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公开(公告)号：US12076968B2
公开(公告)日：2024-09-03
申请号：US18546030
申请日：2021-10-11
发明人： Yukihiro Kamimura , Tomohiro Ito
CPC分类号： B32B37/144 , B32B5/18 , B32B7/10 , B32B7/12 , B32B27/08 , B32B27/286 , B32B27/38 , B32B37/06 , B32B2250/02 , B32B2250/24 , B32B2266/0214 , B32B2307/30 , B32B2307/72 , B32B2307/736
摘要： A method of molding a sandwich panel includes a step of providing, on one or both surfaces of an (a) core material, a prepreg or the prepreg and an adhesive as a (b) skin material. The (a) core material is a super engineering plastic foam having a glass transition temperature of greater than 200° C. The (b) skin material contains: a (b-1) epoxy resin having an average molecular weight of 1300 or more or having a trishydroxymethane-type or cresol novolac-type structure and containing, in a total epoxy resin, an amount of 70 to 100 mass % of an epoxy resin that is semi-solid or solid; a (b-2) epoxy resin containing, in the total epoxy resin, an amount of 0 to 30 mass % of an epoxy resin that is liquid; and a (b-3) curing agent.
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公开(公告)号：US12064941B2
公开(公告)日：2024-08-20
申请号：US16953445
申请日：2020-11-20
申请人： Pyroguard UK Ltd.
CPC分类号： B32B17/10678 , B32B7/023 , B32B7/10 , B32B17/10036 , B32B17/10697 , B32B2250/03 , B32B2250/05 , B32B2250/42 , B32B2305/72 , B32B2307/3065 , B32B2307/412 , B32B2307/71 , B32B2551/00
摘要： This specification generally relates to aqueous compositions for preparing UV stable fire-resistant interlayers. It also relates to UV stable fire-resistant glazing laminates comprising such interlayers, the use of such glazing laminates in construction, and constructions comprising such glazings. An example aqueous composition comprises a mixed alkali metal silicate of general formula SiO2·M2O, where M is K or Na, and other organic and inorganic additives. Glazings with interlayers made with such aqueous compositions are simple to prepare and demonstrate good UV stability and fire-protection properties.
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公开(公告)号：US11767621B2
公开(公告)日：2023-09-26
申请号：US18162952
申请日：2023-02-01
发明人： James T. Burns , Thomas Odum , Derek S. Bass
CPC分类号： D04H1/498 , B32B5/266 , B32B7/09 , B32B7/10 , D04H1/485 , D04H1/542 , D04H18/02 , B32B2250/02 , B32B2250/20 , B32B2262/00 , B32B2307/308 , B32B2471/00
摘要： Described is a composite made from a woven fabric, a non-woven fabric, or a knitted face fabric and a non-woven fabric. The woven fabric, the non-woven fabric, or the knitted face fabric is needle punched such that fibers protrude into the non-woven fabric. The woven fabric, the non-woven fabric, or the knitted face fabric has a first polymer having a first melting point and a second polymer having a second melting point being higher than the first melting point. The nonwoven backing material comprises a third polymer having a third melting point and a fourth polymer having a fourth melting point being higher than the third melting point. The woven fabric, the non-woven fabric, or the knitted face fabric is further bonded to the nonwoven backing material applying heat to at least partially melt or soften the first polymer and the third polymer such that they bond together.
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公开(公告)号：US11738535B2
公开(公告)日：2023-08-29
申请号：US16941418
申请日：2020-07-28
申请人： EEnotech, Inc.
发明人： Cindy Yee Cin Lau , Pei Zhu
IPC分类号： B32B5/26 , B32B5/02 , B32B27/12 , B32B7/12 , B32B7/09 , B32B7/05 , B32B7/10 , B32B5/06 , B32B27/32
CPC分类号： B32B5/26 , B32B5/022 , B32B5/06 , B32B7/05 , B32B7/09 , B32B7/10 , B32B7/12 , B32B27/12 , B32B27/32 , B32B2250/02 , B32B2250/20 , B32B2255/02 , B32B2255/205 , B32B2307/406 , B32B2307/414 , B32B2307/724 , B32B2307/732 , B32B2437/00
摘要： A metallized breathable composite textile includes a lining layer and a metallized non-woven sheet disposed on the lining layer. The metallized non-woven sheet includes a base layer containing a polymer and a metal layer deposited on a first surface of the base layer. The lining layer is connected to the metallized non-woven sheet via point contacts.
