DE3221797A1 - Method of joining metallic inner and outer parts of a composite profile - Google Patents
Method of joining metallic inner and outer parts of a composite profileInfo
- Publication number
- DE3221797A1 DE3221797A1 DE19823221797 DE3221797A DE3221797A1 DE 3221797 A1 DE3221797 A1 DE 3221797A1 DE 19823221797 DE19823221797 DE 19823221797 DE 3221797 A DE3221797 A DE 3221797A DE 3221797 A1 DE3221797 A1 DE 3221797A1
- Authority
- DE
- Germany
- Prior art keywords
- jacket
- outer parts
- composite profile
- insulating
- adhesive
- 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.)
- Withdrawn
Links
Classifications
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- 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
- E06B3/277—Frames with special provision for insulation with prefabricated insulating elements held in position by expansion of the extremities of the insulating elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/3404—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint
- B29C65/342—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint comprising at least a single wire, e.g. in the form of a winding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/3472—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint
- B29C65/3476—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint being metallic
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/481—Non-reactive adhesives, e.g. physically hardening adhesives
- B29C65/4815—Hot melt adhesives, e.g. thermoplastic adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
- B29C65/4835—Heat curing adhesives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4855—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by their physical properties, e.g. being electrically-conductive
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4865—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives
- B29C65/487—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their shape, e.g. being fibres or being spherical
- B29C65/4875—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their shape, e.g. being fibres or being spherical being spherical, e.g. particles or powders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
- B29C65/5021—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being multi-layered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
- B29C65/5035—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being in thread form, i.e. in the form of a single filament, e.g. in the form of a single coated filament
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5057—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/52—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive
- B29C65/54—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts
- B29C65/542—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the way of applying the adhesive between pre-assembled parts by injection
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/124—Tongue and groove joints
- B29C66/1242—Tongue and groove joints comprising interlocking undercuts
- B29C66/12423—Dovetailed interlocking undercuts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/124—Tongue and groove joints
- B29C66/1244—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue
- B29C66/12441—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue being a single wall
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections
- B29C66/4344—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces
- B29C66/43441—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces with two right angles, e.g. for making T-shaped pieces, H-shaped pieces
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/524—Joining profiled elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
- B29C66/3032—Particular design of joint configurations the joint involving an anchoring effect making use of protusions or cavities belonging to at least one of the parts to be joined
- B29C66/30321—Particular design of joint configurations the joint involving an anchoring effect making use of protusions or cavities belonging to at least one of the parts to be joined making use of protusions belonging to at least one of the parts to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
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- 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
- E06B3/26301—Frames with special provision for insulation with prefabricated insulating strips between two metal section members
- E06B3/26305—Connection details
- E06B2003/26309—Connection details using glue
-
- 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
- E06B3/26301—Frames with special provision for insulation with prefabricated insulating strips between two metal section members
- E06B3/26305—Connection details
- E06B2003/26314—Provisions for reducing the shift between the strips and the 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
- E06B3/04—Wing frames not characterised by the manner of movement
- E06B3/263—Frames with special provision for insulation
- E06B3/273—Frames with special provision for insulation with prefabricated insulating elements held in position by deformation of portions of the metal frame members
Abstract
Description
Beschreibung description
Verfahren zum Verbinden der metallischen Innen-und Aussenteile eines Verbundprofils Die Erfindung betrifft ein Verfahren zum Verbinden der metallischen Innen- und Aussenteile eines Verbundprofils mit einem Isoliersteg, der mit seinen Enden in Nuten der Innen- und Aussenteile eingreift, bei dem man im Bereich der Enden des Isolierstegs ein Zusatzmaterial in Form mindestens eines Drahtes, Streifens oder einer Schnur einbringt und es durch Druck und/oder Wärme in seinen Materialeigenschaften derart modifiziert, insbesondere verformt, dass sich ein verbesserter Form-, Kraft- und/oder Stoffschluss zwischen Isoliersteg und den Innen- und Aussenteilen des Verbundprofils ergibt, nach Patent . . Method for connecting the metallic inner and outer parts of a Composite profile The invention relates to a method for connecting the metallic Inner and outer parts of a composite profile with an insulating bar, which with his Ends in grooves of the inner and outer parts engages, in which one in the area of Ends of the insulating bar an additional material in the form of at least one wire, strip or a cord and its material properties through pressure and / or heat modified in such a way, in particular deformed, that an improved form, force and / or material connection between the insulating web and the inner and outer parts of the composite profile results, according to patent. .
