EP3385462A1 - Composant à isolation thermique - Google Patents

Composant à isolation thermique Download PDF

Info

Publication number
EP3385462A1
EP3385462A1 EP17000569.8A EP17000569A EP3385462A1 EP 3385462 A1 EP3385462 A1 EP 3385462A1 EP 17000569 A EP17000569 A EP 17000569A EP 3385462 A1 EP3385462 A1 EP 3385462A1
Authority
EP
European Patent Office
Prior art keywords
thrust bearing
thrust
insulating body
bearing
pressure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP17000569.8A
Other languages
German (de)
English (en)
Other versions
EP3385462B1 (fr
Inventor
Lutz Hollerbuhl
Tina Keller
Enrico Eckardt
Thorsten Heidolf
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.)
Leviat GmbH
Original Assignee
Halfen GmbH and Co KG
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 Halfen GmbH and Co KG filed Critical Halfen GmbH and Co KG
Priority to PL17000569T priority Critical patent/PL3385462T3/pl
Priority to EP17000569.8A priority patent/EP3385462B1/fr
Priority to US15/938,439 priority patent/US20180291620A1/en
Priority to CN201810310123.3A priority patent/CN108691366A/zh
Publication of EP3385462A1 publication Critical patent/EP3385462A1/fr
Application granted granted Critical
Publication of EP3385462B1 publication Critical patent/EP3385462B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/003—Balconies; Decks
    • E04B1/0038—Anchoring devices specially adapted therefor with means for preventing cold bridging
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B5/00—Floors; Floor construction with regard to insulation; Connections specially adapted therefor
    • E04B5/16—Load-carrying floor structures wholly or partly cast or similarly formed in situ
    • E04B5/17—Floor structures partly formed in situ
    • E04B5/23—Floor structures partly formed in situ with stiffening ribs or other beam-like formations wholly or partly prefabricated
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62—Insulation or other protection; Elements or use of specified material therefor
    • E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
    • E04B1/76—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to heat only
    • E04B1/78—Heat insulating elements
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/36—Bearings or like supports allowing movement
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/38—Connections for building structures in general
    • E04B1/41—Connecting devices specially adapted for embedding in concrete or masonry
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62—Insulation or other protection; Elements or use of specified material therefor
    • E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
    • E04B1/76—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to heat only
    • E04B2001/7679—Means preventing cold bridging at the junction of an exterior wall with an interior wall or a floor
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2103/00—Material constitution of slabs, sheets or the like
    • E04B2103/02—Material constitution of slabs, sheets or the like of ceramics, concrete or other stone-like material

