WO2003046390A2 - Method for fixing an insert in a component consisting of a lightweight material - Google Patents
Method for fixing an insert in a component consisting of a lightweight material Download PDFInfo
- Publication number
- WO2003046390A2 WO2003046390A2 PCT/DE2002/004227 DE0204227W WO03046390A2 WO 2003046390 A2 WO2003046390 A2 WO 2003046390A2 DE 0204227 W DE0204227 W DE 0204227W WO 03046390 A2 WO03046390 A2 WO 03046390A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- insert
- recess
- component
- thermoplastic material
- sonotrode
- 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.)
- Ceased
Links
Classifications
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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
- B29C66/40—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
- B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
- B29C66/474—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/002—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature
- B22F7/004—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature comprising at least one non-porous part
- B22F7/006—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature comprising at least one non-porous part the porous part being obtained by foaming
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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
- B29C65/08—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
-
- 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
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/64—Joining a non-plastics element to a plastics element, e.g. by force
- B29C65/645—Joining a non-plastics element to a plastics element, e.g. by force using friction or ultrasonic vibrations
-
- 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
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
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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
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
-
- 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 protrusions or cavities belonging to at least one of the parts to be joined
- B29C66/30325—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined making use of cavities belonging to at least one of the parts to be joined
- B29C66/30326—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined making use of cavities belonging to at least one of the parts to be joined in the form of porosity
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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
- B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
-
- 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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/832—Reciprocating joining or pressing tools
- B29C66/8322—Joining or pressing tools reciprocating along one axis
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B13/00—Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose
- F16B13/14—Non-metallic plugs or sleeves; Use of liquid, loose solid or kneadable material therefor
- F16B13/141—Fixing plugs in holes by the use of settable material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/04—Devices for fastening nuts to surfaces, e.g. sheets, plates
- F16B37/048—Non-releasable devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
-
- 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
- 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
- B29C66/74—Joining plastics material to non-plastics material
- B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
- B29C66/7422—Aluminium or alloys of aluminium
-
- 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
- B29C66/74—Joining plastics material to non-plastics material
- B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
- B29C66/7428—Transition metals or their alloys
- B29C66/74283—Iron or alloys of iron, e.g. steel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2001/00—Articles provided with screw threads
- B29L2001/005—Nuts
Definitions
- the invention relates to a method of the type specified in the preamble of claim 1.
- Components made of lightweight materials are increasingly used in vehicle construction in order to reduce the component mass with sufficient strength and rigidity. But they are also used in many areas of mechanical engineering application and characterized by the resolution of the compact and solid structure in an open or closed-cell structure.
- metal mounting elements such as screws, bolts, pins od.
- suitable joining methods are needed, since the mounting elements can not be easily permanently attached to the components.
- Gluing is one of the low-heat joining methods, in which no local weakening of the joining zone but a planar cohesive connection of the joining parts takes place. Their strength is usually higher than that of the cellular material.
- the joining method "gluing" in particular in mixed construction, d. H. have multifunctional properties when using different metallic and / or non-metallic materials and additionally perform tasks such as electrochemical insulation and sealing function. Disadvantages with regard to the process speed are the curing times, which are often several hours at room temperature, of suitable, in particular thermoset reaction adhesives. A shortening of the
- Curing times would indeed be possible by increasing the curing temperature, but requires further expenditure on equipment and financial commitment.
- a method of the type described above is known (DE 695 03 284 T2), in which a plate-shaped, made of foam or honeycomb material component is covered on opposing broad sides with cover layers or thermoplastic material and provided with a specific for receiving an insert recess.
- the insert is made of thermoplastic material and has at its axial ends so-called sacrificial edges which are plasticized by ultrasonic vibrations and melted with the edges of the two cover layers adjoining the recess. This method is therefore only applicable if both the inserts and the outer layers of a thermoplastic material or the inserts are provided in a complex process step with thermoplastic sacrificial edges.
- the invention is based on the technical problem that
- Ultrasonic energy are connected to a likewise made of metal component can.
- the connection must not be made surface by contacting the insert with the component at the intended broadsides, but rather can be made substantially voluminous in the recess itself by means of an intermediate layer of thermoplastic material. If a component made of a (metallic) cellular material is used, then there is the further advantage that the thermoplastic material can penetrate deep into the pores of the material and thereby form a positive connection with the latter. The same applies to the side of the insert when it is provided at its protruding into the recess outer surface with suitable for receiving the thermoplastic material wells.
- the joining method according to the invention requires neither a recess passing through the component nor any cover layers and can be carried out largely independently of the materials provided for the component and the insert.
- FIG. 1 shows a schematic section through a component to be provided with an insert in a first stage of the method according to the invention
- FIG. 2 to 4 of Figure 1 corresponding views of further stages of the method according to the invention.
- Fig. 5 is a view corresponding to Figure 2 in magnification.
- FIGS. 6 and 7 of FIG. 1 corresponding views when using alternative embodiments of the method according to the invention.
- FIGS. 1 to 4 is a component 1 with a z. B.
- cylindrical recess 2 is provided, which incorporated from a broad side 3 ago and in the manner of a Blind bore is formed.
- the recess 2 has a central axis 4, which extends in the embodiment substantially perpendicular to the broad side 3.
- a body 5 is arranged made of a thermoplastic material, which is formed in the embodiment as hülsenfö ⁇ niger or hollow cylindrical hollow body and has an axial height, which is expedient equal to the depth of the recess 2. In the inserted state according to FIG. 1, the body 5 therefore terminates flush with the broad side 3.
- An insert 6 is intended to be introduced into the recess 2 and firmly connected to the component 1.
- the insert 6 has at its upper end, in particular Fig. 4 shows, provided with an internal thread 7, axial bore 8.
- a fastening screw od after the attachment of the insert 6 on the component 1.
- the like. Are screwed, whereby the insert 6 forms a mounting element by means of which any other components can be firmly connected to the component 1.
- the bore 8 is used, as shown in FIGS. 1 to 3, when carrying out the joining method according to the invention also for receiving the free end of a sonotrode 9, which is provided with an external thread in the internal thread 7 and are firmly screwed into the bore 8 can.
- the attachment of the insert 6 in the recess 2 according to the invention z.
- Example characterized in that first introduced the body 5 made of thermoplastic material in the recess 2 and then the previously bolted to the sonotrode insert 9 9 in the direction of the arrow of the recess 2 is coaxially approximated to the central axis 4 (Fig. 1).
- the sonotrode 9 is activated or set into mechanical ultrasonic oscillations until the thermoplastic material of the body 5 has been largely or completely plasticized and thereby comes close to the body the recess 2 enclosing the circumference of the component 1 and the opposite outer lateral surface of the insert 6 conforms.
- the sonotrode 9 as needed, just before or after Contacting the insert 6 with the body 5 are activated.
- the sonotrode 9 is suitably attached to a converter, not shown, the z. B. formed as a piezoelectric vibration generator and in turn is coupled to a motor, hydraulic or pneumatic operated feed unit.
- a converter not shown
- the z. B. formed as a piezoelectric vibration generator and in turn is coupled to a motor, hydraulic or pneumatic operated feed unit.
