the thickness e * of the reinforced wing.
  • the Fig. 6 shows that the width b of the groove 40 must be such that the flame of the cutting torch 50 can not burn the oblique flank 52 of the excess thickness of material 24.
  • Fig. 7 differs from the execution of the Fig. 3 in that the thickness of material 24 is divided in two by a longitudinal groove 60 extending above the core 12. This longitudinal groove 60 facilitates the rolling of the beam because it allows better guidance of the beam in the rolling mill.
  • Fig. 8 differs from the execution of the Fig. 5 in that a sheet pile connection 70 is carried by a U-shaped section 72 which is slid over the wing tip 21. This U-shaped section 72 is then fastened to the wing tip 21 by means of two angular welds 74, 74 '.
  • the Fig. 9 present, as the Fig. 7 , an embodiment in which the thickness of material 24 is divided in two by a longitudinal groove 60 extending above the core 12. This embodiment is distinguished by curved connecting surfaces 80, 82.

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  • Engineering & Computer Science (AREA)
  • Structural Engineering (AREA)
  • Civil Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Mining & Mineral Resources (AREA)
  • Paleontology (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Curtains And Furnishings For Windows Or Doors (AREA)
  • Bulkheads Adapted To Foundation Construction (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Load-Bearing And Curtain Walls (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)
  • Impact Printers (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Floor Finish (AREA)

Abstract

The inventive girder (10) for a support wall curtain comprises a core (12) and two parallel wings (14, 16) which are supported by said core and provided with connection means (20). Said wings (14, 16) are reinforced on the largest part of the width thereof on the side opposite to the core (12) by an excessive material thickness which starts only at a certain distance (d1) from the longitudinal edges of the wing, thereby leaving the thinner wing ends (21) carrying said connection means (20) free. The non-reinforced ends (21) of the wings make it possible to use a conventional connection systems (18) in order to integrate such a girder (10) provided with a high resistant module into the support wall curtains.

Description

La présente invention concerne une poutrelle pour un rideau de soutènement et un rideau de soutènement comprenant de telles poutrelles.The present invention relates to a beam for a retaining curtain and a retaining curtain comprising such beams.

État de la techniqueState of the art

Des rideaux de soutènement formés, soit exclusivement de poutrelles soit de poutrelles et de palplanches, sont connus depuis longtemps. Ils ont l'avantage de présenter des modules de résistance très importants pour un poids surfacique avantageux. Les raccords entre deux poutrelles ou une poutrelle et une palplanche se font au niveau des bords des ailes des poutrelles.Retaining curtains formed, either exclusively of beams or beams and sheet piles, have been known for a long time. They have the advantage of presenting very important resistance modules for an advantageous surface weight. The connections between two beams or a beam and a sheet pile are made at the edges of the flanges of the beams.

PROFILARBED S.A. (Luxembourg) commercialise sous la désignation "HZ" un système intégré pour réaliser des rideaux de soutènement. Ce système intégré comprend des poutrelles spéciales, appelées poutrelles HZ. Le bord des ailes de ces poutrelles HZ se termine par un bourrelet de section sensiblement triangulaire, qui est en saillie par rapport à la surface extérieure de l'aile. Sur ce bord d'aile à bourrelet, on peut glisser un profilé de raccord de type RH ou de type RZ permettant d'y raccorder une autre poutrelle HZ ou une palplanche AZ.PROFILARBED S.A. (Luxembourg) sells under the designation "HZ" an integrated system for making retaining curtains. This integrated system includes special beams, called HZ beams. The edge of the wings of these beams HZ ends with a substantially triangular section bead, which is projecting relative to the outer surface of the wing. On this beaded wing edge, it is possible to slide a RH or RZ-type connection profile making it possible to connect another HZ beam or AZ sheet pile.

Il est également connu de déformer à froid les bords d'ailes de la poutrelle de façon à leur conférer un profil ondulé. Sur un tel bord ondulé, on peut alors glisser un profilé de raccord qui permet d'y raccorder soit un autre bord d'aile d'une poutrelle soit une griffe d'une palplanche. Un tel système est par exemple décrit dans la demande de brevet EP-A-0072118 .It is also known to cold deform the flange edges of the beam so as to give them a wavy profile. On such a corrugated edge, one can then slide a connecting section which allows to connect either another wing edge of a beam or a claw of a sheet pile. Such a system is for example described in the patent application EP-A-0072118 .

Il est aussi connu de souder des griffes de palplanches aux bords d'ailes de la poutrelle pour y raccorder des palplanches.It is also known to weld sheet pile claws to the flange edges of the beam to connect sheet piles.

