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1. 发明申请

US20120312922A1 Boron Fiber Reinforced Structural Components 有权
标题翻译：硼纤维增强结构件
公开(公告)号：US20120312922A1
公开(公告)日：2012-12-13
申请号：US13157647
申请日：2011-06-10
申请人： Richard R. Rosman
发明人： Richard R. Rosman
IPC分类号： B64C1/06 , B32B5/26 , B23P11/00 , B64C1/12 , B29C65/42
CPC分类号： B64C1/26 , B32B5/12 , B32B5/26 , B32B2260/023 , B32B2260/046 , B32B2262/10 , B32B2313/02 , B32B2605/18 , B64C1/065 , B64C1/12 , B64C2001/0072 , Y02T50/43 , Y10T29/49826 , Y10T428/23
摘要： This disclosure is directed to a boron reinforced composite structural member. The concepts and technologies illustrated in this disclosure are taught within the context of a boron reinforced aircraft keel. A boron reinforced composite structural member may be constructed of a structural member core and a surrounding structural member casing. In one embodiment, the structural member core includes alternating layers of boron fiber reinforced plies and layers of interior carbon fiber reinforced plies. The boron fiber reinforced plies are oriented in a longitudinal direction, and the interior carbon fiber reinforced plies are oriented diagonally, perpendicular, and parallel to the boron fiber reinforced plies. The structural member casing includes layers of exterior carbon fiber reinforced plies that substantially surround the structural member core.
摘要翻译：本公开涉及硼增强复合结构构件。在本发明中说明的概念和技术在硼增强飞机龙骨的背景下被教导。硼增强复合结构构件可以由结构构件芯和周围结构构件壳体构成。在一个实施例中，结构构件芯包括硼纤维增强层和内部碳纤维增强帘布层的交替层。硼纤维增强帘布层在纵向方向上定向，并且内部碳纤维增强层对角线，垂直并平行于硼纤维增强层。结构构件壳体包括基本上围绕结构构件芯的外部碳纤维增强层的层。

2. 发明授权

US09170071B2 Mosaic extremity protection system with transportable solid elements 有权
标题翻译：具有可移动固体元素的马赛克末端保护系统
公开(公告)号：US09170071B2
公开(公告)日：2015-10-27
申请号：US12902285
申请日：2010-10-12
申请人： Charles A Howland
发明人： Charles A Howland
IPC分类号： F41H5/08 , F41H1/02 , F41H5/04 , B32B37/12
CPC分类号： F41H1/02 , B32B37/12 , B32B2307/542 , B32B2313/02 , B32B2323/04 , F41H5/0428 , F41H5/0435 , F41H5/0457 , F41H5/0471 , F41H5/0492 , Y10T156/1092 , Y10T156/1093
摘要： A flexible armor system adaptable to a garment suitable for extremity protection uses a planar array of polygon-shaped solid elements which detach upon projectile impact and combine their mass with the projectile for reduced velocity and increased impact area. The solid elements are bonded between an elastic strike-side spall cover and a high tensile strength flexible backer layer, and are further supported by a substantial fiber pack. In embodiments, the solid elements are ceramic, and are commutated but remain essentially intact after the projectile impact. Edge bars can cover junctures between solid elements, and center buttons can cover intersections between the junctures. Edge bars and center buttons can also be ceramic. The ceramic parts can include titanium backing layers. After formation, ceramic cores can be compressed upon cooling by an outer ceramic layer having a higher coefficient of thermal expansion, the outer layer being formed by glazing or doping.
摘要翻译：适用于适用于肢体保护的衣服的灵活装甲系统使用多边形固体元件的平面阵列，其在射弹冲击时分离，并将其质量与射弹组合以降低速度并增加冲击面积。固体元件结合在弹性冲击侧分离盖和高抗拉强度的柔性衬垫层之间，并且由实质的纤维包进一步支撑。在实施方案中，固体元素是陶瓷的，并且在弹丸冲击之后被换向但基本保持不变。边缘条可以覆盖实体元素之间的连接点，并且中心按钮可以覆盖交叉点之间的交叉点。边条和中心按钮也可以是陶瓷。陶瓷部件可以包括钛背衬层。形成后，可以通过具有较高热膨胀系数的外部陶瓷层冷却陶瓷芯，外层由玻璃或掺杂形成。

