EP2923022B1 - Rahmen - Google Patents

Rahmen Download PDF

Info

Publication number
EP2923022B1
EP2923022B1 EP13801472.5A EP13801472A EP2923022B1 EP 2923022 B1 EP2923022 B1 EP 2923022B1 EP 13801472 A EP13801472 A EP 13801472A EP 2923022 B1 EP2923022 B1 EP 2923022B1
Authority
EP
European Patent Office
Prior art keywords
wing
casing
frame
internal
coupling
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
EP13801472.5A
Other languages
English (en)
French (fr)
Other versions
EP2923022A1 (de
Inventor
Giuseppe VESCA
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.)
Serrametal Srl
Original Assignee
Serrametal Srl
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Serrametal Srl filed Critical Serrametal Srl
Publication of EP2923022A1 publication Critical patent/EP2923022A1/de
Application granted granted Critical
Publication of EP2923022B1 publication Critical patent/EP2923022B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/04—Wing frames not characterised by the manner of movement
    • E06B3/263—Frames with special provision for insulation
    • E06B3/26343—Frames with special provision for insulation with two or more separate insulating zones alternating with metal section members
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/30—Coverings, e.g. protecting against weather, for decorative purposes
    • E06B3/301—Coverings, e.g. protecting against weather, for decorative purposes consisting of prefabricated profiled members or glass
    • E06B3/303—Covering metal or plastic frames with wooden profiled members
    • E06B3/304—Covering metal or plastic frames with wooden profiled members the frames consist of two metal section members with insulating zone in between
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/30—Coverings, e.g. protecting against weather, for decorative purposes
    • E06B3/308—Wing frames covered on the outside by a rigidly-mounted outer frame
    • E—FIXED CONSTRUCTIONS
    • E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
    • E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
    • E06B3/00—Window sashes, door leaves, or like elements for closing wall or like openings; Layout of fixed or moving closures, e.g. windows in wall or like openings; Features of rigidly-mounted outer frames relating to the mounting of wing frames
    • E06B3/54—Fixing of glass panes or like plates
    • E06B3/5427—Fixing of glass panes or like plates the panes mounted flush with the surrounding frame or with the surrounding panes

