DE19523900C1 - Process for the pretreatment of a plastic surface to be glued - Google Patents
Process for the pretreatment of a plastic surface to be gluedInfo
- Publication number
- DE19523900C1 DE19523900C1 DE19523900A DE19523900A DE19523900C1 DE 19523900 C1 DE19523900 C1 DE 19523900C1 DE 19523900 A DE19523900 A DE 19523900A DE 19523900 A DE19523900 A DE 19523900A DE 19523900 C1 DE19523900 C1 DE 19523900C1
- Authority
- DE
- Germany
- Prior art keywords
- laser
- glued
- adhesive
- track
- plastic
- 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.)
- Expired - Fee Related
Links
- 238000000034 method Methods 0.000 title claims description 39
- 239000004033 plastic Substances 0.000 title claims description 33
- 229920003023 plastic Polymers 0.000 title claims description 33
- 230000005855 radiation Effects 0.000 claims description 8
- 239000000049 pigment Substances 0.000 claims description 5
- 239000003365 glass fiber Substances 0.000 claims description 4
- 239000012764 mineral filler Substances 0.000 claims description 2
- 239000006229 carbon black Substances 0.000 claims 1
- 230000001070 adhesive effect Effects 0.000 description 50
- 239000000853 adhesive Substances 0.000 description 48
- 230000008018 melting Effects 0.000 description 8
- 238000002844 melting Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 6
- 239000000835 fiber Substances 0.000 description 5
- 239000011148 porous material Substances 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 239000002131 composite material Substances 0.000 description 3
- 238000011161 development Methods 0.000 description 3
- -1 polybutylene terephthalate Polymers 0.000 description 3
- 229920000642 polymer Polymers 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 239000004071 soot Substances 0.000 description 3
- 238000005979 thermal decomposition reaction Methods 0.000 description 3
- 229920009788 PA66 GF30 Polymers 0.000 description 2
- 229920006497 PA66-GF30 Polymers 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229920006332 epoxy adhesive Polymers 0.000 description 2
- 238000005530 etching Methods 0.000 description 2
- 229920001155 polypropylene Polymers 0.000 description 2
- 238000007788 roughening Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229920007776 PBT GF30 Polymers 0.000 description 1
- 229920007017 PBT-GF30 Polymers 0.000 description 1
- 229920012055 PEEK GF30 Polymers 0.000 description 1
- 229920006927 PEEK-GF30 Polymers 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000004734 Polyphenylene sulfide Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920001707 polybutylene terephthalate Polymers 0.000 description 1
- 229920000069 polyphenylene sulfide Polymers 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/0006—Working by laser beam, e.g. welding, cutting or boring taking account of the properties of the material involved
-
- 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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0078—Measures or configurations for obtaining anchoring effects in the contact areas between layers
- B29C37/0082—Mechanical anchoring
-
- 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
- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/16—Surface shaping of articles, e.g. embossing; Apparatus therefor by wave energy or particle radiation, e.g. infrared heating
-
- 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
-
- 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
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/024—Thermal pre-treatments
- B29C66/0246—Cutting or perforating, e.g. burning away by using a laser or using hot air
-
- 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
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- 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
-
- 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
- B29C66/30321—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 protrusions belonging to at least one of the parts to be joined
- B29C66/30322—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 protrusions belonging to at least one of the parts to be joined in the form of rugosity
-
- 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
- B29C66/3034—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes
-
- 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
- B29C66/731—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 intensive physical properties of the material of the parts to be joined
- B29C66/7316—Surface properties
- B29C66/73161—Roughness or rugosity
-
- 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
- B29C66/733—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 optical properties of the material of the parts to be joined, e.g. fluorescence, phosphorescence
- B29C66/7332—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 optical properties of the material of the parts to be joined, e.g. fluorescence, phosphorescence at least one of the parts to be joined being coloured
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/16—Composite materials, e.g. fibre reinforced
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/30—Organic material
- B23K2103/42—Plastics
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
- B29C35/0805—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
- B29C2035/0838—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using laser
-
- 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
- B29C2791/00—Shaping characteristics in general
- B29C2791/004—Shaping under special conditions
- B29C2791/009—Using laser
-
- 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
-
- 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
- B29C66/72—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 structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
-
- 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
- B29C66/72—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 structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
- B29C66/72143—Fibres of discontinuous lengths
-
- 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
-
- 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
- B29C66/7394—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 thermoset
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/0005—Condition, form or state of moulded material or of the material to be shaped containing compounding ingredients
- B29K2105/0032—Pigments, colouring agents or opacifiyng agents
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/16—Fillers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2309/00—Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
- B29K2309/08—Glass
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Plasma & Fusion (AREA)
- Thermal Sciences (AREA)
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Description
Die Erfindung betrifft ein Verfahren zur Vorbehandlung von wenigstens einer zu verklebenden Oberfläche aus Kunststoff nach der Gattung des Hauptanspruchs.The invention relates to a method for pretreating at least one plastic surface to be glued according to the genus of the main claim.
Zur Verbesserung der Festigkeits- und Dichtigkeitseigen
schaften von beispielsweise Kunststoff/Kunststoff oder
Kunststoff/Stahl-Klebverbindungen sind eine Reihe von
konventionellen Behandlungsverfahren bekannt, mit denen
wenigstens eine zu verklebende Oberfläche vorbehandelt wird.
Ein mechanisches Behandlungsverfahren kann darin bestehen,
daß mit einer besandeten Oberfläche, wie Schleifpapier oder
durch Sandstrahlen die zu behandelnde Klebfläche aufgerauht
wird. Desweiteren ist eine Reihe von physikalischen
Behandlungsverfahren bekannt, wie Corona und
Niederdruckplasma-Entladung als auch eine Vorbehandlung mit
einem Excimer-Laser (UV-Laser). R. Bütje, u. a.:
"Klebflächenvorbehandlung von Kunststoffen durch Excimer-Laser",
Laser und Optoelektronik 21 (1989) 6, S. 62-66.To improve the strength and tightness properties of, for example, plastic / plastic or plastic / steel adhesive bonds, a number of conventional treatment processes are known, with which at least one surface to be bonded is pretreated. A mechanical treatment process can consist in roughening the adhesive surface to be treated with a sanded surface such as sandpaper or by sandblasting. Furthermore, a number of physical treatment methods are known, such as corona and low-pressure plasma discharge and pretreatment with an excimer laser (UV laser). R. Bütje, among others:
"Adhesive surface pretreatment of plastics by excimer laser", Laser und Optoelektronik 21 (1989) 6, pp. 62-66.
