公开(公告)号：US10000299B2

公开(公告)日：2018-06-19

申请号：US14838442

申请日：2015-08-28

申请人： THE BOEING COMPANY

发明人： Waeil M. Ashmawi ,  Sahrudine Apdalhaliem

IPC分类号： B64F5/00 ,  B29C65/02 ,  B01J35/06 ,  B64C1/10 ,  B01J31/06 ,  B29C65/54 ,  B29C65/48 ,  B29K701/12 ,  B29L9/00 ,  B29L31/30

CPC分类号： B64F5/40 ,  B01J31/06 ,  B29C65/14 ,  B29C66/112 ,  B29C66/116 ,  B29C66/532 ,  B29C73/22 ,  B29K2701/12 ,  B29K2713/00 ,  B29L2009/00 ,  B29L2031/3082 ,  B64C1/062 ,  B64C1/10 ,  B64C1/12

摘要： Methods and apparatuses are disclosed relating to multilayer 3D textile composite materials containing self-healing resins for use as protective structures on stationary objects, and moving objects including, without limitation, vehicles including spacecraft and aircraft.

公开(公告)号：US20180155858A1

公开(公告)日：2018-06-07

申请号：US15737665

申请日：2016-06-17

申请人： Groz-Beckert KG

发明人： Ezzeddine Laourine

IPC分类号： D03D3/00 ,  D03D13/00 ,  D03D15/00 ,  D03D49/70

CPC分类号： D03D3/00 ,  B29C70/22 ,  B29K2671/12 ,  B29K2713/00 ,  B29K2995/0077 ,  D03D13/00 ,  D03D13/004 ,  D03D15/00 ,  D03D41/008 ,  D03D47/18 ,  D03D47/23 ,  D03D47/39 ,  D03D49/06 ,  D03D49/70 ,  D10B2331/06 ,  D10B2403/03 ,  D10B2505/02

摘要： A two-dimensional fabric (20) used to produce a three-dimensional composite part has a binding system (21) with binding warp threads (23) and/or binding weft threads (24) and a reinforcing system (22) with reinforcing weft threads (25) and/or reinforcing warp threads (26). At least some of the inserted reinforcing threads (25) are shortened reinforcing weft threads (25a) and/or shortened reinforcing warp threads (26a). Their thread length (L) is less than that of the binding weft threads (24) or the binding warp threads (23). The shortened reinforcing thread's (25a), (26a) free ends are located in a respective thread end position (30) or (31). The respective thread length (L) and the respective thread end positions (30), (31) of a shortened reinforcing thread (25a), (26a) in the two-dimensional fabric (20) are predetermined based on the three-dimensional shape of the composite part to be produced to reduce cutting waste when producing preforms and cutting effort.

公开(公告)号：US09988156B2

公开(公告)日：2018-06-05

申请号：US14696073

申请日：2015-04-24

申请人： IHI Corporation ,  IHI AEROSPACE CO., LTD.

发明人： Agamu Tanaka ,  Hideo Morita ,  Ikuo Okumura ,  Yuu Shigenari ,  Takashi Harada ,  Yusuke Dan

IPC分类号： B64D29/02 ,  F01D25/24 ,  F01D21/04 ,  B29C70/44 ,  B29C33/30 ,  B29C70/22 ,  B29C70/24 ,  B29C70/54 ,  B29L31/00 ,  B29K101/10 ,  B29L9/00 ,  B29L22/00 ,  B29L23/00

CPC分类号： B64D29/02 ,  B29C33/301 ,  B29C70/22 ,  B29C70/222 ,  B29C70/24 ,  B29C70/446 ,  B29C70/54 ,  B29K2101/10 ,  B29K2713/00 ,  B29L2009/00 ,  B29L2022/00 ,  B29L2023/003 ,  B29L2031/7504 ,  B29L2031/772 ,  F01D21/045 ,  F01D25/24 ,  F01D25/243 ,  F05D2220/36 ,  F05D2300/603 ,  F05D2300/6034 ,  Y02T50/672

摘要： A cylindrical case includes a case main body, and a groove disposed annularly at one end of the case main body. A peripheral wall of the case main body is formed by alternately laminating a biaxial fabric layer, which includes a biaxial fabric of a non-crimp structure composed of reinforcing fiber bands having an orientation angle of ±45°, and a roving layer. A groove wall of the groove is formed by alternately laminating the biaxial fabric layer, which continues to the case main body side, and a triaxial fabric layer, which includes a triaxial fabric of a non-crimp structure composed of reinforcing fiber bands having an orientation angle of ±45° and a reinforcing fiber band having an orientation angle of 0°.

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：US09937683B2

公开(公告)日：2018-04-10

申请号：US14746365

申请日：2015-06-22

申请人： Panasonic Intellectual Property Management Co., Ltd.

