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1.发明申请EPOXY RESIN COMPOSITION, FIBER-REINFORCED COMPOSITE MATERIAL, AND METHOD FOR PRODUCING THE SAME 审中-公开环氧树脂组合物，纤维增强复合材料及其制造方法公开(公告)号：US20110097568A1
公开(公告)日：2011-04-28
申请号：US12934614
申请日：2009-03-23
CPC分类号： C08J5/047 , B29C70/06 , B29C70/443 , B29C71/02 , B29K2063/00 , B29K2307/04 , C08G59/3209 , C08G59/38 , C08G59/5033 , C08J3/20 , C08J5/04 , C08J2363/00 , C08J2463/02 , C08J2477/06 , C08K7/02 , C08L63/00 , Y10T428/249922
摘要： Disclosed herein are an epoxy resin composition for fiber-reinforced composite materials which has low viscosity, high Tg, high elastic modulus, and excellent fracture toughness and a fiber-reinforced composite material using such an epoxy resin composition which has excellent thermal properties, compressive strength, impact resistance, fatigue resistance, and open-hole tensile strength and which is suitable for producing structural parts of aircraft and the like. The epoxy resin composition comprises at least a given bifunctional epoxy resin as a component (A), a liquid aromatic diamine curing agent as a component (B), and core-shell polymer particles as a component (C), wherein the core-shell polymer particles as the component (C) contain epoxy groups in their shell and have a volume-average particle size of 50 to 300 nm.
摘要翻译： 本文公开了一种具有低粘度，高Tg，高弹性模量和优异的断裂韧性的纤维增强复合材料用环氧树脂组合物，以及使用这种环氧树脂组合物的纤维增强复合材料，其具有优异的热性能，抗压强度 耐冲击性，耐疲劳性和露天拉伸强度，适用于制造飞机等的结构部件。 环氧树脂组合物至少包含作为组分（A）的给定双官能环氧树脂，作为组分（B）的液体芳族二胺固化剂和作为组分（C）的核 - 壳聚合物颗粒），其中核 - 壳 作为（C）成分的聚合物粒子在其壳中含有环氧基，其体积平均粒径为50〜300nm。
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2.发明授权公开(公告)号：US10538637B2
公开(公告)日：2020-01-21
申请号：US15017575
申请日：2016-02-05
IPC分类号： B29C70/06 , C08J5/04 , C08G59/50 , C08G59/32 , C08L63/00 , C08J3/20 , C08G59/38 , B29C70/44 , B29C71/02 , C08K7/02 , B29K63/00 , B29K307/04
摘要： Disclosed herein are an epoxy resin composition for fiber-reinforced composite materials which has low viscosity, high Tg, high elastic modulus, and excellent fracture toughness and a fiber-reinforced composite material using such an epoxy resin composition which has excellent thermal properties, compressive strength, impact resistance, fatigue resistance, and open-hole tensile strength and which is suitable for producing structural parts of aircraft and the like. The epoxy resin composition comprises at least a given bifunctional epoxy resin as a component (A), a liquid aromatic diamine curing agent as a component (B), and core-shell polymer particles as a component (C), wherein the core-shell polymer particles as the component (C) contain epoxy groups in their shell and have a volume-average particle size of 50 to 300 nm.
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3.发明授权Binder composition, reinforcing-fiber base material, preform, fiber-reinforced composite material, and manufacturing method therefor 有权粘合剂组合物，增强纤维基材，预成型体，纤维增强复合材料及其制造方法公开(公告)号：US09062203B2
公开(公告)日：2015-06-23
申请号：US13496759
申请日：2010-09-14
申请人： Shinji Kochi , Kenichi Yoshioka , Masayuki Miyoshi
发明人： Shinji Kochi , Kenichi Yoshioka , Masayuki Miyoshi
CPC分类号： C08L77/06 , B29C70/48 , C08J5/04 , C08J5/24 , C08J2377/06 , C08K5/435 , C08K7/02 , D04H1/587 , Y10T428/31511 , Y10T428/31728 , Y10T442/3195
摘要： A binder composition comprising [A] an amorphous polyamide with a glass transition temperature of 140° C. or higher having a dicyclohexylmethane skeleton in the molecule and [B] a sulfonamide compound is used to provide a binder composition, a reinforcing-fiber base material and a preform respectively most suitable for RTM, which respectively exhibit excellent impact resistance and physical properties remaining stable over the variations of molding conditions and can be used for producing a fiber-reinforced composite material most suitable for members such as primary structures of aircraft.
