| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | JPS5317634B2 - | JP8342676 | 1976-07-13 | JPS5317634B2 | 1978-06-09 | |
| 62 | 캡슐화된 렌즈 재귀반사형 시팅 | KR1020037013014 | 2002-03-06 | KR1020030085093A | 2003-11-01 | 레벤스타인,세스 |
| 본 발명에 따라, 개선된 결합제층(11)을 함유하는 캡슐화된-렌즈 재귀반사형 시팅(10)이 개시된다. 이 결합제층(11)은 (A) 염화비닐 공중합체, (B) 열가소성 폴리우레탄, 및 (C) 아미노플라스트 수지를 포함하는 필름-형성 혼합물로부터 얻어진다. 그러한 결합제층은 금속화된 비드들(14)에 대해서 및 아크릴 필름들 등의 각종 커버 필름들(15)에 대한 개선된 접착성을 나타낸다. | ||||||
| 63 | FLOORING ASSEMBLY WITH HEAT DISSIPATION LAYER | EP13753764.3 | 2013-08-19 | EP2909394A2 | 2015-08-26 | DESING, James, E.; BIDDLE, Andrew, J. |
| A composite, heat dissipating panel for a compartment includes a panel made up of a first skin, a second skin positioned below the first skin, and a core encapsulated within the panel between the first and second skins and peripheral closeouts. A heat dissipation layer is provided in the panel at or above the first skin. | ||||||
| 64 | FEUERFESTES LAMINAT | EP11770344.7 | 2011-09-21 | EP2619002A1 | 2013-07-31 | ULLRICH, Gerald; HORVATH, Michael; KETZER, Michael; GLEICH, Klaus, Friedrich |
| Laminate comprises: (a) a symmetrically or asymmetrically arranged laminate core made of a matrix comprising organic binder resin, inorganic fillers and inorganic and/or organic fibers; (b) at least one supporting layer applied on at least one of the two surfaces of the laminate core; (c) at least one adhesive layer applied on the surface of the supporting layer facing away from the laminate core; and (d) at least one decorative layer that is applied on the surface of the adhesive layer facing away from the laminate core, where the decorative layer is formed multilayered. Laminate comprises: (a) a symmetrically or asymmetrically arranged laminate core made of a matrix comprising (in wt.%) organic binder resin (17), inorganic fillers (45-85) and inorganic and/or organic fibers (10-25); (b) at least one supporting layer comprising at least one layer, preferably at least two layers made of textile fabric exhibiting an end solidified B-stage binder portion of 5-30 wt.%, based on the total weight of the textile surface with the binder after its conversion into B-stage state, applied on at least one of the two surfaces of the laminate core; (c) at least one adhesive layer comprising at least one layer, preferably at least two layers made of textile fabric exhibiting an end solidified B-stage binder portion of 40-80 wt.%, based on the total weight of the textile surface with the binder after its conversion into B-stage state, applied on the surface of the supporting layer facing away from the laminate core; and (d) at least one decorative layer that is applied on the surface of the adhesive layer facing away from the laminate core, where the decorative layer is formed multilayered. The laminate core is formed multilayered, where the individual core layers after completion of product, are connected inseparably with each other and also with underlying and overlying functional layers. The laminate core exhibits: a density of at least 1.70 g/cm 3>, preferably at least 1.80 g/cm 3>determined according to EN ISO 1183-1:2004; a flexural strength of at least 35 MPa, preferably at least 45 MPa, determined according to EN ISO 178:2003; and a flexural modulus of at least 7 GPa, preferably at least 8.5 GPa, determined according to EN ISO 178:2003. Independent claims are also included for: (1) a laminate precursor comprising (i) a symmetrically or asymmetrically arranged laminate core exhibiting at least two layers, preferably at least three layers made of mineral filled textile fabric, which is solidified with a binder portion (5-20 wt.%, based on the total weight of the fabric with the binder), and is impregnated with a core formulation (60-90 wt.%) comprising (in wt.%) thermally curable natural and/or synthetic resin (1-20, preferably 8-12), inorganic fillers (40-90, preferably 50-75) and diluting water (1-30, preferably 9-18), where the obtained core layers are dried upto a residual water content of upto 8 wt.%, preferably upto 5 wt.