JPH06503522A - Process for the preparation of thermoplastic honeycomb sandwich structures - Google Patents
Process for the preparation of thermoplastic honeycomb sandwich structuresInfo
- Publication number
- JPH06503522A JPH06503522A JP4502833A JP50283391A JPH06503522A JP H06503522 A JPH06503522 A JP H06503522A JP 4502833 A JP4502833 A JP 4502833A JP 50283391 A JP50283391 A JP 50283391A JP H06503522 A JPH06503522 A JP H06503522A
- Authority
- JP
- Japan
- Prior art keywords
- honeycomb
- thermoplastic
- skin
- film
- preparation
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining 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
- B29C65/1429—Joining 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 way of heating the interface
- B29C65/1432—Joining 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 way of heating the interface direct heating of the surfaces to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining 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
- B29C65/1429—Joining 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 way of heating the interface
- B29C65/1464—Joining 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 way of heating the interface making use of several radiators
- B29C65/1467—Joining 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 way of heating the interface making use of several radiators at the same time, i.e. simultaneous welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/481—Non-reactive adhesives, e.g. physically hardening adhesives
- B29C65/4815—Hot melt adhesives, e.g. thermoplastic adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
- B29C65/5057—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/03—After-treatments in the joint area
- B29C66/034—Thermal after-treatments
- B29C66/0342—Cooling, e.g. transporting through welding and cooling zone
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/438—Joining sheets for making hollow-walled, channelled structures or multi-tubular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—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
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/534—Joining single elements to open ends of tubular or hollow articles or to the ends of bars
- B29C66/5346—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat
-
- 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
- B29C66/725—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 hollow-walled or honeycombs
- B29C66/7254—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 hollow-walled or honeycombs honeycomb structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—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
- B29C66/834—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools moving with the parts to be joined
- B29C66/8341—Roller, cylinder or drum types; Band or belt types; Ball types
- B29C66/83411—Roller, cylinder or drum types
- B29C66/83413—Roller, cylinder or drum types cooperating rollers, cylinders or drums
-
- 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
- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
- B29C66/914—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux
- B29C66/9141—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature
- B29C66/91411—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature of the parts to be joined, e.g. the joining process taking the temperature of the parts to be joined into account
-
- 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
- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
- B29C66/914—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux
- B29C66/9161—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the heat or the thermal flux, i.e. the heat flux
- B29C66/91641—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the heat or the thermal flux, i.e. the heat flux the heat or the thermal flux being non-constant over time
- B29C66/91643—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the heat or the thermal flux, i.e. the heat flux the heat or the thermal flux being non-constant over time following a heat-time profile
- B29C66/91645—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the heat or the thermal flux, i.e. the heat flux the heat or the thermal flux being non-constant over time following a heat-time profile by steps
-
- 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
- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
- B29C66/919—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
- B29C66/9192—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams
- B29C66/91921—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature
- B29C66/91931—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature in explicit relation to the fusion temperature or melting point of the material of one of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/04—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the partial melting of at least one layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/08—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the cooling method
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/0036—Heat treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
- B29C35/0805—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
- B29C2035/0822—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using IR radiation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/10—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using hot gases (e.g. combustion gases) or flames coming in contact with at least one of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining 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
- B29C65/1403—Joining 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
- B29C65/1412—Infrared [IR] radiation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- 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
- B29C65/5092—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 tape handling mechanisms, e.g. using vacuum
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—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
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/534—Joining single elements to open ends of tubular or hollow articles or to the ends of bars
- B29C66/5346—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat
- B29C66/53461—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat joining substantially flat covers and/or substantially flat bottoms to open ends of container bodies
- B29C66/53462—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat joining substantially flat covers and/or substantially flat bottoms to open ends of container bodies joining substantially flat covers and substantially flat bottoms to open ends of container bodies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
- B29C66/73921—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7394—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoset
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B2037/0092—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding in which absence of adhesives is explicitly presented as an advantage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/02—Cellular or porous
- B32B2305/024—Honeycomb
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2310/00—Treatment by energy or chemical effects
- B32B2310/04—Treatment by energy or chemical effects using liquids, gas or steam
- B32B2310/0409—Treatment by energy or chemical effects using liquids, gas or steam using liquids
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Health & Medical Sciences (AREA)
- Electromagnetism (AREA)
- Toxicology (AREA)
- High Energy & Nuclear Physics (AREA)
- Plasma & Fusion (AREA)
- Laminated Bodies (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるため要約のデータは記録されません。 (57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】 熱可塑性ハニカムサンドイッチ構造の準備のためのプロセス発明の背景 発明の分野 本発明は、面ノート又はスキンが迅速かつ費用効果のある方法で繊維強化又は非 強化熱可塑性ハニカムに適用される、ハニカムサンドイッチ構造の準備に関する 。[Detailed description of the invention] Process for the preparation of thermoplastic honeycomb sandwich structures Background of the invention field of invention The present invention allows surface notes or skins to be quickly and cost-effectively fiber-reinforced or non-fiber-reinforced. Concerning the preparation of honeycomb sandwich structures as applied to reinforced thermoplastic honeycombs .
