WO2016117062A1 - 炭素繊維強化樹脂材の締結構造 - Google Patents

炭素繊維強化樹脂材の締結構造 Download PDF

Info

Publication number
WO2016117062A1
WO2016117062A1 PCT/JP2015/051608 JP2015051608W WO2016117062A1 WO 2016117062 A1 WO2016117062 A1 WO 2016117062A1 JP 2015051608 W JP2015051608 W JP 2015051608W WO 2016117062 A1 WO2016117062 A1 WO 2016117062A1
Authority
WO
WIPO (PCT)
Prior art keywords
collar
carbon fiber
resin material
reinforced resin
fiber reinforced
Prior art date
Application number
PCT/JP2015/051608
Other languages
English (en)
French (fr)
Inventor
雅稔 森
大久保　洋志
Original Assignee
日産自動車株式会社
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 日産自動車株式会社 filed Critical 日産自動車株式会社
Priority to CN201580074086.5A priority Critical patent/CN107208678B/zh
Priority to JP2016570405A priority patent/JP6332475B2/ja
Priority to PCT/JP2015/051608 priority patent/WO2016117062A1/ja
Priority to US15/539,766 priority patent/US10132342B2/en
Priority to EP15878757.2A priority patent/EP3249242B1/en
Publication of WO2016117062A1 publication Critical patent/WO2016117062A1/ja

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F16B5/0241—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread with the possibility for the connection to absorb deformation, e.g. thermal or vibrational
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/561—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using screw-threads being integral at least to 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
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with 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
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/64—Joining a non-plastics element to a plastics element, e.g. by force
    • 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
    • B29C66/11—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
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/116—Single bevelled joints, i.e. one of the parts to be joined being bevelled in the joint area
    • B29C66/1162—Single bevel to bevel joints, e.g. mitre joints
    • 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
    • B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
    • B29C66/126—Tenon and mortise 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
    • B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/474—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/731—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
    • B29C66/7311—Thermal properties
    • B29C66/73111—Thermal expansion coefficient
    • B29C66/73112—Thermal expansion coefficient of different thermal expansion coefficient, i.e. the thermal expansion coefficient of one of the parts to be joined being different from the thermal expansion coefficient of the other part
    • 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
    • B29C66/74—Joining plastics material to non-plastics material
    • B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • 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
    • B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
    • B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
    • B29C65/4835—Heat curing adhesives