Aujourd'hui, on a besoin de rideaux de soutènement avec des modules de résistance de plus en plus élevés. Un moyen pour augmenter sensiblement le module de résistance d'une poutrelle est d'augmenter la hauteur de son âme. Or, la hauteur maximale de l'âme de la poutrelle est bien entendu déterminée par la largeur du train de laminage. Par conséquent, pour laminer des poutrelles plus hautes, il faudrait construire de nouveaux trains de laminage plus larges. Un autre moyen pour augmenter le module de résistance des poutrelles est d'augmenter l'épaisseur de leurs ailes. Ceci impliquerait cependant de concevoir de nouveaux systèmes de raccord pour ailes épaisses.Today, we need retaining curtains with higher and higher resistance modules. One way to substantially increase the resistance module of a beam is to increase the height of its soul. However, the maximum height of the core of the beam is of course determined by the width of the rolling mill. Therefore, to laminate higher joists, new, larger rolling mills would have to be constructed. Another way to increase the resistance module of the beams is to increase the thickness of their wings. This would imply, however, the design of new thick wing fitting systems.

Un système de raccord pour des poutrelles avec ailes épaisses est connu du document DE 583 471 . Il s'agit de poutrelles de faible hauteur, la hauteur de l'âme étant égale à la largeur de l'aile, qui peuvent être montées dans le rideau de soutènement avec leur âme soit perpendiculaire soit parallèle à l'axe du rideau. Une aile de cette poutrelle comporte une rainure laminée ou usinée le long de chaque bord longitudinal dans la surface interne de l'aile et un palier laminé ou usiné dans le bord latéral de l'aile. La rainure et le palier permettent de raccorder les bouts d'ailes de deux poutrelles adjacentes à l'aide de profilés de raccords spéciaux et de raccorder une aile d'une première poutrelle transversalement entre les deux ailes d'une deuxième poutrelle. Il s'agit dès lors d'un système de raccord très spécial, qui a été conçu en 1927 pour une mise en oeuvre particulières de poutrelles de faible hauteur et qui n'a probablement jamais connu de succès.A connecting system for joists with thick wings is known from the document DE 583 471 . These are small joists, the height of the soul being equal to the width of the wing, which can be mounted in the retaining curtain with their soul either perpendicular or parallel to the axis of the curtain. A wing of this beam has a groove rolled or machined along each longitudinal edge in the inner surface of the wing and a bearing rolled or machined in the side edge of the wing. The groove and the bearing make it possible to connect the ends of the wings of two adjacent beams by means of special connector profiles and to connect a wing of a first beam transversely between the two wings of a second beam. It is therefore a very special connection system, which was designed in 1927 for a particular implementation of low joists and which has probably never been successful.

Le document US 4,550,582 considéré comme l'art antérieur le plus proche, décrit une méthode de laminage de poutrelles avec griffes pour rideau de soutènement. Lors du laminage on forme le long des bords d'aile des éléments de serrure complémentaires, pouvant s'enclencher de façon analogue aux raccords LARSEN connus pour les palplanches. Un premier type d'élément de serrure comprend un "doigt recourbé" et "un pouce" définissant une chambre de serrure. Un deuxième type d'élément de serrure comprend un bourrelet apte à être reçu dans la chambre de serrure. Le long de l'élément de serrure dudit deuxième type est agencée une projection à laquelle on attribue plusieurs fonctions. Une première fonction serait d'accroître la stabilité d'un empilage de poutrelles. La poutrelle allongée sur une aile repose en effet sur ladite projection et sur l'élément de serrure dudit premier type, qui a sensiblement la même hauteur que ladite projection. Une deuxième fonction serait de former un appui pour un élément de guidage lors de l'enfoncement d'une poutrelle dans le sol. Une troisième fonction serait d'équilibrer les sections transversales des ailes par rapport à l'âme. Enfin, on mentionne également que ladite projection augmenterait le module de section de la poutrelle. Cependant, le laminage de telles griffes et projections est une opération difficile et quasi impossible pour une poutrelle avec des ailes ayant une épaisseur de plus de 22 mm. De plus, la pratique devrait encore montrer si ce système de raccord nouveau fait ses preuves sur les chantiers.The document US 4,550,582 considered the closest prior art, describes a method of rolling beams with claws for retaining curtain. During lamination, additional locking elements are formed along the wing edges, which can be engaged similarly to known LARSEN fittings for sheet piles. A first type of lock member includes a "bent finger" and "an inch" defining a lock chamber. A second type of lock member comprises a bead adapted to be received in the lock chamber. Along the lock element of said second type is arranged a projection to which several functions are assigned. A first function would be to increase the stability of a stack of beams. The elongated beam on a wing rests indeed on said projection and on the lock element of said first type, which has substantially the same height as said projection. A second function would be to form a support for a guide element when driving a beam into the ground. A third function would be to balance the cross sections of the wings with respect to the soul. Finally, it is also mentioned that said projection would increase the section module of the beam. However, the rolling of such claws and projections is a difficult operation and almost impossible for a beam with wings having a thickness of more than 22 mm. In addition, the practice should still show if this new connection system is proving itself on construction sites.