(Patentanmeldung P 32 03 631.0).(Patent application P 32 03 631.0).
Es ist Aufgabe der Erfindung, das Verfahren nach dem Hauptpatent zu verbessern, insbesondere die Einbringung von Zusatzmaterialien, die gleichzeitig eine Klebe- und eine Formschlussverbindung ergeben, zu erleichtern und hierdurch die Herstellung der in Rede stehenden Verbundprofile bei gesteigerter Schubfestigkeit zu rationalisieren.It is the object of the invention to provide the method according to the main patent improve, especially the introduction of additional materials, at the same time result in an adhesive and a form-fit connection, to facilitate and thereby the production of the composite profiles in question with increased shear strength to streamline.
Die Aufgabe wird erfindungsgemäss dadurch gelöst, dass man als Zusatzmaterial einen in Querrichtung des Materials expandierbaren Körper verwendet, auf den ein klebefähiger Mantel aufgebracht ist.The object is achieved according to the invention in that the additional material an expandable body used in the transverse direction of the material, onto which a adhesive coat is applied.
Hierbei führt der expandierende, die "Seele" des Zusatzmaterials bildende Körper zu einem verbesserten Formschluss, während der aus einem Kleber bestehende Mantel - unterstützt durch die Expansion der "Seele" - zu einer stoffschlüssigem, grossflächigen Klebeverbindung führt.Here, the expanding, forming the "soul" of the additional material, leads Body for an improved form fit, while that consists of an adhesive Coat - supported by the expansion of the "soul" - to a cohesive, large adhesive bond leads.
Die nachstehende Beschreibung bevorzugter Ausführungsformen der Erfindung dient im Zusammenhang mit beiliegender Zeichnung der weiteren Erläuterung. Es zeigen: Fig. 1 eine schaubildliche Schnittansicht eines Verbundprofils für Fenster, Türen, Fassadenelemente o.dgl.; Fig.1a ein draht- oder schnurförmiges Zusatzmaterial, bestehend aus einer von einem Mantel umhüllten Seele; Fig. 2 Teilansichten im Bereich A in Fig.1 zur bis Darstellung verschiedener Verfahren zum Ver-Fig. 5 binden der metallischen Innen- und Aussenteile des in Fig.1 dargestellten Verbundprofils; Fig. 6 schaubildliche Schnittansichten bevorzugter und 7 Ausführungsformen von Zusatzmaterialien mit zusätzlichem Gleitschutz; Fig. 8 Teilansichten ähnlich Fig. 2 bis 5 zur Dar-und 9 stellung anderer bevorzugter Ausführungsformen des erfindungsgemässen Verfahrens.The following description of preferred embodiments of the invention serves for further explanation in connection with the accompanying drawing. Show it: 1 is a diagrammatic sectional view of a composite profile for windows, doors, Facade elements or the like; Fig.1a a wire or cord-shaped additional material, consisting from a soul wrapped in a cloak; Fig. 2 partial views in area A in Fig. 1 to illustrate various methods for Ver-Fig. 5 tie the metallic Inner and outer parts of the composite profile shown in Figure 1; Fig. 6 diagrammatic Sectional views of preferred and 7 embodiments of additional materials with additional Anti-skid; 8 partial views similar to FIGS. 2 to 5 for the representation and 9 position of others preferred embodiments of the method according to the invention.
Die Fig. 1 zeigt ein z.B. für die Herstellung von Fenstern, Türen, Fassadenelementen o.dgl. geeignetes Metall-Verbundprofil 1 mit einem Innenteil 2 und einem Aussenteil 3, die beide durch zwei längs verlaufende Isolierstege- 4, 5 miteinander verbunden sind. Die Teile 2, 3 können beispielsweise aus Aluminium, Aluminiumlegierung oder Stahl bestehen. Die Isolierstege 4, 5, welche eine wärmedämmende Brücke zwischen den Teilen 2, 3 herstellen, bestehen aus hochfestem Kunststoff mit schlechten Wärmeleitungseigenschaften, beispielsweise aus glasfaserverstärktem Polyamid.Fig. 1 shows a e.g. for the production of windows, doors, Facade elements or the like. suitable metal composite profile 1 with an inner part 2 and an outer part 3, both of which are supported by two longitudinal insulating bars 4, 5 are connected to each other. The parts 2, 3 can for example made of aluminum, aluminum alloy or steel. The insulating bars 4, 5, which Create a heat insulating bridge between parts 2, 3, are made of high strength Plastic with poor heat conduction properties, for example made of glass fiber reinforced Polyamide.
