CN110014660A - 用于制造载具构件的方法、载具构件及具有载具构件的载具 - Google Patents

用于制造载具构件的方法、载具构件及具有载具构件的载具 Download PDF

Info

Publication number
CN110014660A
CN110014660A CN201811556176.XA CN201811556176A CN110014660A CN 110014660 A CN110014660 A CN 110014660A CN 201811556176 A CN201811556176 A CN 201811556176A CN 110014660 A CN110014660 A CN 110014660A
Authority
CN
China
Prior art keywords
surface region
strenthening member
carrier
cooling
carrier component
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
Application number
CN201811556176.XA
Other languages
English (en)
Inventor
彼得·林德
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of CN110014660A publication Critical patent/CN110014660A/zh
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • 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
    • B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/08—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • B29C65/22—Heated wire resistive ribbon, resistive band or resistive strip
    • B29C65/221—Heated wire resistive ribbon, resistive band or resistive strip characterised by the type of heated wire, resistive ribbon, band or strip
    • 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
    • B29C65/34—Joining 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"
    • B29C65/3404—Joining 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" characterised by the type of heated elements which remain in the joint
    • B29C65/344—Joining 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" characterised by the type of heated elements which remain in the joint being a woven or non-woven fabric or being a mesh
    • 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
    • B29C65/82—Testing the joint
    • 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
    • B29C66/032—Mechanical after-treatments
    • B29C66/0324—Reforming or reshaping the joint, e.g. folding over
    • 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
    • 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
    • B29C66/112—Single lapped joints
    • B29C66/1122—Single lap to lap joints, i.e. overlap joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
    • B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/472—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially flat
    • B29C66/4722—Fixing strips to surfaces other than edge faces
    • 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
    • B29C66/532—Joining single elements to the wall of tubular articles, hollow articles or bars
    • 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
    • B29C66/61—Joining from or joining on the inside
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
    • B29C66/72141—Fibres of continuous length
    • 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
    • B29C66/90—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
    • B29C66/9141—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
    • B29C66/91441—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 the temperature being non-constant over time
    • 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
    • B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
    • F28F21/02—Constructions of heat-exchange apparatus characterised by the selection of particular materials of carbon, e.g. graphite
    • 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
    • B29C65/34—Joining 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"
    • B29C65/3472—Joining 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" characterised by the composition of the heated elements which remain in the joint
    • B29C65/3476—Joining 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" characterised by the composition of the heated elements which remain in the joint being metallic
    • B29C65/348—Joining 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" characterised by the composition of the heated elements which remain in the joint being metallic with a polymer coating
    • 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
    • B29C65/34—Joining 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"
    • B29C65/3472—Joining 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" characterised by the composition of the heated elements which remain in the joint
    • B29C65/3484—Joining 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" characterised by the composition of the heated elements which remain in the joint being non-metallic
    • B29C65/3492—Joining 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" characterised by the composition of the heated elements which remain in the joint being non-metallic being carbon
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00—Use of elements other than metals as reinforcement
    • B29K2307/04—Carbon
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2671/00—Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone, or derivatives thereof, for preformed parts, e.g. for inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3085—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Textile Engineering (AREA)
  • Architecture (AREA)
  • Transportation (AREA)
  • General Engineering & Computer Science (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

用于由纤维强化的塑料制造载具构件的方法，具有以下步骤：提供表层区域，表层区域带有内侧、外侧和布置在内侧处的容纳区段，表层区域由纤维强化的热塑性材料组成；提供带有连接面的加固构件，加固构件由纤维强化的热塑性材料组成；使加固构件和表层区域接触，使得连接面位于容纳区段上；面状地加热接合区，加固构件的连接面和容纳区段位于该接合区中，使得加固构件和表层区域相互焊接在一起；冷却接合区；将由加固构件和表层区域形成的组合的所获得的几何形状与可预设的几何形状比较；如果所获得的几何形状与可预设的几何形状有偏差，重新加热接合区、使加固构件和表层区域变形且冷却。还提出一种载具构件以及具有所述载具构件的载具。