% and the resin is converted into a reactive B-stage state, component (b), component (c), and component (d); and (2) producing the laminate, comprising (A) forming or introducing the symmetrically or asymmetrically arranged laminate core, (B) supplying at least one supporting layer, which is applied on at least one of the two surfaces of the laminate core, (C) supplying at least one adhesive layer, which is applied on the surface of the supporting layer facing away from the laminate core, (D) supplying at least one decorative layer, which is applied on the surface of the adhesive layer facing away from the laminate core, and (E) laminating the above layers under the influence of pressure and temperature. | ||||||
| 65 | LAMINATE FOR USE AS OUTER COVERING OF BATTERY AND SECONDARY BATTERY | EP02762933 | 2002-08-30 | EP1422767A4 | 2006-03-15 | ARAO HIDEKI; HIROMITSU MASASHI; GOTO TAKAKAZU; TANAKA KAZUYA; SHIMIZU AKIO; MORITA RYOJI |
| The present invention relates to a laminate for battery encasement comprising aluminum foil and an inner layer, wherein a resin film layer that comprises an aminated phenol polymer (A), an acrylic polymer (B), a phosphorus compound (C), and a zirconium compound (D) lies between the aluminum foil and the inner layer. The laminate for battery encasement of the present invention is excellent in adhesiveness, gas impermeability, etc., and therefore can be suitably used as a material for encasing a secondary battery, particularly a lithium ion polymer secondary battery. | ||||||
| 66 | VERFAHREN ZUR HERSTELLUNG VON LAGERMATERIALIEN SOWIE NACH DIESEM VERFAHREN HERGESTELLTE LAGERMATERIALIEN UND VERWENDUNG DER LAGERMATERIALIEN | EP02779124.3 | 2002-09-24 | EP1436144A1 | 2004-07-14 | ADAM, Achim; FUCHSBERGER, Stefan; SCHLÜTER, Joachim |
| Disclosed is a method for the production of support materials, wherein a web of a metal support fabric is continuously provided with a sliding layer covering the support fabric on one side and predominantly containing polytetrafluorethylene (PTFE). The support fabric is coated with a paste made of the material of the sliding layer and one side of said support fabric is guided in full contact with another web of material during the coating process. | ||||||
| 67 | VERFAHREN ZUR HERSTELLUNG VON LAGERMATERIALIEN SOWIE NACH DIESEM VERFAHREN HERGESTELLTE LAGERMATERIALIEN UND VERWENDUNG DER LAGERMATERIALIEN | EP02776717.7 | 2002-09-24 | EP1429902A1 | 2004-06-23 | ADAM, Achim; FUCHSBERGER, Stefan; SCHLÜTER, Joachim |
| A method for the production of bearing materials is disclosed, in which a strip of a metallic woven support is continuously provided with a slip layer mostly comprising polytetrafluoroethylene (PTFE), covering one side thereof. The woven support is coated on one side with a paste of the material for the slip layer, whereby the woven support runs with the lower surface thereof in full-surface contact with a roller during and directly after the coating. | ||||||
| 68 | ARTICLE COMPOSITE ET PROCEDE DE FABRICATION DE CELUI-CI | EP95918023.0 | 1995-04-18 | EP0756540A1 | 1997-02-05 | CASSAT, Robert; FAURE, Jean-Paul |
| A composite material and a method for making same are disclosed. A composite article including an electrically and/or thermally insulating substrate and protective layers on each side thereof is particularly disclosed. Said material includes protective layers consisting of fibres of a heat-stable material flocked onto the insulating substrate, and a heat-stable coating resin. The resulting protective layer has improved protective properties, particularly moisture-proofness. The composite material may also be used as a metal layer carrier for forming flexible printed electrical circuits. | ||||||
| 69 | Honeycomb noise attenuation structure | EP91303436.9 | 1991-04-17 | EP0509166A1 | 1992-10-21 | Rose, Philip M.; Yu, Jia |
A double layer structural honeycomb sandwich noise suppression panel (10) for use in severe environments such as aircraft turbine engine housings. Two honeycomb core sheets (12) having multiple cells transverse to the sheets are sandwiched around and bonded to a septum sheet (14) consisting of a wire cloth sheet alone or bonded to a sheet of perforated material. A thin sheet of impervious material (16) is bonded to one surface of the sandwich and a facing (18) of thin perforated sheet material is bonded to the other sandwich surface. The panel has improved simplicity, structural strength with unusually light weight. |
