161 |
Composite laminate and a manufacturing method thereof having an attenuation intermediate layer |
JP2009547244 |
2007-12-12 |
JP5460333B2 |
2014-04-02 |
サルバトール エル リグオール,; トゥアン クアン カオ,; ジョシュア エム モンゴメリー, |
Composite laminates used in structural applications include an interlayer of soft material that provides damping action to reduce noise and vibration. The interlayer may comprise a viscoelastic material which deforms under stress caused by shock, noise or vibration. A reinforcement may be embedded in the viscoelastic material to maintain the mechanical strength and stiffness of the laminate. The reinforcement may include individual or woven fibers or ridged tubes that provide the interlayer with stiffness. |
162 |
Fabrication and application of nanofiber ribbons and sheets and twisted and non-twisted nanofiber yarns |
JP2013065711 |
2013-03-27 |
JP2013174038A |
2013-09-05 |
CHAN MEI; FANG SHAOLI; BAUGHMAN RAY H; ZAKHIDOV ANVAR A; ATKINSON KENNETH ROSS; ALIEV ALI E; LI SERGEY; WILLIAMS CHRIS |
PROBLEM TO BE SOLVED: To provide nanofiber yarns, ribbons, and sheets, and to provide methods of making said yarns, ribbons, and sheets; and to provide applications of said yarns, ribbons, and sheets.SOLUTION: Provided is a nanotube yarns, a ribbon and a sheet having the following unique properties and unique property combinations: toughness comparable to that of fibers used for bullet proof vests, resistance to failure at knots, high electrical and thermal conductivities, high reversible absorption of energy, up to 13% strain-to-failure compared with the few percent strain-to-failure of other fibers with similar toughness, very high resistance to creep, retention of strength even when heated in air at 450°C for one hour, and very high radiation and UV resistance, even when irradiated in air. |
163 |
Production method and rewinding method of graphite film, as well as the method of manufacturing a graphite composite film and graphite punching goods |
JP2012500496 |
2011-02-14 |
JP5048166B2 |
2012-10-17 |
真琴 三代; 雄介 太田; 卓 稲田; 敬 稲田; 泰司 西川 |
A graphite film showing an extremely low average tearing force is more likely to suffer from various kinds of defects, such as splitting, winding deviation, wrinkling, and poor dimensional accuracy, in a step of producing the graphite film and in a step of processing the graphite film. However, these defects can be prevented by using a graphite film that satisfies the following requirements: 1) having an average tearing force of not more than 0.08 N as determined by Trouser tear method in accordance with JIS K7128; and 2) having sag of not less than 5 mm and not greater than 80 mm as determined by a method of film windability evaluation in accordance with JIS C2151. |
164 |
Fabrication and application of nanofiber ribbon and sheet, and twisted and non-twisted nanofiber yarn |
JP2012036396 |
2012-02-22 |
JP2012111691A |
2012-06-14 |
CHAN MEI; FANG SHAOLI; BAUGHMAN RAY H; ZAKHIDOV ANVAR A; ATKINSON KENNETH ROSS; ALIEV ALI E; LI SERGEY; WILLIAMS CHRIS |
PROBLEM TO BE SOLVED: To provide nanofiber yarns, ribbons, and sheets; methods for making the yarns, ribbons, and sheets; and applications of the yarns, ribbons, and sheets.SOLUTION: In some embodiments, the nanotube yarns, ribbons, and sheets comprise carbon nanotubes. Particularly, such carbon nanotube yarns provide unique properties and property combinations such as extreme toughness, resistance to failure at knots, high electrical and thermal conductivity, high absorption of energy that occurs reversibly, up to 13% strain-to-failure compared with the few percent strain-to-failure of other fibers with similar toughness, very high resistance to creep, retention of strength even when heated in air at 450°C for one hour, and very high radiation and UV resistance, even when irradiated in air. |
165 |
Method and core complex to produce a core complex comprising a cover layer on both sides |
JP2011504391 |
2009-02-20 |
JP2011516317A |
2011-05-26 |
コラックス,ミヒャエル; ドルジンスキー,ヴォルフ−ディートリヒ |