Description

用于制造载具构件的方法、载具构件及具有载具构件的载具
技术领域
本发明涉及一种用于由纤维强化的塑料制造载具构件的方法，以及一种载具构件或者一种带有这样的载具构件的载具。
背景技术
较大的载具且尤其交通飞行器越来越多地借助于由纤维强化的塑料制成的构件来制造。构件尤其在交通飞行器的情况下常常是大规格的，以便减小连接多个构件的耗费。但是在使用大规格的由纤维强化的塑料制成的构件时有时可能会产生形状偏差或应修整的表面。如果例如表层区域配备有加固构件，则有时将表层区域的预制件和加固构件的预制件共同安放到成型模具上，以便紧接着共同在高压釜中加热以便硬化。由于层厚不同，在加热之后可能发生不同速度的冷却。例如在连接区域中的加固构件还未完全冷却，而相邻的不带有加固构件的表层区域已经完全冷却。由此可能发生不同的膨胀，其反映为在外表面上的一定的波纹。
此外对于纤维强化的塑料而言可能发生以下情况：嵌入到基质中的纤维部分地叠置或不完全笔直地取向。由此产生相对细小的、但是可见的波纹。
尤其在航空工业中用于纤维强化塑料的连接方法常常基于使用铆钉。有时不能排除，这样的铆接连接导致在制造的构件的外表面处的可看见的铆钉。
这三种类型的形状偏差能够通过不同的措施消除。对于它们而言共同点是，附加地至少局部地施加薄的材料层，以便紧接着以去除材料的方式处理构件的整个表面。这可能是费劲的且此外提高了所制造的构件的重量。如果构件为飞行器的部件，则应尽可能防止上述情况。
发明内容
值得期望的是，具有一种方法，以尤其由纤维强化的塑料制造大规格的构件，该方法不会导致所提及的形状偏差。
因此本发明的目的是，给出一种用于由纤维强化的塑料制造构件的方法，在该方法中能够在没有附加地施加材料的情况下产生特别有利的构件和表面质量。
该目的通过一种用于由纤维强化的塑料制造载具构件的方法来实现。有利的改进方案和实施方式能够从实施例和下文的描述中得出。
给出一种用于由纤维强化的塑料制造载具构件的方法。该方法具有以下步骤：提供至少一个表层区域，所述表层区域带有内侧、外侧和布置在所述内侧处的容纳区段，其中所述表层区域由纤维强化的热塑性材料组成；提供带有连接面的至少一个加固构件，其中所述加固构件由纤维强化的热塑性材料组成；使所述至少一个加固构件和所述至少一个表层区域接触，使得所述连接面位于所述容纳区段上；面状地加热接合区，所述加固构件的连接面和所述容纳区段位于该接合区中，使得所述至少一个加固构件和所述至少一个表层区域相互焊接在一起；冷却所述接合区；将由加固构件和表层区域形成的组合的所获得的几何形状与可预设的几何形状进行比较；且如果所获得的几何形状与所述可预设的几何形状有偏差，则重新加热所述接合区、使所述加固构件和所述表层区域变形且冷却以便达到所述可预设的几何形状。
原则上，该方法与已知的方法的区别在于，代替纤维强化的基于热固性塑料的材料，使用带有增强纤维的热塑性材料。适合用于实现基质的热塑性材料可以包括PPS(聚苯硫醚)、PEEK(聚醚醚酮)、PEKK(聚醚酮酮)或其他。
此外，增强纤维也能够根据使用目的进行选择并且例如包含碳纤维、玻璃纤维、芳族聚酰胺纤维、凯夫拉纤维等。这种材料的使用导致在可能的形状偏差的可修正性方面的特别优点。对于热固性塑料材料而言能够将增强纤维嵌入到液态的或糊状的部件中，其由树脂体系制成。在树脂硬化之后不再能够在该处执行形状修正。硬化的过程是不可逆的且必须采取一定的预防措施：在树脂硬化时实现或者维持期望的形状。
但是通过使用热塑性材料以用于嵌入增强纤维能够实现几何形状的后续修正。如果在开头提及的示例中实施带有表层区域的内侧的加固构件，那么理论上即使在使用热塑性纤维强化的塑料时在硬化时也可能产生一定的形状偏差。但是这种形状偏差根据本发明通过如下方式消除，即在确认与理论几何形状有偏差之后能够重新执行局部加热，以便以机械的方式将由加固构件和表层区域形成的复合物改变到期望的理论几何形状。硬化的过程在热塑性材料中完全是可逆的。