Definitions

  • the present invention relates to a fastening structure of a carbon fiber reinforced resin (hereinafter referred to as “CFRP”) material.
  • CFRP carbon fiber reinforced resin
  • Patent Document 1 discloses a technique for fastening a CFRP material and a bracket using bolts and nuts.
  • the resin constituting CFRP has a property of creep deformation
  • a metal collar is attached to the CFRP material so that the axial force of the bolt is received by the metal collar. It may be. By doing so, it is possible to suppress the occurrence of loosening of the bolt due to the thinning caused by creep deformation or the like in the resin material constituting the CFRP material over time, resulting in a decrease in the axial force of the bolt.
  • liquid for example, rainwater or seawater
  • the metal collar may be eroded and corrosion may occur.
  • an electrically insulating adhesive is applied to the inner peripheral surface of the prepared hole of the CFRP material to which the metal collar is to be attached to electrically insulate the CFRP material from the metal collar. It is preferable to keep it.
  • the present invention suppresses the electrical corrosion of the metal collar by suppressing the electrical contact between the outer periphery of the metal collar and the inner peripheral surface of the pilot hole provided in the CFRP material. It aims at providing the fastening structure of CFRP material which can be performed.
  • the outer periphery of the metal collar has a tapered portion that is inclined with respect to the central axis of the collar, and the inner peripheral surface of the through hole in the CFRP material has electrical insulation. It has a contact portion that contacts the tapered portion of the collar through the adhesive.
  • the inclination angle of the collar taper portion and the contact portion of the CFRP material is determined by the displacement in the direction perpendicular to the surface of the contact portion of the CFRP material and the displacement in the direction perpendicular to the surface of the taper portion of the collar. An angle equivalent to the balanced angle is set.
  • the metal collar can be inserted into the through hole without scraping the adhesive out of the pilot hole (through hole) provided in the CFRP material, and the outer periphery of the metal collar and the through hole of the CFRP material can be inserted. It can suppress that an inner peripheral surface contacts electrically. Further, by setting the inclination angles of the tapered portion and the contact portion as described above, the vertical distance between the taper portion surface and the contact portion surface is kept constant even when the temperature changes. For this reason, it becomes possible to suppress damage to the adhesive layer due to the adhesive due to deformation due to the difference in thermal expansion or contraction between the CFRP material and the metal collar.
  • the metal collar can be prevented from being in electrical contact with the outer periphery of the metal collar and the inner peripheral surface of the pilot hole provided in the CFRP material. Color electroerosion can be suppressed.
  • FIG. 1 is a cross-sectional view showing a fastening structure of a CFRP material according to an embodiment of the present invention.
  • FIG. 2 is a partially enlarged view of a CFRP material fastening structure according to an embodiment of the present invention.
  • the CFRP material 10 shown in FIG. 1 is formed in a flat plate shape, but the entire CFRP material 10 may not be formed in a flat plate shape, and at least a fastening portion with the article 11 to be fastened is formed in a flat plate shape. Just do it.
  • the upper surface 10a in the drawing is referred to as “front surface” for the sake of convenience
  • the lower surface 10b in the drawing is referred to as “back surface” for the sake of convenience.
  • These “front surface” and “back surface” do not specify the direction of the collar 14 fixed to the CFRP material 10 but indicate one of the surfaces.
  • the fastening structure of the CFRP material 10 fastens the CFRP material 10 that is a fastening object and the article 11 to be fastened using a fastener (bolt 12 in this embodiment).
  • a fastener bolt 12 in this embodiment.
  • the CFRP material 10 is formed with a through hole (prepared hole) 13 that penetrates the front surface 10a and the back surface 10b, and the through hole 13 is made of metal.
  • a collar (metal color) 14 is inserted and attached.
  • the bolt 12 is inserted inward of the collar 14 with the object 11 to be fastened on the collar 14, and then the bolt 12 is screwed into a bolt hole 15 provided in the object 11 to be fastened with the CFRP material 10 and the object to be fastened.
  • the fastener 11 is fastened.
  • the CFRP material 10 can be applied to vehicle components such as a hood (bonnet), a door panel, a bumper, a trunk lid, a rear gate, a fender panel, a side body panel, and a roof panel. Moreover, the CFRP material 10 is not limited to the structural member for vehicles, but can be applied to various structural members.
  • the CFRP material 10 can be molded using a known method such as a hot press molding method or an autoclave molding method. Specifically, for example, a prepreg in which a fiber material is impregnated in advance with a matrix resin is prepared for each layer, and a predetermined number of the prepregs cut into a predetermined shape are stacked, and pressed and heated in a heating press or an autoclave. The CFRP material 10 is formed by heating. Further, the CFRP material 10 may be molded by a method (resin transfer molding method) in which a fiber preform in which each fiber material is arranged in a predetermined orientation direction is sealed in a mold and a matrix resin is injected under pressure into the mold. Good.
  • a method resin transfer molding method
  • the matrix resin is not particularly limited, and examples thereof include known thermosetting resins such as epoxy resins, phenol resins, unsaturated polyester resins, vinyl ester resins, polyimide resins, polycarbonate resins, polyamide resins, polyphenylene sulfide (PPS) resins, and the like.
  • a thermoplastic resin can be used.
  • the carbon fiber which comprises the said fiber material is not specifically limited, For example, a PAN-type carbon fiber, a pitch-type carbon fiber, and a rayon-type carbon fiber can be used.
  • the inner periphery of the metal collar 14 has a bolt insertion hole 16 into which the bolt 12 can be inserted. Further, the outer periphery of the metal collar 14 has a tapered portion 17 that is inclined with respect to the central axis CL of the collar 14. That is, the collar 14 is set to have a tapered shape with different outer diameters at one end portion and the other end portion in the central axis CL direction.
  • the collar 14 is formed in a truncated cone shape or a truncated pyramid shape as a whole, and has a first flat surface portion 18 with which the fastened object 11 abuts at a small diameter side end portion and a bolt 12 at a large diameter side end portion.
  • abuts is formed.
  • the inner peripheral surface of the through-hole 13 of the CFRP material 10 has an abutting portion 21 that abuts against the tapered portion 17 of the collar 14 via an adhesive 20 having electrical insulation. That is, the through-hole 13 is set in a tapered shape having different inner diameters at the end on the front surface 10a side and the end on the back surface 10b side of the CFRP material 10.
