子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | JPS4961271A - | JP5709673 | 1973-05-22 | JPS4961271A | 1974-06-13 | |
| 122 | FUSED SHEET FOR ELECTROMAGNETIC WAVE ABSORPTION-EXTINCTION AND SHIELDING, AND FOR ELECTRONIC EQUIPMENT HIGH HEAT DISSIPATION, AND METHOD OF MANUFACTURING THE SAME | US15317154 | 2016-09-06 | US20180162098A1 | 2018-06-14 | Hak Sik JOO |
| The present invention discloses a fused sheet for electromagnetic wave absorption/extinction and shielding, and for electronic equipment high heat dissipation. The fused sheet for electromagnetic wave absorption/extinction and shielding, and for electronic equipment high heat dissipation of the present invention includes a premolded graphite sheet prepared by molding a graphite substrate into a sheet form having a density in a range of 0.1-1.5 g/cm3 and an incomplete state of crystal structure; and a porous metal sheet having a plurality of pores connected to upper and lower surfaces of the porous metal sheet, wherein the premolded graphite sheet is stacked on one surface of the porous metal sheet, and press molded to be integrally attached and combined, so as to have a density of 1.6 g/cm3-6.0 g/cm3 | ||||||
| 123 | Three-Dimensional Printed Composite Articles | US14835697 | 2015-08-25 | US20180141305A9 | 2018-05-24 | Robert Swartz; Buckley Crist; Eugene Gore; Joseph M. Jacobson |
| A 3D object according to the invention comprises substrate layers infiltrated by a hardened material. The 3D object is fabricated by a method comprising the following steps: Position powder on all or part of a substrate layer. Repeat this step for the remaining substrate layers. Stack the substrate layers. Transform the powder into a substance that flows and subsequently hardens into the hardened material. The hardened material solidifies in a spatial pattern that infiltrates positive regions in the substrate layers and does not infiltrate negative regions in the substrate layers. In a preferred embodiment, the substrate is carbon fiber and excess substrate is removed by abrasion. | ||||||
| 124 | Methods for Fabricating Three-Dimensional Printed Composites | US14835685 | 2015-08-25 | US20180126666A9 | 2018-05-10 | Robert Swartz; Buckley Crist; Eugene Gore; Joseph M. Jacobson |
| A 3D object according to the invention comprises substrate layers infiltrated by a hardened material. The 3D object is fabricated by a method comprising the following steps: Position powder on all or part of a substrate layer. Repeat this step for the remaining substrate layers. Stack the substrate layers. Transform the powder into a substance that flows and subsequently hardens into the hardened material. The hardened material solidifies in a spatial pattern that infiltrates positive regions in the substrate layers and does not infiltrate negative regions in the substrate layers. In a preferred embodiment, the substrate is carbon fiber and excess substrate is removed by abrasion. | ||||||
| 125 | OUTER COATING FOR SHIP HULL | US15572088 | 2016-05-25 | US20180094144A1 | 2018-04-05 | Christian BUMM |
| The invention relates to an outer coating of a ship's hull in the underwater area, wherein the coating comprises a bottom layer on the hull exterior, said layer being made of an adhesive or an ethylene-propylene-diene rubber and being particularly designed as a film, and a superimposed top layer made of an ultra high-molecular weight polyethylene. | ||||||
| 126 | WET COATING COMPOSITIONS FOR PAPER SUBSTRATES, PAPER SUBSTRATES COATED WITH THE SAME AND PROCESS FOR COATING A PAPER SUBSTRATE WITH THE SAME | US15809600 | 2017-11-10 | US20180072915A1 | 2018-03-15 | Yvon MONGRAIN; Guillaume TURGEON |