但是所给出的方法还具有特别的优点：能够实际上完全放弃铆接连接。由于材料的可逆的硬化，还可以局部熔化材料，从而两个待相互连接的构件的熔化的区域彼此渗透，从而由此实际上实现整体的构件。因此，为了建立连接不必通过钻孔、去毛刺、清洁、密封、引入铆接体且使铆接体变形来建立铆接连接。局部加热即已足够，通过该局部加热，两个相关的接合配对(尤其在另外的压紧力作用下)能够达到材料配合的连接。
通过局部面状地加热在待连接的部件之间的连接区域，还能够将由表层区域和加固构件形成的复合物的整个加热限制在非常小的区域、也就是说相当小的体积上。由此由于构件中的温度梯度产生本身明显更小的膨胀效果。
加热应该限制在非常薄的层上，以便充分利用该优点。连接区域能够通过电感方法、使用加热电阻或通过传导加热，其中将加热层整合至待相互连接的构件之一是优选的。
因此能够通过根据本发明的方法限制或者取消使用铆接。由此引起的通过突出的铆钉头造成的不平坦的表面等等能够得以避免。同时能够明显降低且此外明显更简单地排除制造的构件的由于加热引起的波纹。因此不需要附加地将材料施加到所制造的构件的外表面上。
就此而言应指出的是，在表层区域的内侧处的容纳区段不必具有特别的构造。相反地，该容纳区段可以是限定的面状区域，该至少一个加固构件的连接面放置在该面状区域中。此外，该至少一个加固构件的连接面在最简单的情况中仅仅是这样的面，即该面的走向与容纳区段对应。连接面仅仅用于，在该至少一个加固构件和该至少一个表层区域之间建立齐平的面接触，以便紧接着通过局部加热引起焊接。
在一种有利的实施方式中提出，所述至少一个表层区域具有平行地铺开增强纤维且将所述增强纤维嵌入到热塑性的基质材料中。这应如此理解，即纤维束为此能够通过机械梳理或类似的过程加工成带有彼此平行的增强纤维的扁平的层组件。通过梳理增强纤维，增强纤维能够尤其以预定的间距且以精确调整的取向和预定的层厚嵌入到基质材料中。例如，在热塑性树脂中能够提供带有平行纤维的此类扁平的层组件作为薄的窄的无纺带或织物层。它们能够邻接于较大的表层区域在相应的成型模具上以期望的纤维方向放置且相互连接。由此能够抑制不同量的增强纤维的重叠，这能够消除制造的构件的细微的波纹。
在本发明的一种有利的实施方式中，此外执行将可传导的层放置到所述连接面和/或所述容纳区段上这一步骤，其中所述面状地加热包含在所述可传导的层上施加电压。可传导的层尤其用作电阻加热层。可传导的层能够实施为薄膜或织物。该层的材料应有足够的可传导性且能够尤其由金属材料制造和/或包含较高比例的碳。有意义的是，限定这样的联接导线、联接点等等，即其与可传导的层连接且从连接区域伸出，从而可导电的层能够与外部的电源接触。为此，所述层设置成，通过施加电压触发电流流动通过层，该电流由于层的电阻而导致层加热。由此能够针对性地仅仅加热连接面和容纳区段。所述层应在此实施成尽可能细，使得其随后保留在制造的构件中仅仅导致可忽略的重量增加。但是所述层还应如此设计尺寸，即，能够实现足够的加热功率。一般而言在该实施方式中可能要注意的是，在可传导的层加热时监测或限制电压和/或出现的电流强度，从而能够防止损坏可传导的层。
所述可传导的层以由线形元件形成的网的形式由包含碳的材料制造。为此可能例如考虑碳纤维或碳纳米管。利用线形元件可能形成正方形的、长方形的或另外规则成型的网孔。由此能够以网孔的方式执行连接区域的加热。由此根据网孔的尺寸加热整个连接区域。不必用仅仅用于加热目的的材料来填满被包围的面。
在一种特别有利的实施方式中，可传导的层由碳纳米管形成的网组成，这些碳纳米管具有特别高的抗拉强度和对于加热目的足够的可导电性。整合这样的网导致明显的重量优势，因为由于碳纳米管造成的额外引入的重量实际上是不可测量的。
