公开(公告)号：EP3299297B1

公开(公告)日：2018-12-12

申请号：EP16400043.2

申请日：2016-09-27

申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH

发明人： Rack, Andreas ,  Rosplesch, David ,  Jonke, Dietrich

IPC分类号： B64D45/02 ,  B29C65/00 ,  B29L31/30 ,  B05D5/12 ,  B05D7/02 ,  B05D1/02 ,  B29C65/56 ,  B64C1/12 ,  C23C24/04 ,  H01R4/64

CPC分类号： B05D5/12 ,  B05D1/025 ,  B05D7/02 ,  B05D2201/02 ,  B29C65/562 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/131 ,  B29C66/21 ,  B29C66/43 ,  B29C66/43441 ,  B29C66/52441 ,  B29C66/54 ,  B29C66/543 ,  B29C66/721 ,  B29C66/7212 ,  B29K2995/0005 ,  B29L2031/3082 ,  B29L2031/3088 ,  B64C1/12 ,  B64D45/02 ,  C23C24/04 ,  H01R4/64 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10

摘要： The invention is related to a rotary wing aircraft that comprises a structural arrangement (6) with at least one first fiber reinforced polymer component (7a) and at least one second fiber reinforced polymer component (7b) that are spaced apart from each other by an interspace (11) and that are rigidly attached to an associated structural component (8), wherein the at least one first fiber reinforced polymer component (7a) and the at least one second fiber reinforced polymer component (7b) are at least partly interconnected by means of an electrically conductive connection (9), and wherein the electrically conductive connection (9) comprises at least one sprayed layer (15) of electrically conductive particles (14), the at least one sprayed layer (15) of electrically conductive particles (14) being provided in the interspace (11).

公开(公告)号：EP3271170B1

公开(公告)日：2018-11-14

申请号：EP16716977.0

申请日：2016-03-18

申请人： Kongsberg Actuation Systems II, Inc.

发明人： MENTINK, Laurentius, Andreas, Gerardus

IPC分类号： B32B25/08 ,  B32B25/16 ,  B32B27/08 ,  B32B27/18 ,  B32B27/32 ,  B32B27/34 ,  B32B1/08 ,  B32B27/30 ,  F16L11/10 ,  F16L11/12

CPC分类号： F16L11/125 ,  B29C47/065 ,  B29K2023/12 ,  B29K2023/16 ,  B29K2105/12 ,  B29K2105/16 ,  B29K2507/04 ,  B29K2995/0005 ,  B29K2995/0016 ,  B29L2023/005 ,  B32B1/08 ,  B32B5/10 ,  B32B7/02 ,  B32B25/08 ,  B32B25/16 ,  B32B27/08 ,  B32B27/18 ,  B32B27/304 ,  B32B27/32 ,  B32B27/34 ,  B32B2264/108 ,  B32B2274/00 ,  B32B2307/202 ,  B32B2307/3065 ,  B32B2323/10 ,  B32B2323/16 ,  B32B2377/00 ,  B32B2597/00 ,  F16L11/10

摘要： A flame resistant hose assembly is disclosed. The hose assembly comprises a tubular inner layer and a flame resistant layer. The tubular inner layer has an interior radial surface and an exterior radial surface and defines a longitudinal axis. The flame resistant layer is disposed about and covers the exterior radial surface of the tubular inner layer. The flame resistant layer is formed N from a flame resistant material comprising a polymeric binder and expandable graphite in an amount of from about 5 to about 40 parts by weight based on 100 parts by weight of the flame resistant material. The flame resistant layer expands when heated to a temperature of about 220° C. or greater and maintains a post-expansion coverage of the exterior radial surface of the tubular inner layer of greater than about 95%.

公开(公告)号：EP2256030B1

公开(公告)日：2018-08-01

申请号：EP09726416.2

申请日：2009-03-23

申请人： Mitsubishi Heavy Industries, Ltd.

发明人： KAMINO, Yuichiro ,  OGURI, Kazuyuki ,  NAKAMURA, Koichi

IPC分类号： B64C1/00 ,  B64D45/02 ,  F16B5/02 ,  F16B33/06 ,  F16B35/00

CPC分类号： B64C3/26 ,  B29C65/562 ,  B29C65/564 ,  B29C66/1122 ,  B29C66/43441 ,  B29C66/474 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72321 ,  B29C66/742 ,  B29C70/088 ,  B29C70/885 ,  B29D99/001 ,  B29K2105/06 ,  B29K2305/02 ,  B29K2305/10 ,  B29K2307/00 ,  B29K2309/08 ,  B29K2705/10 ,  B29K2995/0005 ,  B29L2009/003 ,  B29L2031/3082 ,  B29L2031/3085 ,  B64D45/02 ,  F16B33/004 ,  F16B35/06 ,  F16B37/14 ,  B29K2307/04 ,  B29K2079/08 ,  B29K2071/00

摘要： Provided is an aircraft assembly equipped with a lightning protection structure that is not easily destroyed by lightning current and that is highly reliable. In an aircraft assembly including a skin (10) in which a CFRP layer (12) serves as a main structure; a shear-tie (11) that support the skin (10) from the inside; and a fastener (1) that couples the skin (10) and the shear-tie (11), a copper foil (13) and an outside GRFP layer (14) are provided on an outer surface side of the skin (10), in this order towards the outside, and a copper paint layer (19), which contains copper powder, is provided on the outside GFRP layer (14).