  • the contact portion 21 (through hole 13) of the CFRP material 10 is formed as a conical or pyramid-shaped hole as a whole, and between the contact portion 21 of the CFRP material 10 and the tapered portion 17 of the collar 14, The adhesive layer by the adhesive 20 is interposed over the entire circumference.
  • the end portion (small diameter side end portion) of the collar 14 on the fastened object 11 side faces the fastened object 11 on the front surface 10a or the back surface 10b of the CFRP material 10.
  • the object to be fastened 11 is disposed away from the CFRP material 10 by projecting toward the fastened object 11 from the surface and bringing the fastened object 11 into contact with the end of the protruding collar 14. Yes. That is, an appropriate gap 22 is provided between the CFRP material 10 and the fastened object 11 so that the CFRP material 10 and the fastened object 11 do not interfere when the CFRP material 10 is thermally expanded in the thickness direction. It has been.
  • taper portion 17 of the collar 14 and the contact portion 21 of the CFRP material 10 gradually increase in the radial direction perpendicular to the central axis CL as the distance from the fastened object 11 side increases in the cross section passing through the central axis CL of the collar 14. It is formed in a divergent shape that becomes larger.
  • the adhesive 20 only needs to have electrical insulation, and for example, an epoxy resin adhesive or a urethane resin adhesive can be used.
  • the adhesive 20 may be a thermosetting adhesive or a thermoplastic adhesive.
  • the material of the fastened object 11 is not particularly limited, and a metal material, a resin material, or the like can be used.
  • the material of the bolt 12 (fastener) is not particularly limited, and a metal material, a resin material, or the like can be used.
  • the fastener used to fasten the CFRP material 10 and the article to be fastened 11 is not limited to the bolt 12, and for example, a combination of a bolt and a nut, a pin, a rivet, a tapping bolt, a stud bolt, or the like may be used. it can.
  • the displacement in the direction perpendicular to the surface of the contact portion 21 of the CFRP material 10 and the displacement in the direction perpendicular to the surface of the tapered portion 17 of the collar 14 due to thermal deformation (thermal expansion or contraction) due to temperature change is expressed by the following equation (1).
  • the vertical distance between the surface of the tapered portion 17 and the surface of the contact portion 21 (the thickness of the adhesive layer by the adhesive 20) is kept constant even when the temperature changes. It is.
  • ⁇ ct is the thermal expansion coefficient in the direction perpendicular to the CFRP material (out-of-plane direction)
  • ⁇ cl is the thermal expansion coefficient in the in-plane direction of the CFRP material
  • ⁇ m is the thermal expansion of the collar. Is a change in temperature
  • ⁇ is an inclination angle of the tapered portion.
  • the “in-plane direction” and “out-of-plane direction” refer to a direction perpendicular to the front surface 10a or the back surface 10b of the CFRP material 10, and the “in-plane direction” refers to the in-plane direction (out-of-plane direction). The direction perpendicular to it.
  • thermal expansion coefficient ⁇ m of the collar 14 a catalog value or a measured value of the thermal expansion coefficient of the metal material constituting the collar 14 can be used. Further, as the thermal expansion coefficients ⁇ ct and ⁇ cl of the CFRP material 10, a catalog value or a measured value of the thermal expansion coefficient of the CFRP constituting the CFRP material 10 can be used. If there is no useful catalog value or the like, the thermal expansion coefficient ⁇ ct of the CFRP constituting the CFRP material 10 can be substituted with the catalog value of the resin material constituting the CFRP material 10.
  • the vertical distance between the surface of the taper portion 17 and the surface of the contact portion 21 is as follows. It remains constant as the temperature changes. For this reason, it becomes possible to suppress that the adhesive bond layer by the adhesive 20 is damaged by the deformation
  • the inclination angle of the taper portion 17 and the inclination angle of the contact portion 21 are set to be equal to each other. Further, the inclination angles of the taper portion 17 and the contact portion 21 are set to an angle equivalent to the angle ⁇ satisfying the expression (1) or (2).
  • the inclination angle of the taper portion 17 and the contact portion 21 is determined by the displacement (D1 + D2) in the direction perpendicular to the surface of the contact portion 21 of the CFRP material 10 due to thermal deformation accompanying temperature change and the surface of the taper portion 17 of the collar 14. Is set to an angle equivalent to the angle ⁇ that balances the displacement D3 in the direction perpendicular to.
  • the inclination angle of the taper portion 17 and the contact portion 21 is set to an angle (acute angle) equal to or less than the angle ⁇ satisfying the above-described formula (1) or (2).
  • the CFRP is larger than the case of setting the angle (obtuse angle) larger than the angle ⁇ satisfying the above formula (1) or (2).
  • the relative displacement due to the temperature change between the material 10 and the metal collar 14 is reduced, and the adhesive layer formed by the adhesive 20 is more difficult to break.
  • the outer periphery of the metal collar 14 has a tapered portion 17 that is inclined with respect to the central axis CL of the collar 14.
  • the inner peripheral surface of the through-hole 13 in the CFRP material 10 has an abutting portion 21 that abuts against the tapered portion 17 of the collar 14 via an adhesive 20 having electrical insulation.
  • the inclination angle of the taper portion 17 of the collar 14 and the contact portion 21 of the CFRP material 10 is determined by the displacement in the direction perpendicular to the surface of the contact portion 21 of the CFRP material 10 due to thermal deformation accompanying temperature change and the surface of the taper portion 17 of the collar 14. It is set to an angle equivalent to the angle that balances the displacement in the direction perpendicular to.
  • the metal collar 14 can be inserted into the through-hole 13 without scraping the adhesive 20 out of the pilot hole (through-hole 13) provided in the CFRP material 10. It can suppress that the inner peripheral surface of the through-hole 13 of the CFRP material 10 contacts electrically. Further, by setting the inclination angles of the taper portion 17 and the contact portion 21 as described above, the vertical distance between the surface of the taper portion 17 and the contact portion 21 surface is kept constant even if the temperature changes. Be drunk. For this reason, it becomes possible to suppress that the adhesive bond layer by the adhesive 20 is damaged by the deformation
  • the taper portion 17 of the collar 14 and the contact portion 21 of the CFRP material 10 have a radial distance orthogonal to the central axis CL as the distance from the fastened object 11 side increases in the cross section passing through the central axis CL of the collar 14. It is formed in a divergent shape that gradually increases.
  • the metal collar 14 can be prevented from dropping from the CFRP material 10 together with the article 11 to be fastened.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Connection Of Plates (AREA)
  • Bolts, Nuts, And Washers (AREA)