此外加热还能够通过局部引入超声波来进行。在也称为超声波焊接的此类方法中，通过将超声振动转换为机械振动产生热量。经由以超声焊极形式的接口将振动引向一个或两个接合配对物。这导致边界面和分子摩擦，其导致局部加热。在当前情况中有意义的是，给该至少一个加固构件加载声波。尤其通过非常短的、以一定的模式定时的声脉冲能够在连接区域中实现局部的集中的加热。
在一种特别优选的实施方式中，冷却包括在冷却时维持所述连接区域的适度的加热这一步骤。因此通过维持热输入影响连接区域(构件在该连接区域中相互焊接在一起)的冷却。这可以通过以下方式实现，即可传导的层与控制单元连接，该控制单元与电源连接。控制单元能够例如为了执行对于焊接足够的加热而将一定的电压施加到可导电的层处或设定一定的电流强度。尤其在最大电流强度的情况下实现最大加热功率。为了冷却目的，至少在某一时刻且在至少某一段持续时间上能够减小该加热功率。加热功率优选地如此减小，即，使得从连接区域向外的热损失超过那时还输送的加热功率。这意味着，热损失相对于简单地分离可传导的层有明显延迟。这导致连接区域的更平缓的冷却，由此可能的热应力和膨胀效果还可以进一步降低。可设想的是，控制单元设立成，在冷却期间执行多次加热功率降低。合理的此类步骤的数量及其分别的持续时间取决于接合配对物的类型和特性。优选地，这样的控制单元可能设立成，基于根据理论或根据实验确定的冷却曲线来确定加热功率降低步骤的数量及其持续时间。
在另一种有利的实施方式中，放置可导电的层包含整合传感器导线，该传感器导线能够与控制单元连接，其中所述控制单元通过以下方式来控制冷却：基于借助于所述传感器导线确定的温度通过输送热功率通过将电功率输送到所述可导电的层处。传感器导线能够由与可导电的层相同的材料或用与可导电的层类似的材料特性来提供。这样的传感器导线能够在可导电的层的一定部分上延伸且能够从外部与控制单元电连接。传感器导线构成为，取决于温度改变其电阻。控制单元能够基于测量的电阻确定在连接区域中的温度。基于在连接区域中确定的温度能够调整加热功率以便进行受引导的冷却。由此能够基本上放弃根据实验或根据理论确定冷却曲线，并且直接基于在连接区域中的当前的温度进行冷却。
加热和变形的附加步骤能够例如包括将成型模具安置到所述表层区域的内侧处且施加向外、即在所述表层区域的外侧的方向上的起变形作用的力。成型模具能够例如与该至少一个加固构件相匹配且在重复加热之后允许轻微的形状修正。
然而重复加热能够在比仅仅连接区域更大的区域上扩展。由此还能够在相邻的区域中降低热应力，从而实现可预设的几何形状。重复加热能够尤其通过加热装置实现，该加热装置布置在成型模具处。
本发明此外涉及一种载具构件，该载具构件具有至少一个表层区域和至少一个布置在表层区域的内侧处的加固构件，其中载具构件利用上面提及的方法制造。
此外本发明涉及一种载具，该载具具有至少一个这样的载具构件。该载具能够尤其为飞行器且优选为交通飞行器。
此外本发明可以涉及一种系统，该系统设立成用于由纤维强化的塑料制造载具构件。该系统可以具有控制单元、成型模具、加热装置和测量装置。控制单元此外可以与加热装置连接。控制单元可以设立成，操控加热装置以用于加热在上文提及的表层构件和该至少一个加固构件之间的连接区域，且借助于测量装置探测在冷却之后经由测量装置确定的几何形状是否与可预设的几何形状有偏差。如果有偏差，控制单元可以如此操控成型模具和加热装置，使得进行重复加热且成型模具执行变形。
附图说明
本发明的其它特征、优点和应用可能性从对实施例的以下说明和附图中得出。在此，所有所描述的和/或图示的特征自身和以任意组合构成本发明的主题，而不依赖于其在各实施例中的组合。此外，在附图中相同的附图标记代表相同或相似的物体。
图1显示了待制造的载具构件的部分截面。
图2显示了加固构件以及布置在其上的用于加热连接区域的可传导的层的细节图。
图3显示了在制造表层区域时增强纤维的铺开情况。
图4显示了加固构件的连接区域的细节图。
