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公开(公告)号：US09552905B2
公开(公告)日：2017-01-24
申请号：US14408751
申请日：2013-06-07
Applicant: BAE Systems Plc
Inventor： Martyn John Hucker , David William Gough , Michael Dunleavy , Sajad Haq
CPC classification number: H01B9/006 , B32B5/26 , B32B2250/20 , B32B2260/046 , B32B2262/0253 , B32B2262/0261 , B32B2262/0269 , B32B2262/0276 , B32B2262/062 , B32B2262/101 , B32B2262/106 , B32B2307/202 , B32B2307/204 , B32B2307/206 , B32B2605/00 , B60R16/0207 , B60R16/023 , B60R16/03 , H01B9/003 , H01G11/22 , H01R43/24 , Y02E60/13 , Y02T10/7022 , Y10T29/49171
Abstract: According to the invention there is provided a Structural integrated wiring loom comprising at least one conductor comprising at least one first conductive fiber ply, wherein said at least one first conductive fiber ply comprises at least two electrical connectors, a separator structure comprising at least one first non-conductive fiber ply, and at least one second non-conductive fiber ply, said separator structure encapsulating said at least one conductor, a screen structure which encapsulates said separator structure, said screen structure comprising at least one second conductive fiber ply and at least one third conductive fiber ply, wherein said device is encapsulated a binder matrix. The device may be used to replace structural panels on a vehicle vessel or craft, to transfer electrical power or RF signals, data transmission around a composite structure.
Abstract translation: 根据本发明，提供了一种结构集成布线织机，其包括至少一个包括至少一个第一导电纤维层的导体，其中所述至少一个第一导电纤维层包括至少两个电连接器，分离器结构包括至少一个第一导电纤维层 非导电纤维层和至少一个第二非导电纤维层，所述隔离结构封装所述至少一个导体，屏蔽结构，其封装所述隔板结构，所述屏幕结构包括至少一个第二导电纤维帘布层和至少 第三导电纤维层，其中所述装置被包封粘合剂基质。 该装置可用于替代车辆船舶或船上的结构面板，以传递电力或RF信号，围绕复合结构的数据传输。
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公开(公告)号：US20140311328A1
公开(公告)日：2014-10-23
申请号：US14358783
申请日：2012-11-14
Applicant: BAE SYSTEMS plc
Inventor： Sajad Haq , Caroline Joleen Morley
CPC classification number: F41H5/02 , B64D7/00 , F41H1/02 , F41H5/0485 , F41H7/00 , F41H7/02 , Y10T442/2623
Abstract: According to the invention there is provided a fibrous armour material for dissipating the kinetic energy of a moving object which is impregnated with a shear thickening fluid, in which the shear thickening fluid includes particles of a thickening agent suspended in a liquid, and the volume fraction of the thickening agent in the shear thickening fluid is selected so that the shear thickening fluid has a viscosity-shear stress characteristic substantially corresponding to curve B or lying between curve B and curve D as shown in FIG. 2.
Abstract translation: 根据本发明，提供了一种用于消散被剪切增稠流体浸渍的运动物体的动能的纤维装甲材料，其中剪切增稠流体包括悬浮在液体中的增稠剂的颗粒，体积分数 选择剪切增稠流体中的增稠剂，使得剪切增稠流体具有基本上对应于曲线B或位于曲线B和曲线D之间的粘度剪切应力特性，如图1所示。 2。
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公开(公告)号：US09855681B2
公开(公告)日：2018-01-02
申请号：US14760632
申请日：2014-01-13
Applicant: BAE SYSTEMS plc
Inventor： Sajad Haq , Michael Dunleavy , Hazel Anne Dyke , Amy Elizabeth Dyke
IPC: B29B15/10 , B29B15/12 , D06M11/49 , C08J5/10 , C08K3/22 , B29B11/16 , C03C25/10 , C03C25/46 , C09D1/00 , C03C25/42 , B29K309/08 , B29K505/08
CPC classification number: B29B15/122 , B29B11/16 , B29K2309/08 , B29K2505/08 , B29K2995/0008 , C03C25/42 , C03C25/46 , C03C25/47 , C08J5/10 , C08K3/22 , C08K2003/2265 , C09D1/00 , D06M11/49
Abstract: Ferrite compositions, particularly ferrite coated substrates and more particularly fiber plys coated with ferrites in fiber reinforced polymer composites (FRPC), and composites with a plurality of functionalized fiber layers, include a magnetic ferrite composition for coating a substrate, said composition comprising a resin, and dispersed therein ferrite particulates, wherein said ferrite particulates have an average longest dimension of less than 500 nm. The composition may be used to provide a ferrite composite structure comprising at least one fiber ply, with at least one layer of a magnetic ferrite composition deposed thereon, wherein said ply is substantially encapsulated in a binder matrix to form a fiber reinforced polymer composite.