- suitable devices are for. B. in devices for ultrasonic welding generally known.
- the body 5 For carrying out the described joining method, it is expedient for the body 5 to have an outer cross-section K 1 (FIG. 5) which is slightly smaller than that
- Inner cross-section A; the recess 2 is, and therefore can be easily inserted into the recess 2 with a small gap.
- the z. B. cylindrical insert 6 have an outer cross-section E a , which is slightly larger than the inner cross-section K ; of the body 5 is. This ensures that the cavity formed between the insert 6 and the peripheral wall of the recess 2 has a slightly smaller volume than the body 5 and the thermoplastic material is therefore displaced radially to the central axis 4 during insertion of the insert 6 and during melting.
- thermoplastic material can therefore occur in particular in open pores and other formed in the peripheral wall of the recess 2 cavities, as they are in particular when using metallic-cellular materials and other lightweight materials, and in this way parallel to the central axis 4 a positive connection with the Enter peripheral wall of the recess 2.
- the preferably consisting of a hard, solid metal insert 6 is provided in a particularly preferred embodiment of the invention on its outer, originally cylindrical lateral surface with at least one recess 11 (Fig. 5), the z. B. is formed by a circumferential, incorporated into the lateral surface notch, groove, groove or other recess and can stand next to them corresponding ribs 12 with the dimension E a .
- a plurality of such recesses 11 is provided.
- the thermoplastic material 10 as shown in FIGS. 3 and 4 can also penetrate into the depressions 11 during the melting process in order to form a positive connection with the outer jacket surface of the insert 6. After cooling, the thermoplastic material 10 then forms a hard plug, which connects the insert 6 not only materially, but also positively with the component 1 and therefore could be removed again in the direction of the central axis 4 only with a very high withdrawal force.
- the insert 6 is provided at its lower end with a chamfer 14 which, when introduced into the recess 2 or the body 5, serves as an insertion bevel and centering means and the radial displacement of the plasticized material of the body 5 can promote.
- a chamfer 14 which, when introduced into the recess 2 or the body 5, serves as an insertion bevel and centering means and the radial displacement of the plasticized material of the body 5 can promote.
- the insert 6 at an ⁇ axial end or in a region which is arranged above its portion to be located in the recess 2, to be provided with a circumferential flange 15 which has a larger outer cross-section than the measure e a in Fig. 5 corresponds to, and hang up at the fastening operation on the broad side 3 of the component 1.
- the flange 15 may cover the connection gap and, if appropriate, prevent the lateral outflow of plasticized material before the final curing.
- FIG. 6 shows an exemplary embodiment in which an insert 16 has at its upper end an axially projecting lug 17 provided with an external thread section and onto which a sonotrode 18 provided with a corresponding internal thread is screwed becomes. After Fügeyerfahren and after removing the sonotrode 18 of the insert 16 therefore forms a mounting element, at its approach 17 z. B. a nut or a provided with a corresponding internal thread further component can be attached. It is clear that the bore 8 and the internal thread 7 (FIG. 4) could also be formed on a projection of the insert 6 protruding beyond the component 1. Moreover, the arrangement and the procedure in the exemplary embodiment according to FIG. 6 correspond to those according to FIGS. 1 to 5.
- a difference from Fig. 1 to 5 is that a component 19 is used from a composite construction, in which z. B. a metallic-cellular material 20 is coated on both sides with a cover layer 21 of metal or other material. Otherwise this embodiment corresponds to that of FIGS. 1 to 5.
- the inserts 6, 16 may alternatively be provided instead of an inner or outer threaded portion and inner bores with parallel to the central axis 4 elongated grooves for receiving spring pins or in the manner of studs with cylindrical projections, the transverse bores for receiving dowels or the like.
- the particular shape of the insert 6, 16 depends on the needs of the case.
- the properties or features of the insert 6, 16 (for example, external cross-section E a in FIG. 5) which are important for the joining method , only the part to be introduced into the recess 2 or to be located in the recess 2 relate, while an additional, after completion of the joining process from the recess 2 outstanding portion of the insert 6 can be made substantially free.
- the insert 6 may also be so short that it disappears completely in the recess 2, in particular if it has no flange 15.
- a further embodiment of the invention provides that the recess 2 and / or at least the outer lateral surface of the section of the insert 6, 16 located in the recess 2 are non-circular (eg oval or angular), thereby increasing the height relative to a rotationally symmetrical shaping To achieve anti-rotation.
- the recess 2 completely enforce the component 1, in which case the component 1 would have to be deposited on the implementation of the joining method on a suitable base, which generates a force F counter to the counterpressure.
- the component 1 and the material 20 of the component 19 may be suitable especially for lightweight construction materials such.
- lightweight construction materials such as aluminum, steel and magnesium foams and other metals are produced with high porosity. But other materials are useful, provided that they are not adversely affected by the sonotrodes 9, 18 acting on them with ultrasonic vibrations.
- the body 5 preferably thermoplastic materials such. As polyamide (PA), polycarbonate (PC) or acrylonitrile butadiene styrene (ABS) used, which are easily plasticized by ultrasonic energy.
- PA polyamide
- PC polycarbonate
- ABS acrylonitrile butadiene styrene
- the inserts 6, 16 should eventually consist of a metal or a metal alloy, although other, sufficiently hard and non-thermoplastic meltable plastics would be suitable.
- the invention is not limited to the described embodiments, which can be modified in many ways. This applies in particular to the described dimensions and geometric shapes of the various parts. It should also be noted that the outer contour of the introduced into the recess 2 portion of the insert 6, 16 does not have to coincide with the inner contour of the recess 2 surrounding circumferential wall identical. It is only necessary that the body 5 has a sufficiently large volume to the space between the recess wall and the outer surface of the insert 6, 16 as completely as possible, ie volumetric fill. For this purpose, it would also be possible to form the body 5 substantially solid and instead form the insert 6, 16 at least on its underside as a hollow body, so that excess thermoplastic material can be accommodated in a cavity of the insert.
- the axial height of the body 5 could also be smaller than the depth of the recess 2.
- the body 5 z. B. formed as a hollow body and optionally with a slight interference fit on the insert 6, 16 is pushed until it z. B. from below against the flange 15th (Fig. 5) abuts.
- the measure K 1 (FIG. 5) to be slightly larger than the dimension A; to choose. Also combinations of these two variants are possible.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Connection Of Plates (AREA)
Abstract
Description
Verfahren zum Befestigen eines Einsatzes an einem Bauteil aus einem Leichtbau- WerkstoffMethod for attaching an insert to a component made of a lightweight material
Die Erfindung betrifft ein Verfahren der im Oberbegriff des Anspruchs 1 angegebenen Gattung.The invention relates to a method of the type specified in the preamble of claim 1.