The invention relates to a method for manufacturing a core composite (1, 20, 26) having a folded honeycomb core (2, 21, 29) provided on both sides with cover layers (3, 4, 22, 23, 27, 28) wherein the folded honeycomb core (2, 21, 29) has a number of drainage-enabling channels (5). First a core filler material (16, 17) is introduced into the folded honeycomb core (2, 21, 29) at least in some areas in order to provide the filler material with sufficient stability for the subsequent sewing process. The cover layers (3, 4, 22, 23, 27, 28) which are not yet impregnated with a curable plastics material are then placed on the folded honeycomb core (2, 21, 29) and stitched to this along the base lines (6 to 8) and/or apex lines (9, 10) at least in some sections by means of a sewing thread (19). The infiltration of the overall structure with a curable plastics material is then carried out followed by hardening by applying pressure and/or temperature. The core filler material (16, 17) can to complete the process be removed again completely from the folded honeycomb core (2, 21, 29) by being dissolved and washed out or by melting and flowing out. Delamination of the cover layers (3, 4, 22, 23, 27, 28) from the folded honeycomb core (2, 21, 29) is prevented by the stitching so that core composites (1, 20, 26) manufactured by the method according to the invention can be used in the primary structure of aircraft. The invention further relates to a core composite (1, 20, 26) manufactured according to the provisions of the method. |
166 |
Method for producing a graphite film |
JP2007518993 |
2006-05-30 |
JP4659827B2 |
2011-03-30 |
睦明 村上; 修平 若原; 泰司 西川 |
In order to obtain a graphite film having an excellent thermal diffusivity, a high density, and excellent flatness without flaws, recesses and wrinkles on the surface, the process for producing a graphite film according to the present invention comprises the graphitization step for a raw material film made of a polymer film and/or a carbonized polymer film and/or the post-planar pressurization step for the film in this order to prepare a graphite film, wherein the graphitization step is a step of thermally treating two or more stacked raw material films at a highest temperature of 2,000° C. and includes a method of electrically heating the raw material films themselves and/or a method of thermally treating the films while applying pressure to the films planarly, and the post-planar pressurization step includes a method of planarly pressurizing the one raw material film or the multiple stacked raw material films after graphitization by single-plate press or vacuum press. |
167 |
グラファイトフィルムの製造方法、およびその方法で製造されたグラファイトフィルム |
JP2007518993 |
2006-05-30 |
JPWO2006129632A1 |
2009-01-08 |
西川 泰司; 泰司 西川; 修平 若原; 村上 睦明; 睦明 村上 |
熱拡散率に優れ、密度が高く、表面に傷、凹み、皺がない、平坦性に優れたグラファイトフィルムを得るために、本発明のグラファイトフィルムの製造方法は、高分子フィルム、及び/又は、炭素化した高分子フィルムからなる原料フィルムを順に、グラファイト化工程、及び/又は、後面状加圧工程を経てグラファイトフィルムとする製造方法であって、前記グラファイト化工程は、原料フィルムを2枚以上積層した状態で最高温度が2000℃以上の熱処理をする工程であって、原料フィルム自体を、通電加熱する方法、及び/又は、面状に加圧しながら熱処理する方法、を含み、前記後面状加圧工程は、グラファイト化後の原料フィルムを1枚、又は複数枚重ねた状態で単板プレスや真空プレスにより面状に加圧する方法、を含む。 |
168 |
Conductive sheet for electronic parts packaging container |
JP2001532957 |
2000-10-26 |
JP4072814B2 |
2008-04-09 |
健志 宮川; 和裕 小杉; 正徳 日向野; 美基雄 清水 |
|
169 |
Resin composition, the molded article and the conductive sheet |
JP2001532957 |
2000-10-26 |
JP2003512207A |
2003-04-02 |
健志 宮川; 和裕 小杉; 正徳 日向野; 美基雄 清水 |
(57)【要約】 アクリロニトリル−ブタジエン−スチレン共重合体系樹脂及び/又はポリスチレン系樹脂を含有してなる熱可塑性樹脂の基材層の少なくとも片面に、ポリカーボネート系樹脂に5〜50重量%のカーボンブラックを含有してなる導電性樹脂組成物を積層してなる導電シート。 基材層が更にポリカーボネート系樹脂を熱可塑性樹脂に対し1〜50重量%を含有してなる請求項1の導電シート。 |
170 |
Heat-resistant coated member |
JP2001354673 |
2001-11-20 |
JP2003073794A |
2003-03-12 |
TAKAI YASUSHI; HAMAYA NORIAKI; KANEYOSHI MASAMI |
PROBLEM TO BE SOLVED: To provide a heat-resistant coated member which has satisfactory heat resistance, corrosion resistance, and non-reactiveness, and is effectively used for sintering or heat-treating metal or ceramic under vacuum, an inert atmosphere or a reduced atmosphere. SOLUTION: The heat-resistant coated member is characterized in that a substrate including materials selected among Mo, Ta, W, Zr, Al, Ti, carbon, alloys thereof, oxide ceramics thereof, non-oxide ceramics, and carbide-based materials, is coated with a layer which includes oxides containing rare earth elements as a main component. |
171 |
Multilayer fuel and vapor tube |
JP51465596 |
1995-10-11 |
JP3356288B2 |
2002-12-16 |
ニー、タオ; ヌーン、デイビッド・エル; ミッチェル、フランク・エル |
|
172 |
Composite mat |
JP2000519206 |
1998-10-28 |
JP2001521847A |
2001-11-13 |
エリザベス ウェイド、キャスリーン; ステプレー、ヴァルテ; ディンウッディー、ジョン; ジョン ホートン、デイビッド; サミュエル ボフィー、スチュアート |
(57)【要約】 自動車に触媒コンバータを取り付けるための複合マットであって、無機繊維とバインダからなる層よりなり、径の細い棒を包んだときのマットの割れを防ぎ、触媒コンバータのモノリスを包んだときにマットを容易にケーシングに挿入できるように摩擦が低い特徴を有した可撓性シートまたはコーティングを設けて改良した。 |
173 |
Thermal insulation composite gasket |
JP20778689 |
1989-08-10 |
JPH0646070B2 |
1994-06-15 |
ロバート、アングロ、マーキュリー |
|
174 |
Insulating composite gasket |
JP20778689 |
1989-08-10 |
JPH02113172A |
1990-04-25 |
ROBAATO ANGURO MAAKIYURII |