公开(公告)号：EP3336876A1

公开(公告)日：2018-06-20

申请号：EP16834837.3

申请日：2016-04-05

申请人： Toshiba Electron Tubes & Devices Co., Ltd.

发明人： KATO, Takeshi ,  HARA, Takanobu ,  MIYAMURA, Masayoshi

IPC分类号： H01J35/16

CPC分类号： H01J35/16 ,  B29C45/14336 ,  B29C45/14639 ,  B29K2083/00 ,  B29K2995/0005 ,  B29K2995/0007

摘要： According to an embodiment, an X-ray tube comprises a cathode (11) for emitting electrons, an anode (12) having an anode target (12a) with which electrons emitted from the cathode (11) collides to radiate X-rays, a glass container (16) housing the cathode (11) and the anode (12), an anode rod (14) extending from the anode (12) to an outside of the glass container (16), an annular metal member (17) through which the anode rod (14) is inserted, the annular metal member (17) connecting the anode (12) and the glass container (16) to maintain an inside of the glass container (16) in vacuum, and an electrically insulating molding resin member (15) charged into a space (S) formed between the anode rod (14) and outer surfaces of the glass container (16) and the metal member (17).

公开(公告)号：EP3334591A1

公开(公告)日：2018-06-20

申请号：EP16758007.5

申请日：2016-08-10

申请人： Cytec Industries Inc.

发明人： LENZI, Fiorenzo

IPC分类号： B29C70/02

CPC分类号： B32B5/06 ,  B29C70/025 ,  B29K2105/048 ,  B29K2105/08 ,  B29K2105/0854 ,  B29K2995/0005 ,  B32B5/022 ,  B32B5/024 ,  B32B5/08 ,  B32B5/26 ,  B32B37/15 ,  B32B38/08 ,  B32B2260/021 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/08 ,  B32B2262/10 ,  B32B2262/101 ,  B32B2262/105 ,  B32B2262/106 ,  B32B2262/12 ,  B32B2262/14 ,  B32B2264/108 ,  B32B2305/02 ,  B32B2305/10 ,  B32B2305/20 ,  B32B2307/202 ,  B32B2307/206 ,  B32B2307/30 ,  B32B2307/3065 ,  B32B2571/00 ,  B32B2605/18 ,  B32B2607/00

摘要： A thermally expandable and electrically conductive material capable of providing lightning strike protection and burn-through resistance, containing electrically conductive fibers; thermally expandable particles; and a curable matrix resin comprising one or more thermoset resins, wherein the electrically conductive fibers and the thermally expandable particles are embedded in the curable matrix resin.

公开(公告)号：EP3333293A1

公开(公告)日：2018-06-13

申请号：EP17204797.9

申请日：2017-11-30

申请人： The Boeing Company

发明人： TSOTSIS, Thomas K ,  SPRENGARD, Joseph E

IPC分类号： D04H1/4242 ,  D04H1/4374 ,  D04H1/732 ,  D04H3/02 ,  D04H3/14 ,  B29C70/08 ,  D04H5/02 ,  D04H5/08

CPC分类号： B32B5/08 ,  B29C70/081 ,  B29C70/34 ,  B29K2301/12 ,  B29K2307/04 ,  B29K2995/0005 ,  B29K2995/0089 ,  B29K2995/0091 ,  B29L2031/30 ,  B29L2031/3076 ,  B32B5/022 ,  B32B5/12 ,  B32B5/26 ,  B32B37/04 ,  B32B37/203 ,  B32B2260/023 ,  B32B2262/02 ,  B32B2262/106 ,  B32B2262/14 ,  B32B2307/202 ,  B32B2307/558 ,  B32B2307/56 ,  B32B2313/04 ,  B32B2398/20 ,  B32B2605/00 ,  B32B2605/18 ,  D04H1/4242 ,  D04H1/4374 ,  D04H3/14 ,  D04H5/02 ,  D04H5/08

摘要： A fiber-modified interlayer includes a nonwoven fabric layer formed of continuous fibers, and discontinuous fibers attached to the nonwoven fabric, the fiber-modified interlayer is attached to at least one reinforcing layer of structural tows to form an interlayer-toughened reinforcing fabric, at least one layer of the interlayer-toughened reinforcing fabric is infused with a matrix material and cured to form a composite structure.