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公开(公告)号：US20230249444A1
公开(公告)日：2023-08-10
申请号：US18300085
申请日：2023-04-13
申请人： RENOLIT SE
CPC分类号： B32B27/08 , B32B7/10 , B32B27/302 , B32B27/306 , B32B27/32 , B32B27/34 , B32B27/365 , B32B2250/05 , B32B2250/42 , B32B2307/412 , B32B2307/54 , B32B2307/546 , B32B2307/558 , B32B2307/7244 , B32B2307/7246 , B32B2307/7248 , B32B2307/736 , B32B2439/80 , B32B2535/00
摘要： Laminate structure comprising an alternating stack of layers from polymer blends AC and BD having the sequence -AC-[BD-AC-]n with n from 4 to 36, wherein the layer thickness of layers AC and layers BD is less than 3 μm, wherein A and B are thermoplastic polymers and C and D are thermoplastic elastomers, wherein the thermoplastic polymer B has functional barrier properties, wherein the amount of the thermoplastic elastomers C and D in the polymer blends AC and BD is each from 3 to 45 wt.-%, and polymer B and elastomer D are essentially incompatible.
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公开(公告)号：US20230175177A1
公开(公告)日：2023-06-08
申请号：US18162952
申请日：2023-02-01
发明人： James T. Burns , Thomas Odum , Derek S. Bass
CPC分类号： D04H1/498 , B32B7/09 , D04H18/02 , B32B5/266 , B32B7/10 , D04H1/485 , D04H1/542 , B32B2471/00 , B32B2250/20 , B32B2262/00 , B32B2307/308 , B32B2250/02
摘要： Described is a composite made from a woven fabric, a non-woven fabric, or a knitted face fabric and a non-woven fabric. The woven fabric, the non-woven fabric, or the knitted face fabric is needle punched such that fibers protrude into the non-woven fabric. The woven fabric, the non-woven fabric, or the knitted face fabric has a first polymer having a first melting point and a second polymer having a second melting point being higher than the first melting point. The nonwoven backing material comprises a third polymer having a third melting point and a fourth polymer having a fourth melting point being higher than the third melting point. The woven fabric, the non-woven fabric, or the knitted face fabric is further bonded to the nonwoven backing material applying heat to at least partially melt or soften the first polymer and the third polymer such that they bond together.
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公开(公告)号：US20190240874A1
公开(公告)日：2019-08-08
申请号：US16265966
申请日：2019-02-01
申请人： Jeonjin Co.,Ltd.
发明人： Ho Seok YANG
CPC分类号： B29C33/405 , B28B7/348 , B29C33/3842 , B29C67/243 , B29K2823/04 , B29K2823/12 , B29K2913/00 , B32B3/02 , B32B3/08 , B32B3/263 , B32B3/30 , B32B5/02 , B32B7/10 , B32B25/02 , B32B25/10 , B32B25/14 , B32B37/00 , B32B2250/04 , B32B2250/42 , B32B2307/554
摘要： The present disclosure herein relates to a mold for manufacturing a slab. More particularly, the mold includes a first fabric layer, a first rubber layer disposed on the first fabric layer, a second fabric layer disposed on the first rubber layer, and a second rubber layer disposed on the second fabric layer. Here, the second rubber layer includes a base part and a frame part extending from an edge of the base part. Also, the base part and the frame part are integrated with each other.