图5显示了来自图1的部分截面以及布置在其上的来自图4的加固构件。
图6显示了根据本发明的方法基于框图的示图。
图7显示了一种飞行器，其具有一个或多个利用根据本发明方法制造的载具构件。
具体实施方式
图1以示意图显示了表层区域2以及加固构件4。表层区域2具有外侧6、内侧8以及设置在该内侧处的容纳区段10。加固构件4示例性地构造为用于飞行器的表壳的纵向加固元件(桁条)。加固构件4仅示范性地具有两个支腿12，这两个支腿提供分段的连接面14。连接面14与在表层区域2的内侧8上的容纳区段10面接触。
不仅表层区域2而且加固构件4由纤维强化的热塑性塑料制造。热塑性塑料能够例如为具有嵌入的碳纤维作为增强纤维的PEEK或PEKK。
增强纤维在该示图中仅仅简述。通过加热在加固构件4和表层区域2之间的连接区域(该连接区域包含容纳区段10和连接面14)，两个构件2和4能够相互焊接在一起。由此部分区域地熔化热塑性基质材料，从而局部地在接合区域中实现两个部件2和4的材料的混匀。因此在冷却之后，存在实际上整体的复合物。
局部加热能够尤其通过布置可导电的层16实现。该可导电的层在图2中由碳纳米管18形成的网组成，这些碳纳米管具有多个网孔20。通过将可导电的层16与电源22连接加热层16，从而仅仅在接合区域中执行加热。
加热能够通过可选的控制单元21控制。控制单元21以及相应的联接线路以虚线示出。此外在连接区域冷却时能够维持轻微的加热，从而冷却更平缓地进行。这能够尤其通过控制单元21通过降低电流供应来实现。
此外可选地能够设置有传感器导线23，借助于该传感器导线，控制单元21能够监测在连接区域的内部中的温度。基于这种监测能够进行冷却控制。
当部件2和4的纤维相互平行地取向且不具有特别的波纹时，则实现了特别有利的表面质量。为此在图3中示出，用于制造尤其表层区域2的纤维束24能够通过梳理铺开。由此完美地提供彼此平行以及并排取向的纤维26，这些纤维能够并入到热塑性基质材料28中。可设想的是，制造由热塑性塑料制成且带有经梳理的纤维的纤维强化材料的多个层且将该多个层幅面状地或带状地组合在一起。
图4显示了带有连接面的多个区段32或部段的加固构件30的变体，该多个区段或部段设有在上文示出的由碳纳米管制成的网。加固构件30能够此外示例性地具有切口34，根据图1的加固构件4能够伸延通过该切口。因此加固构件30可能为隔板的一部分，而加固构件4是纵向加固元件(桁条)的一部分。
来自图4的元件在图5中以组合在一起的形式示出带有表层区域2，其能够形成隔板的一部分。以黑实线指示的面可以解释为连接区域36，在该连接区域中执行焊接。
在图6中示意性地以框图显示了根据本发明的方法。该方法具有步骤：提供38至少一个表层区域2，该表层区域带有内侧8、外侧6和布置在内侧8处的容纳区段10；提供40带有连接面14的至少一个加固构件；使该至少一个加固构件和该至少一个表层区域接触42，使得连接面位于容纳区段上；面状地加热44接合区，加固构件的连接面和容纳区段位于该接合区中，使得该至少一个加固构件和该至少一个表层区域相互焊接在一起；冷却46接合区；将由加固构件和表层区域形成的组合的确定的几何形状与可预设的几何形状进行比较48；且如果确定的几何形状与可预设的几何形状有偏差，则重新加热50接合区、使加固构件和表层区域变形52且冷却54以便达到可预设的几何形状。该方法能够此外包含将可传导的层放置56到连接面和/或容纳区段上。在冷却46时，此外还能够维持58连接区域的适度的加热。
最后图7公开了交通飞行器60，该交通飞行器具有至少一个通过根据本发明的方法制造的构件62。该构件仅仅示例性地以虚线指示。所有其他构件同样可以利用根据本发明的方法制造。
补充性地应指出的是，“具有”并不排除其他的元件或步骤，并且“一个”或“一种”不排除多数。此外应指出的是，已经参照上述实施例之一描述的特征还可以与上文描述的另外实施例的其他特征组合使用。