Definitions

  • the invention relates to a thermally insulating component of the type specified in the preamble of claim 1.
  • thermally insulating component of the generic type known.
  • Such thermally insulating components with an insulating body are used in joints between load-bearing building parts, for example between building ceilings and balcony slabs.
  • pressure thrust bearings are provided in the insulating body, which protrude on a longitudinal side of the device in the building ceiling and on the opposite longitudinal side in the balcony slab.
  • tension rods are also provided.
  • thermally insulating component for connecting a building ceiling and a balcony slab comprising an insulating body and tension rods for receiving tensile forces, shear force rods for receiving shear forces and pressure elements for receiving pressure forces.
  • the invention has for its object to provide a thermally insulating component of the generic type, which has an improved insulating effect.
  • thermally insulating component having the features of claim 1.
  • thermally insulating components which have pressure thrust bearing for receiving horizontal forces and vertical forces are often oversized with regard to the absorption of vertical forces.
  • the invention now provides for replacing at least one of the thrust thrust bearing by a thrust bearing.
  • the thrust bearing is designed exclusively for receiving horizontal forces.
  • For the transmission of the same horizontal forces as a thrust bearing have thrust bearing in normal load and installation situations a reduced cross-section.
  • the thermally insulating component can be well adapted to the forces acting.
  • Horizontal forces are compressive forces and tensile forces. In installation position, the compressive forces and tensile forces act advantageously in the horizontal direction, in particular in the transverse direction of the component.
  • Vertical forces are shear forces acting in the vertical direction of the component. Vertical forces are advantageous in the installed position in the vertical direction.
  • the transverse direction advantageously extends in the horizontal direction from one to the other building part.
  • the transverse direction is in particular perpendicular to the longitudinal direction.
  • the transverse direction is advantageously also perpendicular to the longitudinal sides of the insulating body.
  • the long sides are advantageously aligned approximately vertically.
  • the longitudinal sides need not be flat, but may be structured, for example by extending at the top and / or bottom of the insulator in the longitudinal direction extensions.
  • the vertical direction of the insulating body runs vertically in the installation position.
  • the longitudinal side advantageously extends approximately in the longitudinal direction and approximately in the vertical direction.
  • Bearing and thrust bearing differ in the type of forces that can be absorbed by the respective bearing. Thrust bearings are designed only for receiving horizontal forces acting in a transverse direction of the thermally insulating component. In the thrust bearing prevails thereby a uniaxial stress state. Pressure bearings are advantageously formed with a small height and arranged near the bottom of the thermally insulating component. This results in a low center of gravity in the thermally insulating component and preferably in the vertical direction a large distance to zugkraftübertragenden components.
  • Pressure thrust bearings are designed to absorb horizontal forces and vertical forces.
  • the vertical forces act in the connection plane perpendicular to the horizontal forces, ie in the vertical direction of the insulating body.
  • the horizontal forces acting on the thrust thrust bearing have an axial offset relative to one another, so that a biaxial stress state results in the thrust thrust bearing.
  • the height of the thrust bearing measured on this longitudinal side in the vertical direction is advantageously smaller than the height of the thrust thrust bearing measured on this longitudinal side of the insulating body in the vertical direction.
  • Pressure thrust bearings have to absorb the torque introduced by the horizontal forces on at least one longitudinal side, in particular at least in the installed state of a balcony slab longitudinal side, advantageously a much larger measured in the vertical direction height than thrust bearing.
  • the height of the thrust bearing is advantageously less than 50%, in particular less than 30%, of the height of the pressure thrust bearing on this longitudinal side of the insulating body on the at least one longitudinal side.
  • the height of thrust bearing and thrust bearing is measured on the same longitudinal side of the insulator in the vertical direction.
  • the pressure thrust bearings are advantageous over the long sides over with a projection of at least 1.0 cm.
  • the supernatant is about 2.0 cm.
  • the supernatant is measured between the thrust bearing and the immediately adjacent to the pressure thrust bearing region of the insulator, so that for the supernatant, for example, at the top and bottom of the insulator extending extensions, strips or the like are not taken into account.
  • the pressure thrust bearings protrude beyond each longitudinal side with at least one projection. It can be provided that have the pressure thrust bearing on each longitudinal side adjacent to the top and another adjacent to the bottom arranged projection. However, it can also be provided that the thrust thrust bearings on one longitudinal side have a projection on the upper side and on the opposite longitudinal side a projection on the underside. In an alternative design, a projection arranged between the upper side and the lower side may also be advantageous.
  • the supernatant of the pressure thrust bearing is measured at the region projecting furthest beyond the longitudinal side, in particular at the at least one projection. The supernatant advantageously forms a projection surface in the vertical direction over which forces acting in the vertical direction, ie in the vertical direction, can be transmitted.
  • the thrust thrust bearing may also have one or more recesses, over the projection surface in the vertical direction acting vertical forces, namely shear forces can be transmitted.
  • the transmittable thrust depends on the total size of the projection surface.
  • the projection surface can be formed by a single projection or a single depression or can be composed of the projection surfaces on a plurality of projections or depressions.
  • the thrust bearings can also survive with a projection over the long sides. It can also be provided that the end faces of the thrust bearing flush in the long sides lie. However, the thrust bearings do not form a horizontal projection surface on which forces can be transmitted.
  • the thermally insulating component may have at least one tension rod, at least one pressure rod and / or at least one transverse force rod which respectively protrude through the insulating body.
  • thermally insulating component pressure thrust bearing, thrust bearing and tension rods but no pressure rods and no shear force rods has. This is particularly advantageous for thermally insulating components for connecting projecting plates.
  • thermally insulating component pressure thrust bearing, thrust bearing, tension rods and transverse force rods, but no pressure rods.
  • the thermally insulating component has pressure thrust bearing, thrust bearing and transverse force rods.
  • This thermally insulating component advantageously has no tension rods and no pressure rods.
  • the thermally insulating component contains pressure thrust bearings, pressure bearings, pressure rods and transverse force rods, but no tension rods.
  • a thermally insulating component which can serve for example for connecting projecting plates and has a higher load capacity for bending moments, has advantageous thrust bearing, thrust bearing, tension rods and pressure rods, but no shear force rods.
  • thermally insulating component which is used in particular for connecting continuous plates, and with which a maximum load capacity is achieved, it is advantageously provided that the thermally insulating component pressure thrust bearing, thrust bearing, tension rods, pressure rods and transverse force rods has.
  • the insulating body advantageously has an underside running longitudinally between the longitudinal sides. In the installed position, the underside of the thermally insulating component is advantageously below.
  • the thrust bearing and thrust bearing are advantageously arranged near the bottom of the thermally insulating component.