Résumé de l'inventionSummary of the invention

Un objet de la présente invention est de proposer une poutrelle pouvant être aisément laminée avec un module de résistance plus élevé, sans devoir augmenter de façon notable sa hauteur, et dont la mise en oeuvre dans des rideaux de soutènement peut se faire en ayant recours à différentes systèmes de raccords qui ont fait leurs preuves sur les chantiers.An object of the present invention is to provide a beam that can be easily laminated with a higher resistance module, without having to increase its height significantly, and whose Installation in retaining curtains can be done using various connection systems that have proven themselves on construction sites.

Cet objet est atteint par une poutrelle pour rideaux de soutènement selon les revendications 1, 3 ou 4. Le renforcement des ailes par une surépaisseur de matière, localisée du côté opposé à l'âme, permet d'augmenter sensiblement le module de résistance de la poutrelle, sans augmentation notable de sa hauteur. Les bouts d'ailes non-renforcés, dont l'épaisseur est comparable à l'épaisseur d'aile d'une poutrelle classique pour rideaux de soutènement, permettent par contre d'utiliser quasi tous les systèmes de raccord connus pour l'intégration d'une poutrelle dans un rideau de soutènement.This object is achieved by a beam for retaining curtain according to claims 1, 3 or 4. The reinforcement of the wings by a material thickness, located on the opposite side to the core, allows to significantly increase the resistance module of the beam, without any notable increase in height. The non-reinforced wing tips, whose thickness is comparable to the wing thickness of a conventional beam for retaining curtains, allow on the other hand to use almost all connection systems known for the integration of a beam in a retaining curtain.

Dans une première exécution, les moyens de raccord portés par les bouts d'ailes comprennent un bourrelet de raccord. Une poutrelle de ce type peut par exemple être facilement intégrée dans un rideau de soutènement en utilisant des éléments de raccords comparables aux profilés de raccord de type "RH" ou de type "RZ" du système "HZ" de PROFILARBED S.A.. Il sera noté que l'épaisseur maximale de la surépaisseur de matière est de préférence supérieure à la hauteur du bourrelet, de façon à ce que le bourrelet soit en retrait par rapport à une surface d'appui formée par la surépaisseur de matière de l'aile. Reste à noter que pour les profilés de raccord de type "RH" ou de type "RZ", le bourrelet de l'aile doit avoir une section triangulaire. Il n'est cependant pas exclu de concevoir des profilés de raccord nécessitant un bourrelet de raccord avec une autre section.In a first embodiment, the connecting means carried by the wingtips comprise a connecting bead. For example, a beam of this type can be easily integrated into a retaining wall using connecting elements comparable to the "RH" or "RZ" type connection profiles of the "HZ" system of PROFILARBED SA. that the maximum thickness of the thickness of material is preferably greater than the height of the bead, so that the bead is recessed relative to a bearing surface formed by the material thickness of the wing. It should be noted that for "RH" type or "RZ" type connection profiles, the wing bead must have a triangular section. However, it is not excluded to design connecting profiles requiring a connecting bead with another section.

Dans une autre exécution, non couverte par les revendications, au moins un des bouts d'ailes d'épaisseur plus faible présente un profil longitudinal ondulé pour former directement le moyen de raccord. Une poutrelle de ce type peut par exemple être facilement intégrée dans un rideau de soutènement tel que décrit dans la demande de brevet EP-A-0072118 .In another embodiment, not covered by the claims, at least one of the lower thickness wing tips has a corrugated longitudinal profile to directly form the connecting means. A beam of this type can for example be easily integrated into a retaining curtain as described in the patent application. EP-A-0072118 .

Les moyens de raccord peuvent également comprendre un profilé de raccord pour une palplanche qui est soudé bout à bout sur une face latérale d'un des bouts d'ailes d'épaisseur plus faible. Un tel profilé de raccord pour une palplanche peut aussi être porté par un profilé en U glissé sur un des bouts d'ailes d'épaisseur plus faible et fixé à ce bout d'aile à l'aide de deux soudures angulaires. Cette dernière exécution ne fait pas l'objet des revendications.The coupling means may also comprise a connecting section for a sheet pile which is welded end to end on a lateral face of one of the wing tips of smaller thickness. Such a connecting section for a sheet pile can also be carried by a U-shaped section slid on one of the wing tips of lower thickness and fixed to this wing tip by means of two angular welds. This latter embodiment is not the subject of the claims.

