DK176367B1 - Materialelag til optagelse af overskydende lim - Google Patents
Materialelag til optagelse af overskydende lim Download PDFInfo
- Publication number
- DK176367B1 DK176367B1 DK200501302A DKPA200501302A DK176367B1 DK 176367 B1 DK176367 B1 DK 176367B1 DK 200501302 A DK200501302 A DK 200501302A DK PA200501302 A DKPA200501302 A DK PA200501302A DK 176367 B1 DK176367 B1 DK 176367B1
- Authority
- DK
- Denmark
- Prior art keywords
- glue
- adhesive
- layer
- parts
- joint
- Prior art date
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
- B29C66/50—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
- B29C66/63—Internally supporting the article during joining
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
- B29C65/485—Multi-component adhesives, i.e. chemically curing as a result of the mixing of said multi-components
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4865—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives
- B29C65/487—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their shape, e.g. being fibres or being spherical
- B29C65/488—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their shape, e.g. being fibres or being spherical being longitudinal, e.g. fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
- B29C65/5028—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being textile in woven or non-woven form
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—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
- B29C66/114—Single butt joints
- B29C66/1142—Single butt to butt joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—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
- B29C66/116—Single bevelled joints, i.e. one of the parts to be joined being bevelled in the joint area
- B29C66/1162—Single bevel to bevel joints, e.g. mitre joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—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
- B29C66/32—Measures for keeping the burr form under control; Avoiding burr formation; Shaping the burr
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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
- B29C66/41—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
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/524—Joining profiled elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—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
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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
- B29C66/543—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 joining more than two hollow-preforms to form said hollow articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—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
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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
- B29C66/80—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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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J5/00—Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
- B29C65/4835—Heat curing adhesives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4865—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives
- B29C65/4885—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding containing additives characterised by their composition being non-plastics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
- B29C65/5014—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being fibre-reinforced
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—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
- B29C66/727—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 being porous, e.g. foam
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3085—Wings
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
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- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
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- Y10T428/249955—Void-containing component partially impregnated with adjacent component
- Y10T428/249958—Void-containing component is synthetic resin or natural rubbers
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
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Description
DK 176367 B1
Opfindelsen angår en metode til sammenlimning af i det mindste to dele samt et emne omfattende i det mindste to sammenlimede dele herunder specielt 5 en vinge til et vindenergianlæg.
Baggrund
For at sikre en stærk sammenlimning af dele i en konstruktion er det vigtigt at 10 påføre tilstrækkeligt med lim til limfladerne. Som oftest flyder der derfor en vis mængde overskydende lim ud fra alle sider af limsamlingen, når delene presses sammen. Store tolerancer på delemnerne og dermed relativt store variationer på den endelige størrelse af limfugen gør det ligeledes svært at bestemme den nødvendige og tilstrækkelige mængde lim til en stærk sam-15 ling, hvilket løses enklest og hurtigst med at påføre lim i rigelige mængder.
Som regel fjernes den udflydende lim, og limfugen gøres glat både af æstetiske hensyn og ofte også af forskellige funktionelle hensyn. Dette kan gøres ved enten ganske enkelt at skrabe eller tørre limen af, inden den er hærdet færdig eller ved at fjerne den mekanisk, eksempelvis ved slibning.
20
Ved sammenlimning af helt eller delvist lukkede konstruktioner eller konstruktioner med specielle geometrier kan det imidlertid være svært eller ligefrem umuligt at fjerne overskydende lim presset ud fra samlingen. Dette er eksempelvis tilfældet for vinger til vindenergianlæg, som består af vingeskalier, 25 der limes sammen med indre afstivende bjælker. Her sidder den overskydende lim på indersiden af vingen i store ’grater’. Hvis disse ikke fjernes, vil de, når vingen tages i brug, i nogen grad brække af og rasle rundt i vingens indre. Dette er uønskværdigt i sig selv, fordi det sker under stor støjudbredelse til gene for vindmøllens omgivelser. Med tiden bliver limklumperne pulve-30 riseret af at blive kastet rundt, men ses da at indgå forbindelse med fugtighed og indtrængende vand i vingen og danne store hårde klumper, som dels DK 176367 B1 2 stopper drænhuller til og dels yder store slagpåvirkninger på vingens indre dele under vingens rotation.