Bauelemente aus Leichtbau- Werkstoffen, insbesondere Metallschäumen und anderen (metallisch-) zellularen Werkstoffen, werden zunehmend im Fahrzeugbau genutzt, um bei hinreichender Festigkeit und Steifϊgkeit die Bauteilmasse zu verringern. Sie finden aber auch in weiten Bereichen des Maschinenbaus Anwendung und zeichnen durch die Auflösung der kompakten und massiven Struktur in eine offen- oder geschlossenporige zellulare Struktur aus. Für den industriellen (Groß-) Einsatz derartiger Werkstoffe oder mit diesen hergestellter Werkstoffverbunde ist es erforderlich, sie mit vorzugsweise aus Metall gefertigten Montageelementen wie z. B. Schrauben, Bolzen, Stiften od. dgl. zu versehen. Dazu werden geeignete Fügeverfahren benötigt, da die Montageelemente nicht ohne weiteres dauerhaft fest an den Bauteilen befestigt werden können.Components made of lightweight materials, in particular metal foams and other (metallic) cellular materials, are increasingly used in vehicle construction in order to reduce the component mass with sufficient strength and rigidity. But they are also used in many areas of mechanical engineering application and characterized by the resolution of the compact and solid structure in an open or closed-cell structure. For the industrial (large) use of such materials or with these produced composite materials, it is necessary to use preferably made of metal mounting elements such. As screws, bolts, pins od. Like. To provide. For this purpose, suitable joining methods are needed, since the mounting elements can not be easily permanently attached to the components.
Als grundsätzlich geeignete Fügeverfahren haben sich das Kleben, Schrauben, Löten und spezielle Schweißverfahren erwiesen. Dies gilt allerdings nicht uneingeschränkt.Bonding, screwing, soldering and special welding processes have proved to be fundamentally suitable joining methods. However, this is not unlimited.
Beim direkten Schweißen von Metallschäumen treten Probleme auf, welche schaumseitig auf die sehr geringe und vor allem ungleichmäßige Dicke der zu verschweißenden Bereiche zurückzuführen sind. Die relativ hohe Schweißtemperatur impliziert Eigenspannungen in der Wärmeeinflußzone und führt meistens zu Verzug.In the case of direct welding of metal foams, problems arise which are foam-side due to the very small and especially uneven thickness of the areas to be welded. The relatively high welding temperature implies residual stresses in the heat affected zone and usually leads to distortion.
Beim Löten von Schaumwerkstoffen können aufgrund des Eindringens von Lötflußmitteln in die poröse Schaumstruktur Korrosionsprobleme sowie Beeinflußungen der Eigenschaften des zellularen Werkstoffs im Kontaminationsbereich auftreten. Weiterhin ist die Festigkeit gelöteter Verbindungen oft erheblich geringer als die technische Streckgrenze des Schaumwerkstoffs bei gleicher Dichte.When soldering foamed materials, corrosion problems as well as influences on the properties of the cellular material in the contamination area can occur due to the penetration of soldering flux into the porous foam structure. Furthermore, the strength of soldered joints is often significantly lower than the technical yield strength of the foam material at the same density.
Das ausschließlich kraftschlüssige Fügeverfahren "Schrauben" ist aufgrund unzureichender Festigkeit der Schaumstruktur kaum einsetzbar.The exclusively non-positive joining process "screws" is hardly usable due to insufficient strength of the foam structure.
Ideal wäre ein flächen- bzw. volumenhaftes und stoffschlüssiges Fügeverfahren. Dieser Forderung entspricht das Kleben als Fügetechnik. Nahezu alle Werkstoffgruppen lassen sich miteinander verbinden, ohne daß die Werkstoffeigenschaften der Fügeteile unzulässig verändert werden. Das Kleben zählt zu den wärmearmen Fügeverfahren, bei dem keine lokale Schwächung der Fügezone sondern eine flächenhafte stoffschlüssige Verbindung der Fügeteile erfolgt. Deren Festigkeit 'ist in der Regel höher als die des zellularen Werk- Stoffs. Weiterhin kann das Fügeverfahren "Kleben" insbesondere bei Mischbauweise, d. h. bei Verwendung unterschiedlicher metallischer und/oder nichtmetallischer Werkstoffe multifunktionale Eigenschaften aufweisen und zusätzlich Aufgaben wie elektrochemische Isolation und Dichtfunktion übernehmen. Nachteilig bezüglich der Verfahrensgeschwindigkeit sind die bei Raumtemperatur oft mehrere Stunden dauernden Aushärtungszeiten geeigneter, insbesondere duroplastischer Reaktionsklebstoffe. Eine Verkürzung derIdeal would be a surface or voluminous and cohesive joining process. This requirement corresponds to bonding as a joining technique. Almost all material groups can be combined with one another without the material properties of the components being changed inadmissibly. Gluing is one of the low-heat joining methods, in which no local weakening of the joining zone but a planar cohesive connection of the joining parts takes place. Their strength is usually higher than that of the cellular material. Furthermore, the joining method "gluing" in particular in mixed construction, d. H. have multifunctional properties when using different metallic and / or non-metallic materials and additionally perform tasks such as electrochemical insulation and sealing function. Disadvantages with regard to the process speed are the curing times, which are often several hours at room temperature, of suitable, in particular thermoset reaction adhesives. A shortening of the
Aushärtungszeiten wäre zwar durch eine Erhöhung der Aushärtungstemperatur möglich, erfordert aber weiteren apparativen Aufwand und finanziellen Einsatz.Curing times would indeed be possible by increasing the curing temperature, but requires further expenditure on equipment and financial commitment.
Im Falle des Einbringens von Montageelementen in Form von Einsätzen, mit denen Schrauben, Stifte, Muttern od. dgl. fest verbunden werden könnten, erlauben metallisch zellulare Werkstoffe (z. B. Metallschäume) das Ein- oder Umschäumen dieser Einsätze direkt beim Herstellungsprozeß. Hierfür kommen jedoch nur Kompaktwerkstoffe in Frage, welche einen höheren Schmelzpunkt als die herrschenden Prozeßtemperaturen beim Schäumen aufweisen. Die Verwendung solcher Einsätze aus Kompaktwerkstoff erfordert wegen der erheblichen thermischen Belastung ein größeres Volumen und widerspricht damit dem Leichtbaugedanken, der hinter dem Einsatz von zellularen Werkstoffen steht. Andererseits ist durch das Umschäumen die Position des Befestigungselements eindeutig festgelegt, und etwaige Toleranzüberlagerungen können unter Umständen nicht mehr ausgeglichen werden.In the case of the introduction of mounting elements in the form of inserts, with which screws, pins, nuts od. Like. Be firmly connected, allow metallic cellular materials (eg., Metal foams) the on or foaming of these inserts directly at the manufacturing process. For this purpose, however, only compact materials come into question, which have a higher melting point than the prevailing process temperatures during foaming. The use of such inserts made of compact material requires because of the considerable thermal load a larger volume and thus contradicts the lightweight design, which is behind the use of cellular materials. On the other hand, the position of the fastener is clearly defined by the foaming, and any tolerance overlays may not be compensated under certain circumstances.