De préférence, la surépaisseur de matière présente une symétrie par rapport au plan médian de l'âme. Pour faciliter le laminage de la poutrelle, la surépaisseur de matière sur l'aile est avantageusement divisée en deux par une gorge longitudinale s'étendant au dessus de l'âme.Preferably, the extra material thickness has a symmetry with respect to the median plane of the core. To facilitate the rolling of the beam, the extra thickness of material on the wing is advantageously divided in two by a longitudinal groove extending above the core.

Le rapport entre l'épaisseur desdits bouts d'ailes et l'épaisseur de l'âme est de préférence compris entre 1,0 et 1,7. Le rapport entre l'épaisseur maximale de l'aile au niveau de la surépaisseur de matière et l'épaisseur des bouts d'ailes est de préférence compris entre 1,5 et 4,0. Les bouts d'ailess auront de préférence une épaisseur comprise entre 10 mm et 25 mm. Si l'épaisseur maximale d'une aile au niveau de la surépaisseur de matière est comprise entre 40 mm et 60 mm, on pourra le plus souvent assurer que dans un rideau de soutènement les raccords soient agencés en retrait par rapport aux surfaces d'appui formées par les surépaisseurs de matière.The ratio between the thickness of said wingtips and the thickness of the core is preferably between 1.0 and 1.7. The ratio between the maximum thickness of the wing at the thickness of the material and the thickness of the wingtips is preferably between 1.5 and 4.0. The ends of the garments will preferably have a thickness of between 10 mm and 25 mm. If the maximum thickness of a wing at the thickness of material is between 40 mm and 60 mm, it will most often be ensured that in a retaining wall the connections are arranged set back from the bearing surfaces. formed by the extra thicknesses of material.

La présente invention est surtout intéressante pour augmenter le module de résistance d'une poutrelle haute, c'est-à-dire pour laquelle le rapport entre la hauteur d'âme (H) et la largeur d'aile (B) est supérieur à 2, car elle permet d'obtenir une augmentation notable de son module de résistance sans augmentation supplémentaire notable de sa hauteur.The present invention is especially interesting for increasing the resistance modulus of a high beam, that is to say for which the ratio between the core height (H) and the wing width (B) is greater than 2, because it makes it possible to obtain a notable increase in its resistance modulus without any significant additional increase in its height.

Dans un rideau de soutènement selonles revendications 11 ou 12, au moins deux poutrelles selon l'invention sont raccordées aux niveau de leurs ailes à l'aide de profilés de raccord. Les surépaisseurs de matière forment avantageusement des surface d'appui qui définissent un plan d'appui agencé devant les profilés de raccord (en d'autres termes, les profilés de raccord sont agencés en retrait par rapport au plan d'appui défini par les surépaisseurs de matière des ailes). Une lierne peut alors prendre directement appui sur les surfaces d'appui formées par les surépaisseurs de matière, sans être gênée par les profilés de raccord.In a retaining wall according to claims 11 or 12, at least two beams according to the invention are connected at their wings with connecting profiles. The thicknesses of material advantageously form bearing surfaces which define a support plane arranged in front of the connecting profiles (in other words, the connecting profiles are arranged set back with respect to the support plane defined by the extra thicknesses of wings material). A lierne can then bear directly on the bearing surfaces formed by the material thicknesses, without being hindered by the connecting profiles.

Brève description des dessinsBrief description of the drawings

Des exécutions avantageuses de la présente invention sont décrites sur base des dessins annexés, dans lesquels:

  • Fig. 1: est une vue d'une paire de poutrelles raccordées au niveau de leurs ailes adjacentes;
  • Fig. 2: est une vue d'un rideau de soutènement mixte comprenant deux paires de poutrelles selon la Fig. 1 et une paire de palplanches en forme de Z raccordant les deux paires de poutrelles;
  • Fig. 3: est un détail schématique d'une première exécution d'un bout d'aile d'une poutrelle;
  • Fig. 4: est un détail schématique d'une deuxième exécution d'un bout d'aile d'une poutrelle;
  • Fig. 5: est un détail schématique d'une troisième exécution d'un bout d'aile d'une poutrelle avec une griffe pour y raccorder une palplanche;
  • Fig. 6: est un détail schématique montrant le finissage d'un bout d'aile d'une poutrelle avec un bourrelet;
  • Fig. 7: est un détail schématique d'une variante de l'exécution de la Fig. 3;
  • Fig. 8: est un détail schématique non couvert par les revendications d'un bout d'aile d'une poutrelle avec un raccord soudé muni d'une griffe de palplanche;
  • etFig. 9: est un détail schématique d'une variante de l'exécution de la Fig. 3.
Advantageous embodiments of the present invention are described on the basis of the accompanying drawings, in which:
  • Fig. 1 : is a view of a pair of connected beams at their adjacent wings;
  • Fig. 2 : is a view of a mixed retaining curtain comprising two pairs of beams according to the Fig. 1 and a pair of Z-shaped sheet piles connecting the two pairs of beams;
  • Fig. 3 : is a schematic detail of a first execution of a wingtip of a beam;
  • Fig. 4 : is a schematic detail of a second execution of a wingtip of a beam;
  • Fig. 5 : is a schematic detail of a third execution of a wingtip of a beam with a claw to connect a sheet pile;
  • Fig. 6 : is a schematic detail showing the finishing of a wingtip of a beam with a bead;
  • Fig. 7 : is a schematic detail of a variant of the execution of the Fig. 3 ;
  • Fig. 8 : is a schematic detail not covered by the claims of a wingtip of a beam with a welded connection fitted with a sheet pile claw;
  • etFig. 9: is a schematic detail of a variant of the execution of the Fig. 3 .