| A wet coating composition useful for coating a cellulosic fiber-based substrate is provided. The composition includes two aqueous emulsions. The first emulsion includes an oxidized paraffin/polyethylene wax and the second emulsion includes an ethylene/acrylic acid copolymer wax, ethylene/acrylic amide copolymer wax, ethylene/acrylic acid/acrylic amide copolymer wax or a mixture thereof. The oxidized paraffin/polyethylene wax has a surface energy less than or equal to 25 mN/m being substantially dispersive energy. The wet coating composition when dried forms a coating having a surface energy ranging from 20 to 60 mN/m being the sum of dispersive and polar energies. A process for treating a cellulosic fiber-based substrate with the wet coating composition, a substrate coated and articles including the coated substrate are also described. The process involves a heating step to allow migration of the coating towards a core of the cellulosic fiber-based substrate. | ||||||
| 127 | Fiber architecture optimization for ceramic matrix composites | US14208407 | 2014-03-13 | US09908305B2 | 2018-03-06 | Adam L. Chamberlain; Andrew J. Lazur |
| Creating a ceramic matrix structure may include alternating different layers of fiber fabric to achieve porosity, infiltration, and/or other objectives. Different layers of the ceramic matrix structure may be configured differently to achieve different objectives in different regions of the ceramic matrix structure. The fiber tow spacing, fiber count and/or other characteristics may be varied within individual layers and/or among different layers of the ceramic matrix structure. | ||||||
| 128 | Fiber-reinforced composite material and method for manufacturing the same | US14614831 | 2015-02-05 | US09890483B2 | 2018-02-13 | Koichiro Hayashi |
| A fiber-reinforced composite material for increasing adhesive strength between a first composite material layer including a fibrous substrate with reinforcement fiber bundles arranged crosswise, and a second composite material layer including second reinforcement fibers arranged randomly. The first composite material layer including a fibrous substrate having reinforcement fiber bundles crossing and being drawn and aligned first reinforcement fibers; and first thermoplastic resin, with at least each of the reinforcement fiber bundles is impregnated; and a second composite material layer including second reinforcement fibers arranged randomly in second thermoplastic resin. The first composite material layer and the second composite material layer bonded to each other. The first composite material layer has bores on at least a surface thereof that is to be bonded with the second composite material layer. The second reinforcement fibers and the second thermoplastic resin enter into the bores. | ||||||
| 129 | PERFORATED CERAMIC MATRIX COMPOSITE PLY, CERAMIC MATRIX COMPOSITE ARTICLE, AND METHOD FOR FORMING CERAMIC MATRIX COMPOSITE ARTICLE | US15146288 | 2016-05-04 | US20170320232A1 | 2017-11-09 | Peter de DIEGO |
| A ceramic matrix composite article, method for forming the article, and perforated ply which may be incorporated therein are disclosed. The article includes at least one shell ply forming an exterior wall having first and second portions and defining a plenum. An annular brace formed of at least one structural support ply is disposed within the plenum, including a first integral portion integral with and part of the first portion of the exterior wall, a first curved portion extending from the first integral portion and curving across the article plenum to the second portion of the exterior wall, a second integral portion integral with and part of the second portion of the exterior wall, a second curved portion extending from the second integral portion and curving across the article plenum to the first curved portion, and an overlap in which the first and second curved portions are integral. | ||||||
| 130 | COMPOSITE STRUCTURE AND MANUFACTURING METHOD THEREOF | US15125518 | 2015-03-11 | US20170291387A1 | 2017-10-12 | Yuji YAMASHITA; Kiyohito KONDO; Takeki MATSUMOTO; Hirokazu KAWABE; Yoshiteru INAMOTO |