3. 发明申请

US20140366713A1 MOSAIC EXTREMITY PROTECTION SYSTEM WITH TRANSPORTABLE SOLID ELEMENTS 有权
标题翻译：具有可移动固体元件的MOSAIC极限保护系统
公开(公告)号：US20140366713A1
公开(公告)日：2014-12-18
申请号：US14472468
申请日：2014-08-29
申请人： Warwick Mills Inc.
发明人： Charles A. Howland
IPC分类号： F41H1/02 , B32B37/12 , F41H5/04
CPC分类号： F41H1/02 , B32B37/12 , B32B2307/542 , B32B2313/02 , B32B2323/04 , F41H5/0428 , F41H5/0435 , F41H5/0457 , F41H5/0471 , F41H5/0492 , Y10T156/1092 , Y10T156/1093
摘要： A method of protecting a user from a strike by a maximum threat includes adhesively bonding a plurality of solid elements to a support structure in a planar array, dimensions and material properties of the solid elements, support structure, and adhesive being selected to cause an impacted solid element to be dislodged by the maximum threat, and to combine its mass with the projectile for reduced velocity and increased impact area. The support structure is configured to fail in tensile and to allow the combined projectile and solid element to pass through the support structure. The solid elements can be ceramic, and can be commutated upon impact while remaining substantially intact. The solid elements can include titanium backing layers. After formation, ceramic cores can be compressed upon cooling by an outer ceramic layer having a higher coefficient of thermal expansion, the outer layer being formed by glazing or doping.
摘要翻译：保护用户免受最大威胁的冲击的方法包括将多个固体元件粘合到平面阵列中的支撑结构上，固体元件，支撑结构和粘合剂的尺寸和材料特性被选择以引起受影响的固体元素被最大威胁所抵消，并将其质量与弹丸相结合，以降低速度和增加冲击面积。支撑结构被配置成不能拉伸并允许组合的射弹和固体元件穿过支撑结构。固体元素可以是陶瓷，并且可以在冲击时进行换向，同时保持基本完整。固体元件可以包括钛背衬层。形成后，可以通过具有较高热膨胀系数的外部陶瓷层冷却陶瓷芯，外层由玻璃或掺杂形成。

4. 发明申请

US20110023697A1 MOSAIC EXTREMITY PROTECTION SYSTEM WITH TRANSPORTABLE SOLID ELEMENTS 有权
标题翻译：具有可移动固体元件的MOSAIC极限保护系统
公开(公告)号：US20110023697A1
公开(公告)日：2011-02-03
申请号：US12902285
申请日：2010-10-12
申请人： Charles A. Howland
发明人： Charles A. Howland
IPC分类号： F41H5/04 , F41H5/02
CPC分类号： F41H1/02 , B32B37/12 , B32B2307/542 , B32B2313/02 , B32B2323/04 , F41H5/0428 , F41H5/0435 , F41H5/0457 , F41H5/0471 , F41H5/0492 , Y10T156/1092 , Y10T156/1093
摘要： A flexible armor system adaptable to a garment suitable for extremity protection uses a planar array of polygon-shaped solid elements which detach upon projectile impact and combine their mass with the projectile for reduced velocity and increased impact area. The solid elements are bonded between an elastic strike-side spall cover and a high tensile strength flexible backer layer, and are further supported by a substantial fiber pack. In embodiments, the solid elements are ceramic, and are commutated but remain essentially intact after the projectile impact. Edge bars can cover junctures between solid elements, and center buttons can cover intersections between the junctures. Edge bars and center buttons can also be ceramic. The ceramic parts can include titanium backing layers. After formation, ceramic cores can be compressed upon cooling by an outer ceramic layer having a higher coefficient of thermal expansion, the outer layer being formed by glazing or doping.
摘要翻译：适用于适用于肢体保护的衣服的灵活装甲系统使用多边形固体元件的平面阵列，其在射弹冲击时分离，并将其质量与射弹组合以降低速度并增加冲击面积。固体元件结合在弹性冲击侧分离盖和高抗拉强度的柔性衬垫层之间，并且由实质的纤维包进一步支撑。在实施方案中，固体元素是陶瓷的，并且在弹丸冲击之后被换向但基本保持不变。边缘条可以覆盖实体元素之间的连接点，并且中心按钮可以覆盖交叉点之间的交叉点。边条和中心按钮也可以是陶瓷。陶瓷部件可以包括钛背衬层。形成后，可以通过具有较高热膨胀系数的外部陶瓷层冷却陶瓷芯，外层由玻璃或掺杂形成。

