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1.发明公开CAP, CAP MOLD, SECURING STRUCTURE PART USING CAP, AND METHOD FOR MOUNTING CAP 有权CAP，瓶盖模具，固定COMPONENT由盖总成盖和方法来
公开(公告)号：EP3106380A4
公开(公告)日：2017-04-12
申请号：EP15768941
申请日：2015-03-05
发明人： BESSHO MASAHIRO , ISHIKAWA NAOMOTO , KAMIHARA NOBUYUKI , KAMINO YUICHIRO , TANAKA HISASHI , MASUKAWA TAKAHISA
CPC分类号： F16B33/004 , B29C45/2618 , B29C45/262 , B29C45/2622 , B29L2031/727 , B64D45/02 , F16B37/14
摘要： A cap (9) is applied to a securing structure part (1) for securing structure elements (3, 3) using a fastener (5) passed through through-holes (3a) formed in the structure elements (3, 3), and a collar (7) fastened to the tip part (5a) of the fastener (5), and is mounted in a non-engaged state to the tip part (5a) of the fastener (5) and the collar (7). A filler engaging part (91) for engaging with a cured filler (11), said engaging part (91) configured with a female thread that turns about a center axis (CL), is formed on the inner peripheral surface (9e) of the cap (9). The filler engaging part (91) is provided with: a first helical engagement part (91a) formed in the region near the cap inner part of the inner peripheral surface (9e) in the center axis (CL) direction; and a second helical engagement part (91b) formed in the region near the cap opening-end part (9a) in the center axis (CL) direction, the inner diameter of the second helical engagement part (91b) being greater than that of the first helical engagement part (91a), and having a helical direction that is opposite to that of the first helical engagement part (91a).
摘要翻译： 的盖（9）被施加到一个固定结构部件（1），用于固定结构元件（3,3），使用紧固件（5）穿过通孔（3）在所述结构元件形成（3，3），和 紧固到所述紧固件（5）的末端部（5a），并且被安装在非接合状态到所述紧固件（5）的前端部（5a）和所述套环的轴环（7）（7）。 填料配合部（91），用于与固化的填料（11）接合，所述接合有阴螺纹部分配置（91）做转动绕中心轴线（CL）的内周表面上形成（9E）的 盖（9）。 填料卡合部（91）设置有：在所述内周面（9E）在中心轴线（CL）的方向的帽内部附近的区域形成的第一螺旋啮合部（91A）; 和第二螺旋啮合部（91B）形成在中心轴的帽开口端部（9A）（CL）的方向，所述第二螺旋形接合部分的内径（91B）比其的更大的附近的区域 第一螺旋啮合部（91A），以及具有螺旋形的方向所做的是相对于该第一螺旋那样卡合部（91A）的。
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公开(公告)号：EP2573930A4
公开(公告)日：2016-03-09
申请号：EP11783609
申请日：2011-05-19
发明人： KAMIHARA NOBUYUKI , KAMINO YUICHIRO , HASHIGAMI TOORU , MAKIMURA HIROKI , HIGASHIDE KOKI , KITAOKA MASAKI , ISHIMARU NAOTATSU
摘要： Damage can be prevented even when a large current and high voltage load is imposed. A current generation device (1) uses the power supplied from a power supply device (2) to supply, to a test piece (9) under lightning protection test, current that simulates current flowing when lightning occurs. The current generation device (1) comprises: an electric double-layer capacitor that stores power supplied from the power supply device (2) and discharges the stored power; a semiconductor switch (3) for switching whether the power stored on the electric double-layer capacitor is supplied to the test piece (9) or not; and a protection portion (4) connected between the semiconductor switch (3) and the test piece (9) and used for, when current having a predetermined value or more flows through the semiconductor switch (3), disconnecting the connection between the semiconductor switch (3) and the test piece (9).
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公开(公告)号：EP3263633A4
公开(公告)日：2018-05-23
申请号：EP16803106
申请日：2016-05-23
发明人： KAMIHARA NOBUYUKI , ABE TOSHIO
IPC分类号： B29C35/08 , B29C70/02 , B29K105/16 , C08J5/10
CPC分类号： B29C43/52 , B29C35/0272 , B29C35/0805 , B29C43/003 , B29C70/025 , B29C2035/0855 , B29C2035/0861 , B29K2105/162 , C08J5/041 , C08J5/10 , C08J2300/22 , C08J2300/24
摘要： In order to simplify the equipment for heating a thermosetting resin or a thermoplastic resin and to reduce manufacturing costs of a molded resin article by saving energy, this resin composite material (1A-1I) is formed by combining a fibrous reinforcing material (2) and a thermosetting or thermoplastic matrix resin (3), wherein a metal nanomaterial (4) which self-heats after absorbing electromagnetic waves is added to the matrix resin (3). The frequency of the electromagnetic waves is preferably within the range of 3 MHz to 3 GHz. The metal nanomaterial (4) is preferably nanofibers or nanocoils, and the material is preferably platinum or gold.