PURPOSE: To prevent the back flow of heat and provide thermal insulation instead of asbestos by overlapping a metal layer, a thermally insulating fireproof fiber layer, and a flexible graphite layer, arranging the thermally insulating fireproof fiber layer between the metal layer and the flexible graphite layer, and connecting each layer by a connection means. CONSTITUTION: A core or projection 109 is punched on a metallic sheet used in a metallic layer 103, and a fireproof fiber sheet 105 and a flexible graphite sheet 107 are pressed on the projection 109 to manufacture this insulating composite gasket. Consequently, the back flow of heat is suppressed, exhaust gas is sealed, a section between a head and a muffler is thermally insulated stably at a high temperature, and it can be used instead of asbestos. |
175 |
JPS616441B2 - |
JP9364980 |
1980-07-08 |
JPS616441B2 |
1986-02-26 |
MATSUDA SHUNSUKE; KOMATSU YASUMITSU |
|
176 |
Production of tone arm |
JP9364980 |
1980-07-08 |
JPS5718001A |
1982-01-29 |
MATSUDA SHIYUNSUKE; KOMATSU YASUMITSU |
PURPOSE:To realize a light-weight tone arm having a high rigidity and small internal loss, by stacking a graphite flake lamination sheet onto a carbon fiber prepreg in a pipe form. CONSTITUTION:A carbon fiber prepreg 1 is formed by arraying the yarns of carbon fiber in a prescribed direction with every row. A graphite flake lamination sheet 2 is formed by kneading the graphite and the thermosetting resin and formed into a lamination sheet after coating the kneaded graphite and thermosetting resin on a polyester sheet by a roller. Then the prepreg 1 and the sheet 2 are wound around a steel core material 4 and then heated up. Thus the material 4 is expanded with heat, and a roll-up material is pressed. The hardening progresses under an application of pressure. For such pipe, a low rigidity in the direction of diameter can be compensated by the graphite lamination sheet, and the lengthwise rigidity becomes higher than the graphite lamination sheet owing to the carbon fiber. |
177 |
JPS5492471U - |
JP16782677 |
1977-12-14 |
JPS5492471U |
1979-06-30 |
|
By bonding a graphite sheet possessing tightness to at least one surface of carbon fiber felt sheet possessing gas permeability by means of a carbonaceous binder, a multilayer thermally insulating material suitable for use in a heating furnace employing a nonoxidizing atmosphere is obtained. This insulating material has mechanical strength which does not decrease with a long period of use and gives rise to little contamination of articles being heated in the furnace. |
178 |
PRODUCTION OF FUNCTIONALISED SUBSTRATE |
EP10805278.8 |
2010-12-22 |
EP2516691B1 |
2018-10-24 |
PALMER, Richard; SONG, Mi Yeon |
The present invention resides in a functionalised substrate and a method of producing the same. The method comprises providing a substrate in the form of a tape, and depositing metallic clusters on a surface of the tape to thereby create a functionalised surface layer. The functionalised surface layer may be separated from the tape and used in applications including catalysis and surface science. |
179 |
PACKAGING MATERIAL FOR PACKAGING OF LIGHT-SENSITIVE GOODS AND METHOD FOR PRODUCING SAID PACKAGING MATERIAL |
EP16750757.3 |
2016-08-04 |
EP3334662A1 |
2018-06-20 |
PETERSSON, Marcus; BALOGH, Joakim |
A packaging material for packaging of light-sensitive goods, said packaging material comprising a first layer and a second layer, at least one hole penetrating said first layer and being covered by said second layer, and a light barrier, wherein said light barrier comprises a layer of ink being essentially nontransparent to light and provided on said second layer to at least partly cover said hole. The disclosure further relates to a method for providing a light barrier covering a hole in a packaging material as well as to a package for packaging of light-sensitive goods. |
180 |
2-DIMENSIONAL CARBON MATERIAL |
EP16731305.5 |
2016-06-17 |
EP3310708A1 |
2018-04-25 |
LIVINGSTON, Andrew Guy; KARAN, Santanu; SAIZ GUTIERREZ, Eduardo; GARCIA ROCHA, Victoria; JIANG, Zhiwei |
2-dimensional carbon thin films are described, as well as their processes of preparation, and their specific uses. The 2-dimensional carbon thin films are fabricated by preparing an organic polymeric thin film precursor, which is then subjected to a carbonisation process to remove at least some of the non-carbon atoms. Using the disclosed process, 2-dimensional carbon thin films having improved dimensional characteristics can be reliably prepared, which presents clear advantages in applications which have until now been restricted to the use of 2-dimensional carbon thin films having less useful dimensions. |