Abstract

　金属製のカラー（１４）の外周は、カラー（１４）の中心軸（ＣＬ）に対して傾斜するテーパー部（１７）を有する。炭素繊維強化樹脂（以下、「ＣＦＲＰ」と称する）材（１０）における貫通孔（１３）の内周面は、電気的絶縁性を有する接着剤（２０）を介してカラー（１４）のテーパー部（１７）と当接する当接部（２１）を有する。カラー（１４）のテーパー部（１７）およびＣＦＲＰ材（１０）の当接部（２１）の傾斜角度は、温度変化に伴う熱変形によるＣＦＲＰ材（１０）の当接部（２１）表面に垂直な方向の変位とカラー（１４）のテーパー部（１７）表面に垂直な方向の変位とが釣り合う角度と同等の角度に設定される。

Description

炭素繊維強化樹脂材の締結構造
　本発明は、炭素繊維強化樹脂（以下、「ＣＦＲＰ」と称する）材の締結構造に関する。
　従来から、締結具を用いてＣＦＲＰ材と被締結物とを締結するＣＦＲＰ材の締結構造が公知である（例えば、特許文献１参照）。特許文献１には、ボルトおよびナットを用いてＣＦＲＰ材とブラケットとを締結する技術が開示されている。
　ＣＦＲＰを構成する樹脂はクリープ変形する性質を有するので、高強度のボルトを締結具として使用する場合、金属製のカラーをＣＦＲＰ材に装着して、ボルトの軸力を金属製のカラーで受けるようにすることがある。このようにすることにより、経時的にＣＦＲＰ材を構成する樹脂材にクリープ変形などによる肉痩せが生じてボルトの軸力が低下して、ボルトのゆるみが発生することを抑制することができる。
　このような締結構造では、液体（例えば、雨水や海水など）がＣＦＲＰ材と金属製のカラーとの間の隙間に浸入し、ＣＦＲＰ材と金属製のカラーとが接触している部分に液体が付着した場合に、金属製のカラーが電食し腐食が発生する可能性がある。このため、例えば、電気的絶縁性を有する接着剤を、金属製のカラ－を装着するＣＦＲＰ材の下穴の内周面に塗布し、ＣＦＲＰ材と金属製のカラーとを電気的に絶縁しておくことが好ましい。
特開２００７－２９２１０６号公報
　しかしながら、前述の締結構造では、金属製のカラーをＣＦＲＰ材に設けた下穴に挿入する際に、カラーの角部によって、接着剤が下穴の外へ掻き出され、金属製のカラーの外周とＣＦＲＰ材に設けた下穴の内周面とが電気的に接触する可能性があるという問題があった。
　そこで、本発明は、金属製のカラーの外周とＣＦＲＰ材に設けた下穴の内周面とが電気的に接触することを抑制することにより、金属製のカラーの電食を抑制することができるＣＦＲＰ材の締結構造を提供することを目的とする。
　本発明に係るＣＦＲＰ材の締結構造では、金属製のカラーの外周は、カラーの中心軸に対して傾斜するテーパー部を有し、ＣＦＲＰ材における貫通孔の内周面は、電気的絶縁性を有する接着剤を介してカラーのテーパー部と当接する当接部を有する。カラーのテーパー部およびＣＦＲＰ材の当接部の傾斜角度は、温度変化に伴う熱変形によるＣＦＲＰ材の当接部表面に垂直な方向の変位とカラーのテーパー部表面に垂直な方向の変位とが釣り合う角度と同等の角度に設定される。
　接着剤をＣＦＲＰ材に設けた下穴（貫通孔）の外へ掻き出さずに金属製のカラーを貫通孔に挿入することが可能になり、金属製のカラーの外周とＣＦＲＰ材の貫通孔の内周面とが電気的に接触することを抑制することができる。また、前述のようにテーパー部および当接部の傾斜角度を設定することにより、テーパー部表面と当接部表面との間の垂直間距離は温度が変化しても一定に保たれる。このため、ＣＦＲＰ材と金属製のカラーとの熱膨張差または熱収縮差による変形に起因して接着剤による接着剤層が破損することを抑制することが可能になる。従って、本発明に係るＣＦＲＰ材の締結構造によれば、金属製のカラーの外周とＣＦＲＰ材に設けた下穴の内周面とが電気的に接触することを抑制することにより、金属製のカラーの電食を抑制することができる。
図１は、本発明の実施形態に係るＣＦＲＰ材の締結構造を示す断面図である。 図２は、本発明の実施形態に係るＣＦＲＰ材の締結構造の部分拡大図である。
　以下、本発明の実施形態を図面とともに詳述する。
　本発明の実施形態に係るＣＦＲＰ材１０の締結構造を図１および図２に基づいて説明する。
　図１に示すＣＦＲＰ材１０は、平板状に形成されているが、ＣＦＲＰ材１０全体が平板状に形成されていなくてもよく、少なくとも被締結物１１との締結部が平板状に形成されていればよい。また、ＣＦＲＰ材１０の図中の上下両面のうち図中上側の面１０ａを便宜的に「表面」と称し、図中下側の面１０ｂを便宜的に「裏面」と称する。これらの「表面」および「裏面」は、ＣＦＲＰ材１０に固定されるカラー１４の向きを特定するものではなく、いずれか一方の面を示すものである。
　図１に示すように、本実施形態に係るＣＦＲＰ材１０の締結構造は、締結物であるＣＦＲＰ材１０と被締結物１１とを締結具（本実施形態では、ボルト１２）を用いて締結するものである。本実施形態に係るＣＦＲＰ材１０の締結構造では、ＣＦＲＰ材１０に表面１０ａと裏面１０ｂとを貫通する貫通孔（下穴）１３を形成し、貫通孔１３に筒状に形成された金属製のカラー（金属カラー）１４を挿入して装着する。そして、カラー１４に被締結物１１を重ね合わせた状態でカラー１４の内方にボルト１２を挿入したのちボルト１２を被締結物１１に設けたボルト孔１５にねじ込むことによって、ＣＦＲＰ材１０と被締結物１１とを締結する。
　ＣＦＲＰ材１０は、例えば、フード（ボンネット）、ドアパネル、バンパー、トランクリッド、リアゲート、フェンダパネル、サイドボディパネル、ルーフパネルなど車両用構成部材に適用することができる。また、ＣＦＲＰ材１０は、車両用構成部材に限定されず、各種構成部材に適用することが可能である。
　ＣＦＲＰ材１０は、ホットプレス成形法やオートクレーブ成形法など公知の方法を用いて成形することができる。具体的には、例えば、各層ごとに予めマトリックス樹脂を繊維材に含浸させたプリプレグを用意し、このプリプレグを所定形状に裁断したものを所定枚数積層して、加熱プレスやオートクレーブ内で加圧および加熱することでＣＦＲＰ材１０を成形する。また、各繊維材を所定の配向方向で配列した繊維プリフォームを金型に封入し、金型内にマトリックス樹脂を加圧注入する方法（レジントランスファー成形法）でＣＦＲＰ材１０を成形してもよい。
　前記マトリックス樹脂は、特に限定されず、例えば、エポキシ樹脂、フェノール樹脂、不飽和ポリエステル樹脂、ビニルエステル樹脂、ポリイミド樹脂、ポリカーボネート樹脂、ポリアミド樹脂、ポリフェニレンスルフィド（ＰＰＳ）樹脂など公知の熱硬化性樹脂や熱可塑性樹脂を用いることができる。また、前記繊維材を構成する炭素繊維は、特に限定されず、例えば、ＰＡＮ系炭素繊維、ピッチ系炭素繊維、レーヨン系炭素繊維を用いることができる。
　金属製のカラー１４の内周は、ボルト１２を挿通可能なボルト挿通孔１６を有する。また、金属製のカラー１４の外周は、カラー１４の中心軸ＣＬに対して傾斜するテーパー部１７を有する。つまり、カラー１４は、中心軸ＣＬ方向の一方側の端部と他方側の端部とで外径が異なるテーパー形状に設定されている。カラー１４は、全体としては円錐台形状または角錐台形状に形成され、小径側端部に被締結物１１が当接する第１平面部１８が形成されていると共に、大径側端部にボルト１２の頭部が当接する第２平面部１９が形成されている。
　一方、ＣＦＲＰ材１０の貫通孔１３の内周面は、電気的絶縁性を有する接着剤２０を介してカラー１４のテーパー部１７と当接する当接部２１を有する。つまり、貫通孔１３は、ＣＦＲＰ材１０の表面１０ａ側の端部と裏面１０ｂ側の端部とで内径が異なるテーパー形状に設定されている。ＣＦＲＰ材１０の当接部２１（貫通孔１３）は、全体としては円錐形状または角錐形状の穴に形成され、ＣＦＲＰ材１０の当接部２１とカラー１４のテーパー部１７との間には、全周に亘って接着剤２０による接着剤層が介在している。