Definitions

  • the present invention relates to a frame according to the features of the pre-characterizing part of claim 1.
  • frame is intended to designate the set of a casing and of a wing applied on the casing itself, being “casing" the fixed frame of the frame that is applied to the opening of a building and is suitable for the assembly of a movable wing with respect to the casing for opening and closing the opening of the building, being “wing” the movable part of the frame which is movable with respect to the casing according to opening directions that may be, by only way of example but not limited to the purposes of the present invention, cross-sectional opening and closing directions as in the case of sliding doors, tilted opening and closing directions as in the case of pivot-hung frames, opening and closing directions with rotation of the wing as regards to a lateral or intermediate hinging line as in the case of doors, windows, skylights, etc., or combinations of the above-mentioned opening movements as in the case of wings which may be selectively opened by means of sliding or by means of pivot-hung opening or in the case of wings which may be selectively opened by lateral hinging rotation or by
  • wing is intended to indicate the movable part of the frame which can take different shapes, as, only by way of example but not limited to the purposes of the present invention, doors and windows.
  • frame is intended to designate a set of the four perimeter elements that are mutually fixed one after the other to form a perimeter, generally quadrangular structure, but that can also have other shapes, e.g. triangular, trapezoidal, circular, elliptic shapes that are to be included within then present invention.
  • the word "frame” can be either referred to the perimeter structure of the casing or of the wing.
  • both the casing or fixed frame of the frame and the wing or movable frame usually consist of perimeter elements, generally four elongated perimeter elements composing two stanchions and two cross-pieces.
  • the perimeter elements are mutually fixed one after the other to form a perimeter structure which is generally quadrangular, but that can also have other shapes e.g. triangular, trapezoidal, circular, elliptic or more complex shapes.
  • the mutual connection of each of the perimeter elements constitutes a frame that is applied in a fixed way within an opening of a wall of a building, where the wing of the frame will be placed.
  • the mutual connection of the perimeter elements constitutes a frame defining an internal space suitable for placing a glass herein or, generally, a closing panel for the internal space delimited by the frame of the wing.
  • the end of each perimeter element is cut to 45° in order to be connected to the corresponding end of the adjacent perimeter element, also cut to 45°.
  • the mutual connection of the perimeter elements can be performed according to various methods, known for the purposes of the present invention, as, for example, sticking, fixing with screws, coupling angle devices, etc.
  • Such obtained frames can be aesthetically unattractive and, therefore, they are successively covered with finishing elements that may be applied both on the internal side of the frame, i.e. the one inwardly facing the building, and on the external side the frame, i.e. the one outwardly facing the building.
  • thermo-insulating materials for example polystyrene or polyurethane foams, and/or by providing suitable gaskets between the wing or movable part and the casing or fixed frame of the frame.
  • suitable thermo-insulating materials for example polystyrene or polyurethane foams
  • gaskets between the wing or movable part and the casing or fixed frame of the frame.
  • composite structures are used wherein the frame consists of various elements some of which are metallic elements acting as structural support and other elements are made of insulating materials as to eliminate any thermal bridges.
  • Patent WO 00/50722 describes a three element set of section bars for frames in which a first central plastic section constituting the central part of the frame is connected, outwardly facing the frame, to a metallic section while, inwardly facing the inside the frame, to one or more wooden laths or to one or more metallic, plastic or other material sections.
  • the central plastic section has a tubular section and both the central plastic section and the external metallic section can have the same cross profile either for the wing or the casing.
  • the mutual fixing of sections is performed by connecting notches protruding from coupling fins which are able to firmly clamp within the corresponding channel insertion adapted to internally house said notches by means of grooves throughout the length of the sections thereof.
  • Coupling by means of notches and insertion channels extends throughout the entire length of the sections and, though allowing a pressure insertion of a section onto the other, the uncoupling does not to occur by pulling a section orthogonally with respect to the other but it requires to longitudinally slide a section with respect to the other throughout the entire length of the same until uncoupling is completed.
  • the internal cover can also be fitted to the insulating section by means of snap fitting.
  • Patent EP 0 657 612 describes a set of section bars for frames based on the use of two elements provided with protrusions and recesses mutually staggered in order to allow mutual pressure coupling with provision for axial movement to allow dismounting thereof.
  • Patent WO 01/69027 describes a frame wherein using a single section bar, having two opposite sides with shapes that are respectively intended to house a sheet of glass and upon installation of hardware and gasket, frames or door and window casings are produced, such that both the fixed frame or case and the perimeter framework of the wings are made from portions of the section itself.
  • the casing includes additional section bars adapted to reciprocally couple in order to form the frame and further specific sections which, therefore, are not the same as other sections used in the frame, said further sections are intended to create the central pillar in the two-wing windows or the perimeter rabbet sections.
  • the number of sections to be assembled becomes significant as it is necessary to provide at least one supporting structural section for the frame of the casing, at least one insulating element towards the external side of the casing, at least one insulating element towards the internal side of the casing, at least one external finishing element of the casing, at least one internal finishing element of the casing, at least one supporting structural section for the frame of the wing, at least one insulating element towards the external side of the wing, at least one insulating element towards the internal side of the wing, at least one external finishing element of the wing, at least one internal finishing element of the wing.
  • thermal bridges causing thermal dispersion e.g. those corresponding to the internal structure of the wing or the internal structure of the casing, which is fixed to the wall of the building at the opening obtained from the wall itself.
  • the aim of this invention is to provide a frame consisting of at least one wing and a corresponding casing allowing a reduction in the number of perimeter elements necessary to complete the frame of the wing and the frame of the casing.
  • Further aim of the present invention is to provide a composite structure for each frame allowing a reduction of thermal bridges in the frame.
  • the solution according to the present invention allows achieving a consistent reduction in the number of perimeter elements needed to complete the frame of the wing and the frame of the casing.
  • This will advantageously involve both the cost of production of the frame, which will be less expensive, as each single component will cost less, and the cost for warehouse management, either for the manufacturer of section bars and for the final dealer, as well as for the window and door fitter performing the final assembly.
  • the solution according to the present invention advantageously allows achieving a better efficiency from the point of view of reduction of thermal bridges in the frame.
  • An additional advantage of the solution, according to the present invention is that it allows easy customization of both the internal and external finishing elements of the frame, which can also be advantageously assembled on the frame upon the assembly of the frame when installing it in the building, as they could also be easily and readily subsequently replaced.
  • the structure according to the present invention also enables to integrate anti-burglary features suitable to prevent tampering of frames by unauthorized parties.
  • the solution according to the present invention simplifies installation procedures thereby reducing installation time.
  • the frame (1) consists of a casing (2) or fixed frame, of at least a wing (3) or movable frame and of hardware elements (4) interconnecting the casing (2) and the wing (3).
  • Each frame (1) on a same casing (2) or fixed frame may have one or more wings (3).
  • the hardware elements (4) can include hinges or, generally, interconnecting means allowing different movements of the wing e.g.
  • opening directions may be, by only way of example and without limitation for the purposes of the present invention, cross-sectional opening and closing directions as in the case of sliding doors, tilted opening and closing directions as in the case of pivot-hung frames, opening and closing directions with rotation of the wing as regards to an intermediate or side hinging line as in the case of doors, windows, skylights, etc., or combinations of the above-mentioned opening movements as in the case of wings which may be selectively opened by means of sliding or by means of pivot-hung opening or in the case of wings which may be selectively opened by lateral hinging rotation or by means of pivot-hung opening.
  • the corresponding frames generally consists of a set of four perimeter elements and are mutually fixed one after the other to form a perimeter structure which is generally a quadrangular structure, but which can also have other shapes e.g. triangular, trapezoidal, circular, elliptic shapes, that are included within the present invention.
  • Mutual connection of the perimeter elements can be performed according to various methods known for the purposes of the present invention, as for example sticking, fixing with screws, angle coupling devices, etc.
  • the mutual connection of the perimeter elements will form a frame that is fixedly applied within the opening of a wall in a building and that constitutes the housing for the installation of the wing (3) of the frame.
  • the mutual connection of the perimeter elements will form a frame defining an internal space adapted for the application herein of a panel or a glass (23) closing the internal space defined by the frame of the wing thereof.
