| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | Prepreg and carbon fiber reinforced composite material | JP2013124260 | 2013-06-13 | JP5541394B2 | 2014-07-09 | 信之 荒井; 憲光 夏目; 健一 吉岡; 順子 川崎; 宏 竹崎 |
| 162 | Carbon fiber reinforced composite material epoxy resin composition, a prepreg and carbon fiber reinforced composite material | JP2012125575 | 2012-06-01 | JP5522199B2 | 2014-06-18 | 信之 荒井; 憲光 夏目; 健一 吉岡; 順子 川崎; 宏 竹崎 |
| 163 | Rotor blade and fan | JP2012104433 | 2012-05-01 | JP2013231402A | 2013-11-14 | MUROOKA TAKESHI |
| PROBLEM TO BE SOLVED: To secure sufficient fluttering resistance of a fan rotor blade 23 while reducing the weight of the fan rotor blade 23.SOLUTION: A rotor blade body 37 includes: multiple first composite sheet groups 51 that are overlapped based on a pattern in which multiple composite sheets 49 are overlapped from a blade thickness center TC side toward a dorsal surface 39 side, and are provided in a blade thickness direction TD; and multiple second composite sheet groups 53 that are overlapped based on a pattern in which the multiple composite sheets 49 are overlapped from the blade thickness center TC side toward a ventral surface 41 side, and are provided in the blade thickness direction TD. A combined direction CD of orientation directions of reinforcing fibers of the multiple composite sheets 49 in the first composite sheet groups 51 and the second composite sheet groups 53 is inclined 20-45 degrees toward the rear edge side with respect to a span direction SD. | ||||||
| 164 | Prepreg and carbon fiber-reinforced composite material | JP2013124260 | 2013-06-13 | JP2013224435A | 2013-10-31 | ARAI NOBUYUKI; NATSUME NORIMITSU; YOSHIOKA KENICHI; KAWASAKI JUNKO; TAKEZAKI HIROSHI |
| PROBLEM TO BE SOLVED: To provide a prepreg capable of providing a carbon fiber-reinforced composite material having both excellent impact resistance and electroconductivity.SOLUTION: A prepreg includes [A] a carbon fiber and [B] a thermosetting resin. and satisfying at least either of the following (1) and (2): (1) including [C] a thermoplastic resin particle or fiber and [D] an electroconductive particle or fiber, where a weight ratio expressed by [blend amount (part by weight) of [C]]/[blend amount (part by weight) of [D]] is 1 to 1,000; (2) including an electroconductive particle or fiber where the nucleus or core of [E] the thermoplastic resin is covered by an electroconductive substance. | ||||||
| 165 | A fiber-reinforced composite molded article | JP2013517085 | 2011-07-01 | JP2013537490A | 2013-10-03 | ヤラ ミラレイ ボルヤ、アダスメ; クロード ドゥモラール、ジャン; ラーセン、フレミング; ショエフリンガー、マンフレット |
| The present invention regards a fibre-reinforced composite moulding with an outer (102) structure and an inner structure (106), wherein the outer structure (102) is formed from at least one layer of fibrous reinforcing material and a cured first resin material, and the inner structure (106) is formed from a plurality of layers of fibrous reinforcing material and a second cured resin material, wherein the viscosity of the uncured first resin material is lower than the viscosity of the uncured second resin material and wherein in the composite moulding the two cured resin materials are at least partially mixed with each other. It also regards a process for the production of such a fibre-reinforced composite moulding. | ||||||
| 166 | Multilayer corrosion-resistant protective film | JP2013527330 | 2011-09-02 | JP2013536776A | 2013-09-26 | イー．マークス ライアン; エム．ジェネン ジェイ; イー．マイヤー ダニエル; ジェイ．シュルツ ウイリアム; エル．トンプソン ウエンディ |