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公开(公告)号：US09816788B2
公开(公告)日：2017-11-14
申请号：US14358783
申请日：2012-11-14
Applicant: BAE SYSTEMS plc
Inventor： Sajad Haq , Caroline Joleen Morley
CPC classification number: F41H5/02 , B64D7/00 , F41H1/02 , F41H5/0485 , F41H7/00 , F41H7/02 , Y10T442/2623
Abstract: According to the invention there is provided a fibrous armor material for dissipating the kinetic energy of a moving object which is impregnated with a shear thickening fluid, in which the shear thickening fluid includes particles of a thickening agent suspended in a liquid, and the volume fraction of the thickening agent in the shear thickening fluid is selected so that the shear thickening fluid has a viscosity-shear stress characteristic substantially corresponding to curve B or lying between curve B and curve D as shown in FIG. 2.
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公开(公告)号：US09238332B2
公开(公告)日：2016-01-19
申请号：US14358779
申请日：2012-11-06
Applicant: BAE SYSTEMS plc
Inventor： Michael Dunleavy , Sajad Haq , Caroline Joleen Morley
CPC classification number: B29C70/021 , B64D7/00 , F41H1/02 , F41H5/0478 , F41H5/0485 , F41H7/00
Abstract: According to the invention there is provided an arrangement of protective material for dissipating the kinetic energy of a moving object including one or more layers of fibrous armour material encased within a sealed encasement, in which the sealed encasement is formed from a textile armour material which is impregnated with a polymeric substance.
Abstract translation: 根据本发明，提供了一种用于消散运动物体的动能的保护材料的布置，包括一个或多个包裹在密封包装内的纤维装甲材料层，其中密封的包装由纺织品装甲材料形成， 用聚合物浸渍。
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Patent Agency Ranking
公开(公告)号：US20150162140A1
公开(公告)日：2015-06-11
申请号：US14418995
申请日：2013-07-31
Applicant: BAE SYSTEMS PLC
Inventor： Martyn John Hucker , Michael Dunleavy , Sajad Haq
CPC classification number: H01G11/52 , B32B37/24 , B32B2457/16 , H01G11/36 , H01G11/38 , H01G11/40 , H01G11/58 , H01G13/04 , Y02B10/30 , Y02E60/13 , Y02T10/7022 , Y10T29/417 , Y10T156/10
Abstract: According to the invention there is provided a component including a supercapacitor and a method of producing same. The component comprises a first (12) and second (14) electrode and a separator structure (16) which separates the two electrodes and contains a liquid or gel electrolyte. The first and second electrode structures are each formed from a composite material (10) which includes electrically conductive fibres and electrochemically active material in a binder matrix and the supercapacitor is formed to be structurally inseparable from the rest of the component. Further, the component forms a structural capacitor. The obtained structural capacitor could be used in aircraft structure to save weight.
Abstract translation: 根据本发明，提供了包括超级电容器的组件及其制造方法。 该组件包括第一电极（12）和第二电极（14）以及隔离两个电极并包含液体或凝胶电解质的分离器结构（16）。 第一和第二电极结构各自由复合材料（10）形成，复合材料（10）在粘合剂基质中包括导电纤维和电化学活性材料，并且超级电容器形成为在结构上与组分的其余部分不可分离。 此外，该部件形成结构电容器。 获得的结构电容器可用于飞机结构，以减轻重量。
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公开(公告)号：US20150162114A1
公开(公告)日：2015-06-11
申请号：US14408751
申请日：2013-06-07
Applicant: BAE Systems Plc
Inventor： Martyn John Hucker , David William Gough , Michael Dunleavy , Sajad Haq
IPC: H01B9/00 , B60R16/03 , B60R16/023 , H01R43/24 , B60R16/02
CPC classification number: H01B9/006 , B32B5/26 , B32B2250/20 , B32B2260/046 , B32B2262/0253 , B32B2262/0261 , B32B2262/0269 , B32B2262/0276 , B32B2262/062 , B32B2262/101 , B32B2262/106 , B32B2307/202 , B32B2307/204 , B32B2307/206 , B32B2605/00 , B60R16/0207 , B60R16/023 , B60R16/03 , H01B9/003 , H01G11/22 , H01R43/24 , Y02E60/13 , Y02T10/7022 , Y10T29/49171
Abstract: According to the invention there is provided a Structural integrated wiring loom comprising at least one conductor comprising at least one first conductive fibre ply, wherein said at least one first conductive fibre ply comprises at least two electrical connectors, a separator structure comprising at least one first non-conductive fibre ply, and at least one second non-conductive fibre ply, said separator structure encapsulating said at least one conductor, a screen structure which encapsulates said separator structure, said screen structure comprising at least one second conductive fibre ply and at least one third conductive fibre ply, wherein said device is encapsulated a binder matrix. The device may be used to replace structural panels on a vehicle vessel or craft, to transfer electrical power or RF signals, data transmission around a composite structure.