Die ultraviolette Strahlung der Excimer-Laser wird in Kunststoffen sehr stark absorbiert. Diese emittierte Strahlung hoher Intensität bewirkt, daß bei hochmolekularen Stoffen, wie Kunststoffen, ein Aufbrechen der Molekülketten durch fotochemische Prozesse erfolgt. Dadurch kommt es zur Bildung von polaren Gruppen an der Oberfläche, die sich wiederum positiv auf die Haftungseigenschaften auswirken können.The ultraviolet radiation from the excimer laser is in Very strongly absorbed plastics. This emitted High intensity radiation causes high molecular weight Substances, such as plastics, break the molecular chains through photochemical processes. This leads to Formation of polar groups on the surface, which in turn can have a positive effect on the adhesive properties.
Aus der DE 39 03 153 A1 ist ein Verfahren zur Behandlung von zu verklebenden Oberflächen aus Faserverbundwerkstoffen bekannt, bei dem mittels einer von einem CO₂-Laser erzeugten Laserstrahlung das ausgehärtete Polymer des Faserverbundwerkstoffes bis in eine definierte Tiefe abgetragen wird. Die oberste Faserlage des Laserverbundwerkstoffs wird freigelegt, wobei die Fasern jedoch keine kennbare Schädigung davontragen sollen. Durch das Abschmelzen des ausgehärteten Polymers an der Oberfläche wird somit aufgrund der an die Oberfläche getretenen Faserstruktur eine strukturierte Oberfläche erzeugt, die sich als Haftgrund für einen Kleber eignet.DE 39 03 153 A1 describes a method for the treatment of surfaces to be bonded from fiber composite materials known in which generated by a CO₂ laser Laser radiation the cured polymer of the Fiber composite material to a defined depth is removed. The top fiber layer of the Laser composite is exposed, leaving the fibers but should not suffer any noticeable damage. By melting of the cured polymer on the surface is thus due to the surface Fiber structure creates a textured surface that is suitable as a primer for an adhesive.
Ohne ein Abtragen des Kunststoffes an der Oberfläche kommt die Lehre der DE 42 28 040 A1 aus. Hierbei wird durch Bestrahlen der zu verklebenden Oberfläche mit UV-Strahlung die Molekularstruktur des Kunststoffmaterials an der Oberfläche aufgespalten. Ein physikalisches Aufrauhen der Oberfläche wird mit diesem Verfahren nicht erzielt.Without removing the plastic on the surface comes the teaching of DE 42 28 040 A1. Here is by Irradiate the surface to be glued with UV radiation the molecular structure of the plastic material on the Split surface. A physical roughening of the Surface is not achieved with this process.
Aus der US 4 925 523 ist ein Verfahren zum Abtragen und Ätzen von Substraten aus Polymeren bekannt, wobei zum Abtragen beziehungsweise Ätzen eine gepulste UV-Laser-Strahlung eingesetzt wird.From US 4 925 523 a method for removing and Etching of substrates made of polymers is known, with the Removing or etching a pulsed UV laser radiation is used.
Das erfindungsgemäße Verfahren mit den kennzeichnenden Merkmalen des Hauptanspruchs führt zu einer wesentlichen Verbesserung der Festigkeits- und Dichtigkeitseigenschaften der Klebverbindungen, indem durch das erfindungsgemäße Verfahren die wirksame Klebefläche vergrößert wird.The method according to the invention with the characteristic features of the main claim leads to a substantial improvement in Strength and tightness properties of the adhesive connections, by the effective by the inventive method Adhesive area is enlarged.
Durch das zumindest teilweise Aufschmelzen und Wiedererstarren der zu verklebenden Oberfläche des Kunststoffes wird eine rauhe Oberflächenstruktur geschaffen, die im wesentlichen durch Poren und/oder Aufwerfungen geprägt ist. Gleichzeitig kann die durch wenigstens teilweise Aufschmelzen vorbehandelte Kunststoffoberfläche Hinterschneidungen aufweisen, die nach dem Aufschmelzen der Oberfläche durch Erstarren der vorbehandelten Kunststoffoberfläche entstehen können.By at least partially melting and re-solidifying the surface of the plastic to be glued becomes rough Surface structure created essentially by pores and / or poses. At the same time, the through pretreated at least partially melting Plastic surface have undercuts that after the Melt the surface by solidifying the pretreated Plastic surface can arise.
Diese rauhe Oberflächenstruktur ist insbesondere dann von Vorteil, wenn zwei miteinander zu verklebende Kunststoffoberflächen gemäß dem erfindungsgemäßen Verfahren vorbehandelt worden sind. Diese Hinterschneidungen können wesentlich zu der Erhöhung der Klebfestigkeit beitragen, da sie bei der Beanspruchung der Klebverbindung durch darauf einwirkende Kräfte als Widerhaken beziehungsweise Verhakungen zumindest teilweise ineinandergreifen können und somit eine höhere Klebfestigkeit zur Folge haben.This rough surface structure is particularly of Advantage if two to be glued together Plastic surfaces according to the inventive method have been pretreated. These undercuts can contribute significantly to the increase in adhesive strength as they when the adhesive connection is stressed by it acting forces as barbs or hooks can interlock at least partially and thus one result in higher adhesive strength.
Ein weiterer Vorteil des erfindungsgemäßen Verfahrens zur Vorbehandlung von zu verklebenden Kunststoffoberflächen liegt in der verbesserten Klima- und Temperaturwechsel beständigkeit. Die nach dem Aufschmelzen erstarrte rauhe Oberflächenstruktur der vorbehandelten und zu verklebenden Oberfläche bleibt in ihrer Struktur über eine längere Zeitdauer vollständig erhalten, ohne daß eine Änderung der Haftungseigenschaften der Klebefläche eintritt.Another advantage of the inventive method for Pretreatment of plastic surfaces to be glued lies in the improved climate and temperature changes resistance. The rough solidified after melting Surface structure of the pretreated and to be glued The surface remains in its structure over a longer period Time period fully preserved without changing the Adhesive properties of the adhesive surface occurs.