　本実施形態に係るＣＦＲＰ材１０の締結構造では、カラー１４における被締結物１１側の端部（小径側端部）を、ＣＦＲＰ材１０の表面１０ａまたは裏面１０ｂのうち被締結物１１に対向した面よりも被締結物１１側に向けて突出させると共に、この突出したカラー１４の端部に被締結物１１を当接させることにより、被締結物１１をＣＦＲＰ材１０から離間させて配置している。つまり、ＣＦＲＰ材１０と被締結物１１との間には、ＣＦＲＰ材１０が厚さ方向に熱膨張した場合にＣＦＲＰ材１０と被締結物１１とが干渉しないように、適度な隙間２２が設けられている。また、カラー１４のテーパー部１７およびＣＦＲＰ材１０の当接部２１は、カラー１４の中心軸ＣＬを通る断面において、被締結物１１側から離れるに従って中心軸ＣＬに直交する径方向の距離が徐々に大きくなる末広がり形状に形成されている。
　前記接着剤２０は、電気的絶縁性を有するものであればよく、例えば、エポキシ樹脂系接着剤、ウレタン樹脂系接着剤を用いることができる。また、この接着剤２０は、熱硬化性の接着剤であってもよく、熱可塑性の接着剤であってもよい。
　被締結物１１の材質は、特に限定されず、金属材料や樹脂材料などを用いることができる。ボルト１２（締結具）の材質も、特に限定されず、金属材料や樹脂材料などを用いることができる。また、ＣＦＲＰ材１０と被締結物１１とを締結するのに用いる締結具は、ボルト１２に限定されず、例えば、ボルトおよびナットの組み合わせ、ピン、リベット、タッピングボルト、スタッドボルトなどを用いることもできる。
　次に、カラー１４のテーパー部１７およびＣＦＲＰ材１０の当接部２１のカラー１４の中心軸ＣＬに対する傾斜角度（テーパー角度）を決定する方法を図２に基づいて説明する。なお、図２では、接着剤２０による接着剤層は、図示の簡略化のために省略されている。
　温度変化に伴う熱変形（熱膨張または熱収縮）によるＣＦＲＰ材１０の当接部２１表面に垂直な方向の変位とカラー１４のテーパー部１７表面に垂直な方向の変位とが以下の式（１）に示す関係を満たす場合に、温度が変化しても、テーパー部１７表面と当接部２１表面との間の垂直間距離（接着剤２０による接着剤層の厚さ）が一定に保たれる。
　（εｃｔｓｉｎθ+εｃｌｃｏｓθ）ｔ＝εｍｔ　・・・（１）
　式（１）中、εｃｔはＣＦＲＰ材の面直方向（面外方向）の熱膨張率であり、εｃｌはＣＦＲＰ材の面内方向の熱膨張率であり、εｍはカラーの熱膨張率であり、ｔは温度変化であり、θはテーパー部の傾斜角度である。
　ここで、「面直方向」および「面外方向」とは、ＣＦＲＰ材１０の表面１０ａまたは裏面１０ｂに垂直な方向をいい、「面内方向」とは、面直方向（面外方向）に対して垂直な方向をいう。
　前記の式（１）から、以下の式（２）が導き出される。
　εｃｔｓｉｎθ+εｃｌｃｏｓθ＝εｍ　・・・（２）
　この式（２）は、前記の式（１）の両辺を温度変化ｔで除したものである。
　カラー１４の熱膨張率εｍは、カラー１４を構成する金属材料の熱膨張率のカタログ値または測定値を用いることができる。また、ＣＦＲＰ材１０の熱膨張率εｃｔ、εｃｌは、ＣＦＲＰ材１０を構成するＣＦＲＰの熱膨張率のカタログ値または測定値を用いることができる。ＣＦＲＰ材１０を構成するＣＦＲＰの面直方向の熱膨張率εｃｔは、有用なカタログ値などがない場合には、ＣＦＲＰ材１０を構成する樹脂材料のカタログ値で代用することができる。
　テーパー部１７および当接部２１の傾斜角度を前記の式（１）または（２）を満たす角度θに設定することにより、テーパー部１７表面と当接部２１表面との間の垂直間距離は温度が変化しても一定に保たれる。このため、ＣＦＲＰ材１０と金属製のカラー１４との熱膨張差または熱収縮差による変形に起因して接着剤２０による接着剤層が破損することを抑制することが可能になる。
　テーパー部１７の傾斜角度と、当接部２１の傾斜角度とは、互いに等しい角度に設定される。また、テーパー部１７および当接部２１の傾斜角度は、前記の式（１）または（２）を満たす角度θと同等の角度に設定される。
　換言すれば、テーパー部１７および当接部２１の傾斜角度は、温度変化に伴う熱変形によるＣＦＲＰ材１０の当接部２１表面に垂直な方向の変位（Ｄ１＋Ｄ２）とカラー１４のテーパー部１７表面に垂直な方向の変位Ｄ３とが釣り合う角度θと同等の角度に設定される。
　より好ましくは、テーパー部１７および当接部２１の傾斜角度は、前記の式（１）または（２）を満たす角度θ以下の角度（鋭角）に設定される。このような角度にテーパー部１７および当接部２１の傾斜角度を設定することにより、前記の式（１）または（２）を満たす角度θよりも大きい角度（鈍角）に設定した場合よりもＣＦＲＰ材１０と金属製のカラー１４との温度変化による相対変位が小さくなり、接着剤２０による接着剤層がより破損しにくくなる。
　以下に、本実施形態による作用効果を説明する。
　（１）本実施形態に係るＣＦＲＰ材１０の締結構造では、金属製のカラー１４の外周は、カラー１４の中心軸ＣＬに対して傾斜するテーパー部１７を有する。ＣＦＲＰ材１０における貫通孔１３の内周面は、電気的絶縁性を有する接着剤２０を介してカラー１４のテーパー部１７と当接する当接部２１を有する。カラー１４のテーパー部１７およびＣＦＲＰ材１０の当接部２１の傾斜角度は、温度変化に伴う熱変形によるＣＦＲＰ材１０の当接部２１表面に垂直な方向の変位とカラー１４のテーパー部１７表面に垂直な方向の変位とが釣り合う角度と同等の角度に設定される。
　接着剤２０をＣＦＲＰ材１０に設けた下穴（貫通孔１３）の外へ掻き出さずに金属製のカラー１４を貫通孔１３に挿入することが可能になり、金属製のカラー１４の外周とＣＦＲＰ材１０の貫通孔１３の内周面とが電気的に接触することを抑制することができる。また、前述のようにテーパー部１７および当接部２１の傾斜角度を設定することにより、テーパー部１７表面と当接部２１表面との間の垂直間距離は温度が変化しても一定に保たれる。このため、ＣＦＲＰ材１０と金属製のカラー１４との熱膨張差または熱収縮差による変形に起因して接着剤２０による接着剤層が破損することを抑制することが可能になる。従って、本実施形態に係るＣＦＲＰ材１０の締結構造によれば、金属製のカラー１４の外周とＣＦＲＰ材１０の貫通孔１３の内周面とが電気的に接触することを抑制することにより、金属製のカラー１４の電食を抑制することができる。
　（２）カラー１４における被締結物１１側の端部を、ＣＦＲＰ材１０の表面１０ａまたは裏面１０ｂのうち被締結物１１に対向した面よりも被締結物１１側に向けて突出させると共に、この突出したカラー１４の端部に被締結物１１を当接させることにより、被締結物１１をＣＦＲＰ材１０から離間させて配置した。
　締結物であるＣＦＲＰ材１０と被締結物１１との間に隙間２２があるので、ＣＦＲＰ材１０が厚さ方向に熱膨張した場合であっても、ＣＦＲＰ材１０と被締結物１１とが干渉することを抑制することができる。
　（３）カラー１４のテーパー部１７およびＣＦＲＰ材１０の当接部２１は、カラー１４の中心軸ＣＬを通る断面において、被締結物１１側から離れるに従って中心軸ＣＬに直交する径方向の距離が徐々に大きくなる末広がり形状に形成されている。
　例えば接着剤２０による接着強度が低下した場合であっても、金属製のカラー１４が被締結物１１と共にＣＦＲＰ材１０から脱落することを防止することができる。
　以上、実施例に沿って本発明の内容を説明したが、本発明はこれらの記載に限定されるものではなく、種々の変形及び改良が可能であることは、当業者には自明である。
１０　ＣＦＲＰ材（炭素繊維強化樹脂材）
１１　被締結物
１２　ボルト（締結具）
１３　貫通孔
１４　カラー
１７　テーパー部
２０　接着剤
２１　当接部