Description d'une exécution préféréeDescription of a preferred execution

La Fig. 1 montre deux poutrelles 10, 10' raccordées entre elles. Une telle poutrelle 10, 10' comprend une âme 12, 12' et deux ailes 14, 16, 14', 16'. L'âme 12, 12' supporte les ailes 14, 16, 14', 16' de façon à ce que la poutrelle 10, 10' ait une section en forme d'un chiffre romain I, avec un premier plan de symétrie constitué par le plan médian 11 de l'âme 12, 12' et un deuxième plan de symétrie 15 qui est perpendiculaire au plan médian de l'âme 12, 12'. La hauteur H de l'âme 12, 12' est environ le double de la largeur B de l'aile 14, 16, 14', 16'.The Fig. 1 shows two beams 10, 10 'connected to each other. Such a beam 10, 10 'comprises a core 12, 12' and two wings 14, 16, 14 ', 16'. The web 12, 12 'supports the wings 14, 16, 14', 16 'so that the beam 10, 10' has a section in the form of a Roman numeral I, with a first plane of symmetry consisting of the median plane 11 of the core 12, 12 'and a second plane of symmetry 15 which is perpendicular to the median plane of the core 12, 12'. The height H of the core 12, 12 'is approximately twice the width B of the flange 14, 16, 14', 16 '.

Les deux poutrelles sont raccordées au niveau de leur ailes 14, 16, 14', 16' à l'aide de profilés de raccords 18 connus en soi, par exemple à l'aide de raccords RH commercialisés par PROFILARBED S.A. (Luxembourg). Les ailes 14, 16, 14', 16' comprennent le long de chaque bord longitudinal un bourrelet 20, 20' de section sensiblement triangulaire. Le profilé de raccord 18 est glissé sur ces bords longitudinaux des ailes 14, 16, 14', 16', de façon à ce que les bourrelets de raccord 20 engagent les chambres de serrure des raccords 18. Cette méthode de raccord est bien connue et est largement utilisée pour la construction de rideaux de soutènement.The two beams are connected at their flanges 14, 16, 14 ', 16' using connection profiles 18 known per se, for example using HR fittings marketed by PROFILARBED S.A. (Luxembourg). The wings 14, 16, 14 ', 16' comprise along each longitudinal edge a bead 20, 20 'of substantially triangular section. The connecting section 18 is slid over these longitudinal edges of the wings 14, 16, 14 ', 16', so that the connecting beads 20 engage the lock chambers of the connectors 18. This method of connection is well known and is widely used for the construction of retaining curtains.