  • the distance of the thrust bearing to the bottom is advantageously less than 3 cm, in particular less than 2 cm.
  • the distance of the thrust bearing thrust to the bottom is less than 3 cm, in particular less than 2 cm.
  • the distance of the thrust bearing and the distance of the thrust thrust bearing to the bottom are approximately equal.
  • the distance of the thrust bearing to the bottom is advantageously 80% to 120% of the distance of the thrust bearing to the bottom.
  • the building parts can move in the transverse direction to each other.
  • the region of the thrust thrust bearing projecting over the longitudinal sides of the insulating body is formed at least partially in a radius about at least one axis extending in the vertical direction.
  • the projecting over the longitudinal sides of the insulating body region of the thrust bearing is advantageously at least partially formed in a radius around at least one axis extending in the vertical direction.
  • both the region of the thrust thrust bearing projecting beyond the longitudinal sides of the insulating body and the region of the thrust bearing projecting over the longitudinal sides of the insulating body are at least partially in a radius of about formed at least one axis extending in the vertical direction.
  • the thrust bearing and the thrust bearing can move in the manner of joints with respect to the building parts.
  • Different radii can be provided for different areas of the thrust bearing or thrust bearing. It may be advantageous that all the centers of the different radii of a thrust bearing or thrust bearing are on one longitudinal side on the same axis. Also, an offset between the centers of the radii in plan view of the thrust bearing thrust bearing may be advantageous.
  • the centers of the radii are then on different axes extending in the vertical direction.
  • the centers of the radii lie between the planes formed by the longitudinal sides of the insulating body, ie within the insulating body.
  • the centers of the radii lie on planes parallel to the longitudinal sides of the insulator.
  • An arrangement in the extension of the longitudinal side of the insulating body may be advantageous.
  • the at least one axis is not outside of the insulator.
  • Fig. 1 schematically shows a thermally insulating component 1, which is arranged in a parting line 4 between two structural parts, in the embodiment of a balcony slab 2 and a building ceiling 3.
  • the component 1 has an insulating body 5, which has an elongated, in the embodiment, a cuboid shape.
  • the insulating body 5 is used for at least partial thermal separation of the building ceiling 3 from the balcony slab 2.
  • the insulating body 5 has a longitudinal direction 6 which extends in the longitudinal direction of the parting line 4 between the balcony slab 2 and the building ceiling 3.
  • the longitudinal direction 6 is aligned horizontally in the installed position.
  • the insulating body 5 also has a transverse direction 7, which is perpendicular to the longitudinal direction 6 in the embodiment.
  • the insulating body 5 has a first, on the balcony slab 2 along the longitudinal side 9 and an opposite second, on the building ceiling 3 along longitudinal side 10.
  • the transverse direction 7 extends from the balcony slab 2 to the building ceiling 3 and transverse to the longitudinal sides 9 and 10. Die Transverse direction 7 is advantageously arranged horizontally in the installed position.
  • the insulating body 5 also has a vertical direction 8, which is perpendicular to the longitudinal direction 6 and the transverse direction 7 and which is advantageously oriented vertically in the installed position.
  • the insulating body 5 has an underside 13, which is arranged in the installation position below and which extends between the longitudinal sides 9 and 10.
  • the bottom 13 is advantageously aligned horizontally and perpendicular to the vertical direction 8.
  • the insulating body 5 has an underside 13 opposite top 14, which is also aligned horizontally and perpendicular to the vertical direction 8 in the embodiment.
  • the top 14 is arranged in mounting position on top of the insulating body 5.
  • the measured length in the longitudinal direction 6 of the insulating 5 can be selected adapted to the application.
  • the insulating body 5 has a width g measured in the transverse direction 7 and a height h measured in the vertical direction 8. In the exemplary embodiment, the height h is greater than the width g.
  • the insulating body 5 may be formed, for example, as a box which is filled with insulating material.
  • the insulating body 5 is not suitable in particular for receiving the forces between the balcony slab 2 and the building ceiling 3 to be transmitted.
  • thrust bearing 11 and thrust bearing 12 are arranged in the insulating body.
  • the thrust bearing 11 and the thrust bearing 12 are arranged alternately in the longitudinal direction 6 in the embodiment.
  • another, in particular another regular arrangement of pressure bearings 12 and thrust bearing bearings 11 may be advantageous.
  • An irregular arrangement of pressure bearings 12 and thrust bearing bearings 11 may be advantageous.
  • the thrust bearings 12 have a distance n from adjacent pressure thrust bearings 11.
  • Adjacent thrust thrust bearings 11 have a distance p from each other.
  • Adjacent thrust bearings 12 have a distance o to each other.
  • the distances o and p can be the same for all thrust bearings 12 or all thrust thrust bearings 11, so that the thrust bearings 12 and thrust thrust bearings 11 are arranged at a uniform distance from one another.
  • the distance n is equal in the embodiment between all pressure slide bearings 11 and thrust bearings 12.
  • the horizontal forces F H and vertical forces Fv are to be transferred from the balcony slab 2 in the building ceiling, the in Fig. 1 are shown schematically.
  • the horizontal forces F H include compressive forces F D and tensile forces Fz, which in Fig. 1 are also shown schematically.
  • the horizontal forces F H act in the installed position advantageous in the horizontal direction.
  • the vertical forces Fv include thrust forces in both directions, ie up and down.
  • the vertical forces Fv act in the installed position advantageous in the vertical direction.
  • the thrust bearing 11 are provided to absorb the horizontal forces F H and the vertical forces F V .
  • the number and size of the thrust bearing 11 is dimensioned in this embodiment so that all male vertical forces F V can be transmitted from the pressure slide bearings 11.
  • the thrust thrust bearings 11 do not have to transmit the entire vertical forces F V.
  • the thrust bearings 12 are provided, which are provided exclusively for receiving horizontal forces F H. This is achieved in that the thrust bearing 12 has no horizontal projection surface, can be transmitted via the vertical forces Fv. If the thrust bearing 12 protrudes beyond the longitudinal sides 9 and 10 into the balcony slab 2 and the building ceiling 3, then soft material such as expanded polystyrene (EPS) or the like may be arranged on the thrust bearing 12, the thrust bearing 12 may be rounded with a large radius or have an air gap in the vertical direction to the surrounding concrete of the balcony slab 2 or the building ceiling 3. As a result, it can be prevented structurally with a pressure bearing 12 projecting into the balcony slab 2 or the building ceiling 3 that vertical forces Fv, ie thrust forces, can be introduced into the thrust bearing 12.
  • EPS expanded polystyrene
  • a thermally insulating component 1 which has exclusively thrust bearing 11 for receiving the horizontal forces F H , in particular the pressure forces F D , and the vertical forces F V .
  • the number of pressure thrust bearings 11 is reduced.
  • Some of the pressure thrust bearings 11, in the exemplary embodiment every second pressure thrust bearing 11, are replaced by thrust bearings 12.
  • Tension rods, not shown, may be provided.
  • the thrust bearing 12 and the thrust bearing 11 differ in their geometric design.
  • the pressure thrust bearings 11 have a height c measured in the vertical direction 8 on the longitudinal side 9, which is significantly greater than a height d of the thrust bearing 12 measured in the same direction on the longitudinal side 9.
  • the height d of the thrust bearing 12 is advantageously less than 50%, in particular less than 30% of the height c of the thrust thrust bearing 11.
  • a comparatively large height c of the thrust thrust bearing 11 is required.
  • the vertical forces F V generate at the thrust bearing 11, a moment which is supported over the vertical distance of the introduced horizontal forces F H.
  • the acting forces are in Fig.