Ein weiterer Vorteil des erfindungsgemäßen Verfahrens liegt darin, daß durch den Einsatz eines Lasers eine gezielte und definierte Vorbehandlung ermöglicht ist. Dadurch können bevorzugt eng begrenzte Klebflächen vorbehandelt werden, ohne daß benachbarte empfindliche elektrische oder elektronische Bauteile geschädigt werden.Another advantage of the method according to the invention lies the fact that by using a laser a targeted and defined pretreatment is made possible. This allows preferably narrowly delimited adhesive surfaces are pretreated without that neighboring sensitive electrical or electronic Components are damaged.
Eine vorteilhafte Weiterbildung des Verfahrens ist die Vorbehandlung der zu verklebenden Kunststoffoberfläche durch ein wenigstens teilweise thermisches Zersetzen der obersten Randschicht der Klebfläche. Dies führt zu einer weiteren Erhöhung der Rauhigkeit der vorbehandelten Oberflächenstruktur, so daß dadurch die wirksame Klebfläche weiter vergrößert werden kann. Die Klebfestigkeit kann um ein weiteres Maß erhöht werden.An advantageous development of the method is Pretreat the plastic surface to be glued an at least partial thermal decomposition of the top one Edge layer of the adhesive surface. This leads to another Increasing the roughness of the pretreated Surface structure, so that the effective adhesive surface can be further enlarged. The adhesive strength can be a further measure can be increased.
Eine weitere vorteilhafte Ausführungsform des Verfahrens ist der Einsatz des Lasers im Infrarot-Bereich zwischen 780 nm bis 1 mm, vorzugsweise 1,06 µm bis 10,6 µm. In diesem Wellenlängenbereich kann erreicht werden, daß die Kunststoffe in der obersten Randschicht und einer unmittelbar darunterliegenden Zone zumindest teilweise thermisch zersetzt als auch aufgeschmolzen werden.Another advantageous embodiment of the method is the use of the laser in the infrared range between 780 nm to 1 mm, preferably 1.06 µm to 10.6 µm. In this Wavelength range can be achieved that the plastics in the top edge layer and one immediately underlying zone at least partially thermally decomposed be melted as well.
Nach einer weiteren vorteilhaften Weiterbildung des Verfahrens wird der Laser linienförmig über die zu verklebende Oberfläche geführt. In Abhängigkeit der durch die eingestellten Parameter des Lasers, wie beispielsweise Energiedichte, Pulsdauer bzw. Pulsfrequenz als auch Vorschubgeschwindigkeit kann die Größe der zu erzeugenden bzw. entstehenden Poren und/oder Aufwerfungen bestimmt wer den. Bei der linienförmigen Führung des Lasers über die vorzubehandelnde Oberfläche entsteht somit eine gewisse Spurbreite. Die Lage der nachfolgenden Spur des Lasers in entgegengesetzter Richtung zu der zuvor erzeugten Spurbreite ist dabei derart bestimmt, daß die in der weiteren, parallel dazu verlaufenden Spur entstehenden Poren und/oder Aufwerfungen nahezu unmittelbar an die Poren und/oder Aufwerfungen der zuvor erzeugten Spur angrenzen, so daß ein Spurüberlapp von nahezu Null vorgesehen sein kann. Somit kann die Klebfläche nahezu vollständig durch den Laser beispielsweise linienförmig abgescannt und vorbehandelt werden. Der Laser kann sowohl im Zick-Zack-Betrieb über die zu behandelnde Fläche als auch immer nur von einer Seite zur anderen geführt werden.According to a further advantageous development of the The laser process becomes linear across the process adhesive surface led. Depending on the through the set parameters of the laser, such as Energy density, pulse duration or pulse frequency as well Feed rate can be the size of the generated or the resulting pores and / or poses the. With the linear guidance of the laser over the pretreated surface thus creates a certain Track width. The location of the subsequent trace of the laser in opposite direction to the previously created track width is determined so that in the further, parallel pores and / or traces that run along this Poses almost immediately on the pores and / or Border on the previously generated track so that a Almost zero track overlap can be provided. So can the adhesive surface almost completely by the laser for example, scanned in line and pretreated will. The laser can be used in zigzag mode surface to be treated as well as only from one side to the others.
Nach einer vorteilhaften Weiterbildung des Verfahrens ist vorgesehen, daß die Aufwerfungen und/oder Poren, die in einer Reihe liegen und eine Spur bilden, ebenfalls einen Überlapp aufweisen, der nahezu Null ist, d. h., daß die jeweilige Aufwerfung an die nächstfolgende angrenzt. Somit kann bei hoher Bearbeitungsgeschwindigkeit die wirksame Klebfläche stark vergrößert werden, was zu einer Verbesserung der Festigkeitseigenschaften der Klebverbindung führt.According to an advantageous development of the method provided that the poses and / or pores in a Lie in a row and form a track, also an overlap have almost zero, d. that is, the respective Posing adjacent to the next one. Thus at high processing speed the effective adhesive surface be greatly enlarged, leading to an improvement in Strength properties of the adhesive bond leads.
Der Laser kann vorteilhafterweise gepulst auf die vorzubehandelnde Oberfläche einwirken, wobei vor teilhafterweise ein Q-switch-Betrieb dafür vorgesehen ist, dessen Q-switch-Frequenz bis zu 50 kHz betragen kann. Desweiteren ist vorteilhafterweise vorgesehen, daß zumindest die zu verklebende Oberfläche eingelagerte Farbpigmente aufweist. Dadurch kann eine wesentliche Erhöhung des Absorptions-Koeffizienten erzielt werden, der den Effekt des thermischen Zersetzens als auch des Aufschmelzens der Oberfläche begünstigt. Insbesondere ist dies der Fall, wenn Ruß in dem Kunststoff eingelagert ist. Die Einlagerung derartiger Pigmente kann vorteilhafterweise in einem Bereich von 0,02 Volumen-% bis 20 Volumen-% liegen. Dadurch kann mit einer relativ geringen Energie und einer kurzen Bearbeitung- bzw. Einwirkdauer eine relativ hohe Oberflächenrauhigkeit erzielt werden. Eine chemische Veränderung der Oberfläche spielt bei diesen Prozessen eine eher untergeordnete Rolle.The laser can advantageously be pulsed onto the pretreat surface to be treated, before partly a Q-switch operation is provided for whose Q-switch frequency can be up to 50 kHz. Furthermore, it is advantageously provided that at least the surface to be glued embedded color pigments having. This can significantly increase the Absorption coefficient can be achieved, the effect of thermal decomposition and melting of the Favored surface. In particular, this is the case if Soot is stored in the plastic. The storage Such pigments can advantageously range from 0.02% by volume to 20% by volume. This allows using a relatively low energy and a short processing or Exposure time a relatively high surface roughness be achieved. A chemical change in the surface plays a rather subordinate role in these processes.
