EP2520733B1 - Dachrinnenbefestigungssystem, Dach mit dem Dachbefestigungssystem und entsprechende Anwendung - Google Patents

Dachrinnenbefestigungssystem, Dach mit dem Dachbefestigungssystem und entsprechende Anwendung Download PDF

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Publication number
EP2520733B1
EP2520733B1 EP12166359.5A EP12166359A EP2520733B1 EP 2520733 B1 EP2520733 B1 EP 2520733B1 EP 12166359 A EP12166359 A EP 12166359A EP 2520733 B1 EP2520733 B1 EP 2520733B1
Authority
EP
European Patent Office
Prior art keywords
attachment assembly
wing
gripping
clamping
wings
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.)
Not-in-force
Application number
EP12166359.5A
Other languages
English (en)
French (fr)
Other versions
EP2520733B8 (de
EP2520733A1 (de
Inventor
Jacques De Saint Gilles
Didier Salvan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Innovax
Original Assignee
Innovax
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Filing date
Publication date
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Publication of EP2520733A1 publication Critical patent/EP2520733A1/de
Application granted granted Critical
Publication of EP2520733B1 publication Critical patent/EP2520733B1/de
Publication of EP2520733B8 publication Critical patent/EP2520733B8/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04D—ROOF COVERINGS; SKY-LIGHTS; GUTTERS; ROOF-WORKING TOOLS
    • E04D13/00—Special arrangements or devices in connection with roof coverings; Protection against birds; Roof drainage ; Sky-lights
    • E04D13/04—Roof drainage; Drainage fittings in flat roofs, balconies or the like
    • E04D13/064—Gutters
    • E04D13/072—Hanging means
    • E04D13/0722—Hanging means extending mainly under the gutter