Die Isolierstege 4, 5 regen mit ihren im Querschnitt schwalbenschwanzförmig ausgebildeten Enden 6 in entsprechend ausgebildete, längs verlaufende Nuten 7 der Verbundprofilteile 2, 3 hinein (vgl. Fig. 2). Dabei bildet sich im fertigen Verbundprofil 1 zwischen den Isolierstegen 4, 5 und Wandabschnitten 8, 9 der Teile 2 bzw. 3 eine längsweise durchgehende Kammer 11 aus. Die Isolierstege 4, 5 werden zunächst mit ihren Enden längsweise in die Nuten 7 eingesetzt, beispielsweise eingezogen. Anschliessend wird in Längsrichtung des Profils ein Ziehdorn durch die Kammer 11 hindurchgezogen, wodurch die in dieser Kammer liegenden, die Nut 7 begrenzenden Stege (in Fig.2 mit 12 bezeichnet) an die Enden 6 der Isolierstege 4, 5 angedrückt werden, so dass die Isolierstege 4, 5 schliesslich zwischen dem erwähnten Steg 12 und einem gegenüberliegenden Nutensteg (in Fig.2 mit 13 bezeichnet) formschlüssig gehalten sind.The insulating webs 4, 5 rain with their dovetail-shaped cross-section formed ends 6 in correspondingly formed, longitudinal grooves 7 of the Composite profile parts 2, 3 into it (see. Fig. 2). This forms in the finished composite profile 1 between the insulating webs 4, 5 and wall sections 8, 9 of the parts 2 and 3, respectively longitudinally continuous chamber 11 from. The insulating bars 4, 5 are initially with their ends inserted lengthwise into the grooves 7, for example drawn in. Afterward a mandrel is drawn through the chamber 11 in the longitudinal direction of the profile, whereby the webs lying in this chamber, delimiting the groove 7 (in FIG 12) are pressed against the ends 6 of the insulating webs 4, 5, so that the Finally, insulating webs 4, 5 between the mentioned web 12 and an opposite one Groove web (denoted by 13 in Figure 2) are held in a form-fitting manner.
Die Fig. 2 bis 5 und 8, 9 zeigen jeweils Ausschnitte im Bereich des in Fig.1 mit A bezeichneten Kreises. Verschiedene Ausführungsformen erfindungsgemässer Verfahren werden anschliessend unter Zugrunde legen dieses Ausschnittes A an Hand der erwähnten Figuren erläutert. Diese Ausführungen beziehen sich in gleicher Weise auch auf die übrigen drei, in Fig. licht eigens bezeichneten Stellen, an welchen jeweils die schwalbenschwanzförmigen Enden 6 der Isolierstege 4, 5 in entsprechende Nuten 7 der Verbundprofilteile eingefügt sind.FIGS. 2 to 5 and 8, 9 each show details in the area of the in Figure 1 with A designated circle. Various embodiments according to the invention Procedures are then based on this section A at hand of the figures mentioned. These statements refer in the same way also to the other three places, specially marked in Fig. Licht, at which the dovetail-shaped ends 6 in each case the insulating bars 4, 5 are inserted into corresponding grooves 7 of the composite profile parts.