Eine weitere vorteilhafte Ausgestaltung des Verfahrens kann darin liegen, daß glasfaserverstärkter Kunststoff vorbehandelt wird. Dabei kann während des Einwirkens mit dem Laser auf die Oberfläche durch den Laserstrahl ein zumindest teilweises Freilegen von Glasfasern erfolgen, die nach dem Verkleben von zwei Klebflächen den Verhakungseffekt erhöhen können. Dadurch kann eine weitere Verbesserung der Festigkeitseigenschaften von Klebverbindungen geschaffen werden.A further advantageous embodiment of the method can are that glass fiber reinforced plastic is pretreated. It can be while working with the Laser onto the surface by the laser beam at least partial exposure of glass fibers take place after the Gluing two adhesive surfaces increases the interlocking effect can. This can further improve the Strength properties of adhesive bonds created will.
Ein bevorzugtes Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt und in der nachfolgenden Beschreibung näher erläutert. Es zeigen:A preferred embodiment of the invention is in the Drawing shown and in the description below explained in more detail. Show it:
Fig. 1 eine schematische Schnittdarstellung einer nach dem erfindungsgemäßen Verfahren vorbehandelten Oberfläche aus Kunststoff, Fig. 1 is a schematic sectional view of a pre-treated according to the inventive method the surface of plastic,
Fig. 2 eine schematische Schnittdarstellung von zwei vorbehandelten Oberflächen aus Kunststoff, die eine Klebverbindung bilden und Fig. 2 is a schematic sectional view of two pretreated plastic surfaces that form an adhesive connection and
Fig. 3 eine Draufsicht auf eine teilweise vorbehandelte Klebfläche. Fig. 3 is a plan view of a partially pretreated adhesive surface.
Fig. 1 zeigt eine Schnittdarstellung eines Kunststoffteils 11 mit einer vorbehandelten und zu verklebenden Oberfläche 12 und einer unvorbehandelten Oberfläche 13. Das Kunststoffteil 11 kann aus einem Thermoplast, Duroplast oder Elastomer hergestellt sein, wobei bevorzugt thermoplastische Kunststoffe, wie beispielsweise Polyamid, Polybuthylenterephthalat, Polyphenylensulfid, Polypropylen oder dergleichen verwendet werden. Fig. 1 shows a sectional view of a plastic part 11 with a pretreated surface to be bonded 12 and a pretreated surface 13 of. The plastic part 11 can be made of a thermoplastic, thermoset or elastomer, preferably thermoplastic materials such as polyamide, polybutylene terephthalate, polyphenylene sulfide, polypropylene or the like are used.
Die zu verklebende Oberfläche 12 wird mit einem Festkörperlaser vorbehandelt, der vorteilhafterweise mit einer im Infrarotbereich liegenden Wellenlänge zwischen 780 nm bis 1 mm betrieben wird. Als besonders vorteilhaft hat sich ein Nd-YAG-Laser mit 1,06 µm Wellenlänge herausgestellt, mit dem eine deutliche Steigerung der Klebfestigkeit erzielbar ist. Zur Vorbehandlung kann ein gütegeschalteter Laser, also im Q-switch-Betrieb, eingesetzt werden, der vorteilhafterweise mit einer Q-switch-Frequenz bis 50 kHz betrieben wird. Die gepulste Energie kann dabei mit einer mittleren Leistungsdichte bis zu 10 MW/mm² und einer Pulsdauer von 50 ns bis 500 ns eingebracht werden, wobei dabei die mittlere Energiedichte zwischen 0,005 J/mm² bis 10 J/mm² betragen kann.The surface 12 to be glued is pretreated with a solid-state laser, which is advantageously operated with a wavelength in the infrared range between 780 nm to 1 mm. An Nd-YAG laser with a wavelength of 1.06 µm, with which a significant increase in the adhesive strength can be achieved, has proven to be particularly advantageous. A Q-switched laser, that is to say in Q-switch operation, can be used for the pretreatment, which is advantageously operated with a Q-switch frequency of up to 50 kHz. The pulsed energy can be introduced with an average power density of up to 10 MW / mm² and a pulse duration of 50 ns to 500 ns, whereby the average energy density can be between 0.005 J / mm² to 10 J / mm².
Die auf die zu verklebende Oberfläche 12 einwirkenden gepulsten Laserstrahlen bewirken, daß eine oberste Randschicht 14 zumindest teilweise thermisch zersetzt wird und eine darunterliegende Zone 15 zumindest teilweise aufge schmolzen wird. Dadurch entstehen Aufwerfungen 16, die unmittelbar nach dem Aufschmelzen erstarren und Vertiefungen oder Mulden zurücklassen. Durch eine linienförmige Führung des Lasers wird eine Vielzahl von Aufwerfungen 16 in einer Spur 26 (Fig. 3) aneinandergereiht. Durch die Bildung von Aufwerfungen 16 wird eine rauhe Oberfläche erzeugt, durch die die wirksame Klebfläche vergrößert und somit eine Verbesserung der Festigkeitseigenschaften der Klebverbindung erzielt wird. Zusätzlich kann dieser relativ groben Rauhigkeit der Oberfläche 12 zumindest an der obersten Randschicht 14 eine feinere Rauhigkeit 17 überlagert sein. Dadurch kann eine weitere Verbesserung der Festigkeitseigenschaft von Klebverbindungen 21 geschaffen sein. The pulsed laser beams acting on the surface 12 to be bonded cause an uppermost edge layer 14 to be at least partially thermally decomposed and an underlying zone 15 to be at least partially melted. This creates poses 16 which solidify immediately after melting and leave depressions or depressions behind. By means of a linear guiding of the laser, a large number of projections 16 are lined up in a track 26 ( FIG. 3). The formation of projections 16 produces a rough surface, through which the effective adhesive surface is increased and thus an improvement in the strength properties of the adhesive connection is achieved. In addition, this relatively coarse roughness of the surface 12 can be overlaid with a finer roughness 17 at least on the uppermost edge layer 14 . This can create a further improvement in the strength property of adhesive bonds 21 .
Die in einer Vielzahl von unterschiedlichen Formen erstarrten Aufwerfungen 16 können darüber hinaus auch Hinterschneidungen 18 aufweisen, die ebenfalls eine Verbesserung der Haftung des Klebstoffes bewirken.The projections 16 , which have solidified in a large number of different shapes, can also have undercuts 18 , which likewise improve the adhesion of the adhesive.