  • the horizontal forces F H are in the embodiment only compressive forces F D.
  • the horizontal forces F H may also include tensile forces Fz in an alternative embodiment.
  • the thrust bearing 12 record only the pressure forces F D , the height d of the thrust bearing 12 is significantly lower.
  • the dimensions of the thrust bearing 12 and the thrust bearing 11 are respectively measured on the respective longitudinal side 9, 10 directly to the thrust bearing 12 and thrust bearing 11.
  • the height c of the pressure thrust bearing 11 can be the same on both longitudinal sides 9 and 10. However, it can also be provided that the thrust thrust bearings 11 on the longitudinal side 10 have a significantly lower height than on the longitudinal side 9.
  • the height of the thrust bearing 11 on the longitudinal side 10 may correspond in an advantageous design approximately the height d of the thrust bearing 12.
  • both the thrust bearing 12 and the pressure thrust bearing 11 are arranged near the bottom 13 of the insulating body 5.
  • the thrust bearing 11 have the bottom 13 a distance a.
  • the distance a is advantageously less than 3 cm, in particular less than 2 cm.
  • the thrust bearing 12 have the bottom 13 a distance b.
  • the distance b is advantageously less than 3 cm, in particular less than 2 cm. Distances a and b between 1 cm and 2 cm are considered particularly advantageous.
  • the distance b of the thrust bearing 12 to the bottom 13 is advantageous 80% to 120% of the distance a of the thrust bearing 11 to the bottom 13. In a preferred embodiment, the distances a and b are the same.
  • Fig. 1 also shows, the thrust bearing 11 protrude beyond the longitudinal side 9.
  • the pressure thrust bearing 11 protrude beyond the opposite longitudinal side 10.
  • the thrust bearing 11 have projections 16 and 17, which will be described in more detail below and with which the pressure thrust bearing 11 protrude beyond the longitudinal sides 9 and 10.
  • the supernatant e at the projections 16 and 17 is advantageously more than 1.0 cm, in particular more than 1.5 cm.
  • the thrust bearing 12 are with a supernatant f on the long sides 9, 10, which is less than the supernatant e of the thrust thrust bearing 11 in the embodiment.
  • the thrust bearing 12 is formed and / or arranged so that no projection surface is formed in the vertical direction 8 by the supernatant f, attack the vertical forces Fv and can be introduced into the thrust bearing 12. As a result, only horizontal forces F H are transmitted via the thrust bearing 12.
  • the supernatant f can also be zero, so that the thrust bearing 12 are flush in the longitudinal sides 9, 10.
  • the projections e and f are in the transverse direction 7, in particular perpendicular to the respective longitudinal side 9 or 10, and measured directly at the respective thrust bearing 12 or pressure thrust bearing 11.
  • the Fig. 2 to 4 show different embodiments of thrust bearing 12.
  • the in Fig. 2 shown thrust bearing 12 has a cuboid base body, are formed on the rounded, in the embodiment, semi-cylindrical end portions 15.
  • the thrust bearing 12 has a length k, which in the installed state in the transverse direction 7 (FIG. Fig. 1 ) of the insulating body 5 is measured.
  • the length k is the largest extension of the thrust bearing 12.
  • the end regions 15 are the regions which protrude beyond the longitudinal sides 9 and 10 of the insulating body 5. In the embodiment, the end portions 15 extend with a radius s about an axis 31.
  • the axis 31 is in the installed state in the insulating body 5 advantageous in the area between the planes formed by the longitudinal sides 9 and 10 of the insulating body 5.
  • the axis 31 is therefore advantageously within the insulating body.
  • an arrangement of the axis 31 in the extension of the longitudinal side 9 and 10 may also be advantageous.
  • the thrust bearing 12 has a width m, which is aligned in the installed position in the longitudinal direction 6.
  • the width m is significantly smaller than the length k.
  • the width m may for example be 15% to 60% of the length k.
  • the thrust bearing 12 also has the also in Fig. 1 shown height d, which is significantly smaller than the length k. In the exemplary embodiment, the height d is smaller than the width m.
  • Fig. 3 shows a thrust bearing 12 which is cylindrical.
  • the longitudinal center axis of the thrust bearing 12 is to be arranged in the transverse direction 7 in the insulating body 5.
  • the thrust bearing 12 has end faces 32, which are advantageously arranged flush in the installed state in the longitudinal sides 9 and 10 and do not protrude beyond this. In an alternative embodiment, the end faces 32 may be convexly bulged and protrude beyond the longitudinal sides 9 and 10, respectively.
  • the thrust bearing 12 has a length k 'which corresponds to the width g of the insulating body 5.
  • the height d and the width m of the thrust bearing 12 are the same due to the cylindrical shape.
  • the width m may for example be 15% to 60% of the length k '.
  • Fig. 4 shows a thrust bearing 12, which is formed as a cuboid.
  • the thrust bearing 12 has end faces 32 which come to lie in the installed state in the longitudinal sides 9 and 10.
  • the thrust bearing 12 has a length k 'measured in the transverse direction 7 and a width m measured in the longitudinal direction 6 which is significantly smaller than the length k'.
  • the end faces 32 are flat.
  • the end faces 32 are convexly bulged and in the installed state over the longitudinal sides 9 and 10 over.
  • Other forms of thrust bearings 12 may be advantageous. It can be provided to provide the end faces 32 of the thrust bearing 12 with a sliding layer.
  • Fig. 5 shows an embodiment of a pressure thrust bearing 11.
  • the pressure thrust bearing 11 has an upper side 18 which is arranged in the installed position in a parting line 4 above, as well as a lower mounting position in the bottom 19.
  • the bottom 19 and the top 18 are flat and parallel aligned to the longitudinal direction 6 and the transverse direction 7.
  • the thrust thrust bearing 11 has a width l, which is aligned in the longitudinal direction 6 and which is significantly smaller than the height c of the thrust thrust bearing 11.
  • the thrust bearing 11 also has a length i, which is measured in the transverse direction 7 and which is greater than the width g of the insulating body 5.
  • the thrust bearing 11 is, as well Fig. 1 shows, so arranged in Isolierköper 5 that the pressure thrust bearing 11 protrudes on both end faces 9 and 10 on the insulating body 5.
  • the pressure thrust bearing 11 has at the over the longitudinal sides 9 and 10 protruding areas end faces 33.
  • the end faces 33 are not parallel to the vertical direction 8, but curved.
  • the end faces 33 have a central region 21, in which the projection over the longitudinal sides 9 and 10 is only small.
  • a projection 16 is arranged, which is around the supernatant e ( Fig. 1 ) protrudes beyond the longitudinal side 9.
  • a corresponding projection 17 is arranged, which also protrudes to the supernatant e on the longitudinal side 9. This in Fig.
  • a pressure thrust bearing 11 is mirror-symmetrical to three planes, namely to a plane defined by the vertical direction 8 and the longitudinal direction 6, to a plane defined by the vertical direction 8 and the transverse direction 7 and to a plane defined by the longitudinal direction 6 and the transverse direction 7 ,
  • the thrust bearing 11 can be used in any orientation in the insulating body 5.
  • the longitudinal side 9 and the longitudinal side 10 can thereby be oriented both to the balcony slab 2 and to the building ceiling 3.
  • Fig. 6 shows an embodiment of a component 1, which in addition to the insulating body 5, the pressure slide bearings 11 and the thrust bearings 12 tension rods 26, pressure rods 27 and transverse force rods 28 has.
  • Fig. 6 are schematically both tension rods 26 and pressure rods 27 and transverse force rods 28 shown. Which of these elements a component 1 can be selected adapted to the particular application. As a result, the component 1 can be well adapted to the particular application.
  • An advantageous embodiment of a thermally insulating component 1 advantageously comprises thrust bearing 11, thrust bearing 12 and tension rods 26.
  • the tension rods 26 are arranged closer to the upper side 14 of the insulating body 5 than at the bottom 13.
  • the tension rods 26 are closer to the top 14 of the Insulator 5 arranged as the tops 18 of the thrust thrust bearing 11th
  • a further advantageous embodiment of a component 1 has pressure thrust bearing 11, pressure bearing 12, tension rods 26 and transverse force rods 28.