関連技術の説明 ハニカムパネルは、例外的に軽量の剛性平面又は適度な曲線構造が必要とされる 、輸送及び航空宇宙産業において使用される。過去において、多(のハニカムは 、繊維強化材を熱硬化性樹脂で含浸させ、手でハニカムをレイアップすることに より準備された。−立方フィードのハニカムは、しばしば、準備と硬化のために 24時間以上を費やした。最近、繊維強化及び非強化の熱可塑性ハニカムがまた 、使用されているが、今まで、その生産量は、時間及び労働集約的であった。同 時係属出願第071531.184号において、熱可塑性ハニカムの生産のため の連続方法が開示され、これらの構造要素の使用を増大させる。Description of related technology Honeycomb panels require an exceptionally lightweight rigid planar or moderately curved structure. , used in the transportation and aerospace industries. In the past, honeycombs of , the fiber reinforcement was impregnated with thermosetting resin and the honeycomb was laid up by hand. More prepared. − Cubic feed honeycombs are often It took over 24 hours. Recently, fiber-reinforced and non-reinforced thermoplastic honeycombs have also been , has been used, but until now, its production has been time and labor intensive. same In currently pending application no. 071531.184, for the production of thermoplastic honeycombs. A continuous method of increasing the use of these structural elements is disclosed.
いずれの方法によってもハニカムの生産に続いて、仕上げコアが、要求厚の平面 セグメントに切り込み又はスリットを入れられ、そして熱硬化する熱硬化性フィ ルム接着剤、例えば、ビスマレイミド又はエポキシ樹脂が、一般に繊維強化プリ プレグ又はラミネートであるスキンをコアに結合するたメ化使用される。面シー トとフィルム接着剤を有するコア組立体は、圧力か組立体に加えられる間加熱さ れる。一般に数時間の硬化時間に続いて、ハニカムサンドイッチパネルは、意図 した応用のために適切なサイズに切断される。Following the production of honeycomb by either method, a finished core is produced with a flat surface of the required thickness. A thermosetting film that is cut or slit into segments and then heat cured. Luminous adhesives, such as bismaleimide or epoxy resins, are commonly used in fiber-reinforced plastics. A laminate is used to bond the skin, which may be a preg or laminate, to the core. Menshi The core assembly with adhesive and film adhesive is heated while pressure is applied to the assembly. It will be done. Following a curing time, typically several hours, honeycomb sandwich panels are cured as intended. cut to the appropriate size for the application.
先行技術のプロセスによって実施された如く、ハニカムを面シートに結合するプ ロセスは、時間を消費し、比較的高価なフィルム接着剤を使用し、その接着力、 粘性と硬化サイクルは、しばしば、各特定応用に対して調整されなければならな い。The process of bonding the honeycomb to the face sheet as performed by prior art processes The process uses time-consuming and relatively expensive film adhesives, and their adhesive strength Viscosity and curing cycles often must be adjusted for each specific application. stomach.