For at undgå dette er det derfor ønskværdigt at fjerne den overskydende lim, 5 som presses ud fra limfugerne, når vingen samles. Dette kan gøres manuelt et stykke ind i vingen, hvilket imidlertid dels er en arbejds- og tidskrævende proces og dels ikke er ideelt af arbejdsmiljøårsager. Alternativt kan såkaldte limfangere, der ligner lange smalle tagrender, monteres inde i vingen, i hvilke limen render ned under samlingen, og som eventuelt derefter trækkes ud af 10 vingen igen. Dette er dog en omstændelig og tidskrævende proces.
I DK 175718 er den indre afstivende bjælke sat sammen af to bjælkedele, hvilket giver mulighed for at højdejustere den samlede højde af bjælken, således at der til en hvis grad kan kompenseres for dimensionsunøjagtigheder 15 på vingeskalierne. Bjælkedelene skal dog stadig limes sammen, hvorfor der også her er problemer med overskydende lim fra limsamlingerne. I skriftet anvendes såkaldte samlingspaneler, som monteres på kropsdelene rækkende henover samlingsfladen men med en spalte imellem, hvori en del af den overskydende lim så kan flyde ud i. Denne metode svarer til brugen af de 20 førnævnte limfangere og besidder de samme ulemper.
Det er kendt eksempelvis fra WO 03046394 at undgå grater af udflydende lim ved at lave specielle udformninger af den ene eller begge konstruktionsdeles limflader for eksempelvis med langsgående riller eller udskæringer, 25 hvori overskydende lim kan rende ned. Dette kræver imidlertid en mekanisk forarbejdning af samlefladerne, hvilket fordyrer limeprocessen betragteligt. Endvidere vil sådanne riller eller udskæringer kun kunne optage en vis mængde lim, og udflydende lim kan således ikke forhindres helt, hvis limfugen eksempelvis skal kompensere for store tolerancer og unøjagtigheder på 30 delemnerne og heraf følgende meget svingende behov for lim.
DK 176367 B1 3
Formål og beskrivelse af opfindelsen
Det er således et formål med opfindelsen at finde frem til en løsning på ovennævnte problem med overskydende og udflydende lim.
5 Dette opnås ifølge opfindelsen ved et emne omfattende i det mindste to sammeniimede dele, hvor mindst et lag med åben struktur indgår i det mindste delvist i limsamlingen mellem delene og optager overskydende lim uden for limsamlingen. Herved opnås det fordelagtige, at det ekstra og overflødige lim opsuges af det porøse lag og derved fastholdes ved limfugen uden sene-10 re at ville brække af. Det porøse materiale kan samtidig fungere som armering af limen og således også gøre limsamlingen stærkere. Dette muliggør videre at anvende en tyndere og mere letflydende lim, som er lettere at pumpe, og hvilket derfor kan øge hastigheden af limeprocessen. Endvidere er emnet ifølge opfindelsen fordelagtig ved, at det ikke er nødvendigt med spe-15 cielle udformninger eller forarbejdninger af delenes samleflader, idet det porøse lag kan udformes med en så høj fleksibilitet, at det let kan deformeres til at følge limfladernes form. Samtidig kan et lag porøst materiale udfylde og tilpasse sig limfuger af varierende tykkelser ved ganske enkelt at blive trykket passende sammen under limningen.
20 I en udførselsform af opfindelsen omfatter emnet et porøst lag, hvilket er i det mindste delvist preimpregneret med lim. Herved opnås på enkel vis en god kontrol med, dels hvor limen ligger og dels den udlagte mængde. Et forimpregneret materialelag er desuden enkelt og hurtigt at lægge på den 25 ene eller begge samiingsflader, og lagets placering kan styres præcist med enkle midler.
I en udførselsform har det porøse lag struktur som en svamp (med åbne porer) eller en netstruktur. Disse materialer er fordelagtige ved at kunne yde 30 kun ringe modstand mod limens fordeling, men samtidig virke ved at optage og fastholde og armere limen i materialet.