Daneben ist es zur Herstellung einer festen Verbindung zwischen einem Bauteil aus einem zellularen Material und einem Bauteil aus einem kompakten Material bekannt (DE 199 17 132 AI), die beiden Bauteile aneinander zu legen und dann durch Ultraschallschweißen miteinander zu verbinden. Zur Herstellung fester und dauerhafter Verbindungen sind allerdings verhältnismäßig große Kontaktflächen erforderlich, die nicht immer erwünscht sind und auch nicht immer zur Verfugung stehen.In addition, it is known for producing a fixed connection between a component made of a cellular material and a component made of a compact material (DE 199 17 132 A1), to place the two components together and then to connect them together by ultrasonic welding. For the production of solid and permanent compounds, however, relatively large contact surfaces are required, which are not always desirable and are not always available.
Zur Verbindung von plattenförmigen Bauteilen wäre es weiterhin möglich, die eine Platte mit einer Aussparung zu versehen, in diese einen hülsenförmigen Einsatz einzusetzen und dessen Boden dann durch Ultraschallschweißen mit der anderen Platte zu verbinden (DE 196 10 636 C2). Eine solche Befestigungsart setzt allerdings voraus, daß zumindest der Einsatz aus einem durch Ultraschallenergie schweißfähigen Material besteht, was aus Stabilitätsgründen nicht immer erwünscht ist. Außerdem steht bei einer solchen Verfahrensweise mit dem Boden des Einsatzes nur eine vergleichsweise kleine Kontaktfläche für die herzustellende, kraftschlüssige Verbindung zur Verfügung.For the connection of plate-shaped components, it would also be possible to provide a plate with a recess, to use in this a sleeve-shaped insert and then connect the bottom by ultrasonic welding to the other plate (DE 196 10 636 C2). However, such a type of fastening presupposes that at least the insert consists of a material that can be welded by ultrasonic energy, which is not always desirable for stability reasons. In addition, in such a procedure with the bottom of the insert only a relatively small contact surface for the produced, non-positive connection available.
Bei einem weiteren bekannten Verfahren (US-PS 4 817 264) werden mit Flanschen versehene, nietartige Einsätze verwendet, die in durchgehende Bohrungen der Bauteile eingesetzt und auf der von den Flanschen entfernten, aus den Bohrungen herausragenden Enden durch Ultraschallenergie plastifiziert und zu Nietköpfen verformt werden, wie dies beim Ultraschallschweißen allgemein üblich ist. Die Fügung erfolgt hier ausschließlich durch Formschluß und setzt eine das Bauteil vollständig durchsetzende Aussparung voraus. Ist stattdessen eine Aussparung in Form einer Blindbohrung erwünscht, dann muß erst einmal ein Aufnahmekörper aus thermoplastischem Material in der Aussparung befestigt werden, was in einem besonderen Arbeitsgang durch Bildung einer Kleb- und Schnappverbindung verfolgt. Danach wird der eigentliche Einsatz durch Ultraschallenergie im Aufhahmekörper befestigt, so daß sich ein vergleichsweise aufwändiges und nur mit geeigneten, am Bauteil befestigten Deckschichten durchfuhrbares Fügeverfahren ergibt.In another known method (US Pat. No. 4,817,264), flanged, rivet-type inserts are used, which are inserted into through holes of the components and plasticized on the flanges remote from the holes projecting ends by ultrasonic energy and deformed into rivet heads , as is common practice in ultrasonic welding. The joining is done here exclusively by positive engagement and requires a component completely penetrating recess. If instead a recess in the form of a blind bore is desired, then first a receiving body of thermoplastic material must be secured in the recess, which is followed in a particular operation by forming a glued and snap connection. Thereafter, the actual use is fixed by ultrasonic energy in the Aufhahmekörper, so that there is a comparatively complex and durchfuhrbares only with suitable, attached to the component surface layers joining process.
Schließlich ist ein Verfahren der eingangs bezeichneten Gattung bekannt (DE 695 03 284 T2), bei dem ein plattenförmiges, aus Schaumstoff oder Wabenmaterial bestehendes Bauteil auf gegenüber liegenden Breitseiten mit Deckschichten oder thermoplastischem Material belegt und mit einer zur Aufnahme eines Einsatzes bestimmten Aussparung versehen wird. Der Einsatz besteht aus thermoplastischem Material und weist an seinen axialen Enden sogenannte Opferränder auf, die durch Ultraschallschwingungen plastifiziert und mit den an die Aussparung grenzenden Rändern der beiden Deckschichten ver- schmolzen werden. Dieses Verfahren ist daher nur anwendbar, wenn sowohl die Einsätze als auch die Deckschichten aus einem thermoplastischen Material bestehen oder die Einsätze in einem aufwendigen Verfahrensschritt mit thermoplastischen Opferrändern versehen werden.Finally, a method of the type described above is known (DE 695 03 284 T2), in which a plate-shaped, made of foam or honeycomb material component is covered on opposing broad sides with cover layers or thermoplastic material and provided with a specific for receiving an insert recess. The insert is made of thermoplastic material and has at its axial ends so-called sacrificial edges which are plasticized by ultrasonic vibrations and melted with the edges of the two cover layers adjoining the recess. This method is therefore only applicable if both the inserts and the outer layers of a thermoplastic material or the inserts are provided in a complex process step with thermoplastic sacrificial edges.
Vor diesem Hintergrund liegt der Erfindung das technische Problem zugrunde, dasAgainst this background, the invention is based on the technical problem that
Verfahren der eingangs bezeichneten Gattung so weiterzuentwickeln, daß es sich auch zur Verbindung von metallischen Einsätzen an Bauteilen aus metallisch-zellularen Werkstoffen oder daraus hergestellten Verbundwerkstoffen eignet, auf einfache Weise eine dauerhaft gute Befestigung der Einsätze in den Bauteilen ermöglicht und vom Prinzip her weder Deckschichten noch durchgehende Aussparungen für die Einsätze erfordert.Process of the type described at the outset so that it is also suitable for the connection of metallic inserts to components made of metallic-cellular materials or composites thereof, in a simple way allows a permanent good attachment of the inserts in the components and in principle neither cover layers still continuous recesses required for the inserts.
Zur Lösung dieses Problems dienen die kennzeichnenden Merkmale des Anspruchs 1.To solve this problem serve the characterizing features of claim 1.
