CA1125155A - Method of fusion bonding non-elastomeric thermoplastic elements with a block structure elastomeric bonding element interposed at the bonding interface - Google Patents

Method of fusion bonding non-elastomeric thermoplastic elements with a block structure elastomeric bonding element interposed at the bonding interface

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Publication number
CA1125155A
CA1125155A CA311,039A CA311039A CA1125155A CA 1125155 A CA1125155 A CA 1125155A CA 311039 A CA311039 A CA 311039A CA 1125155 A CA1125155 A CA 1125155A
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CA
Canada
Prior art keywords
bonding
elastomeric
elements
component parts
bonding element
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
Application number
CA311,039A
Other languages
French (fr)
Inventor
Clyde P. Repik
Alfred F. Leatherman
Gordon E. Pickett
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of CA1125155A publication Critical patent/CA1125155A/en
Expired legal-status Critical Current

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    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint 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
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/36Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction
    • B29C65/3604Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the type of elements heated by induction which remain in the joint
    • B29C65/3608Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the type of elements heated by induction which remain in the joint comprising single particles, e.g. fillers or discontinuous fibre-reinforcements
    • B29C65/3612Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the type of elements heated by induction which remain in the joint comprising single particles, e.g. fillers or discontinuous fibre-reinforcements comprising fillers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
    • B29C65/36Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction
    • B29C65/3668Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the means for supplying heat to said heated elements which remain in the join, e.g. special induction coils
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General 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
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General 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
    • B29C66/71General 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General 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
    • B29C66/71General 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
    • B29C66/712General 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 the composition of one of the parts to be joined being different from the composition of the other part
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/812General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • B29C66/8122General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps characterised by the composition of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/32Layered products comprising a layer of synthetic resin comprising polyolefins
    • BPERFORMING OPERATIONS; TRANSPORTING
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    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/36Layered products comprising a layer of synthetic resin comprising polyesters
    • B32B27/365Layered products comprising a layer of synthetic resin comprising polyesters comprising polycarbonates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B32B37/1207Heat-activated adhesive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
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    • B32B38/0036Heat treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/10Interconnection of layers at least one layer having inter-reactive properties
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J5/00Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J5/00Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
    • C09J5/06Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers involving heating of the applied adhesive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • B29C2035/0822Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using IR radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
    • B29C2035/0844Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using X-ray
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/1403Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the type of electromagnetic or particle radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/1403Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the type of electromagnetic or particle radiation
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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    • B29C65/1403Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the type of electromagnetic or particle radiation
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    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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    • B29C65/1477Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation making use of an absorber or impact modifier
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
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    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/34Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
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    • B29C65/3672Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the composition of the elements heated by induction which remain in the joint
    • B29C65/3676Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the composition of the elements heated by induction which remain in the joint being metallic
    • B29C65/368Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" heated by induction characterised by the composition of the elements heated by induction which remain in the joint being metallic with a polymer coating
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    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/83General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
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    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2398/00Unspecified macromolecular compounds
    • B32B2398/20Thermoplastics

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  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)
  • Adhesives Or Adhesive Processes (AREA)

Abstract

ABSTRACT OF THE DISCLOSURE
A solid block elastomeric bonding element is interposed between the surfaces of non-elastomeric thermoplastic elements to be joined by a fusion bond.
The heat necessary for fusion bonding is obtained for optimum results by the incorporation of heat generating particles in the elastomeric bonding element. The particles are indirectly heatable by a high frequency alternating magnetic field or other suitable field for heating the fusion bonding element to a fusion tempera-ture suitable for producing bonding of the non-elastomeric elements. A copolyester block elastomer bonding element is particularly useful for bonding polycarbonate, polyvinyl chloride or polyvinylidene chloride elements to each other, and a copolymer block elastomer is particularly useful for bonding polypropylene and high density polyethylene elements to each other.

