| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 181 | HEATED FLOOR PANELS WITH THERMALLY CONDUCTIVE AND ELECTRICALLY INSULATING FABRIC | US15385494 | 2016-12-20 | US20180176989A1 | 2018-06-21 | Jin Hu; Galdemir Cezar Botura |
| A floor panel assembly includes an insulating layer which protects a sheet heater, first and second structural layers, and a honeycomb layer for support. The floor panel assembly allows for heating of the cabin of an aircraft without mechanical damage to the sheet heater. | ||||||
| 182 | MULTILAYER BODY AND ELECTRONIC COMPONENT | US15879469 | 2018-01-25 | US20180166216A1 | 2018-06-14 | Hiroshige ADACHI |
| A multilayer body includes a multilayer structure including a glass ceramic layer including a glass and a filler and a ferrite layer including a ferrite, in which the glass ceramic layer has a glass content of about 30.0% or more by weight and about 80.0% or less by weight and a filler content of about 20.0% or more by weight and about 70.0% or less by weight, the glass included in the glass ceramic layer includes about 0.5% or more by weight and about 5.0% or less by weight R2O (R represents at least one selected from the group consisting of Li, Na, and K), about 0% or more by weight and about 5.0% or less by weight Al2O3, about 10.0% or more by weight and about 25.0% or less by weight B2O3, and about 70.0% or more by weight and about 85.0% or less by weight SiO2 based on the total weight of the glass, and the filler included in the glass ceramic layer includes at least one of SiO2 and Al2O3 and also includes about 5.0% or more by weight and about 15.0% or less by weight of a ferrite based on the total weight of the glass and the filler. | ||||||
| 183 | Method of bonding a metallic component to a non-metallic component using a compliant material | US14601520 | 2015-01-21 | US09969654B2 | 2018-05-15 | Benjamin T. Fisk; Grant O. Cook, III |
| A means for attaching a metallic component to a non-metallic component using a compliant material having thermal properties intermediate those of the metallic component to a non-metallic component is provided. The method can accommodate CTE mismatches and wear-type problems common to many assemblies of dissimilar materials. In particular, the method provides a sufficient wear surface to accommodate relative motion and provide a durable wear surface that does not excessively wear/gall/mico-weld itself together and provides the necessary damping and motion for proper operation in aeronautical applications. | ||||||
| 184 | Method for forming CMC article | US15479872 | 2017-04-05 | US09931818B1 | 2018-04-03 | Jason Robert Parolini; Jon Conrad Schaeffer; Arthur S. Peck; Srikanth Chandrudu Kottilingam; Canan Uslu Hardwicke |
| A method for forming a CMC article is disclosed, including forming a CMC precursor ply assembly. Forming the CMC precursor ply assembly includes laying up a plurality of CMC precursor plies and entraining a melt infiltration agent to form an entrained agent supply. Each of the plurality of CMC precursor plies includes a matrix precursor and a plurality of ceramic fibers. The plurality of CMC precursor plies and the entrained agent supply are arranged to form the CMC precursor ply assembly, which includes an article conformation. The method further includes carbonizing the CMC precursor ply assembly, infusing the melt infiltration agent from the entrained agent supply into the plurality of CMC precursor plies, and densifying the CMC precursor ply assembly with the melt infiltration agent to form the CMC article. | ||||||
| 185 | Structural polyurethane adhesive | US14779847 | 2014-05-14 | US09914862B2 | 2018-03-13 | Steffen Kelch; Wolfgang Roock; Florian Ittrich |
| The present invention relates to a two-component polyurethane adhesive consisting of a polyol component and a polyisocyanate component, wherein the polyol component comprises a triol with a molar mass of 1,000 to 10,000 g/mol, a diol having two primary hydroxy groups and a molar mass of 60 to 150 g/mol, a poly(trimethylene oxide) diol or a poly(tetramethylene oxide) diol with a molar mass of 200 to 3,000 g/mol and an aliphatic polyamine. The adhesive is characterized by high early strength, a low temperature dependence of the mechanical properties, good adhesion and the possibility of controlled thermally induced release of adhesion. | ||||||