  • the wing (3) may either include a panel or a glass (23) closing the multitude defined by the frame of the wing (3) thereof.
  • the frame (1) according to the present invention effectively optimizes various perimeter elements constituting the frame of the casing (2) and of the wing (3), through a careful and synergic design of the casing (2) and the wing (3), according to an inventive structure which now is not available on the market and which advantageously allows achieving a high reduction of manufacturing costs and management costs of warehouses where the several components have to be stored.
  • the solution according to the present invention provides the realization of section bars constituting the perimeter elements of the frame of casing (2) and wing (3) that are characterized by a wide versatility, allowing the use of same section bars both on the frame of the casing (2) and on the frame of the wing (3).
  • the inventive structure includes three main perimeter elements that are used for the construction both of the frame of the casing (2) and for the construction of the frame of the wing (3).
  • the frame of the casing (2) includes:
  • the frame of the wing (3) includes:
  • the connecting element (10, 16) is in the form of extruded aluminium or steel.
  • the insulating element (8, 20) is an insulating material, a particularly special synthetic resins, developed for the specific application.
  • the fixing means (11, 15) is an insulating material, a particularly special synthetic resins, developed for the specific application.
  • the casing (2) includes a connecting element of the casing (10) provided, at the surface facing the insulating element of the casing (8), with interlocking connecting means consisting of a range of protrusions (27) and recesses (28) mutually and correspondingly coupling to a range of recesses (28) and protrusions (27) on the insulating element of the casing (8) at the surface facing the connecting element of the casing (10).
  • the connecting element of the casing (10) is provided with a first insertion site (29) equipped with notched coupling means (30) to house the fixing means on the casing (11) on a reciprocal engaging condition, said fixing means being inserted within the first insertion site (29) and remains locked in said site due to the engaging action practiced by the notched coupling means (30) on the fixing means on the casing (11) thereof.
  • the wing (3) consists of a connecting element of the wing (16) provided, at the surface facing the insulating element of the wing (20), with interlocking connecting means consisting of a range of protrusions (27) and recesses (28) mutually and correspondingly coupling to a range of recesses (28) and protrusions (27) on the insulating element of the wing (20) at the surface facing the connecting element of the wing (16).
  • the connecting element of the wing (16) is provided with a first insertion site (29) equipped with notched coupling means (30) to house the fixing means on the wing (15) on a reciprocal engaging condition, said fixing means being inserted within the first insertion site (29) and remains locked in said site due to the engaging action practiced by the notched coupling means (30) on the fixing means on the wing (15) thereof.
  • This solution advantageously provides a supporting structure which is totally insulated both from external environment and internal environment, with significant benefits for thermal insulation of the frame (1).
  • aluminium section bars are extruded in aluminium alloy 6060 UNI 9006/1 T5, suitable for furnace painting with polyester powders or electrocolouring (oxidation).
  • the external and internal finishing section bars can be of various materials, as it will be explained in the following description. Thanks to a detailed research on section bars and a deep design analysis, glasses with various thickness and of different kind, according to the insulating degree required as well as cover panels in the case of frames that are not equipped with glass, can be inserted.
  • the insulating element (8, 20) is a continuous perimeter insulating element going along the whole perimeter of the frame both on the frame of the casing (2) and the frame of the wing (3). Detailed studies provided said continuous profile section consisting of synthetic resins, which were designed and developed for the specific application providing a section bar with optimal thermal insulation while showing an excellent stability thereof.
  • Synthetic resins can be inserted in the frame according to customers requests and specific features related to certain requirements e.g. thermal insulation properties to be achieved, presence of humidity, etc.
  • resins can be easily separated from others materials on the frame due to the dismounting readiness thereof.
  • dismounting of the frame for the removal of resins and their replacement with other resins having different features would be provided.
  • the casing (2) it comprises an external finishing element (7) which is secured by screws (13) on the insulating element of the casing (8).
  • the fixing is made by means of screws that are accessible only when the wing (3) is in an opened condition, so that the external finishing element (7) provides both an aesthetic customizable cover element and a securing anti-burglary element, meaning that when the wing (3) is in a closed condition, the external finishing element (7) blocks the access to the fixing screws (13) allowing access to the internal structure of the frame (1).
  • the external finishing elements (7) also constitutes the rabbet element of the panel or glass (23) of the wing (3), which, in a closing condition of the wing (3), abuts on the external finishing element (7) interposing itself between a first rabbet gasket (5). Consequently, the external finishing element (7) acts as rabbet element for closing the wing and as supporting element of the sealing gasket.
  • a second rabbet gasket (6) completes insulation between the external and internal side of the frame (1), more precisely a second rabbet gasket (6) preferably shuts and seals the openings between the peripherally external portion of the frame of the wing (3) and the peripherally internal portion of the frame of the casing (2).
  • said second gasket of rabbet (6) is fixed on the frame of the casing (2) corresponding to the site of a groove undercut insertion perimeter internally obtained on the frame of the casing (2) thereof, and particularly corresponding to the insulating element of the casing (8), said second rabbet gasket (6) protruding from the frame of the casing (2) towards the direction facing the wing (3) in order to contact the perimeter end of the wing (3) when the latter is in a closing condition.
  • the casing (2) includes an internal coating (12), which is coupled and fastened on the fixing means on the casing (11).
  • the fixing means on the casing (11) delimits a second insertion site (31) equipped with coupling means (30) notched to house the internal coating (12) in mutual engaging condition, which is advantageously inserted within the second insertion site (31) and remains locked in this site due to the engaging effect exerted by the coupling means (30) notched on the fixing means, exerting a sealing force on the internal coating (12) itself.
  • Such coupling method also helps achieving high insulating performance for the frame (1).
  • the casing (3) can also be provided with a perimeter gasket (9) constituting insulating and sealing means of the opening of the building within which the frame (1) is inserted, said frame (1) being yet integrated, on its peripherically external surface, with sealing means avoiding openings between the frame and the insertion space of the building, that can cause airflow from the inside to the outside of the building and vice-versa.
  • a perimeter gasket (9) constituting insulating and sealing means of the opening of the building within which the frame (1) is inserted, said frame (1) being yet integrated, on its peripherically external surface, with sealing means avoiding openings between the frame and the insertion space of the building, that can cause airflow from the inside to the outside of the building and vice-versa.
  • the panel or glass (23) is inserted within a hollow peripherally defined inside the frame of the wing (3) from a surface of the insulating element of the wing (20) and is locked in position by a glazing bead element (21) provided with a protection gasket (22).
  • the glazing bead element (21) is fixed on the insulating element of the wing (20) by means of screws (13).
  • the glazing bead element (21) in this case, only has an aesthetic function for the elements and not a sealing function. In this case as well, the adopted solution allows the removal of thermal bridges as the panel or glass (23) comes into contact only with thermally insulating elements preventing the contact with thermally conductive elements.
  • Assembly is completed by injecting a sealing compound (25) in the gap between the panel or glass (23) and the insulating element of the wing (20).
  • the screws (13) fixing the glazing bead element (21) are protected by a screw-cover element (24).
  • the screw-cover element (24) is advantageously secured by jointly coupling the screw heads and/or the protruding elements of the insulating element of the wing (20), consequently constituting an aesthetic covering element that could be customizable and easily replaceable.
  • the wing (3) includes a finishing internal covering (17) which can also be realized with multiple parts, e.g. by coupling a first covering element (18) to a second covering element (19).
  • fixing means on wing (15) delimits a second insertion site (31) provided with coupling means (30) notched to house in mutual engaging condition the internal covering (17), which is advantageously inserted within the second insertion site (31) and remains blocked in this site due to the engaging effect exerted by the coupling means (30) notched on the fixing means, exerting a sealing force on the internal covering (17) itself.
  • the finishing internal covering (17) consists of two parts, i.e. a first covering element (18) and a second covering element (19), being the first covering element (18) coupled and fastened on the fixing means on the wing (15) by means of the above-described coupling system and being the second covering element (19) locked:
  • all the finishing elements both of the casing (2) and of the wing (3) are easily removable and replaceable elements.
  • This solution is advantageous in many respects. Firstly, it provides frames (1) ready to be assembled allowing the end-user to choose the kind of finishings, which may be chosen even at the last minute, for example before or during the assembly of the frame, also allowing the end-user to choose the finishings upon the final assembly to verify the aesthetic effect obtained in combination with other architectonic elements on the building.
  • the assembly operations of the frame are simplified since all the fastening elements are fully accessible before the following implementation of finishings.