Claims (3)

  1. 　締結物である炭素繊維強化樹脂材に表面と裏面とを貫通する貫通孔を形成し、この貫通孔に筒状に形成された金属製のカラーを挿入して装着し、このカラーに被締結物を重ね合わせた状態で前記カラーの内方に締結具を挿入したのち締結具を締め付けることによって、前記炭素繊維強化樹脂材と前記被締結物とを締結する炭素繊維強化樹脂材の締結構造であって、
    　前記金属製のカラーの外周は、前記カラーの中心軸に対して傾斜するテーパー部を有し、
    　前記炭素繊維強化樹脂材における前記貫通孔の内周面は、電気的絶縁性を有する接着剤を介して前記カラーのテーパー部と当接する当接部を有し、
    　前記カラーのテーパー部および前記炭素繊維強化樹脂材の当接部の傾斜角度は、温度変化に伴う熱変形による前記炭素繊維強化樹脂材の当接部表面に垂直な方向の変位と前記カラーのテーパー部表面に垂直な方向の変位とが釣り合う角度と同等の角度に設定される
    　ことを特徴とする炭素繊維強化樹脂材の締結構造。
  2. 　前記カラーにおける前記被締結物側の端部を、前記炭素繊維強化樹脂材の前記表面または裏面のうち前記被締結物に対向した面よりも前記被締結物側に向けて突出させると共に、この突出したカラーの端部に前記被締結物を当接させることにより、前記被締結物を前記炭素繊維強化樹脂材から離間させて配置したことを特徴とする請求項１に記載の炭素繊維強化樹脂材の締結構造。
  3. 　前記カラーのテーパー部および前記炭素繊維強化樹脂材の当接部は、前記カラーの中心軸を通る断面において、前記被締結物側から離れるに従って前記中心軸に直交する径方向の距離が徐々に大きくなる末広がり形状に形成されていることを特徴とする請求項１または２に記載の炭素繊維強化樹脂材の締結構造。
PCT/JP2015/051608 2015-01-22 2015-01-22 炭素繊維強化樹脂材の締結構造 WO2016117062A1 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
CN201580074086.5A CN107208678B (zh) 2015-01-22 2015-01-22 碳纤维强化树脂材料的紧固构造
JP2016570405A JP6332475B2 (ja) 2015-01-22 2015-01-22 炭素繊維強化樹脂材の締結構造
PCT/JP2015/051608 WO2016117062A1 (ja) 2015-01-22 2015-01-22 炭素繊維強化樹脂材の締結構造
US15/539,766 US10132342B2 (en) 2015-01-22 2015-01-22 Fastening structure for carbon fiber-reinforced resin material
EP15878757.2A EP3249242B1 (en) 2015-01-22 2015-01-22 Fastening structure for carbon fiber-reinforced resin material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2015/051608 WO2016117062A1 (ja) 2015-01-22 2015-01-22 炭素繊維強化樹脂材の締結構造