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公开(公告)号：US20180244024A1
公开(公告)日：2018-08-30
申请号：US15442318
申请日：2017-02-24
发明人： Masato USHIJIMA
IPC分类号： B32B27/32 , B32B27/30 , B32B15/085
CPC分类号： B32B27/32 , B32B7/10 , B32B15/085 , B32B27/08 , B32B27/308 , B32B2255/06 , B32B2255/10 , B32B2255/205 , B32B2255/26 , B32B2255/28 , B32B2270/00 , B32B2274/00 , B32B2307/30 , B32B2307/408 , B32B2307/516 , B32B2307/518 , B32B2307/538 , B32B2307/54 , B32B2307/748 , B32B2405/00 , B44C1/1708
摘要： A release film including a monoaxially or biaxially oriented multilayer polyolefin-based film having a crystallizable polyolefin core film layer and at least one coextruded skin layer having a poly-4-methyl-1-pentene composition blended with an olefin copolymer elastomer modifier. The film's release surface has a peeling force value of 1500 g/inch or less and a 60° angle surface gloss of below 50 gloss units (GU). An embodiment is a film structure having (a) a metal transfer carrier film having polyolefin as described above and (b) a coated metal layer having a metal layer and a coating layer, wherein the coating layer lies between the metal layer and the metal transfer carrier film, wherein the metal transfer carrier film is configured to allow transfer of the coated metal layer onto a substrate, so that after transfer of the coated metal layer onto the substrate, the coating layer is located on top of the substrate.
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公开(公告)号：US20180186139A1
公开(公告)日：2018-07-05
申请号：US15804210
申请日：2017-11-06
发明人： Ajay Padsalgikar
CPC分类号： B32B37/06 , B29C59/08 , B29C65/4895 , B29C66/028 , B29C66/71 , B32B7/10 , B32B7/12 , B32B27/08 , B32B27/28 , B32B27/40 , B32B2535/00 , C08G77/16 , C08J5/121 , C08J7/04 , C08J2375/04 , C08J2383/04 , C09J5/02 , C09J175/04 , C09J2475/003 , C09J2475/006 , C09J2483/006 , C09J2483/008 , Y10T428/31598 , B29K2083/00 , B29K2075/00
摘要： The invention relates to a process for bonding a silicone or silicone based material to a polyurethane and use of the bonded silicone-polyurethane in the manufacture of biomaterials, devices, articles or implants, in particular long term implantable medical devices in the fields of cardiology, orthopaedics, plastic surgery and gastroenterology. The process involves the steps of (a) flame treating a surface of the silicone or silicone based material and (b) bonding the polyurethane to the flame treated surface of the silicone or silicone based material.
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10.发明申请公开(公告)号：US20180155055A1
公开(公告)日：2018-06-07
申请号：US15817826
申请日：2017-11-20
发明人： Tamara Blanco Varela , José Sanchez Gomez , Leire Segura Martinez De Ilarduya , Mariano Morales Monge
CPC分类号： B64D45/02 , B29C70/885 , B32B3/26 , B32B5/00 , B32B5/02 , B32B7/00 , B32B7/02 , B32B7/04 , B32B7/06 , B32B7/10 , B32B9/00 , B32B9/04 , B32B15/00 , B32B15/02 , B32B15/04 , B32B15/08 , B32B15/14 , B32B15/20 , B32B27/00 , B32B27/06 , B32B27/28 , B32B2250/00 , B32B2262/00 , B32B2262/106 , B32B2307/10 , B32B2307/102 , B32B2307/20 , B32B2307/202 , B32B2307/30 , B32B2307/3065 , B32B2307/50 , B32B2307/558 , B32B2307/56 , B32B2307/732 , B32B2457/00 , B32B2457/10 , B32B2571/00 , B32B2605/00 , B32B2605/18 , H01M2/0267 , H01M2/0295
摘要： A structural composite component, in particular for an aircraft or spacecraft, includes: a lightning strike protection layer; and a composite battery including a cathode layer and a separation layer, wherein the lightning strike protection layer is formed integrated with the cathode layer, and wherein the separation layer is configured for providing acoustic damping, and/or fire barrier, and/or impact resistance to the structural composite component. A method for configuring such a structural composite component; and an aircraft or spacecraft including such a structural composite component are also described.
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