DK 176367 B1 4 I en yderligere udførselsform omfatter det porøse lag en filt af fibre. En sådan filt kan fremstilles ved lave produktionsomkostninger af mange forskellige slags fibermateriale.
5 I endnu en udførselsform er det porøse lag fremstillet af et fibermateriale, såsom eksempelvis glasfibre, plastfibre eller naturfibre, hvilke materialer er fordelagtige ved at kunne virke armerende på limsamlingen.
Opfindelsen angår desuden et emne ifølge ovenstående, hvor emnet udgør 10 en eller flere dele af en vinge til et vindenergianlæg samt anvendelsen af et eller flere af tidligere omtalte emner til fremstilling af en vinge til et vindenergianlæg. Fordelene hermed er som beskrevet i det ovenstående.
Opfindelsen angår desuden en metode til sammenlimning af i det mindste to 15 dele, hvilken metode omfatter trinnet at placere et porøst lag i det mindste delvist i limsamlingen til optagelse af overskydende lim fra limsamlingen.
Endelig angår opfindelsen desuden en metode til sammenlimning af i det mindste to dele ifølge førnævnte, som yderligere omfatter trinnet at fjerne et 20 yderste beskyttelseslag fra det porøse lag inden det porøse lag placeres i det mindste delvist i limsamlingen. Beskyttelseslaget kan eksempelvis være en siliconebelagt afrivningsfolie som kendt fra forskellige typer tape.
Kort beskrivelse af tegninger 25 I de følgende beskrives opfindelsen med henvisning til figurerne, hvor figur 1 viser sammenlimningen af to dele med et porøst lag i limsamlingen før og efter limning, 30 figur 2 viser sammenlimningen af to dele med et lag af svampeagtig struktur i limsamlingen før og efter limning, DK 176367 B1 5 figur 3 viser en limsamling med et porøst lag preimprægneret med lim før og efter limning, 5 figur 4 viser en sammenlimning af to dele med limflader af uens dimensioner før og efter limning, figur 5 viser et tværsnit af en vinge til et vindenergianlæg, 10 figur 6 viser i større detaljer limsamlingen ved en vindmøllevinges forkant, figur 7 viser i større detaljer limsamlingen ved en vindmøllevinges bagkant, figur 8 viser i større detaljer limsamlingerne øverst ved en vindmøllevinges 15 afstivende bjælker, og figur 9 viser en limsamling før og efter samling med et porøst lag anvendt som hjælpemiddel.
20 Beskrivelse af udførelsesformer
Figur 1 viser to dele 101 af en konstruktion, som sammenlimes til ét emne 102. Til venstre er delene 101 vist, før de er sat sammen, og til højre er det færdigt limede emne 102 vist. Limen 103 påføres som i en almindelig limeproces en eller begge samleflader 104, hvorefter et lag af et porøst materiale 25 105 placeres mellem limfladerne, og delene trykkes sammen som illustreret med pilene 106. For at opnå en stærk limsamling er det vigtigt, at der påføres en tilstrækkelig mængde lim, hvilket mest enkelt og hurtigst sikres ved at påføre rigeligt. Almindeligvis, og hvis det er muligt, fjernes den overskydende lim, som presses ud til siderne, når delene presses sammen. Dette gøres 30 dels af æstetiske grunde dels af funktionelle grunde, således at graterne af lim ikke senere brækker af og er til gene. Ifølge nærværende opfindelse lø- DK 176367 B1 6 ses dette problem imidlertid af det porøse lag materiale 105, i hvilket det overskydende lim flyder gennem og ud i. Efter endt limning er det overskydende lim således optaget og fastholdt ved limsamlingen af det porøses materiale 105 som illustreret til højre i figur 1, og limen vil således ikke senere 5 kunne brække eller falde af.
Laget 105, som limes med ind i emnet, skal være af en sådan struktur, at limen kan trænge igennem laget uden nævneværdig modstand og blive fastholdt i det. Dette opnås i en udførselsform af opfindelsen ved at anvende en 10 net-agtig struktur 107 som illustreret i figur 1. Materialet kan eksempelvis være fremstillet som en fleece eller en måtte af fibre, eksempelvis glasfibre, plastfibre og/eller naturfibre. Strukturen af fibrene kan være uordnet, som fremkommet ved teknikker fra filtning og curling, og som eksempelvis er kendt fra forskellige filterelementer. Alternativt kan fibrene være vævede eller 15 strikket i en ordnet tredimensional struktur som kendt fra eksempelvis fordelingsnet ved injektionsstøbning.
