| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 261 | Structural adhesive materials | US12601826 | 2008-06-02 | US08840813B2 | 2014-09-23 | Ian Aspin; Marine Godot |
| An adhesive material comprising at least one adhesive polymeric resin, at least one low aspect ratio metal-coated additive, and at least one high aspect ratio metal-coated additive. There is additionally provided an adhesive material comprising at least one adhesive polymeric resin, and one of either; a) low aspect ratio metal-coated additives present in the range 0.2 wt. % to 30 wt. % of the adhesive material; or b) discrete high aspect ratio metal-coated additives present in the range 0.2 wt. % to 25 wt. % of the adhesive material. | ||||||
| 262 | Adhering method using electrostatic powder adhesive, and powder adhesive to be used in adhering method | US13510106 | 2010-11-26 | US08790755B2 | 2014-07-29 | Takefumi Murai; Yoshimi Shibata |
| Provided is an adhering method which comprises spray-coating an adherend with a powder adhesive and then using the adherend, thereby enabling the formation of an automobile interior part having good heat tolerance and high adhesion strength. The adhering method to be used for forming an automobile interior part involves a step for spray-coating an adherend (4) with a powder adhesive (6) with the use of an electrostatic powder spray gun (5). If necessary, the adhering method may further involve a step for inciting the powder adhesive, which has been spray-coated on the adherend, by heating with an infrared heater. | ||||||
| 263 | Low-CTE, lightweight hybrid materials with high durability in outspace | US13192966 | 2011-07-28 | US08703842B1 | 2014-04-22 | Ming-Yung Chen; Chenggang Chen |
| Light-weight hybrid materials with significantly-reduced coefficient of thermal expansion, low density, and high durability in the aggressive environment such as low-earth orbit are disclosed. The high performance polymer materials can include epoxy, cyanoester, bismalmeide, polyimide, vinylester, polyamide, polyacrylate, and others; with their applications as matrix in the carbon fiber-reinforced or glass fiber-reinforced composite. The fillers for the hybrid include one or two or all, of the following components: the layered-silicate, negative-CTE powder, and low-density material. | ||||||
| 264 | AIRCRAFT STRUCTURES BONDED WITH ADHESIVE INCLUDING MAGNETOSTRICTIVE MATERIAL | US13732270 | 2012-12-31 | US20140023837A1 | 2014-01-23 | Robert J. Miller; Diane C. Rawlings; Kenneth A. Krienke; James H. Mabe; Robert T. Ruggeri; Dan J. Clingman |
| First and second aircraft structures are bonded together with an adhesive including strain-sensitive magnetostrictive material. The magnetostrictive material has a magnetomechanical coefficient greater than e−5. | ||||||
| 265 | Multi-layer aircraft adhesive | US12644266 | 2009-12-22 | US08551620B2 | 2013-10-08 | Alfredo M. Reyes, Jr.; Michael A. Cosman; Apolinar R. Quinto |
| A multi-layer aircraft adhesive composition is provided having a first layer prepared from a first composition having a Part A and a Part B. Part A contains a plasticizer, a crosslinking agent, and an adhesion promoter. Part B contains a moisture resister and an abrasion resister. The composition has a second layer formed over at least a portion of the first layer. The second layer is prepared from a second composition having a Part C and a Part D. Part C contains at least one polythiol functional polymer, at least one epoxy resin, at least one sulfur containing material that is different from the at least one polythiol functional polymer, at least one plasticizer, and at least one filler. Part D contains at least one plasticizer, at least one of manganese dioxide or lead oxide, and at least one alkaline agent. | ||||||
| 266 | OPTICAL CURABLE RESIN COMPOSITE FOR LAMINATING OPTICAL SUBSTRATES AND METHOD THEREOF | US13277228 | 2011-10-20 | US20130101827A1 | 2013-04-25 | CHIN-YU CHEN |
| In an optical curable resin (OCR) composite for laminating optical substrates and a method of using the OCR composite to laminating two optical substrates, the OCR composite is formed by projecting an ultraviolet light to cure a liquid adhesive containing a plurality of bead-shaped elastic particles, and the method includes the steps of coating the liquid adhesive onto a first optical substrate, stacking the first optical substrate to a second optical substrate, such that each particle is separated between the first and second optical substrates, and projecting the ultraviolet light onto the first and second optical substrate again to cure the liquid adhesive, so that the particles are separated to form a gap with equal heights between the first and second optical substrates to enhance the lamination efficiency and quality of the optical substrates. | ||||||