Publications (1)

Publication Number Publication Date
WO2016117062A1 true WO2016117062A1 (ja) 2016-07-28

Family

ID=56416628

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2015/051608 WO2016117062A1 (ja) 2015-01-22 2015-01-22 炭素繊維強化樹脂材の締結構造

Country Status (5)

Country Link
US (1) US10132342B2 (ja)
EP (1) EP3249242B1 (ja)
JP (1) JP6332475B2 (ja)
CN (1) CN107208678B (ja)
WO (1) WO2016117062A1 (ja)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019009042A1 (ja) * 2017-07-04 2019-01-10 住友電装株式会社 端子台
JP2019190390A (ja) * 2018-04-26 2019-10-31 トヨタ自動車株式会社 プロテクタ
JP2019190392A (ja) * 2018-04-26 2019-10-31 トヨタ自動車株式会社 プロテクタ及びプロテクタ製造方法
WO2020202461A1 (ja) 2019-04-02 2020-10-08 日本製鉄株式会社 金属－炭素繊維強化樹脂材料複合体および金属－炭素繊維強化樹脂材料複合体の製造方法
WO2020202457A1 (ja) 2019-04-02 2020-10-08 日本製鉄株式会社 金属－炭素繊維強化樹脂材料複合体

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9932831B2 (en) * 2014-05-09 2018-04-03 United Technologies Corporation High temperature compliant metallic elements for low contact stress ceramic support
US11287223B2 (en) * 2017-09-30 2022-03-29 Robert E. Stewart Mounting and fastening system mounting adapter
US11047417B2 (en) 2018-10-11 2021-06-29 GM Global Technology Operations LLC Fastening assembly
DE102018125979A1 (de) * 2018-10-19 2020-04-23 Airbus Operations Gmbh Verfahren und System zum Verbinden zweier Bauteile
US10816583B2 (en) * 2018-11-28 2020-10-27 The Boeing Company Differential capacitive probe for measuring contact resistance

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03272828A (ja) * 1990-03-23 1991-12-04 Honda Motor Co Ltd 繊維強化複合材の圧縮締結部構造
JPH11223164A (ja) * 1998-02-05 1999-08-17 Honda Motor Co Ltd 樹脂製部材の締結構造
WO2007142354A1 (ja) * 2006-06-09 2007-12-13 Mitsubishi Heavy Industries, Ltd. ファスナ
JP2011133009A (ja) * 2009-12-24 2011-07-07 Across Corp 円錐面を備えたファスナー

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US860829A (en) * 1906-03-29 1907-07-23 Oscar A R M Schmidt Razor.
US4650385A (en) 1983-05-17 1987-03-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Daze fasteners
US4512699A (en) * 1983-05-17 1985-04-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Daze fasteners
IT1222810B (it) * 1987-10-02 1990-09-12 Nuovi Pignone Ind Meccaniche E Perno smontabile per l'accoppiamento ruotabile di due elementi di ridotto ingombro assiale,particolarmente adatto per i leverismi delle macchine tessili
US5022805A (en) 1989-02-16 1991-06-11 Rolls-Royce Incorporated Cantilever mounting system for structural members having dissimilar coefficients of thermal expansion
CN1174175C (zh) * 1997-08-27 2004-11-03 株式会社日立制作所 螺纹连接构造及螺纹连接方法
JP2002036286A (ja) * 2000-07-26 2002-02-05 Denso Corp インサート金具および樹脂成形品の取付構造
GB2380236B (en) * 2001-09-29 2005-01-19 Rolls Royce Plc A wall structure for a combustion chamber of a gas turbine engine
US7153054B2 (en) * 2004-05-20 2006-12-26 United Technologies Corporation Fastener assembly for attaching a non-metal component to a metal component
US7261489B2 (en) * 2004-05-20 2007-08-28 United Technologies Corporation Fastener assembly for attaching a non-metal component to a metal component
WO2007025687A1 (de) * 2005-08-30 2007-03-08 Richard Bergner Verbindungstechnik Gmbh & Co Kg Befestigungsvorrichtung
JP2007292106A (ja) 2006-04-21 2007-11-08 Toyota Motor Corp 炭素繊維強化樹脂材の結合構造
JP2007332980A (ja) * 2006-06-12 2007-12-27 Toyota Motor Corp フランジ付カラーナットを含む締結構造体
JP4730217B2 (ja) 2006-06-12 2011-07-20 トヨタ自動車株式会社 フランジ付カラーを含む締結構造体
DE102007041949B3 (de) * 2007-09-04 2009-06-10 Böllhoff Verbindungstechnik GmbH Befestiger
DE102008037155A1 (de) * 2008-08-08 2010-02-11 Fischerwerke Gmbh & Co. Kg Lastdämpfer für einen Anker
DE102009035785A1 (de) * 2009-08-01 2010-03-25 Daimler Ag Verbindungsanordnung eines Verkleidungsteils an einem Trägerteil im Innenraum eines Kraftwagens
JP5713980B2 (ja) * 2012-10-15 2015-05-07 三菱航空機株式会社 耐雷ファスナおよび航空機
DE102012112867B4 (de) * 2012-12-21 2014-08-14 Deutsches Zentrum für Luft- und Raumfahrt e.V. Befestigungsanordnung für Bauteile mit unterschiedlichen thermischen Ausdehnungskoeffizienten
FR3006394B1 (fr) * 2013-05-28 2015-06-19 Herakles Assemblage a liaison auto-serrante en temperature
PT2990178T (pt) * 2014-08-29 2019-04-03 Helmholtz Zentrum Geesthacht Método para unir uma peça de trabalho de plástico a outra peça de trabalho
US10093221B2 (en) * 2015-07-07 2018-10-09 Burton Technologies, Llc Light module fastening assembly having a snap wedge assembly with ball stud and insert
FR3038942B1 (fr) * 2015-07-17 2018-03-02 Safran Ceramics Assemblage par liaison mecanique comportant au moins une piece en materiau composite
JP6260592B2 (ja) * 2015-07-24 2018-01-17 トヨタ自動車株式会社 異種材接合構造及び異種材接合体の製造方法