Abstract translation: 根据本发明，提供了一种结构集成布线织机，其包括至少一个包括至少一个第一导电纤维层的导体，其中所述至少一个第一导电纤维层包括至少两个电连接器，分离器结构包括至少一个第一导电纤维层 非导电纤维层和至少一个第二非导电纤维层，所述隔离结构封装所述至少一个导体，屏蔽结构，其封装所述隔板结构，所述屏幕结构包括至少一个第二导电纤维帘布层和至少 第三导电纤维层，其中所述装置被包封粘合剂基质。 该装置可用于替代车辆船舶或船上的结构面板，以传递电力或RF信号，围绕复合结构的数据传输。
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公开(公告)号：US10570659B2
公开(公告)日：2020-02-25
申请号：US15314652
申请日：2015-02-02
Applicant: BAE Systems plc
Inventor： Sajad Haq , Hazel Anne Dyke , Michael Dunleavy , Harry John Finn
IPC: E06B5/18 , G02B5/20 , H01Q1/52 , H01Q15/00 , H01Q17/00 , H05K9/00 , H01Q5/22 , B32B17/10 , G21F7/03
Abstract: An electro-optic window is provided, together with a method of manufacturing the window. The window (3) is made of a material substantially transparent to at least one of infra-red, visible and UV radiation and treated to have reduced RF/MICROWAVE transmission characteristics by the provision of a grid (1) set into at least one surface (2) thereof. The grid (1) is formed of a material selected to be either reflective or absorptive to RF/MICROWAVE radiation.
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公开(公告)号：US09831045B2
公开(公告)日：2017-11-28
申请号：US14418995
申请日：2013-07-31
Applicant: BAE SYSTEMS PLC
Inventor： Martyn John Hucker , Michael Dunleavy , Sajad Haq
CPC classification number: H01G11/52 , B32B37/24 , B32B2457/16 , H01G11/36 , H01G11/38 , H01G11/40 , H01G11/58 , H01G13/04 , Y02B10/30 , Y02E60/13 , Y02T10/7022 , Y10T29/417 , Y10T156/10
Abstract: According to the invention there is provided a component including a supercapacitor and a method of producing same. The component comprises a first (12) and second (14) electrode and a separator structure (16) which separates the two electrodes and contains a liquid or gel electrolyte. The first and second electrode structures are each formed from a composite material (10) which includes electrically conductive fibers and electrochemically active material in a binder matrix and the supercapacitor is formed to be structurally inseparable from the rest of the component. Further, the component forms a structural capacitor. The obtained structural capacitor could be used in aircraft structure to save weight.
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公开(公告)号：US09819032B2
公开(公告)日：2017-11-14
申请号：US14772249
申请日：2014-02-26
Applicant: BAE SYSTEMS PLC
Inventor： Martyn John Hucker , Sajad Haq , Michael Dunleavy
IPC: H01M6/32 , H01M2/16 , H01M2/18 , H01M4/12 , H01M4/24 , H01M4/34 , H01M4/36 , H01G11/04 , H01G11/18 , H01G11/56 , H01G11/62 , H01G11/78
CPC classification number: H01M6/32 , H01G11/04 , H01G11/18 , H01G11/56 , H01G11/62 , H01G11/78 , H01M2/1613 , H01M2/1666 , H01M2/18 , H01M4/12 , H01M4/244 , H01M4/34 , H01M4/364 , H01M2220/20 , Y02E60/13
Abstract: This invention relates to the formation of standby structural composite electrical energy storage devices, and a method of producing same. The device may be a standby battery or supercapacitor with first and second electrodes which are separated by a separator structure, wherein the device contains an electrolyte retained in a reservoir. The use of at least one valve allows the addition, removal of electrolyte fluids, and venting of any outgassing by products.
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