摘要:
Provided are an adhesive that makes it possible to bond thermoplastic resins to each other in a short time and to obtain excellent adhesive strength, a structure bonded by this adhesive, and a bonding method using this adhesive. The adhesive bonds a first member (11) containing a thermoplastic resin or a thermoplastic resin reinforced by carbon fibers and a second member (12) containing this thermoplastic resin or this thermoplastic resin reinforced by carbon fibers. The adhesive has a thermoplastic resin as the base material and contains a metallic nano material that generates heat by absorbing electromagnetic waves, in this base material.
摘要:
Provided is a method for producing a metal nanocoil, which has excellent mass productivity and is capable of reducing the production cost. This method for producing a metal nanocoil comprises: a step wherein a metal thin film is formed on the surface of a core that is formed of a nanofiber of a polymer in a state where a tension is applied to the core, thereby producing a metal-coated nanofiber; a step wherein the tension applied to the metal-coated nanofiber is relaxed; and a step wherein the metal-coated nanofiber is heated to a temperature that is equal to or higher than the boiling point or the thermal decomposition temperature of the polymer and equal to or lower than the melting point of the metal thin film in a state where the tension is relaxed, so that the core is vaporized and the thin film is shrunk into a coil shape, thereby forming a hollow metal nanocoil.
摘要:
Provided are a method for molding a composite material, whereby the occurrence of temperature unevenness in the composite material during heating is reduced, a composite material, a pressing head, and a device for molding a composite material. The method for molding a composite material has an electroconductive wire-shaped material arranging step and a magnetic field application step. The electroconductive wire-shaped material arranging step comprises arranging, in an unreacted composite material 10 having reinforcing fibers 12, a plurality of electroconductive wire-shaped materials 16 at an interval wider than the interval between the reinforcing fibers 12 along a direction intersecting with the reinforcing fibers 12 in the plane in which the reinforcing fibers 12 are aligned. The magnetic field application step comprises applying a magnetic field 42 in a direction intersecting with the plane in which the reinforcing fibers 12 are aligned.
摘要:
A composite material forming method that reduces the occurrence of temperature unevenness in a composite material during heating is provided. The composite material forming method is a method for forming a composite material 10 including reinforcing fibers 12, and includes an equipotential-material connecting step and a magnetic-field applying step. The equipotential-material connecting step is a step of connecting end portions of the reinforcing fibers 12 with equipotential materials 16 to form an electroconductive loop including the reinforcing fibers 12 in the composite material 10 before reaction. The magnetic-field applying step is a step of applying a magnetic field 42 in a direction intersecting a plane formed by the electroconductive loop.
摘要:
Provided are a crystallinity measurement device, a resin-containing material manufacturing device, a crystallinity measurement method, and a resin-containing material manufacturing method capable of calculating crystallinity easily and accurately even when materials other than crystalline thermoplastic resin are included in addition to crystalline thermoplastic resin. A crystallinity measurement device 10 includes a Raman spectroscopy unit 11 and an analysis unit 13. The Raman spectroscopy unit 11 acquires a Raman spectrum of resin-containing material 1 including crystalline thermoplastic resin. The analysis unit 13 calculates the crystallinity of the crystalline thermoplastic resin based on the intensity of a low-wavenumber spectrum that is a spectrum in a region of less than 600 cm -1 , in the Raman spectrum.
摘要:
Provided are a compression head for reducing the occurrence of temperature unevenness in a composite material during heating, a composite-material molding device, and a composite-material molding method. A compression head 20 is provided on the other side of a pre-reaction composite material 2 from a magnetic field coil 30 provided on one side of the composite material 2, the compression head 20 facing the magnetic field coil 30 via the composite material 2. The compression head 20 has a compression head body 22 and a high-thermal-conductivity-material layer 24. The compression head body 22 is formed from a material that is transparent to a magnetic field 32 applied by the magnetic field coil 30. The high-thermal-conductivity-material layer 24 is formed on the side of the compression head body 22 that faces the composite material 2, and is transparent to the magnetic field 32 applied by the magnetic field coil 30 and is formed from a material having higher thermal conductivity than the composite material 2.
摘要:
There is provided a cap capable of achieving enhanced safety by inhibiting the occurrence of sparks thereinside even if a lightning current has flowed through a fastener, a fastening structure using the same, and an aircraft including the fastening structure. A cap (27) according to the present invention is attached so as to cover a portion of a fastener (15) that couples an upper skin (3) of an aircraft and a stringer (11) located inside the upper skin (3), the portion projecting through the stringer (11), wherein an outer surface (33) of the cap that comes into contact with an interior space of the upper skin (3) is a curved surface, and the cap is made of a conductive material.
摘要:
Provided is a method for bonding composite materials together in which bonding regions are suitably put into a semi-cured state and the composite materials are efficiently bonded together while the quality of the bonding strength of the composite materials is suitably maintained. The method for bonding a first composite material and a second composite material together includes the following respective steps. In step S12, a first bonding region of the first composite material is prepared to be maintained in a softened state. In step S14, a first non-bonding region of the first composite material is heated to be put into a cured state. In step S16, the first bonding region is put into a heatable state. In step S18, the first bonding region is heated to be put into a semi-cured state. In step S32, the first bonding region having been put into the semi-cured state is pressed in contact with a second bonding region of the second composite material that becomes a softened state or a semi-cured state. In step S34, the first bonding region and the second bonding region having been brought into contact with each other and pressed in the contacting and pressing step are heated to be put into a cured state.