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公开(公告)号：EP3384226A1
公开(公告)日：2018-10-10
申请号：EP16809160.1
申请日：2016-11-30
发明人： SZYNISZEWSKI, Stefan , VOGEL, Rene , HIPKE, Thomas
CPC分类号： E04C2/292 , A43B7/32 , B32B3/08 , B32B5/02 , B32B5/18 , B32B5/245 , B32B7/08 , B32B7/12 , B32B9/046 , B32B15/046 , B32B15/18 , B32B15/20 , B32B27/065 , B32B2250/03 , B32B2250/40 , B32B2260/021 , B32B2260/046 , B32B2262/105 , B32B2262/106 , B32B2264/107 , B32B2266/045 , B32B2266/06 , B32B2266/08 , B32B2307/546 , B32B2307/558 , B32B2307/56 , B32B2307/732 , B32B2437/02 , B32B2605/00 , F41H5/0442 , F41H5/0492
摘要： The invention provides a security panel comprising a face plate disposed adjacent to a metallic foam having a plurality of rigid particles therein. The invention extends to a method of manufacturing the security panel and uses of the security panel. The invention also extends to shock absorption panels and footwear articles comprising such panels.
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公开(公告)号：EP2756048A2
公开(公告)日：2014-07-23
申请号：EP12773435.8
申请日：2012-09-10
发明人： LEE, Jiannrong , SUN, Yuhao , AUNG, Maung, Kyaw , TSENG, Chin-Jen , CHANG, Chiapu , ROKUTANDA, Shuji , LIANG, Rong-Chang
CPC分类号： C09J9/02 , B32B3/10 , B32B5/16 , B32B7/12 , B32B27/14 , B32B27/281 , B32B27/285 , B32B27/286 , B32B27/308 , B32B27/36 , B32B27/365 , B32B37/12 , B32B37/14 , B32B37/226 , B32B38/06 , B32B38/10 , B32B2255/10 , B32B2255/26 , B32B2264/105 , B32B2266/045 , B32B2307/202 , B32B2309/08 , B32B2310/0843 , B32B2457/00 , B65G17/36 , C08K9/02 , C08K2201/001 , C09J7/00 , C09J7/10 , C09J2201/28 , C09J2201/602 , C09J2203/326 , C09J2205/102 , C09J2433/00 , C09J2461/00 , C09J2463/00 , H05K3/321 , Y10T156/1066 , Y10T428/24893 , Y10T428/249921
摘要： A method for fabricating an electronic device or component such as an anisotropic conductive film comprising: distributing a plurality of conductive particles into an array of microcavities formed on a surface of a continuous carrier belt, rotating the belt carrying the conductive particles while conveying a surface of an adhesive layer into contact with the surface of the rotating belt, transferring the conductive particles from the microcavities on the belt to the adhesive layer in predefined locations in the adhesive layer corresponding to the array of microcavities on the belt, and separating the adhesive layer from the surface of the belt. In one embodiment, the position of the microcavities is varied in a controlled manner.
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3.发明授权RUMPFSEGMENT UND VERFAHREN ZUR HERSTELLUNG DES RUMPFSEGMENTS 有权VERFAHREN ZUR HERSTELLUNG DES RUMPFSEGMENTS的RUMPFSEGMENT
公开(公告)号：EP2414227B1
公开(公告)日：2014-01-01
申请号：EP10714224.2
申请日：2010-03-30
CPC分类号： B64C1/12 , B32B1/00 , B32B3/12 , B32B3/266 , B32B5/02 , B32B5/18 , B32B5/22 , B32B5/245 , B32B5/32 , B32B7/02 , B32B15/046 , B32B27/02 , B32B27/04 , B32B2260/021 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2266/02 , B32B2266/0214 , B32B2266/045 , B32B2307/536 , B32B2307/718 , B32B2605/18 , B64C1/40 , B64C2001/0072 , B64C2211/00 , B64D11/00 , B64D13/00 , Y02T50/43 , Y02T50/44 , Y02T50/46 , Y10T29/49
摘要： A fuselage segment of an aircraft fuselage is provided with an outer skin and an inner skin that are spaced apart from one another by a core, wherein conduits for system installations are integrated into the core, as well as a method for manufacturing such a fuselage segment.