摘要翻译： 使用包含[A]分子内具有二环己基甲烷骨架的玻璃化转变温度为140℃以上的无定形聚酰胺和[B]磺酰胺化合物的粘合剂组合物来提供粘合剂组合物，增强纤维基材 和分别最适合于RTM的预成型件，其分别在成型条件的变化下表现出优异的抗冲击性和物理性能，并且可用于生产最适合于诸如飞行器的主要结构的部件的纤维增强复合材料。
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4.发明申请BINDER COMPOSITION, REINFORCING-FIBER BASE MATERIAL, PREFORM, FIBER-REINFORCED COMPOSITE MATERIAL, AND MANUFACTURING METHOD THEREFOR 有权粘合剂组合物，增强纤维基材，预制品，纤维增强复合材料及其制造方法公开(公告)号：US20120178329A1
公开(公告)日：2012-07-12
申请号：US13496759
申请日：2010-09-14
申请人： Shinji Kochi , Kenichi Yoshioka , Masayuki Miyoshi
发明人： Shinji Kochi , Kenichi Yoshioka , Masayuki Miyoshi
CPC分类号： C08L77/06 , B29C70/48 , C08J5/04 , C08J5/24 , C08J2377/06 , C08K5/435 , C08K7/02 , D04H1/587 , Y10T428/31511 , Y10T428/31728 , Y10T442/3195
摘要： A binder composition comprising [A] an amorphous polyamide with a glass transition temperature of 140° C. or higher having a dicyclohexylmethane skeleton in the molecule and [B] a sulfonamide compound is used to provide a binder composition, a reinforcing-fiber base material and a preform respectively most suitable for RTM, which respectively exhibit excellent impact resistance and physical properties remaining stable over the variations of molding conditions and can be used for producing a fiber-reinforced composite material most suitable for members such as primary structures of aircraft.
摘要翻译： 使用包含[A]分子内具有二环己基甲烷骨架的玻璃化转变温度为140℃以上的无定形聚酰胺和[B]磺酰胺化合物的粘合剂组合物来提供粘合剂组合物，增强纤维基材 和分别最适合于RTM的预成型件，其分别在成型条件的变化下表现出优异的抗冲击性和物理性能，并且可用于生产最适合于诸如飞行器的主要结构的部件的纤维增强复合材料。
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5.发明申请PREPREG, FIBER-REINFORCED COMPOSITE MATERIAL, AND PROCESS FOR PRODUCING PREPREG 审中-公开PREPREG，纤维增强复合材料和生产PREPREG的方法公开(公告)号：US20130130584A1
公开(公告)日：2013-05-23
申请号：US13811183
申请日：2011-07-20
申请人： Takayuki Fujiwara , Jun Misumi , Ayumi Matsuda , Kenichi Yoshioka
发明人： Takayuki Fujiwara , Jun Misumi , Ayumi Matsuda , Kenichi Yoshioka
IPC分类号： B32B5/28
CPC分类号： B32B5/28 , B29C70/50 , B29K2063/00 , C08J5/24 , C08J2363/00 , Y10T156/10 , Y10T442/671 , Y10T442/674
摘要： There is provided a prepreg which contains components (A) to (C) as mentioned below, wherein the component (A) is arranged on one surface or both surfaces of a layer comprising the components (B) and (C): (A) a nonwoven fabric comprising a thermoplastic elastomer and/or a polyolefin each of which has a value of tan θ of 0.06 or more at 10° C. as measured in a viscoelasticity measurement and is incompatible with the component (B); (B) a first epoxy resin composition; and (C) a reinforcing fiber. There are also provided a fiber-reinforced composite material which has excellent rigidity, strength, and vibration-damping performance, a prepreg which can be used suitably for the production of the fiber-reinforced composite material, and a process for producing the prepreg.