Die Erfindung bringt den Vorteil mit sich, daß durch das zusätzliche Einbringen eines Körpers aus thermoplastischem Material ein aus Metall bestehender Einsatz durchThe invention has the advantage that by the additional introduction of a body made of thermoplastic material is an existing metal insert
Ultraschallenergie mit einem ebenfalls aus Metall bestehenden Bauteil verbunden werden kann. Die Verbindung muß dabei nicht flächig durch Kontaktierung des Einsatzes mit dem Bauteil an dafür vorgesehenen Breitseiten erfolgen, sondern kann vielmehr im wesentlichen volumenhaft in der Aussparung selbst mit Hilfe einer Zwischenschicht aus thermoplastischem Material vorgenommen werden. Wird ein Bauteil aus einem (metallisch-) zellularen Werkstoff verwendet, dann ergibt sich der weitere Vorteil, daß das thermoplastische Material tief in die Poren des Werkstoffs eindringen und dadurch eine formschlüssige Verbindung mit diesem eingehen kann. Dasselbe gilt auf der Seite des Einsatzes, wenn dieser an seiner in die Aussparung ragende Außenfläche mit zur Aufnahme des thermoplastischen Materials geeigneten Vertiefungen versehen wird. Das erfindungs- gemäße Fügeverfahren erfordert außerdem weder eine das Bauteil durchsetzende Aussparung noch irgendwelche Deckschichten und ist weitgehend unabhängig von den für das Bauteil und den Einsatz vorgesehenen Materialien durchführbar.Ultrasonic energy are connected to a likewise made of metal component can. The connection must not be made surface by contacting the insert with the component at the intended broadsides, but rather can be made substantially voluminous in the recess itself by means of an intermediate layer of thermoplastic material. If a component made of a (metallic) cellular material is used, then there is the further advantage that the thermoplastic material can penetrate deep into the pores of the material and thereby form a positive connection with the latter. The same applies to the side of the insert when it is provided at its protruding into the recess outer surface with suitable for receiving the thermoplastic material wells. Moreover, the joining method according to the invention requires neither a recess passing through the component nor any cover layers and can be carried out largely independently of the materials provided for the component and the insert.
Weitere vorteilhafte Merkmale der Erfindung ergeoen sich aus den Unteransprüchen,Further advantageous features of the invention emerge from the subclaims,
Die Erfindung wird nachfolgend in Verbindung mit den beiliegenden Zeichnungen an Ausführungsbeispielen näher erläutert. Es zeigen:The invention will be explained in more detail below in connection with the accompanying drawings of exemplary embodiments. Show it:
Fig. 1 einen schematischen Schnitt durch ein mit einem Einsatz zu versehendes Bauteil in einer ersten Stufe des erfindungsgemäßen Verfahrens;1 shows a schematic section through a component to be provided with an insert in a first stage of the method according to the invention;
Fig. 2 bis 4 der Fig. 1 entsprechende Ansichten von weiteren Stufen des erfindungsgemäßen Verfahrens;Fig. 2 to 4 of Figure 1 corresponding views of further stages of the method according to the invention.
Fig. 5 eine der Fig. 2 entsprechende Ansicht in Vergrößerung; undFig. 5 is a view corresponding to Figure 2 in magnification. and
Fig. 6 und 7 der Fig. 1 entsprechende Ansichten bei Anwendung von alternativen Ausführungsbeispielen des erfindungsgemäßen Verfahrens.FIGS. 6 and 7 of FIG. 1 corresponding views when using alternative embodiments of the method according to the invention.
Beim Ausführungsbeispiel nach Fig. 1 bis 4 ist ein Bauteil 1 mit einer z. B. zylindrischen Aussparung 2 vorgesehen, die von einer Breitseite 3 her eingearbeitet und nach Art einer Blindbohrung ausgebildet ist. Die Aussparung 2 weist eine Mittelachse 4 auf, die im Ausführungsbeispiel im wesentlichen senkrecht zur Breitseite 3 verläuft. In der Aussparung 2 ist ein Körper 5 aus einem thermoplastischen Material angeordnet, der im Ausführungsbeispiel als hülsenföπniger bzw. hohlzylindrischer Hohlkörper ausgebildet ist und eine axiale Höhe besitzt, die zweckmäßig gleich der Tiefe der Aussparung 2 ist. Im eingesetzten Zustand nach Fig. 1 schließt der Körper 5 daher bündig mit der Breitseite 3 ab.In the embodiment of FIGS. 1 to 4 is a component 1 with a z. B. cylindrical recess 2 is provided, which incorporated from a broad side 3 ago and in the manner of a Blind bore is formed. The recess 2 has a central axis 4, which extends in the embodiment substantially perpendicular to the broad side 3. In the recess 2, a body 5 is arranged made of a thermoplastic material, which is formed in the embodiment as hülsenföπniger or hollow cylindrical hollow body and has an axial height, which is expedient equal to the depth of the recess 2. In the inserted state according to FIG. 1, the body 5 therefore terminates flush with the broad side 3.
Ein Einsatz 6 ist dazu vorgesehen, in die Aussprung 2 eingebracht und fest mit dem Bauteil 1 verbunden zu werden. Der Einsatz 6 weist an seinem oberen Ende, wie insbesondere Fig. 4 zeigt, eine mit einem Innengewinde 7 versehene, axiale Bohrung 8 auf. In diese Bohrung 8 kann nach der Befestigung des Einsatzes 6 am Bauteil 1 eine Befestigungsschraube od. dgl. eingedreht werden, wodurch der Einsatz 6 ein Montageelement bildet, mittels dessen an sich beliebige weitere Bauteile fest mit dem Bauteil 1 verbunden werden können.An insert 6 is intended to be introduced into the recess 2 and firmly connected to the component 1. The insert 6 has at its upper end, in particular Fig. 4 shows, provided with an internal thread 7, axial bore 8. In this bore 8, a fastening screw od after the attachment of the insert 6 on the component 1. The like. Are screwed, whereby the insert 6 forms a mounting element by means of which any other components can be firmly connected to the component 1.
Die Bohrung 8 dient, wie Fig. 1 bis 3 zeigen, bei der Durchführung des erfindungs- gemäßen Fügeverfahrens außerdem zur Aufnahme des freien Endes einer Sonotrode 9, das mit einem in das Innengewinde 7 passenden Außengewinde versehen ist und fest in die Bohrung 8 eingedreht werden kann.The bore 8 is used, as shown in FIGS. 1 to 3, when carrying out the joining method according to the invention also for receiving the free end of a sonotrode 9, which is provided with an external thread in the internal thread 7 and are firmly screwed into the bore 8 can.
Die Befestigung des Einsatzes 6 in der Aussparung 2 erfolgt erfindungsgemäß z. B. dadurch, daß zunächst der Körper 5 aus thermoplastischem Material in die Aussparung 2 eingebracht und dann der vorher an die Sonotrode 9 angeschraubte Einsatz 9 in Richtung des eingezeichneten Pfeils der Aussparung 2 koaxial zur Mittelachse 4 angenähert wird (Fig. 1). Sobald das untere Ende des Einsatzes 6 den Körper 5 erreicht hat (Fig. 2), wird die Sonotrode 9 so lange aktiviert bzw. in mechanische Ultraschallschwingungen versetzt, bis das thermoplastische Material des Körpers 5 weitgehend oder vollständig plastifiziert ist und sich dadurch dicht an die die Aussparung 2 umschließende Umfangs and des Bauteils 1 sowie die ihr gegenüber liegende äußere Mantelfläche des Einsatzes 6 anschmiegt. Natürlich kann die Sonotrode 9 je nach Bedarf auch kurz vor oder nach dem Inberührungbringen des Einsatzes 6 mit dem Körper 5 aktiviert werden.The attachment of the insert 6 in the recess 2 according to the invention z. Example, characterized in that first introduced the body 5 made of thermoplastic material in the recess 2 and then the previously bolted to the sonotrode insert 9 9 in the direction of the arrow of the recess 2 is coaxially approximated to the central axis 4 (Fig. 1). As soon as the lower end of the insert 6 has reached the body 5 (FIG. 2), the sonotrode 9 is activated or set into mechanical ultrasonic oscillations until the thermoplastic material of the body 5 has been largely or completely plasticized and thereby comes close to the body the recess 2 enclosing the circumference of the component 1 and the opposite outer lateral surface of the insert 6 conforms. Of course, the sonotrode 9 as needed, just before or after Contacting the insert 6 with the body 5 are activated.