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03272828A (ja) * 1990-03-23 1991-12-04 Honda Motor Co Ltd 繊維強化複合材の圧縮締結部構造
JPH11223164A (ja) * 1998-02-05 1999-08-17 Honda Motor Co Ltd 樹脂製部材の締結構造
WO2007142354A1 (ja) * 2006-06-09 2007-12-13 Mitsubishi Heavy Industries, Ltd. ファスナ
JP2011133009A (ja) * 2009-12-24 2011-07-07 Across Corp 円錐面を備えたファスナー

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019009042A1 (ja) * 2017-07-04 2019-01-10 住友電装株式会社 端子台
JP2019016447A (ja) * 2017-07-04 2019-01-31 住友電装株式会社 端子台
US11221032B2 (en) 2017-07-04 2022-01-11 Sumitomo Wiring Systems, Ltd. Terminal block
JP2019190390A (ja) * 2018-04-26 2019-10-31 トヨタ自動車株式会社 プロテクタ
JP2019190392A (ja) * 2018-04-26 2019-10-31 トヨタ自動車株式会社 プロテクタ及びプロテクタ製造方法
CN110410250A (zh) * 2018-04-26 2019-11-05 丰田自动车株式会社 保护器及保护器的制造方法
CN110410250B (zh) * 2018-04-26 2021-03-16 丰田自动车株式会社 保护器及保护器的制造方法
US10975817B2 (en) * 2018-04-26 2021-04-13 Toyota Jidosha Kabushiki Kaisha Protector and method for manufacturing protector
WO2020202461A1 (ja) 2019-04-02 2020-10-08 日本製鉄株式会社 金属－炭素繊維強化樹脂材料複合体および金属－炭素繊維強化樹脂材料複合体の製造方法
WO2020202457A1 (ja) 2019-04-02 2020-10-08 日本製鉄株式会社 金属－炭素繊維強化樹脂材料複合体
US11667107B2 (en) 2019-04-02 2023-06-06 Nippon Steel Corporation Metal-carbon fiber reinforced resin material composite
US11969969B2 (en) 2019-04-02 2024-04-30 Nippon Steel Corporation Metal-carbon fiber reinforced resin material composite and method for manufacturing metal-carbon fiber reinforced resin material composite

Also Published As

Publication number Publication date
JPWO2016117062A1 (ja) 2017-11-09
JP6332475B2 (ja) 2018-05-30
EP3249242B1 (en) 2019-10-09
US10132342B2 (en) 2018-11-20
EP3249242A4 (en) 2018-03-14
CN107208678A (zh) 2017-09-26
EP3249242A1 (en) 2017-11-29
CN107208678B (zh) 2018-10-30
US20180266463A1 (en) 2018-09-20

Similar Documents

Publication Publication Date Title
JP6332475B2 (ja) 炭素繊維強化樹脂材の締結構造
EP2812248B1 (en) Connecting arrangement and method for providing such connecting arrangement
EP2452086B1 (en) Nut, fastening arrangement and method of fastening
US4817264A (en) Fastener and assembly process
US20150102160A1 (en) Lightning protection fastener and aircraft
US20150322993A1 (en) Apparatus and methods for providing a threaded fixing in a crushable or brittle material
US20060062650A1 (en) Hybrid fastener apparatus and method for fastening
US20120074257A1 (en) Lightning-resistant fastener, cap, and method of mounting lightning-resistant fastener
US20120155987A1 (en) Lightning-resistant fastener and mounting structure of lightning-resistant fastener
JP2009204159A (ja) 部品締結構造
US20050201845A1 (en) Hybrid fastener apparatus and method for fastening
US20230160505A1 (en) Composite connectors and methods of manufacturing the same
EP3361108B1 (en) Load-indicating washer
US20180117959A1 (en) Vehicle wheel
JP5958371B2 (ja) 締結構造
US20090155017A1 (en) Secure composite fastener
CN104482011A (zh) 一种双固锚栓
JP2017082843A (ja) 車両構成部品同士の締結構造
US10590970B2 (en) Plastic component comprising a connecting element
RU2691725C1 (ru) Заклепка и способ получения неразъемного заклепочного соединения в углекомпозитных конструкциях
US9151319B2 (en) Mounting structure
JP2010228337A (ja) 繊維強化プラスチック構造体およびその接続方法
JP2010025177A (ja) 繊維強化プラスチック構造体とその締結構造及び製造方法
US20130284343A1 (en) Method for attaching a headless rivet nut to a sandwich panel
JP2016053594A5 (ja) ノッキングセンサの製造方法

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 15878757

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 2016570405

Country of ref document: JP

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 15539766

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

REEP Request for entry into the european phase

Ref document number: 2015878757

Country of ref document: EP