Description

112SlSS
Background of _he _nvention This invention relates to a solid thermoplastic elastomer bonding film for fusion bonding or sealing of plastic elements to themselves and to other surfaces.
Plastic elements are widely employed in various products. Although thermoplastics such as polyvinyl chloride and the like can be readily bonded adhesively or thermally to themselves, various other thermoplastics are not readily bonded to another element. For example, polycarbonates, polypropylene and the like are difficult to bond to another surface, particularly without adversely affecting the plastic material. For example, polycarbonate may be bonded to poly-carbonate or other surfaces by ultrasonic welding, spin welding and the like. Such processes, however, have generally resulted in embrittlement of the polycarbonate.
- Even with such processes, the polycarbonate cannot be bonded to certain surfaces such as glass.
Various adhesives have been suggested in which a liquid is applied between elements and the surfaces joined by drying of the liquid adhesive. Recent adhesive agents employing particular liquid thermoplastic elastomers having - a block copolymer structure and sold by Phillips Petroleum Company and Shell Oil Company are discussed in MODERN
PLASTICS ENCYCLOPEDIA, 1975-1976 edition. These liquid adhesives, however, do not provide the thermal heat seal type of bond of the present application, require a drying step and have other limitations.
Generally the thermoplastic elastomers are employed as the material for forming of various end products, coatings, and the like. Such materials have the characteristic ` - llZ~155 of ~ulcanized rubber while permitting the rapid processing advantages of the general class of thermoplastics and have generally been employed in molding and similar forming of end products. Various thermal methods of bonding thermo-plastic elements such as polyethylenes to each other em-ploying an interposed bonding agent have been described in the prior art. Methods of bonding such plastic elements to each other employing an interposed bonding layer are disclosed, for example, in U.S. Patent 3,461,014 to James and 3,574,031 to Heller. The latter patent particularly discloses carrier elements incorporating suitable energy responsive particles which are dispersed throughout the carrier element. By subjecting the assembly to a suitable field the interfaces are converted to another state to form a firm thermal bond. The above and similar prior art has provided for joinder of various plastic members. Like ! elements of polycarbonates, polypropylene and the like have been bonded to eachother where a low strength weld is acceptable by a direct thermal weld, but in many applications the melting of the material is not desirable. Also, as noted above, certain plastic materials such as polycarbonates, polypropylene and the like present particular bonding difficulties when employing an interposed bonding agent. Generally a bond of the elements to glass and the like has not been feasible.
Summary of the Present Invention The present invention is directed to a unique bonding method employing a solid thermoplastic elastomer of a block structure in the form of a thin film as an interposed bonding element between non-elastomeric surfaces and effecting a fusion bond by heating of the element to a fusion bondin~ temperature. Although, wi~hin the broadest aspect of this invention, any thermoplastic elastomer may be employed in bonding of appropriately related non-elastomeric surfaces, the inventors have found that the block-type elastomers provide unique fusion bonding, and particularly when selected from the group consisting of a copolyester block elastomer such as an elastomer derived from terephthalic acid, polytetramethylene ether glycol, and 1,4-butanediol;
and a copolymer block elastomer such as an elastomer of rigid polystyrene end blocks with a polybutadiene, a polyisoprene, a ethylene-butylene or a ethylene-propylene-rubber-type center block; or a radial copolymer, such as an elastomer of polybuta-diene center and rigid polystryrene end blocks. The copolyester elastomer provides a particularly satisfactory agent producing a bond which is vastly superior to the conventional pressure sensitive adhesive bonds, and to those obtained with other thermoplastic elastomers. Where bonding to certain material such as glass, the inventors have discovered that a primer such as phenoxy resin is advantageously applied to the glass to enhance adhesion of the copolyester elastomer element to the primer. This creates a firm bonding of polycarbonate or the like to glass. Desirable bonds can be obtained with elastomeric bonding agents by heating of the bonding elements to a state approaching a semi-liquid or molten without necessarily simultaneous melting of the elements to be bonded.
For example, polypropylene and polycarbonate elements are firmly bonded to like and to different elements by employing a thin solid film of thermoplastic elastomer interposed between such elements to be bonded and heated to melt the elastomer and form a fusion bond. -The procedure creates a bond which, with ll~S~55 an integral joining of ~he materials, is of a signifi-cantly superior strength.
The solid film may be provided with bond enhancement material such as the resin of one surface to be bonded, or the resin of the other surface, or both.
Although not essential, the thermoplastic elastomeric bonding film is preferably and uniquely heated to its melting temperature without simultaneously heating the elements completely to their melting tempera-ture. The film is, in accordance with one unique featureof the preferred embodiment, heated by a field means which generates heat within the film and thus rapidly raises the film to the bonding temperature without causing any adverse effect on the elements. The previously identified Heller patent discloses a particularly satisfactory method of heating a film employing hysteresis losses in non-conductive particles within the carrier element. Other field phenomena may, of course, be employed. For example, dielectric heating may be employed if the thermoplastic elastomer has a sufficiently high dielectric loss characteristic or suitable high loss particles may be placed within the carrier film such as broadly referenced in U.S. Patent 3,574,031. Radiant energy may also be employed by introducing carbon black or the like into the thermoplastic elastomer carrier element.
In the more particular aspects of this invention, applicants have discovered that the elastomeric bonding agent produces highly reliable bonding of elements of non-elastomeric thermoplastic, such as polycarbonate, polypro-pylene and polyvinyl chloride to themselves and one another, .. . . .