Der Einsatz 6 wird nach seinem Aufsetzen auf den Körper 5 kontinuierlich oder schrittweise mit einer Kraft F in Pfeilrichtung weiter vorgeschoben, bis er vorzugsweise auf dem Boden der Aussparung 2 aufliegt (Fig. 3) und das plastifizierte thermoplastische Material 10 des Körpers 5 (Fig. 3 und 4) vollständig in den Zwischenraum zwischen der Umfangs- wand der Aussparung 2 und der Mantelfläche des Einsatzes 6 eingetreten und gleichförmig in diesem verteilt ist. Anschließend wird die Sonotrode 9 aus der Bohrung 8 herausgedreht und entfernt (Fig. 4). Das erkaltete thermoplastische Material 10 stellt dann eine innige und feste Verbindung des Einsatzes 6 mit dem Bauteil 1 her. Das gesamte Fügeverfahren einschließlich des Erkaltens des thermoplastischen Materials dauert nur wenige Sekunden.The insert 6, after being placed on the body 5, is advanced continuously or stepwise with a force F in the direction of the arrow until it preferably rests on the bottom of the recess 2 (FIG. 3) and the plasticized thermoplastic material 10 of the body 5 (FIG. 3 and 4) completely into the space between the peripheral wall of the recess 2 and the lateral surface of the insert 6 occurred and is uniformly distributed in this. Subsequently, the sonotrode 9 is rotated out of the bore 8 and removed (FIG. 4). The cooled thermoplastic material 10 then establishes an intimate and firm connection of the insert 6 with the component 1. The entire joining process, including the cooling of the thermoplastic material takes only a few seconds.
Zur Einführung des Einsatzes 6 in die Aussparung 2 ist die Sonotrode 9 zweckmäßig an einem nicht dargestellten Konverter befestigt, der z. B. als piezoelektrischer Schwingungs- erzeuger ausgebildet und seinerseits mit einer motorisch, hydraulisch oder pneumatisch betriebenen Vorschubeinheit gekoppelt ist. Hierfür geeignete Vorrichtungen sind z. B. bei Geräten zur Ultraschallschweißung allgemein bekannt.To introduce the insert 6 in the recess 2, the sonotrode 9 is suitably attached to a converter, not shown, the z. B. formed as a piezoelectric vibration generator and in turn is coupled to a motor, hydraulic or pneumatic operated feed unit. For this purpose, suitable devices are for. B. in devices for ultrasonic welding generally known.
Für die Durchführung des beschriebenen Fügeverfahrens ist es zweckmäßig, wenn der Körper 5 einen Außenquerschnitt K^ (Fig. 5) besitzt, der geringfügig kleiner als derFor carrying out the described joining method, it is expedient for the body 5 to have an outer cross-section K 1 (FIG. 5) which is slightly smaller than that
Innenquerschnitt A; der Aussparung 2 ist, und daher mit einem geringen Spaltmaß leicht in die Aussparung 2 eingeführt werden kann. Dagegen sollte der z. B. zylindrische Einsatz 6 einen Außenquerschnitt Ea aufweisen, der etwas größer als der Innenquerschnitt K; des Körpers 5 ist. Dadurch wird erreicht, daß der zwischen dem Einsatz 6 und der Umfangs- wand der Aussparung 2 gebildete Hohlraum ein etwas kleineres Volumen als der Körper 5 aufweist und das thermoplastische Material daher beim Einführen des Einsatzes 6 und beim Schmelzen radial zur Mittelachse 4 verdrängt wird. Überschüssiges thermoplastisches Material kann daher insbesondere in offene Poren und sonstige in der Umfangswand der Aussparung 2 ausgebildete Kavitäten eintreten, wie sie insbesondere bei Anwendung von metallisch-zellularen Werkstoffen und anderen Leichtbau- Werkstoffen vorhanden sind, und auf diese Weise parallel zur Mittelachse 4 eine formschlüssige Verbindung mit der Umfangswand der Aussparung 2 eingehen.Inner cross-section A; the recess 2 is, and therefore can be easily inserted into the recess 2 with a small gap. In contrast, the z. B. cylindrical insert 6 have an outer cross-section E a , which is slightly larger than the inner cross-section K ; of the body 5 is. This ensures that the cavity formed between the insert 6 and the peripheral wall of the recess 2 has a slightly smaller volume than the body 5 and the thermoplastic material is therefore displaced radially to the central axis 4 during insertion of the insert 6 and during melting. Excess thermoplastic material can therefore occur in particular in open pores and other formed in the peripheral wall of the recess 2 cavities, as they are in particular when using metallic-cellular materials and other lightweight materials, and in this way parallel to the central axis 4 a positive connection with the Enter peripheral wall of the recess 2.
Der vorzugsweise aus einem harten, festen Metall bestehende Einsatz 6 ist bei einem besonders bevorzugten Ausfuhrungsbeispiel der Erfindung an seiner äußeren, ursprünglich zylindrischen Mantelfläche mit wenigstens einer Vertiefung 11 (Fig. 5) versehen, die z. B. durch eine umlaufende, in die Mantelfläche eingearbeitete Kerbe, Rille, Nut oder sonstige Ausnehmung gebildet ist und neben sich entsprechende Rippen 12 mit dem Maß Ea stehen läßt. Vorzugsweise ist eine Mehrzahl derartiger Vertiefungen 11 vorgesehen. Dadurch kann das thermoplastische Material 10, wie Fig. 3 und 4 zeigen, beim Schmelzvorgang auch in die Vertiefungen 11 eindringen, um eine formschlüssige Verbindung mit der äußeren Mantelfläche des Einsatzes 6 einzugehen. Nach dem Erkalten bildet das thermoplastische Material 10 dann einen harten Pfropfen, der den Einsatz 6 nicht nur stoffschlüssig, sondern auch formschlüssig mit dem Bauteil 1 verbindet und daher in Richtung der Mittelachse 4 nur mit einer sehr hohen Abzugskraft wieder entfernt werden könnte.The preferably consisting of a hard, solid metal insert 6 is provided in a particularly preferred embodiment of the invention on its outer, originally cylindrical lateral surface with at least one recess 11 (Fig. 5), the z. B. is formed by a circumferential, incorporated into the lateral surface notch, groove, groove or other recess and can stand next to them corresponding ribs 12 with the dimension E a . Preferably, a plurality of such recesses 11 is provided. As a result, the thermoplastic material 10, as shown in FIGS. 3 and 4, can also penetrate into the depressions 11 during the melting process in order to form a positive connection with the outer jacket surface of the insert 6. After cooling, the thermoplastic material 10 then forms a hard plug, which connects the insert 6 not only materially, but also positively with the component 1 and therefore could be removed again in the direction of the central axis 4 only with a very high withdrawal force.