| 186 | Producing electrophoretic display with seamless front surface | US14686681 | 2015-04-14 | US09862176B1 | 2018-01-09 | Robert Zehner |
| Methods and systems for producing an electro-optic display with a barrier layer for a seamless front surface of a user device. One method of manufacturing includes the following: providing a backplane comprising at least one electrode; disposing a first layer of lamination adhesive above the backplane; disposing a layer of electro-optic material above the first layer of lamination adhesive; disposing a second layer of lamination adhesive above the layer of electro-optic material; disposing a barrier layer, supported by a release film, above the second layer of lamination adhesive; applying a sealing material to peripheral portions of the backplane to form an underfill edge seal between the backplane and the barrier layer; removing the release film; and disposing a front-surface material above the barrier layer. | ||||||
| 187 | HANDHELD MOBILE DEVICE WITH HIDDEN ANTENNA FORMED OF METAL INJECTION MOLDED SUBSTRATE | US15697373 | 2017-09-06 | US20170373377A1 | 2017-12-28 | Jason Sean Gagne-Keats |
| The disclosed embodiments include a housing of a handheld mobile device. The housing includes a ceramic layer forming a continuous outermost surface of the handheld mobile device, and an antenna layer adjacent to the ceramic layer. The antenna layer including conductive elements formed from a metal injection molded substrate, and an antenna break formed of non-conductive material electrically separating the conductive elements to collectively form an antenna of the handheld mobile device that is hidden by the ceramic layer from an exterior view of the handheld mobile device. | ||||||
| 188 | Toilet pan body and its method of manufacturing | US14382226 | 2013-03-01 | US09834917B2 | 2017-12-05 | Garry Moore |
| A ceramic toilet pan having a raised rear portion to which a hinge tube may be accurately located and fixed in position for example by adhesive using a jig despite variations in pan body size due to ceramic firing, a water pump and air pump being provided for flushing the toilet pan when a seat and lid are in a closed position. The seat and lid are rotationally mounted to the pan by a horizontal hinge pin located in the hinge tube and a latch member is provided for latching the lid and seat closed. A cistern is also provided having an overflow weir. | ||||||
| 189 | LASER PROCESSING OF SAPPHIRE SUBSTRATE AND RELATED APPLICATIONS | US15585305 | 2017-05-03 | US20170291844A1 | 2017-10-12 | Sasha Marjanovic; Garrett Andrew Piech; Sergio Tsuda; Robert Stephen Wagner |
| A method of laser processing a material to form a separated part. The method includes focusing a pulsed laser beam into a laser beam focal line, viewed along the beam propagation direction, directed into the material, the laser beam focal line generating an induced absorption within the material, the induced absorption producing a hole or fault line along the laser beam focal line within the material, and directing a defocused carbon dioxide (CO2) laser from a distal edge of the material over the plurality of holes to a proximal edge of the material. | ||||||
| 190 | Joining dissimilar materials using an epoxy resin composition | US15343468 | 2016-11-04 | US09761374B2 | 2017-09-12 | Chao Li; Stephen John Rigby; Clay Lynwood Fellers; Marco James Mason; Saboura Rokhsair Azar |
| An epoxy resin composition is disclosed for joining dissimilar materials. The identified epoxy resin compositions can fee used to seal metallic and non-metallic components of a capacitor. Specifically the epoxy resin composition can be applied to joints between a non-metallic capacitor bushing and a metallic tank cover and metallic terminal cap. Once the epoxy resin composition is cored, it can provide a seal that can withstand the stresses and environmental conditions to which a capacitor is subjected. | ||||||
| 191 | ELECTRODE PATTERN FORMING METHOD AND ELECTRIC COMPONENT MANUFACTURING METHOD | US15395059 | 2016-12-30 | US20170207026A1 | 2017-07-20 | Kunio IWAKOSHI; Seiji GOTO |