Sur la Fig. 1, les lignes interrompues 22, 22' représentent la trace de la face externe des ailes d'une poutrelle HZ classique produite par PROFILARBED S.A. (Luxembourg). On voit que dans les nouvelles poutrelles 10, 10', les deux ailes 14, 16, 14', 16' sont renforcées du côté opposé à l'âme par une surépaisseur de matière 24, 26, 24', 26' qui commence uniquement à une certaine distance des bords de l'aile. A une certaine distance d1 du bord de l'aile, l'épaisseur de l'aile augmente graduellement pour atteindre une valeur maximale e* à une distance d2 du bord (d1 < d2). L'épaisseur de l'aile 14 reste alors égale à e* jusqu'à une distance d2 du bord opposé de l'aile, pour ensuite diminuer de façon symétrique par rapport au plan médian de l'âme 12, 12'. Les surépaisseurs de matière 24, 26, 24', 26' laissent ainsi subsister des bouts d'ailes 21, 21' ayant sensiblement la même épaisseur e que les ailes d'une poutrelle HZ classique. Ces bouts d'ailess 21 portent les bourrelets de raccord 20, respectivement d'autres moyens de raccords (c.f. Fig. 5 et 8). Dans l'exécution montrée, l'épaisseur e* est environ le double de l'épaisseur e des bouts d'ailes 21. En pratique, ce rapport peut varier entre 1,5 et 4,0. Il sera cependant noté qu'une épaisseur e* de l'ordre de 50 mm permet aux surépaisseurs 24, 26, 24', 26' de définir des surfaces d'appui 27, 29, 27', 29' situées devant les profils de raccord 18. Sur la Fig. 1, on voit ainsi une lierne 31 qui prend appui sur les surfaces d'appui 29, 29' sans être gênée par les profilés de raccord 18 reliant les ailes 26 et 26'. L'épaisseur e des bouts d'ailess 21 est généralement comprise entre 10 mm et 25 mm. Le rapport entre l'épaisseur e des bouts d'ailess 21 et l'épaisseur de l'âme 12 est généralement compris entre 1,0 et 1,7. Une nouvelle poutrelle 10, 10' peut facilement avoir un module de résistance qui est au moins 50% plus élevé que celui d'une poutrelle HZ classique équivalente.On the Fig. 1 , the broken lines 22, 22 'represent the trace of the outer face of the wings of a conventional HZ beam produced by PROFILARBED SA (Luxembourg). It can be seen that in the new beams 10, 10 ', the two wings 14, 16, 14', 16 'are reinforced on the opposite side to the core by a material allowance 24, 26, 24', 26 'which starts only at a certain distance from the edges of the wing. At a certain distance d1 from the edge of the wing, the thickness of the wing gradually increases to reach a maximum value e * at a distance d2 from the edge (d1 <d2). The thickness of the wing 14 then remains equal to e * up to a distance d2 from the opposite edge of the wing, and then decreases symmetrically with respect to the median plane of the core 12, 12 '. The extra thicknesses of material 24, 26, 24 ', 26' thus leave wing tips 21, 21 'having substantially the same thickness e as the wings of a conventional HZ beam. These ends of garlic 21 carry the connecting beads 20, respectively other connecting means (cf. Fig. 5 and 8 ). In the embodiment shown, the thickness e * is about twice the thickness e of the wingtips 21. In practice, this ratio can vary between 1.5 and 4.0. It will however be noted that a thickness e * of the order of 50 mm allows the extra thicknesses 24, 26, 24 ', 26' to define bearing surfaces 27, 29, 27 ', 29' located in front of the profiles. fitting 18. On the Fig. 1 , we thus see a link 31 which bears on the bearing surfaces 29, 29 'without being hindered by the connecting sections 18 connecting the wings 26 and 26'. The thickness e of garlic ends 21 is generally between 10 mm and 25 mm. The ratio between the thickness of the ends of the garments 21 and the thickness of the core 12 is generally between 1.0 and 1.7. A new beam 10, 10 'can easily have a resistance modulus which is at least 50% higher than that of an equivalent conventional HZ beam.

La Fig. 2 montre comment deux paires 30, 32 de ces poutrelles 10, 10' peuvent former avec une paire 34 de palplanches en Z un rideau de soutènement mixte. Des profilés de raccords 36, 36' aptes à raccorder les palplanches 34 aux ailes des poutrelles 30, 32 sont par exemple ceux commercialisés par PROFILARBED S.A. (Luxembourg) sous la désignation raccord RZ-U, respectivement RZ-D. On voit également que ces raccords sont tous légèrement en retrait par rapport aux surfaces d'appui formées par les surépaisseurs de matière sur les ailes des poutrelles.The Fig. 2 shows how two pairs 30, 32 of these beams 10, 10 'can form with a pair 34 of sheet pile Z a mixed retaining wall. Fittings profiles 36, 36 'adapted to connect the sheet piles 34 to the flanges of the beams 30, 32 are for example those marketed by PROFILARBED SA (Luxembourg) under the designation connection RZ-U, respectively RZ-D. We also see that these connections are all slightly set back from the bearing surfaces formed by the extra thickness of material on the flanges of the beams.

La Fig. 3 montre un détail schématique d'une première exécution d'un bout d'aile d'une poutrelle. On voit notamment que le bourrelet 20 a une hauteur h plus faible que l'épaisseur renforcée e* de l'aile 14. On constate aussi que la surépaisseur de matière 24 commence par une rampe 40. Sur la Fig. 4, les raccords de la rampe 40' et du bourrelet 20 au bout d'aile 21 sont arrondis, de même que le raccord de la rampe 40' à la surface d'appui 27.The Fig. 3 shows a schematic detail of a first execution of a wingtip of a beam. In particular, it can be seen that the bead 20 has a height h which is smaller than the reinforced thickness e * of the flange 14. It can also be seen that the material allowance 24 begins with a ramp 40. Fig. 4 , the connections of the ramp 40 'and the bead 20 at the wing tip 21 are rounded, as is the connection of the ramp 40' to the bearing surface 27.