Bei der Ausführungsform gemäss Fig. 2 wird in eine längs verlaufende Ausnehmung 14 am schwalbenschanzförmigen Ende 6 des Isoliersteges 4 ein Zusatzmaterial in Gestalt einer biegsamen Schnur oder eines biegsamen Drahtes 15 eingelegt und durch entsprechende Verformung des Nutensteges 12 gemeinsam mit dem Ende 6 in der von diesem Steg und dem gegenüberliegenden Nutensteg 13 gebildeten Nut eingeschlossen. Der Durchmesser des Drahtes 15 ist vorzugsweise so gewählt, dass er sich in die Nut 14 leicht einlegen, insbesondere einstecken lässt und an seinem Platze verharrt. Wie dargestellt, besteht der Draht 15 aus einem durchgehenden, zentralen, eine "Seele" bildenden Körper 16, der ringsum von einem Mantel 17 umhüllt ist.In the embodiment according to FIG. 2, a longitudinal one is used Recess 14 at the dovetail-shaped end 6 of the insulating web 4 is an additional material inserted in the form of a flexible cord or a flexible wire 15 and by corresponding deformation of the groove web 12 together with the end 6 in the Enclosed by this web and the opposite groove web 13 formed groove. The diameter of the wire 15 is preferably chosen so that it is in the Easily insert groove 14, in particular can be inserted and remain in place. As shown, the wire 15 consists of a continuous, central, a "core" forming body 16 which is encased all around by a jacket 17.
Das den Körper 16 bildende Material ist so gewählt, dass es durch Druck und/oder Wärme in Querrichtung (radial) expandiert und hierdurch das Ende 6 des Isolierstegs 4 unter Ausbildung eines verbesserten Formschlusses in die Nut 7 hineinpresst. Das den Mantel 17 bildende Material ist ein Kleber, der bei Anwendung von Druck und/oder Wärme zu fliessen beginnt und sich in die Zwischenräume zwischen dem Ende 6 des Isolierstegs 4 und der Nut 7 ergiesst, wenn das Material des Körpers 16 sich expandiert. Auf diese Weise wird eine grossflächige Klebeverbindung zwischen dem Ende 6 des Isolierstegs 4 und der Innenseite der Nut 7 vermittelt, wie schematisch dargestell#4#Insgesamt in Fig.3 dargestell t Insgesamt wird durch diese Massnahme die Schubfestigkeit der beiden das Verbundprofil 1 bildenden Teile 2, 3 durch Ausbildung einer verstärkten Klebe- und Formschlussverbindung erhöht.The material forming the body 16 is chosen so that it through Pressure and / or heat in the transverse direction (radial) expands and thereby the end 6 of the insulating web 4 with the formation of an improved form fit in the groove 7 presses into it. The material forming the jacket 17 is an adhesive which, when used of pressure and / or heat begins to flow and spread into the spaces between the end 6 of the insulating web 4 and the groove 7 pours out when the material of the body 16 expands. In this way, a large-area adhesive connection between the end 6 of the insulating web 4 and the inside of the groove 7 mediated, as shown schematically illustrated # 4 # Overall in FIG. 3, this measure the shear strength of the two parts 2, 3 forming the composite profile 1 through training a reinforced adhesive and form-fit connection increased.
Der Körper 16 ist vorzugsweise ein Monofilament aus Kunststoff, insbesondere aus gerecktem oder ungerecktem einheitlichem oder Copolyamid oder Äthylencopolymerisat oder jonomerem Kunststoff. Als Material für den Mantel 17 eignen sich Schmelzkleber in der Form von Copolymerisaten auf Acrylsäure- und Acrylsäureesterbasis oder Sthylencopolymeri aten sowie jonomere Schmelzkleber; auch Duroplaste sind für den Mantel 17 verwendbar.The body 16 is preferably a monofilament made of plastic, in particular made of stretched or unstretched uniform or copolyamide or ethylene copolymer or ionomeric plastic. Melt adhesives are suitable as the material for the jacket 17 in the form of copolymers based on acrylic acid and acrylic acid esters or ethylene copolymers aten as well as ionomer hot melt adhesive; Duroplasts can also be used for the jacket 17.