  • the solution provides easy maintenance of the frame; for example, in the case of wood finishings, the only finishings in wood will be easily removed in order to proceed with the removal of old paint and repainting of the finishings, thereof.
  • it also allows a fast, simple, economic and easy replacement of desired finishing elements of the frames (1) at any time, to modify both external and internal aesthetics of the building, and to replace any damaged materials. It is therefore possible to achieve high flexibility in the production of section bars; in their assembling when producing frames of casing (2) and wing (3) and in the installation of the frame (1), providing a lower cost supply of customized products and a.personal service according to the needs of each customer.
  • the external and internal finishing elements (7, 12, 17, 24) can be in wood, plastic, aluminium, steel or any other lining, with no change on the main structure of the frame (1).
  • an "overcoat” consisting of material different from the insulating and supporting structure is applied to the elements of the frame both of the casing (2) and of the wing (3), said overcoat hiding the structural and insulating elements.
  • These finishing elements can be mounted on construction, actually allowing the end-user to choose the type of finishing at a later stage.
  • Hooking of the external and internal finishing elements (7, 12, 17, 24) can be done by means of the shown coupling with the fixing means (11, 15), which can be a plastic extruded or a special fixing small block.
  • the system is versatile and fits present and/or future needs of the client such as change of finishings, enhanced thermal and acoustic insulation, armor plating.
  • dismounting of sections thanks to the described systems of jointly mutual coupling also allows maximizing the use of segments of material thereof, which can also be reused.
  • odd portions from the insulating element (8, 20) can be longitudinally coupled for the creation of further frames, thus minimizing waste production.
  • the wing (3) also includes a third rabbet gasket (14) placed at the coupling surface between the wing (3) and the casing (2) when the wing is in a closed position.
  • the third rabbet gasket (14) is fixed on the internal covering (17) of the wing (3) and is pressed against the internal coating (12) of the casing (2) to seal the perimeter profile of the wing (3) when it is in a closing condition. It will be apparent, however, that this gasket can be also placed according to different installation solutions, provided that it is a perimeter sealing element of the coupling edge in abutment between the wing (3) and the casing (2).
  • the external finishing element (7) when the wing (3) is closed, internally creates a gap (33) between the external finishing element (7) itself and the wing (3), said gap being subject to condensation of moisture phenomena due to the air herein.
  • the external finishing element (7) is equipped with bores (26) allowing possible condensation to flow, at least on the perimeter side of the frame (1) which is a downwardly facing perimeter side, i.e. towards the ground.
  • the high insulating performance of the frame (1) achieved by mutual coupling mechanisms with no thermal bridges and by studying and developing innovative solutions from the point of view of employed materials, together with the synergic choice of suitable sections shapes to be used both for the realization of the frame of the casing (2) and for the realization of the frame of the wing (3), have also resulted in a reduction of the overall size of the frame (1), by reducing the size of individual section bars of the composite structure forming it, being favourable for lightness, ease of assembly and installation and the overall costs of the product.
  • the internal covering (17) and the internal lining can be realized in many different materials according to preferences, e.g. solid wood or the like.
  • the frame of the casing (2) and of the wing (3) is constituted of a core made by an aluminium pipe with structural function, i.e. the connecting element (10, 16), and by a special plastic extruded profile having a thermal bridge function, i.e. the insulating element (8, 20), joined to each other by means of a stable mechanical hooking assured by roll-forming of the corresponding sections.
  • Gaskets (5, 6, 14, 22) are preferably made of high quality elastomers with limited and simple geometric shapes whilst ensuring high technical performance.
  • the frame (1) according to the present invention can provide multiple openings of the wing, according to known solutions, for the purposes of the present invention.
  • Exemplary, opening mechanisms with side hinged wing, orthogonally opening with respect to the wall, such as transom-window, bottom-hinged wing, horizontally moving and side-scrolling wing, can be provided.
  • the connecting element (10, 16) may have section size within 20 mm and 40 mm in height, preferably approximately 30 mm and within 20 mm and 50 mm in width, preferably approximately 36 mm.
  • the insulating element (8, 20) may have section size within 30 mm and 60 mm in height, preferably approximately 35 mm and within 20 mm and 60 mm in width, preferably approximately 30 mm.
  • the glass (23) or the panel can have a thickness within 24 and 36 mm.
  • the present invention relates to a frame (1) made up of a casing (2) comprising first perimeter elements (8, 10, 11) obtained from first elongated section components and made up of at least one wing (3) comprising second perimeter elements (20, 16, 15) obtained from second elongated section components, wherein the casing (2) is adapted to be inserted within an opening obtained on a wall or on a roof of a building and wherein the wing (3) can be selectively opened and closed on the first perimeter elements (8, 10, 11) of the casing (2) and further wherein the first perimeter elements (8, 10, 11) of the casing (2) include at least two section bars being identical in section to the section of two section bars corresponding to the second perimeter elements (20, 16,15) of the at least one wing (3).
  • the first perimeter elements (8, 10, 11) of the casing (2) include three section bars being identical in section to the section of the three section bars corresponding to the second perimeter elements (20, 16, 15) of the at least one wing (3).
  • Sections bars being identical in section include interlocking coupling means (27, 28, 30) mutually engaging the at least two perimeter elements selected among the first perimeter elements (8, 10, 11) and the second perimeter elements (20, 16, 15).
  • the present invention ( Fig. 1 , Fig. 2 , Fig. 3 , Fig. 4 , Fig. 5 ) relates to a frame (1) made up of a casing (2) and of at least one wing (3).
  • the terms "at least one wing” are to be indented as that the frame (1) may include a single wing as well as two or more wings.
  • the casing (2) is adapted to be inserted within an opening obtained on a wall or on a roof of a building.
  • the casing (2) includes a plurality of first perimeter elements (8, 10, 11) obtained from first elongated section bar components, said first perimeter elements (8, 10, 11) forming a first framework defining a first inner surface where the at least one wing (3) has to be applied.
  • the at least one wing (3) includes a plurality of second perimeter elements (20, 16, 15) obtained from second elongated section bar components, said perimeter second elements (20, 16,15) forming a second framework defining a second inner surface.
  • the at least one wing (3) is adapted to be applied on the casing (2) by means of hardware elements (4) suitable to allow mutual engaging of the wing (3) and the casing (2), said engaging enabling the movement of the wing (3) with respect to the casing (2) at least in two positions:
  • the first elongated section bar components forming the first perimeter elements (8, 10, 11) of the casing (2) are identical to the second elongated section bar components forming the second perimeter elements (20, 16, 15) of the at least one wing (3), said first perimeter elements (8, 10, 11) including first elements being identical in section to second elements of the second perimeter elements (20, 16, 15).
  • the first elongated section bar components forming the first perimeter elements (8, 10, 11) of the casing (2) include at least one elongated section bar component constituting a connecting element of the casing (10) and the second elongated section bar components forming the second perimeter elements (20, 16, 15) of the at least one wing (3) include at least one elongated section bar component constituting a connecting element of the at least one wing (16), said elongated section bar constituting this connecting element of the casing (10) being it identical to the elongated section bar constituting this connecting element of the at least one wing (16), in a sense that said elongated section bars are identical in section being them obtained from the same section bar, constituting a connecting element (10, 16) being it obtained from a section bar shared by the casing (2) and the at least one wing (3).
  • the first elongated section bar components forming the first perimeter elements (8, 10, 11) of the casing (2) include at least one elongated section bar component constituting an insulating element of the casing (8) and the second elongated section bar components forming the second perimeter elements (20, 16, 15) of the at least one wing (3) include at least one elongated section bar component constituting an insulating piece of the at least one wing (20), the elongated section bar constituting this insulating element of the casing (8) being identical to the elongated section bar constituting this insulating element of the at least one wing (20), in a sense that said elongated section bars are identical in section being them obtained from the same section bar, constituting an insulating element (8, 20) being it obtained from a section bar shared by the casing (2) and the at least one wing (3).
  • the first elongated section bar components forming the first perimeter elements (8, 10, 11) of the casing (2) include at least one elongated section bar component constituting a fixing means on the casing (11).
  • the second elongated section bar components forming the second perimeter elements (20, 16, 15) of the at least one wing (3) include at least one elongated section bar component constituting a fixing means on the wing (15).
  • the elongated section bar constituting this fixing means on the casing (11) is identical to the elongated section bar constituting the fixing means on the wing (15), in a sense that said elongated section bars are identical in section being them obtained from the same section bar, constituting a fixing means (11, 15) being it an element obtained from a section bar shared by the casing (2) and the at least one wing (3).
  • the frame structures of the casing (2) and the wing (3) are obtained from identical section bar elements (8, 10, 11), consistently decreasing the amount of section bars required for the production of the frame (1).