摘要翻译： 提供了如下所述的含有组分（A）至（C）的预浸料，其中组分（A）设置在包含组分（B）和（C）的层的一个表面或两个表面上：（A） 包含热塑性弹性体和/或聚烯烃的无纺布，其各自在10℃下的tanθ值为0.06或更大，如在粘弹性测量中测量的，并且与组分（B）不相容; （B）第一环氧树脂组合物; 和（C）增强纤维。 还提供了具有优异的刚性，强度和减振性能的纤维增强复合材料，可适用于纤维增强复合材料的生产的预浸料，以及预浸料的制造方法。
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公开(公告)号：US20110291056A1
公开(公告)日：2011-12-01
申请号：US13195982
申请日：2011-08-02
IPC分类号： H01B1/24
CPC分类号： C08J5/24 , B32B5/022 , B32B5/22 , B32B5/26 , B32B27/12 , B32B2255/02 , B32B2255/26 , B32B2260/021 , B32B2260/046 , B32B2262/106 , B32B2264/0214 , B32B2264/105 , B32B2264/108 , B32B2305/076 , B32B2305/08 , B32B2307/202 , B32B2307/558 , B32B2603/00 , B32B2605/18 , C08J2363/00 , C08J2477/00 , C08L63/00 , C08L2201/02 , D06M11/74 , D06M11/83 , D06M15/53 , D06M15/63 , D06M2101/40 , D06M2200/00 , Y10T428/24 , Y10T428/24994 , Y10T428/249942 , Y10T428/249948 , Y10T428/249949 , Y10T428/24995 , Y10T428/25 , Y10T428/254 , Y10T442/2418 , Y10T442/2426 , Y10T442/645
摘要： A prepreg containing a carbon fiber [A] and a thermosetting resin [B], and in addition, satisfying at least one of the following (1) and (2).(1) a thermoplastic resin particle or fiber [C] and a conductive particle or fiber [D] are contained, and weight ratio expressed by [compounding amount of [C] (parts by weight)]/[compounding amount of [D] (parts by weight)] is 1 to 1000.(2) a conductive particle or fiber of which thermoplastic resin nucleus or core is coated with a conductive substance [E] is contained.
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7.发明申请TITANIUM OR TITANIUM ALLOY, ADHESIVE RESIN COMPOSITION, PREPREG AND COMPOSITE MATERIAL 审中-公开钛或钛合金，粘合树脂组合物，PREPREG和复合材料公开(公告)号：US20110048638A1
公开(公告)日：2011-03-03
申请号：US12941735
申请日：2010-11-08
申请人： Tomoyuki SHINODA , Kenichi Yoshioka
发明人： Tomoyuki SHINODA , Kenichi Yoshioka
CPC分类号： B32B15/092 , B32B7/12 , B32B15/00 , B32B15/06 , B32B15/14 , B32B2274/00 , B32B2419/00 , B32B2605/08 , B32B2605/18 , C23C26/00 , C23C30/00 , Y10T428/31663
摘要： The present invention relates to a composite material using titanium or a titanium alloy, and concerns such a composite material obtained through processes in which after an imidazole compound has been applied to the surface of titanium or a titanium alloy, an adhered is adhered thereto. The composite material of the present invention is obtained by adhering the adhere thereto by using an adhesive resin composition containing a thermoplastic resin having a fracture energy release rate G1C of 4500 J/m2 or more. The present invention makes it possible to provide a composite material using titanium or a titanium alloy, which exerts a superior adhesive strength stably at room temperature as well as even after exposure to a high-temperature, high humidity condition.
摘要翻译： 本发明涉及使用钛或钛合金的复合材料，并且涉及这样的复合材料，其通过在将咪唑化合物施加到钛或钛合金的表面之后附着到其上的方法获得。 本发明的复合材料通过使用含有断裂能释放速率G1C为4500J / m 2以上的热塑性树脂的粘合性树脂组合物来粘附附着物而获得。 本发明使得可以提供使用钛或钛合金的复合材料，其在室温下以及甚至在暴露于高温，高湿度条件之后都能稳定地发挥优异的粘合强度。
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公开(公告)号：US20090117800A1
公开(公告)日：2009-05-07
申请号：US12090921
申请日：2006-10-13
申请人： Hitoshi Nakatsuka , Tadayoshi Koizumi , Kazuhiko Tanaka , Nobuhiro Koga , Masao Kawamoto , Kenichi Yoshioka
发明人： Hitoshi Nakatsuka , Tadayoshi Koizumi , Kazuhiko Tanaka , Nobuhiro Koga , Masao Kawamoto , Kenichi Yoshioka
CPC分类号： A41D31/0066 , D01F1/09 , D01F8/14 , D02J1/22 , Y10T428/2924 , Y10T428/2927 , Y10T428/2929 , Y10T428/2931 , Y10T442/3146
摘要： An electrically conductive composite fiber comprising an electrically conductive layer formed of a polyester-based polymer (A) having a melting point of 200° C. or higher and containing from 23 to 33% by weight of electrically conductive carbon black, and a protective layer formed of a polyester-based polymer (B) having a melting point of 210° C. or higher, wherein the difference between the SP value of the (A) and the SP value of the (B) is adjusted to not greater than a predetermined value and the fiber strength and the elongation at break are adjusted within certain ranges. This can make it possible to obtain an electrically conductive composite fiber that has a superior antistatic performance, which is not degraded very much over a practical wearing for a long term, though it contains only a relatively small amount of electrically conductive carbon black, and that is suitable for the field of clothing such as clean room wears and working wears.