~1251S~
as well as the bonding o~ such elements to other dissimilar nonelastomeric thermoplastic elements and even nonplastic elements. Thus, polycarbonate elements and polyvinyl chloride elements can be joined to themselves with a high strength bond such as 125 pounds per inch width of 180 peel strength em-ploying a thin bonding element of copolyester elastomer such as sold by DuPont under the trademark Hytrel #4055 and 4056. Such a bonding element is also highly satisfactory for bonding of polycarbonate elements to polyvinyl chloride and either of such elements to polyvinylidene chloride (PVDC).
The block copolymer elastomeric element sold by Shell Develop-ment Company under the trademark Kraton G provides a highly satisfactory agent for bonding of polypropylene to high density polyethylene using just a single layer of material.
A bond strength on the order of 50 pounds per inch of width in 180~ peel strength is readily obtained. Further, Kraton 3000 has been found to bond high impact polystyrene elements to each other with a lap joint strength on the order of 500 p,i. A "Solprene" elastomer of Phillips Petroleum Company and which is a radial block copolymer of polybutadiene center blocks and polystrene end blocks bonds ABS (acrylonitrile butadiene-styrene) elements to each other with a lap joint strength of 240 psi.
The precise mechanics involved are not readily apparent nor does the literature suggest any reason to believe the block elastomers are satisfactory as interposed fusion bonding elements for fusion bonding non-elastomeric elements. However, such an elastomeric bonding element does bond non-elastomeric elements which have not previously been satisfactorily joined by a fusion bond with any signi-- ficant strength levels, such as produced by the present invention.

, . ,, ~ ~

112S~SS

The block elasto~eric materials woulcl appear to have certain characteristics which are related to producing a high strength or superior bond. In particular, the block elastomeric resin has a high degree of chemical stability.
In preparing an elastomeric bonding element with the dispersed heat-generating particles, the resin is melted and the heat-generating particles introduced and the mixture is then finally hot-pressed to form a ilm or sheet. The hot material could, of course, be extruded or calendered to form the desired sheet. While hot, and partly as accentuated by the heat generating particles, oxidation of the resin normally is created.
The inventors have noted that, in fact, the elastomeric resin does not significantly oxidize. Addition of a chemical oxidation retarder such as employed in Hytrel 4056 improves the bond characteristic and would appear to support the above analysis. This characteristic of the elastomers combined with the ability to use a fusion bonding temperature generally less than the customary fusion bonding temperature of the non-elastomeric element or elements, appears to be a significant factor in the optimum structure and me~hods of the invention, and, particularly, contributing to the unique and unexpected bond strengths obtained by the combination of the elastomeric bonding element and the non-elastomeric elements to be joined.
Brief Description of the Drawing The drawing furnished herewith illustrates a preferred construction of the present invention in which the above advantages and features are clearly disclosed as ~i 25i ~ S