5. 发明授权

US09453710B2 Mosaic extremity protection system with transportable solid elements 有权
标题翻译：具有可移动固体元素的马赛克末端保护系统
公开(公告)号：US09453710B2
公开(公告)日：2016-09-27
申请号：US14472468
申请日：2014-08-29
申请人： Warwick Mills Inc.
发明人： Charles A. Howland
IPC分类号： F41H5/08 , F41H1/02 , F41H5/04 , B32B37/12
CPC分类号： F41H1/02 , B32B37/12 , B32B2307/542 , B32B2313/02 , B32B2323/04 , F41H5/0428 , F41H5/0435 , F41H5/0457 , F41H5/0471 , F41H5/0492 , Y10T156/1092 , Y10T156/1093
摘要： A method of protecting a user from a strike by a maximum threat includes adhesively bonding a plurality of solid elements to a support structure in a planar array, dimensions and material properties of the solid elements, support structure, and adhesive being selected to cause an impacted solid element to be dislodged by the maximum threat, and to combine its mass with the projectile for reduced velocity and increased impact area. The support structure is configured to fail in tensile and to allow the combined projectile and solid element to pass through the support structure. The solid elements can be ceramic, and can be commutated upon impact while remaining substantially intact. The solid elements can include titanium backing layers. After formation, ceramic cores can be compressed upon cooling by an outer ceramic layer having a higher coefficient of thermal expansion, the outer layer being formed by glazing or doping.
摘要翻译：保护用户免受最大威胁的冲击的方法包括将多个固体元件粘合到平面阵列中的支撑结构上，固体元件，支撑结构和粘合剂的尺寸和材料特性被选择以引起受影响的固体元素被最大威胁所抵消，并将其质量与弹丸相结合，以降低速度和增加冲击面积。支撑结构被配置成不能拉伸并允许组合的射弹和固体元件穿过支撑结构。固体元素可以是陶瓷，并且可以在冲击时进行换向，同时保持基本完整。固体元件可以包括钛背衬层。形成后，可以通过具有较高热膨胀系数的外部陶瓷层冷却陶瓷芯，外层由玻璃或掺杂形成。

6. 发明授权

US09180960B2 Boron fiber reinforced structural components 有权
标题翻译：硼纤维增强结构件
公开(公告)号：US09180960B2
公开(公告)日：2015-11-10
申请号：US13157647
申请日：2011-06-10
申请人： Richard R. Rosman
发明人： Richard R. Rosman
IPC分类号： B32B5/26 , B64C1/06 , B64C1/12 , B64C1/26 , B32B5/12 , B64C1/00
CPC分类号： B64C1/26 , B32B5/12 , B32B5/26 , B32B2260/023 , B32B2260/046 , B32B2262/10 , B32B2313/02 , B32B2605/18 , B64C1/065 , B64C1/12 , B64C2001/0072 , Y02T50/43 , Y10T29/49826 , Y10T428/23
摘要： This disclosure is directed to a boron reinforced composite structural member. The concepts and technologies illustrated in this disclosure are taught within the context of a boron reinforced aircraft keel. A boron reinforced composite structural member may be constructed of a structural member core and a surrounding structural member casing. In one embodiment, the structural member core includes alternating layers of boron fiber reinforced plies and layers of interior carbon fiber reinforced plies. The boron fiber reinforced plies are oriented in a longitudinal direction, and the interior carbon fiber reinforced plies are oriented diagonally, perpendicular, and parallel to the boron fiber reinforced plies. The structural member casing includes layers of exterior carbon fiber reinforced plies that substantially surround the structural member core.
摘要翻译：本公开涉及硼增强复合结构构件。在本发明中说明的概念和技术在硼增强飞机龙骨的背景下被教导。硼增强复合结构构件可以由结构构件芯和周围结构构件壳体构成。在一个实施例中，结构构件芯包括硼纤维增强层和内部碳纤维增强帘布层的交替层。硼纤维增强帘布层在纵向方向上定向，并且内部碳纤维增强层对角线，垂直并平行于硼纤维增强层。结构构件壳体包括基本上围绕结构构件芯的外部碳纤维增强层的层。