||||||
| 70 | FLOORING ASSEMBLY WITH HEAT DISSIPATION LAYER | EP17190230.7 | 2013-08-19 | EP3282067A3 | 2018-07-18 | DESING, James E.; BIDDLE, Andrew J. |
A composite, heat dissipating panel for a compartment includes a panel made up of a first skin, a second skin positioned below the first skin, and a core encapsulated within the panel between the first and second skins and peripheral closeouts. A heat dissipation layer is provided in the panel at or above the first skin. |
||||||
| 71 | FLOORING ASSEMBLY WITH HEAT DISSIPATION LAYER | EP17190230.7 | 2013-08-19 | EP3282067A2 | 2018-02-14 | DESING, James E.; BIDDLE, Andrew J. |
A composite, heat dissipating panel for a compartment includes a panel made up of a first skin, a second skin positioned below the first skin, and a core encapsulated within the panel between the first and second skins and peripheral closeouts. A heat dissipation layer is provided in the panel at or above the first skin. |
||||||
| 72 | METALLIC COATING OF COMPOSITE MATERIALS | EP07858781.3 | 2007-12-06 | EP2102388A1 | 2009-09-23 | CORDON, Thomas Joseph; STEELE, Mark Raymond |
| 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 (10) comprising a resin-based composite material (12) with a metallic coating (14) on a surface, or part surface (16) thereof, the metallic coating (14) comprising an outer electroplated preform, and an inner keying structure (20) which is located generally between said electroplated preform (18) and the composite material (12) to provide attachment of the electroplated preform (18) on the composite material (12). | ||||||
| 73 | VERFAHREN ZUR HERSTELLUNG VON LAGERMATERIALIEN UND VERWENDUNG DER NACH DIESEM VERFAHREN HERGESTELLTEN LAGERMATERIALIEN | EP02776717.7 | 2002-09-24 | EP1429902B1 | 2008-02-27 | ADAM, Achim; FUCHSBERGER, Stefan; SCHLÜTER, Joachim |
| A method for the production of bearing materials is disclosed, in which a strip of a metallic woven support is continuously provided with a slip layer mostly comprising polytetrafluoroethylene (PTFE), covering one side thereof. The woven support is coated on one side with a paste of the material for the slip layer, whereby the woven support runs with the lower surface thereof in full-surface contact with a roller during and directly after the coating. | ||||||
| 74 | BAUPLATTE | EP04709570.8 | 2004-02-10 | EP1511623B1 | 2006-05-17 | HASCH, Joachim; GOTTFRIED, Stefan |
| The invention relates to a building board used as a ceiling or wall element for building construction. The inventive building board is characterised in that it consists in a plurality of OSB boards (1, 2, 3; 1a, 2a, 3a; 1b, 2b, 3b) which are disposed side by side and interconnected by multilayer bonding. | ||||||
| 75 | BALLISTIC RESISANT AND FIRE RESISTANT COMPOSITE ARTICLES | EP03808186.5 | 2003-10-09 | EP1560709A2 | 2005-08-10 | NGUYEN, Huy, X.; DICKSON, Larry |
| Ballistically resistant and fire resistant composite articles for aircraft interiors and other applications. Composite articles are provided having a flexural modulus of at least about 80,000 lbs/sq. in (552 MPa), a flexural strength at yield of at least about 800 lbs/sq. in. (5.52 MPa), an areal density of about 0.9 lb/ft2 (4.40 kg/m2) to about 1.5 lb/ft2 (5.86 kg/m2), a fire resistance meeting the requirements of §25.853 Title 14 of the United States Code, Jan. 1, 2002, and a V0 velocity of at least about 1430 ft/sec (427 m/s) when tested by United States Federal Aviation Administration Advisory Circular 25.795.2, 10 Jan. 2002, using .44 Magnum Jacketed Hollow Point (JHP) bullets of 240 grains (15.6 g) mass and using 9 mm Full Metal Jacketed, Round Nose (FMJ RN) bullets of 124 grains (8.0 g) mass. | ||||||