Das Kunststoffteil 11 kann insbesondere im Bereich der zu verklebenden Oberfläche 12 eingelagerte Farbpigmente 19 aufweisen. Die Farbpigmente 19 können mit einem Anteil von 0,02 Vol.-% bis 20 Vol.-% vorgesehen sein. Dabei kann es sich vorteilhaft um Ruß handeln, da dieser bei der Behandlung mit einem Laser im Infrarotbereich einen hohen Absorptions-Ko effizient aufweist, wodurch eine relativ niedere Energie ausreicht, um die erforderliche bzw. gewünschte Größe der Aufwerfungen 16 zu erzeugen. Vorteilhafterweise kann eine sehr kurze Behandlungszeit erzielt werden kann. Dadurch lassen sich die Taktzeiten für die Vorbehandlung von Kunststoffteilen 11 um ein erhebliches Maß reduzieren, wodurch auch die Herstellkosten gesenkt werden können.The plastic part 11 can in particular have colored pigments 19 embedded in the area of the surface 12 to be glued. The color pigments 19 can be provided in a proportion of 0.02% by volume to 20% by volume. Soot can advantageously be soot, since it has a high absorption coefficient when treated with a laser in the infrared range, as a result of which a relatively low energy is sufficient to produce the required or desired size of the projections 16 . A very short treatment time can advantageously be achieved. As a result, the cycle times for the pretreatment of plastic parts 11 can be reduced to a considerable extent, as a result of which the manufacturing costs can also be reduced.
In Fig. 2 ist eine Klebverbindung 21 aus zwei Kunststoffteilen 11, 11′ in einem schematischen Querschnitt dargestellt. Zwischen den beiden vorbehandelten Oberflächen 12, 12′ ist Klebstoff 22 eingebracht. Es handelt sich dabei beispielsweise um einen 1 K-Epoxid-Klebstoff. Desweiteren können in Abhängigkeit der verwendeten Werkstoffe für die Klebverbindung 21 weitere geeignete und bekannte Kleber eingesetzt werden. Die nach dem Aufschmelzen durch die La serstrahlen während des Erstarrungsprozesses gebildeten Hinterschneidungen 18 der Aufwerfungen 16 bewirken, daß beispielsweise eine höhere Festigkeit zwischen Kleber und Aufwerfung 16 ermöglicht ist, da es hierbei bereits zu einem Verhakungseffekt kommen kann. Desweiteren kann dieser Verhakungseffekt erzielt werden, wenn beispielsweise zwei Hinterschneidungen 18, 18′ der Aufwerfungen 16, 16′ sich gegenseitig hintergreifen können, so daß eine zusätzliche Verbesserung der Festigkeitseigenschaft der Klebverbindung 21 geschaffen werden kann. Vorteilhafterweise können die Berge und Täler der Aufwerfungen 16 zumindest teilweise ineinander greifen.In Fig. 2, an adhesive connection 21 from two plastic parts 11 , 11 'is shown in a schematic cross section. Between the two pretreated surfaces 12 , 12 ', adhesive 22 is introduced. For example, it is a 1-component epoxy adhesive. Furthermore, depending on the materials used for the adhesive connection 21, further suitable and known adhesives can be used. The undercuts 18 of the poses 16 formed after the melting by the laser rays during the solidification process have the effect that, for example, a higher strength between the adhesive and poses 16 is made possible, since this can already lead to a tangling effect. Furthermore, this interlocking effect can be achieved if, for example, two undercuts 18 , 18 'of the projections 16 , 16 ' can engage behind one another, so that an additional improvement in the strength property of the adhesive connection 21 can be created. Advantageously, the peaks and valleys of the projections 16 can at least partially interlock.
Ferner können zumindest die zu verklebenden Oberflächen 12, 12′ mineralische Füllstoffe als auch Glasfaserteilchen 23 enthalten, die mit einem Gewichtsanteil von 5% bis 75% eingebracht sein können. Während des Vorbehandlungsprozesses durch zumindest teilweise thermisches Zersetzen und Aufschmelzen der zu verklebende Oberflächen 12, 12′ werden die Glasfasern 23 zumindest teilweise freigelegt, so daß diese ebenfalls dazu beitragen, daß bei der Klebverbindung 21 ein Verhakungseffekt eintritt.Furthermore, at least the surfaces to be bonded 12 , 12 'contain mineral fillers as well as glass fiber particles 23 , which can be introduced with a weight fraction of 5% to 75%. During the pretreatment process by at least partially thermal decomposition and melting of the surfaces to be bonded 12 , 12 ', the glass fibers 23 are at least partially exposed, so that they also contribute to the fact that a sticking effect occurs in the adhesive connection 21 .
In Fig. 3 ist eine Draufsicht auf eine zu verklebende Oberfläche 12 eines Kunststoffteils 11 dargestellt. Der Laserstrahl wird linienförmig über die zu verklebende Oberfläche 12 geführt, wodurch in einer Linie liegende Aufwerfungen 16 erzeugt werden, deren Randbereiche bei angepaßter Q-switch-Frequenz unmittelbar aneinandergrenzen und einen Überlapp von nahezu Null aufweisen. Dadurch wird die Oberfläche bei kleinstmöglicher Bearbeitungszeit nahezu vollständig bearbeitet und vorbehandelt und führt zu einer wesentlichen Vergrößerung der wirksamen Klebfläche. Die Aufwerfungen 16 sind der Einfachheit halber rund dargestellt und können in der Realität in weiteren unterschiedlichen Formen auftreten.In Fig. 3 a top view is shown on an adherend surface 12 of a plastic part 11. The laser beam is guided in a line over the surface 12 to be bonded, as a result of which line-shaped projections 16 are generated, the edge regions of which adjoin one another at an adapted Q-switch frequency and have an overlap of almost zero. As a result, the surface is almost completely processed and pretreated with the shortest possible processing time and leads to a substantial increase in the effective adhesive area. The poses 16 are shown round for the sake of simplicity and can occur in reality in further different forms.
