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公开(公告)号：US20090004480A1
公开(公告)日：2009-01-01
申请号：US11770263
申请日：2007-06-28
IPC分类号： B32B15/08
CPC分类号： B32B17/04 , B32B15/08 , B32B15/20 , B32B27/281 , B32B2307/206 , B32B2605/18 , Y10T428/31529 , Y10T428/31678
摘要： An exemplary embodiment provides a composite substrate including a resin matrix that has embedded therein a flex circuit and reinforcing filler. The flex circuit includes a metallic circuit on a film that is co-cured with the resin matrix. The metallic circuit may be configured for any of a variety of functions, including for example, dissipating energy generated by a lightning strike on the composite substrate. The flex circuit may also provide a platform for implementation of other communication and maintenance functions.
摘要翻译： 示例性实施例提供了一种复合衬底，其包括嵌入柔性电路和增强填料的树脂基体。 柔性电路包括在与树脂基体共固化的膜上的金属电路。 金属电路可以被配置用于各种功能中的任一种，包括例如消散由复合衬底上的雷击产生的能量。 柔性电路还可以提供用于实现其他通信和维护功能的平台。
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公开(公告)号：US07934676B2
公开(公告)日：2011-05-03
申请号：US12056139
申请日：2008-03-26
IPC分类号： B64D45/02
CPC分类号： B64D45/02 , Y10T428/24612 , Y10T428/24917
摘要： A pre-fabricated article for a composite aircraft component includes a dielectric layer and a pre-fabricated metalized pattern on the dielectric layer. The metalized pattern is fabricated on the dielectric layer prior to integration with the composite aircraft component. The metalized pattern diverts EME current away from EME protection areas of the aircraft component.
摘要翻译： 用于复合飞机部件的预制制品包括电介质层和介电层上的预制金属化图案。 在与复合飞行器部件集成之前，在电介质层上制造金属化图案。 金属化图案将EME电流远离飞机部件的EME保护区域。
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公开(公告)号：US07883050B2
公开(公告)日：2011-02-08
申请号：US11770263
申请日：2007-06-28
CPC分类号： B32B17/04 , B32B15/08 , B32B15/20 , B32B27/281 , B32B2307/206 , B32B2605/18 , Y10T428/31529 , Y10T428/31678
摘要： An aircraft component includes a composite structure and a metallic circuit on a film. The film is co-cured with the composite structure. The metallic circuit is patterned to dissipate energy generated by lightning strikes on the composite structure. The metal circuit is also patterned to provide connectivity for multi-function apparatus.
摘要翻译： 飞机部件包括复合结构和薄膜上的金属电路。 该膜与复合结构共固化。 金属电路被图案化以消散由复合结构上的雷击产生的能量。 金属电路也被图案化以提供多功能设备的连接。
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4.发明授权Circuit joining assembly materials for multi-layer lightning protection systems on composite aircraft 有权复合飞机上用于多层防雷系统的电路接合组装材料公开(公告)号：US07829796B2
公开(公告)日：2010-11-09
申请号：US11935993
申请日：2007-11-06
IPC分类号： H01R12/04
CPC分类号： H05K3/225 , H05K1/0393 , H05K2201/09672 , H05K2201/1028 , H05K2203/173
摘要： An exemplary embodiment provides a multi-layer circuit joining assembly material configured to repair multi-layer flex circuits deployed on or in a composite surface as a lightning protection system. The multi-layer circuit joining assembly material includes a first conductive layer having a first end portion, a second conductive layer having a second end portion, and a dielectric material between the first conductive layer and the second conductive layer.
摘要翻译： 示例性实施例提供了多层电路接合组件材料，其被配置为修复部署在复合表面上或复合表面中的多层柔性电路作为防雷系统。 多层电路接合组件材料包括具有第一端部的第一导电层，具有第二端部的第二导电层，以及位于第一导电层和第二导电层之间的介电材料。
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5.发明申请公开(公告)号：US20090114427A1
公开(公告)日：2009-05-07
申请号：US11935993
申请日：2007-11-06
IPC分类号： H05K1/03
CPC分类号： H05K3/225 , H05K1/0393 , H05K2201/09672 , H05K2201/1028 , H05K2203/173
摘要： An exemplary embodiment provides a multi-layer circuit joining assembly material configured to repair multi-layer flex circuits deployed on or in a composite surface as a lightning protection system. The multi-layer circuit joining assembly material includes a first conductive layer having a first end portion, a second conductive layer having a second end portion, and a dielectric material between the first conductive layer and the second conductive layer.