| An electrode pattern forming method capable of forming an electrode pattern having a desired thickness in each of a plurality of areas on an identical surface by an ink-jet method is provided. In a method of forming an electrode pattern including a first conductive portion and a second conductive portion connected with each other onto a work piece by an ink-jet method, a first area corresponding to at least part of the first conductive portion and a second area corresponding to at least part of the second conductive portion are defined on an identical surface of the work piece, conductive ink droplets are ejected toward the first area and the second area to form the first conductive portion and the second conductive portion, and a resolution of conductive ink droplets differs between the first area and the second area. | ||||||
| 192 | Method of manufacturing flexible display panel and method of manufacturing flexible display apparatus | US14303909 | 2014-06-13 | US09664935B2 | 2017-05-30 | Sun-Ho Kim |
| A method of manufacturing a flexible display panel includes forming an adhesive layer by depositing an inorganic material on a flexible substrate, forming a hydroxyl group on a surface of the adhesive layer by modifying the surface of the adhesive layer, laminating a glass substrate to the modified surface of the adhesive layer and forming a heat-treated layer by heating the glass substrate and the adhesive layer. | ||||||
| 193 | Ceramic laminate sheet with flexibility and preparation method thereof | US13939905 | 2013-07-11 | US09640304B2 | 2017-05-02 | Il Hwan Yoo; Jin Cheol Kim; Tae Kyoung Kim; Dong Gyu Lee; Yu Jin Lee |
| Disclosed is a ceramic laminate sheet comprising a ceramic sheet having a plurality of cracks and a polymer resin layer disposed on one side or both sides of the ceramic sheet, wherein the plurality of cracks pass through the ceramic sheet from one side to the other side thereof, the cracks divide the ceramic sheet into a plurality of pieces, grooves for formation of the cracks are not provided in one side and the other side of the ceramic sheet. | ||||||
| 194 | COMPOSITE THERMAL BARRIER FOR COMBUSTION CHAMBER SURFACES | US15278696 | 2016-09-28 | US20170089260A1 | 2017-03-30 | Dana Craig Bookbinder; Roy Joseph Bourcier; William Edward Lock; Richard Curwood Peterson; Irene Marjorie Slater; Pushkar Tandon; Christopher John Warren |
| A composite thermal barrier and methods of applying the composite thermal barrier to a metallic surface within a combustion chamber of an engine. The composite thermal barrier includes at least one metallic support structure, a metallic skin, and an insulation material. The metallic support structure is connected to a metallic surface within the combustion chamber of the engine. The metallic skin is disposed adjacent to the metallic support structure to define a void space between the metallic skin and the metallic surface. The insulation material is contained within the volume to form the composite thermal barrier. | ||||||
| 195 | Joining Dissimilar Materials Using an Epoxy Resin Composition | US15343468 | 2016-11-04 | US20170053742A1 | 2017-02-23 | Chao Li; STEPHEN JOHN RIGBY; CLAY LYNWOOD FELLERS; MARCO JAMES MASON; SABOURA ROKHSAIR AZAR |
| An epoxy resin composition is disclosed for joining dissimilar materials. The identified epoxy resin compositions can fee used to seal metallic and non-metallic components of a capacitor. Specifically the epoxy resin composition can be applied to joints between a non-metallic capacitor bushing and a metallic tank cover and metallic terminal cap. Once the epoxy resin composition is cored, it can provide a seal that can withstand the stresses and environmental conditions to which a capacitor is subjected. | ||||||
| 196 | Method of Bonding a Metallic Component to a Non-Metallic Component Using a Compliant Material | US14601520 | 2015-01-21 | US20170015596A1 | 2017-01-19 | Benjamin T. Fisk; Grant O. Cook, III |
| A means for attaching a metallic component to a non-metallic component using a compliant material having thermal properties intermediate those of the metallic component to a non-metallic component is provided. The method can accommodate CTE mismatches and wear-type problems common to many assemblies of dissimilar materials. In particular, the method provides a sufficient wear surface to accommodate relative motion and provide a durable wear surface that does not excessively wear/gall/mico-weld itself together and provides the necessary damping and motion for proper operation in aeronautical applications. | ||||||
