公开(公告)号：US20240300209A1

公开(公告)日：2024-09-12

申请号：US18118827

申请日：2023-03-08

申请人： JETZERO, INC.

发明人： Mark Allan Page

IPC分类号： B32B5/06 ,  B32B5/02 ,  B32B5/26 ,  B32B37/15 ,  B64C1/12 ,  B64C39/00 ,  B64F5/10

CPC分类号： B32B5/073 ,  B32B5/024 ,  B32B5/26 ,  B32B37/15 ,  B64C1/12 ,  B64C39/00 ,  B64F5/10 ,  B32B2250/20 ,  B32B2255/02 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/106 ,  B32B2305/10 ,  B32B2313/04 ,  B32B2605/18 ,  B64C2039/105

摘要： A composite assembly for a blended wing body aircraft, the composite assembly comprising: a first assembly comprising a first molded part, wherein the first molded part comprises a first plurality of fibers, the first molded part partially infused with a first resin, a second assembly oriented relative to the first assembly, the second assembly comprising a second molded part wherein the second molded part comprises a second plurality of fibers, the second molded part partially infused with a second resin, and a joining region, the joining region comprising at least a portion of first plurality of fibers and at least a portion of second plurality of fibers, the at least a portion of first plurality of fibers and the at least a portion of second plurality of fibers substantially adjacent and infused with a third resin.

公开(公告)号：US20240173944A1

公开(公告)日：2024-05-30

申请号：US18244830

申请日：2023-09-11

申请人： ECORE INTERNATIONAL INC.

发明人： Arthur B. Dodge, III ,  John McFalls

IPC分类号： B32B25/04 ,  B32B5/02 ,  B32B5/16 ,  B32B5/18 ,  B32B5/24 ,  B32B5/30 ,  B32B7/04 ,  B32B7/12 ,  B32B9/02 ,  B32B9/04 ,  B32B25/08 ,  B32B25/10 ,  B32B25/16 ,  B32B27/08 ,  B32B27/12 ,  B32B27/30 ,  B32B27/34 ,  B32B27/36 ,  B32B27/40 ,  B32B37/08 ,  B32B37/12 ,  B32B37/20 ,  B32B38/00 ,  B32B39/00 ,  B32B41/00 ,  D06N7/00 ,  E04F15/10

CPC分类号： B32B25/04 ,  B32B5/022 ,  B32B5/024 ,  B32B5/026 ,  B32B5/16 ,  B32B5/18 ,  B32B5/24 ,  B32B5/30 ,  B32B7/04 ,  B32B7/12 ,  B32B9/02 ,  B32B9/025 ,  B32B9/045 ,  B32B25/08 ,  B32B25/10 ,  B32B25/16 ,  B32B27/08 ,  B32B27/12 ,  B32B27/30 ,  B32B27/302 ,  B32B27/304 ,  B32B27/34 ,  B32B27/36 ,  B32B27/40 ,  B32B37/203 ,  B32B39/00 ,  D06N7/0084 ,  E04F15/105 ,  E04F15/107 ,  B32B37/08 ,  B32B37/1207 ,  B32B38/0004 ,  B32B38/0036 ,  B32B38/1875 ,  B32B41/00 ,  B32B2260/025 ,  B32B2260/046 ,  B32B2262/0253 ,  B32B2262/0261 ,  B32B2262/0276 ,  B32B2262/062 ,  B32B2262/101 ,  B32B2264/02 ,  B32B2264/0207 ,  B32B2264/067 ,  B32B2272/00 ,  B32B2305/08 ,  B32B2305/10 ,  B32B2305/70 ,  B32B2307/102 ,  B32B2307/3065 ,  B32B2307/536 ,  B32B2307/546 ,  B32B2307/558 ,  B32B2307/732 ,  B32B2307/734 ,  B32B2309/02 ,  B32B2319/00 ,  B32B2327/06 ,  B32B2419/04 ,  B32B2471/00 ,  D06N2203/048 ,  D06N2205/106 ,  D06N2209/067 ,  Y02P70/62 ,  Y10T428/31739 ,  Y10T428/31855 ,  Y10T428/31938

摘要： A laminated surface covering including a facing material made of vinyl and a backing material comprising a rubber component. The rubber component comprising at least a matrix of bonded rubber granules. A bonding material disposed between the facing material and the backing material. The facing material configured to melt at a temperature between 165° F. and 248° F. infiltrating the backing material thereby essentially encasing the rubber granules of the matrix and providing fire retardation and smoke suppression qualities.