Wie Fig. 5 weiter zeigt, ist der Einsatz 6 an seinem unteren Ende mit einer Fase 14 versehen, die bei seiner Einführung in die Aussparung 2 bzw. den Körper 5 als Ein- führungsschräge und Zentriermittel dienen und die radiale Verdrängung des plastifizierten Materials des Körpers 5 fördern kann. Außerdem ist es möglich, den Einsatz 6 an einem υ axialen Ende bzw. in einem Bereich, der oberhalb seines in der Aussparung 2 zu liegen kommenden Teilstücks angeordnet ist, mit einem umlaufenden Flansch 15 zu versehen, der einen größeren Außenquerschnitt besitzt, als dem Maß Ea in Fig. 5 entspricht, und sich beim Befestigungsvorgang auf die Breitseite 3 des Bauteils 1 auflegt. Dadurch kann die Dauerfestigkeit der Verbindung gegenüber Kippbewegungen quer zur Mittelachse 4 beim späteren Gebrauch verbessert werden. Außerdem kann der Flanseh 15 den Verbindungsspalt abdecken und gegebenenfalls das seitliche Ausfließen von plastifiziertem Material vor der endgültigen Aushärtung verhindern.As further shown in FIG. 5, the insert 6 is provided at its lower end with a chamfer 14 which, when introduced into the recess 2 or the body 5, serves as an insertion bevel and centering means and the radial displacement of the plasticized material of the body 5 can promote. In addition, it is possible to provide the insert 6 at an υ axial end or in a region which is arranged above its portion to be located in the recess 2, to be provided with a circumferential flange 15 which has a larger outer cross-section than the measure e a in Fig. 5 corresponds to, and hang up at the fastening operation on the broad side 3 of the component 1. As a result, the fatigue strength of the connection with respect to tilting movements transversely to the central axis 4 during later use can be improved. In addition, the flange 15 may cover the connection gap and, if appropriate, prevent the lateral outflow of plasticized material before the final curing.
Fig. 6 zeigt ein Ausfuhrungsbeispiel, bei dem ein Einsatz 16 an seinem oberen Ende einen mit einem Außengewindeabschnitt versehenen, axial vorstehenden Ansatz 17 aufweist, auf den eine mit einem entsprechenden Innengewinde versehene Sonotrode 18 aufgeschraubt wird. Nach dem Fügeyerfahren und nach dem Entfernen der Sonotrode 18 bildet der Einsatz 16 daher ein Montageelement, an dessen Ansatz 17 z. B. eine Mutter oder ein mit einem entsprechenden Innengewinde versehenes weiteres Bauteil befestigt werden kann. Dabei ist klar, daß auch die Bohrung 8 und das Innengewinde 7 (Fig. 4) an einem über das Bauteil 1 vorstehenden Ansatz des Einsatzes 6 ausgebildet sein könnten. Im übrigen entsprechen die Anordnung und die Verfahrensweise beim Ausfuhrungsbeispiel nach Fig. 6 denen nach Fig. 1 bis 5.6 shows an exemplary embodiment in which an insert 16 has at its upper end an axially projecting lug 17 provided with an external thread section and onto which a sonotrode 18 provided with a corresponding internal thread is screwed becomes. After Fügeyerfahren and after removing the sonotrode 18 of the insert 16 therefore forms a mounting element, at its approach 17 z. B. a nut or a provided with a corresponding internal thread further component can be attached. It is clear that the bore 8 and the internal thread 7 (FIG. 4) could also be formed on a projection of the insert 6 protruding beyond the component 1. Moreover, the arrangement and the procedure in the exemplary embodiment according to FIG. 6 correspond to those according to FIGS. 1 to 5.
Beim Ausführungsbeispiel nach Fig. 7 besteht ein Unterschied zu Fig. 1 bis 5 darin, daß ein Bauteil 19 aus einer Verbundkonstruktion verwendet wird, bei dem z. B. ein metallisch-zellularer Werkstoff 20 beidseitig mit je einer Deckschicht 21 aus Metall oder einem anderen Material belegt ist. Im übrigen entspricht dieses Ausführungsbeispiel dem nach Fig. 1 bis 5.In the embodiment of FIG. 7, a difference from Fig. 1 to 5 is that a component 19 is used from a composite construction, in which z. B. a metallic-cellular material 20 is coated on both sides with a cover layer 21 of metal or other material. Otherwise this embodiment corresponds to that of FIGS. 1 to 5.
Die Einsätze 6, 16 können alternativ anstelle eines Innen- oder Außengewindeabschnitts auch Innenbohrungen mit parallel zur Mittelachse 4 verlängerten Nuten zur Aufnahme von Federstiften oder nach Art von Stehbolzen mit zylindrischen Ansätzen versehen sein, die Querbohrungen zur Aufnahme von Paßstiften oder dgl. aufweisen. Die jeweilige Form des Einsatzes 6, 16 richtet sich nach den Bedürfhissen des Einzelfalls. Außerdem ist klar, daß die für das Fügeverfahren wichtigen, oben erläuterten Eigenschaften bzw. Merkmale des Einsatzes 6, 16 (z. B. Außenquerschnitt Ea in Fig. 5) nur das in die Aussparung 2 einzubringende bzw. in dieser zu liegen kommende Teilstück betreffen, während ein zusätzlicher, nach Beendigung des Fügeverfahrens aus der Aussparung 2 herausragender Abschnitt des Einsatzes 6 im wesentlichen frei gestaltet werden kann. Wie Fig. 4 zeigt, kann der Einsatz 6 allerdings auch so kurz sein, daß er völlig in der Aussparung 2 verschwindet, insbesondere wenn er keinen Flansch 15 aufweist.The inserts 6, 16 may alternatively be provided instead of an inner or outer threaded portion and inner bores with parallel to the central axis 4 elongated grooves for receiving spring pins or in the manner of studs with cylindrical projections, the transverse bores for receiving dowels or the like. The particular shape of the insert 6, 16 depends on the needs of the case. In addition, it is clear that the properties or features of the insert 6, 16 (for example, external cross-section E a in FIG. 5) which are important for the joining method , only the part to be introduced into the recess 2 or to be located in the recess 2 relate, while an additional, after completion of the joining process from the recess 2 outstanding portion of the insert 6 can be made substantially free. However, as shown in FIG. 4, the insert 6 may also be so short that it disappears completely in the recess 2, in particular if it has no flange 15.
Eine weitere Ausgestaltung der Erfindung sieht vor, die Aussparung 2 und/oder zumindest die äußere Mantelfläche des in der Aussparung 2 befindlichen Teilstücks des Einsatzes 6, 16 unrund (z. B. oval oder eckig) auszubilden, um dadurch gegenüber einer rotationssymmetrischen Formgebung eine erhöhte Verdrehsicherung zu erreichen. Außerdem könnte die Aussparung 2 das Bauteil 1 völlig durchsetzen, in welchem Fall das Bauteil 1 bei der Durchführung des Fügeverfahrens auf einer geeigneten Unterlage abgelegt werden müßte, die einen der Kraft F entgegengerichteten Gegendruck erzeugt.A further embodiment of the invention provides that the recess 2 and / or at least the outer lateral surface of the section of the insert 6, 16 located in the recess 2 are non-circular (eg oval or angular), thereby increasing the height relative to a rotationally symmetrical shaping To achieve anti-rotation. In addition, could the recess 2 completely enforce the component 1, in which case the component 1 would have to be deposited on the implementation of the joining method on a suitable base, which generates a force F counter to the counterpressure.