Claims (12)

1.一种用于由纤维强化的塑料制造载具构件的方法，所述方法具有以下步骤：
-提供(38)至少一个表层区域(2)，所述表层区域带有内侧(8)、外侧(6)和布置在所述内侧(8)处的容纳区段(10)，其中所述表层区域(2)由纤维强化的热塑性材料组成，
-提供(40)带有连接面(14)的至少一个加固构件(4，30)，其中所述加固构件(4，30)由纤维强化的热塑性材料组成，
-使所述至少一个加固构件(4，30)和所述至少一个表层区域(2)接触(42)，使得所述连接面(14)位于所述容纳区段(10)上，
-面状地加热(44)接合区，所述加固构件(4，30)的所述连接面(14)和所述容纳区段(10)位于所述接合区中，使得所述至少一个加固构件(4，30)和所述至少一个表层区域(2)相互焊接在一起，
-冷却(46)所述接合区，
-将由加固构件(4，30)和表层区域(2)形成的组合的所获得的几何形状与可预设的几何形状进行比较(48)，且
-如果所获得的几何形状与所述可预设的几何形状有偏差，则重新加热(50)所述接合区、使所述加固构件(4，30)和所述表层区域(2)变形(52)且冷却(54)以便达到所述可预设的几何形状。
2.根据权利要求1所述的方法，
其中所述提供所述至少一个表层区域(2)包括平行地铺开增强纤维(26)且将所述增强纤维(26)嵌入到热塑性的基质材料中。
3.根据权利要求1或2所述的方法，
此外具有以下步骤：将可传导的层(16)放置到所述连接面(14)和/或所述容纳区段(10)上，
其中所述面状地加热包含在所述可传导的层(16)上施加电压。
4.根据权利要求3所述的方法，
其中所述可传导的层(16)以由线形的元件形成的网的形式由包含碳的材料制造。
5.根据权利要求3或4所述的方法，
其中所述可传导的层(16)由碳纳米管形成的网组成。
6.根据权利要求1或2所述的方法，
其中所述加热包括局部引入超声波。
7.根据以上权利要求之一所述的方法，
其中所述冷却具有以下步骤：在冷却时维持所述接合区的适度的加热。
8.根据权利要求3和7所述的方法，
其中所述放置可导电的层(16)包含整合传感器导线(23)，所述传感器导线能够与控制单元(21)连接，
其中所述控制单元(21)通过以下方式来控制冷却：基于借助于所述传感器导线(23)确定的温度通过将电功率输送到所述可导电的层(16)处来输送热功率。
9.根据以上权利要求之一所述的方法，
其中所述附加的加热和变形步骤包括将成型模具安置在所述表层区域(2)的内侧处且施加向外的起变形作用的力。
10.一种载具构件，所述载具构件具有至少一个表层区域(2)和至少一个布置在所述表层区域(2)的内侧处的加固构件(4，30)，其中所述载具构件利用根据权利要求1至9之一所述的方法制造。
11.一种载具(60)，所述载具具有至少一个根据权利要求10所述的载具构件。
12.根据权利要求11所述的载具(60)，其中所述载具(60)为飞行器(60)。
CN201811556176.XA 2017-12-21 2018-12-19 用于制造载具构件的方法、载具构件及具有载具构件的载具 Pending CN110014660A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102017130927.6A DE102017130927A1 (de) 2017-12-21 2017-12-21 Verfahren zum Herstellen eines Fahrzeugbauteils aus einem faserverstärkten Kunststoff
DE102017130927.6 2017-12-21