  • Wie Fig. 6 schematically shows, a transverse force bar 28 extends on the longitudinal side 9 closer to the top 14 than on the bottom 13.
  • a transverse force bar 28 extends obliquely toward the bottom 13 and leaves the insulator 5 on the longitudinal side 10 in a range
  • a further transverse force bar 28 is guided in the opposite direction and runs on the longitudinal side 9 closer to the bottom 13, in the insulating body 5 obliquely toward the top 14 and leaves the insulating body 5 on the longitudinal side 10 closer to the top 14 than at the bottom 13.
  • only one of the transverse force rods 28 may be provided.
  • the arrangement of tension rods 26 and transverse force rods 28 results in a higher shear force capacity of the component. 1
  • a further advantageous variant of a component 1 has pressure thrust bearing 11, thrust bearing 12 and transverse force rods 28.
  • an optimized ratio of the transmittable horizontal forces F H , in particular the pressure forces F D , to the transmittable vertical forces F V can be achieved.
  • a component 1 which comprises thrust thrust bearing 11, thrust bearing 12, pressure rods 27 and transverse force rods 28.
  • a component 1 which is used in particular for connection for supported plates, an optimized ratio of the transferable horizontal force F H , in particular the pressure force F D to the transferable vertical force Fv.
  • the pressure rods 27 extend at a distance to the bottom 13, approximately the distance a, b of the thrust thrust bearings 11 or the thrust bearing 12 to the bottom 13 (FIGS. Fig. 1 ) corresponds.
  • a component 1 is provided, the pressure thrust bearing 11, pressure bearing 12, tension rods 26 and pressure rods 27 includes.
  • a component 1 is particularly suitable for cantilevered plates in which an increased capacity for bending moments is required.
  • a component 1 pressure thrust bearing 11, thrust bearing 12, tension rods 26, pressure rods 27 and transverse force rods 28 are provided.
  • a component 1 is particularly advantageous for the connection of continuous plates.
  • the arrangement of tension rods 26, pressure bars 27 and transverse force bars 28 in a component 1, a maximum load capacity of the device 1 can be achieved.
  • the arrangement of the tension rods 26, pressure rods 27 and / or transverse force rods 28 is advantageous as in Fig. 6 shown and how to Fig. 6 described provided.
  • Fig. 7 schematically shows the arrangement of the thrust bearing 11 in the insulating 5. How Fig. 7 shows, the thrust bearing 11 protrudes on each longitudinal side 9, 10 with a protruding portion 20 beyond the longitudinal sides 9 and 10 also.
  • Fig. 7 Also shown is the arrangement of the projections 16 and 17 on the upper side 18 and the lower side 19 and the central region 21, which is arranged between the projections 16 and 17.
  • the pressure thrust bearing 11 projects with the supernatant e the long sides 9 and 10 also.
  • the thrust thrust bearing 11 projects beyond the longitudinal sides 9 and 10 with a reduced projection v.
  • the supernatant e is advantageously at least 0.5 cm, in particular at least 1.0 cm larger than the reduced supernatant v.
  • the difference between the projection e and the reduced projection v is advantageously matched to the number of load-bearing projections 16, 17 on each side of the pressure-slide bearing 11.
  • a load-bearing projection 16 or 17 is provided in each side of the thrust bearing 11.
  • the respective other projection 16, 17 acts due to an air gap at the top 18 and the bottom 19 is not load-bearing.
  • the projections 16 are therefore provided only for receiving upward and the projections 17 only for receiving downward forces.
  • the supernatant e is advantageously at least 1.0 cm larger than the reduced supernatant v.
  • the supernatant e may be smaller, advantageously by at least 0.5 cm larger than the reduced supernatant v.
  • the vertical forces Fv are transmitted via the mutually facing pressure surfaces 36 of the projections 16 and 17.
  • an air gap to the surrounding concrete is formed with conventional installation, so that no vertical forces F V can be introduced into the pressure thrust bearing 12 at the top 18 and the bottom 19.
  • the projection surface 35 which is perpendicular to the vertical direction, of the pressure surface 36 is decisive, which in FIG Fig. 8 is shown schematically.
  • the projection surface 35 is the area formed in a vertical direction in plan view 8 between the outer contour of the central region 21 and the outer contour of the projections 16 and 17, respectively.
  • the projection surface 35 only the areas of the pressure thrust bearing 11 are taken into account, which lie non-positively between the adjacent components, ie the building ceiling 3 and the concrete slab 2.
  • the projection surface 35 can be formed on projections or recesses.
  • the pressure thrust bearing 11 is provided on the projections 16 with rounded corners 30. Die Vorsprünge 16 Sind in der Zeichnungschreib.
  • the radius u at the rounded corners 30 is in the in the Fig. 7 to 9 shown embodiment of a thrust bearing 11 is smaller than half the width of the thrust bearing 1 11 Fig. 9 ).
  • a straight section 34 is thereby formed on the projections 16, in which the projection 16 extends parallel to the longitudinal side 9 and 10, respectively.
  • the radius u extends about an axis 23.
  • the axis 23 is advantageously between the longitudinal sides 9 and 10.
  • the thrust thrust bearing 11 is formed at its extending in the vertical direction 8 edges advantageously rounded with a radius x about an axis 37.
  • the thrust bearing 12 is advantageously rounded off with a radius s about an axis 31 ( Fig. 2 ).
  • the axes 37 of the radii x lie in the central region 21 of the thrust thrust bearings 11 and the axes 31 of the radii s of the thrust bearing 12 of a component 1 in a common plane which runs parallel to the longitudinal side 9.
  • Fig. 10 shows an embodiment of the thrust bearing 11, in which the projections 16 are executed in a radius r.
  • the radius r extends around an axis 23.
  • the axis 23 is advantageously between the extension of the longitudinal side 9 and the extension of the longitudinal side 10, ie in the insulating body 5, as in Fig. 10 is shown schematically for the longitudinal side 9.
  • the radius r is thus greater than the supernatant e ( Fig. 1
  • another arrangement of the axis 23 may be advantageous.
  • the projection 16 as well as the projection 17 extends over the entire projection 20 in a constant radius r.
  • FIGS. 11 and 12 show a further embodiment of a thrust bearing 11.
  • the projections 16 and 17 are provided on their sides facing each with a groove 22.
  • the middle region 21 is set back in a side view with respect to the projections 16 and 17, so that the thrust-thrust bearing 11 projects less far beyond the longitudinal sides 9 and 10 in the middle region 21.
  • the tops 18 and 19 are flat and parallel to each other.
  • the pressure thrust bearing 11 is formed symmetrically to a plane spanned by the longitudinal direction 6 and the transverse direction 7, to a plane spanned by the transverse direction 7 and in the vertical direction 8, and to a plane spanned by the longitudinal direction 6 and the vertical direction 8.
  • Fig. 12 shows the outer contour of the projections 16 in a radius r about an axis 23.
  • the axis 23 extends in the installed state in the vertical direction 8 (FIG. Fig. 1 ) and in extension of the longitudinal side 9 and 10.
  • the groove 22 closes in the embodiment directly to the end face 33 at.
  • the groove 22 extends in a radius t about the axis 23.
  • the end face 33 extends in the radius t about the axis 23.
  • the groove 22 forms in the installed state an undercut in the transverse direction 7 and in the longitudinal direction 6, as in the groove 22, the material the concrete slab 2 or the building ceiling 3, for example concrete, can intervene.
  • Fig. 12 shows the outer contour of the projections 16 in a radius r about an axis 23.
  • the axis 23 extends in the installed state in the vertical direction 8 (FIG. Fig. 1 ) and in extension of the longitudinal side 9 and 10.
  • the groove 22 closes in the embodiment directly to the end face 33 at
  • the radius r is greater than half the width w of the thrust thrust bearing 11 in the region lying between the projections 16 and 17.
  • the width w is advantageously measured centrally between the projections 16 and 17. It may be advantageous to form the pressure thrust bearing 11 without the grooves 22.
  • each two projections 16 and 17 are arranged on the top 18 and the bottom 19.
  • a projection 16 is disposed on the upper side 18.
  • no projection 16 is arranged.
  • the projection 16 is advantageously arranged on the building ceiling 3 facing end face 43 of the pressure slide bearing 11.