Bei besonders bevorzugten Ausführungsformen der Erfindung können die für die Bildung des Körpers 16 und/oder des Mantels 17 verwendeten Materialien auch ein bei Anwendung von Druck und/oder Wärme expandierendes Treibmittel enthalten, welches die Querausdehnung des Körpers 16 bzw.In particularly preferred embodiments of the invention, the materials used for the formation of the body 16 and / or the jacket 17 as well contain a propellant that expands when pressure and / or heat are applied, which is the transverse extent of the body 16 or
die grossflächige Verteilung des Mantelmaterials in der Nut 7 begünstigen. Als Treibmittel können beispielsweise verwendet werden: Azodicarbonamide und/oder Natriumbicarbonat Das an Hand von Fig. 4 und 5 dargestellte Verfahren gemäss der Erfindung läuft genauso ab wie das an Hand der Fig. 2 und 3 erläuterte Verfahren. Während jedoch in Fig.2 und 3 der Körper 16 ringsum vom Mantel 17 umgeben ist, bedeckt in Fig. 4 und 5 der Mantel 17 den Körper 16 zunächst nur an dessen Oberseite, wobei Körper 16 und Mantel 17 die Gestalt eines flexiblen Bandes oder Streifens haben.favor the large-area distribution of the jacket material in the groove 7. The following can be used as propellants, for example: azodicarbonamides and / or Sodium bicarbonate The method illustrated with reference to FIGS. 4 and 5 according to FIG The invention proceeds in exactly the same way as the method explained with reference to FIGS. 2 and 3. However, while in Figure 2 and 3 the body 16 is surrounded all around by the jacket 17, covered in Fig. 4 and 5, the jacket 17, the body 16 initially only on its upper side, wherein Body 16 and jacket 17 are in the form of a flexible band or strip.
Bei Anwendung von Druck und/oder Wärme expandiert der Körper 16, während der Mantel 17 schmilzt und in die Zwischenräume zwischen dem Ende 6 des Steges 4 und der Nut 7 eindringt. Die Fig.4 zeigt den Anfangs-, die Fig. 5 den Endzustand.When pressure and / or heat is applied, the body 16 expands while the jacket 17 melts and into the spaces between the end 6 of the web 4 and the groove 7 penetrates. FIG. 4 shows the initial state, FIG. 5 the final state.
Wie in Fig. 4 und 5 schematisch dargestellt, weist der Boden der Nut 7 zusätzlich eine Querrändelung 18 auf, in welche das expandierende Material des Körpers 16 sowie das schmelzflüssige Material des Mantels 17 eindringen kann. Hierdurch ergibt sich ein- weiterhin verbesserter Form- und Stoffschluss zwischen Isoliersteg 4 und Verbundprofilteil. Eine Rändelung 18 könnte im übrigen auch auf den dem Ende 6 des Isolierstegs 4 zugewandten Innenseiten der Stege 12, 13 vorgesehen werden. Eine entsprechende Aufrauhung oder Rändelung könnten im übrigen auch die Innenseiten der Nut 7 bei der Ausführungsform gemäss Fig. 2 und 3 aufweisen. Auch bei dem Verfahren nach Fig. 4 und 5 könnten die Materialien des Körpers 16 und des Mantels 17 wieder mit einem Treibmittel der oben beschriebenen Art versehen sein.As shown schematically in Fig. 4 and 5, the bottom of the groove 7 also has a transverse knurling 18, in which the expanding material of the Body 16 and the molten material of the jacket 17 can penetrate. Through this the result is a further improved form and material fit between the insulating web 4 and composite profile part. A knurling 18 could also be on the end 6 of the insulating web 4 facing inner sides of the webs 12, 13 are provided. A corresponding roughening or knurling could also be used on the inside of the groove 7 in the embodiment according to FIGS. Even with the procedure 4 and 5, the materials of the body 16 and the jacket 17 could be used again be provided with a propellant of the type described above.
Die in Fig. 6 dargestellte Ausführungsform einer Schnur oder eines Drahtes 15 besteht wiederum aus einem Innenkörper 16 und einem diesen umgebenden Mantel 17. In den Mantel 17 sind harte, scharfkantige Partikel 19, insbesondere Metallteilchen, Metallspäne, Quarzkörner o.dgl.# eingebettet, die beim Expandieren des Körpers 16 und beim Schmelzen des Mantels 17den Reibschluss gegenüber den Innenseiten der Nut 7 erhöhen, wodurch die Schubfestigkeit zwischen dem Isoliersteg 4, 5 und den Verbundprofilteilen 2, 3 weiterhin erhöht ist.The embodiment shown in Fig. 6 of a cord or one Wire 15 in turn consists of an inner body 16 and a surrounding it Shell 17. In the shell 17 are hard, sharp-edged particles 19, in particular Metal particles, metal shavings, quartz grains or the like. # Embedded that when expanding of the body 16 and when the jacket 17 melts the frictional engagement with respect to the inner sides the groove 7 increase, whereby the shear strength between the insulating web 4, 5 and the composite profile parts 2, 3 is still increased.