Zur Vorbehandlung der zu verklebenden Oberfläche 12 wird zunächst eine Spur 26′ von Aufwerfungen 16 entlang Pfeilrichtung 24 durch die linienförmige Führung des Lasers gebildet, der eine nächste Spur 26′ mit Pfeilrichtung 25 folgt. Dabei sind die Aufwerfungen 16 vorteilhafterweise derart angeordnet, daß sie bei der Annäherung an einen runden Durchmesser in deren Zwischenräumen 27 nahezu aneinander anliegen. Zumindest jedoch ist die parallel zu einer ersten Spur 26 verlaufende zweite Spur 26′ derart ausgebildet, daß ein Spurüberlapp innerhalb der Spur 26, 26′ nahezu Null ist. Die linienförmige Führung des Lasers kann sowohl längs als auch quer zu einer Längsseite einer beispielsweisen quadratischen oder rechteckförmigen Klebfläche geführt sein. Ebenso kann eine kreisförmige oder schraubenlinienförmige Führung zur Vorbehandlung der Klebfläche vorgesehen sein.For the pretreatment of the surface 12 to be glued, first a track 26 'of projections 16 along arrow direction 24 is formed by the linear guidance of the laser, which is followed by a next track 26 ' with arrow direction 25 . The projections 16 are advantageously arranged in such a way that when they approach a round diameter, they almost abut one another in the spaces 27 between them. At least, however, the second track 26 'running parallel to a first track 26 ' is designed such that a track overlap within the track 26 , 26 'is almost zero. The linear guidance of the laser can be performed both lengthways and crossways to a long side of a square or rectangular adhesive surface, for example. A circular or helical guide for pretreating the adhesive surface can also be provided.
Eine Strahlablenkung zur Erzeugung der Spur 26, 26′, 26′′ usw. erfolgt über einen Galvanometerscanner. Dadurch kann eine präzise Führung des Laserstrahls erzielt werden, der insbesondere bei zu verklebenden Oberflächen 12, die im Subquadratmillimeter-Bereich liegen können, genau gesteuert und vorbehandelt werden.A beam deflection to generate the track 26 , 26 ', 26 '', etc. takes place via a galvanometer scanner. As a result, a precise guidance of the laser beam can be achieved, which is precisely controlled and pretreated, in particular in the case of surfaces 12 to be bonded, which can lie in the sub-square millimeter range.
Ein Vergleich unterschiedlicher Vorbehandlungsverfahren zeigt, daß durch das erfindungsgemäße Verfahren eine wesentliche Erhöhung der Klebfestigkeit erzielt worden ist, wobei dies insbesondere bei dem Werkstoff Polypropylen am deutlichsten wird. Dem Vergleich wurde ein Zugscherversuch nach DIN 53 283 mit einem Überlapp von 5 mm zugrundegelegt, d. h., daß die sich überlappenden und vorbehandelten Oberflächen 12, 12′ über eine Breite von 5 mm überdecken und somit eine 5 mm breite Klebverbindung 21 bilden. Für die Klebverbindung 21 wurde ein 1 K-Epoxid-Klebstoff verwendet.A comparison of different pretreatment processes shows that a significant increase in the adhesive strength has been achieved by the process according to the invention, this being particularly clear in the case of polypropylene. The comparison was based on a tensile shear test according to DIN 53 283 with an overlap of 5 mm, ie that the overlapping and pretreated surfaces 12 , 12 'overlap a width of 5 mm and thus form a 5 mm wide adhesive connection 21 . A 1-component epoxy adhesive was used for the adhesive connection 21 .
Die Klebverbindung 21 ist zwischen zwei schwarzen Fügeteilen hergestellt worden.The adhesive connection 21 has been produced between two black joining parts.
PG-GF30 ist im unbehandelten Zustand praktisch nicht verklebbar. Die Vorbehandlung der Kunststoffoberflächen durch Bestrahlung mit Corona über eine Zeitdauer von 3 Sekunden ergab eine Klebfestigkeit von 0,5 N/mm². Eine Verbesserung der Klebfestigkeit demgegenüber ergab die Bestrahlung durch Niederdruckplasma über eine Zeitdauer zwischen 60 Sekunden bis 120 Sekunden, wodurch eine Klebfestigkeit von 2,5 N/mm² erzielt wurde. Die Vorbehandlung mittels eines Excimer-Lasers erhöhte die Klebfestigkeit bis auf 5,2 N/mm². Die Vorbehandlung von Kunststoffoberflächen mittels Festkörperlaser gemäß dem erfindungsgemäßen Verfahren ergab eine Klebfestigkeit von 9 N/mm². Ähnliche Ergebnisse ergab es für die Werkstoffe PEEK-GF30, PBT-GF30, PA66-GF30 trocken, PA66-GF30 feucht.PG-GF30 is practically not in the untreated state can be glued. The pretreatment of the plastic surfaces by Irradiation with Corona over a period of 3 seconds gave an adhesive strength of 0.5 N / mm². An improvement the adhesive strength, on the other hand, gave the radiation through Low pressure plasma over a period of between 60 seconds up to 120 seconds, resulting in an adhesive strength of 2.5 N / mm² was achieved. Pretreatment using an excimer laser increased the adhesive strength up to 5.2 N / mm². The Pretreatment of plastic surfaces with Solid-state lasers according to the inventive method resulted an adhesive strength of 9 N / mm². It gave similar results for the materials PEEK-GF30, PBT-GF30, PA66-GF30 dry, PA66-GF30 moist.
Es versteht sich von selbst, daß das erfindungsgemäße Verfahren für eine Klebverbindung 21 eingesetzt werden kann, bei der beispielsweise zwei Kunststoffteile miteinander verklebt werden, ein Kunststoffteil und ein Stahlteil, ein Kunststoffteil und ein aus einem weiteren Werkstoff bestehendes Teil. Desweiteren kann eine Klebverbindung aus einem Kunststoffteil mit einer vorbehandelten Oberfläche und einem weiteren Teil mit einer vorbehandelten oder nicht vorbehandelten Oberfläche bestehen.It goes without saying that the method according to the invention can be used for an adhesive connection 21 , in which, for example, two plastic parts are glued together, a plastic part and a steel part, a plastic part and a part consisting of a further material. Furthermore, an adhesive connection can consist of a plastic part with a pretreated surface and another part with a pretreated or non-pretreated surface.