公开(公告)号：US20240157693A1

公开(公告)日：2024-05-16

申请号：US18211646

申请日：2023-06-20

申请人： Textron Systems Corporation

发明人： Michael Robert FAVALORO

IPC分类号： B32B37/18 ,  B32B5/12 ,  B32B37/00 ,  B32B37/10

CPC分类号： B32B37/18 ,  B32B5/12 ,  B32B37/025 ,  B32B37/10 ,  B32B2262/106 ,  B32B2305/10 ,  B32B2307/306 ,  B32B2313/04 ,  B32B2605/18

摘要： Techniques for providing a carbon composite component involve providing a first carbon composite layer having carbon fibers extending along the first carbon composite layer. The techniques further involve providing a second carbon composite layer in contact with the first carbon composite layer, the second carbon composite layer having upright carbon fibers. The techniques further involve providing a third carbon composite layer in contact with the second carbon composite layer, the third carbon composite layer having carbon fibers extending along the third carbon composite layer. The carbon composite layer having upright carbon fibers increases the interlaminar strength of the resulting structure thus providing strength in all dimensions/directions and alleviating the need for additional fasteners and/or 3D carbon/carbon.

公开(公告)号：US11772360B2

公开(公告)日：2023-10-03

申请号：US17807229

申请日：2022-06-16

申请人： The Boeing Company

发明人： Jerry Chungbin ,  Mark Rogalski ,  Everette Gray

IPC分类号： B32B7/08 ,  B29C70/08 ,  B32B5/22 ,  B32B38/18 ,  B32B38/08 ,  B32B37/12 ,  B32B38/00 ,  B32B37/18

CPC分类号： B32B7/08 ,  B29C70/08 ,  B32B5/22 ,  B32B37/18 ,  B32B38/08 ,  B32B38/1808 ,  B32B2037/1253 ,  B32B2038/008 ,  B32B2260/046 ,  B32B2305/10

摘要： Systems and methods for filament fastener that cures with composite part. One embodiment is a method of fabricating a composite part. The method includes placing layers of reinforcement fibers over a tool to form a laminate of composite material to be cured with a first resin, forming a filament fastener comprising bundled fibers with one or more texture elements around the bundled fibers, and coating the filament fastener with a second resin that is chemically compatible with the first resin. The method also includes inserting the filament fastener into the laminate through a plurality of the layers, and curing the filament fastener within the laminate to bind the plurality of the layers of the laminate with the one or more texture elements of the filament fastener via bonding of the first resin and the second resin to form the composite part with delamination resistance.

公开(公告)号：US11766856B2

公开(公告)日：2023-09-26

申请号：US17569043

申请日：2022-01-05

申请人： B/E Aerospace, Inc.

发明人： George T. Franck, III ,  Alvin S. Bartolome ,  Patrick G. Jarvis-Shean

IPC分类号： B32B37/18 ,  B32B37/06 ,  B32B37/14 ,  B32B27/12 ,  B29C70/30 ,  B29C65/00 ,  B32B37/26 ,  B29C65/02 ,  B29C37/00 ,  B29C35/02 ,  B32B27/38 ,  B29D99/00 ,  B32B5/26 ,  B29K101/10 ,  B29K105/08 ,  B29L9/00 ,  B29K101/12 ,  B29K105/00 ,  B29K309/08 ,  B29K307/04

CPC分类号： B32B37/182 ,  B29C35/02 ,  B29C37/0075 ,  B29C65/02 ,  B29C66/7254 ,  B29C66/72141 ,  B29C66/7375 ,  B29C66/7392 ,  B29C66/7394 ,  B29C66/7422 ,  B29C70/30 ,  B29D99/0089 ,  B32B5/26 ,  B32B27/12 ,  B32B27/38 ,  B32B37/06 ,  B32B37/146 ,  B32B37/26 ,  B29C37/0064 ,  B29C2035/0283 ,  B29K2101/10 ,  B29K2101/12 ,  B29K2105/0809 ,  B29K2105/253 ,  B29K2307/04 ,  B29K2309/08 ,  B29L2009/00 ,  B29L2009/003 ,  B32B2037/268 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/101 ,  B32B2305/10 ,  B32B2305/72 ,  B32B2309/025 ,  B32B2315/08 ,  B32B2323/10 ,  B32B2331/00 ,  B32B2363/00 ,  B32B2367/00 ,  B32B2377/00 ,  B32B2379/00

摘要： In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.