  • a projection 17 is provided on the underside 19.
  • the protrusion 17 projects on the longitudinal side 9 of the insulating body 5, and the protrusion 16 on the longitudinal side 10.
  • the protrusions 16 and 17 can each have a groove 22.
  • Fig. 14 shows a further embodiment of a thrust bearing 12, which comprises two bearing bodies 25.
  • Each bearing body 25 may be formed corresponding to one of the thrust bearing 12 of the preceding embodiments.
  • the bearing bodies 25 of the thrust bearing 12 each have at their upper side 18 a recess 24, at which the height of the bearing body 25 is reduced.
  • the bearing bodies 25 each have two projections 29, which are provided over the longitudinal sides 9, 10 of the insulating body 5 (FIGS. Fig. 1 ) to preside.
  • the projections 29 are formed with rounded corners and extend with a constant cross section over the entire height of the bearing body 25.
  • a circular arc-shaped configuration of the projections 29, so a design with a continuous radius may be advantageous.
  • Other configurations of the bearing body 25 may be advantageous.
  • two bearing bodies can be provided for a thrust thrust bearing 11, which are combined to form a common pressure thrust bearing 11.
  • FIGS. 15 and 16 another embodiment of a thrust bearing 11 is shown.
  • the pressure thrust bearing 11 has an end face 33 in which a projection 17 is arranged adjacent to the underside 19. At the top 18 no projection is provided on the front side 33.
  • the thrust-thrust bearing 11 has a vertical direction 8 (FIG. Fig. 1 ) measured height c. As Fig. 15 shows, the height of the thrust bearing 11 decreases from the end face 33 to an opposite end face 43.
  • the end face 33 is provided for installation on a building ceiling 3 facing longitudinal side 10 of the insulating body 5, while the end face 43 on the opposite, a balcony plate 2 facing Long side 9 is provided.
  • the thrust bearing 11 has longitudinal sides 40 which extend between the end faces 33 and 43 approximately in the vertical direction 8.
  • a stiffening strut 39 Adjacent to the bottom 39 is provided on the longitudinal sides 40, a stiffening strut 39 which extends approximately in the transverse direction 7 of the insulating body 5 (FIG. Fig. 1 ).
  • the width 1 of the thrust bearing 11 is smaller in the region to be arranged in the insulating body 5 than at the end faces 33 and 43. In the region to be arranged in the insulating body 5, the width 1 increases from the side facing the end face 33 to the side facing the end face 43.
  • the top 18 of the thrust roller bearing 11 extends inclined in a central region and drops in the direction of the end face 43 out.
  • the thrust bearing 11 has a height c ', which is less than the height c.
  • the height c ' may advantageously be between 40% and 80%, in particular from 50% to 70% of the height c.
  • a thrust bearing 11 can be a reduced heat transfer between the balcony slab 2 and the building ceiling 3 ( Fig. 1 ) to reach.
  • Other asymmetrical configurations of a thrust bearing 11 may be advantageous.
  • the FIGS. 17 and 18 show a thrust bearing 12, which is advantageous in combination with the in the FIGS. 15 and 16 shown thrust bearing 12 is provided in a thermally insulating component 1.
  • the thrust bearing 12 is formed cuboid in the embodiment and has end faces 32. Due to the symmetrical design of the thrust bearing 12 different mounting positions are possible.
  • the thrust bearing 12 has an installed state in the vertical direction 8 (FIG. Fig. 1 ) measured height d.
  • the height d is smaller than the height c of the thrust thrust bearing 11 on the end face 33 (FIG. FIGS. 15 and 16 ). However, the height d can approximately correspond to the height c 'on the front side 43. It can also be provided that the height d is greater than the height c '.
  • the height c of the pressure-slide bearing 11 is greater than the height d of the pressure bearing 12.
  • FIGS. 19 to 24 show further possible arrangements of thrust bearings 12 and pressure thrust bearings 11 in an insulating body 5.
  • the arrangement in Fig. 19 are in the illustrated component 1 four thrust bearing 11 and two thrust bearing 12 symmetrical arranged to the center of the device 1.
  • the two outer thrust bearing 11 each have the same distance p to each other, while the two middle thrust bearing 11 have a reduced distance p 'to each other.
  • the thrust bearings 12 are arranged at a distance n 'to the outer pressure thrust bearings 11, which is significantly smaller than the distance n of the thrust bearing 12 to the adjacent central pressure thrust bearings 11.
  • the thrust bearing 12 have a distance o to each other, which is significantly greater than the distances n, n ', p and p'.
  • Fig. 20 are the thrust bearing 11 as in the embodiment according to Fig. 19 arranged.
  • the thrust bearings 12 are arranged to the first and the third thrust thrust bearing at the reduced distance n 'and have the second or fourth thrust bearing 11, the enlarged distance n. This results in a regular, asymmetric to the center arrangement.
  • An arrangement in which the distance n 'is greater than the distance n may also be advantageous.
  • two thrust bearings 12 and two thrust thrust bearing 11 are provided in the thermally insulating component 1, which are arranged alternately.
  • the thrust bearing 12 have to the adjacent thrust bearing bearings 11 different distances n and n '.
  • the distance p between adjacent thrust bearing bearings 11 and the distance o between adjacent thrust bearings 12 are the same, resulting in a regular arrangement.
  • two thrust bearing 11 and two thrust bearings 12 are provided. Both thrust bearings 12 are arranged between the two pressure slide bearings 11 at a distance o to each other. The distance p between the thrust bearing bearings is at least twice as large as the distance o.
  • Fig. 23 shows how Fig. 22 a symmetrical arrangement of pressure layers 12 and pressure slide bearings 11.
  • the thermally insulating component 1 has five pressure thrust bearings 11 and two thrust bearings 12. At the end regions of the component 1 are each two Thrust bearing 11 is arranged adjacent to each other. Between the two groups of two thrust bearing bearings 11, the two thrust bearings 12 are arranged with a pressure thrust bearing 11 arranged therebetween. The distance n 'of the thrust bearing 12 to the middle pressure thrust bearing 11 is greater than the distance n to the outer pressure thrust bearings 11th
  • Fig. 24 This in Fig. 24 embodiment shown has substantially the same arrangement as the embodiment Fig. 23 , However, the thrust bearings 12 are not arranged symmetrically to the center, but have to in Fig. 24 To the left of the thrust bearing 12 arranged thrust bearing 11, the distance n 'and to the in Fig. 24 each right to the pressure bearing 12 arranged thrust bearing 11, the larger distance n.
  • Another symmetrical or asymmetrical arrangement and number of thrust bearings 12 and pressure thrust bearings 11 may be advantageous.
  • the arrangements shown can be repeated as often as desired to form components 1 of greater length.
  • the thrust bearing 11 and / or the thrust bearing 12 advantageously consist essentially of a castable and / or sprayable, curable material.
  • the material advantageously comprises plastic or a mineral base material.
  • the thrust bearing 11 consist of dimensionally stable plastic or fiber cement.
  • the height of the thrust thrust bearing 11 need not be constant either in the transverse direction 7 or in the longitudinal direction 6, but may change in the transverse direction 7 and / or in the longitudinal direction 6.
  • the thrust bearing 12 and thrust bearing 11 need not have symmetry.
  • the width and / or the supernatant of the thrust bearing 12 and / or the pressure thrust bearing 11 can on the longitudinal side 9 and the longitudinal side 10 be different in size.
  • the radii on the two longitudinal sides 9 and 10 and / or the position of the centers of the radii on the two longitudinal sides 9 and 10 may be different in a thrust bearing 12 and / or at a pressure thrust bearing 11.
  • the thrust bearing 12 and the pressure thrust bearing 11 may have the same length measured in the longitudinal direction 6 in the longitudinal sides 9 and 10. However, different widths for the thrust bearing 12 and the thrust bearing 11 may be advantageous. In particular, if the thrust bearing 12 has a greater width than the pressure thrust bearing 11, it may be advantageous that the thrust bearing 12 has a larger radius at its end faces than the thrust thrust bearing 11. Also, the supernatant f of the thrust bearing 12 in the adjacent component may be greater as the supernatant e of the thrust thrust bearing 11th

