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    EXPLOSIVE SPARK ESTIMATION SYSTEM AND EXPLOSIVE SPARK ESTIMATION METHOD
    1.
    发明公开
    EXPLOSIVE SPARK ESTIMATION SYSTEM AND EXPLOSIVE SPARK ESTIMATION METHOD 审中-公开
    爆炸物爆炸物爆炸物爆炸物爆炸物爆炸物

    公开(公告)号：EP3144649A1

    公开(公告)日：2017-03-22

    申请号：EP16185099.5

    申请日：2016-08-22

    申请人： Fuji Jukogyo Kabushiki Kaisha ,  Kyushu Institute of Technology

    发明人： NISHI, Takayuki ,  OHTSUKA, Shinya

    IPC分类号： G01J3/28 ,  G01J3/443

    CPC分类号： G01J3/443 ,  G01J3/28 ,  G01J3/2803 ,  G01J3/457 ,  G01J2003/1213 ,  G01J2003/2859 ,  G01R31/1218

    摘要： According to one embodiment, an explosive spark estimation system (1) includes a measuring system (3) and a processing system (4). The measuring system (3) is adapted to measure intensity of light, included in a spark (S) occurred from an object (O) to be tested. The light is within at least one specific wavelength band. The processing system (4) is adapted to determine whether the spark (S) is explosiveness based on the intensity of the light. Further, according to one embodiment, an explosive spark estimation method includes: measuring intensity of light, included in a spark (S) occurred from an object (O) to be tested, within at least one specific wavelength band; and determining whether the spark (S) is explosive, based on the intensity of the light.

    摘要翻译： 根据一个实施例，爆炸性火花估计系统（1）包括测量系统（3）和处理系统（4）。 测量系统（3）适于测量包含在从被测物体（O）发生的火花（S）中的光的强度。 光在至少一个特定的波长带内。 处理系统（4）适于基于光的强度来确定火花（S）是否是爆炸性的。 此外，根据一个实施例，一种爆炸性火花估计方法包括：测量在至少一个特定波长带内从待测物体（O）发生的火花（S）中包含的光强度; 并且基于光的强度来确定火花（S）是否是爆炸性的。

    MAGNESIUM-LITHIUM ALLOY, METHOD OF MANUFACTURING MAGNESIUM-LITHIUM ALLOY, AIRCRAFT PART, AND METHOD OF MANUFACTURING AIRCRAFT PART
    5.
    发明公开
    MAGNESIUM-LITHIUM ALLOY, METHOD OF MANUFACTURING MAGNESIUM-LITHIUM ALLOY, AIRCRAFT PART, AND METHOD OF MANUFACTURING AIRCRAFT PART 审中-公开
    镁锂合金，工艺用于生产镁锂合金平面部分及其制造方法的空气供应

    公开(公告)号：EP3072989A1

    公开(公告)日：2016-09-28

    申请号：EP16157205.2

    申请日：2016-02-24

    申请人： Fuji Jukogyo Kabushiki Kaisha

    发明人： MIURA, Ayako

    IPC分类号： C22F1/06 ,  C22C23/00

    CPC分类号： C22F1/06 ,  B62D29/008 ,  C22C23/00

    摘要： According to one embodiment, a magnesium-lithium alloy in which at least lithium is added to magnesium is manufactured by giving a strain to a magnesium-lithium alloy workpiece, after a solution treatment, and progressing an aging of the magnesium-lithium alloy workpiece without a heat treatment. The strain is given by a cold working. The aging is progressed after giving the strain. Further, according to one implementation, an automobile part or an aircraft part includes the above-mentioned magnesium-lithium alloy as a material. Further, according to one embodiment, a method of manufacturing an automobile part or an aircraft part includes processing the above-mentioned magnesium-lithium alloy.