I figur 2 er ligesom i figur 1 vist sammenligningen af to dele 101 før (til venstre) og efter limning (til højre). I denne udførselsform er anvendt et lag mate-20 riale 105 i limsamlingen, som ligesom i figur 1 er porøst, men her har en materialestruktur som en svamp med åbne porer 201. Et sådant materiale tillader ligesom den net-agtige struktur 107 i den tidligere figur, at limen 103 kan trænge igennem laget 105, 201 og sammenføje begge dele 101 til ét emne 102 samtidig med, at den overskydende mængde lim som presses ud af lim-25 samlingen optages og fastholdes i laget 105.
Udover at fastholde den overskydende mængde lim fra limsamlingen kan det porøse lag 105 yderligere virke armerende og øge styrken af limsamlingen.
30 I figur 3 er illustreret yderligere en udførselsform af opfindelsen, hvor det porøse lag materiale 105 er preimpregneret med lim 103 i en del af måtten eller DK 176367 B1 7 laget. Under samlingsprocessen lægges måtten direkte på den ene samle-flade, hvorefter en hærder 302 påføres, umiddelbart inden delene 101 presses sammen. Som i de førnævnte udførselsformer vil limen 103 trænge gennem det porøse lag 105, og det overskydende lim vil optages i materialet.
5 Endvidere kan det porøse lag være preimpregneret med en færdig limblanding, som frigøres til hærdning, eksempelvis ved at et yderste beskyttelseslag pilles af laget 105 lige inden placering på samlefladen 104, ved varme, eller på anden kendt måde.
10 Ved visse emneformer, såsom helt eller delvist lukkede emner, kan det være fordelagtigt, at overskydende lim fjernes fra den ene side af limsamlingen 401, men optages og fastholdes i et porøst lag 105 på den anden limsamlingsside 402, for eksempel hvis denne side er svært tilgængelig. Det porøse lag 105 kan da i en udførselsform placeres i limsamlingen, således at den 15 kun stikker ud til den ene side som illustreret i figur 4. Hvor meget det porøse materiale 105 skal stikke ud fra limsamlingen afhænger af, hvor store mængder lim man vil sikre sig kan optages af materialet Ved sammenlimning af dele fremstillet med store tolerancer kan limfugens tykkelse variere betragteligt hen langs en samling, og mængden af overskydende lim vil derfor ligele-20 des variere. Laget af porøst materiale skal da være så bredt, at al den overskydende mængde lim, hvor limfugen er smallest, kan optages af materialet.
I figuren er ligeledes vist, at samlingsmetoden ikke er begrænset til sammenlimning af delemner 101 med samleflader 104 afens dimensioner, men også kan anvendes på delemner af forskellige dimensioner.
25 I figur 5 er skitseret tværsnittet af en vinge til et vindenergianlæg. Den skitserede vinge er fremstillet af to vingeskaller 501 af fiberforstærkede laminater. Vingeskalierne er limet sammen langs vingens forkant 502 og bagkant 503. I det indre er vingen afstivet af et antal bjælker 504. Når vingen samles, limes 30 først bjælkerne 504 fast på den underste vingeskal. Her kan overskydende lim let fjernes fra limsamlingerne. Dette er imidlertid ikke tilfældet, når den DK 176367 B1 8 øverste vingeskal limes på. Ved de ydre limfuger langs for- og bagkant fjernes det overskydende lim, hvorved sikres en glat overflade på vingen, hvilket er vigtigt for vingens aerodynamiske egenskaber. Ved de indre samlinger ved for- og bagkant og øverst ved bjælkerne er det fordelagtigt at anvende et po-5 røst materiale ifølge nærværende opfindelse til at opsamle den overskydende mængde lim, idet dette ellers vil sidde ved limsamlingerne i store grater.