Definitions

  • the present invention relates to a fastening assembly according to the preamble of claim 1.
  • Prior art is known gutter fixing assemblies comprising a gutter holder having two wings.
  • the two wings are usually separate members and tightened to each other by means of a screw to secure the fastening assembly to the roof.
  • the object of the invention is to propose a fixing assembly for a gutter which is more economical.
  • Another object of the invention is to provide a gutter fastening assembly which allows a simple and fast attachment of the assembly on a roof, and this if possible by limiting or avoiding wear or damage to the roof.
  • the subject of the invention is a fastener assembly having the features of claim 1.
  • the invention may include one or more of the features set forth in the dependent claims.
  • the invention also relates to a roof comprising a roof element and a gutter hook, characterized in that the gutter hook is fixed to the roof element by means of a fastening assembly as described herein. -above.
  • the invention also relates to the use of the fixing assembly as described above, comprising the step of: bringing the fixing assembly into a clamping state of the covering element by pushing on the actuating surface which moves the actuating surface in translation towards the open side (CO) or a free edge.
  • FIG. 1 On the figure 1 is shown a roof 2 having a support member 4 and a gutter hook 6.
  • the figure 1 also shows a fixing assembly, designated by the general reference 8, adapted to fix the gutter hook 6 to the cover element 4.
  • the cover element 4 consists of, for example, a roof element, such as a corrugated cementitious alloy plate.
  • the cover member 4 may be a cover member such as a "steel tray” type sheet, or a composite plastic plate.
  • the cover element 4 has a free 4A edge.
  • the fastening assembly 8 comprises a gutter holder 10 having a profile portion 12 adapted to carry the hook of the gutter 6.
  • the gutter holder 10 also comprises an engagement portion 14 in which can engage the support element 4.
  • the fastening assembly 8 also comprises a clamping element 16 adapted to clamp the cover element 4 to or against the engagement portion 14.
  • This clamping element 16 is made in one piece or in one piece .
  • the fastening assembly 8 is provided with plating means 18 adapted to urge the clamping element 16 against the engagement portion 14 and against the covering element 4.
  • the engagement portion 14 has a first flange 20 and a second flange 22, which are located vis-à-vis, and a core 24 connecting the first and second flanges 20, 22.
  • Both wings 20, 22 define an open side CO which is a side opposite the web 24 and a side CA which is associated with the core 24. In the mounted state, the two wings 20, 22 are arranged on two sides opposite of the support member 4.
  • the fastening assembly 8 also defines an actuating direction D which is a direction extending from the open side CO to the side CA , and which extends substantially parallel to one or the other of the wings 20, 22.
  • the profile portion 12, the first flange 20, the core 24 and the second flange 22 are made in one piece and preferably in one piece.
  • One of the two wings 20, 22 is a clamping wing and the other of the wings 20, 22 is a support wing.
  • the clamping flange is the one against which the clamping member 16 squeezes the cover element 4 and which is in contact with this cover element 4.
  • the first wing 20 constitutes the clamping wing.
  • the support wing is the wing that is out of contact with the cover element 4 and is in this case the second wing 22.
  • the distance between the first flange 20 and the second flange 22 decreases going from the side CA side to the open side CO.
  • the first wing 20 is an intermediate wing, that is to say it lies between the core 24 and the profile portion 12, while the second wing 22 is a free wing that is to say it is adjacent to the core 24 and has a free end.
  • the plating means 18 comprises a cooperating cam surface 26 and counter cam surface 28. These two surfaces 26, 28 are adapted to urge the clamping element 16 against the cover element 4 during a relative displacement in translation between these two surfaces 26, 28.
  • the cam surface 26 is formed by the support flange, thus the second flange 22.
  • the camming surface 28 is formed by the surface of the clamping member 16 which is in contact with the wing 22.
  • the clamping element 16 and the second flange 22 are therefore adapted to urge the clamping element 16 against the cover element 4 by a relative displacement of the clamping element 16 with respect to the second flange 22 towards the side open CO.
  • the plating means 18 are self-locking thereby opposing release of the clamping member 16 only by friction between the cam surfaces 26 and camming surfaces 28 as well as between the clamping member 16 and the cam. cover element 4.
  • the clamping member 16 has a clamping surface that is in contact with the cover member 4. This clamping surface has grooves to generate a large frictional force for a given clamping force.
  • the fastener assembly includes an actuating surface 18A of the plating means 18, which is adapted to actuate the plating means 18 for clamping the support member 4.
  • a thrust force acting on this surface Actuation 18A in a direction directed from the side CA to the open side CO , moves the clamping member 16 relative to the second flange 22 towards the open side.
  • the fastener assembly 8 has a thrust projection 17 which is attached to the clamping member 16 and which forms a striking surface 17A.
  • the actuating surface 18A is in this case constituted by the striking surface 17A.