摘要翻译： 一种导电性复合纤维，其特征在于，具有由聚酯系聚合物（A）形成的导电性层，所述导电层的熔点为200℃以上，含有23〜33重量％的导电性炭黑，以及保护层 由熔点为210℃以上的聚酯类聚合物（B）形成，其中（A）的SP值与（B）的SP值的差被调整为不大于 将预定值和纤维强度和断裂伸长率调整到一定范围内。 这可以获得具有优异的抗静电性能的导电性复合纤维，虽然其仅含有相对少量的导电性炭黑，但是在长期的实际佩戴下，其性能没有劣化，并且 适用于衣物领域，如洁净室磨损和工作服。
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9.发明申请METHOD OF CONTROLLING CRITICALITY OF NUCLEAR FUEL CYCLE FACILITY, METHOD OF PRODUCING URANIUM DIOXIDE POWDER, REACTOR FUEL ROD, AND FUEL ASSEMBLY 有权控制核燃料循环设备关键性的方法，生产二氧化铀粉末的方法，反应器燃料油和燃料装配公开(公告)号：US20090028284A1
公开(公告)日：2009-01-29
申请号：US12120518
申请日：2008-05-14
摘要： A method of controlling the criticality of a nuclear fuel cycle facility includes steps of producing a reactor fuel by adding less than 0.1% by weight of gadolinia to a uranium dioxide powder with a uranium enrichment of greater than 5% by weight and controlling the effective neutron multiplication factor of a uranium dioxide system in a step of handling the reactor fuel to be less than or equal to the maximum of the effective neutron multiplication factor of a uranium dioxide system with a uranium enrichment of 5% by weight.
摘要翻译： 控制核燃料循环设备的关键性的方法包括以下步骤：通过将钆浓度小于5重量％的铀二氧化物粉末加入少于0.1重量％的氧化钆来生产反应堆燃料，并控制有效中子 处理反应堆燃料的步骤中二氧化铀系统的倍增系数小于或等于铀浓缩浓度为5重量％的二氧化铀系统的有效中子倍增系数的最大值。
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10.发明申请Axial void fraction distribution measurement method and neutron multiplication factor evaluating method 审中-公开轴向空隙率分布测量方法和中子倍增因子评估方法公开(公告)号：US20070076839A1
公开(公告)日：2007-04-05
申请号：US11434195
申请日：2006-05-16
申请人： Makoto Ueda , Hironori Kumanomido , Ishi Mitsuhashi , Tsukasa Kikuchi , Kenichi Yoshioka , Tomoharu Sasaki , Kouji Hiraiwa
发明人： Makoto Ueda , Hironori Kumanomido , Ishi Mitsuhashi , Tsukasa Kikuchi , Kenichi Yoshioka , Tomoharu Sasaki , Kouji Hiraiwa
IPC分类号： G21C3/32
摘要： A first intensity Az expressed as Az=az×Eα, a first reference intensity Ao expressed as Ao=ao×Eα, a second intensity Bz expressed as Bz=bz×E, and a second reference intensity Bo=bo×E, are evaluated. The first intensity and the first reference intensity are of radioactive nuclides generated by a neutron capture reaction of a heavy nuclide or a fission product nuclide. The second intensity and the second reference intensity are of radioactive fission product nuclides except nuclides generated by a neutron capture reaction. The reference intensities are measured where the void fraction is known. Also a correlation curve of (az/ao) and a void fraction is evaluated. Finally an axial void fraction distribution is evaluated based on the value of (az/ao) and the correlation curve.
摘要翻译： 表示为第一参考强度A 的第一强度A z > o 表示为第二强度B SUB表达的第二强度B 作为Bζz z x x x x x are are are are are，，，，evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated evaluated 。 第一强度和第一参考强度是由重核素或裂变产物核素的中子捕获反应产生的放射性核素。 第二强度和第二参考强度是放射性裂变产物核素，除了由中子俘获反应产生的核素外。 在已知空隙率的情况下测量参考强度。 此外，还评估了（a z> / / o o o o）和空隙率的相关曲线。 最后，基于（a 1 / z 2 / a 2）的值和相关曲线来评估轴向空隙率分布。
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