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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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公开(公告)号：US20080146479A1
公开(公告)日：2008-06-19
申请号：US11610579
申请日：2006-12-14
IPC分类号： C11D10/02
CPC分类号： C11D3/2065 , C11D3/2003 , C11D3/2072 , C11D3/40 , C11D3/43 , C11D11/0041
摘要： The present invention includes a process using environmentally benign materials for the removal of adhesive residues from hard substrates, particularly vehicles, e.g., cars, trucks, buses, aerospace vehicles including airplanes, and the like. The invention uses an absorbable indicator (tracer) dye to aid in detection of remaining residues that may be in need of additional cleaning. The process uses a novel adhesive remover composition comprising a non-halogenated organic solvent, a non-abrasive thickening agent, a surfactant, glycerine, and an absorbable indicator dye. The invention provides a cost effective, safe, environmentally friendly adhesive remover composition specifically formulated for removal of, e.g., pressure sensitive adhesive residues from large areas of aircraft composite and aluminum surfaces, as well as others.
摘要翻译： 本发明包括使用环境友好材料从硬质基材，特别是汽车，例如汽车，卡车，公共汽车，包括飞机在内的航空航天车辆等中去除粘合剂残留物的方法。 本发明使用可吸收指示剂（示踪剂）染料来辅助检测可能需要额外清洁的剩余残留物。 该方法使用包含非卤化有机溶剂，非研磨性增稠剂，表面活性剂，甘油和可吸收的指示剂染料的新型粘合剂去除剂组合物。 本发明提供了一种具有成本效益，安全，环保的粘合剂去除剂组合物，其具体配制用于从飞机复合材料和铝表面的大面积以及其它物质中除去例如压敏粘合剂残余物。
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公开(公告)号：US07759298B2
公开(公告)日：2010-07-20
申请号：US11610579
申请日：2006-12-14
CPC分类号： C11D3/2065 , C11D3/2003 , C11D3/2072 , C11D3/40 , C11D3/43 , C11D11/0041
摘要： The present invention includes a process using environmentally benign materials for the removal of adhesive residues from hard substrates, particularly vehicles, e.g., cars, trucks, buses, aerospace vehicles including airplanes, and the like. The invention uses an absorbable indicator (tracer) dye to aid in detection of remaining residues that may be in need of additional cleaning. The process uses a novel adhesive remover composition comprising a non-halogenated organic solvent, a non-abrasive thickening agent, a surfactant, glycerine, and an absorbable indicator dye. The invention provides a cost effective, safe, environmentally friendly adhesive remover composition specifically formulated for removal of, e.g., pressure sensitive adhesive residues from large areas of aircraft composite and aluminum surfaces, as well as others.
摘要翻译： 本发明包括使用环境友好材料从硬质基材，特别是汽车，例如汽车，卡车，公共汽车，包括飞机在内的航空航天车辆等中去除粘合剂残留物的方法。 本发明使用可吸收指示剂（示踪剂）染料来辅助检测可能需要额外清洁的剩余残留物。 该方法使用包含非卤化有机溶剂，非研磨性增稠剂，表面活性剂，甘油和可吸收的指示剂染料的新型粘合剂去除剂组合物。 本发明提供了一种具有成本效益，安全，环保的粘合剂去除剂组合物，其具体配制用于从飞机复合材料和铝表面的大面积以及其它物质中除去例如压敏粘合剂残余物。
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公开(公告)号：US20080146480A1
公开(公告)日：2008-06-19
申请号：US11610622
申请日：2006-12-14
申请人： Ralph E. Dufresne , William M. Egan
发明人： Ralph E. Dufresne , William M. Egan
IPC分类号： C11D10/02
CPC分类号： C11D3/43 , C11D3/124 , C11D3/18 , C11D3/2003 , C11D3/2006 , C11D3/2024 , C11D3/2034 , C11D3/2044 , C11D3/2065 , C11D3/2068 , C11D3/2072 , C11D3/2079 , C11D3/2093 , C11D3/2096 , C11D3/222 , C11D3/26 , C11D3/28 , C11D3/30 , C11D3/3409
摘要： The present invention includes a process using environmentally friendly materials for the removal of adhesive residues from hard substrates, particularly vehicles, e.g., cars, trucks, buses, aerospace vehicles including airplanes, and the like. The process uses a novel adhesive remover composition comprising one or more non-halogenated organic solvents, a non-abrasive thickening agent, a surfactant, and a vapor-pressure modulating agent. The total Hansen Solubility Parameter (δt) at 25° C. for each of the non-halogenated organic solvents is from about 14 MPa1/2 to about 24 MPa1/2. The invention provides a cost effective, safe, environmentally friendly adhesive remover composition specifically formulated for removal of, e.g., pressure sensitive adhesive residues from large areas of aircraft composite and aluminum surfaces, as well as others.
摘要翻译： 本发明包括使用环境友好的材料从硬质基材，特别是汽车，例如汽车，卡车，公共汽车，包括飞机在内的航空航天车辆等去除粘合剂残留物的方法。 该方法使用包含一种或多种非卤化有机溶剂，非研磨性增稠剂，表面活性剂和蒸汽压力调节剂的新型粘合剂去除剂组合物。 对于每种非卤化有机溶剂，在25℃下的总Hansen溶解度参数（deltat）为约14MPa 1/2至约24MPa 1/2倍 >。 本发明提供了一种具有成本效益，安全，环保的粘合剂去除剂组合物，其具体配制用于从飞机复合材料和铝表面的大面积以及其它物质中除去例如压敏粘合剂残余物。
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公开(公告)号：US4662975A
公开(公告)日：1987-05-05
申请号：US827711
申请日：1986-02-10
CPC分类号： H05K3/002 , G01N17/00 , G01N27/205 , H05K1/0268 , H05K2203/0554 , H05K2203/163 , H05K3/0055
摘要： A probe that is used to determine the etch rate of a nonconductive material is comprised of a substrate of the material itself, plated on opposite sides with a conductive material. A first side of the probe has a small area of the plating removed to expose the substrate. The other side has an annular portion of the plating removed to define a wafer of plating isolated from the remainder of the plating. A lead wire is connected to the wafer and the entire second side of the probe is coated with an insulating mask. The probe is immersed in a bath of the etching solution. A voltage source is connected to the probe and to an electrode also immersed in the bath. A measurement device is connected in the circuit to detect current flow. When the etching bath dissolves the substrate through the exposed portion, a circuit is completed with the lead wire and the current flow is detected. The time from immersion of the probe to the beginning of current flow is used to calculate etch rate. Preferably the probe in constructed so that it remains in the bath in a passive state until actuated from a remote control circuit. In this manner, a plurality of probes can be placed in the bath and activated seriatim to conduct periodic etch rate measurements.
摘要翻译： 用于确定非导电材料的蚀刻速率的探针由材料本身的衬底组成，在导电材料的相对侧上镀覆。 探针的第一侧具有移除的电镀区域以露出衬底。 另一侧具有移除的镀层的环形部分，以限定与镀层的其余部分分离的镀覆晶片。 引线连接到晶片，并且探针的整个第二侧涂覆有绝缘掩模。 将探针浸入蚀刻溶液的浴中。 电压源连接到探针和也浸没在浴中的电极。 电路中连接有一个测量装置，以检测电流。 当蚀刻槽通过暴露部分溶解基板时，用引线完成电路并检测电流。 使用探针浸入电流开始的时间来计算蚀刻速率。 优选地，探针被构造成使得其保持在浴中处于被动状态，直到从遥控电路致动。 以这种方式，可以将多个探针放置在浴中并激活串联以进行周期性蚀刻速率测量。
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