Claims (11)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19523900A DE19523900C1 (en) | 1995-06-30 | 1995-06-30 | Process for the pretreatment of a plastic surface to be glued |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19523900A DE19523900C1 (en) | 1995-06-30 | 1995-06-30 | Process for the pretreatment of a plastic surface to be glued |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE19523900C1 true DE19523900C1 (en) | 1997-01-16 |
Family
ID=7765707
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19523900A Expired - Fee Related DE19523900C1 (en) | 1995-06-30 | 1995-06-30 | Process for the pretreatment of a plastic surface to be glued |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE19523900C1 (en) |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0957058A3 (en) * | 1998-05-13 | 2000-04-05 | L.G.L. Electronics S.p.A. | Device for the self-adjusted braking of the yarn for weft feeders |
| FR2796388A1 (en) * | 1999-07-16 | 2001-01-19 | Robert Stehle | surface treatment for aerospace applications, etc includes changing surface roughness measured perpendicular and in plane of surface before applying adhesive or decorative material |
| DE10105893A1 (en) * | 2001-02-09 | 2002-08-22 | Bosch Gmbh Robert | Laminar component, is produced by forming micro-structured cut-outs in the surface of one of the seam sections using a laser, and then adhering the surfaces together |
| EP1398144A3 (en) * | 2002-09-16 | 2004-12-15 | Sellner GmbH | Laminated trim element |
| WO2010012705A1 (en) * | 2008-07-28 | 2010-02-04 | Robert Bosch Gmbh | Component composite and method for manufacturing a component composite |
| DE102008063651A1 (en) * | 2008-12-18 | 2010-07-01 | Institut Für Verbundwerkstoffe Gmbh | Method for connecting two workpieces, involves removing matrix materials at surfaces of workpieces in joining zone chemically, thermally or mechanically to expose individual fibers |
| WO2011020640A1 (en) * | 2009-08-17 | 2011-02-24 | Robert Bosch Gmbh | Component composite and method for producing a component composite |
| WO2011098329A1 (en) * | 2010-02-11 | 2011-08-18 | Robert Bosch Gmbh | Ignition coil |
| US8209831B2 (en) | 2006-02-02 | 2012-07-03 | Daimler Ag | Surface conditioning for thermal spray layers |
| EP2669041A1 (en) * | 2012-05-30 | 2013-12-04 | EADS Deutschland GmbH | Method for the nanostructuring and chemical modification of ceramic, glass, carbon, boron, silicon and composite materials |
| EP2669040A1 (en) * | 2012-05-30 | 2013-12-04 | EADS Deutschland GmbH | Method for the nanostructuring of ceramic, glass, carbon, boron, silicon and compound materials |
| US20150367538A1 (en) * | 2013-02-12 | 2015-12-24 | Polyplastics Co., Ltd. | Grooved resin molded part |
| CN105291449A (en) * | 2014-06-26 | 2016-02-03 | 宝理塑料株式会社 | Composite molding product and manufacturing method thereof |
| CN108237326A (en) * | 2016-12-26 | 2018-07-03 | 本田技研工业株式会社 | Junction structure and its manufacturing method |
| US10232547B2 (en) | 2014-03-25 | 2019-03-19 | Polyplastics Co., Ltd. | Composite molded article and method for manufacturing same |
| CN110383597A (en) * | 2017-01-16 | 2019-10-25 | 株式会社自动网络技术研究所 | Connection structural bodies |
| CN110871566A (en) * | 2018-08-31 | 2020-03-10 | 空中客车防卫和太空有限责任公司 | Method for the surface nanostructuring of carbon fibers in fiber composite plastics based on sulfur and aromatic hydrocarbons |
| CN109136802B (en) * | 2018-08-15 | 2020-05-29 | 沈阳工业大学 | Laser pretreatment corrosion-resistant strengthening process for aluminum alloy |
| CN112212905A (en) * | 2019-07-12 | 2021-01-12 | 大陆-特韦斯贸易合伙股份公司及两合公司 | Sensor with sealed envelope and exposed area |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4925523A (en) * | 1988-10-28 | 1990-05-15 | International Business Machines Corporation | Enhancement of ultraviolet laser ablation and etching organic solids |
| DE3903153A1 (en) * | 1989-02-02 | 1990-08-09 | Fraunhofer Ges Forschung | SURFACE TREATMENT OF FIBER COMPOSITES |
| DE4133620C1 (en) * | 1991-10-10 | 1993-04-22 | Maho Ag, 8962 Pfronten, De | |
| DE4228040A1 (en) * | 1992-05-12 | 1993-11-18 | Barberan Sa | Surface prepn. of plastic profiles for use with hot-melt adhesive - by irradiating with pulsed short wavelength radiation, esp. 320-440 nm UV, to form surface micro-cavities to allow penetration of adhesive |
-
1995
- 1995-06-30 DE DE19523900A patent/DE19523900C1/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4925523A (en) * | 1988-10-28 | 1990-05-15 | International Business Machines Corporation | Enhancement of ultraviolet laser ablation and etching organic solids |
| DE3903153A1 (en) * | 1989-02-02 | 1990-08-09 | Fraunhofer Ges Forschung | SURFACE TREATMENT OF FIBER COMPOSITES |
| DE4133620C1 (en) * | 1991-10-10 | 1993-04-22 | Maho Ag, 8962 Pfronten, De | |
| DE4228040A1 (en) * | 1992-05-12 | 1993-11-18 | Barberan Sa | Surface prepn. of plastic profiles for use with hot-melt adhesive - by irradiating with pulsed short wavelength radiation, esp. 320-440 nm UV, to form surface micro-cavities to allow penetration of adhesive |
Non-Patent Citations (1)
| Title |
|---|
| R.Bütje, u.a., "Klebflächenvorbehandlung von Kunststoffen durch Excimer-Laser", Laser und Optoelektronik 21 (1989), S.62-66 * |
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0957058A3 (en) * | 1998-05-13 | 2000-04-05 | L.G.L. Electronics S.p.A. | Device for the self-adjusted braking of the yarn for weft feeders |
| FR2796388A1 (en) * | 1999-07-16 | 2001-01-19 | Robert Stehle | surface treatment for aerospace applications, etc includes changing surface roughness measured perpendicular and in plane of surface before applying adhesive or decorative material |
| DE10105893A1 (en) * | 2001-02-09 | 2002-08-22 | Bosch Gmbh Robert | Laminar component, is produced by forming micro-structured cut-outs in the surface of one of the seam sections using a laser, and then adhering the surfaces together |
| EP1398144A3 (en) * | 2002-09-16 | 2004-12-15 | Sellner GmbH | Laminated trim element |
| US8209831B2 (en) | 2006-02-02 | 2012-07-03 | Daimler Ag | Surface conditioning for thermal spray layers |