  • the insulating element of the casing (8) and the insulating element of the at least one wing (20) are shaped in section according to an essentially quadrangular shape.
  • the connecting element of the casing (10) and the connecting element of the at least one wing (16) are shaped in section according to an essentially quadrangular shape.
  • the insulating element of the casing (8) is able to couple with the connecting element of the casing (10) and similarly the insulating element of the at least one wing (20) is able to couple with the connecting element of the at least one wing (16).
  • Mutual coupling of the insulating element of the casing (8) and the connecting element of the casing (10) and mutual coupling of the insulating element of the at least one wing (20) and connecting element of the at least one wing (16) occurs by means of a series of recesses (28) with undercut shape and protrusions (27) having an essentially complementary form in respect to said undercut shape with a base side being shorter than an end side with a section form essentially corresponding to a triangle trunk.
  • Recesses (28) extend longitudinally with respect to the length of the section bar from which they are obtained.
  • Protrusions (27) extend longitudinally with respect to the length of the section bar from which they are obtained.
  • Each protrusion (27) is adapted to be inserted within a corresponding recess (28) with mutual locking achieved by coupling the triangle trunk shape of the protrusion (27) with the undercut shape of the recess (28). It will be readily understood that a greater number of protrusions or recesses than those depicted, as well as different forms for mutual coupling, can be provided.
  • the connecting element (10, 16) further includes a first insertion site (29) essentially "C" shaped which is open at one side near a first opening (34) and is delimited at the opposite side, with respect to the first opening (34), by a rabbet bottom from where two mutually parallel arms (36) extend, delimiting this essentially "C” shape.
  • the first insertion site (29) is adapted for the insertion of the fixing means (11, 15). Fixing the fixing means (11, 15) within the first insertion site (29) is performed by means of coupling means (30) on the arms (36) in the form of coupling notches engaging the coupling surface between the arms (36) and the fixing means (11, 15).
  • the fixing means (11, 15) constitutes a coupling interface between the connecting element (10, 16) and the finishing element constituting the internal coverings (12, 17) of an internal side of the frame (1), being internal referred with respect to the building on which the frame (1) is mounted, with internal meaning the side of the frame (1) facing the interior.
  • the connecting element (10, 16) is formed from elongated section bar components of aluminium or steel and the insulating element (8, 10) is formed from elongated section bar components of insulating material, preferably plastic material.
  • Coupling between the connecting element (10, 16) and the insulating element (8, 10) constitutes an insulating coupling suitable for the elimination of thermal bridges between the internal side and an external side of the frame (1), internal being referred with respect to the building on which the frame (1) is mounted, with internal meaning the side of the frame (1) facing the interior; external being referred to the opposite side of the frame (1) with respect to the internal side, i.e. the side of the frame (1) facing the outside the building.
  • the fixing means (11, 15) is formed from elongated section bar components of insulating material, preferably of plastic material. Coupling between the connecting element (10, 16) and the fixing means (11, 15) constitutes an insulating coupling suitable for the elimination of thermal bridges between the internal side and the external side of the frame (1), internal being referred with respect to the building on which the frame (1) is mounted, with internal meaning the side of the frame (1) facing the interior; external being referred to the opposite side of the frame (1) with respect to the internal side, i.e. the side of the frame (1) facing the outside of the building.
  • the internal coverings (12, 17) include a first internal covering (12) adapted to be fixed on the connecting element of the casing (10) by means of first fixing means (11) of these fixing means (11, 15).
  • the internal coverings (12, 17) further include a second internal covering (17) suitable to be fixed on the connecting element of the at least one wing (16) by means of second fixing means (15) of these fixing means (11, 15).
  • the internal coverings (12, 17) form easy to be interchanged finishing elements, in a sense that mutual fixing between internal coverings (12, 17) and the fixing means (11, 15) allows a fast removal of internal coverings (12, 17) for their replacement and/or maintenance.
  • the mutual fixing between the internal coverings (12, 17) and the fixing means (11,15) is performed by means of an insertion block (37) protruding from the internal coverings (12, 17) at the coupling surface with the fixing means (11, 15).
  • the insertion block (37) is preferably an integral part of the coverings, being directly formed on the same.
  • the insertion block (37) is adapted to be inserted within a second insertion site (31) obtained on the fixing means (11, 15).
  • the second insertion site (31) is essentially "C" shaped and is open at one side near a second opening (39) being delimited at the opposite side, with respect to this second opening (39), by a rabbet bottom from where two mutually parallel arms (36) extend, delimiting the essentially "C” shape.
  • the fixing of the internal coverings (12, 17) within this first insertion site (29) is done by means of:
  • the internal coverings (12, 17) consists of a material selected from the group consisting of wood, plastic, aluminium, steel or equivalent other materials, as required for the customization of the frame (1).
  • the second internal covering (17) preferably consists of a first element (18) and of a second element (19) in which the first element (18) constitutes the coupling interface with the connecting element of the at least one wing (16) to fix this second internal covering (17) and where the second element (19) is fixed with interlocking between the first element (18) and a standstill element (39) protruding from the insulating element of the at least one wing (20).
  • the frame includes at least one connecting element of the casing (10) or at least one connecting element of said at least one wing (16).
  • This connecting element (10,16) includes a first insertion site (29) essentially "C" shaped which is delimited by two arms (36).
  • the first insertion site (29) is adapted for inserting insertion blocks (37) obtained on internal coverings (12, 17) forming finishing elements of an internal side of the frame (1), internal being referred with respect to the building on which said frame (1) is mounted, with internal meaning the side of the frame (1) facing the interior. Fixing of internal coverings (12, 17) is performed by means of coupling notches (30) on the arms (36).
  • the coupling notches (30) engage on a surface coupling the insertion blocks (37) or the fixing means (11, 15) of the internal coverings (12, 17).
  • the surface coupling the insertion blocks (37) or the fixing means (11, 15) is ( Fig. 1 , Fig. 2 , Fig, 3 ) an essentially smooth coupling surface with no coupling recesses with said coupling notches (30) therefore achieving an easily releasable coupling interface.
  • the internal coverings (12, 17) form easy to be interchanged finishing elements, in a sense that mutual fixing between the internal coverings (12, 17) and the first insertion site (29) allows a fast removal of said internal coverings (12,17) for their replacement and/or maintenance.
  • the frame (1) includes on the at least one wing (3) a glass or a closing panel (23) that is applied to the second frame defining the second internal surface of the at least one wing (3), i.e. it closes the space delimited by the frame constituting the wing (3).
  • the glass or the panel (23) is fixed on the at least one wing (3) by means of a glazing bead element (21) by interposing a protection gasket (22), said glazing bead element (21) being fixed on the insulating element of the wing (20) by means of screws (13).
  • the frame (1) will include a sealing product (25) injected in the gap between the panel or glass (23) and the insulating element of the wing (20).
  • a screw-cover element (24) is provided, which is fixed in an interlocking manner to the screw heads (13), said screw-cover element (24) constituting an easy to be interchanged finishing element, in a sense that the mutual fixing of this screw-cover element (24) allows a fast removal of the screw-cover element (24) for its replacement and/or maintenance.
  • the frame (1) includes an external finishing element (7) which is secured by screws (13) to the insulating element of the casing (8), said screws (13) being located near an enclosed gap (33) between the at least one wing (3) and the casing (2).
  • the screws (13) are accessible only when the at least one wing (3) is in an open condition with respect to the casing (2), so that the external finishing element (7) constitutes both an easily replaceable cover element, and a security anti-burglary element.
  • the external finishing element (7) constitutes also a rabbet element of the panel or glass (23) when the at least one wing (3) is in a closing position with respect to the casing (2), with interposing a first rabbet gasket (5).
  • the external finishing element (7) includes a second rabbet gasket (6) at the coupling surface between the external finishing element (7) and the insulating element of the wing (20), this second rabbet gasket (6) being suitable to seal, together with the first rabbet gasket (5), the enclosed gap (33) between the at least one.wing (3) and the casing (2), when the wing (3) is in a closing position with respect to the casing (2).
  • the casing (3) also includes a perimeter gasket (9) adapted as insulating and sealing means of the coupling interface between the frame (1) and the internal walls of the opening of the building within which the frame (1) itself is inserted.
  • the perimeter gasket (9) constitutes a sealing mean integrated in the frame (1) for sealing the perimeter surface of the insertion space of the building, this solution overall improving the insulating performance of the frame (1).
  • the perimeter gasket (9) is fixed on the casing (3) by interlocking a coupling protrusion of the perimeter gasket (9) within a second opening (35) formed on the connecting element of the casing (10) at the coupling interface between the casing and the space located on the wall of the building and within which the casing (3) itself is inserted.
  • the wing (3) can be for example from the group consisting of sliding and/or bottom-hinged wing and/or side-hinged wing, single wing, double wing.