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Acoustics & Sound (AREA)
  • Building Environments (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
EP17000569.8A 2017-04-05 2017-04-05 Composant à isolation thermique Active EP3385462B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
PL17000569T PL3385462T3 (pl) 2017-04-05 2017-04-05 Termoizolacyjny element budowlany
EP17000569.8A EP3385462B1 (fr) 2017-04-05 2017-04-05 Composant à isolation thermique
US15/938,439 US20180291620A1 (en) 2017-04-05 2018-03-28 Thermally insulating construction element
CN201810310123.3A CN108691366A (zh) 2017-04-05 2018-04-03 起热隔离作用的结构元件

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP17000569.8A EP3385462B1 (fr) 2017-04-05 2017-04-05 Composant à isolation thermique

Publications (2)

Publication Number Publication Date
EP3385462A1 true EP3385462A1 (fr) 2018-10-10
EP3385462B1 EP3385462B1 (fr) 2020-03-04

Family

ID=58544680

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17000569.8A Active EP3385462B1 (fr) 2017-04-05 2017-04-05 Composant à isolation thermique

Country Status (4)

Country Link
US (1) US20180291620A1 (fr)
EP (1) EP3385462B1 (fr)
CN (1) CN108691366A (fr)
PL (1) PL3385462T3 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016124736A1 (de) * 2016-12-19 2018-06-21 Schöck Bauteile GmbH Bauelement zur Wärmedämmung
GB201819196D0 (en) * 2018-11-26 2019-01-09 Ancon Ltd Building element, system and method
US20220010545A1 (en) * 2020-07-09 2022-01-13 Meadow Burke, Llc Reinforcement for a connector in a precast concrete panel

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1564336A1 (fr) 2004-02-11 2005-08-17 HALFEN GmbH & CO. Kommanditgesellschaft Elément de construction thermo-isolant
DE102011054275A1 (de) 2011-10-07 2013-04-11 Max Frank Gmbh & Co Kg Kragplattenanschlusselement

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1058548A (en) * 1912-10-14 1913-04-08 Francois Cancalon Construction of armored-concrete floors and ceilings.
DE10102930A1 (de) * 2001-01-23 2002-07-25 Schoeck Entwicklungsgmbh Bauelement zur Wärmedämmung
DE59208345D1 (de) * 1991-02-15 1997-05-22 Reto Bonomo Wärmedämmendes Kragplattenanschlusselement und Verwendung desselben
DE20010770U1 (de) * 2000-06-13 2000-09-21 Diesler Joerg Hochwärmedämmender Bewehrungskorb mit wärmedämmenden Bewehrungsgliedern
DE10102931A1 (de) * 2001-01-23 2002-07-25 Schoeck Entwicklungsgmbh Bauelement zur Wärmedämmung
DE102005039025A1 (de) * 2005-08-18 2007-02-22 Schöck Bauteile GmbH Bauelement zur Wärmedämmung
DE102006011335A1 (de) * 2006-03-09 2007-09-13 Schöck Bauteile GmbH Bauelement zur Wärmedämmung
DE102006011336A1 (de) * 2006-03-09 2007-09-13 Schöck Bauteile GmbH Bauelement zur Wärmedämmung
PL1892344T3 (pl) * 2006-08-22 2009-04-30 Halfen Gmbh Termoizolacyjny element konstrukcyjny
DE102008029701A1 (de) * 2008-06-24 2009-12-31 Schöck Bauteile GmbH Bauelement zur Wärmedämmung und Dämmmaterial für Bauanwendungen
US8991124B2 (en) * 2008-10-17 2015-03-31 Schöck Bauteile GmbH Concrete material, construction element for a thermal insulation, and brick-shaped thermally insulating element, each using the concrete material
DE102011122589A1 (de) * 2011-12-30 2013-07-04 Schöck Bauteile GmbH Bauelement zur Wärmedämmung
EP2653625B1 (fr) * 2012-04-20 2018-11-21 HALFEN GmbH Composant à isolation thermique
DE202013006229U1 (de) * 2013-07-11 2014-10-13 H-Bau Technik Gmbh Thermisch isolierendes Bauteil
CN205804643U (zh) * 2016-04-27 2016-12-14 青岛被动屋工程技术有限公司 一种用于室内外结构连接的断桥隔热构件
CN205857423U (zh) * 2016-07-22 2017-01-04 欧联（杭州）节能建筑技术研究有限公司 用于建筑外维护结构下的断桥非金属保温构件