| 76 | LAMINATE FOR USE AS OUTER COVERING OF BATTERY AND SECONDARY BATTERY | EP02762933.6 | 2002-08-30 | EP1422767A1 | 2004-05-26 | ARAO, Hideki c/o DAI NIPPON PRINTING CO., LTD.; HIROMITSU,Masashi c/o DAI NIPPON PRINTING CO.,LTD.; GOTO, Takakazu c/o DAI NIPPON PRINTING CO., LTD.; TANAKA, Kazuya c/o NIHON PARKERIZING CO., LTD.; SHIMIZU, Akio c/o NIHON PARKERIZING CO., LTD.; MORITA, Ryoji c/o NIHON PARKERIZING CO., LTD. |
The present invention relates to a laminate for battery encasement comprising aluminum foil and an inner layer, wherein a resin film layer that comprises an aminated phenol polymer (A), an acrylic polymer (B), a phosphorus compound (C), and a zirconium compound (D) lies between the aluminum foil and the inner layer. The laminate for battery encasement of the present invention is excellent in adhesiveness, gas impermeability, etc., and therefore can be suitably used as a material for encasing a secondary battery, particularly a lithium ion polymer secondary battery. |
||||||
| 77 | SYNTACTIC FOAM SHEET MATERIAL | EP95929401 | 1995-07-27 | EP0772516A4 | 1998-11-25 | MEREER CHARLES L; PHILIPPS THOMAS E |
| A syntactic structural foam product (10) in flat sheet form or curved three-dimensional form adaptable to such uses as a light weight structural core for composite laminates, is made of a mixture of hollow ceramic microspheres (11, 12) and dry resin powder (14), of either thermosetting or a high-temperature thermoplastic resin, distributed in the interstices of the mass of microspheres for integration of the mixture into desired form upon heating and cooling. Resin powder collected as a waste by-product from resin coating materials can be recycled in the production of the desired product. The foam product is produced by first intermixing the microspheres and powdered resin by physical agitation of the mixture and depositing the mixture as a layer over a surface having a release agent thereover within a dimension defining region between boundary members and then supplying heat with or without pressure to the layer at a temperature and for a time period sufficient to effect a melting of the resin powder and thereafter cooling the resin in a hardened condition to integrate the mixture into the product desired after which the product is withdrawn from the forming zone. Reinforcing elements such as glass or carbon fibers (15) can be selectively included in the mixture for predetermined desired physical and mechanical properties. | ||||||
| 78 | SYNTACTIC FOAM SHEET MATERIAL | EP95929401.0 | 1995-07-27 | EP0772516A1 | 1997-05-14 | MEREER, Charles, L.; PHILIPPS, Thomas, E. |
| A syntactic structural foam product (10) in flat sheet form or curved three-dimensional form adaptable to such uses as a light weight structural core for composite laminates, is made of a mixture of hollow ceramic microspheres (11, 12) and dry resin powder (14), of either thermosetting or a high-temperature thermoplastic resin, distributed in the interstices of the mass of microspheres for integration of the mixture into desired form upon heating and cooling. Resin powder collected as a waste by-product from resin coating materials can be recycled in the production of the desired product. The foam product is produced by first intermixing the microspheres and powdered resin by physical agitation of the mixture and depositing the mixture as a layer over a surface having a release agent thereover within a dimension defining region between boundary members and then supplying heat with or without pressure to the layer at a temperature and for a time period sufficient to effect a melting of the resin powder and thereafter cooling the resin in a hardened condition to integrate the mixture into the product desired after which the product is withdrawn from the forming zone. Reinforcing elements such as glass or carbon fibers (15) can be selectively included in the mixture for predetermined desired physical and mechanical properties. | ||||||
| 79 | 導電性ロールおよびその製造方法 | JP2013199866 | 2013-09-26 | JP6099535B2 | 2017-03-22 | 笹木原 直明; 鵜飼 浩; 竹山 可大 |
| 80 | Metal coating of the composite material | JP2009540840 | 2007-12-06 | JP5450086B2 | 2014-03-26 | トマス・ジョセフ・コードン; マーク・レイモンド・スティール |
QQ群二维码
意见反馈
意见反馈