| 197 | Laminated ceramic electronic component and manufacturing method therefor | US14805491 | 2015-07-22 | US09536669B2 | 2017-01-03 | Akihiro Motoki; Syunsuke Takeuchi; Makoto Ogawa; Seiichi Nishihara; Kenichi Kawasaki; Shuji Matsumoto |
| In a method of forming a plating layer for an external terminal electrode by applying, for example, copper plating to an end surface of a component main body with respective ends of internal electrodes exposed, and then applying a heat treatment at a temperature of about 1000° C. or more in order to improve the adhesion strength and moisture resistance of the external terminal electrode, the plating layer may be partially melted to decrease the bonding strength of the plating layer. In the step of applying a heat treatment at a temperature of about 1000° C. or more to a component main body with plating layers formed thereon, the average rate of temperature increase from room temperature to the temperature of about 1000° C. or more is set to about 100° C./minute or more. This average rate of temperature increase maintains a moderate eutectic state in the plating layer and ensures a sufficient bonding strength of the plating layer. | ||||||
| 198 | LIGHT CONVERTER ASSEMBLIES WITH ENHANCED HEAT DISSIPATION | US15118075 | 2015-03-10 | US20160369954A1 | 2016-12-22 | Maria Anc; Alan Lenef |
| The present disclosure is directed to light converter assemblies with enhanced heat dissipation. A light converter assembly may comprise a confinement material applied to at least a first substrate and a phosphor material also deposited on the first substrate so as to be surrounded by the confinement material. The first substrate may be hermetically sealed to a second substrate using the confinement material so that the phosphor material is confined between the substrates and protected from atmospheric contamination. The substrates may comprise, for example, sapphire to allow for light beam transmission and heat conductance. Confinement materials that may be employed to seal the first substrate to the second substrate may include, for example, silicon or a metal (e.g., silver, copper, aluminum, etc.) The phosphor material may comprise, for example, at least one quantum dot material. | ||||||
| 199 | Solid body joining of a carrier body and a cover layer, particularly by anodic bonding | US14547318 | 2014-11-19 | US09507062B2 | 2016-11-29 | Carsten Pampuch; Khaldoun Halalo; Volker Schmidt |
| In a method for solid body joining of a carrier body (10) and a cover layer (20), in particular by anodic bonding, the cover layer (20) is pressed with a pressing force against a curved carrier body surface (11), wherein the pressing force during the solid body joining is distributed by way of a pressure intermediary device (30) areally and simultaneously over the whole cover layer (20) and is directed perpendicularly to the curvature of the carrier body surface (11). A composite component comprising a carrier body (10) and a cover layer (20) is also disclosed, wherein a curved areal joining region (13) is formed between a cover layer surface (21) and a carrier body surface (11). | ||||||
| 200 | APPARATUS AND METHOD FOR HEAT-SHEILDING FAN DUCT INNER WALL | US14670020 | 2015-03-26 | US20160280355A1 | 2016-09-29 | Rory Lee Deichert |
| A system and method for heat shielding an inner wall of a fan duct of an aircraft nacelle from engine heat. The system may include a heat shield and an insulation blanket. The heat shield may have a first layer of high temperature composite material bonded to a first surface of an insulant material and a second layer of high temperature composite material bonded to a second surface of the insulant material. The first layer of high temperature composite material may also be bonded to the inner wall. The insulation blanket may be positioned between the heat shield and the engine, and may be fastened to the heat shield and/or the inner wall. | ||||||
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