发明人： Kazuma Oikawa ,  Kei Toyota ,  Daido Kohmyohji ,  Shigeaki Sakatani

IPC分类号： B32B5/18 ,  B32B5/02 ,  B32B5/26 ,  B32B7/00 ,  B32B7/02 ,  B32B9/00 ,  B32B9/04 ,  H01L23/373 ,  B29C65/02 ,  B29C65/00 ,  B32B7/04 ,  B32B17/06 ,  B32B37/06 ,  B32B37/18 ,  G06F1/16 ,  H01L23/36 ,  B29K707/04 ,  B29L31/34

CPC分类号： B32B5/18 ,  B29C65/02 ,  B29C66/7294 ,  B29C66/73113 ,  B29C66/7444 ,  B29K2707/04 ,  B29K2713/00 ,  B29K2715/003 ,  B29L2031/3481 ,  B32B5/022 ,  B32B5/026 ,  B32B5/26 ,  B32B7/005 ,  B32B7/02 ,  B32B7/04 ,  B32B9/007 ,  B32B9/047 ,  B32B17/06 ,  B32B37/06 ,  B32B37/182 ,  B32B2250/02 ,  B32B2250/03 ,  B32B2266/0228 ,  B32B2266/0278 ,  B32B2266/0285 ,  B32B2266/04 ,  B32B2266/057 ,  B32B2266/06 ,  B32B2266/102 ,  B32B2266/126 ,  B32B2305/22 ,  B32B2307/302 ,  B32B2307/304 ,  B32B2307/706 ,  B32B2313/04 ,  B32B2457/00 ,  B32B2457/04 ,  G06F1/1656 ,  H01L23/36 ,  H01L23/373 ,  H01L2924/0002 ,  H01L2924/00

摘要： A composite sheet includes a graphite layer, a heat insulation layer including a fiber and a heat insulation material and a fiber layer located between the graphite layer and the heat insulation layer, wherein the fiber layer comprises the fiber. An electronic apparatus includes an electronic component that involves heat generation, a housing and the composite sheet, wherein the composite sheet is placed between the electronic component and the housing.

公开(公告)号：US09931794B2

公开(公告)日：2018-04-03

申请号：US14756567

申请日：2015-09-18

申请人： Pascale Industries, Inc.

发明人： Willorage Rathna Perera

IPC分类号： B29C70/22 ,  B29C70/54 ,  D06B3/06

CPC分类号： D06B3/06 ,  B29B15/122 ,  B29C70/30 ,  B29K2713/00 ,  D06B1/14 ,  D06B11/0026

摘要： Yarns for use in manufacture of composite structures are intermittently coated with adhesive, and may be twisted as well. These yarns are then woven into fabric, and heat and pressure applied to the intermittently-coated yarns to provide dimensional stability and to prevent unravelling of the fabric during cutting and handling. The fabric is then disposed in a mold or over a mandrel, and a curable resin applied and caused to cure. Provision of the adhesive in intermittent fashion limits propagation of cracks that may form at the location of the adhesive, which does not bond well to the curable resin.

公开(公告)号：US09914274B2

公开(公告)日：2018-03-13

申请号：US14645714

申请日：2015-03-12

申请人： NIKE, Inc.

发明人： David P. Jones ,  Ryan R. Larson

IPC分类号： B29D35/12 ,  B29C67/00 ,  A43B13/14 ,  B33Y80/00 ,  B33Y10/00 ,  A43B1/04 ,  A43B3/00 ,  A43B23/02 ,  A43D11/00 ,  B29C70/78 ,  B29C64/112 ,  B29L31/50

CPC分类号： B29D35/12 ,  A43B1/04 ,  A43B3/0084 ,  A43B13/14 ,  A43B23/0235 ,  A43B23/026 ,  A43D11/00 ,  A43D2200/00 ,  A43D2200/60 ,  B29C64/112 ,  B29C70/78 ,  B29K2713/00 ,  B29L2031/50 ,  B33Y10/00 ,  B33Y80/00

摘要： Methods and systems are disclosed for apparel assembly using three-dimensional printing directly onto fabric apparel materials. Disclosed is a method and system for direct three-dimensional printing and assembly of an article of apparel, including designing a three-dimensional pattern for printing, positioning at least a portion of the article on a tray in a three-dimensional printing system, the portion being positioned substantially flat on the tray, printing a three-dimensional material directly onto the article using the designed pattern, curing the printed material, and removing the article from the three-dimensional printing system.