発明の目的 熱可塑性ハニカムコアは、面シートに以前接着された、又は好ましくは、分離要 素として供給された熱可塑性フィルムの使用により、面シートに結合されること が、不測にも発見された。このプロセスにより、比較的安価かつ容易に利用可能 な熱可塑性フィルムが使用され、面ンートの結合のためのサイクル時間は、数時 間からほんの数秒に縮小される。Purpose of invention The thermoplastic honeycomb core may have been previously bonded to the face sheet or, preferably, separated by a separation element. be bonded to the face sheet by the use of a thermoplastic film supplied as a blank; was discovered unexpectedly. This process makes it relatively cheap and easy to use. A thermoplastic film is used and the cycle time for bonding is several hours. reduced to just a few seconds.
図面の簡単な説明 第1図は、熱可塑性結合フィルムを接着した面シートに結合されるハニカムコア の側面図である。Brief description of the drawing Figure 1 shows a honeycomb core bonded to a face sheet with a thermoplastic bonding film bonded to it. FIG.
第2図は、分離熱可塑性結合フィルムを使用する、面シートに結合されるハニカ ムコアの側面図である。Figure 2 shows a honeycomb bonded to a face sheet using a separate thermoplastic bonding film. It is a side view of Mukoa.
第3図は、放射熱バンクとプラテンを使用するプロセスの側面図である。FIG. 3 is a side view of a process using a radiant heat bank and platen.
第4図は、第3図によって示されたプロセスの頂面図である。FIG. 4 is a top view of the process illustrated by FIG.
好ましい実施態様の説明 本発明のプロセスにおいて使用される熱可塑性ハニカムは、30重量パーセント を重えない、少量の熱硬化性樹脂を含む樹脂系から準備されたものを含む、事実 上、任意の形式である。使用される熱可塑性物質としては、限定的ではないが、 ポリエチレン、ポリプロピレン、ポリオキシメチレン、ポリアリレンエーテル、 ポリエーテルケトン、ポリスルホン、ポリエーテルスルホン、ポリアミド、ポリ アラミド、ポリベンゾイミダゾール、ポリイミド、熱可塑性ポリウレタン、等が ある。熱硬化性樹脂の小部分としては、例えば、ビスマレイミド樹脂、エポキシ 樹脂、ンアナート樹脂、イソシアナート樹脂、熱硬化性ポリイミド、等が挙げら れる。Description of preferred embodiments The thermoplastic honeycomb used in the process of the invention is 30% by weight fact, including those prepared from resin systems containing small amounts of thermosetting resins, without overlapping above, in any format. Thermoplastic materials used include, but are not limited to: polyethylene, polypropylene, polyoxymethylene, polyarylene ether, polyetherketone, polysulfone, polyethersulfone, polyamide, poly Aramid, polybenzimidazole, polyimide, thermoplastic polyurethane, etc. be. As a small part of thermosetting resin, for example, bismaleimide resin, epoxy resin, ananate resin, isocyanate resin, thermosetting polyimide, etc. It will be done.
熱可塑性ハニカムは、繊維強化材で強化される。強化材は、スパンボンデツド繊 維、保全性を設けるために随意的に縫われた及び/又は大きさを決められたラン ダム連続又はチョップ繊維、織物、一方向テープ又はこれらの組み合わせの形式 である。使用繊維としては、ガラス、石英、炭素(炭素/黒鉛)、窒化ホウ素、 炭化ケイ素、セラミックス、等の無機繊維、又は前述の熱可塑性物質から準備さ れたものの如く有機合成繊維がある。Thermoplastic honeycombs are reinforced with fiber reinforcement. The reinforcement material is spunbonded fiber. optionally sewn and/or sized runs to provide security and integrity. Forms of dam continuous or chopped fibers, woven fabrics, unidirectional tapes or combinations thereof It is. The fibers used include glass, quartz, carbon (carbon/graphite), boron nitride, prepared from inorganic fibers such as silicon carbide, ceramics, or the aforementioned thermoplastics. There are organic synthetic fibers such as
面シートは、金属、繊維強化熱硬化性樹脂又は熱可塑性物質、又は非強化熱可塑 性物質である。面シートとハニカムコアは、熱可塑性結合フィルムに粘着するこ とができる。好ましくは、ハニカム、面シートと結合フィルムにおいて使用され る熱可塑性物質は同一である。The face sheet can be made of metal, fiber-reinforced thermosetting resin or thermoplastic, or unreinforced thermoplastic. It is a sexual substance. The face sheet and honeycomb core are bonded to a thermoplastic bonding film. I can do it. Preferably used in honeycomb, face sheet and bonding film The thermoplastics used are the same.