well as others which will be readily understood from the following description.
In the drawing:
Fig. 1 is a partial schematic view showing an initial step in the process of the present invention for obtaining thermal bonding of a pair of non-elastomeric thermoplastic elements employing an interposed elastomeric bonding element having heat-generating particles as heat sources;
Fig. 2 shows a subsequent step in the bondîng process of Fig. l;
Fig. 3 shows an induction heating unit suitable for the bonding process of the present invention;
Fig. 4 shows the finished bonded assembly;
Fig. 5 shows a test fixture for testing the peel strength of the bonds; and Fig. 6 is an illustration of a prior art type bond.
Description of the Preferred Embodiment Referring to Fig. 1, the process of the present invention is shown in bonding a first thermoplastic non-elastomeric layer or element 1 to a second thermoplastic non-elastomeric layer or element 2 by a thermal bond at overlapping joinder interface portions 3 and 4. A bonding element 5 of an elastomeric material is interposed between the elements 1 and 2 at the interface portions 3 and 4.
Layers 1 and 2 may typically be formed of any one of various plastics including those which have not been successfully joined by thermal bonding or only with weak bonds, such as typical polycarbonates, polypropylene and high density poly-ethylene.

~12~1SS
The term "elastomeric" element is employed herein to define that class of thermoplastic material possessing the properties of high resiliency or memory and containing co-polymers and terpolymers.
In a particular unique teaching of this invention, the block-type elastomers are employed as a unique interposed bonding element for fusion bonding of non-elastomeric elements.
Such materials have a rubber-like characteristic and have been found by the present inventors to produce highly effective fusion bonding of non-elastomeric thermoplastic elements. A
discussion of elastomers as to structure, application and characteristic is set forth in the 1976-1977 edition of MODERN
PLASTICS ENCYCLOPEDIA (Pages 103-108), as well as in the early 1975-1976 edition (Pages 94-96). As disclosed therein, these materials have been widely employed and are well-known in the art of molded products, conventional glue and/or adhesive sealants. Further, such materials generally are chemically stable and are not subject to significant oxidation when melted.
Typical elastomers which have been employed in the present in-vention include a copolyester block elastomer derived from terephthalic acid, polytetramethylene ether glycol, and 1, 4-butanediol manufactured and sold by E. I. duPont de Nemours &
Company, Inc. under the trademark Hytrel; a copolymer radial block elastomer of polystyrene and polybutadiene sold by~Phillips Petroleum Company under the trademark Solprene Plastomers, a block copolymer of rigid polystyrene end blocks and center blocks of polybutadiene, polyisoprene,ethylene-butylene or ' -ethylene-propylene sold by Shell Development Company under the trademark Kraton, and particularly the last two center-block types sold under the trademark Kraton G.

The elastomeric ma-terial selected for bonding element 5 is uniquely related to the material of elements 1 and 2 for optimum results, as set forth hereinafter in the discussion of the several elastomeric materials described in the latter article.
In the illustrated embodiment of Fig. 1, heat source particles 6 are incorporated in the bonding element 5 and are preferably particles which are responsive to a suitable high frequency magnetic energy field to form individual heat sources for rapidly heating of the surfaces to a bonding temperature. The particles may be incorporated into element 5 in any suitable manner such as by the selective insertion and mixing during extrusion of such an element, mixing and rolling or pressing a hot mix of the resin and particles, heating of the plastic element to soften the interface and pressing the particles into the plastic or the like.
The heat generating particles 6 are selected to form individual heat sources in the presence of suitable energy field. For example, different particles may be activated by suitable high frequency, alternating magnetic and electrical fields. The separate susceptor particles may, of course, be responsive to other fields such as a radiant field, including infrared radiation in which case the susceptor particles may comprise carbon black.
When a high frequency magnetic field is used as the energy source, the susceptor particles 6 preferably consist of fine particles of a ferromagnetic, nonconductive, metallic oxideselected from gamma Fe203, Fe304 and mixtures thereof which are responsive to the application of the high frequency alternating magnetic field as more fully dis-closed in the previously identified Heller Paten~ 3,574,031.
Gamma Fe203 has been found particularly suitable for use in the method of the present invention. The particles 6 may be incorporated in quantities of less than 2% to more than 50% by weight respective to the thermoplastic material, quantities of 10% to 30% by weight being typical.
The unique ability of the aforesaid oxides resides in their ability to retain their heat generating charac-teristics even when reduced to submicron sizes. Particles sized as small as .01 microns may be used, although typic-ally the particles may range up to 20 microns and in some cases may even be larger.
The use of the more minute particles facili-tates incorporation into a thin bonding element with the advantages of the rapid susceptor heating of the bonding - element to the melting temperature without simultaneously complete melting of the base plastic element~ l and 2. The dispersion of the susceptor in the thermoplastic material as a result of the bonding does not appreciably alter the chemical or physical properties of the thermoplastic material.
Layers 1 and 2 with bonding element 5 interposed therebetween are located in direct abuttment as shown in Fig. 2 and then exposed to the appropriate energy field.
In the present embodiment, the particulate susceptor par-ticles 6 in element S are activated by an alternating magnetic field which may be established by a coil 7, in accordance with known technology, such as diagrammatically shown in Fig. 3. The coil 7 is energized by the current of the high frequency alternating current power source 8.