Publications (1)

Publication Number Publication Date
CN110014660A true CN110014660A (zh) 2019-07-16

Family

ID=64456893

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811556176.XA Pending CN110014660A (zh) 2017-12-21 2018-12-19 用于制造载具构件的方法、载具构件及具有载具构件的载具

Country Status (4)

Country Link
US (1) US10987877B2 (zh)
EP (1) EP3501801B1 (zh)
CN (1) CN110014660A (zh)
DE (1) DE102017130927A1 (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110722802A (zh) * 2019-09-26 2020-01-24 沈阳航空航天大学 基于超声辅助的轻质合金与热塑性复合材料的连接方法

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102018112684A1 (de) * 2018-05-28 2019-11-28 Airbus Operations Gmbh Verfahren und Vorrichtung zum Herstellen eines Bauteils aus Faserverbundwerkstoff

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4309905A (en) * 1979-12-26 1982-01-12 Maizenberg Mikhail I Method for detecting non-uniformities of magnetic materials and device for effecting same
US8213849B2 (en) * 2009-07-20 2012-07-03 Xerox Corporation Inductively heated carbon nanotube fuser
DE102011051071A1 (de) * 2011-06-15 2012-12-20 Synview Gmbh Verfahren zur Herstellung faserverstärkter Formteile
US20160136879A1 (en) * 2014-11-18 2016-05-19 The Boeing Company Susceptor Welding Tape
DE102015109483B4 (de) * 2015-06-15 2020-10-01 Lisa Dräxlmaier GmbH Faserverbundbauteil
DE102015114786A1 (de) * 2015-09-03 2017-03-09 Dieffenbacher GmbH Maschinen- und Anlagenbau Verfahren und Vorrichtung zur Herstellung von faserverstärkten Kunststoffteilen
EP3178635B1 (en) * 2015-12-11 2019-10-30 Airbus Operations GmbH Method for welding together a first object and a second object
DE102016210124A1 (de) * 2016-06-08 2017-12-14 Airbus Operations Gmbh Verfahren zur Integration einer Hinterbaustruktur-Baugruppe in eine Struktur eines Luft- oder Raumfahrzeugs
DE102016210086A1 (de) * 2016-06-08 2017-12-14 Airbus Operations Gmbh Verfahren zum Herstellen eines Strukturbauteils für ein Luft- oder Raumfahrzeug, sowie Anordnung
US20170355150A1 (en) * 2016-06-14 2017-12-14 GM Global Technology Operations LLC Ultrasonic weld-bonding of thermoplastic composites
DE102017217294A1 (de) * 2017-09-28 2019-03-28 Airbus Operations Gmbh Verfahren zum Widerstandsschweißen von Faserverbundbauteilen zu einer Faserverbundstruktur, Faserverbundstruktur und Faserverbundbauteil

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110722802A (zh) * 2019-09-26 2020-01-24 沈阳航空航天大学 基于超声辅助的轻质合金与热塑性复合材料的连接方法

Also Published As

Publication number Publication date
US20190202141A1 (en) 2019-07-04
US10987877B2 (en) 2021-04-27
DE102017130927A1 (de) 2019-06-27
EP3501801B1 (de) 2021-03-17
EP3501801A1 (de) 2019-06-26

Similar Documents

Publication Publication Date Title
US5705796A (en) Reinforced composites formed using induction thermoplastic welding
US9586362B2 (en) Thermoplastic welding apparatus and method
CN110014660A (zh) 用于制造载具构件的方法、载具构件及具有载具构件的载具
Tsiangou et al. On the sensitivity of ultrasonic welding of epoxy-to polyetheretherketone (PEEK)-based composites to the heating time during the welding process
CN112399912B (zh) 用于通过电磁焊接来接合模制部件的方法和设备
US10252472B2 (en) Method for joining fiber-reinforced plastic material
JP2005536583A (ja) 接合部硬化を加速する方法
US20170057155A1 (en) Method and system for reinforcing a workpiece
KR20140139493A (ko) 탄소 섬유 프리폼, 탄소 섬유 강화 플라스틱, 탄소 섬유 프리폼의 제조 방법
JP2017513241A (ja) 蓋部を用いる電気的デバイスの搭載方法、および、当該方法における使用に適した蓋部
JP6757174B2 (ja) 複合材料の接合方法
JPH04504386A (ja) 複合材料の接合方法
JPH07505342A (ja) 熱可塑性接着のための加熱手段
US20160136879A1 (en) Susceptor Welding Tape
US10994493B2 (en) Method and apparatus for welding a thermoset object to a further object via thermoplastic outer layers
EP3178635B1 (en) Method for welding together a first object and a second object
KR20180026456A (ko) 물체의 상호 접합
JP5962387B2 (ja) ワイヤーハーネス及びワイヤーハーネスの製造方法
KR101921053B1 (ko) 통전압접장치 및 통전압접방법
NL2027363B1 (en) Resistance welding methods and apparatus
JPS6174824A (ja) スキーぐつ用のパツドの製造、特にスキーぐつ用インナシユーの製造のための方法
JPH1016061A (ja) 熱可塑性合成樹脂で成形された成形品を熱融着する方法及びこの方法に用いられる発熱体
US20240181720A1 (en) Pressure Tool, Pressing Apparatus And Method For Welding Plastics Components
JP7171818B1 (ja) 融着方法および構造体
JP2024500699A (ja) 成形部品の電磁スポット溶接のための方法及び装置

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination