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公开(公告)号：EP3596160A1
公开(公告)日：2020-01-22
申请号：EP18710065.6
申请日：2018-03-16
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公开(公告)号：EP3375811A1
公开(公告)日：2018-09-19
申请号：EP17382139.8
申请日：2017-03-17
发明人： BLANCO VARELA, Tamara , SÁNCHEZ GÓMEZ, Jose , LAZCANO UREÑA, Silvia , PALERMO, Vincenzo , TREOSSI, Emanuele , MIROTTA, Nicola , SCIDÀ, Alessandra
CPC分类号： C08J7/047 , B32B5/26 , B32B27/18 , B32B27/20 , C08J7/042 , C08J7/06 , C08J2363/00 , D06N3/0063 , D06N3/12 , D06N2209/125 , D06N2209/128 , D06N2213/03
摘要： The present invention provides a multifunctional diffusion barrier comprising at least one organic polymer and a 2D graphene or 2D graphene derivative material, wherein it comprises a gradient concentration of the 2D graphene (derivative) material. It also relates to the method for preparing it. The multifunctional diffusion barrier of the invention can be used as a liquid and/or gas barrier, or as structural material, or as sealing material, or as a self-cleaning material or as protective material against UV radiation in aeronautical, automotive, marine or building field. In particular, the multifunctional diffusion barrier of the invention is particularly suitable in producing parts of aircraft such as a fuel tank, a fuel tank conduit and a gasket.
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公开(公告)号：EP3636427A1
公开(公告)日：2020-04-15
申请号：EP18382723.7
申请日：2018-10-11
发明人： VÁZQUEZ CASTRO, Jesús Javier , GARCÍA MARTÍN, Diego , HERNAIZ LÓPEZ, Guillermo , BLANCO VARELA, Tamara , BARBARA, Olivier
IPC分类号： B32B5/16 , B32B5/22 , B32B5/24 , B32B5/26 , B32B5/30 , B32B7/08 , B32B15/14 , B32B15/16 , B32B27/12 , B32B27/14 , B32B27/28 , B32B27/30 , B32B3/04 , F16L59/02
摘要： Fireproof and thermal insulator product (1), which comprises a material combination of:
- an Earth Silicate material, and
- alumina,
such that the alumina is bonded onto the Earth Silicate material or is diffused inside the Earth Silicate material.-
4.发明公开
公开(公告)号：EP3326799A1
公开(公告)日：2018-05-30
申请号：EP16382550.8
申请日：2016-11-23
发明人： BLANCO VARELA, Tamara , SANCHEZ GOMEZ, Jose , SEGURA MARTINEZ DE ILARDUYA, Leire , MORALES MONGE, Mariano
IPC分类号： B32B5/00 , B32B5/02 , B32B7/00 , B32B7/02 , B32B7/04 , B32B7/10 , B32B9/00 , B32B9/04 , B32B15/00 , B32B15/02 , B32B15/04 , B32B15/20 , B32B27/00 , B32B27/06 , B32B27/28 , B32B3/26
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： The invention refers to a structural composite component (1, 1'), in particular for an aircraft or spacecraft (10), comprising: a lightning strike protection layer (2, 2'); and a composite battery (3) comprising a cathode layer (4, 4') and a separation layer (7), wherein the lighting strike protection layer (2, 2') is formed integrated with the cathode layer (4, 4'), and wherein the separation layer (7) is configured for providing acoustic damping, and/or fire barrier, and/or impact resistance to the structural composite component (1, 1'). The invention further provides a method for configuring such a structural composite component (1, 1'); and an aircraft or spacecraft (10) comprising such a structural composite component (1, 1').
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公开(公告)号：EP3593972A1
公开(公告)日：2020-01-15
申请号：EP18382508.2
申请日：2018-07-09
发明人： BLANCO VARELA, Tamara , BUTRAGUEÑO MARTINEZ, Asuncion , VAZQUEZ CASTRO, Jesus Javier , MARTIN MORENO, Zulima
摘要： The invention refers to a panel structure (1) for an aircraft comprising at least one composite layer (3, 4) and at least one carbon nanotube (CNT) paper (2) laid over the at least one composite layer (3, 4), wherein the CNT paper (2) comprises an aggregation of carbon nanotubes suitable to be heated up to the curing temperature of the panel structure (1). The CNT paper (2) can be attached between two composite layers (3, 4). Alternatively, the CNT paper (2) can be attached to a surface of one composite layer (3, 4) to form the outermost layer of the structure (1) to cure the composite layers (3,4). In this last case, the CNT paper (2) may be covered by an Alkaline Earth Silicate layer (5). The invention provides a heatable panel structure (1). In addition, the panel structure (1) configuration allows the inspection of effects of accidental damages.
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公开(公告)号：EP2660048B1
公开(公告)日：2017-04-19
申请号：EP11854446.9
申请日：2011-12-27
IPC分类号： B32B27/00 , B32B5/26 , B32B7/02 , B32B7/04 , B32B15/08 , B32B15/14 , B32B27/04 , B32B27/12 , B32B5/02 , B32B5/12 , B32B7/12
CPC分类号： B64C1/40 , B32B5/022 , B32B5/024 , B32B5/12 , B32B5/26 , B32B7/02 , B32B7/045 , B32B7/12 , B32B2260/023 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2307/102 , B32B2307/202 , B32B2307/558 , B32B2605/18 , Y10T428/24851 , Y10T428/24995 , Y10T428/249951
摘要： The invention relates to a structure of composite material (1), comprising a continuous first layer (10) of composite material (1), a second layer (20) of viscoelastic material, and a continuous impact-protection third layer (30). The first layer (10) is formed by structural components in the form of a matrix (11) and fibers (12). The second layer (20) of viscoelastic material is added on top of the first layer (10) and said second layer (20) can be continuous or non-continuous. If a non-continuous second layer is used, elongate, circular or square cavities (25) are arranged inside said layer (20). Optionally, reinforcements (13) comprising carbon nanofibers or nanotubes are provided in either of the first and second layers (10, 20). The third layer (30) of impact-protection material is added in a continuous manner on top of the second layer (20), said third layer (30) forming the outermost layer of the composite material (1). In addition, this third layer (30) is electrically conductive. The composite material (1) has noise attenuation, impact resistance and electric conductivity properties.
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7.发明公开MULTIFUNCTIONAL COMPOSITE MATERIAL INCLUDING A VISCOELASTIC INTERLAYER 有权MULTIFUNKELLELLER VERBUNDWERKSTOFF MIT EINER VISKOELASTISCHEN ZWISCHENSCHICHT
公开(公告)号：EP2660048A1
公开(公告)日：2013-11-06
申请号：EP11854446.9
申请日：2011-12-27
IPC分类号： B32B27/00
CPC分类号： B64C1/40 , B32B5/022 , B32B5/024 , B32B5/12 , B32B5/26 , B32B7/02 , B32B7/045 , B32B7/12 , B32B2260/023 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2307/102 , B32B2307/202 , B32B2307/558 , B32B2605/18 , Y10T428/24851 , Y10T428/24995 , Y10T428/249951
摘要： The invention relates to a structure of composite material (1), comprising a continuous first layer (10) of composite material (1), a second layer (20) of viscoelastic material, and a continuous impact-protection third layer (30). The first layer (10) is formed by structural components in the form of a matrix (11) and fibers (12). The second layer (20) of viscoelastic material is added on top of the first layer (10) and said second layer (20) can be continuous or non-continuous. If a non-continuous second layer is used, elongate, circular or square cavities (25) are arranged inside said layer (20). Optionally, reinforcements (13) comprising carbon nanofibers or nanotubes are provided in either of the first and second layers (10, 20). The third layer (30) of impact-protection material is added in a continuous manner on top of the second layer (20), said third layer (30) forming the outermost layer of the composite material (1). In addition, this third layer (30) is electrically conductive. The composite material (1) has noise attenuation, impact resistance and electric conductivity properties.
摘要翻译： 本发明涉及复合材料（1）的结构，其包括复合材料（1）的连续第一层（10），粘弹性材料的第二层（20）和连续冲击保护第三层（30）。 第一层（10）由基体（11）和纤维（12）形式的结构部件形成。 粘弹性材料的第二层（20）被添加在第一层（10）的顶部上，并且所述第二层（20）可以是连续的或不连续的。 如果使用非连续的第二层，则细长的圆形或方形空腔（25）布置在所述层（20）的内部。 任选地，包括碳纳米纤维或纳米管的增强件（13）设置在第一和第二层（10,20）中的任一个中。 冲击保护材料的第三层（30）以连续的方式添加到第二层（20）的顶部，所述第三层（30）形成复合材料（1）的最外层。 此外，该第三层（30）是导电的。 复合材料（1）具有噪声衰减，抗冲击性和导电性。
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