摘要翻译： 示例性实施例提供了多层电路接合组件材料，其被配置为修复部署在复合表面上或复合表面中的多层柔性电路作为防雷系统。 多层电路接合组件材料包括具有第一端部的第一导电层，具有第二端部的第二导电层，以及位于第一导电层和第二导电层之间的介电材料。
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公开(公告)号：US20090001217A1
公开(公告)日：2009-01-01
申请号：US12056139
申请日：2008-03-26
CPC分类号： B64D45/02 , Y10T428/24612 , Y10T428/24917
摘要： A pre-fabricated article for a composite aircraft component includes a dielectric layer and a pre-fabricated metalized pattern on the dielectric layer. The metalized pattern is fabricated on the dielectric layer prior to integration with the composite aircraft component. The metalized pattern diverts EME current away from EME protection areas of the aircraft component.
摘要翻译： 用于复合飞机部件的预制制品包括电介质层和介电层上的预制金属化图案。 在与复合飞行器部件集成之前，在电介质层上制造金属化图案。 金属化图案将EME电流远离飞机部件的EME保护区域。
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7.发明授权公开(公告)号：US08658256B2
公开(公告)日：2014-02-25
申请号：US13527795
申请日：2012-06-20
申请人： Shahnaz Shokri , Quynhgiao N. Le , Christopher Broadbent , Alexandra Elena Corona , Terrell Diane Riley
发明人： Shahnaz Shokri , Quynhgiao N. Le , Christopher Broadbent , Alexandra Elena Corona , Terrell Diane Riley
IPC分类号： B05D1/06
CPC分类号： H01B1/04 , B05D1/04 , B05D1/045 , B05D2201/02 , B05D2203/35 , B05D2601/20 , C23C30/00 , F01D5/288 , F05D2230/31 , F41H3/00 , Y02T50/671 , Y02T50/673 , Y10T428/24893 , Y10T428/249921
摘要： Methods include applying an electric charge to a coating material that includes carbon nanotubes and a carrier, such as paint, and depositing the electrically charged coating material to a substrate. In some methods, the applying includes utilizing an electrostatic sprayer. In some methods, the substrate is isolated from ground during the depositing. In some methods, the substrate is an insulator. Some methods result in regions of carbon nanotubes that are substantially longitudinally aligned after the depositing. Coated substrates may include a coating with carbon nanotubes that are substantially longitudinally aligned. Aircraft, spacecraft, land vehicles, marine vehicles, wind turbines, and apparatuses that may be susceptible to lightning strikes or other types of electromagnetic effects and that include a coated substrate also are disclosed.
摘要翻译： 方法包括将电荷施加到包括碳纳米管的涂层材料和诸如涂料的载体上，并将带电涂层材料沉积到基底上。 在一些方法中，应用包括利用静电喷雾器。 在一些方法中，在沉积期间将衬底与地离开。 在一些方法中，衬底是绝缘体。 一些方法导致在沉积之后基本纵向排列的碳纳米管区域。 涂覆的基底可以包括具有基本上纵向对准的碳纳米管的涂层。 还公开了可能易受雷击或其他类型的电磁效应的飞机，航天器，陆地车辆，船用车辆，风力涡轮机以及包括涂覆基板的设备。
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公开(公告)号：US07835130B2
公开(公告)日：2010-11-16
申请号：US11867886
申请日：2007-10-05
CPC分类号： B64D37/32 , B32B33/00 , B32B38/162 , B32B2038/0092 , B32B2307/204 , B32B2605/18 , B64D45/02 , Y02T50/44 , Y10T428/31678
摘要： A method and apparatus for lighting protection. In one advantageous embodiment a method forms a lighting protection system on a composite surface of an aircraft. A dielectric coating is formed on the composite surface in which the dielectric coating covers a metal feature exposed on the composite surface. A metal adhesion promoter is applied in a pattern on the dielectric coating and over additional areas of the composite surface, including a grounding feature to form a metal adhesion promoter layer. A metal coating is formed on the metal adhesion promoter layer to create a path from an area including the metal feature to the grounding feature.