~2~15S

lligh frequency power source 8 may typically operate in a frequency range of .4 to S000 megahertz with a frequency range of 2 to 30 megahertz being typical for the conven-tional hairpin coil schematically shown in Fig. 3. A
pair of opposed flat pieces of copper plates 9 and 10 are soldered or otherwise firmly affixed to the inner faces or side of the coil 7. The plates 9 and 10 in one unit were approximately one quarter (1/4) inch wide and several inches long. Force is applied across the tubing at the copper plates 9 and 10 in any suitable manner, as diagrammatically shown by the force arrows 11 and 12, to permit collapsing of the coil and plates 9 and 10 toward each other for applying pressure across elements located therebetween. By releasing of the clamping force 11 - 12, the assembled or stacked elements can be moved through the coil 7 to make successive seals or joinders.
The activated particulate susceptor particles 6 of element 5 increase in temperature and define dispersed heat sources along the bonding interface and rapidly raise the surface of only element 5 to the melting temperature with the elements 1 and 2 softened by conduction. Although a time on the order of a fraction of a second may be adequate with appropriate particle loading, power levels, and the like, longer heating times work equally well and may be achieved with less input power to coil 7.
As soon as the bonding element has reached the melting temperature, the application of the alternating magnetic field is preferably removed as by deenergizing high frequency power source 8. Thus, generally a good thermal bond to elements 1 and 2 requires that the element 5 5~SS
is converted to a softened or viscous state. However~ the element 5 must be retained between the surfaces or elements to form the bond.
In the procedure followed in each of the particular examples discussed herein, the bonding element 5 was formed by dispersing substantially 20% by weight of magnetic iron oxide (Fe203) into the selected elastomeric resin and then hot press-ing the particle-bearing resin to a thickness of substantially 8 to 10 mils. The substrate elements 1 and 2 were flat pieces of the identified plastic about 1 inch wide by 4 to 5 inches long. A 1 inch square bonding element 5 was located between the aligned ends of elements 1 and 2, as shown in Figs. 1 and
2, and the assembled elements were pinched within the coil plates 9 and 10. After heating to bond, the bonded assembly, as shown in Fig. 4, is removed and placed, as shown in Fig. 5, in a tensile machine 13 to determine the bond strength. In ; particular, the free ends 14 and 15 of elements 1 and 2 were bent open and placed in the jaws 16 of the tensile machine 13.
Actuation thereof causes the jaws to spread and elements 1 and 2 to be pulled to separation, with the force required indicated by the tensile machine.
More particularly, non-elastomeric elements 1 and 2 formed of polycarbonate, polyvinyl chloride or PVDC, are bonded with a high strength joint by employing for element 5 a thermo-plastic copolyester elastomer derived from terephthalic acid,polytetramethylene ether glycol and 1, 4-butanediol, such as made and sold by the E.I. duPont de Nemours & Company, Inc., Wilmington, Del. 19898, under the trademark Hytrel.
The copolyester elastomer is available in pellet and powder form and can be readily molded and formed. The material can be readily formed into a thin, solid bonding element 5.