熱可塑性フィルムは、接合される材料と融和性でなければならない。Thermoplastic films must be compatible with the materials being joined.
好ましくは、前述の如く、熱可塑性フィルムは、ハニカム材料と同一熱可塑性物 質である。融和性は、ハニカムからスキンを除去するために必要な力を決定する ことにより評定される。フィルムの厚さは、広く変化するが、好まじ綱は、約0 .05mm〜1.Qmm、さらに好ましくは、接されるか、又は面シートと非融 和性であるならば、接着される。さらに、スキンに融接又は接着される分離フィ ルムの代わりに、ハニカムに融着することができる十分な熱可塑性物質を含むス キンを使用することは、発明の精神内にある。そのようなスキンはまた、一体フ イルム/スキンユニットとして考えられる。本発明の目的は、スキンをコアに結 合する時完全に熱硬化性樹脂の使用を回避するが、約10重量パーセントよりも 少ない、限定量の熱硬化性樹脂を含む、熱可塑性結合フィルムを使用することは 、なお発明の精神内にある。そのようなフィルムは、完全熱可塑性材料と同様に 作用すると期待される。Preferably, as mentioned above, the thermoplastic film is the same thermoplastic as the honeycomb material. It is quality. Compatibility determines the force required to remove the skin from the honeycomb It is evaluated by The thickness of the film varies widely, but the preferred thickness is about 0 .. 05mm~1. Qmm, more preferably in contact with or non-fused with the face sheet. If it is compatible, it will be glued. Furthermore, a separate filament that is fusion welded or glued to the skin Instead of a lume, a strip containing enough thermoplastic material can be fused to the honeycomb. It is within the spirit of the invention to use Kin. Such skins also It can be considered as an illum/skin unit. The object of the present invention is to connect the skin to the core. Avoid the use of thermosets completely when combining, but less than about 10 weight percent The use of thermoplastic bonding films containing small, limited amounts of thermosetting resins is , still within the spirit of the invention. Such films are fully thermoplastic as well as It is expected that it will work.
発明のプロセスにおいて、結合フィルムは、面シート又はしばしば呼ばれる如く スキンに以前付着されたかに拘わらず、例えば、赤外線放射又は熱ガス噴射の加 熱手段により融点まで加熱され、ハニカム上に置かれ、そして押圧され、これに より、いろいろな構成要素を結合する。熱可塑性物質の融解の潜熱は、ハニカム における熱可塑性物質を溶解させ、結合フィルムと面シートに融着させるために 十分である。しばしば、融解の潜熱は、十分に高く、冷空気ブラスト又は水又は 他の液体による組立体の冷却が必要とされる。熱可塑性フィルムは溶融温度まで 加熱する代わりに、結合点においてフィルムを溶融押出ししても良い。In the process of invention, the bonding film is a face sheet or as it is often called. For example, the application of infrared radiation or hot gas jets, regardless of whether the skin has been previously attached to It is heated to its melting point by thermal means, placed on a honeycomb, and pressed onto it. By combining various components. The latent heat of melting of thermoplastics is in order to melt the thermoplastic and fuse it to the bonding film and face sheet. It is enough. Often the latent heat of fusion is sufficiently high that cold air blast or water or Cooling of the assembly with other liquids is required. Thermoplastic film up to melting temperature Instead of heating, the film may be melt extruded at the bond point.
