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1. 发明申请

US20090004480A1 COMPOSITES WITH INTEGRATED MULTI-FUNCTIONAL CIRCUITS 有权
标题翻译：具有集成多功能电路的复合材料
公开(公告)号：US20090004480A1
公开(公告)日：2009-01-01
申请号：US11770263
申请日：2007-06-28
申请人： Ralph E. Dufresne , Quynhgiao N. Le , David F. Feider
发明人： Ralph E. Dufresne , Quynhgiao N. Le , David F. Feider
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。

2. 发明授权

US07934676B2 Pre-fabricated article for EME protection of an aircraft 有权
标题翻译：用于飞机EME保护的预制品
公开(公告)号：US07934676B2
公开(公告)日：2011-05-03
申请号：US12056139
申请日：2008-03-26
申请人： Ralph E. Dufresne , David F. Feider , Quynhgiao N. Le
发明人： Ralph E. Dufresne , David F. Feider , Quynhgiao N. Le
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。

3. 发明授权

US07883050B2 Composites with integrated multi-functional circuits 有权
标题翻译：具有集成多功能电路的复合材料
公开(公告)号：US07883050B2
公开(公告)日：2011-02-08
申请号：US11770263
申请日：2007-06-28
申请人： Ralph E. Dufresne , Quynhgiao N. Le , David F. Feider
发明人： Ralph E. Dufresne , Quynhgiao N. Le , David F. Feider
IPC分类号： B64D45/02 , H05F3/00
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。

4. 发明授权

US07829796B2 Circuit joining assembly materials for multi-layer lightning protection systems on composite aircraft 有权
标题翻译：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
申请人： David F. Feider , Ralph E. Dufresne , Quynhgiao N. Le
发明人： David F. Feider , Ralph E. Dufresne , Quynhgiao N. Le
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。

5. 发明申请

US20090114427A1 CIRCUIT JOINING ASSEMBLY MATERIALS FOR MULTI-LAYER LIGHTNING PROTECTION SYSTEMS ON COMPOSITE AIRCRAFT 有权
标题翻译：复合飞机多层次雷击保护系统电路组合材料
公开(公告)号：US20090114427A1
公开(公告)日：2009-05-07
申请号：US11935993
申请日：2007-11-06
申请人： David F. Feider , Ralph E. Dufresne , Quynhgiao N. Le
发明人： David F. Feider , Ralph E. Dufresne , Quynhgiao N. Le
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。

6. 发明申请

US20090001217A1 PRE-FABRICATED ARTICLE FOR EME PROTECTION OF AN AIRCRAFT 有权
标题翻译：用于EME保护飞机的预制品
公开(公告)号：US20090001217A1
公开(公告)日：2009-01-01
申请号：US12056139
申请日：2008-03-26
申请人： Ralph E. Dufresne , David F. Feider , Quynhgiao N. Le
发明人： Ralph E. Dufresne , David F. Feider , Quynhgiao N. Le
IPC分类号： B64C1/00 , B32B3/10 , B32B37/06 , G03F7/20
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。

7. 发明申请

US20080146479A1 COMPOSITION AND METHOD FOR REMOVING ADHESIVE RESIDUE 有权
标题翻译：用于去除粘合残留物的组合物和方法
公开(公告)号：US20080146479A1
公开(公告)日：2008-06-19
申请号：US11610579
申请日：2006-12-14
申请人： Ralph E. Dufresne , James F. Kirchner , David F. Feider
发明人： Ralph E. Dufresne , James F. Kirchner , David F. Feider
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。

8. 发明授权

US07759298B2 Thickened composition and method for removing adhesive residue 有权
标题翻译：增稠组合物和去除粘合剂残留物的方法
公开(公告)号：US07759298B2
公开(公告)日：2010-07-20
申请号：US11610579
申请日：2006-12-14
申请人： Ralph E. Dufresne , James F. Kirchner , David F. Feider
发明人： Ralph E. Dufresne , James F. Kirchner , David F. Feider
IPC分类号： C11D3/40 , C11D3/44 , C11D1/83
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。

9. 发明授权

US4965433A Vacuum pickup tool with integrally heated soldering tip 失效
标题翻译：带整体加热焊接头的真空拾取工具
公开(公告)号：US4965433A
公开(公告)日：1990-10-23
申请号：US281985
申请日：1988-12-09
申请人： Kurt F. Hanke , Wesley C. Lund , David F. Feider
发明人： Kurt F. Hanke , Wesley C. Lund , David F. Feider
IPC分类号： B23K1/00 , B23K3/047 , H05K13/04
CPC分类号： H05K13/0408 , B23K1/0004 , B23K3/047 , B23K3/0478
摘要： A vacuum pickup tool (10) having a handle (16) and a barrel (22) mounted thereto with a tip (24) that is heated by a temperature control unit (114). The barrel (22) and tip (24) include a longitudinal axial bore (41) attached to an air source through connector (116) to provide vacuum through an axial opening (62) and the tip (24) to hold a Z-clip (74) to the barrel (22). Actuation of a trigger (28) deactivates the vacuum and simultaneously heats the tip (24) to solder the clip (74) onto a wire wrapped pin (64) inserted through a circuit board (66). A thermocouple (54) and controller 114 monitor and control the temperature of the tip (24) as preset by the temperature control (114) on an instrument assembly (96).
摘要翻译：具有手柄（16）和安装在其上的筒体（22）的真空拾取工具（10）具有由温度控制单元（114）加热的尖端（24）。枪管（22）和尖端（24）包括通过连接器（116）附接到空气源的纵向轴向孔（41），以通过轴向开口（62）和尖端（24）提供真空以保持Z形夹（74）连接到枪管（22）。触发器（28）的致动使真空去激活并且同时加热尖端（24）以将夹子（74）焊接到通过电路板（66）插入的缠绕线（64）上。热电偶（54）和控制器114监测和控制由仪器组件（96）上的温度控制（114）预设的尖端（24）的温度。

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