Som tidligere omtalt vil disse eventuelt brække af senere og rasle rundt inde i vingen som følge af de normalt forekommende tøjninger i vingen, når denne under brug giver sig og arbejder. Især ved bjælkesamlingerne er problemet 10 stort, idet man her påfører ekstra store mængder lim for at tage højde for de forholdsvis store tykkelsesvariationer af limfugerne, der kan forekomme som følge af selv små unøjagtigheder af bjælkernes placering. Limsamlingerne ved vingens for- og bagkant og ved det øverste af bjælkerne er vist i større detaljer i figurerne 6-8.
15
En mulig limsammenføjning ifølge en udførselsform af opfindelsen af vingens forkant 502 er vist i figur 6. De to vingeskaller 501 er afsluttet skævt for at opnå en stærkere sammenføjning. I den indre del af limfugen 402 og stikkende ud i det indre af vingen er lagt et lag materiale 105 med net-agtig 20 struktur, hvilket dels armerer limen og dels optager og fastholder den del af den overskydende lim 103, som er presset ud fra den indre side af limfugen.
På ydersiden 401 fjernes overskydende lim, således at vingens yderside er glat og med bedst mulige aerodynamiske egenskaber.
25 Tilsvarende gøres ved vingens bagkant 503 som illustreret i figur 7. Imellem vingeskaliernes 501 limflader er placeret et porøst materiale 105, som i det indre af vingen optager det overskydende lim 103 fra limsamlingen.
Endelig er i figur 8 vist limsamlingen mellem bjælkerne 504 og den øverste 30 vingeskal 501. Her er ligeledes lagt et lag porøst materiale 105 mellem delene, der skal samles, hvilket materiale limen 103 kan trænge igennem med DK 176367 B1 9 forholdsvis ringe modstand, fylde limfugen ud og samtidig fastholde det overskydende lim 103. Som i de øvrige eksempler forhindres den overskydende lim således i at flyde ned og ud i det indre af vingen eller at sidde fasttørret i store grater. I den viste udførselsform er lagt en bred måtte 801 af porøst 5 materiale 105 ovenover begge bjælker 504. I stedet for én bred måtte kan anvendes et mindre stykke materiale for hver bjælkedel for sig, alt efter hvad der er procesmæssigt lettest og enklest at håndtere.
En yderligere anvendelsesmulighed for det porøse lag ifølge opfindelsen er 10 illustreret i figur 9. Her ses en limsamling - i dette tilfælde ved vingespidsen 901 - før (til venstre) og efter samling (til højre). På den ene vingeskals 501 samleflade 104 er det porøse materiale 105 lagt et stykke fra vingeskallens yderste kant og placeret, således at det kan anvendes til styre udlægningen af limen 103 efter. Endvidere kan tykkelsen af det porøse materiale i usam-15 mentrykket tilstand dimensioneres således, at den kan bruges som målestok og hjælpemiddel for bestemmelse og styring af den optimale dosering af lim.
Når limen udlægges i en mængde svarende til højden af det porøse materiale, er der således udlagt den tilstrækkelige og nødvendige mængde. Udlægningen af limen kan herved forenkles og styres betragteligt bedre, både hvad 20 angår placeringen og doseringsmængden af limen.
Det må forstås, at opfindelsen, således som den er omtalt i nærværende beskrivelse og figurer, kan modificeres eller ændres og fortsat være omfattet af beskyttelsesomfanget af de nedenstående patentkrav.
Claims (10)
1. Et emne omfattende i det mindste to sammenlimede dele kendetegnet ved, at mindst et lag med åben struktur indgår i det mindste delvist i limsam- 5 lingen mellem delene og optager overskydende lim uden for limsamlingen.
2. Et emne ifølge krav 1, hvor laget er i det mindste delvist preimpregneret med lim.
3. Et emne ifølge et eller flere af kravene 1-2, hvor laget har struktur som en svamp (med åbne porer).
4. Et emne ifølge et eller flere af kravene 1-2, hvor laget har netstruktur.
5. Et emne ifølge et eller flere af kravene 1-2, hvor laget omfatter en filt af fibre.
6. Et emne ifølge et eller flere af kravene 1-2 og/eller kravene 4-5, hvor laget er fremstillet af et fibermateriale, såsom eksempelvis glasfibre, plastfibre eller 20 naturfibre.