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1564336A1 (fr) 2004-02-11 2005-08-17 HALFEN GmbH & CO. Kommanditgesellschaft Elément de construction thermo-isolant
DE102011054275A1 (de) 2011-10-07 2013-04-11 Max Frank Gmbh & Co Kg Kragplattenanschlusselement

Also Published As

Publication number Publication date
US20180291620A1 (en) 2018-10-11
PL3385462T3 (pl) 2020-11-16
EP3385462B1 (fr) 2020-03-04
CN108691366A (zh) 2018-10-23

Similar Documents

Publication Publication Date Title
DE102018205997B4 (de) Siebsystem mit genuteten Traversen
EP2653625B1 (fr) Composant à isolation thermique
EP1892344A1 (fr) Elément de construction thermo-isolant
EP3385462B1 (fr) Composant à isolation thermique
DE19711813C2 (de) Thermisch isolierendes Bauelement
DE4203815A1 (de) Betonfertigplatte fuer einen verbundboden
DE19543768A1 (de) Balkonanschluß
EP1463862B1 (fr) Element de connexion de dalles en console et ensemble de connexion de dalles en console comprenant de tels elements de connexion de dalles en console
EP3296476B1 (fr) Dispositif de liaison d'un mur de bâtiment à une dalle de sol ou de plafond et élément de moulage d'un tel système
EP3502350A1 (fr) Raccordement de deux éléments de paroi de guidage
EP0657592B1 (fr) Elément de construction pour isolation thermique
EP0933482B1 (fr) Elément préfabriqué pour dalle de balcon en porte-à-faux
EP2080845B1 (fr) Elément préfabriqué en bois
DE202021105966U1 (de) Abstandhalterleiste
AT520195B1 (de) Dämmmaterialfreier Hochlochziegel mit tragender Lamellenstruktur zur Gebäudekonstruktion
EP3545210B1 (fr) Agencement d'amortissement et de ressort et son procédé de fabrication
DE202020102526U1 (de) Mehrprofilpaneel
WO2015062617A1 (fr) Panneau composite
EP3663474A1 (fr) Dispositif d'isolement thermique entre un mur de bâtiment bétonné et un plancher, ainsi que procédé de fabrication
DE4434658C2 (de) Dämmplatte und Verfahren zur Herstellung einer Dämmplatte
EP3733988B1 (fr) Élément de construction thermo-isolant
EP1612342A2 (fr) Brique perforée, procédé et filière
EP3202991A1 (fr) Composant à isolation thermique
DE202016101363U1 (de) Formsteinverbundsystem
DE19804729A1 (de) Baustein, insbesondere auf der Basis zementgebundenen Blähtons

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

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

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

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

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17P Request for examination filed

Effective date: 20190328

RBV Designated contracting states (corrected)

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

17Q First examination report despatched

Effective date: 20190506

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20190930

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

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

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1240505

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200315

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502017004029

Country of ref document: DE

Representative=s name: PATENTANWAELTE DIPL.-ING. W. JACKISCH & PARTNE, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502017004029

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: ISLER AND PEDRAZZINI AG, CH

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

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

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: 20200304

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: 20200304

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: 20200604

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

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: 20200304

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: 20200604

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: 20200605

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: 20200304

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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

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: 20200304

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: 20200304

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: 20200304

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: 20200304

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: 20200704

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: 20200729

Ref country code: ES

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: 20200304

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: 20200304

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: 20200304

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502017004029

Country of ref document: DE

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: 20200304

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

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: 20200304

Ref country code: LU

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

Effective date: 20200405

26N No opposition filed

Effective date: 20201207

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: 20200304

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: 20200405

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

Effective date: 20210405

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 502017004029

Country of ref document: DE

Owner name: LEVIAT GMBH, DE

Free format text: FORMER OWNER: HALFEN GMBH, 40764 LANGENFELD, DE

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

Ref country code: GB

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

Effective date: 20210405

REG Reference to a national code

Ref country code: BE

Ref legal event code: HC

Owner name: LEVIAT GMBH; DE

Free format text: DETAILS ASSIGNMENT: CHANGE OF OWNER(S), CHANGE OF OWNER(S) NAME; FORMER OWNER NAME: HALFEN GMBH

Effective date: 20220211

REG Reference to a national code

Ref country code: NL

Ref legal event code: PD

Owner name: LEVIAT GMBH; DE

Free format text: DETAILS ASSIGNMENT: CHANGE OF OWNER(S), MERGE; FORMER OWNER NAME: HALFEN GMBH

Effective date: 20220316

REG Reference to a national code

Ref country code: AT

Ref legal event code: HC

Ref document number: 1240505

Country of ref document: AT

Kind code of ref document: T

Owner name: LEVIAT GMBH, DE

Effective date: 20220406

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: 20200304

Ref country code: MT

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: 20200304

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: 20200304

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200304

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: 20200304

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

Ref country code: PL

Payment date: 20230329

Year of fee payment: 7

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

Effective date: 20230522

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

Ref country code: IT

Payment date: 20230426

Year of fee payment: 7

Ref country code: FR

Payment date: 20230424

Year of fee payment: 7

Ref country code: DE

Payment date: 20230420

Year of fee payment: 7

Ref country code: CH

Payment date: 20230502

Year of fee payment: 7

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

Ref country code: SE

Payment date: 20230420

Year of fee payment: 7

Ref country code: AT

Payment date: 20230420

Year of fee payment: 7

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

Ref country code: BE

Payment date: 20230419

Year of fee payment: 7

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

Ref country code: NL

Payment date: 20240418

Year of fee payment: 8