    摘要翻译： 。根据一个实施例，其中镁 - 锂合金中的至少锂加入到镁是通过施加应变的镁 - 锂合金工件中，固溶处理后，并进展到镁 - 锂合金工件的老化没有制造 热处理。 该菌株是通过冷加工给出。 老龄化正在给扭伤后的进展。 此外，gemäß到一个实施中，以汽车零件或飞机上部分包括上述的镁 - 锂合金作为材料。 此外，gemäß一个实施例，制造汽车部件的或航空器部件的方法包括处理上述镁 - 锂合金。

    PREPREG, FIBRE-REINFORCED COMPOSITE MATERIAL, AND PARTICLE-CONTAINING RESIN COMPOSITION
    7.
    发明公开
    PREPREG, FIBRE-REINFORCED COMPOSITE MATERIAL, AND PARTICLE-CONTAINING RESIN COMPOSITION 有权
    PREPREG，FASERVERSTÄRKTERVERBUNDSTOFF UND PARTIKELHALTIGE HARZZUSAMMENSETZUNG

    公开(公告)号：EP3072917A1

    公开(公告)日：2016-09-28

    申请号：EP14863175.7

    申请日：2014-10-28

    申请人： JX Nippon Oil & Energy Corporation ,  Fuji Jukogyo Kabushiki Kaisha

    发明人： MINAMI Masaki ,  MATSUMOTO Takayuki ,  FUKUDA Yoshihiro ,  SEKINE Naoyuki ,  NAKAJIMA Masanori

    IPC分类号： C08J5/24

    CPC分类号： C08J5/24 ,  B32B5/30 ,  B32B2605/18 ,  C08J2379/04 ,  C08J2463/00 ,  C08J2477/02 ,  C08J2477/06

    摘要： The prepreg comprises: a reinforcing fiber layer including reinforcing fibers and a resin composition with which the space between fibers of the reinforcing fibers is impregnated and which contains (A) a benzoxazine resin, (B) an epoxy resin, and (C) a curing agent having 2 or more phenolic hydroxy groups in a molecule; and a surface layer provided on a surface of the reinforcing fiber layer and containing (A) a benzoxazine resin, (B) an epoxy resin, (C) a curing agent having 2 or more phenolic hydroxy groups in a molecule, and (D) polyamide resin particles having an average particle size of 5 to 50 µm, wherein the polyamide resin particles include a polyamide 12 resin particle and a polyamide 1010 resin particle.

    摘要翻译： 预浸料包括：包含增强纤维的增强纤维层和浸渍增强纤维的纤维之间的空间的树脂组合物，其含有（A）苯并恶嗪树脂，（B）环氧树脂，（C）固化 在一个分子中具有2个或更多个酚羟基的试剂; （A）苯并恶嗪树脂，（B）环氧树脂，（C）分子中具有2个以上酚羟基的固化剂的表面层，（D）在所述强化纤维层的表面上设置的表面层， 平均粒径为5〜50μm的聚酰胺树脂粒子，其中聚酰胺树脂粒子包括聚酰胺12树脂粒子和聚酰胺1010树脂粒子。

    ULTRASONIC TEST SYSTEM, ULTRASONIC TEST METHOD AND METHOD OF MANUFACTURING AIRCRAFT PART
    8.
    发明公开
    ULTRASONIC TEST SYSTEM, ULTRASONIC TEST METHOD AND METHOD OF MANUFACTURING AIRCRAFT PART 审中-公开
    超声波测试仪，超声波清洗机，VERFAHREN ZUR HERSTELLUNG EINES FLUGZEUGBAUTEILS

    公开(公告)号：EP3070467A1

    公开(公告)日：2016-09-21

    申请号：EP16158078.2

    申请日：2016-03-01

    申请人： Fuji Jukogyo Kabushiki Kaisha

    发明人： TAKAHASHI, Kohei

    IPC分类号： G01N29/04 ,  G01N29/34

    CPC分类号： G01N29/041 ,  B23P6/00 ,  G01N29/043 ,  G01N29/12 ,  G01N29/348 ,  G01N2291/0289 ,  G01N2291/0427 ,  G01N2291/044 ,  G01N2291/048 ,  G01N2291/2694

    摘要： According to one embodiment, an ultrasonic test system includes an ultrasonic transmission part including at least one ultrasonic transducer, an ultrasonic detection part including at least one sensor and damage detection part consisting of circuitry. The ultrasonic transducer transmits a first ultrasonic wave and a second ultrasonic wave toward a test region. The first ultrasonic wave has a relatively low frequency. The second ultrasonic wave has a frequency higher than the frequency of the first ultrasonic wave. The sensor detects a reflected wave of the first ultrasonic wave and the second ultrasonic wave which has passed through the test region. The reflected wave is from the test region. The damage detection circuitry is configured to detect a damage in the test region, based on the reflected wave of the first ultrasonic wave and the second ultrasonic wave which has passed through the test region.