| 航空機の前端を雨食及び砂食から保護するために有用であり得る、多層ポリマーフィルムを提示する。 典型的には、１層以上の第２の材料と交互に積層された２層以上の第１の材料を含み、第１及び第２の材料が異なる材料であり、第１及び第２の材料が第１及び第２のポリマーを含み、第１及び第２の材料が第１及び第２のショア硬度を有し、第１のショア硬度が第２のショア硬度よりも高くてその差が５Ａ、又はより典型的には１０Ａを上回る、表面保護フィルムである。 | ||||||
| 167 | Prepreg and carbon fiber reinforced composite material | JP2013077396 | 2013-04-03 | JP5293905B2 | 2013-09-18 | 信之 荒井; 憲光 夏目; 健一 吉岡; 順子 川崎; 宏 竹崎 |
| 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. | ||||||
| 168 | Epoxy resin composition for carbon fiber-reinforced composite material, prepreg and carbon fiber-reinforced composite material | JP2012125575 | 2012-06-01 | JP2012197447A | 2012-10-18 | ARAI NOBUYUKI; NATSUME NORIMITSU; YOSHIOKA KENICHI; KAWASAKI JUNKO; TAKEZAKI HIROSHI |
| PROBLEM TO BE SOLVED: To provide a prepreg capable of providing a carbon fiber-reinforced composite material having both excellent impact resistance and conductivity.SOLUTION: The prepreg contains [A] a carbon fiber and [B] a thermosetting resin, and satisfies at least one of the following (1) and (2). (1) The prepreg contains [C] a thermoplastic resin particle or fiber, and [D] a conductive particle or fiber, and the weight ratio of [a blend amount (pts.wt) of [C]]/[a blend amount (pts.wt) of [D]] is 1 to 1,000. (2) The prepreg contains a conductive particle or fiber in which a nucleus or core of [E] a thermoplastic resin is coated with a conductive substance. | ||||||
| 169 | Thin ply laminate | JP2012108588 | 2012-05-10 | JP2012196967A | 2012-10-18 | TSAI STEPHEN W; KAWABE KAZUMASA |
| PROBLEM TO BE SOLVED: To provide fiber composite materials that provide delamination resistance and minimum gauge.SOLUTION: Fiber composite materials using thin plies with a thickness of less than 0.08 mm provide improved delamination resistance and thinner minimum gauge for laminates. Thin plies may be hybridized with conventional plies, interlaced for strength, and used with adhesives as reinforcement in bonding. | ||||||
| 170 | Prepreg and carbon fiber-reinforced composite material | JP2012106390 | 2012-05-08 | JP2012188670A | 2012-10-04 | ARAI NOBUYUKI; NATSUME NORIMITSU; YOSHIOKA KENICHI; KAWASAKI JUNKO; TAKEZAKI HIROSHI |
| PROBLEM TO BE SOLVED: To provide a prepreg which is a carbon fiber-reinforced composite material having excellent impact resistance together with electrical conductivity.SOLUTION: The prepreg contains a carbon fiber, and a thermosetting resin, and satisfies at least any one of following (1) and (2). (1) a thermoplastic resin particle or fiber and an electrically conductive particle or fiber are contained wherein the weight ratio of the former to the latter is 1-1,000. (2) The electrically conductive particle or fiber whose thermoplastic resin nucleus or core is coated with an electrically conductive substance is contained. | ||||||
| 171 | Prepreg and carbon fiber reinforced composite material | JP2010185837 | 2010-08-23 | JP5029742B2 | 2012-09-19 | 健一 吉岡; 憲光 夏目; 順子 川崎; 宏 竹崎; 信之 荒井 |
| 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. | ||||||
| 172 | Prepreg and carbon fiber reinforced composite material | JP2011142642 | 2011-06-28 | JP5013008B2 | 2012-08-29 | 健一 吉岡; 憲光 夏目; 順子 川崎; 宏 竹崎; 信之 荒井 |
| 173 | Prepreg and carbon fiber reinforced composite material | JP2007203880 | 2007-08-06 | JP4969363B2 | 2012-07-04 | 健一 吉岡; 憲光 夏目; 順子 川崎; 宏 竹崎; 信之 荒井 |
| 174 | Metal coating of the composite material | JP2009540840 | 2007-12-06 | JP2010513706A | 2010-04-30 | トマス・ジョセフ・コードン; マーク・レイモンド・スティール |