Landscapes

  • Engineering & Computer Science (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Wing Frames And Configurations (AREA)
  • Building Environments (AREA)
  • Window Of Vehicle (AREA)
  • Glass Compositions (AREA)

Claims (16)

  1. Rahmen (1) bestehend aus einem Gehäuse (2) mit ersten Umfangselementen (8, 10, 11) aus ersten verlängerten Profilstabteilen und gebildet von mindestens einem Flügel (3) mit zweiten Umfangselementen (20, 16, 15) aus zweiten verlängerten Profilstabteilen, wobei das Gehäuse (2) geeignet ist, in eine Öffnung an einer Wand oder auf einem Dach eines Gebäudes eingefügt zu werden, wobei der mindestens eine Flügel (3) auf den ersten Umfangselementen (8, 10, 11) des Gehäuses (2) selektiv zu öffnen und verschließbar ist, wobei die ersten Umfangselemente (8, 10, 11) des Gehäuses (2) mindestens zwei Profilstäbe umfassen, mit identischem Querschnitt wie der Querschnitt von zwei entsprechenden Profilstäben der zweiten Umfangselemente (20, 16, 15) des mindestens eines Flügels (3), wobei der Rahmen (1) mindestens ein Verbindungselement des Gehäuses (10) umfasst und mindestens ein Verbindungselement des mindestens einen Flügels (16), wobei das Verbindungselement (10, 16) eine erste Einsatzstelle (29) umfasst, die im wesentlichen "C"-förmig ist und von zwei Armen (36) abgegrenzt ist, wobei die erste Einsatzstelle (29) zum Einfügen von Einsatzblöcken (37) angepasst ist, die auf inneren Abdeckungen (12, 17) erhalten werden, wobei die zweiten Umfangselemente (20, 16, 15) mindestens ein verlängertes Profilstabteil umfassen, das ein Isolierelement (20) für den mindestens einen Flügel bildet, wobei das Verbindungselement des Gehäuses (10) ein verlängertes Profilstabteil ist und das Verbindungselement des mindestens eines Flügels (16) ein verlängertes Profilstabteil ist, wobei der verlängerte Profilstab, der das Verbindungselement des Gehäuses (10) bildet, derselbe ist wie der verlängerte Profilstab, der das Verbindungselement des mindestens eines Flügels (16) bildet, so dass besagte verlängerte Profilstäbe den gleichen Querschnitt haben, da sie aus denselben Profilstäben gebildet sind, und so ein Verbindungselement (10, 16) bilden, das aus einem Profilstab erhalten wird und von den Gehäuse (2) und dem mindestens einen Flügel (3) geteilt wird, wobei die ersten verlängerten Profilstabteile aus den ersten Umfangselementen (8, 10, 11) des Gehäuses (2) gebildet werden, einschließlich mindestens eines verlängerten Profilstabteils, das ein Isolierelement des Gehäuses (8) bildet, und die zweiten verlängerten Profilstabteile aus den zweiten Umfangselementen (20, 16, 15) des mindestens eines Flügels (3) gebildet werden, umfassen mindestens besagtes verlängertes Profilstabteil, das besagtes Isolierelement (20) des mindestens einen Flügels bildet, wobei die verlängerten Profilstäbe, die das Isolierelement des Gehäuses (8) bilden, gleich den verlängerten Profilstäben sind, die das Isolierelement des mindestens einen Flügels (20) bilden, so dass besagte verlängerte Profilstäbe den gleichen Querschnitt haben, da sie von demselben Profilstab herrühren, zur Bildung eines Isolierelements (8,20), das von einem Profilstab erhalten wird, der von dem Gehäuse (2) und dem mindestens einen Flügel (3) geteilt wird, und wobei weiter der mindestens eine Flügel (3) eine Glasscheibe oder Platte (23) umfasst, die auf dem mindestens einen Flügel (3) aufgebracht wird,
    wobei die Glasscheibe oder Platte (23) auf dem mindestens einen Flügel (3) mittels eines Glashalteleistenelements (21) befestigt ist, mit einer Schutzdichtung (22) dazwischen, wobei das Glashalteleistenelement (21) auf dem Isolierelement (20) des Flügels mittels Schrauben (13) befestigt ist und die Platte oder Glasscheibe (23) in einen Hohlraum eingefügt wird, der peripher in dem Rahmen des Flügels (3) definiert ist, von einer Oberfläche des Isolierelements (20) des Flügels her, und von dem Glashalteleistenelement (21) verriegelt wird, wobei die inneren Abdeckungen (12, 17) Ausbauelemente einer Innenseite des Rahmens (1) bilden, wobei sich "innere" auf das Gebäude bezieht, auf das der Rahmen (1) montiert wird, wobei "innere" die Seite des Rahmens (1) bedeutet, die dem Innern zugewandt ist, wobei die Befestigung der inneren Abdeckungen (12, 17) mittels Kupplungsrasten (30) auf den Armen (36) durchgeführt wird, wobei die Kupplungsrasten (30) auf einer Oberfläche eingreifen, die die Einsatzblöcke (37) der inneren Abdeckungen (12, 17) koppelt, wobei die Oberfläche, die die Einsatzblöcke (37) verbindet, eine im wesentlichen glatte Kupplungsfläche ist, ohne Kupplungsvertiefungen mit besagten Kupplungsrasten (30), so dass eine leicht lösbare Kupplungsschnittstelle entsteht, wobei die inneren Abdeckungen (12, 17) leicht austauschbare Ausbauelemente bilden, so dass die gegenseitige Befestigung zwischen den inneren Abdeckungen (12, 17) und der ersten Einsatzstelle (29) eine schnelle Entfernung der inneren Abdeckungen (12, 17) für deren Austausch und/oder Wartung gestattet, wobei die Befestigung der inneren Abdeckungen (12, 17) in der ersten Einsatzstelle (29), die im wesentlichen "C" förmig ist, durch Dazwischenlegen eines Befestigungsmittels (11,1 5) durchgeführt wird, während die Befestigung des Befestigungsmittels (11, 15) in der ersten Einsatzstelle (29) mittels der Kupplungsrasten (30) auf den Armen (36) erfolgt, wobei das Befestigungsmittel (11, 15) eine Kupplungsschnittstelle zwischen dem Verbindungselement (10, 16) und den inneren Abdeckungen (12,17) bildet.
  2. Rahmen (1) nach Anspruch 1, gekennzeichnet dadurch, dass die ersten Umfangselemente (8, 10, 11) des Gehäuses (2) drei Profilstäbe umfassen, die identisch im Querschnitt mit dem Querschnitt von drei entsprechenden Profilstäben der zweiten Umfangselemente (20, 16, 15) des mindestens eines Flügels (3) sind.
  3. Rahmen (1) nach einem beliebigen der vorhergehenden Ansprüche, gekennzeichnet dadurch, dass die Profilstäbe, die identisch im Querschnitt sind, ineinandergreifende Kupplungsmittel (27, 28, 30) zum gegenseitigen Eingreifen zwischen mindestens zwei Umfangselemente umfassen, die unter den ersten Umfangselementen (8, 10, 11) und den zweiten Umfangselementen (20, 16, 15) ausgewählt werden.
  4. Rahmen (1) nach einem beliebigen der vorigen Ansprüche, gekennzeichnet dadurch, dass die ersten Umfangselemente (8, 10, 11) eine erste Rahmenfassung bilden, die eine erste Innenfläche definiert, durch Anbringung des besagten mindestens einen Flügels (3), und die zweiten Umfangselemente (20, 16, 15) eine zweite Rahmenfassung bilden, die eine zweite Innenfläche definiert, wobei besagter mindestens ein Flügel (3) geeignet ist, auf dem Gehäuse (2) mittels Hardwareelemente (4) angebracht zu werden, die das gegenseitige Eingreifen des Flügels (3) und des Gehäuses (2) gestatten, wobei der Eingriff eine Bewegung des Flügels (3) im Vergleich zu dem Gehäuse (2) in mindestens zwei Positionen gestattet, wobei in der ersten Position der Flügel (3) in Anschlagzustand auf dem Gehäuse (2) ist, mit Schließung der ersten Innenfläche, die von der ersten Rahmenfassung des Gehäuses (2) definiert wird, wobei in der zweiten Position der Flügel (3) zumindest teilweise beabstandet von der ersten Rahmenfassung des Gehäuses (2) ist, mit entsprechender mindestens teilweiser Öffnung der ersten Innenfläche, die von der ersten Rahmenfassung des Gehäuses (2) definiert wird, wobei die ersten verlängerten Profilstabteile von den ersten Umfangselementen (8, 10, 11) des Gehäuses (2) gebildet werden, die identisch mit den zweiten verlängerten Profilstabteilen sind, die von den zweiten Umfangselementen (20, 16, 15) des mindestens eines Flügels (3) gebildet werden, wobei die ersten Umfangselemente (8, 10, 11) erste Elemente umfassen, die im Querschnitt identisch mit zweiten Elementen der zweiten Umfangselemente (20, 16, 15) sind.
  5. Rahmen (1) nach Anspruch 1, gekennzeichnet dadurch, dass das Verbindungselement (10, 16) aus verlängerten Profilstabteilen aus Aluminium oder Stahl erhalten wird und das Isolierelement (8,10) aus verlängerten Isoliermaterial-Profilstabteilen erhalten wird, vorzugsweise aus Kunststoff, wobei die Kupplung zwischen Verbindungselement (10, 16) und Isolierelement (8, 10) eine Isolierkupplung bildet, die zur Beseitigung von Wärmebrücken zwischen der Innenseite und einer Außenseite des Rahmens (1) geeignet ist, "Innen" bezieht sich auf das Gebäude, auf das der Rahmen (1) montiert wird, und bedeutet die Seite des Rahmens (1), die zum Innern weist, "Außen" bezieht sich auf die gegenüberliegende Seite des Rahmens (1) im Vergleich zu der Innenseite, d.h. die Seite des Rahmens (1), die zur Außenseite des Gebäudes hin weist.