    摘要翻译： 根据一个实施例，超声波测试系统包括包括至少一个超声波换能器的超声波发射部分，包括至少一个传感器的超声波检测部分和由电路组成的损伤检测部分。 超声波换能器向测试区域发送第一超声波和第二超声波。 第一超声波具有相对较低的频率。 第二超声波的频率高于第一超声波的频率。 传感器检测第一超声波和穿过测试区域的第二超声波的反射波。 反射波来自测试区域。 损伤检测电路被配置为基于已经通过测试区域的第一超声波和第二超声波的反射波来检测测试区域中的损坏。

    METHOD AND DEVICE FOR TESTING WATER DROPLET SHEDDING ABILITY OF AIRCRAFT WING
    9.
    发明公开
    METHOD AND DEVICE FOR TESTING WATER DROPLET SHEDDING ABILITY OF AIRCRAFT WING 有权
    VERFAHREN UND VORRICHTUNG ZUM TESTEN DERWASSERTROPFENABSTOSSUNGSFÄHIGKEITEINESFLUGZEUGFLÜGELS

    公开(公告)号：EP3069998A1

    公开(公告)日：2016-09-21

    申请号：EP16158003.0

    申请日：2016-03-01

    申请人： Fuji Jukogyo Kabushiki Kaisha

    发明人： TANAKA, Taro

    IPC分类号： B64D15/00 ,  B64D15/20 ,  G09B9/16

    CPC分类号： G01M99/00 ,  B64D15/00 ,  B64D15/20 ,  G01M9/02 ,  G01M9/06 ,  G01M9/067 ,  G09B25/00

    摘要： There are provided a method and a device for testing water droplet shedding ability of an aircraft wing. A cylindrical member (2) simulating an aircraft wing (W) and having hydrophobicity that differs across a boundary position (2b) in a circumferential direction is used. Air is blown by using a blower (3) toward a surface of the cylindrical member (2) in an airflow direction (D) perpendicular to an axial direction of the cylindrical member (2). A water droplet is supplied by using a water supply cylinder (4 to a portion of the surface of the cylindrical member (2) on a leading edge side with respect to a flow of the air. An image of the water droplet that moves on the surface of the cylindrical member (2 across the boundary position (2b) due to the flow of the air is captured by using a camera (5).

    摘要翻译： 提供了一种用于测试飞机机翼的水滴脱落能力的方法和装置。 使用模拟飞行器机翼（W）并且具有在周向方向上在边界位置（2b）上不同的疏水性的圆柱形构件（2）。 在与圆柱形部件（2）的轴向垂直的气流方向（D）上，使用鼓风机（3）向筒状部件（2）的表面吹出空气。 通过使用供水筒（4）相对于空气流在前缘侧的筒状部件（2）的表面的一部分供给水滴， 通过使用照相机（5）捕获由于空气流动导致圆柱形构件（跨越边界位置（2b）的两个）表面。

    DRILLING MACHINE AND METHOD OF MANUFACTURING DRILLED PRODUCT
    10.
    发明公开
    DRILLING MACHINE AND METHOD OF MANUFACTURING DRILLED PRODUCT 审中-公开
    BOHRMASCHINE UND VERFAHREN ZUR HERSTELLUNG EINES GEBOHRTEN PRODUKTS

    公开(公告)号：EP3069807A1

    公开(公告)日：2016-09-21

    申请号：EP16155137.9

    申请日：2016-02-11

    申请人： Fuji Jukogyo Kabushiki Kaisha

    发明人： ONO, Yuzuru ,  YOKONO, Tsukasa ,  HIRAI, Hisayuki ,  SHIBATA, Shigeru

    IPC分类号： B23B41/00 ,  B23Q9/02 ,  B64F5/00

    CPC分类号： B23B41/006 ,  B23B2215/04 ,  B23Q9/02 ,  B64F5/10

    摘要： According to one embodiment, a drilling machine includes a drilling structure and a travelling machine. The drilling structure drills an object to be drilled composed of at least one structural object on a platy part. The travelling machine positions the drilling structure in a travelling direction of the travelling machine by travelling in a longitudinal direction of the at least one structural object using the at least one structural object as a guide.

    摘要翻译： 根据一个实施例，钻机包括钻孔结构和行进机。 该钻井结构在由板状部分上的至少一个结构物体构成的钻孔物体上钻探。 移动机械使用至少一个结构体作为引导件，沿着至少一个结构物体的纵向行进，沿行进机械的行进方向定位钻孔结构。