摘要翻译： 飞机机身的机身部分设置有通过芯彼此间隔开的外皮和内皮，其中用于系统安装的导管被集成到芯中，以及用于制造这样的机身部分的方法 。
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4.发明公开STRUKTURBAUTEIL MIT ZUMINDEST EINER HAUPTLAST-TRAGENDE BEPLANKUNGSSCHALE UND EINER TRÄGERSTRUKTUR ZUR BEFESTIGUNG DER HAUPTLAST-TRAGENDEN BEPLANKUNGSSCHALE SOWIE STRÖMUNGSKÖRPER MIT EINEM SOLCHEN STRUKTURBAUTEIL 有权与至少一个KEY LAST佩带BEPLANKUNGSSCHALE和结构件的载体结构，用于固定主LAST佩带BEPLANKUNGSSCHALE和流动机身采用这样的结构成分
公开(公告)号：EP2595877A1
公开(公告)日：2013-05-29
申请号：EP11741107.4
申请日：2011-07-20
CPC分类号： B64C1/12 , B32B3/02 , B32B3/06 , B32B3/08 , B32B3/28 , B32B3/30 , B32B5/18 , B32B7/04 , B32B2266/0214 , B32B2266/04 , B32B2266/045 , B32B2307/102 , B32B2307/54 , B32B2307/5825 , B32B2605/18 , B32B2607/00 , B64C3/20 , B64C3/26 , B64D45/00 , B64D2045/0085 , G01N19/08 , Y10T428/239 , Y10T428/24 , Y10T428/24322 , Y10T428/249923
摘要： The invention relates to a structural component (1), comprising at least one main-load-bearing covering shell (B) and a carrier structure (T) for fixing the covering shell, wherein the covering shell (B) is designed in the form of a sandwich and formed by an inner skin section (11), an outer skin section (12) and a shear-load-absorbing core layer (13) which is disposed between said two sections and connects the inner and the outer skin sections (11, 12) to one another in a planar manner, wherein the carrier structure (T) is formed by at least one panel-shaped connecting part (22) which extends between and transversely to said inner and outer skin sections and is connected along a reference longitudinal direction (L-R) to the covering shell (B). In order to support the covering shell (B) on the carrier structure, the connecting part is located outside the carrier structure (T) and is fastened to the inner skin section (11) resting thereon in a planar manner, wherein at least one profiled support (V0; V1, V2, V3, V4) extending along the reference longitudinal direction (L-R) is provided in the covering shell (B) in order to form a reinforcing section in the connecting region (14) of the panel-shaped connecting part (22). The profiled support is connected to the inner skin section (11) and the outer skin section (12) in order to stabilise the covering shell (B) when the latter sustains damage and thereby provides support from the outside.
摘要翻译： 本发明涉及的结构部件的流体的（1），包括至少一个衬壳（B）那样载有主负载，具有芯层（33），所述内衬壳做吸音减震剪切负荷和确实包括一个多元化 在泡沫层的纵向延伸旁边的海誓山盟布置核心层部分（33A），所述worin核心层部分在两侧由一个核心层加强区域抵靠彼此相互连接（37） 穿过核心层垂直地延伸到核心层（33）的纵向延伸。
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公开(公告)号：EP2595876A1
公开(公告)日：2013-05-29
申请号：EP11741106.6
申请日：2011-07-20
CPC分类号： B64C1/12 , B32B3/02 , B32B3/06 , B32B3/08 , B32B3/28 , B32B3/30 , B32B5/18 , B32B7/04 , B32B2266/0214 , B32B2266/04 , B32B2266/045 , B32B2307/102 , B32B2307/54 , B32B2307/5825 , B32B2605/18 , B32B2607/00 , B64C3/20 , B64C3/26 , B64D45/00 , B64D2045/0085 , G01N19/08 , Y10T428/239 , Y10T428/24 , Y10T428/24322 , Y10T428/249923
摘要： The invention relates to a structural component (1) of a flow body, comprising at least one lining shell (B) that carries a main load, said lining shell having a core layer (33) that absorbs shear load and that comprises a plurality of core-layer sections (33a) arranged next to each other in the longitudinal extension of the foam layer, wherein said core-layer sections are connected to each other at the sides lying against each other by a core-layer reinforcement area (37), which extends through the core layer perpendicularly to the longitudinal extension of the core layer (33).