| 267 | ANISOTROPIC CONDUCTIVE ADHESIVE, METHOD OF PRODUCING THE SAME, CONNECTION STRUCTURE AND PRODUCING METHOD THEREOF | US13703962 | 2011-06-28 | US20130087373A1 | 2013-04-11 | Jun Sakamoto; Misao Konishi |
| In an anisotropic conductive adhesive including a magnetic powder such as nickel-coated resin particles used as conductive particles, the conductive particles are present in an insulating adhesive composition without being aggregated. The magnetic powder used as the conductive particles is at least partially composed of a magnetic material. In this case, demagnetization has been performed on the conductive particles in a powder form that have not been dispersed in the insulating adhesive composition, the conductive particles in a paste obtained by dispersing the conductive particles in the insulating adhesive composition, or the conductive particles in a film formed from the paste, before establishment of an anisotropic conductive connection using the anisotropic conductive adhesive. | ||||||
| 268 | AIRCRAFT STRUCTURES BONDED WITH ADHESIVE INCLUDING MAGNETOSTRICTIVE MATERIAL | US11956216 | 2007-12-13 | US20120305167A1 | 2012-12-06 | Diane C. Rawlings; Robert J. Miller; Kenneth A. Krienke; James H. Mabe; Robert T. Ruggeri; Dan J. Clingman |
| First and second aircraft structures are bonded together with an adhesive including strain-sensitive magnetostrictive material. | ||||||
| 269 | Compounds for preventing ghost odour | US12657861 | 2010-01-28 | US08287631B2 | 2012-10-16 | Rudiger Baum; Hans-Jurgen Schmidt; Thomas Wunder; Christos Savides |
| The invention relates to compounds from the groups of (A) electrophiles, (B) nucleophiles, (C) alkylating agents, (D) antioxidants and (E) oxidizing agents as odor preventatives for reducing so-called ghost odor which is induced by 2-methyl-4-isothiazolin-3-one and/or octyl-4-isothiazolin-3-one. The invention further relates to biocide compositions which comprise 2-methyl-4-isothiazolin-3-one and/or octyl-4-isothiazolin-3-one and also one or more odor preventatives, and to the use of odor preventatives for preventing ghost odor. | ||||||
| 270 | ADHERING METHOD USING ELECTROSTATIC POWDER ADHESIVE, AND POWDER ADHESIVE TO BE USED IN ADHERING METHOD | US13510106 | 2010-11-26 | US20120231176A1 | 2012-09-13 | Takefumi Murai; Yoshimi Shibata |
| Provided is an adhering method which comprises spray-coating an adherend with a powder adhesive and then using the adherend, thereby enabling the formation of an automobile interior part having good heat tolerance and high adhesion strength. The adhering method to be used for forming an automobile interior part involves a step for spray-coating an adherend (4) with a powder adhesive (6) with the use of an electrostatic powder spray gun (5). If necessary, the adhering method may further involve a step for inciting the powder adhesive, which has been spray-coated on the adherend, by heating with an infrared heater. | ||||||
| 271 | Photocurable pressure-sensitive adhesive composition | US12663151 | 2008-06-04 | US08217096B2 | 2012-07-10 | Hiroji Fukui |
| The present invention provides a photocurable pressure-sensitive adhesive composition which has sufficient adhesion before being irradiated with light, and after being irradiated with light, keeps a sufficient pot life and has a short cure-completion time at a room temperature. A cured product produced from the composition has high adhesion force to adherends difficult to be attached, and excellent durability. The photocurable pressure-sensitive adhesive composition comprises a crosslinking compound (A) that is crosslinkable by the action of a base, a photobase generator (B) which becomes active upon light irradiation to generate a base, and a tackifying component (C). | ||||||
| 272 | Composite material, especially multilayer material, and adhesive or bonding material | US12086983 | 2006-08-10 | US08119220B2 | 2012-02-21 | Xinhe Tang; Ka Chun Tse; Ernst Hammel; Ben Zhong Tang |
| Disclosed is a multilayer material in which at least two components are jointed to each other via an adhesive bond. The adhesive bond is formed by an adhesive or bonding layer containing nanofiber material in a matrix that is suitable as an adhesive. | ||||||
| 273 | Printed Circuit Board made from a Composite Material | US13274851 | 2011-10-17 | US20120031653A1 | 2012-02-09 | Xinhe Tang; Ka Chun Tse; Ernst Hammel |
| Disclosed is a multilayer material in which at least two components are jointed to each other via an adhesive bond. The adhesive bond is formed by an adhesive or bonding layer containing nanofiber material in a matrix that is suitable as an adhesive. | ||||||