7. Et emne ifølge et eller flere af kravene 1-6, hvor emnet udgør en eller flere dele af en vinge til et vindenergianlæg.
8. En metode til sammenlimning af i det mindste to dele omfattende trinnet at placere mindst et lag med åben struktur i det mindste delvist i limsamlingen til optagelse af overskydende lim fra limsamlingen.
9. En metode til sammenlimning af i det mindste to dele ifølge krav 8 yderli-30 gere omfattende trinnet at fjerne et yderste beskyttelseslag fra laget inden laget placeres i det mindste delvist i limsamlingen. DK 176367 B1
10. Anvendelse af et eller flere emner ifølge et eller flere af kravene 1-7 til fremstilling af en vinge til et vindenergianlæg.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DK200501302A DK176367B1 (da) | 2005-09-19 | 2005-09-19 | Materialelag til optagelse af overskydende lim |
| AT06775990T ATE452952T1 (de) | 2005-09-19 | 2006-09-14 | Materialschicht zur aufnahme von überschüssigem klebstoff |
| BRPI0616225-8A BRPI0616225A2 (pt) | 2005-09-19 | 2006-09-14 | elemento constituÍdo de duas partes ligadas por adesço, lÂmina para uma turbina eàlica e mÉtodo de efetuar a junÇço de pelo menos duas partes por adesço |
| CN2006800344385A CN101268160B (zh) | 2005-09-19 | 2006-09-14 | 用于吸收多余粘合剂的材料层 |
| PCT/DK2006/000505 WO2007048408A1 (en) | 2005-09-19 | 2006-09-14 | A layer of material for uptake of excess adhesive |
| EP20060775990 EP1926790B1 (en) | 2005-09-19 | 2006-09-14 | A layer of material for uptake of excess adhesive |
| PL06775990T PL1926790T3 (pl) | 2005-09-19 | 2006-09-14 | Warstwa materiału do pobierania nadmiaru kleju |
| US11/992,118 US8426018B2 (en) | 2005-09-19 | 2006-09-14 | Layer of material for uptake of excess adhesive |
| DE200660011343 DE602006011343D1 (de) | 2005-09-19 | 2006-09-14 | Materialschicht zur aufnahme von überschüssigem klebstoff |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DK200501302A DK176367B1 (da) | 2005-09-19 | 2005-09-19 | Materialelag til optagelse af overskydende lim |
| DK200501302 | 2005-09-19 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DK200501302A DK200501302A (da) | 2007-03-20 |
| DK176367B1 true DK176367B1 (da) | 2007-10-01 |
Family
ID=37546896
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DK200501302A DK176367B1 (da) | 2005-09-19 | 2005-09-19 | Materialelag til optagelse af overskydende lim |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US8426018B2 (da) |
| EP (1) | EP1926790B1 (da) |
| CN (1) | CN101268160B (da) |
| AT (1) | ATE452952T1 (da) |
| BR (1) | BRPI0616225A2 (da) |
| DE (1) | DE602006011343D1 (da) |
| DK (1) | DK176367B1 (da) |
| PL (1) | PL1926790T3 (da) |
| WO (1) | WO2007048408A1 (da) |
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| US8075275B2 (en) * | 2007-09-27 | 2011-12-13 | General Electric Company | Wind turbine spars with jointed shear webs |
| CN101868619B (zh) | 2007-11-14 | 2012-09-05 | 维斯塔斯风力系统有限公司 | 风力涡轮机叶片及制造风力涡轮机叶片的方法 |
| US7740453B2 (en) | 2007-12-19 | 2010-06-22 | General Electric Company | Multi-segment wind turbine blade and method for assembling the same |
| US8171633B2 (en) | 2007-12-19 | 2012-05-08 | General Electric Company | Method for assembling a multi-segment wind turbine blade |