  6. Rahmen (1) nach einem beliebigen der vorigen Ansprüche, gekennzeichnet dadurch, dass die ersten verlängerten Profilstabteile, die von den ersten Umfangselementen (8, 10, 11) des Gehäuses (2) herrühren, mindestens eines der besagten Befestigungsmittel (11, 15) in Form eines verlängerten Profilstabteils umfassen, das ein Befestigungsmittel auf dem Gehäuse (11) bildet, und die zweiten verlängerten Profilstabteile, die von den zweiten Umfangselementen (20, 16, 15) des mindestens eines Flügels (3) erhalten werden, umfassen mindestens eines der besagten Befestigungsmittel (11, 15) in Form eines verlängerten Profilstabteils, das ein Befestigungsmittel auf dem Flügel (15) bildet, wobei der verlängerte Profilstab, der das Befestigungsmittel auf dem Gehäuse (11) bildet, gleich dem verlängerten Profilstab ist, der das Befestigungsmittel auf dem Flügel (15) bildet, so dass besagte verlängerte Profilstäbe den gleichen Querschnitt haben, da sie aus demselben Profilstab erhalten wurden, und das Befestigungsmittel (11, 15) bilden, das aus einem Abschnitt erhalten wird, der von dem Gehäuse (2) und dem mindestens einen Flügel (3) geteilt wird.
  7. Rahmen (1) nach einem beliebigen der vorigen Ansprüche, gekennzeichnet dadurch, dass das Isolierelement des Gehäuses (8) und das Isolierelement des mindestens einen Flügels (20) im wesentlichen viereckig im Querschnitt sind und weiter gekennzeichnet dadurch, dass das Verbindungselement des Gehäuses (10) und das Verbindungselement des mindestens eines Flügels (16) im Querschnitt im wesentlichen viereckig sind, wobei das Isolierelement des Gehäuses (8) sich mit dem Verbindungselement des Gehäuses (10) verkuppeln kann und das Isolierelement des mindestens einen Flügels (20) sich mit dem Verbindungselement des mindestens einen Flügels (16) verkuppeln kann, wobei die gegenseitige Kupplung zwischen dem Isolierelement des Gehäuses (8) und dem Verbindungselement des Gehäuses (10) und die gegenseitige Kupplung zwischen dem Isolierelement des mindestens einen Flügels (20) und dem Verbindungselement des mindestens einen Flügels (16) mittels einer Reihe von Vertiefungen (28) mit Hinterschnittform und Vorsprüngen (27) durchgeführt wird, mit einer Form. die im wesentlichen komplementär zu der Hinterschnittform ist, wobei eine Basisseite kürzer als eine Endseite ist und eine Form im Querschnitt im wesentlichen einem Kegelstumpf entspricht, wobei die Vertiefungen (28) und in Längsrichtung in Bezug auf die Längenausdehnung des Abschnitts verlaufen, auf dem die Vertiefungen (28) erhalten werden, wobei die Vorsprünge (27) in Längsrichtung in Bezug auf die Längenausdehnung des Abschnitts verlaufen, auf dem die Vorsprünge (27) erhalten werden, wobei jeder der Vorsprünge (27) geeignet ist, um in einen entsprechenden Hohlraum der Vertiefungen (28) mit Ineinandergreifen eingefügt zu werden, das mittels der Kupplung zwischen besagter Form, die einem Kegelstumpf des Vorsprungs (27) entspricht, und besagter Form mit Hinterschnitt des Hohlraums (28) durchgeführt wird.
  8. Rahmen (1) nach einem beliebigen der vorigen Ansprüche, gekennzeichnet dadurch, dass das Befestigungsmittel (11, 15) von verlängerten Isoliermaterial-Profilstabteilen herrührt, vorzugsweise aus Kunststoff, wobei die Kupplung zwischen Verbindungselement (10, 16) und Befestigungsmittel (11, 15) eine Isolierkupplung bildet, die zur Beseitigung von Wärmebrücken zwischen der Innenseite und einer Außenseite des Rahmens (1) geeignet ist, wobei sich "innen" auf das Gebäude bezieht, auf das der Rahmen (1) montiert wird, und die Seite des Rahmens (1) bedeutet, die zum Innern weist, "außen" bezieht sich auf die gegenüberliegende Seite des Rahmens (1) im Vergleich zu der Innenseite, d.h. die Seite des Rahmens (1), die zur Außenseite des Gebäudes hin weist.
  9. Rahmen (1) nach einem beliebigen der vorigen Ansprüche von 6 bis 8, gekennzeichnet dadurch, dass die inneren Abdeckungen (12, 17) eine erste innere Abdeckung (12) umfassen, die auf dem Verbindungselement des Gehäuses (10) befestigt werden kann, und eine zweite innere Abdeckung (17) umfassen, die auf dem Verbindungselement des mindestens einen Flügels (16) befestigt werden kann, wobei die inneren Abdeckungen (12, 17) Ausbauelemente bilden, die leicht ausgetauscht werden können.
  10. Rahmen (1) nach einem beliebigen der vorigen Ansprüche, gekennzeichnet dadurch, dass die gegenseitige Befestigung zwischen den inneren Abdeckungen (12, 17) und den Befestigungsmitteln (11,15) mittels des Einsatzblocks (37) durchgeführt wird, der von den inneren Abdeckungen (12, 17) an der Kupplungsfläche mit den Befestigungsmitteln (11,15) vorspringt, wobei der Einsatzblock (37) in eine zweite Einsatzstelle (31), die auf den Befestigungsmitteln (11, 15) erhalten wird, eingefügt werden kann, wobei die zweite Einsatzstelle (31) im wesentlichen "C"-förmig ist und an einer Seite nahe einer zweiten Öffnung (39) offen und auf der gegenüberliegenden Seite in Bezug auf die zweite Öffnung (39) von einem Falzboden abgegrenzt wird, von dem aus zwei zueinander parallele Arme (36) verlaufen und die im wesentlichen "C"-Form begrenzen, wobei die Befestigung der inneren Abdeckungen (12, 17) in der ersten Einsatzstelle (29) mittels der folgenden durchgeführt wird:
    - Verbindungsmittel (30) auf den Armen (36), vorzugsweise in Form von Kupplungsrasten, die in die Kupplungsfläche zwischen den Armen (36) und dem Einsatzblock (37) eingreifen;
    - Zwischenblockiermittel (32) in Form von einem oder mehreren Dübeln, die gemeinsam in entsprechende Aushöhlungen (38) auf dem Einsatzblock (37) eingefügt werden.
  11. Rahmen (1) nach einem beliebigen der vorigen Ansprüche von 9 bis 10, gekennzeichnet dadurch, dass die zweite innere Abdeckung (17) aus einem ersten Element (18) und einem zweiten Element (19) besteht, wobei das erste Element (18) die Kupplungsschnittstelle mit dem Verbindungselement des mindestens einen Flügels (16) bildet, um die zweite innere Abdeckung (17) zu befestigen, und wobei das zweite Element (19) durch Ineinandergreifen zwischen dem ersten Element (18) und einem Stillstandselement (39) befestigt ist, das von dem Isolierelement des mindestens einen Flügels (20) vorspringt.
  12. Rahmen (1) nach dem vorherigen Anspruch, gekennzeichnet dadurch, dass er ein Schraubenabdeckelement (24) über den Köpfen der Schrauben (13) umfasst, das durch Ineinandergreifen befestigt ist und ein Endbearbeitungselement bildet, das leicht ausgetauscht werden kann, so dass die gegenseitige Befestigung des Schraubenabdeckelements (24) eine schnelle Entfernung des Schraubenabdeckelements (24) zwecks Austausch und/oder Wartung gestattet.
  13. Rahmen (1) nach einem beliebigen der vorigen Ansprüche, gekennzeichnet dadurch, dass er ein äußeres Endbearbeitungselement (7) umfasst, das mittels Schrauben (13) auf dem Isolierelement des Gehäuses (8) befestigt ist, wobei die Schrauben (13) nahe einer Lücke (33) zwischen dem mindestens einen Flügel (3) und dem Gehäuse (2) platziert sind und nur dann zugänglich sind, wenn der mindestens eine Flügel (3) in einer Öffnungsbedingung im Vergleich zu dem Gehäuse (2) ist, wobei das äußere Endbearbeitungselement (7) sowohl ein leicht austauschbares Abdeckungselement als auch ein Sicherheits-Diebstahlsschutzelement bildet.
  14. Rahmen (1) nach dem vorherigen Anspruch, gekennzeichnet dadurch, dass das äußere Endbearbeitungselement (7) ein Falzelement der Platte oder Glasscheibe (23) bildet, wenn der mindestens eine Flügel (3) in einer Schließstellung im Vergleich zu dem Gehäuse (2) ist, durch Dazwischenlegen einer ersten Falzdichtung (5).
  15. Rahmen (1) nach dem vorherigen Anspruch, gekennzeichnet dadurch, dass das äußere Endbearbeitungselement (7) eine zweite Falzdichtung (6) an der Kupplungsfläche zwischen dem äußeren Endbearbeitungselement (7) und dem Isolierelement des Flügels (20) umfasst, wobei die zweite Falzdichtung (6) geeignet ist, zusammen mit der ersten Falzdichtung (5), besagte Lücke (33) zwischen dem mindestens einen Flügel (3) und dem Gehäuse (2) abzudichten, wenn der mindestens eine Flügel (3) in einer Schließstellung im Vergleich zu dem Gehäuse (2) ist, wobei das äußere Endbearbeitungselement (7) bei Bedarf vorgesehen ist, mindestens in der Nähe der Umfangsseite des Rahmens (1), die eine nach unten gerichtete Umfangseite ist, d.h. zum Boden hin, mit Bohrungen (26), so dass eventuelle Kondensation abfließen kann.
  16. Rahmen (1) nach einem beliebigen der vorigen Ansprüche von 9 bis 15, gekennzeichnet dadurch, dass er eine dritte Falzdichtung (14) umfasst, die an der Kupplungsfläche zwischen dem mindestens einen Flügel (3) und dem Gehäuse (2) platziert ist, wobei die dritte Falzdichtung (14) auf der inneren Abdeckung (17) des Flügels (3) befestigt ist und gegen die innere Auskleidung (12) des Gehäuses (2) gedrückt wird, um das Umfangsprofil des mindestens einen Flügels (3) abzudichten, wenn es in einer Schließstellung gegen das Gehäuse (2) steht.
EP13801472.5A 2012-11-20 2013-11-18 Rahmen Not-in-force EP2923022B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT000195A ITUD20120195A1 (it) 2012-11-20 2012-11-20 "serramento"
PCT/EP2013/003474 WO2014079556A1 (en) 2012-11-20 2013-11-18 Frame