1~ 2~ ~ 5 In order to obtain optimum high strength joints when bonding polycarbonates, the copolyester elastomer element 5 was rapidly heated to melt and change the elemen-t to a highly viscous state.
Typical examples of bonding with a co-polyester element, without detectable melting of the elements being bonded, are as follows:
Table I.- Peel Bond Results Elements 1 and Bonding Agent Heat Peel Bond 2, thickness Element 5 Cycle Strength, _ Time 1" wide 1/16" PC to PC Hytrel 4055 1 sec 125 lbs 1/8" PC to PC Hytrel 4055 1 sec 162 lbs 1/16" PC to 0.107" PVC Hytrel 4055 1 sec 138 lbs 0.107" PVC to PVC Hytrel 4055 1 sec 155 lbs The elements were clamped in place using air cylinders to apply pressure across the interface bonding portion and the R-F generator operated in the 2 - 7 MEz range. The generator was capable of providing current of several hundred amperes. The resulting bond strengths are unexpectedly high. For example, pressure-sensitive adhesive bonds in peel are generally on the order of 8 pounds per inch width while with the similar polyethylene layered bonding, such as suggested in U.S. Patent 3,574,031, 90 pounds is considered a high quality bGnd.
Further, the direct bonding of polycarbonate materials has, heretofore, presented significant problems.
Thus, conventional spin welding, ultrasonic welding and the like often creates embrittlement of the elements. When a particulate heat source material is added to poly-carbonate to form a bonding element, which is then directly thermally joined, as shown in Fig. 3, a stress can occur under test at the edge of the bond area, as at 17 of Fig. 6, resulting in failure. The failure occurs at the edge of the bond and has an appearance as if a cut had been made in the element.
The bonding element does not appear in the area. Sur-prisingly, with the copolyester elastomer bonding element 5, such a failure has not appeared; even though the bond-ing temperature approaches the melting point of the poly-carbonate.
Similar tests employing a thermoplastic rubber such as the TPR material of Uniroyal Inc., which is an olefin rather than a molecular block type elastomer was also used to bond ! 1/16" and 1/8" thick polypropylene to itself. A peel bond strength of 37 pounds resulted. This is a very low strength compared to those set forth in Table I. ~owever, the polypropylene was readily and directly bonded whereas such material is otherwise, as with adhesives, generally bonded only with substantial difficulty. In this aspect, poly-propylene has also been bonded to itself using a mixture of TPR elastomer and polypropylene. The results showed an improvement over the straight TPR elastomeric element 5 such as in peel strength.
The inventors have E~lrther discovered that polypropylene and high density polyethylene can be joined with a high strength fusion bond using a block copolymer elastomer in which rigid polystyrene end blocks are com-bined with ethylene-butylene, or ethylene-propylene-rubber-13L25~55 type center blocks. Such material is available from Shell Development Company in solid form under the trademark Kraton G for processing into a bonding element 5.
Thus, a Kraton G resin was melted on a hot-roll mill and, while being milled, 20% by weight of susceptor particles Fe203 were dispersed into the resin.
The mixture was removed and hot-pressed into sheet form of 8 - 10 mils thickness. The Hytrel bonding elements used - 10 in Table I were similarly formed. Various Kraton G grades were employed with Kraton G#2705 producing somewhat better ~onds than #7827. Typical examples of bonding with Kraton G as bonding element 5 are as follows:
Table II. - Peel Bond Results _ Elements 1 and Bonding Agent Heat Peel Bond 2, thickness Element 5 Cycle Strength, Time 1" wide _ .
1/16" PP to PP Kraton G 2705 1 sec 43 lbs 24-mil HDPE
to HDPE Kraton G 2705 1.5 sec 54 lbs 20-mil HDPE
20 to HDPE Kraton G 2705 1.5 sec 42 lbs 20-mil HDPE
to 1/16" PP Kraton G 2705 1.5 se~c 44 lbs*
20-mil HDPE -HDPE Kraton G 7827 2.0 sec 17 lbs * substrate broke at bond A slightly better bond is again obtained with the dissimilar materials. However, this might be due to various practical reasons found in the normal functioning of the bonding and testing procedures and operations.
The results in general are, however, highly significant in view of the great difficulty which such non-elastomeric thermoplastic materials have presented in past bonding practice. Although the bond strength is not as great as that found in heat sealing of more conventional thermo-plastics such as polyethylene, a 50 pound bond is generally sufficient to prevent manual hand separation. Further, with the present invention employing the elastomer of a block-type structure, the bond can be repeated employing a conventional pressure bonding apparatus as heretofore discussed. An olefin elastomer TPR 1900 was also employed to bond two HDPE elements but only produced strength of 13 lbs. in peel.
In addition to the above embodiments, Kraton 3000 was employed to bond a pair of overlapping high im-pact polystyrene strips. The strips were approximately 1 inch wide by 1/16 inch thick. A one inch square, -~
inch Kraton 3000 bonding element loaded with 30% by weight of ferric iron oxide (Fe203) was interposed between the overlapping ends of the strips and the assembly heated to the fusion temperature. The bond was tested by pulling in the plane of the strips and was found to have a lap strength of 500 psi. A Solprene elastomer bonding element was similarly applied to bond a pair of ABS
strips and produced a lap strength of 240 psi.
Although described using a high frequency magnetic field, other heating means might be employed within the broadest aspect of this invention. Other particles might be employed which respond by induction, dielectrically or even radiation. Thus, metal conducting particles might be employed with induced eddy currents creating the heat within the bonding element 5.

