METHOD FOR PRODUCING METAL NANOCOIL
    3.
    发明公开
    METHOD FOR PRODUCING METAL NANOCOIL 审中-公开
    生产金属纳米油的方法

    公开(公告)号:EP3257977A1

    公开(公告)日:2017-12-20

    申请号:EP16749233.9

    申请日:2016-02-09

    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.

    摘要翻译: 本发明提供一种批量生产性优异且能够降低制造成本的金属纳米线圈的制造方法。 该金属纳米线圈的制造方法包括:在对芯施加张力的状态下,在由聚合物的纳米纤维形成的芯的表面形成金属薄膜的工序, 涂层纳米纤维; 其中施加于金属涂覆的纳米纤维的张力被松弛的步骤; 以及将金属被覆纳米纤维加热到聚合物的沸点或热分解温度以上的温度且在金属薄膜的熔点以下的状态 松弛张力,使芯部气化并将薄膜收缩成线圈状,由此形成中空的金属纳米线圈。

    COMPRESSION HEAD, COMPOSITE-MATERIAL MOLDING DEVICE, AND COMPOSITE-MATERIAL MOLDING METHOD

    公开(公告)号:EP3733390A1

    公开(公告)日:2020-11-04

    申请号:EP18903832.6

    申请日:2018-12-10

    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.

    CAP, FASTENED STRUCTURE USING SAME, AND AIRCRAFT HAVING SAID FASTENED STRUCTURE
    8.
    发明公开
    CAP, FASTENED STRUCTURE USING SAME, AND AIRCRAFT HAVING SAID FASTENED STRUCTURE 审中-公开
    KAPPE,BEFESTIGTE STRUKTUR DAMIT UND FLUGZEUG MIT DIESER BEFESTIGTEN STRUKTUR

    公开(公告)号:EP2551187A1

    公开(公告)日:2013-01-30

    申请号:EP11759363.2

    申请日:2011-03-22

    IPC分类号: B64C1/00 F16B37/14

    CPC分类号: B64D45/02 F16B37/14

    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.

    摘要翻译: 提供了一种能够通过抑制其内部火花的发生而能够实现增强的安全性的盖,即使雷电流已经通过紧固件流动,使用该紧固件的紧固结构以及包括紧固结构的飞行器也是如此。 根据本发明的盖(27)被附接以覆盖联接飞机的上皮(3)和位于上皮(3)内的纵梁(11)的紧固件(15)的一部分, 通过所述纵梁突出的部分(11),其中与所述上皮肤(3)的内部空间接触的所述盖的外表面(33)是弯曲表面,并且所述盖由导电材料制成。