公开(公告)号：EP3319775A1

公开(公告)日：2018-05-16

申请号：EP16727727.6

申请日：2016-06-09

申请人： OSRAM GmbH

发明人： RÖDER, Karl

IPC分类号： B29C45/16

CPC分类号： B29C45/16 ,  B29C45/1615 ,  B29C2045/169 ,  B29C2045/1693 ,  B29C2045/1696 ,  B29K2069/00 ,  B29K2105/16 ,  B29K2505/00 ,  B29K2905/00 ,  B29K2995/0005 ,  B29L2031/747

摘要： The invention relates to a method (S1-S3) for producing a composite component (1) from a plastic material and an electrically conductive filler material. The method has at least the following steps: molding a molded body (2) from the plastic material, said molded body (2) having at least one recess (3), which is arranged adjacently to at least one projection (6) (S1); pressing the at least one projection (6) such that plastic material (7) of the molded body (2) is thereby displaced into an opening-side region of the adjacent recess (3) (S2); and introducing flowable filler material (9) into at least one recess (3) and solidifying the filler material (9) (S3). A composite component (1) made of plastic material (2) and electrically conductive filler material (9) is produced according to the method (S1-S3). The invention can be used in particular on a lighting device, which comprises at least one plastic/metal composite component (1) in particular.

公开(公告)号：EP2628589B1

公开(公告)日：2018-05-02

申请号：EP13151015.8

申请日：2013-01-11

申请人： The Boeing Company

发明人： O'Brien Gaw, Kevin

IPC分类号： B29C70/64 ,  B29C70/88 ,  H05K9/00 ,  B29C70/54

CPC分类号： B29C70/882 ,  B29C70/545 ,  B29C70/64 ,  B29K2995/0005 ,  Y02T50/43 ,  Y10T156/10

摘要： A composite structure comprising a matrix and a reinforcement. The matrix comprises a substantially nonconductive material. The reinforcement comprises a conductive material. The reinforcement is located within the matrix to form a composite layer. A portion of the reinforcement is exposed at a surface of the composite layer such that electrical conductivity of the composite layer is increased in a direction substantially perpendicular to the composite layer ( Fig. 1 ).

公开(公告)号：EP2496402B8

公开(公告)日：2018-05-02

申请号：EP10773630.8

申请日：2010-11-05

申请人： OPTIMA consumer GmbH

发明人： KIRCHER, Willi

IPC分类号： B29C65/18 ,  B29C65/30 ,  B29C65/78 ,  H05B3/14 ,  B65B7/28 ,  B65B51/14

CPC分类号： B65B7/2878 ,  B29C65/18 ,  B29C65/30 ,  B29C65/7847 ,  B29C66/112 ,  B29C66/131 ,  B29C66/53461 ,  B29C66/8122 ,  B29C66/81262 ,  B29C66/81427 ,  B29C66/8167 ,  B29C66/81821 ,  B29C66/8322 ,  B29C66/91212 ,  B29C66/91221 ,  B29C66/91231 ,  B29C66/9141 ,  B29C66/961 ,  B29K2995/0005 ,  B65B51/14 ,  B29K2909/02

公开(公告)号：EP2953012B1

公开(公告)日：2018-04-18

申请号：EP14746641.1

申请日：2014-01-28

申请人： Suzhou Institute of Nano-tech and Nano-bionics (SINANO) Chinese Academy of Sciences

发明人： ZHANG, Ting ,  WANG, Xuewen ,  XIONG, Zuoping ,  GU, Yang ,  GU, Wen

IPC分类号： G06F3/041 ,  G01L1/18

CPC分类号： G01L1/18 ,  A61B1/00149 ,  A61B3/16 ,  A61B5/0205 ,  A61B5/021 ,  A61B5/024 ,  A61B5/11 ,  A61B5/4803 ,  A61B34/30 ,  A61B2562/0204 ,  A61B2562/0285 ,  B29C41/02 ,  B29C41/42 ,  B29C65/00 ,  B29K2083/00 ,  B29K2995/0003 ,  B29K2995/0005 ,  B29L2009/005 ,  B29L2031/34 ,  B29L2031/7546 ,  G01L1/14 ,  G06F3/041

摘要： The invention provides a piezoresistive electronic skin, a preparation method and a use thereof. The piezoresistive electronic skin uses carbon nanotube film as the conductive layer and uses materials provided with micro-nano patterns, such as polydimethylsiloxane, polyethylene terephthalate, polyvinyl alcohol, polyvinyl formal, polyethylene, and so on, as the substrate, enabling the substrate has advantages of high flexibility and being pliable, and it needs low operating voltage and little power consumption, but has high sensitivity and short response time. More importantly, the invention uses the patterned flexible substrate as the basis, greatly improving the sensitivity of electronic skin reacting to tiny applied force from outside. The invention also provides a capacitive electronic skin and a preparation method thereof. Further, the invention also provides a use of the piezoresistive electronic skin or the capacitive electronic skin on speech recognition, pulse detection, medical robot, etc.