| A composite structure having a laminated structure made of fiber reinforced plastic and metallic material comprises a base member(s) made of metallic material; and a reinforcement member(s) made of fiber reinforced plastic, the reinforcement member(s) comprising: a first reinforcement part(s) made of fiber reinforced plastic including reinforcement fibers which are aligned in a uni-direction, and a second reinforcement part(s) made of fiber reinforced plastic including at least reinforcement fibers which are aligned in a crossing direction relative to the uni-direction in which the reinforcement fibers of the first reinforcement part(s) are aligned, and interposed between the base member(s) and the first reinforcement part(s), the reinforcement member(s) further comprising a thermosetting resin included in a bonding site with the base member(s). | ||||||
| 131 | Methods and apparatus for three-dimensional printed composites based on flattened substrate sheets | US14703372 | 2015-05-04 | US09776376B2 | 2017-10-03 | Robert Swartz; Buckley Crist; Eugene Gore; Joseph M. Jacobson |
| A 3D object according to the invention involves substrate layers infiltrated by a hardened material. The 3D object may be fabricated by a method comprising the following steps: Flatten a substrate layer. Position powder on all or part of a substrate layer. Repeat this step for the remaining substrate layers. Stack the substrate layers. Transform the powder into a substance that flows and subsequently hardens into the hardened material. The hardened material solidifies in a spatial pattern that infiltrates positive regions in the substrate layers and does not infiltrate negative regions in the substrate layers. In a preferred embodiment, the substrate is carbon fiber and excess substrate is removed by abrasion. | ||||||
| 132 | COMPOSITE BODY AND METHOD FOR PRODUCING SAME | US15328723 | 2015-07-24 | US20170239715A1 | 2017-08-24 | Takeshi MIYAKAWA; Hideki HIROTSURU |
| A composite production method includes impregnating a plate-shaped porous inorganic structure and a fibrous inorganic material with a metal while the fibrous inorganic material is arranged to be adjacent to the porous inorganic structure. In the composite structure, first and second phases are adjacent to each other by using a porous inorganic structure having a porous silicon carbide ceramic sintered body and the fibrous inorganic material, the first phase being a phase in which the porous silicon carbide ceramic sintered body is impregnated with the metal, the second phase being a phase in which the fibrous inorganic material is impregnated with the metal, a percentage of the porous silicon carbide ceramic sintered body in the first phase is 50 to 80 volume percent, and a percentage of the fibrous inorganic material in the second phase is 3 to 20 volume percent. A composite is produced by the method. | ||||||
| 133 | ALUMINUM-SILICON CARBIDE COMPOSITE AND PRODUCTION METHOD THEREFOR | US15500210 | 2015-07-29 | US20170236767A1 | 2017-08-17 | Takeshi MIYAKAWA; Motonori KINO; Hideki HIROTSURU |
| An aluminum-silicon carbide composite including flat-plate-shaped composited portion containing silicon carbide and an aluminum alloy, and aluminum layers containing an aluminum alloy provided on both plate surfaces of composited portion, wherein circuit board is mounted on one plate surface and the other plate surface is used as heat-dissipating surface, wherein: the heat-dissipating-surface-side plate surface of the composited portion has a convex curved shape; the heat-dissipating-surface-side aluminum layer has a convex curved shape; ratio (Ax/B) between the average (Ax) of the thicknesses at the centers on opposing short sides of outer peripheral surfaces and thickness (B) at central portions of the plate surfaces satisfies the relationship: 0.91≦Ax/B≦1.00; and a ratio (Ay/B) between the average (Ay) of the thicknesses at the centers on opposing long sides of outer peripheral surfaces and thickness (B) at central portions of the plate surfaces satisfies the relationship: 0.94≦Ay/B≦1.00 and production method therefor. | ||||||
| 134 | METHOD FOR PRODUCING A DOUBLE-WALLED THERMOSTRUCTURAL MONOLITHIC COMPOSTE PART, AND PART PRODUCED | US15514900 | 2015-09-24 | US20170217843A1 | 2017-08-03 | Marc BOUCHEZ; Steffen BEYER; Stephan Schmidt-Wimmer |