7. 发明申请

US20110001398A1 Carbon Nanotube Film Electrode and an Electroactive Device Fabricated with the Carbon Nanotube Film Electrode and a Method for Making Same 审中-公开
标题翻译：碳纳米管薄膜电极和用碳纳米管薄膜电极制造的电活性装置及其制造方法
公开(公告)号：US20110001398A1
公开(公告)日：2011-01-06
申请号：US11937155
申请日：2007-11-08
申请人： Jin Ho Kang , Cheol Park , Joycelyn S. Harrison
发明人： Jin Ho Kang , Cheol Park , Joycelyn S. Harrison
IPC分类号： H01L41/047 , B05D5/12 , B32B37/02
CPC分类号： B32B43/006 , B32B5/16 , B32B37/06 , B32B37/10 , B32B37/14 , B32B2250/02 , B32B2264/108 , B32B2309/12 , B32B2313/02 , B32B2313/04 , B32B2315/02 , B32B2457/00 , B82Y30/00 , C08K7/24 , H01B1/04 , H01L41/0478 , H01L41/29 , H01L41/45 , Y10S977/75 , Y10S977/751 , Y10S977/752 , Y10S977/762 , Y10T156/10 , Y10T428/249921
摘要： A single wall carbon nanotube (SWCNT) film electrode (FE), all-organic electroactive device systems fabricated with the SWNT-FE, and methods for making same. The SWCNT can be replaced by multi-wall carbon nanotubes or few wall carbon nanotubes. The SWCNT film can be obtained by filtering SWCNT solution onto the surface of an anodized alumina membrane. A freestanding flexible SWCNT film can be collected by breaking up this brittle membrane. The conductivity of this SWCNT film can advantageously be higher than 280 S/cm. The EAP actuator layered with the SWNT-FE shows a higher electric field-induced strain than an EAP layered with metal electrodes because the flexible SWNT-FE relieves the restraint of the displacement of the polymeric active layer as compared to the metal electrode. In addition, if thin enough, the SWNT-FE is transparent in the visible light range, thus making it suitable for use in actuators used in optical devices.
摘要翻译：单壁碳纳米管（SWCNT）膜电极（FE），用SWNT-FE制造的全有机电活性器件系统及其制造方法。 SWCNT可以由多壁碳纳米管或几个壁碳纳米管代替。可以通过将SWCNT溶液过滤到阳极化氧化铝膜的表面上来获得SWCNT膜。可以通过破碎这个脆性膜来收集独立的柔性SWCNT膜。该SWCNT膜的电导率可有利地高于280S / cm。与SWNT-FE分层的EAP致动器表现出比用金属电极分层的EAP更高的电场诱导应变，因为与金属电极相比，柔性SWNT-FE减轻了聚合物有源层的位移的限制。另外，如果足够薄，SWNT-FE在可见光范围内是透明的，因此使其适用于光学器件中使用的致动器。

8. 发明申请

US20190184673A1 Creating A True Thermally Conductive Apparel Using Intricate Thermally Functional Coating And Thermally Conductive Yarns 审中-公开
公开(公告)号：US20190184673A1
公开(公告)日：2019-06-20
申请号：US16220969
申请日：2018-12-14
申请人： VF Jeanswear LP
发明人： Dhruv Agarwal , Yongxin Wang , Josue Monge
IPC分类号： B32B5/10 , B32B5/02
CPC分类号： B32B5/10 , A41B1/08 , A41D1/06 , A41D13/005 , A41D31/04 , A41D31/12 , B32B5/022 , B32B5/024 , B32B5/026 , B32B2262/0269 , B32B2262/062 , B32B2262/106 , B32B2307/302 , B32B2313/02 , B32B2313/04 , B32B2317/10 , B32B2317/18 , B32B2437/00 , D06M23/08 , D06N3/0063
摘要： Provided are garments that comprise thermally-conductive materials, the materials comprising a heat-collecting coating disposed on a fibrous base material having a thermally-conductive additive dispersed within. Also provided are methods of fabricating thermally-conductive garments.