摘要翻译： 本发明涉及一种流体的结构部件（1），其包括至少一个承载主负载的衬里壳体（B），所述衬套壳体具有吸收剪切载荷的芯层（33），并且包括多个 所述芯层部分在所述泡沫层的纵向延伸部中彼此相邻布置，其中所述芯层部分通过芯层加强区域彼此相对地彼此连接， 其延伸通过芯层垂直于芯层（33）的纵向延伸。
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公开(公告)号：EP2477578A1
公开(公告)日：2012-07-25
申请号：EP10730958.5
申请日：2010-07-02
申请人： Zimmer Spine, Inc.
发明人： ZHANG, Kai , VALOIS, Christopher J. , FANG, Zhibin , BASSETT, Jeffrey A. , ZAWADZKI, Steven A. , KIRT, David C. , SPANGLE, Steven E.
CPC分类号： A61F2/4465 , A61F2/442 , A61F2/447 , A61F2002/30011 , A61F2002/30014 , A61F2002/30044 , A61F2002/30056 , A61F2002/30065 , A61F2002/30235 , A61F2002/30971 , A61F2250/0023 , A61F2250/0032 , A61F2250/0046 , A61F2310/00131 , A61L31/12 , A61L31/146 , B32B3/266 , B32B15/08 , B32B27/065 , B32B27/285 , B32B27/288 , B32B2255/00 , B32B2255/205 , B32B2266/04 , B32B2266/045 , B32B2266/06 , B32B2266/104 , B32B2307/40 , B32B2307/51 , B32B2307/538 , B32B2307/744 , B32B2535/00
摘要： A composite interbody vertebral implant (10) for facilitating fusion of adjacent vertebrae. The implant includes a first endplate (12) of a porous metal material and a second endplate (14) of a porous metal material which are configured to allow bone in-growth. The implant also includes a polymeric body (16) positioned between and bonded to the first and second endplates (12,14) such that polymeric material of the polymeric body (16) is impregnated into pores of the first and second endplates to bond the components together. The implant include a cavity (26) extending through the composite implant (10) configured to receive bone growth material to facilitate fusion between a first vertebra and a second vertebra.
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公开(公告)号：EP2414227A2
公开(公告)日：2012-02-08
申请号：EP10714224.2
申请日：2010-03-30
IPC分类号： B64C1/06
CPC分类号： B64C1/12 , B32B1/00 , B32B3/12 , B32B3/266 , B32B5/02 , B32B5/18 , B32B5/22 , B32B5/245 , B32B5/32 , B32B7/02 , B32B15/046 , B32B27/02 , B32B27/04 , B32B2260/021 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2266/02 , B32B2266/0214 , B32B2266/045 , B32B2307/536 , B32B2307/718 , B32B2605/18 , B64C1/40 , B64C2001/0072 , B64C2211/00 , B64D11/00 , B64D13/00 , Y02T50/43 , Y02T50/44 , Y02T50/46 , Y10T29/49
摘要： A fuselage segment of an aircraft fuselage is provided with an outer skin and an inner skin that are spaced apart from one another by a core, wherein conduits for system installations are integrated into the core, as well as a method for manufacturing such a fuselage segment.
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公开(公告)号：EP0710178A4
公开(公告)日：1997-06-11
申请号：EP94921502
申请日：1994-07-11
申请人： CHOMERICS INC
发明人： THORNTON STEVEN L
IPC分类号： B32B3/24 , C08K3/00 , C08L101/00 , C09J133/04 , C09J133/06 , C09J175/00 , C09J175/04 , C09J183/00 , C09J183/04 , F28F13/00 , H01L23/373 , H05K7/20 , F28F7/00 , H05K7/00
CPC分类号： B32B27/065 , B32B3/266 , B32B5/18 , B32B27/20 , B32B2266/045 , B32B2307/302 , F28F13/00 , H01L23/3733 , H01L2924/0002 , H05K7/20472 , H01L2924/00
摘要： A thermally conductive interface material formed of a polymeric binder (2), one or more thermally conductive fillers (1) and an expanded metal mesh layer (3) at least partially embedded into one of the major surfaces of the binder is disclosed. Preferably, the interface is a pressure sensitive adhesive material and more preferably, it is in the form of a tape or self-adhesive pads.