  • the thrust projection 17 extends on either side of the core 24 and is adapted to transmit a thrust force acting on the striking surface 17A to the clamping member 16.
  • the thrust protrusion 17 is a stem and extends especially through an opening in the core 24.
  • This embodiment is particularly simple and has few elements.
  • FIG 2 On the figure 2 is shown a second embodiment of a fastener assembly and a cover element 4.
  • the gutter 6 is omitted from the figure 1 .
  • the clamping element 16 is not in contact with the support wing, which is the second wing 22.
  • the plating means 18 comprise a plating element 30 which is a separate element from the clamping element 16 and which is adapted to urge the clamping element 16 towards the clamping flange, which is the first flange 20.
  • L plating element 30 is disposed between the first flange 20 and the second flange 22. The plating element 30 is in contact with the clamping element 16 and with the flange, which is the second flange 22.
  • the plating means 18 are adapted to urge the clamping member 16 toward the clamping wing by moving the plating member 30 toward the open side CO and moving this plating member 30 relative to the clamping member. 16 to the open side.
  • the plating member 30 carries the cam surface 26 and a flange surface 32.
  • the cam surface 26 is adapted to cooperate with the counter cam surface 28 of the clamp member 16, in such a way as to clamp the clamping member 16 against the cover member 4 as the plating member 30 moves from the core side CA to the open side CO , while holding the clamp member 16 stationary in the direction D extending from the open side to the soul side.
  • the two wings 20, 22 are parallel to each other in the direction extending from the open side to the soul side.
  • the cam surface 26 and camming surfaces 28 and the flange surface 32 are formed such that the plating means 18 is self-locking thereby frictionally opposing release of the clamping member 16. on the one hand, between the wing surface 32 and the support wing and, on the other hand, between the cam surface 26 and the counter cam surface 28.
  • the thrust projection 17 is attached to the plating element 30 and not to the clamping member 16.
  • the thrust projection 17 extends on either side of the core 24 and is adapted to transmit the thrust force acting on the striking surface 17A to the plating element 30.
  • the actuating surface 18A is adapted to actuate the plating means 18 to tightening the element 4 by a pushing force on this actuating surface 18A directed in a direction directed from the soul side towards the open side CO.
  • This embodiment operates as follows.
  • the cover element 4 is inserted between the first flange 20 and the support element 16. Then the plating element 30 is displaced in translation towards the open side CO with respect to the clamping element 16. the clamping member 16 is clamped against the cover member 4. During this movement, the support member 16 preferably remains stationary with respect to the wings 20, 22.
  • This embodiment particularly protects the surface of the cover element 4 and makes it possible to adjust the clamping force.
  • the fastening assembly 8 of the figure 2 which includes captive means 40 connecting the gutter holder 10, the clamping member 16 and, if appropriate, the veneer member 30 so as to oppose releasing or preventing release from others at least under the action of their own weight, and this regardless of the orientation of the fastening assembly 8 relative to the force of gravity.
  • the captive means 40 comprise a captive clip 42 covering the second flange 22 and holding the clamping member 16 relative to the gutter 10. The clip clip 42 opposes a release of the clip. clamping member 16, the plating member 30 under the effect of their own weight and regardless of the spatial position of the fastener assembly.
  • the figure 4 shows a third embodiment of a fastener assembly 8. This embodiment differs from the second embodiment only in the arrangement of the cover elements 4, plating 30 and clamping 16.
  • the clamping wing is the second wing 22 and the veneer wing is the first wing 20.
  • the cover element 4 is applied against the second wing 22 while the veneer element 30 applies against the first wing 20.
  • This embodiment is even easier to assemble since the clamping and cladding elements 30 are located lower than in the case of the embodiment of the invention. figure 2 .
  • the engagement portion 14 is made of a ribbed profile.
  • the distance between the first flange 20 and the second flange 22 increases going from the AC side to the open side CO.
  • the fastening assembly 8 comprises a clamp element 50.
  • This clamp element 50 comprises a clamping branch 52 forming the clamping element 16 and an interposed branch 54.
  • the clamping member 16 has a flaring shape extending from the core side CA to the open side CO.
  • the interposed branch extends between the second flange 22 and the cover element 4.
  • the two branches 52, 54 form a slot 56 for receiving the cover element 4.
  • the clamp element 50 also forms, at the bottom of the slot 56, a stop 58.
  • This stop 58 is adapted to oppose a displacement of the clamp element 50 with respect to the cover element 4 and this of the free edge 4A towards the current part of the cover element.
  • the clamping element 16 and the wings 20, 22 are therefore adapted to urge the clamping element 16 and the inserted branch 54 against the cover element 4 by a relative displacement in translation of the wings 20, 22 with respect to the clamp member 16 or clamp member 50 in a direction directed from the side CA to the open side CO.