第1図において、ハニカム(1)は、スキン(2)に以前融着又は接着された結 合熱可塑性フィルム(3)を用いてスキン(2)を上張りされる。源(4)から の赤外線は、融解温度までフィルム(3)を加熱するために使用される。結合は 、圧力ローラー(5)によって実施され、水噴射(6)によっj意的に冷却され る。加圧ローラーの代わりに、組立体は、標準プラーブレスを使用して加圧して も良い。プラテンの表面は、一般に、冷却され、熱サグを除去し、コアの過熱と スキンのブルーミングを防止する。In Figure 1, the honeycomb (1) has been previously fused or glued to the skin (2). A composite thermoplastic film (3) is used to overlay the skin (2). From source (4) Infrared radiation is used to heat the film (3) to melting temperature. The bond is , carried out by a pressure roller (5) and optionally cooled by a water jet (6) Ru. Instead of pressure rollers, the assembly can be pressurized using a standard puller brace. Also good. The platen surface is generally cooled to remove thermal sag and prevent core overheating. Prevents skin blooming.
第2図は、スキンをハニカムに結合する好ましい方法を示す。番号付けは、この 場合、フィルムがスキンに前結合されない分離熱可塑性フィルムであることを除 いて、第1図における如くである。Figure 2 shows a preferred method of bonding the skin to the honeycomb. The numbering is this except that the film is a separate thermoplastic film that is not prebonded to the skin. As shown in FIG.
第3図は、プロセスの一実施態様の側面図である。ハニカムコア(1)は、圧力 プラテン(9,10)の間の領域に案内レール(2)によって案内される。上方 スキン(3)と下方スキン(4)は、それぞれ、上方フィルム層(5)と下方フ ィルム層(6)を用いて、ハニカム(1)に結合される。フィルム層は、赤外線 加熱バンク(7,8)によって加熱され、プラテンが閉じられ、そして圧力が、 冷えるまで維持される。冷却は、プラテン(不図示)上又は内への水噴霧又は空 気衝突によって促進される。FIG. 3 is a side view of one embodiment of the process. Honeycomb core (1) has pressure It is guided by guide rails (2) in the area between the platens (9, 10). Upward The skin (3) and the lower skin (4) are connected to the upper film layer (5) and the lower film layer, respectively. It is bonded to the honeycomb (1) using a film layer (6). The film layer is infrared rays heated by the heating banks (7, 8), the platen is closed and the pressure is It is maintained until it cools down. Cooling can be achieved by water spray or air onto or into the platen (not shown). Facilitated by air collision.
第4図は、頂部からの第3図のプロセスの図である。ハニカムコア(1)は、上 方及び下方プラテン(9,10(頂部プラテンのみが示される))の間のプロセ ス案内レール(2)に沿って移動する。上方及び下方接着フィルム(5,6)は 、上方及び下方赤外線加熱バンク(7,8(上方バンクのみが示される))によ って加熱され、ハニカム(1)と上方及び下方スキン(3,4)の間のプラテン プレス領域に案内レール(2)に沿って折返し動作され、上方及び下方スキン( 3,4)はまた、案内レールに沿ってプラテン領域に折返し動作される。プレス は閉じられ、そして圧力は、熱可塑性接着剤の融解温度よりも低くまで維持され る。最終上張り)、qニカム製品は(11)において出て、プロセスは繰り返さ れる。FIG. 4 is a view of the process of FIG. 3 from the top. The honeycomb core (1) is The process between the upper and lower platens (9, 10 (only the top platen shown)) move along the space guide rail (2). The upper and lower adhesive films (5, 6) are , by upper and lower infrared heating banks (7, 8 (only upper bank shown)). platen between the honeycomb (1) and the upper and lower skins (3, 4). The upper and lower skins ( 3, 4) are also folded back into the platen area along guide rails. press is closed and pressure is maintained below the melting temperature of the thermoplastic adhesive. Ru. final overlay), the q-nicum product emerges in (11) and the process is repeated. It will be done.