摘要翻译： 公开了一种由聚合物粘合剂（2），一种或多种导热填料（1）和至少部分地嵌入粘合剂的主表面之一的多孔金属网层（3）形成的导热界面材料。 优选地，界面是压敏粘合剂材料，更优选地，其是带或自粘垫的形式。
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公开(公告)号：EP3408084A1
公开(公告)日：2018-12-05
申请号：EP17707998.5
申请日：2017-01-26
发明人： RIKLEEN, Leslie , MAGYAR, Michael , O'BRYAN, Eric , MIHALCIK, David , EVANS, Owen , ZAFIROPOULOS, Nicholas , GOULD, George
IPC分类号： B32B5/02 , B32B5/16 , B32B5/18 , B32B5/24 , B32B5/32 , B32B7/02 , B32B7/08 , B32B7/10 , B32B27/32
CPC分类号： B32B5/18 , B32B3/06 , B32B5/02 , B32B5/022 , B32B5/024 , B32B5/026 , B32B5/06 , B32B5/145 , B32B5/16 , B32B5/22 , B32B5/245 , B32B5/32 , B32B7/02 , B32B7/08 , B32B7/10 , B32B7/12 , B32B27/08 , B32B27/304 , B32B27/32 , B32B27/322 , B32B27/40 , B32B37/12 , B32B37/14 , B32B2250/03 , B32B2250/40 , B32B2260/02 , B32B2260/04 , B32B2262/02 , B32B2262/0207 , B32B2262/0238 , B32B2262/0261 , B32B2262/0276 , B32B2262/0292 , B32B2264/0257 , B32B2264/101 , B32B2264/107 , B32B2266/025 , B32B2266/0257 , B32B2266/0278 , B32B2266/0285 , B32B2266/04 , B32B2266/045 , B32B2266/06 , B32B2266/126 , B32B2305/022 , B32B2305/08 , B32B2307/302 , B32B2307/304 , B32B2307/51 , B32B2307/726 , B32B2307/732 , B32B2437/00
摘要： The present disclosure can provide an aerogel composite. The aerogel composite comprises at least one base layer having a top surface and a bottom surface, the base layer comprising a reinforced aerogel composition which comprises a reinforcement material and a monolithic aerogel framework, a first facing layer comprising a first facing material attached to the top surface of the base layer, and a second facing layer comprising a second facing material attached to the bottom surface of the base layer. At least a portion of the monolithic aerogel framework of the base layer extends into at least a portion of both the first facing layer and the second facing layer. The first facing material and the second facing material can each comprise or consist essentially of elastic fibers such as spandex, nylon, lycra, elastane, or combinations thereof.
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公开(公告)号：EP3304588A2
公开(公告)日：2018-04-11
申请号：EP16804113.5
申请日：2016-05-27
发明人： MASLYK, Daniel , ZHAO, Yuan , BERHE, Mulugeta , ALLEN, Scott T.
CPC分类号： H01L23/3736 , B32B3/26 , B32B5/18 , B32B7/12 , B32B9/007 , B32B15/02 , B32B15/20 , B32B25/08 , B32B25/14 , B32B37/12 , B32B38/08 , B32B2260/02 , B32B2266/045 , B32B2305/022 , B32B2307/302 , B32B2307/732 , B32B2309/105 , B32B2311/00 , B32B2457/00 , C09K5/063 , H01L21/02112 , H01L23/3733 , H01L23/3737 , H01L23/427 , H01L23/4275
摘要： In accordance with the present invention, there are provided heat dispersing articles, assemblies containing same, methods for the preparation thereof, and various uses therefor. In one aspect of the present invention, there are provided heat dispersing articles. In another aspect of the present invention, there are provided methods for producing the above-referenced articles. In yet another aspect of the present invention, there are provided assemblies containing the above-referenced articles. In still another aspect of the present invention, there are provided methods for making the above-referenced assemblies. In yet another aspect, there are provided methods to dissipate the heat generated by portable electronic devices.
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