  • the actuating surface 18A is constituted by the core 24.
  • the actuating surface 18A is adapted to actuate the plating means 18 to tighten the element 4 by a thrust force on this surface of actuation 18A directed in a direction directed from the soul side to the open side CO.
  • the clamp element 50 does not have a thrust projection 17.
  • the engagement portion 14 also comprises a guiding device, which is formed in particular by bridges on each side of the intermediate wing 20.
  • the captive means 40 is formed by a device for securing the clip 50 relative to the engagement portion 14.
  • This securing device is formed by a tab 60 cut in the central portion of the intermediate wing 20 and adapted to hook the gripper member 50 to make it movable relative to the engagement portion 14. This is shown in FIG. figure 6 .
  • the clip member 50 has a U-shaped profile open towards the flange 22.
  • the slot 56 is intended to receive a cover element 4.
  • the slot 56 has a flared shape towards the open side CO in the unsolicited state of the clamp element 50.
  • the slot 56 In the tight state of the element of FIG. clip 50, the slot 56 has a width that is constant over its entire length. Cutting of the slot 56 is designed to allow elasticity of the clip member around the cover member 4.
  • This embodiment is mounted as follows.
  • the fastening assembly 8 is slid over the cover member 4 so as to cover the free edge 4A and so that the clamp element 50, more precisely the clamping member 16 and the inserted branch 54 apply. on the support element 4.
  • the stop 58 is applied against the free edge 4A and prevents the clamp element 50 from moving relative to the cover element 4.
  • the core 24, and therefore the actuating surface 18A is moved relative to the clamp member 50 and relative to the cover member 4 toward the edge 4A, thereby squeezing the branches of the element clamp 50 against the cover element 4.
  • This embodiment is easy to manufacture, in particular by stamping, because of the flaring arrangement of the wings 20, 22 and the absence of the thrust projection. Also, the actuating surface 18 is relatively wide since it is formed by the core 24.
  • the fastening assembly 8 consists of 2 parts which brings, greater ease of use and economy of production.
  • the Figures 7 and 8 show clip elements 50 according to two variants.
  • the clip element 50 of the figure 7 is a clip member 50 which is particularly suitable for attachment to a cover member 4 which is a cement board.
  • the width of the slot 56 is between 7 and 9mm.
  • the clip element 50 of the figure 8 is particularly suitable for a cover element 4 which is a plastic plate.
  • the slot 56 has a width that is between 3 and 6mm.
  • the slot 56 has an increasing width from its origin to its open part.
  • the fastener assembly can therefore be used for roofs having cover elements of different materials. The operation remains the same, however.
  • the clamping member 16 carries a stop which is adapted to oppose a displacement of the clamping element 16 with respect to the cover element 4 and this of the free edge 4A towards the running part of the clamping element. blanket.
  • This stop is formed by a retaining nose projecting on the clamping element 16.
  • the clamping element 16 and the second flange 22 are also adapted to urge the clamping element 16 against the cover element 4 by a displacement relative translation in translation of the second flange 22 relative to the clamping element 16 towards the open side CO.
  • This variant is mounted as follows.
  • the fastening assembly 8 is slid over the cover member 4 so as to cover the free edge 4A and so that the second flange 22 and the clamping member 16 are applied to the support member 4.
  • the stop applies against the free edge 4A and prevents the clamping member 16 moves.
  • the second flange 22 is moved relative to the clamping member 16 and relative to the cover member 4 toward the edge 4A, thereby clamping the clamping member 16 against the cover member 4.
  • the invention may also relate to the following features:
  • the plating means comprises a plating member (30) which is adapted to bias the clamp member toward the clamping wing by moving the plating member in said direction towards the open side.
  • the assembly includes a collet (50) having a clamping limb (52), which forms the clamping member (16) and an interposed limb (54).
  • the two wings are parallel to each other in said direction.
  • the plating means comprise the support flange, and in that the distance between the two flanges (20,22) decreases going from the core side (CA) to the open side (CO).
  • the plating means (18) are self-locking means opposing by friction to a release of the clamping element.
  • the fastening assembly comprises captive means (40) connecting the gutter holder (10), the clamping element (16) and, if appropriate, the veneer element, such as so as to oppose a release from each other at least under the action of their own weight, and in particular regardless of the orientation with respect to the force of gravity.
  • the captive means (40) comprises a captive clip (42) covering one of the wings and retaining at least the clamping member (16).
  • Roof comprising a roof element (4) and a gutter hook (6), characterized in that the gutter hook is fixed to the roof element by means of a fixing assembly as defined above .
  • fastener assembly as defined above, comprising the step of: bringing the fastener assembly into a tightening state of the cover member by pushing on the moving actuating surface (18A) the operating surface (18A) in translation towards the open side (CO) or a free edge (4A).