| A fibrous preform (1) is produced, provided with a sandwich structure comprising an intermediate flexible core (4) and two outer fibrous frames (2, 3), respectively arranged on opposing outer faces of said flexible core (4) and assembled by sections of wire (8, 9) passing through said fibrous frames (2, 3), said preform (1) being impregnated with resin. Said preform is then hardened and the core (4) is removed, preferably by pre-densification with chemical vapour infiltration, and the structure produced is then densified with liquid-phase infiltration. | ||||||
| 135 | SYSTEM OF ANTICORROSIVE PROTECTION OF METALLIC CONDUCTING PIPES AND/OR FOUNDATION BASED ON HIGH DENSITY POLYETHYLENE | US14705801 | 2015-05-06 | US20170205019A1 | 2017-07-20 | Jorge Walter Hirales Fragosa |
| The present invention relates to a system of the anticorrosive protection of metallic conducting pipes or foundation. | ||||||
| 136 | METHOD AND ARRANGEMENT FOR PRE-CURING AN ADHESIVE LAYER | US14967330 | 2015-12-13 | US20170136755A1 | 2017-05-18 | Andrew Vaughan; Julien Richeton |
| The invention provides a method for pre-curing an adhesive layer bonding a first component to a second component. The adhesive layer is heated by treating an adhesive layer component as heating the first component with a pair of electrodes that are in electrical contact with a surface of the first component, the pair of electrodes applying a predetermined electrical current (I1, I2) to the first component. The invention further provides an arrangement for pre-curing a layer of adhesive. | ||||||
| 137 | SEGMENTED FLEXIBLE GEL COMPOSITES AND RIGID PANELS MANUFACTURED THEREFROM | US15367986 | 2016-12-02 | US20170081495A1 | 2017-03-23 | Owen R. Evans; Irene Melnikova |
| The present invention describes various methods for manufacturing gel composite sheets using segmented fiber or foam reinforcements and gel precursors. Additionally, rigid panels manufactured from the resulting gel composites are also described. The gel composites are relatively flexible enough to be wound and when unwound, can be stretched flat and made into rigid panels using adhesives. | ||||||
| 138 | FIBROUS PREFORMS FOR USE IN MAKING COMPOSITE PARTS | US15199474 | 2016-06-30 | US20160311175A1 | 2016-10-27 | Jean-Marc Beraud; Jean-Florent Lamethe; Jean-Christophe Minni |
| The present invention concerns preforms made with a new intermediate material composed of a unidirectional layer of carbon fibers with a weight of 100 to 280 g/m2, associated on each of its faces, with a web of thermoplastic fibers having a thickness of 0.5 to 50 microns, preferably 3 to 35 microns, the intermediate material having a total thickness of 80 to 380 microns, preferably from 90 to 320 microns, and a process for manufacturing composite parts from such preforms and the resulting composite parts. | ||||||
| 139 | INTERSCALAR INTEGUMENT POSITION SETTING METHOD AND MANUFACTURE | US15094581 | 2016-04-08 | US20160298202A1 | 2016-10-13 | Mark Tovar |
| A method is disclosed for setting the interscalar integument of a reptile shed for incorporation into a laminar composite. The method includes saturating the reptile shed in a saturating liquid, positioning the saturated reptile shed on a lower platen of a press, lowering an upper platen of the press to contact the saturated reptile shed, flash drying the saturated reptile shed by simultaneously applying heat and pressure using the upper and lower platens for a fixed period of time. | ||||||
| 140 | BIOCIDAL ARTICLE WITH PATTERNED ADHESIVE LAYER | US14645762 | 2015-03-12 | US20160262380A1 | 2016-09-15 | Ronald Steven Cok |
| A biocidal article includes a biocidal material layer having edges, an exposed side, and an adhesive side opposing the exposed side. A patterned adhesive layer is located in contact with the adhesive side and extends to the edges of the biocidal material layer. The patterned adhesive layer includes a non-biocidal portion and a biocidal portion. The biocidal portion includes biocidal materials and extends to at least one edge. | ||||||
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