La Fig. 5 montre un bout d'aile 21 d'une poutrelle sans bourrelet de raccord. Un profilé de raccord 44 pour une palplanche est soudé bout à bout sur la face latérale du bout d'aile 21. On remarquera que l'opération de soudage bout à bout serait beaucoup plus difficile si le bout d'aile 21 avait également l'épaisseur e*.The Fig. 5 shows a wing tip 21 of a beam without connecting flange. A connecting section 44 for a sheet pile is welded end to end on the lateral face of the wing tip 21. Note that the butt welding operation would be much more difficult if the wing tip 21 also had the thickness e *.

La Fig. 6 est un détail schématique montrant le finissage d'un bourrelet de raccord 20. A la sortie du laminoir, le bourrelet de raccord 20 a sensiblement la même hauteur h* que l'épaisseur e*. Un chalumeau coupeur 50 confère alors au bourrelet de raccord 20 sa hauteur finale h qui est plus petite que l'épaisseur e* de l'aile renforcée. La Fig. 6 montre que la largeur b de la gorge 40 doit être telle que la flamme du chalumeau coupeur 50 ne puisse pas brûler le flanc oblique 52 de la surépaisseur de matière 24.The Fig. 6 is a schematic detail showing the finishing of a connecting bead 20. At the outlet of the rolling mill, the connecting bead 20 has substantially the same height h * as the thickness e *. A cutting torch 50 then gives the connecting bead 20 its final height h which is smaller than the thickness e * of the reinforced wing. The Fig. 6 shows that the width b of the groove 40 must be such that the flame of the cutting torch 50 can not burn the oblique flank 52 of the excess thickness of material 24.

L'exécution de la Fig. 7 se distingue de l'exécution de la Fig. 3 en ce que la surépaisseur de matière 24 est divisée en deux par une gorge longitudinale 60 s'étendant au dessus de l'âme 12. Cette gorge longitudinale 60 facilite le laminage de la poutrelle parce qu'elle permet un meilleur guidage de la poutrelle dans le laminoir.The execution of Fig. 7 differs from the execution of the Fig. 3 in that the thickness of material 24 is divided in two by a longitudinal groove 60 extending above the core 12. This longitudinal groove 60 facilitates the rolling of the beam because it allows better guidance of the beam in the rolling mill.

L'exécution de la Fig. 8 se distingue de l'exécution de la Fig. 5 en ce qu'un raccord de palplanche 70 est porté par un profilé en U 72 qui est glissé sur le bout d'aile 21. Ce profilé en U 72 est alors fixé au bout d'aile 21 à l'aide de deux soudures angulaires 74, 74'.The execution of Fig. 8 differs from the execution of the Fig. 5 in that a sheet pile connection 70 is carried by a U-shaped section 72 which is slid over the wing tip 21. This U-shaped section 72 is then fastened to the wing tip 21 by means of two angular welds 74, 74 '.

La Fig. 9 présente, comme la Fig. 7, une exécution dans laquelle la surépaisseur de matière 24 est divisée en deux par une gorge longitudinale 60 s'étendant au dessus de l'âme 12. Cette exécution se distingue par des surfaces de raccord courbes 80, 82.The Fig. 9 present, as the Fig. 7 , an embodiment in which the thickness of material 24 is divided in two by a longitudinal groove 60 extending above the core 12. This embodiment is distinguished by curved connecting surfaces 80, 82.

Claims (13)