In Fig. 7 sind in den Klebemantel 17 und teilweise auch in den expandierfähigen Körper 16 zwei Metalidrähte 20, beispielsweise aus Stahl von dreieckigem Profil und aufgerauhter, insbesondere geriefter Oberfläche eingelegt, wobei die geriefte Oberfläche etwas gegenüber der Umfangsfläche des Mantels 17 vorsteht. die Drähte 20 sind vorzugsweise an ihren drei Seiten aufgerauht, insbesondere quergerieft. Beim Expandieren des Körpers 16 und Schmelzen des Mantels 17 werden die Drähte 20 radial nach aussen verschoben und gelangen in formschlüssigen Eingriff mit den Enden der Nut 7 bzw. der Oberseite des Isolierstegs 4. Wenn insbesondere an den Innenseiten der Nut 7 eine Rändelung oder andere Oberflächenrauhigkeit vorgesehen ist, entsteht ein besonders guter formschlüssiger Eingriff. Die Drähte 20 erstrecken sich, wie aus Fig. 7 ersichtlich ist, achsparallel im Körper 16 und Mantel 17.In Fig. 7 are in the adhesive jacket 17 and partially in the expandable Body 16 two metal wires 20, for example made of steel with a triangular profile and a roughened, in particular grooved surface, the grooved Surface slightly protrudes from the circumferential surface of the jacket 17. the wires 20th are preferably roughened on their three sides, in particular grooved across. When the body 16 is expanded and the jacket 17 melts the wires 20 are displaced radially outward and come into positive engagement with the ends of the groove 7 or the top of the insulating web 4. If in particular a knurling or other surface roughness is provided on the inside of the groove 7 is a particularly good form-fitting engagement. The wires 20 extend As can be seen from FIG. 7, they are axially parallel in the body 16 and jacket 17.
Bei der in Fig.8 gezeigten Ausführungsform ist ein wiederum aus Körper 16 und Mantel 17 bestehender Draht 15 insgesamt in das Ende 6 des Isolierstegs 4 eingelegt und allseits von diesem umschlossen. Im Ende 6 des Isolierstegs 4 erstrecken sich radial verlaufende Kanäle 21, die vom Aussenumfang des Drahtes 15 bis zu den Aussenseiten des Endes 6 reichen. Wenn unter dem Einfluss von Wärme und/oder Druck der Körper 16 expandiert und das Material des Mantels 17 schmilzt, wird das geschmolzene Klebematerial des Mantels 17 durch die Kanäle 21 hindurch in den Zwischenraum zwischen dem Ende 6 des Isolierstegs 4 und den Innenseiten der Nut 7 gepresst, wo es sich gleichmässig verteilt und zu einer verbesserten, grossflächigen Klebeverbindung führt.In the embodiment shown in FIG. 8, one is again made of a body 16 and sheath 17 existing wire 15 as a whole into the end 6 of the insulating web 4 inserted and enclosed on all sides by this. Extend in the end 6 of the insulating web 4 radially extending channels 21 extending from the outer circumference of the wire 15 to the 6 end outsides reach. When under the influence of heat and / or pressure the body 16 expands and the material of the jacket 17 melts, the melted one becomes Adhesive material of the jacket 17 through the channels 21 through into the space between the end 6 of the insulating web 4 and the inside of the groove 7 pressed where it is evenly distributed and for an improved, large-area adhesive bond leads.
Auf diese Weise ist ein gezieltes Einspritzen des Klebstoffes an die gewünschte Stelle möglich£#ie in Fig. 9 dargestellte Verfahrensvariante entspricht in ihrer Wirkungsweise den an Hand von Fig. 2 bis 5 erläuterten Verfahren.In this way, a targeted injection of the adhesive to the desired point possible £ # ie corresponds to the variant of the method shown in FIG the method explained with reference to FIGS. 2 to 5 in their mode of operation.