... . .... . . ..

ss Particles of polymeric type, useful as di-electric heating particles, wouLd include the halogenated polymers such as the polymers and copolymers of vinyl chloride, vinyl fluoride, vinylidene chloride, and vinyli-dene fluoride and the polycarbonates, polyurethanes,polyacetals, and cellulose derivatives amongst others.
The various elastomers such as Hytrel elastomer could also be employed as a bonding element without the necessity of added particles, by employing a suitable dielectric heater or microwave source of sufficiently high frequency, such as the order of 41 2~ . Further, Hytrel elastomers show a higher dielectric loss than, for example, poly-carbonate and thus the necessary melting temperature could be generated in the Hytrel without melting the polycarbonate element to be bonded.
Radiant energy such as infrared energy may also be used in practicing the invention, with or without carbon black particles utilized as the susceptor particles 5 to concentrate heat within the bonding element. An electric lamp and a reflector to focus the energy onto the ele-ment 5 maysupply the source of energy for heating the element-which quickly melts. In radiant heating at least one of the elements 1 or 2 must necessarily be able to transmit a substantial portion of the infrared radiation in order for it to reach the element S. In addition to energy sources such as infrared and lasers, it is to be understood that other forms of radiant energy such as X-ray, ion beams, electronic beams, ultrasonic beams, and nuclear radiation, amongst others, may be used for generating the heat in suitable susceptors selected as being responsive thereto.

. .

~2~155 A further signi~icant bonding result has been obtained employing a primer between the elastomer element and a glass or the like. Thus, by applying of a phenoxy adhesive as a primer, the copolyester elastomer element bonds to glass. Thus by employing multilayers, vinyls, polycarbonates and the like can be firmly and directly bonded to glass.
Further, as the prior art has provided various similar material bonds, the elastomeric bonding element may, of course, include a minor amount of the non-elastomeric materials of the parent element being bonded. However, the elastomer remains the basic bonding element. For example, if a polyethylene and polypropylene are to be bonded, a 50-50 mixture of such materials in a - 15 bonding element does not produce a significant or satis-factory bond. Thus, the additive should constitute a minor part of the elastomeric bonding element.
Further, within the broadest features of this in-vention, the heat might be generated within the elements being 20 joined and transmitted to the bonding element. The heat transferred would be sufficient to raise the bonding element to the fusion bonding temperature.
The present invention thus provides a unique method for bonding of plastic elements including such elements which 25 have been previously bonded with difficulty.