| DE102006004769B4 (en) | 2006-02-02 | 2022-05-25 | Mercedes-Benz Group AG | Surface conditioning for thermal spray coatings |
| WO2010012705A1 (en) * | 2008-07-28 | 2010-02-04 | Robert Bosch Gmbh | Component composite and method for manufacturing a component composite |
| DE102008063651A1 (en) * | 2008-12-18 | 2010-07-01 | Institut Für Verbundwerkstoffe Gmbh | Method for connecting two workpieces, involves removing matrix materials at surfaces of workpieces in joining zone chemically, thermally or mechanically to expose individual fibers |
| WO2011020640A1 (en) * | 2009-08-17 | 2011-02-24 | Robert Bosch Gmbh | Component composite and method for producing a component composite |
| CN102470636A (en) * | 2009-08-17 | 2012-05-23 | 罗伯特·博世有限公司 | Component combination and method for processing component combination |
| CN102470636B (en) * | 2009-08-17 | 2015-11-25 | 罗伯特·博世有限公司 | Component combination and the method for tool member combination |
| WO2011098329A1 (en) * | 2010-02-11 | 2011-08-18 | Robert Bosch Gmbh | Ignition coil |
| CN102741951B (en) * | 2010-02-11 | 2016-05-18 | 罗伯特·博世有限公司 | Ignition coil |
| CN102741951A (en) * | 2010-02-11 | 2012-10-17 | 罗伯特·博世有限公司 | Ignition coil |
| EP2669040A1 (en) * | 2012-05-30 | 2013-12-04 | EADS Deutschland GmbH | Method for the nanostructuring of ceramic, glass, carbon, boron, silicon and compound materials |
| EP2669041A1 (en) * | 2012-05-30 | 2013-12-04 | EADS Deutschland GmbH | Method for the nanostructuring and chemical modification of ceramic, glass, carbon, boron, silicon and composite materials |
| US20150367538A1 (en) * | 2013-02-12 | 2015-12-24 | Polyplastics Co., Ltd. | Grooved resin molded part |
| US9610713B2 (en) * | 2013-02-12 | 2017-04-04 | Polyplastics Co., Ltd. | Grooved resin molded part |
| US10232547B2 (en) | 2014-03-25 | 2019-03-19 | Polyplastics Co., Ltd. | Composite molded article and method for manufacturing same |
| CN105291449A (en) * | 2014-06-26 | 2016-02-03 | 宝理塑料株式会社 | Composite molding product and manufacturing method thereof |
| CN105291449B (en) * | 2014-06-26 | 2018-11-20 | 宝理塑料株式会社 | Composite molded article and its manufacturing method |
| CN108237326A (en) * | 2016-12-26 | 2018-07-03 | 本田技研工业株式会社 | Junction structure and its manufacturing method |
| CN110383597A (en) * | 2017-01-16 | 2019-10-25 | 株式会社自动网络技术研究所 | Connection structural bodies |
| CN109136802B (en) * | 2018-08-15 | 2020-05-29 | 沈阳工业大学 | Laser pretreatment corrosion-resistant strengthening process for aluminum alloy |
| CN110871566A (en) * | 2018-08-31 | 2020-03-10 | 空中客车防卫和太空有限责任公司 | Method for the surface nanostructuring of carbon fibers in fiber composite plastics based on sulfur and aromatic hydrocarbons |
| CN112212905A (en) * | 2019-07-12 | 2021-01-12 | 大陆-特韦斯贸易合伙股份公司及两合公司 | Sensor with sealed envelope and exposed area |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE19523900C1 (en) | Process for the pretreatment of a plastic surface to be glued | |
| DE102011014017B4 (en) | Process for the pretreatment of a fiber composite material | |
| DE112020000517T5 (en) | Composite molding | |
| DE112015001385B4 (en) | Process for producing a composite molded article | |
| DE102004030619A1 (en) | Method for joining workpieces made of plastic | |
| DE112014000775T5 (en) | Grooved resin molding | |
| EP0811667B1 (en) | Method of manufacturing adhesive joints between surfaces, having good mechanical strength | |
| EP1428670A1 (en) | Printing apparatus and printing method using UV radiation curable ink | |
| DE602004007003T2 (en) | METHOD FOR MOUNTING ELEMENTS OF A CONSTRUCTION COMPRISING A WAVE CORE | |
| DE102008018286A1 (en) | Welding process and welding apparatus for a resin element | |
| DE3843230C1 (en) | Process for making a metallic pattern on a base, in particular for the laser structuring of conductor tracks | |
| DE10025360C1 (en) | Decorative strip for internal use in cars comprises upper strip with decorative outer surface which fits into recess in lower strip, inside upwardly-sloping outer section with different decorative outer surface | |
| DE4016210A1 (en) | Upgrading recycled plastics sheet - by activating treating surface applying e.g. adhesive, adding high strength surfaces and e.g. hot pressing | |
| DE102008025354A1 (en) | System to produce microstructured functional surfaces on substrates with laser, by individually/combinedly arranging substrate surfaces and device to couple, guide, focus or form laser beam as ultrashort pulse laser under normal condition | |
| DE10306697A1 (en) | Laser welding, to bond two plastics components together, has a web at one component fitting into an opening in the other, where the opening is filled with molten material by the laser beam heat | |
| DE102020204972A1 (en) | Process for the pretreatment of a paint surface | |
| DE10335446A1 (en) | Laser welding of plastic components involves location of energy absorber film between the two components | |
| EP1289354A1 (en) | Multilayer printed circuit board and process for manufacturing holes therein | |
| DE102019110124A1 (en) | Reactive injection molding process with activation by UV radiation | |
| DE19503038C1 (en) | Process for the production of chip cards | |
| DE10105893A1 (en) | Laminar component, is produced by forming micro-structured cut-outs in the surface of one of the seam sections using a laser, and then adhering the surfaces together | |
| DE102023119077B3 (en) | Method for producing a decorative part decorated with a Lichtenberg figure | |
| DE202008007122U1 (en) | Device for producing microstructured functional surfaces on substrates with at least one laser | |
| EP3645286B1 (en) | Component made up of several stacked layers, as well as a process for its manufacture | |
| DE102015008953B4 (en) | Process for pretreating thermoplastic components for structural bonding - and device for processing a surface |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8100 | Publication of the examined application without publication of unexamined application | ||
| D1 | Grant (no unexamined application published) patent law 81 | ||
| 8364 | No opposition during term of opposition | ||
| 8339 | Ceased/non-payment of the annual fee |