公开(公告)号：US20180010462A1

公开(公告)日：2018-01-11

申请号：US15201979

申请日：2016-07-05

申请人： Safran Aircraft Engines

发明人： Jeremy GUIVARC'H ,  Francois Charleux

IPC分类号： F01D5/14 ,  F01D5/28 ,  B29B11/16 ,  B29C45/02 ,  B29C45/14 ,  B29L31/08

CPC分类号： F01D5/143 ,  B29B11/16 ,  B29C45/02 ,  B29C45/14631 ,  B29K2713/00 ,  B29L2031/082 ,  D03D1/00 ,  D03D13/004 ,  D03D25/005 ,  D10B2505/02 ,  F01D5/282 ,  F01D11/008 ,  F05D2220/36 ,  F05D2240/80 ,  F05D2300/6012 ,  F05D2300/6034

摘要： The invention provides a fitted platform (1) for positioning between two adjacent blades of an aviation turbine engine fan, said platform comprising a flow passage wall (10) made of composite material having a central portion (16) and first and second margins (18) each extending in a longitudinal direction of said wall, each margin extending over a determined distance (D) from the central portion (16) in a transverse direction of said wall, said flow passage wall comprising fiber reinforcement densified by a matrix, the platform being characterized in that the fiber reinforcement present in the central portion (16) presents three-dimensional weaving, and in that the fiber reinforcement present in the first and second margins (18) presents two-dimensional weaving, at least in part. The invention also provides a fan module, a turbine engine, and a method of fabricating such a platform.

公开(公告)号：US20170334101A1

公开(公告)日：2017-11-23

申请号：US15598705

申请日：2017-05-18

申请人： Mohawk Carpet Distribution, Inc.

发明人： Kenneth Mooney ,  David Sandiford

IPC分类号： B29C39/10 ,  B29C39/38 ,  B29K105/20 ,  B29L31/00

CPC分类号： B29C39/10 ,  A47G27/0268 ,  A47G27/045 ,  B29C39/38 ,  B29C47/0009 ,  B29C67/0044 ,  B29K2105/20 ,  B29K2713/00 ,  B29K2995/0039 ,  B29L2031/7322 ,  D06N7/00 ,  Y10T428/16 ,  Y10T428/163 ,  Y10T428/164 ,  Y10T428/19

摘要： Various embodiments are directed to an airline carpet kit comprising a plurality of carpet components collectively forming a substantially continuous floor covering, for example, for use within an aircraft interior. Each of the plurality of carpet components comprises a tufted carpet backing having a plurality of carpet tufts extending from a back surface of the carpet backing and above a top surface of the carpet backing; and an edge strip comprising an amorphous plastic material, wherein the edge strip extends around a lateral edge of the carpet backing between a base portion embedded within a back surface of the carpet backing and an edge surface defining a perimeter edge of the carpet component. The edge surface of a first carpet component abuts an edge surface of an adjacent second carpet component to form an at least substantially continuous floor covering for an aircraft interior.

公开(公告)号：US20170326820A1

公开(公告)日：2017-11-16

申请号：US15527196

申请日：2015-11-10

申请人： Toray Industries, Inc.

发明人： Takashi Fujioka ,  Masato Honma

IPC分类号： B29C70/46 ,  B29C45/14 ,  B29C43/18 ,  B32B5/26 ,  B29B11/12

CPC分类号： B29C70/46 ,  B29B11/12 ,  B29C43/18 ,  B29C43/20 ,  B29C45/14 ,  B29C45/14811 ,  B29C2043/186 ,  B29C2043/188 ,  B29C2043/189 ,  B29K2713/00 ,  B32B3/266 ,  B32B5/022 ,  B32B5/024 ,  B32B5/26 ,  B32B5/28 ,  B32B7/12 ,  B32B27/08 ,  B32B27/12 ,  B32B27/20 ,  B32B27/22 ,  B32B27/26 ,  B32B27/281 ,  B32B27/285 ,  B32B27/286 ,  B32B27/288 ,  B32B27/302 ,  B32B27/308 ,  B32B27/32 ,  B32B27/34 ,  B32B27/36 ,  B32B27/365 ,  B32B27/38 ,  B32B27/40 ,  B32B27/42 ,  B32B33/00 ,  B32B2255/02 ,  B32B2255/205 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/02 ,  B32B2262/0269 ,  B32B2262/04 ,  B32B2262/065 ,  B32B2262/10 ,  B32B2262/101 ,  B32B2262/103 ,  B32B2262/105 ,  B32B2262/106 ,  B32B2262/14 ,  B32B2307/72 ,  B32B2307/724 ,  B32B2419/00 ,  B32B2419/06 ,  B32B2457/00 ,  B32B2605/00 ,  B32B2605/08 ,  B32B2605/18

摘要： A laminate includes reinforcing fibers, thermosetting resin (B) or thermoplastic resin (D), wherein adhesion with other members, particularly in high-temperature atmospheres, is outstanding. The laminate includes: a porous substrate (C) comprising a thermoplastic resin (c), reinforcing fibers (A) and a thermosetting resin (B), or a porous substrate (C) comprising a thermoplastic resin (c), reinforcing fibers (A) and a thermoplastic resin (D); wherein the porous substrate (C) has a gap part continuous in the thickness direction of the laminate, and the melting point or softening point is higher than 180° C., and at least 10% of the surface area of one surface of the porous substrate (C) is exposed on one side of the laminate.