実施例1 30cm対30cmの大きさで、Tyvekスパンホンデッドポリオレフィン製 の19mm厚コアが、Azdel、Inc、によって供給されるガラス繊維ポリ プロピレン含浸マットの2つの1.8mmスキンに結合された。結合フィルムは 、0.50mmポリプロピレンフィルムであり、セラミック赤外線放射加熱要素 によって融点まで加熱された。ハニカムサンドインチを組み立てる全時間は、1 5秒間であり、その内の5秒が、ポリプロピレンフィルムを加熱するために使用 され、5秒が、組立体を圧力結合するために使用され、圧力は、プラテンと圧力 ローラーによって印加された。最小圧力が結合のために必要とされ、そして圧力 は、冷えるまで維持され、5秒間、サンドイッチに水噴霧することにより冷却さ れた。Example 1 Measures 30cm by 30cm and is made of Tyvek spunbond polyolefin The 19mm thick core is made of glass fiber polyester supplied by Azdel, Inc. It was bonded to two 1.8 mm skins of propylene impregnated mat. The bonding film , 0.50mm polypropylene film and ceramic infrared radiant heating element heated to melting point. The total time to assemble the honeycomb sand inch is 1 5 seconds, of which 5 seconds are used to heat the polypropylene film. 5 seconds are used to pressure bond the assembly, the pressure is applied to the platen and the pressure applied by a roller. Minimum pressure is required for bonding, and pressure are kept until cool and cooled by spraying water on the sandwich for 5 seconds. It was.
実施例2 実施例1のプロセスは、ポリエーテルスルホンで含浸されたガラス繊維からでき たコアと0.38mmポリエーテルスルホン含浸ガラス繊維の面ソート又はスキ ンを用いて繰り返された。使用結合フィルムは、ポリエーテルイミド熱可塑性物 質(ULTEM)の0.13mmフィルムであった。全結合時間は、以前と同様 15秒であった。Example 2 The process of Example 1 was performed using glass fibers impregnated with polyether sulfone. A core of 0.38 mm polyethersulfone impregnated glass fiber is sorted or skimmed. It was repeated using The bonding film used is polyetherimide thermoplastic It was a 0.13 mm film of high quality (ULTEM). Total join time is the same as before It was 15 seconds.
実施例3 実施例2が、繰り返されたが、熱が、冷コア上で350℃に加熱されたプラテン により、面シートの外部で供給された。結合の直後に、組立体は、圧力下で水噴 霧輪−って冷却された。最終サンドイッチを生産するための全時間は、約510 秒であった。Example 3 Example 2 was repeated but the heat was applied to the platen heated to 350°C on the cold core. Supplied externally to the face sheet. Immediately after bonding, the assembly is heated under pressure with a water jet. The fog ring was cooled down. The total time to produce the final sandwich is approximately 510 It was seconds.
+1111111111111111111補正書の写しく翻訳文)提出書 ( 特許法第184条の8)平成5年6月2日+1111111111111111111 Copy and translation of amendment) Submission form ( Patent Law Article 184-8) June 2, 1993
Claims (4)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US62225390A | 1990-12-04 | 1990-12-04 | |
US622,253 | 1990-12-04 | ||
PCT/US1991/009023 WO1992010362A1 (en) | 1990-12-04 | 1991-12-03 | Process for the preparation of thermoplastic honeycomb sandwich structures |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH06503522A true JPH06503522A (en) | 1994-04-21 |
Family
ID=24493502
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP4502833A Pending JPH06503522A (en) | 1990-12-04 | 1991-12-03 | Process for the preparation of thermoplastic honeycomb sandwich structures |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0562001A4 (en) |
JP (1) | JPH06503522A (en) |
CA (1) | CA2056867A1 (en) |
WO (1) | WO1992010362A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004195960A (en) * | 2002-11-06 | 2004-07-15 | Britax Aircraft Interiors Uk Ltd | Composite sheet material |
JP2004322369A (en) * | 2003-04-22 | 2004-11-18 | Nissan Motor Co Ltd | Honeycomb structure, its manufacturing method and resin transfer forming method using the honeycomb structure |
JP2005216859A (en) * | 2004-01-27 | 2005-08-11 | Lg Electron Inc | Calcining apparatus and method for green sheet of plasma display panel |
JP2013233796A (en) * | 2012-04-10 | 2013-11-21 | Kurabo Ind Ltd | Multilayer structure |