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公开(公告)号：EP2979976A4
公开(公告)日：2016-09-28
申请号：EP14774804
申请日：2014-02-18
CPC分类号： B64C3/34 , B32B5/00 , B32B7/02 , B32B2439/00 , B64D37/06 , B64D45/02 , H01M8/04208 , Y02P70/56 , Y02T50/44
摘要： The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in a manufacturing process to be reduced, and weight increases to be prevented. The fuel tank comprises a structural member in which carbon fiber reinforced plastic (CFRP) (15) is used, the carbon fiber reinforced plastic (CFRP) (15) comprising a reinforcing material that includes carbon fibers and a matrix that includes plastic. The structural member is formed by laminating a conductive sheet (17) between prepregs of the carbon fiber reinforced plastic (CFRP) (15). In this case, a cut surface (11a) of the structural member formed by cutting the structural member may be exposed on the inside in which fuel is stored.
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公开(公告)号：EP3214112A4
公开(公告)日：2017-11-22
申请号：EP15864708
申请日：2015-10-23
发明人： KAMIHARA NOBUYUKI , ABE TOSHIO
CPC分类号： B64C1/00 , B64C1/40 , B64C2001/0072 , C08J5/042 , C08J2363/00 , F28F2013/001 , F28F2255/06 , Y02T50/433
摘要： A member is provided with a first composite member (11) which is made from a plastic that is reinforced with heat-conductive carbon fibers comprising metal-coated carbon fibers and/or pitch-based carbon fibers, wherein one end or the heat-conductive carbon fibers is arranged at a heat-generating section and the other end of the heat-conductive carbon fibers is arranged at a heat-dissipating section as observed in the fiber direction.
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6.发明公开
公开(公告)号：EP2979977A4
公开(公告)日：2016-12-14
申请号：EP14776202
申请日：2014-01-28
IPC分类号： B64C3/34 , B32B1/02 , B32B5/00 , B32B7/02 , B32B15/08 , B60K15/03 , B64D45/02 , H01M8/00 , H01M8/04
CPC分类号： B64D37/32 , B32B1/02 , B32B7/08 , B32B15/08 , B32B27/12 , B32B27/20 , B32B2262/106 , B32B2307/20 , B32B2605/00 , B32B2605/18 , B64C3/34 , B64D37/005 , B64D37/04 , B64D37/06 , B64D45/02 , Y02T50/44
摘要： The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in quality management to be reduced, and weight increases to be prevented. The fuel tank comprises a structural member that uses a carbon fiber reinforced plastic (CFRP) (15) including a reinforcing material containing carbon fiber and a matrix containing plastic. The structural member is formed by laminating conductive sheets (17) between prepregs of the carbon fiber reinforced plastic (CFRP) (15), and being formed with a fastening hole (22) in which a bolt is fastened.
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公开(公告)号：EP2832773A4
公开(公告)日：2015-11-18
申请号：EP13769159
申请日：2013-03-12
CPC分类号： C08K7/06 , B29C70/882 , B29C70/885 , B32B15/02 , B32B15/08 , B32B15/20 , B32B27/20 , B32B2262/106 , B32B2307/202 , B32B2457/00 , B32B2605/00 , C08J5/042 , H02G13/80 , Y10T428/31678 , Y10T442/10
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公开(公告)号：EP3296728A4
公开(公告)日：2018-07-25
申请号：EP16859399
申请日：2016-09-01
发明人： KAMIHARA NOBUYUKI , ABE TOSHIO
CPC分类号： G01N27/24 , G01N27/205
摘要： The purpose of the present invention is to provide a method for evaluating the bonding state of a bonding section by inspecting a kissing bond using a non-destructive method. Disclosed is a bonding section evaluation method for evaluating the bonding state of a bonding section of a composite material that has the bonding section where a material to be bonded and another material to be bonded are bonded to each other with an adhesive therebetween. In the method, an alternating current signal is applied to the bonding section, a current and a voltage are measured by changing the frequency, evaluation values relating to predetermined electric characteristics are derived on the basis of the current value and the voltage value, which have been obtained by the measurement, the evaluation values are compared with reference relating to the predetermined electric characteristics, and the bonding state of the bonding section is evaluated according to the deviation quantities of the evaluation values from the reference.
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9.发明公开CAP, FASTENED STRUCTURE USING SAME, AND AIRCRAFT HAVING SAID FASTENED STRUCTURE 审中-公开CAP，安装构造以及与此固定结构这架飞机
公开(公告)号：EP2551187A4
公开(公告)日：2016-11-23
申请号：EP11759363
申请日：2011-03-22
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公开(公告)号：EP2832645A4
公开(公告)日：2015-12-02
申请号：EP13769070
申请日：2013-03-15
CPC分类号： B64D37/04 , B60K15/03177 , B64C3/34 , B64D37/08 , Y02T50/44
摘要： The objective of the present invention is to provide: a fuel tank that can prevent an increase in weight and can have reduced cost and working time during a production process, a main wing; an aircraft fuselage; an aircraft, and a mobile body. The fuel tank is provided with a structural member that uses a carbon-fiber-reinforced plastic of which the reinforcing material (15) contains carbon fibers and the matrix (17) contains plastic. The matrix (17) is imparted electrical conductivity. Also, a cut surface (11a) That is of the structural member and that is formed by the strcutural member being cut may be exposed within the fuel tank where a fuel is housed.
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