| DE102008028213A1 (de) * | 2008-06-06 | 2009-12-10 | Gebr. Schmid Gmbh & Co. | Verfahren zum Befestigen eines Silizium-Blocks an einem Träger dafür und entsprechende Anordnung |
| EP2334932B2 (en) * | 2008-08-25 | 2024-05-01 | Vestas Wind Systems A/S | Assembly and method of preparing an assembly |
| US7841835B2 (en) * | 2009-02-20 | 2010-11-30 | General Electric Company | Spar cap for wind turbine blades |
| DE102009046293B4 (de) * | 2009-11-02 | 2013-03-28 | Repower Systems Ag | Rotorblatt mit Entwässerungsbohrung |
| GB0920749D0 (en) * | 2009-11-26 | 2010-01-13 | Blade Dynamics Ltd | An aerodynamic fairing for a wind turbine and a method of connecting adjacent parts of such a fairing |
| US7988422B2 (en) * | 2010-06-25 | 2011-08-02 | General Electric Company | Wind turbine blades with improved bond line |
| WO2012000518A2 (en) * | 2010-07-02 | 2012-01-05 | Vestas Wind Systems A/S | Lap joint |
| DE102010062546A1 (de) * | 2010-12-07 | 2012-06-14 | Repower Systems Se | Verfahren und Vorrichtung zum Herstellen eines Holmkastens für ein Rotorblatt, Holmkasten |
| US8047799B2 (en) * | 2010-12-13 | 2011-11-01 | General Electric Company | Wind turbine blades with improved bond line and associated method |
| US8047800B2 (en) * | 2010-12-13 | 2011-11-01 | General Electric Company | Wind turbine blades with improved bond line and associated method |
| WO2012150948A1 (en) * | 2011-04-30 | 2012-11-08 | Michelin Recherche Et Technique S.A. | Methods and apparatus for joining treads |
| US8262362B2 (en) * | 2011-06-08 | 2012-09-11 | General Electric Company | Wind turbine blade shear web with spring flanges |
| BR112013033157A2 (pt) | 2011-06-30 | 2017-01-31 | Michelin & Cie | métodos e aparelhos para a instalação de um anel de banda de rodagem e uma carcaça de pneu |
| WO2013063760A1 (en) * | 2011-11-01 | 2013-05-10 | General Electric Company | Wind turbine blades with cap-assisted bond configuration and associated bonding method |
| DE102012003378B4 (de) | 2012-02-22 | 2015-01-29 | Nordex Energy Gmbh | Verfahren zum Herstellen einer Blindverklebung zwischen zwei Bauteilen eines Windenergieanlagenrotorblatts |
| GB201215004D0 (en) | 2012-08-23 | 2012-10-10 | Blade Dynamics Ltd | Wind turbine tower |
| GB201217212D0 (en) | 2012-09-26 | 2012-11-07 | Blade Dynamics Ltd | Windturbine blade |
| GB201217210D0 (en) | 2012-09-26 | 2012-11-07 | Blade Dynamics Ltd | A metod of forming a structural connection between a spar cap fairing for a wind turbine blade |
| PL2931498T3 (pl) * | 2012-12-03 | 2020-03-31 | Lm Wp Patent Holding A/S | Sposób wytwarzania łopaty turbiny wiatrowej |
| DE102014207565A1 (de) * | 2014-04-22 | 2015-10-22 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zum Verbinden von Verbindungsabschnitten von wenigstens zwei Bauteilen |
| GB2529186A (en) * | 2014-08-12 | 2016-02-17 | Vestas Wind Sys As | Improvements relating to wind turbine blade manufacture |
| US9945354B2 (en) | 2014-10-27 | 2018-04-17 | General Electric Company | System and method for controlling bonding material in a wind turbine blade |
| CN107107479B (zh) * | 2014-12-26 | 2021-12-03 | 日产自动车株式会社 | 复合材料的表面改性方法、复合材料的接合方法、复合材料、及粘接结构体 |
| US9951750B2 (en) | 2015-07-30 | 2018-04-24 | General Electric Company | Rotor blade with interior shelf for a flat plate spar cap |