JP2017196782A (en) * | 2016-04-26 | 2017-11-02 | 岐阜プラスチック工業株式会社 | Laminate structure |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU650769B2 (en) * | 1991-08-05 | 1994-06-30 | 3A Technology & Management Ltd. | Process for the production of a composite sheet comprising a cellular core and at least one outer layer |
TW274068B (en) * | 1993-05-13 | 1996-04-11 | Ciba Geigy Ag | |
ITBO940290A1 (en) * | 1994-06-23 | 1995-12-23 | Gd Spa | DEVICE FOR WELDING BETWEEN TWO TAPES OF MATERIAL FOR WRAPPING. |
IT233869Y1 (en) * | 1994-07-15 | 2000-02-10 | Rossi Roberto | ARRANGEMENT SUITABLE TO PROMOTE THE CORRECT PLASTIFICATION IN PLASTIFICING MACHINES WITH SOLVENT-FREE ADHESIVES |
FR2739803B1 (en) * | 1995-10-12 | 1997-12-05 | Induplast Sa | METHOD AND DEVICE FOR MANUFACTURING THERMOPLASTIC CORE SANDWICH STRUCTURES |
CA2195050A1 (en) * | 1996-01-29 | 1997-07-30 | Mark David Thiede-Smet | Low-weight and water-resistant honeycomb sandwich panels made by resin transfer molding process |
EP0787578A3 (en) * | 1996-02-05 | 1998-07-15 | C.A. Greiner & Söhne Gesellschaft M.B.H. | Laminated building element and method of manufacture |
ITPS990004A1 (en) * | 1999-02-16 | 2000-08-16 | PROCEDURE FOR THE CONSTRUCTION OF TAMBOURED PANELS AND MACHINE FOR THE REALIZATION OF SUCH PANELS | |
DE10313055B4 (en) * | 2003-03-24 | 2006-12-28 | Homag Holzbearbeitungssysteme Ag | Method and device for producing a lightweight board |
ES2298034B1 (en) * | 2006-05-12 | 2009-02-01 | Jesus Fco. Barberan Latorre | PANEL MANUFACTURING SYSTEM WITH BEE NEST. |
DE102006060940B4 (en) * | 2006-12-20 | 2010-04-01 | Fritz Egger Gmbh & Co. | Method for producing a lightweight board |
JP6546714B2 (en) | 2013-05-31 | 2019-07-17 | ダウ グローバル テクノロジーズ エルエルシー | Method of making a support portion of a solar module |
EP3152052B1 (en) | 2014-06-04 | 2021-08-11 | Bright Lite Structures LLC | Reinforced composite structure |
US10967583B2 (en) | 2015-04-03 | 2021-04-06 | Bright Lite Structures Llc | Apparatus for controllably cutting fibers and related methods |
US20190184646A1 (en) * | 2017-12-14 | 2019-06-20 | Bell Helicopter Textron Inc. | System and method of constructing a thermoplastic component |
CN108705817A (en) * | 2018-07-25 | 2018-10-26 | 浙江浩卓新材料科技有限公司 | A kind of multifunctional light thermoplastic composite board material and preparation method thereof |
CN117621577A (en) | 2018-11-19 | 2024-03-01 | 布莱特利特结构公司 | High strength low heat release composite |
CN113580453A (en) * | 2021-06-29 | 2021-11-02 | 山东格瑞德人工环境产业设计研究院有限公司 | A molding device and method for a variable-thickness thermoplastic honeycomb sandwich protective panel |
CN114701217A (en) * | 2022-03-21 | 2022-07-05 | 江苏奇一科技有限公司 | Continuous fiber reinforced thermoplastic composite board and preparation method and production equipment thereof |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3769129A (en) * | 1968-03-29 | 1973-10-30 | Steel Corp | Method of making an embossed composite sheet |
US3769131A (en) * | 1971-05-03 | 1973-10-30 | Johns Manville | Apparatus and method for laminating flexible layers |
US4249976A (en) * | 1979-04-04 | 1981-02-10 | Grumman Aerospace Corporation | Manufacture of honeycomb sandwich |
JPS6119886A (en) * | 1984-07-09 | 1986-01-28 | Nippon Oil Co Ltd | Production of tile carpet having improved dimensional stability |
US4902365A (en) * | 1987-12-03 | 1990-02-20 | Westlake Sr Edward F | Method for making a composite sheet-like structure |
EP0389978A3 (en) * | 1989-03-28 | 1991-02-27 | Cytec Technology Corp. | Composite panel |
CA2017661A1 (en) * | 1989-05-30 | 1990-11-30 | James E. O'connor | Composite cellular sandwich structure |