  1. A king pile for retaining walls comprising: (a) a rolled beam with a web (12) and two parallel flanges (14, 16) carried by the web (12), said flanges (14, 16) being fitted with connection means along their longitudinal edges, said connection means comprising a connection bulge (20) with a substantially triangular cross-section supported by one of said flange ends (21), and (b) a interlock section (18) slipped onto the longitudinal edge of the flange, in such a way that the connection bulge (20) engages a locking chamber of said interlock section (18); characterized in that said flanges (14, 16) are strengthened, on the side opposite the web (12) over the major part of their width (B), by an extra material thickness (24, 26), which starts only at a certain distance from the longitudinal edges of the flange (14, 16), allowing flange ends (21) of smaller thickness (e) to remain, which carry said connection bulge (20), said extra material thickness (24, 26) of the flange (14, 16) defining a bearing plane (27, 29) located in front of said interlock section (18) slipped onto said longitudinal edge of the flange (14, 16).
  2. The king pile as claimed in claim 1, wherein the maximum thickness (e*) of said extra material thickness (24, 26) is greater than the height of said bulge (20).
  3. A king pile for retaining walls comprising: (a) a rolled beam with a web (12) and two parallel flanges (14, 16) carried by the web (12); and (b) connection means along the longitudinal edges of said flanges (14, 16); characterized in that said flanges (14, 16) are strengthened, on the side opposite the web (12) over the major part of their width (B), by an extra material thickness (24, 26), which starts only at a certain distance from the longitudinal edges of the flange (14, 16), allowing flange ends (21) of smaller thickness (e) to remain, which carry said connection means (20, 44, 70), and said connection means comprise an interlock section (44) for a sheet pile that is welded end to end on a lateral face of one of said flange ends (21) of smaller thickness.
  4. A rolled king pile for retaining walls with a web (12) and two parallel flanges (14, 16) carried by the web (12), said flanges (14, 16) being fitted with connection means (20, 44, 70) along their longitudinal edges, characterized in that said flanges (14, 16) are strengthened, on the side opposite the web (12) over the major part of their width (B), by an extra material thickness (24, 26), which starts only at a certain distance from the longitudinal edges of the flange (14), allowing flange ends (21) of smaller thickness (e) to remain, which carry said connection means (20, 44, 70), and said extra material thickness (24) on a flange (14) is divided in two by a longitudinal groove (60) running above the web (12).
  5. The king pile as claimed in any one of the previous claims, wherein said extra material thickness (24, 26) is symmetrical about the midplane (11) of the web (12).
  6. The king pile as claimed in any one of the previous claims, wherein the ratio of the thickness (e) of said flange ends (21) to the thickness (s) of the web (12) is between 1.0 and 1.7.
  7. The king pile as claimed in any one of the previous claims, wherein the ratio of the maximum thickness (e*) of the flange (14, 16) at said extra material thickness (24, 26) to the thickness (e) of said flange ends (21) is between 1.5 and 4.0.
  8. The king pile as claimed in any one of the previous claims, wherein the thickness (e) of said flange ends (21) is between 10mm and 25mm.
  9. The king pile as claimed in any one of the previous claims, wherein the maximum thickness (e*) of the flange (14, 16) at said extra material thickness (24, 26) is between 40mm and 60mm.
  10. The king pile as claimed in any one of the previous claims, wherein the ratio of the web depth (H) to the flange width (B) is at least equal to 2.
  11. A retaining wall in which at least two king piles (10, 10') as claimed in any one of the previous claims are connected at their flanges (14, 16, 14', 16') by interlock sections (18), and said extra material thicknesses (24, 26, 24' , 26') form bearing surfaces (27, 29, 27', 29'), which define a bearing plane located in front of said interlock sections (18).
  12. A retaining wall in which at least two king piles (10, 10') are connected at their flanges (14, 16, 14', 16') by interlock sections (18), each of said king piles being a rolled beam with a web (12) and two parallel flanges (14, 16) carried by the web (12), said flanges (14, 16) being fitted with connection means (20, 44, 70) along their longitudinal edges, characterized in that said flanges (14, 16) are strengthened, on the side opposite the web (12) over the major part of their width (B), by an extra material thickness (24, 26), which starts only at a certain distance from the longitudinal edges of the flange (14), allowing flange ends (21) of smaller thickness (e) to remain, which carry said connection means (20, 44, 70), and said extra material thicknesses (24, 26, 24', 26') form bearing surfaces (27, 29, 27', 29'), which define a bearing plane located in front of said interlock sections (18).
  13. The retaining wall as claimed in claim 11 or 12, comprising at least one wale (31) bearing on said bearing surfaces (29, 29') formed by said extra material thicknesses (26, 26') in front of said interlock sections (18).
EP04817205.0A 2003-10-14 2004-10-14 Girder for a support wall curtain Expired - Lifetime EP1689939B2 (en)

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LU91043A LU91043B1 (en) 2003-10-14 2003-10-14 Beam for a retaining curtain.
PCT/EP2004/052549 WO2005038148A1 (en) 2003-10-14 2004-10-14 Girder for a support wall curtain

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USD808782S1 (en) * 2016-03-23 2018-01-30 Richard Heindl Connecting element for sheet piles
USD808783S1 (en) * 2016-03-23 2018-01-30 Richard Heindl Connecting element for sheet piles
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JP1735265S (en) 2021-10-04 2023-01-24 Connector for sheet pile
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JP1744188S (en) 2021-10-04 2023-05-16 Connector for sheet pile
JP1744187S (en) 2021-10-04 2023-05-16 Connector for sheet pile
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US20070077129A1 (en) 2007-04-05
LU91043B1 (en) 2005-04-15
EP1689939B1 (en) 2012-04-11
WO2005038148A1 (en) 2005-04-28
ATE553265T1 (en) 2012-04-15
ES2385039T3 (en) 2012-07-17
US7549823B2 (en) 2009-06-23
EP1689939A1 (en) 2006-08-16

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