| A method of manufacturing a composite and of securing a metallic coating to a resin-based composite material, comprising the provision of a keying structure on a metallic electroplated preform and bringing the keying structure and the composite material together under conditions to cause the composite material and the keying structure to interlock. The invention also provides a composite comprising a resin-based composite material with a metallic coating on a surface, or part surface thereof, the metallic coating comprising an outer electroplated preform, and an inner keying structure which is located generally between said electroplated preform and the composite material to provide attachment of the electroplated preform on the composite material. | ||||||
| 175 | Polymer film | JP12901892 | 1992-05-21 | JP3045874B2 | 2000-05-29 | ウォール デビッド; リチャード ベリー マイケル |
| 176 | Polymeric film | JP12901892 | 1992-05-21 | JPH05138836A | 1993-06-08 | MAIKERU RICHIYAADO BERII; DEBITSUDO UOORU |
| PURPOSE: To improve the winding performance of film on a reel and slitting performance by producing surface protrusions of a specific number by applying a particulate additive on a heat-sealable exposed surface to have an average peak height in a specific range measured from the average level of the layer surface. CONSTITUTION: A composite film is obtained by including a heat-sealable layer containing a particulate additive on at least one surface of a support layer of a polymeric material. The exposed surface of the heat-sealable layer contains surface protrusions produced by the particulate additive and the protrusion density is larger than 100/mm<2> . The surface protrusions have an average height in the range of 5 to 400 nm measured from the average level of the heat-sealable layer surface. | ||||||
| 177 | Wide chord fan blade | JP3130892 | 1992-01-23 | JPH04330301A | 1992-11-18 | GAI KURIFU MAAFUI; BARETSUTO JIYOSEFU FUUAMAN |
| PURPOSE: To provide a large-size laminated airfoil which is excellent in weight adequate to a high bypass engine and can endure normal impact and motion conditions in relation to a fan blade in an aircraft turbo fan engine. CONSTITUTION: An airfoil with a wide chip chord is comprised of alternating layers of thin metallic foil 28 and elastomeric layers 30. The exterior surfaces of the airfoil are comprised of the thin, metallic foil 28. The airfoil has a metal sheath 20 secured to the leasing edge. High strength metal members extend through the dovetail root sections 14. COPYRIGHT: (C)1992,JPO | ||||||
| 178 | JPS4838366A - | JP8336972 | 1972-08-22 | JPS4838366A | 1973-06-06 | |
| 179 | 풍력 발전 설비용 로터 블레이드 부재, 로터 블레이드, 그것을 위한 제조 방법 및, 로터 블레이드를 구비한 풍력 발전 설비 | KR1020167007658 | 2014-08-01 | KR101788490B1 | 2017-10-19 | 타일레벤자민; 호프만알렉산더 |
| 본발명은특히청구항제 10 항에따른방법에의해제조된로터블레이드부재, 특히풍력발전설비를위한로터블레이드에지에관한것으로, 경화형수지로함침된섬유재료를포함하는베이스, 표면박막및 상기베이스와표면박막사이에배치된결합층을포함한다. 본발명에따라표면박막은초고분자량폴리에틸렌(UHMWPE)을포함하고, 결합층은제 1 가류된고무층및 제 2 가류된고무층을포함하고, 이경우제 1 가류된고무층은표면박막에할당되고제 2 가류된고무층은베이스에할당되는것이제안된다. | ||||||
| 180 | 적층 구조체 및 터치 패널 모듈 | KR1020167022193 | 2015-01-26 | KR1020160110458A | 2016-09-21 | 고이케다카시; 고바야시히로유키; 니시다데츠지; 츠바타히사시 |
| 적층구조체는, 가요성을갖는투명기판상에금속세선으로구성된메시구조의도전패턴을갖는투명도전부재와, 투명도전부재를보호하기위한보호부재와, 투명도전부재와보호부재의사이에위치하는광학적으로투명한접착제층을구비하는적층체를갖는다. 적층체의두께는 100μm 이상 600μm 이하이다. 접착제층의두께는적층체의두께의 20% 이상이다. 투명도전부재의 150℃에있어서의열수축률은 0.5% 이하이며, 투명도전부재와보호부재의 150℃에있어서의열수축률의차분은투명도전부재의 150℃에있어서의열수축률의 60% 이내이다. 적층구조체는 3차원형상의터치패널모듈에이용된다. | ||||||
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