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Roof Covering Using Slabs Or Stiff Sheets (AREA)

Claims (9)

  1. Befestigungseinheit für einen Dachrinnenhalter der Art, die Folgendes umfasst:
    - einen Dachrinnenhalter (10), der einerseits einen Profilabschnitt (12) aufweist, der ausgelegt ist, um den Dachrinnenhalter (6) zu tragen, und andererseits einen Eingriffsabschnitt (14), in den ein Abdeckelement (4) eingreifen kann,
    wobei der Eingriffsabschnitt (14) zwei Flügel (20, 22) aufweist, darunter einen Spannflügel und einen Stützflügel, und einen Steg (24), der die zwei Flügel miteinander verbindet, wobei die zwei Flügel eine offene Seite (CO) definieren, die dem Steg gegenüber liegt, und eine Stegseite (CA), die mit dem Steg assoziiert ist,
    - ein Spannelement (16), das ausgelegt ist, um das Abdeckelement auf oder gegen den Spannflügel zu spannen,
    wobei die Befestigungseinheit Verkleidungsmittel (18) umfasst, die ausgelegt sind, um das Spannelement (16) auf den Spannflügel hin zu belasten, indem mindestens einer der Flügel (20, 22) mit Bezug auf das Spannelement (16) hin zur offenen Seite (CO) verschoben wird, wobei die Befestigungseinheit eine Betätigungsfläche (18A) des Verkleidungsmittels (18) umfasst, die ausgelegt ist, um die Verkleidungsmittel zu betätigen, um das Abdeckelement (4) durch Drücken in einer Richtung zu spannen, die von der Stegseite (CA) hin zur offenen Seite (CO) gerichtet ist, wobei die Einheit ein Zangenelement (50) umfasst, das einen Spannarm (52) aufweist, der das Spannelement (16) bildet, und einen verzahnten Arm (54) dadurch gekennzeichnet, dass der Spannarm und der verzahnte Arm einen Schlitz (56) zur Aufnahme des Abdeckelements (4) bilden.
  2. Befestigungseinheit nach Anspruch 1, dadurch gekennzeichnet, dass das Zangenelement (50) am Boden des Schlitzes (56) einen Anschlag (58) bildet.
  3. Befestigungseinheit nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass sich der verzahnte Arm (54) zwischen einem zweiten Flügel und dem Abdeckelement erstreckt, und dadurch, dass der zweite Flügel der Stützflügel (22) ist.
  4. Befestigungseinheit nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Verkleidungselemente (18) selbstsperrende Mittel sind, die sich durch Reibung einer Freisetzung des Spannelements entgegensetzen.
  5. Befestigungseinheit nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Befestigungseinheit Verlustsicherungsmittel (40) umfasst, die den Dachrinnenhalter (10), das Spannelement (16) und gegebenenfalls das Verkleidungsmittel derart miteinander verbinden, dass sie sich einer Freisetzung der einen von den anderen mindestens unter der Einwirkung ihres eigenen Gewichts entgegensetzen, und insbesondere unabhängig von der Ausrichtung mit Bezug auf die Schwerkraft.
  6. Befestigungseinheit nach Anspruch 5, dadurch gekennzeichnet, dass die Verlustsicherungsmittel (40) eine Verlustsicherungsklammer (40) umfassen, die einen der Flügel abdeckt und mindestens eine Spannelement (16) zurückhält.
  7. Befestigungseinheit nach Anspruch 5, dadurch gekennzeichnet, dass die Befestigungseinheit aus zwei Stücken besteht.
  8. Dach, umfassend ein Dachelement (4) und einen Dachrinnenhalter (6), dadurch gekennzeichnet, dass der Dachrinnenhalter an das Dachelement mit Hilfe einer Befestigungseinheit nach einem der vorhergehenden Ansprüche befestigt ist.
  9. Verwendung der Befestigungseinheit nach einem der Ansprüche 1 bis 7, umfassend den Folgenden Schritt: Bringen der Befestigungseinheit in einen Spannungszustand des Abdeckelements durch Drücken auf die Betätigungsfläche (18A), wodurch die Betätigungsfläche (18A) in Translation hin zur offenen Seite (CO) oder eine freie Schmalkante (4A) verschoben wird.
EP20120166359 2011-05-02 2012-05-02 Dachrinnenbefestigungssystem, Dach mit dem Dachbefestigungssystem und entsprechende Anwendung Not-in-force EP2520733B8 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1153739A FR2974828B1 (fr) 2011-05-02 2011-05-02 Ensemble de fixation de gouttiere, toit et utilisation correspondants

Publications (3)

Publication Number Publication Date
EP2520733A1 EP2520733A1 (de) 2012-11-07
EP2520733B1 true EP2520733B1 (de) 2013-11-20
EP2520733B8 EP2520733B8 (de) 2013-12-25

Family

ID=46001028

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20120166359 Not-in-force EP2520733B8 (de) 2011-05-02 2012-05-02 Dachrinnenbefestigungssystem, Dach mit dem Dachbefestigungssystem und entsprechende Anwendung

Country Status (3)

Country Link
EP (1) EP2520733B8 (de)
ES (1) ES2448421T3 (de)
FR (1) FR2974828B1 (de)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE643198A (de) *
FR1548560A (de) * 1967-10-24 1968-12-06
FR2134840A5 (de) * 1971-04-22 1972-12-08 Vadot Rene
FR2416316A1 (fr) * 1978-02-06 1979-08-31 Ninin Plismy Sa Anc Ets Support de gouttiere universel
EP1087072A1 (de) * 1999-09-21 2001-03-28 Ets Frenehard Et Michaux S.A. Dachrinnenklemme
FR2906283A1 (fr) * 2006-09-22 2008-03-28 Philippe Paul Girault Dispositif de maintien en suspension d'un element de gouttiere sur une toiture

Also Published As

Publication number Publication date
ES2448421T3 (es) 2014-03-13
FR2974828B1 (fr) 2014-02-07
EP2520733B8 (de) 2013-12-25
FR2974828A1 (fr) 2012-11-09
EP2520733A1 (de) 2012-11-07

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