Publications (2)

Publication Number Publication Date
EP2923022A1 EP2923022A1 (de) 2015-09-30
EP2923022B1 true EP2923022B1 (de) 2018-02-21

Family

ID=47633461

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13801472.5A Not-in-force EP2923022B1 (de) 2012-11-20 2013-11-18 Rahmen

Country Status (6)

Country Link
EP (1) EP2923022B1 (de)
CN (1) CN104919124B (de)
ES (1) ES2669594T3 (de)
IT (1) ITUD20120195A1 (de)
RU (1) RU2639626C2 (de)
WO (1) WO2014079556A1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2525183B (en) * 2014-04-14 2021-01-13 Storm Faith Network Ltd Fenestration products
EP3048233A1 (de) * 2015-01-26 2016-07-27 Ferro Group International S.r.l. Fensterrahmen element mit einem innenprofil, einem äusseren profil und einem zwischenverbindungsprofil
CN106121284B (zh) * 2016-08-17 2019-02-05 广东亿合门窗科技有限公司 一种组合式玻璃屋
CN107269164A (zh) * 2017-07-07 2017-10-20 广东怡发门窗科技有限公司 一种三层结构的断桥铝型材
CN107269165A (zh) * 2017-07-07 2017-10-20 广东怡发门窗科技有限公司 一种断桥铝型材
BE1026247B1 (nl) * 2018-05-03 2019-12-02 Reynaers Aluminium Nv Vleugel voor een raam of deur en raam of deur daarvan voorzien en werkwijze voor het samenstellen van een dergelijke vleugel
RU187124U1 (ru) * 2018-05-21 2019-02-21 Валерий Павлович Левицкий Промышленные окна из сталеалюминиевых материалов
IT201900007914A1 (it) * 2019-06-03 2020-12-03 Uniform S P A Serramento per esterni

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB989304A (en) * 1961-12-08 1965-04-14 Pasche Heinz Improved frame construction for windows, doors and the like
DE4142151C2 (de) * 1991-12-20 1995-10-12 Lanco Lange Fenster Fassaden Fenster für ein Fensterband
ES2076881B1 (es) * 1993-12-02 1998-09-01 Maricurreina Lorenzo Diaz Sistema modular para la formacion de cerramientos acristalados.
IT1314711B1 (it) * 1999-02-25 2002-12-31 Alprogetti Srl Profilati a tre elementi per serramenti di cui quello internointercambiabile
IT1316469B1 (it) * 2000-03-15 2003-04-22 Mixlegno Srl Profilato per serramenti e serramenti cosi' ottenuti.
ES1064815Y (es) * 2007-02-08 2007-08-01 Intxausti Francisco J Lodoso Ensamblaje entre un perfil metalico y un marco de madera, para ventanas y/o puertas.
CN202249523U (zh) * 2011-08-23 2012-05-30 长沙新振升集团有限公司 门窗压线

Also Published As

Publication number Publication date
RU2015124022A (ru) 2017-01-10
CN104919124A (zh) 2015-09-16
EP2923022A1 (de) 2015-09-30
ES2669594T3 (es) 2018-05-28
WO2014079556A1 (en) 2014-05-30
CN104919124B (zh) 2018-06-15
RU2639626C2 (ru) 2017-12-21
ITUD20120195A1 (it) 2014-05-21

Similar Documents

Publication Publication Date Title
EP2923022B1 (de) Rahmen
US7971623B2 (en) Adjustable garage door window frame and method of installation
US5806256A (en) Modular glazing system
US10550624B2 (en) Versatile hybrid window system
US9316041B2 (en) Entry door clearance sidelight
US20090277111A1 (en) Versatile hybrid window system
US7065929B2 (en) Two part window and door assembly and coupling for interconnecting components thereof
KR20180015398A (ko) 현관문 구조
RU2721145C1 (ru) Дверь
CA2912933A1 (en) Invisible window frames
US6301852B1 (en) Window glazing assembly
CA2643557C (en) Window cladding
EP2912250B1 (de) Rollladenkasten
KR102467344B1 (ko) 가변형 레일 창
EP3121361B1 (de) Abdeckleiste
US20140230350A1 (en) Removable Interior Window Trim System and Method
KR200394727Y1 (ko) 폐 합성수지 폼을 이용한 방화문
US11891851B2 (en) Door-ready molding
US20220145693A1 (en) Door-ready molding
WO2015097721A1 (en) A frame for doora with a convex profile cut at 45°, in kit form, characterized by a crossbeam and two preformed side jambs on which to install special removable and reversible strips between them that allow for reversibility
US20240060356A1 (en) Modular barrier panel frame reinforcement systems and methods
NZ583779A (en) Window and door frames and sashes lined with insulating thermoplastic layer
EP1640547A1 (de) Verfahren zum Befestigen eines Abdeckelements an einem Fensterrahmen und Abdeckelement hierfür
AU676795B2 (en) A window or door frame assembly having a decorative trim surface
GB2574228A (en) Door, door-system and method

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20150622

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20161212

RIC1 Information provided on ipc code assigned before grant

Ipc: E06B 3/54 20060101ALN20170626BHEP

Ipc: E06B 3/263 20060101AFI20170626BHEP

Ipc: E06B 3/30 20060101ALI20170626BHEP

RIC1 Information provided on ipc code assigned before grant

Ipc: E06B 3/54 20060101ALN20170710BHEP

Ipc: E06B 3/30 20060101ALI20170710BHEP

Ipc: E06B 3/263 20060101AFI20170710BHEP

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20170904

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602013033428

Country of ref document: DE

Ref country code: AT

Ref legal event code: REF

Ref document number: 971909

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180315

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2669594

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20180528

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180221

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 971909

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180521

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180522

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180521

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602013033428

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20181122

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20181126

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20181130

Year of fee payment: 6

Ref country code: ES

Payment date: 20181203

Year of fee payment: 6

Ref country code: FR

Payment date: 20181122

Year of fee payment: 6

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181118

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20181130

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181130

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181118

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181118

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180221

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602013033428

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180221

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20131118

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180621

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20191118

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200603

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191118

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191130

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20210531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20191119

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230519