| 274 | MOUNTING MEANS | US13255402 | 2010-01-22 | US20110313098A1 | 2011-12-22 | Christian Ronner |
| A mounting system for fixation of two objects includes a single-component aerobic adhesive and a metered amount of moisture added to the adhesive prior to using the adhesive to fixate the objects. The adhesive with the moisture is hardenable while the objects are glued together. | ||||||
| 275 | AIRCRAFT ADHESIVE | US13008417 | 2011-01-18 | US20110143028A1 | 2011-06-16 | Alfredo M. Reyes, JR.; John R. Short; Santo Randazzo |
| A method, composition, and article are disclosed relating to the formation of a hump seal on an aircraft transparency. The method includes applying to the aircraft transparency an adhesive composition having a Part A and a Part B. Part A includes a plasticizer, a cross-linking agent, and an adhesion promoter. Part B includes a moisture resister and an abrasion resister, with the adhesive composition being substantially sulfide free. In one example, the moisture resister includes polybutadiene. In another example, the adhesion promoter includes an epoxy silane. | ||||||
| 276 | ADHESIVE | US12989134 | 2009-04-03 | US20110054074A1 | 2011-03-03 | Gerhard Jonschker; Reiner Friedrich; Joerg Pahnke |
| The present invention relates to an adhesive comprising at least one matrix material and core/shell particles comprising cores having a diameter in the range from 1 nm to 1 μm with a shell comprising oligomers and/or polymers, and to a process for the preparation thereof. | ||||||
| 277 | AN ADHESIVE TAPE | US12682997 | 2007-10-19 | US20100288431A1 | 2010-11-18 | Greet Bossaert; Bart Forier; Myriam Vandenholt; Walter Eevers; Yutaka Tosaki |
| The present invention relates to an adhesive tape, a method of manufacturing thereof and to uses thereof. More specifically, the present invention relates to an adhesive tape that can be used as such in order to join two entities with their respective surfaces together and/or to attach an entity on the surface of a substrate, whilst the peel adhesion is reduced, i.e. the tape can be removed easily, if desired. The adhesive tape comprising: a layer of a thermally shrinkable polymer, said layer having two surfaces opposite each other, a layer of a pressure sensitive adhesive composition on one of said two surfaces, said pressure sensitive adhesive composition comprising an amorphous polymer, thermally expandable particles and/or at least one blocked isocyanate compound. | ||||||
| 278 | PRESSURE SENSITIVE ADHESIVE COMPOSITION COMPRISING A WATER SOLUBLE COMPOUND | US12735209 | 2009-01-08 | US20100280429A1 | 2010-11-04 | Anders Bach; Mads Lykke |
| The present invention relates to a pressure sensitive adhesive composition comprising a continuous phase and a discontinuous phase wherein a) the continuous phase comprises a water vapour permeable hydrophobic polymer; and b) the discontinuous phase comprises a water soluble compound. | ||||||
| 279 | IMPROVED STRUCTURAL ADHESIVE MATERIALS | US12601826 | 2008-06-02 | US20100276645A1 | 2010-11-04 | Ian Aspin; Marino Godot |
| An adhesive material comprising at least one adhesive polymeric resin, at least one low aspect ratio metal-coated additive, and at least one high aspect ratio metal-coated additive. There is additionally provided an adhesive material comprising at least one adhesive polymeric resin, and one of either; a) low aspect ratio metal-coated additives present in the range 0.2 wt. % to 30 wt. % of the adhesive material; or b) discrete high aspect ratio metal-coated additives present in the range 0.2 wt. % to 25 wt. % of the adhesive material. | ||||||
| 280 | MULTI-LAYER AIRCRAFT ADHESIVE | US12644266 | 2009-12-22 | US20100159238A1 | 2010-06-24 | Alfredo M. Reyes, JR.; Michael A. Cosman; Apolinar R. Quinto |
| A multi-layer aircraft adhesive composition is provided having a first layer prepared from a first composition having a Part A and a Part B. Part A contains a plasticizer, a crosslinking agent, and an adhesion promoter. Part B contains a moisture resister and an abrasion resister. The composition has a second layer formed over at least a portion of the first layer. The second layer is prepared from a second composition having a Part C and a Part D. Part C contains at least one polythiol functional polymer, at least one epoxy resin, at least one sulfur containing material that is different from the at least one polythiol functional polymer, at least one plasticizer, and at least one filler. Part D contains at least one plasticizer, at least one of manganese dioxide or lead oxide, and at least one alkaline agent. | ||||||
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