Claims (8)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A thermal fusion bonding method comprising the steps of assemblying thermoplastic non-elastomeric resinous component parts having a non-block-molecular-structure in stacked relationship to be joined over localized bonding interface surfaces with an interposed solid preformed ther-moplastic and elastomeric resinous bonding element having a block-molecular-structure and located extending at least over the extent of the bonding interface, applying pressure over said surfaces to hold said element in firm contact with the interface surfaces, said bonding element having particu-late material dispersed therein and generating induced heat in response to an energy magnetic field applied thereto, mounting said assembly in an air atmosphere at a temperature substantially below the softening temperature of the com-ponent parts and the bonding element, and during a period of applying said pressure applying said energy field to said bonding element to create heat within said particulate material and thereby said bonding element, and wherein said particu-late material in said element serves as the only source of heat at the bonding interface surfaces of said component parts, applying said field for a time period on the order of up to 10 seconds and thereby raising the bonding element to its melting temperature and maintaining the component parts below their melting temperature and thermally bonding of the bonding element to the bonding interface surfaces of said component parts without significant physical change in the component parts, said heat in said element being insuffi-cient to raise the temperature of said component parts sub-stantially above the environmental temperature and thereby to preclude any significant change in said preformed component parts while achieving a thermal bond strength between said component parts measuring in excess of 40 pounds per linear inch when tested in 180-degree peel configuration.
2. The method of claim 1 wherein said particulate material is electrically nonconductive and has a high magnetic coercivity.
3. The bonding method of claim 1 wherein said particulate material is a gamma ferric oxide ferromagnetic powder, and said magnetic field has a high magnetic field intensity at the bonding element and a frequency less than 10 MHz.
4. The method of claim 1 including selecting the energy activatable particulate material from the group consisting of Fe2O3 and Fe3O4, and said radio frequency magnetic field has a frequency less than 10 MHz.
5. The fusion bonding method of claim 1 wherein at least one of the component parts is formed of polypropy-lene and the other part is sele-ted from polygropylene and a high density polyethylene member, said solid elastomeric bonding element being block copolymer of rigid polystyrene end blocks and a saturated olefin rubber midblock of ethylene-butylene of ethylene-propylene.
6. The method of claim 5 wherein said heating step is created on the order of two seconds.
7. The fusion bonding method of claim 1 wherein at least one of said component parts is a polycarbonate and the other is selected from the group consisting of poly-carbonate, polyvinyl chloride and polyvinylidene chloride over an interface bonding portion, and said solid elasto-meric bonding element is a block copolyester of terephtahalic acid, polytetramethylene ether glycol, and 1,4-butanediol.
8. The method of claim 7 wherein said heating step is created on the order of two seconds.
CA311,039A 1977-09-13 1978-09-11 Method of fusion bonding non-elastomeric thermoplastic elements with a block structure elastomeric bonding element interposed at the bonding interface Expired CA1125155A (en)

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US6911262B2 (en) 2000-11-10 2005-06-28 Gentex Corporation Visibly transparent dyes for through-transmission laser welding
US7276136B2 (en) 2000-11-10 2007-10-02 Gentex Corporation Visibly transparent dyes for through-transmission laser welding
US6770158B2 (en) 2002-01-15 2004-08-03 Gentex Corporation Quality management system for pre-processed workpiece
US7201963B2 (en) 2002-01-15 2007-04-10 Gentex Corporation Pre-processed workpiece having a surface deposition of absorber dye rendering the workpiece weld-enabled
US7344774B2 (en) 2002-01-15 2008-03-18 Gentex Corporation Pre-processed workpiece having a surface deposition of absorber dye rendering the workpiece weld-enabled

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GB2061815B (en) 1982-09-22
GB2004497A (en) 1979-04-04
IT1106900B (en) 1985-11-18
IT7851036A0 (en) 1978-09-11
FR2433564B1 (en) 1982-04-30
JPS54141880A (en) 1979-11-05
GB2061814B (en) 1982-09-15
AU555459B2 (en) 1986-09-25
FR2402690A1 (en) 1979-04-06
GB2061814A (en) 1981-05-20
AU2308384A (en) 1984-05-03
JPS5840488B2 (en) 1983-09-06
GB2004497B (en) 1982-09-22
FR2433564A1 (en) 1980-03-14
GB2061815A (en) 1981-05-20
DE2839640A1 (en) 1979-03-22
DE2839640C2 (en) 1991-11-14
FR2402690B1 (en) 1983-10-07
AU3951678A (en) 1980-03-13

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