摘要翻译： 一种照明保护的方法和装置。 在一个有利的实施例中，一种方法在飞行器的复合表面上形成照明保护系统。 在复合表面上形成电介质涂层，其中电介质涂层覆盖暴露在复合表面上的金属特征。 金属粘合促进剂以图案施加在电介质涂层上和复合表面的其它区域上，包括接地特征以形成金属粘附促进剂层。 在金属粘合促进剂层上形成金属涂层以产生从包括金属特征的区域到接地特征的路径。
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公开(公告)号：US07277266B1
公开(公告)日：2007-10-02
申请号：US11277888
申请日：2006-03-29
IPC分类号： H05F3/00
CPC分类号： B64D45/02
摘要： A lightning protection system for protecting composite structures and a method of protecting composite structures from lightning strikes. A dielectric ply is fixed above and completely covers metal surface features, e.g., skin fasteners through a composite skin to a wing fuel tank. A conductive ply is fixed above and completely covers the dielectric ply and extends to an external connection to a platform ground. The conductive ply directs current from lightning strikes away from metal surface features, e.g., to the platform ground. Both plies may be adhesively backed and sequentially pressed into place.
摘要翻译： 一种用于保护复合结构的防雷系统和一种保护复合结构免受雷击的方法。 电介质层被固定在上面并完全覆盖金属表面特征，例如通过复合皮肤到翼片燃料箱的皮肤紧固件。 导电层固定在电介质层的上方并完全覆盖并延伸到与平台接地的外部连接。 导电层将来自雷击的电流从金属表面特征引导到例如平台地面。 两层可以粘合地支撑并顺序压入到位。
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10.发明申请公开(公告)号：US20130344314A1
公开(公告)日：2013-12-26
申请号：US13527795
申请日：2012-06-20
申请人： Shahnaz Shokri , Quynhgiao N. Le , Christopher Broadbent , Alexandra Elena Corona , Terrell Diane Riley
发明人： Shahnaz Shokri , Quynhgiao N. Le , Christopher Broadbent , Alexandra Elena Corona , Terrell Diane Riley
CPC分类号： H01B1/04 , B05D1/04 , B05D1/045 , B05D2201/02 , B05D2203/35 , B05D2601/20 , C23C30/00 , F01D5/288 , F05D2230/31 , F41H3/00 , Y02T50/671 , Y02T50/673 , Y10T428/24893 , Y10T428/249921
摘要： Methods include applying an electric charge to a coating material that includes carbon nanotubes and a carrier, such as paint, and depositing the electrically charged coating material to a substrate. In some methods, the applying includes utilizing an electrostatic sprayer. In some methods, the substrate is isolated from ground during the depositing. In some methods, the substrate is an insulator. Some methods result in regions of carbon nanotubes that are substantially longitudinally aligned after the depositing. Coated substrates may include a coating with carbon nanotubes that are substantially longitudinally aligned. Aircraft, spacecraft, land vehicles, marine vehicles, wind turbines, and apparatuses that may be susceptible to lightning strikes or other types of electromagnetic effects and that include a coated substrate also are disclosed.
摘要翻译： 方法包括将电荷施加到包括碳纳米管的涂层材料和诸如涂料的载体上，并将带电涂层材料沉积到基底上。 在一些方法中，应用包括利用静电喷雾器。 在一些方法中，在沉积期间将衬底与地离开。 在一些方法中，衬底是绝缘体。 一些方法导致在沉积之后基本纵向排列的碳纳米管区域。 涂覆的基底可以包括具有基本上纵向对准的碳纳米管的涂层。 还公开了可能易受雷击或其他类型的电磁效应的飞机，航天器，陆地车辆，船用车辆，风力涡轮机以及包括涂覆基板的设备。
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