公开(公告)号：US20230192197A1

公开(公告)日：2023-06-22

申请号：US18163032

申请日：2023-02-01

申请人： SABIC Global Technologies B.V.

发明人： Craig Lawrence MILNE ,  Gregory E. TREMBLAY ,  Dhanendra Kumar NAGWANSHI ,  Somasekhar Bobba Venkat ,  Arunachala PARAMESHWARA ,  Matthew D. MARKS

IPC分类号： B62D29/04 ,  B29C45/14 ,  B29C70/46 ,  B29C70/50 ,  B60R21/04 ,  B32B3/04 ,  B32B3/12 ,  B32B3/28 ,  B32B5/02 ,  B32B27/08 ,  B32B37/06 ,  B32B37/10 ,  B32B38/18 ,  B62D63/04

CPC分类号： B62D29/043 ,  B29C45/14786 ,  B29C45/14811 ,  B29C70/465 ,  B29C70/506 ,  B32B3/04 ,  B32B3/12 ,  B32B3/28 ,  B32B5/02 ,  B32B27/08 ,  B32B37/06 ,  B32B37/10 ,  B32B38/1808 ,  B32B38/1858 ,  B60R21/04 ,  B62D63/04 ,  B32B2250/24 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2305/10 ,  B32B2305/076 ,  B32B2307/56 ,  B32B2605/08

摘要： In an embodiment, an energy-absorbing device can comprise: a polymer reinforcement structure, wherein the polymer reinforcement structure comprises a polymer matrix and chopped fibers; and a shell comprising 2 walls extending from a back and forming a shell channel, wherein the shell comprises continuous fibers and a resin matrix; wherein the polymer reinforcement structure is located in the shell channel.

公开(公告)号：US20180271216A1

公开(公告)日：2018-09-27

申请号：US15936707

申请日：2018-03-27

申请人： New Balance Athletics, Inc.

发明人： Gabriel La O' ,  Connor James Hutchinson

IPC分类号： A43B23/02 ,  A43B5/00 ,  A43B13/04 ,  A43B13/26 ,  A43B9/00 ,  A43B3/00 ,  A43D95/02 ,  B32B1/00 ,  B32B5/02 ,  B32B5/26 ,  B32B37/24 ,  B32B38/00

CPC分类号： A43B23/027 ,  A43B3/0036 ,  A43B5/00 ,  A43B9/00 ,  A43B13/04 ,  A43B13/26 ,  A43B23/0215 ,  A43B23/0235 ,  A43B23/024 ,  A43B23/0255 ,  A43B23/0265 ,  A43B23/028 ,  A43B23/04 ,  A43D3/02 ,  A43D95/02 ,  A43D2200/10 ,  B32B1/00 ,  B32B5/02 ,  B32B5/26 ,  B32B37/24 ,  B32B38/004 ,  B32B2305/10 ,  B32B2310/022 ,  B32B2437/02 ,  B33Y80/00

摘要： The invention relates to systems and methods for creating wound material portions for incorporation into an article of footwear. More particularly, one method of manufacturing at least a portion of an upper for an article of footwear, in accordance with the invention, includes the steps of providing a support structure, providing a fiber delivery system, tacking a first end of a first fiber onto the support structure, moving the support structure with respect to the fiber delivery system to wind the first fiber around the support structure, cutting a second end of the first fiber upon positioning of the first fiber onto the support structure, and treating at least a portion of the first fiber to fixedly hold it in a wound arrangement and form a fabric layer for incorporation into an article of footwear.