9. 发明授权

US09782953B2 Apparatus and a method for bonding and insulating Nd—Fe—B permanent magnets 有权
公开(公告)号：US09782953B2
公开(公告)日：2017-10-10
申请号：US14953843
申请日：2015-11-30
申请人： Yantai Shougang Magnetic Materials Inc.
发明人： Zhongjie Peng , Daoning Jia , Kunkun Yang
IPC分类号： B32B7/12 , H01F41/02 , B32B15/04 , B32B15/18 , B32B37/00 , B32B37/06 , B32B37/10 , B32B37/12 , B32B37/16 , B32B38/00 , B32B38/10 , B32B38/16 , H01F7/02 , H01F1/057
CPC分类号： B32B7/12 , B32B15/043 , B32B15/18 , B32B37/0053 , B32B37/06 , B32B37/10 , B32B37/12 , B32B37/1284 , B32B37/16 , B32B38/0036 , B32B38/10 , B32B38/162 , B32B2038/0076 , B32B2255/06 , B32B2255/26 , B32B2305/72 , B32B2307/208 , B32B2307/304 , B32B2309/025 , B32B2309/12 , B32B2311/00 , B32B2311/30 , B32B2313/02 , H01F1/0577 , H01F7/021 , H01F41/0253
摘要： A method for bonding a plurality of Nd—Fe—B permanent magnets includes a step of curing the layer of insulating adhesive at an initial temperature of between 20° C. and 250° C. and between 0.1 hr and 24 hr prior to the step of sandwiching. A predetermined clamping pressure of between 0.1 MPa and 10 MPa is then applied to the Nd—Fe—B permanent magnets. The stacked Nd—Fe—B permanent magnet is cured at a predetermined temperature of between 150° C. and 350° C. and between 0.1 hr and 12 hr. A clamping tool apparatus includes at least one of three intermediate guides disposed on the lower plate, in the chamber, spaced from the magnet positioning members, and extends to a proximal end defining a second predetermined distance with the second predetermined distance being less than the first predetermined distance of the magnet positioning members. The upper plate defines a plurality of apertures for receiving the magnet positioning members and the intermediate guides.

10. 发明授权

US09579867B2 Nanotube film electrode and an electroactive device fabricated with the nanotube film electrode and methods for making same 有权
标题翻译：纳米管膜电极和用纳米管膜电极制造的电活性器件及其制造方法
公开(公告)号：US09579867B2
公开(公告)日：2017-02-28
申请号：US13938622
申请日：2013-07-10
申请人： The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
发明人： Jin Ho Kang , Cheol Park , Joycelyn S. Harrison
IPC分类号： B32B5/16 , H01L41/047 , H01L41/29 , H01L41/45 , B32B37/14 , C08K7/24 , B82Y30/00
CPC分类号： B32B43/006 , B32B5/16 , B32B37/06 , B32B37/10 , B32B37/14 , B32B2250/02 , B32B2264/108 , B32B2309/12 , B32B2313/02 , B32B2313/04 , B32B2315/02 , B32B2457/00 , B82Y30/00 , C08K7/24 , H01B1/04 , H01L41/0478 , H01L41/29 , H01L41/45 , Y10S977/75 , Y10S977/751 , Y10S977/752 , Y10S977/762 , Y10T156/10 , Y10T428/249921
摘要： Disclosed is a single wall carbon nanotube (SWCNT) film electrode (FE), all-organic electroactive device systems fabricated with the SWNT-FE, and methods for making same. The SWCNT can be replaced by other types of nanotubes. The SWCNT film can be obtained by filtering SWCNT solution onto the surface of an anodized alumina membrane. A freestanding flexible SWCNT film can be collected by breaking up this brittle membrane. The conductivity of this SWCNT film can advantageously be higher than 280 S/cm. An electroactive polymer (EAP) actuator layered with the SWNT-FE shows a higher electric field-induced strain than an EAP layered with metal electrodes because the flexible SWNT-FE relieves the restraint of the displacement of the polymeric active layer as compared to the metal electrode. In addition, if thin enough, the SWNT-FE is transparent in the visible light range, thus making it suitable for use in actuators used in optical devices.
摘要翻译：公开了单壁碳纳米管（SWCNT）膜电极（FE），用SWNT-FE制造的全有机电活性器件系统及其制造方法。 SWCNT可以被其他类型的纳米管替代。可以通过将SWCNT溶液过滤到阳极化氧化铝膜的表面上来获得SWCNT膜。可以通过破碎这个脆性膜来收集独立的柔性SWCNT膜。该SWCNT膜的电导率可有利地高于280S / cm。与SWNT-FE分层的电活性聚合物（EAP）致动器显示出比用金属电极层叠的EAP更高的电场诱导应变，因为柔性SWNT-FE与金属相比减轻了聚合物有源层的位移的限制电极。另外，如果足够薄，SWNT-FE在可见光范围内是透明的，因此使其适用于光学器件中使用的致动器。

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