| DE112017008048B4 (de) | 2017-11-01 | 2023-10-26 | W. L. Gore & Associates, Co., Ltd. | Schutzabdeckungsbaugruppe mit verbesserter z-festigkeit und elektronisches gerät |
| US12515429B2 (en) | 2019-10-23 | 2026-01-06 | Vestas Wind Systems A/S | Manufacture of wind turbine blades |
| CN112497764B (zh) * | 2020-10-26 | 2022-10-18 | 北京玻钢院复合材料有限公司 | 一种碳纤维复合材料圆管胶接的柔性连接结构及制备方法 |
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| US4169184A (en) * | 1973-05-07 | 1979-09-25 | Joseph Pufahl | Adhesive coated impregnated polyurethane foam |
| SE7412744L (da) * | 1973-10-13 | 1975-04-14 | Rueesch Ferd Ag | |
| US4737548A (en) * | 1984-07-16 | 1988-04-12 | Nippon Petrochemicals | Adhesive resins and laminate articles |
| JPH062371B2 (ja) | 1985-08-30 | 1994-01-12 | 株式会社東芝 | 超音波接合構造 |
| CA2052427A1 (en) * | 1990-12-17 | 1992-06-18 | Gary J. Jacaruso | Bonding of thermoset composite structures |
| JPH0722741A (ja) * | 1993-07-01 | 1995-01-24 | Japan Gore Tex Inc | カバーレイフィルム及びカバーレイフィルム被覆回路基板 |
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| JP3859321B2 (ja) | 1997-09-25 | 2006-12-20 | プレス工業株式会社 | 繊維強化樹脂成形体の溶着方法 |
| US6972141B1 (en) * | 1997-12-12 | 2005-12-06 | 3M Innovative Properties Company | Removable adhesive tape laminate and separable fastener |
| JP2001240820A (ja) * | 2000-02-29 | 2001-09-04 | Nitto Denko Corp | 塗膜保護シート、その製造方法及び施工方法 |
| DE20119422U1 (de) | 2001-11-30 | 2002-03-28 | A. Raymond & Cie, Grenoble | Halte- oder Befestigungselement mit einer Klebefläche zum Aufkleben auf eine Trägerfläche |
| DK175718B1 (da) | 2002-04-15 | 2005-02-07 | Ssp Technology As | Möllevinge |
| US20040023581A1 (en) * | 2002-08-05 | 2004-02-05 | Bersuch Larry R. | Z-pin closeout joint and method of assembly |
| DE10261106A1 (de) * | 2002-12-20 | 2004-07-22 | Tesa Ag | Haftklebemasse für ein- oder beiseitig haftklebrige Klebfolienstreifen und Verfahren zur Herstellung hierzu |
| WO2004076852A2 (en) * | 2003-02-28 | 2004-09-10 | Vestas Wind Systems A/S | Method of manufacturing a wind turbine blade, wind turbine blade, front cover and use of a front cover |
-
2005
- 2005-09-19 DK DK200501302A patent/DK176367B1/da not_active IP Right Cessation
-
2006
- 2006-09-14 PL PL06775990T patent/PL1926790T3/pl unknown
- 2006-09-14 US US11/992,118 patent/US8426018B2/en not_active Expired - Fee Related
- 2006-09-14 CN CN2006800344385A patent/CN101268160B/zh active Active
- 2006-09-14 DE DE200660011343 patent/DE602006011343D1/de active Active
- 2006-09-14 WO PCT/DK2006/000505 patent/WO2007048408A1/en not_active Ceased
- 2006-09-14 AT AT06775990T patent/ATE452952T1/de not_active IP Right Cessation
- 2006-09-14 BR BRPI0616225-8A patent/BRPI0616225A2/pt not_active Application Discontinuation
- 2006-09-14 EP EP20060775990 patent/EP1926790B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN101268160B (zh) | 2012-09-05 |
| WO2007048408A1 (en) | 2007-05-03 |
| BRPI0616225A2 (pt) | 2011-06-14 |
| US20090226702A1 (en) | 2009-09-10 |
| CN101268160A (zh) | 2008-09-17 |
| PL1926790T3 (pl) | 2010-06-30 |
| EP1926790B1 (en) | 2009-12-23 |
| ATE452952T1 (de) | 2010-01-15 |
| EP1926790A1 (en) | 2008-06-04 |
| US8426018B2 (en) | 2013-04-23 |
| DE602006011343D1 (de) | 2010-02-04 |
| DK200501302A (da) | 2007-03-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUP | Patent expired |
Expiry date: 20250919 |