公开(公告)号：US20180111350A1

公开(公告)日：2018-04-26

申请号：US15562942

申请日：2016-03-24

申请人： Mark Reinhard BERLIN ,  Udo SONDERMANN

发明人： Mark Reinhard BERLIN ,  Udo SONDERMANN

IPC分类号： B32B5/26 ,  B29C65/00 ,  B29C65/52 ,  B32B37/12 ,  B32B37/00

CPC分类号： B32B5/26 ,  B29B15/122 ,  B29C65/524 ,  B29C66/41 ,  B29C70/523 ,  B29K2713/00 ,  B29L2009/00 ,  B32B37/0046 ,  B32B37/1284 ,  B32B2305/10

摘要： By use of a process for the production of a fibre-composite material, comprising the following steps: a) one or more fibre bundle(s) is/are drawn by way of one or more spreader device(s) into an impregnation chamber in such a way as to give at least two mutually superposed, spatially separate and spread fibre webs; b) melt is introduced by way of horizontally oriented distributor bars, in each case arranged between two fibre webs; c) the individual fibre webs are caused to converge in such a way that they are mutually superposed and contact one another; d) after the fibre webs have converged they are drawn, at the end of the operating unit, through a take-off die where the first shaping takes place, and also by use of a corresponding device, very good impregnation quality is achieved through a specific wetting method implemented after a high degree of expanding, and also through subsequent relative longitudinal and transverse movements of the individual fibres.

公开(公告)号：US09931818B1

公开(公告)日：2018-04-03

申请号：US15479872

申请日：2017-04-05

申请人： GENERAL ELECTRIC COMPANY

发明人： Jason Robert Parolini ,  Jon Conrad Schaeffer ,  Arthur S. Peck ,  Srikanth Chandrudu Kottilingam ,  Canan Uslu Hardwicke

IPC分类号： B29C65/00 ,  B29C53/82 ,  C03B29/00 ,  C04B35/64 ,  B32B18/00 ,  B32B7/04 ,  B32B5/08 ,  B32B37/12 ,  B32B38/00 ,  C04B35/573 ,  C04B35/532 ,  C04B35/528 ,  C04B35/571 ,  C04B35/524 ,  C04B35/591 ,  C04B35/622

CPC分类号： B32B18/00 ,  B32B5/08 ,  B32B7/04 ,  B32B2305/10 ,  B32B2313/04 ,  B32B2315/02 ,  B32B2603/00 ,  C04B35/524 ,  C04B35/528 ,  C04B35/532 ,  C04B35/571 ,  C04B35/573 ,  C04B35/591 ,  C04B35/62286 ,  C04B35/6267 ,  C04B35/806 ,  C04B2235/48 ,  C04B2235/5224 ,  C04B2235/5228 ,  C04B2235/5236 ,  C04B2235/524 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/616 ,  C04B2237/38 ,  C04B2237/385 ,  C04B2237/58 ,  F01D5/284

摘要： 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.

公开(公告)号：US20180079192A1

公开(公告)日：2018-03-22

申请号：US15267700

申请日：2016-09-16

申请人： Ethicon, Inc.

发明人： Sasa Andjelic ,  Dominick Egidio

IPC分类号： B32B37/10 ,  B29C47/00 ,  B29C55/30 ,  B32B37/06 ,  B32B27/12 ,  B32B5/02 ,  A61L31/10 ,  A61L31/04 ,  A61L31/14 ,  A61F2/00

CPC分类号： B32B37/10 ,  A61F2/0063 ,  A61K9/7007 ,  A61L31/042 ,  A61L31/048 ,  A61L31/10 ,  A61L31/14 ,  A61L31/148 ,  A61L2420/02 ,  B29C47/0004 ,  B29C47/0021 ,  B29C47/0057 ,  B29C47/0064 ,  B29C47/0066 ,  B29C47/92 ,  B29C55/30 ,  B29C2947/92704 ,  B29C2947/92942 ,  B29C2947/92961 ,  B29K2995/004 ,  B29L2031/753 ,  B32B5/022 ,  B32B5/024 ,  B32B5/028 ,  B32B27/00 ,  B32B27/12 ,  B32B37/06 ,  B32B37/15 ,  B32B2037/0092 ,  B32B2305/10 ,  B32B2535/00 ,  C08L67/04

摘要： The invention relates to novel processes for the lamination of semi-crystalline, high-melting point, low glass transition polymeric films, which are extruded and subsequently laminated on various thermally sensitive substrates to form laminated medical device constructs in a specific time interval to allow low processing temperatures to avoid polymer film and/or substrate degradation or heat-related distortions. Also disclosed are laminated medical device constructs made from such processes.