US5022943A (en) * | 1989-08-25 | 1991-06-11 | Eften, Inc. | Method of making thermoformably shaped fibreboard sandwich structures |
-
1991
- 1991-12-03 CA CA002056867A patent/CA2056867A1/en not_active Abandoned
- 1991-12-03 EP EP19920902626 patent/EP0562001A4/en not_active Withdrawn
- 1991-12-03 JP JP4502833A patent/JPH06503522A/en active Pending
- 1991-12-03 WO PCT/US1991/009023 patent/WO1992010362A1/en not_active Application Discontinuation
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004195960A (en) * | 2002-11-06 | 2004-07-15 | Britax Aircraft Interiors Uk Ltd | Composite sheet material |
JP4602659B2 (en) * | 2002-11-06 | 2010-12-22 | プレミアム・エアクラフト・インテリアーズ・ユーケイ・リミテッド | Composite sheet material |
JP2004322369A (en) * | 2003-04-22 | 2004-11-18 | Nissan Motor Co Ltd | Honeycomb structure, its manufacturing method and resin transfer forming method using the honeycomb structure |
JP2005216859A (en) * | 2004-01-27 | 2005-08-11 | Lg Electron Inc | Calcining apparatus and method for green sheet of plasma display panel |
JP2013233796A (en) * | 2012-04-10 | 2013-11-21 | Kurabo Ind Ltd | Multilayer structure |
JP2017196782A (en) * | 2016-04-26 | 2017-11-02 | 岐阜プラスチック工業株式会社 | Laminate structure |
Also Published As
Publication number | Publication date |
---|---|
CA2056867A1 (en) | 1992-06-05 |
EP0562001A4 (en) | 1993-10-20 |
EP0562001A1 (en) | 1993-09-29 |
WO1992010362A1 (en) | 1992-06-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JPH06503522A (en) | Process for the preparation of thermoplastic honeycomb sandwich structures | |
US5316604A (en) | Process for the preparation of thermoplastic sandwich structures | |
US5066536A (en) | Fibre reinforced thermoplastic composite structures | |
US5667881A (en) | Integral thermoset/thermoplastic composite joint | |
US5139596A (en) | Continuous process for the preparation of thermoplastic honeycomb | |
US5078821A (en) | Method and apparatus for producing composites of materials exhibiting thermoplastic properties | |
FI107593B (en) | A method for making a composite sheet from a honeycomb structure and at least one cover layer | |
US8657990B2 (en) | Nanotube-enhanced interlayers for composite structures | |
EP2931497B1 (en) | Joining composite components using low temperature thermoplastic film fusion | |
US6743742B1 (en) | Method of partially embedding non-woven fiber mat to reinforcing fibers impregnated with a thermoplastic resin and composition therefrom | |
JP6966848B2 (en) | Composite structure with reinforcing material and its manufacturing method | |
US6039832A (en) | Thermoplastic titanium honeycomb panel | |
EP0605235A2 (en) | Ceiling material for vehicles and production process thereof | |
US20070095459A1 (en) | Sandwich panel with interior barrier | |
JP2007015385A (en) | Composite honeycomb sandwich structure | |
US7138031B2 (en) | Mandrel and method for manufacturing composite structures | |
JPH02269131A (en) | Raw material for light-weight structure, and method and device for producing honeycomb structure therefrom | |
JP5045330B2 (en) | Manufacturing method of fiber reinforced plastic structure | |
US5219642A (en) | Fibre reinforced stuctural thermoplastic composite materials | |
JPH0919964A (en) | Manufacture of laminated sheet | |
JPH07178859A (en) | Laminate and production thereof | |
EP3616890B1 (en) | Preform shaping method and composite forming method | |
US5942307A (en) | Lightweight building board | |
EP0401991A2 (en) | Fibre reinforced structural thermoplastic composite materials | |
JPH10278184A (en) | Continuous fiber reinforced thermoplastic resin laminate and its production |