Das Bauteil 1 und der Werkstoff 20 des Bauteils 19 können vor allem aus für Leichtbauten geeigneten Werkstoffen wie z. B. Aluminium-, Stahl- und Magnesiumschäumen und anderen Metallen mit großer Porigkeit hergestellt werden. Aber auch andere Materialien sind brauchbar, sofern diese durch die mit Ultraschallschwingungen auf sie einwirkenden Sonotroden 9, 18 nicht ungünstig beeinflußt werden. Dagegen werden für den Körper 5 vorzugsweise thermoplastische Kunststoffe wie z. B. Polyamid (PA), Polycarbonat (PC) oder Acrylnitrilbutadienstyrol (ABS) verwendet, die durch Ultraschallenergie leicht plastifizierbar sind. Die Einsätze 6, 16 sollten schließlich aus einem Metall oder einer Metalllegierung bestehen, obwohl auch andere, ausreichend harte und nicht thermoplastisch schmelzbare Kunststoffe geeignet wären.The component 1 and the material 20 of the component 19 may be suitable especially for lightweight construction materials such. As aluminum, steel and magnesium foams and other metals are produced with high porosity. But other materials are useful, provided that they are not adversely affected by the sonotrodes 9, 18 acting on them with ultrasonic vibrations. In contrast, for the body 5 preferably thermoplastic materials such. As polyamide (PA), polycarbonate (PC) or acrylonitrile butadiene styrene (ABS) used, which are easily plasticized by ultrasonic energy. The inserts 6, 16 should eventually consist of a metal or a metal alloy, although other, sufficiently hard and non-thermoplastic meltable plastics would be suitable.
Die Erfindung ist nicht auf die beschriebenen Ausführungsbeispiele beschränkt, die auf vielfache Weise abgewandelt werden können. Dies gilt insbesondere für die beschriebenen Abmessungen und geometrischen Formen der verschiedenen Teile. Außerdem ist zu beachten, daß die Außenkontur des in die Aussparung 2 eingeführten Teilstücks des Einsatzes 6, 16 nicht mit der Innenkontur der die Aussparung 2 umgebenden Umfangs- wand identisch übereinstimmen muß. Es ist nur erforderlich, daß der Körper 5 ein ausreichend großes Volumen besitzt, um den Zwischenraum zwischen der Aussparungswand und der äußeren Mantelfläche des Einsatzes 6, 16 möglichst vollständig, d. h. volumenhaft auszufüllen. Dazu wäre es auch möglich, den Körper 5 im wesentlichen massiv auszubilden und stattdessen den Einsatz 6, 16 zumindest an seiner Unterseite als Hohlkörper auszubilden, damit überschüssiges thermoplastisches Material in einem Hohlraum des Einsatzes aufgenommen werden kann. Außerdem könnte die axiale Höhe des Körpers 5 auch kleiner als die Tiefe der Aussparung 2 sein. Weiter wäre es möglich, den Körper 5 und den Einsatz 6, 16 gleichzeitig in die Aussparung 2 einzufuhren, indem der Körper 5 z. B. als Hohlkörper ausgebildet und gegebenenfalls mit leichtem Preßsitz auf den Einsatz 6, 16 aufgeschoben wird, bis er z. B. von unten her gegen den Flansch 15 (Fig. 5) anstößt. In diesem Fall wäre es sogar möglich, das Maß K^ (Fig. 5) geringfügig größer als das Maß A; zu wählen. Auch Kombinationen dieser beiden Varianten sind möglich. Möglich wäre es natürlich auch, die axiale Länge des in der Aussparung zu liegen kommenden Teilstücks des Einsatzes 6 kürzer als die in axialer Richtung gemessene Tiefe der Aussparung 2 zu bemessen. Weiter könnte die Sonotrode 9, 18 mit anderen, als den beschriebenen Mitteln mit dem Einsatz 6, 16 gekoppelt werden. Schließlich vesteht sich, daß die verschiedenen Merkmale auch in anderen als den dargestellten und beschriebenen Kombinationen angewendet werden können. The invention is not limited to the described embodiments, which can be modified in many ways. This applies in particular to the described dimensions and geometric shapes of the various parts. It should also be noted that the outer contour of the introduced into the recess 2 portion of the insert 6, 16 does not have to coincide with the inner contour of the recess 2 surrounding circumferential wall identical. It is only necessary that the body 5 has a sufficiently large volume to the space between the recess wall and the outer surface of the insert 6, 16 as completely as possible, ie volumetric fill. For this purpose, it would also be possible to form the body 5 substantially solid and instead form the insert 6, 16 at least on its underside as a hollow body, so that excess thermoplastic material can be accommodated in a cavity of the insert. In addition, the axial height of the body 5 could also be smaller than the depth of the recess 2. Further, it would be possible to insert the body 5 and the insert 6, 16 at the same time in the recess 2 by the body 5 z. B. formed as a hollow body and optionally with a slight interference fit on the insert 6, 16 is pushed until it z. B. from below against the flange 15th (Fig. 5) abuts. In this case, it would even be possible for the measure K 1 (FIG. 5) to be slightly larger than the dimension A; to choose. Also combinations of these two variants are possible. Of course, it would also be possible to dimension the axial length of the section of the insert 6 coming into the recess shorter than the depth of the recess 2 measured in the axial direction. Furthermore, the sonotrode 9, 18 could be coupled to the insert 6, 16 by means other than those described. Finally, it is understood that the various features can also be used in combinations other than those illustrated and described.
Claims
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2002351673A AU2002351673A1 (en) | 2001-11-17 | 2002-11-14 | Method for fixing an insert in a component consisting of a lightweight material |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10156640.9 | 2001-11-17 | ||
| DE10156640 | 2001-11-17 | ||
| DE10250118.1 | 2002-10-22 | ||
| DE10250118A DE10250118A1 (en) | 2001-11-17 | 2002-10-22 | Method for attaching an insert to a component made of a lightweight material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2003046390A2 true WO2003046390A2 (en) | 2003-06-05 |
| WO2003046390A3 WO2003046390A3 (en) | 2003-09-12 |
Family
ID=26010608
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/DE2002/004227 Ceased WO2003046390A2 (en) | 2001-11-17 | 2002-11-14 | Method for fixing an insert in a component consisting of a lightweight material |
Country Status (2)
| Country | Link |
|---|---|
| AU (1) | AU2002351673A1 (en) |
| WO (1) | WO2003046390A2 (en) |
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Also Published As
| Publication number | Publication date |
|---|---|
| AU2002351673A1 (en) | 2003-06-10 |
| WO2003046390A3 (en) | 2003-09-12 |
| AU2002351673A8 (en) | 2003-06-10 |
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