Im Gegensatz zu Fig. 2 bis 5 ist in Fig. 9 der biegsame, aus Körper 16 und Mantel 17 bestehende Draht 15 nicht in eine Nut im Ende 6 des Steges 4, sondern in eine Nut 22 des Verbundprofilteiles 3 eingelegt. Beim Expandieren des Körpers 16 und Schmelzen des aus Kleber bestehenden Mantels 17 wird einerseits das Ende 6 des Isoliersteges 4 unter Erzeugung eines verbesserten Formschlusses fest in die Nut 7 hineingepresst, während andererseits der Kleber des Mantels 17 sich gleichmässig zwischen dem Ende 6 und den Innenseiten der Nut 7 verteilt.In contrast to FIGS. 2 to 5, FIG. 9 shows the flexible, solid body 16 and sheath 17 existing wire 15 not in a groove in the end 6 of the web 4, but inserted into a groove 22 of the composite profile part 3. When expanding of Body 16 and melting of the jacket 17 consisting of adhesive is on the one hand the End 6 of the insulating web 4 firmly to produce an improved form fit pressed into the groove 7, while on the other hand the adhesive of the jacket 17 is evenly distributed between the end 6 and the inner sides of the groove 7.
Claims (12)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19823221797 DE3221797A1 (en) | 1982-06-09 | 1982-06-09 | Method of joining metallic inner and outer parts of a composite profile |
AT83100783T ATE26604T1 (en) | 1982-02-03 | 1983-01-27 | METHOD OF JOINING THE INSIDE AND OUTSIDE METALLIC PARTS OF A COMPOSITE PROFILE. |
EP83100783A EP0085410B2 (en) | 1982-02-03 | 1983-01-27 | Process for joining the metallic inner and outer parts of a composite profile member |
DE8383100783T DE3370979D1 (en) | 1982-02-03 | 1983-01-27 | Process for joining the metallic inner and outer parts of a composite profile member |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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DE19823221797 DE3221797A1 (en) | 1982-06-09 | 1982-06-09 | Method of joining metallic inner and outer parts of a composite profile |
Publications (1)
Publication Number | Publication Date |
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DE3221797A1 true DE3221797A1 (en) | 1983-12-15 |
Family
ID=6165729
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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DE19823221797 Withdrawn DE3221797A1 (en) | 1982-02-03 | 1982-06-09 | Method of joining metallic inner and outer parts of a composite profile |
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DE (1) | DE3221797A1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3545887A1 (en) * | 1985-12-23 | 1987-07-02 | Gartner & Co J | Heat-insulated insulating profile |
DE9013374U1 (en) * | 1990-09-21 | 1991-12-05 | Hymer Ag, 7967 Bad Waldsee, De | |
DE4235687A1 (en) * | 1992-10-22 | 1994-05-05 | Klemens Schlachter | Building heat-insulation system - has profiled members securing panes etc. and held apart by hard foam material |
WO2002086008A1 (en) * | 2001-04-20 | 2002-10-31 | Mazzer Materie Plastiche Di Giacomo Ezio Mazzer & C. S.N.C. | Heat-sensitive adhesive insert for heat-insulating composite metal sections |
EP3680091A1 (en) * | 2019-01-11 | 2020-07-15 | Subaru Corporation | Joint structure |
US11225825B2 (en) * | 2018-06-12 | 2022-01-18 | Arconic Technologies Llc | Thermal separator with integrated fluid seal |
-
1982
- 1982-06-09 DE DE19823221797 patent/DE3221797A1/en not_active Withdrawn
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3545887A1 (en) * | 1985-12-23 | 1987-07-02 | Gartner & Co J | Heat-insulated insulating profile |
DE9013374U1 (en) * | 1990-09-21 | 1991-12-05 | Hymer Ag, 7967 Bad Waldsee, De | |
DE4235687A1 (en) * | 1992-10-22 | 1994-05-05 | Klemens Schlachter | Building heat-insulation system - has profiled members securing panes etc. and held apart by hard foam material |
WO2002086008A1 (en) * | 2001-04-20 | 2002-10-31 | Mazzer Materie Plastiche Di Giacomo Ezio Mazzer & C. S.N.C. | Heat-sensitive adhesive insert for heat-insulating composite metal sections |
US11225825B2 (en) * | 2018-06-12 | 2022-01-18 | Arconic Technologies Llc | Thermal separator with integrated fluid seal |
EP3680091A1 (en) * | 2019-01-11 | 2020-07-15 | Subaru Corporation | Joint structure |
EP3954532A1 (en) * | 2019-01-11 | 2022-02-16 | Subaru Corporation | Joint structure |
EP3974161A1 (en) * | 2019-01-11 | 2022-03-30 | Subaru Corporation | Joint structure |
US11339813B2 (en) | 2019-01-11 | 2022-05-24 | Subaru Corporation | Joint structure |
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