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公开(公告)号：US20170327950A1
公开(公告)日：2017-11-16
申请号：US15151203
申请日：2016-05-10
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld , De'Andre James Cherry
IPC: C23C16/46 , C23C16/455
CPC classification number: C23C16/46 , C23C16/448 , C23C16/455 , C23C16/48
Abstract: A method for chemical vapor deposition on a substrate is disclosed. The method may include directing a process gas into a reaction chamber, and heating the process gas in the reaction chamber. Heating the process gas in the reaction chamber may decompose the process gas to thereby generate a plurality of decomposition products. The method may also include applying one or more biasing fields and/or waves to the process gas upstream of the substrate, and reacting the process gas with the substrate. The one or more biasing fields and/or waves may include electromagnetic waves, electric fields, and/or magnetic fields. The biasing fields and/or waves may urge at least a portion of the process gas towards or away from the substrate.
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公开(公告)号：US20170232641A1
公开(公告)日：2017-08-17
申请号：US15043358
申请日：2016-02-12
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld , Arthur August Rugtvedt , Jeffrey Lynn Duce
Abstract: Systems and methods are provided for enhancement of vacuum bagging processes for a composite part. One system includes dispensers configured to dispense materials onto a forming tool for a composite part, and a controller. The controller is able to identify a selected location for placing the composite part on the tool, to direct the dispensers to apply a mold release agent onto the tool based on the selected location, to apply a sealant onto the tool proximate to the selected location, to lay up a ply of constituent material for the composite part atop the mold release agent at the selected location, to apply a pressure pad material atop the constituent material, to apply a breather material atop the pressure pad, and to apply vacuum bag material atop the ply proximate to the selected location to cover the ply as well as the sealant.
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公开(公告)号：US20170037200A1
公开(公告)日：2017-02-09
申请号：US15297363
申请日：2016-10-19
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld
CPC classification number: C08J5/042 , C08J5/005 , C08J5/24 , C08J2363/00 , C08J2379/04 , C08J2379/08 , C08K9/04
Abstract: Composite materials are augmented with functionalized graphene having added amine groups, benzoxazine groups, imide groups, or a combination of amine groups and imide groups on a surface of the graphene, epoxide groups formed on at least one edge of the graphene and/or holes formed through the graphene. The functionalized graphene is integrated into a composite material as a supplement to or as a replacement for either the carbon reinforcement material or the resin matrix material to increase strength of the composite materials, and may be in the form of a functionalized graphene nanoplatelet, a flat graphene sheet or film, or a rolled or twisted graphene sheet or film.
Abstract translation: 在石墨烯的表面上添加有胺基，苯并嗪基，酰亚胺基或胺基和酰亚胺基的组合的官能化石墨烯增强了复合材料，形成在石墨烯的至少一个边缘上的环氧基和/或形成的孔 通过石墨烯。 功能化石墨烯被整合成复合材料，作为碳增强材料或树脂基质材料的补充或替代，以增加复合材料的强度，并且可以是官能化的石墨烯纳米血小板，扁平 石墨烯片或薄膜，或卷状或扭曲的石墨烯片或薄膜。
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公开(公告)号：US20170024854A1
公开(公告)日：2017-01-26
申请号：US14540408
申请日：2014-11-13
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld
CPC classification number: G06T3/4053 , B64C39/022 , B64C2201/123 , B64C2201/148 , B64D3/00 , B64D47/08 , G06T2207/10012 , G06T2207/10044 , G06T2207/30212 , G06T2207/30232
Abstract: A deployable airborne sensor array system and method of use are provided herein. The system includes a tether configured to be coupled to and deployed from an aircraft and a plurality of airborne vehicles coupled to the tether. Each of the plurality of airborne vehicles includes different lift characteristics to form a three-dimensional (3D) array of airborne vehicles. Each airborne vehicle includes a sensing device configured to generate sensor data associated with a target. The system also include a computing device configured to process the sensor data received from each of said plurality of airborne vehicles and generate an image of the target based on the sensor data.
Abstract translation: 本文提供了可部署的机载传感器阵列系统和使用方法。 该系统包括被配置为联接到飞行器并且从飞行器部署并且耦合到系绳的多个机载车辆的系绳。 多个机载车辆中的每一个都包括不同的升力特性以形成空中车辆的三维（3D）阵列。 每个机载车辆包括被配置为产生与目标相关联的传感器数据的感测装置。 该系统还包括被配置为处理从所述多个机载车辆中的每一个接收的传感器数据并基于传感器数据生成目标的图像的计算装置。
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65.发明授权Growth of carbon nanotube (CNT) leads on circuits in substrate-free continuous chemical vapor deposition (CVD) process 有权碳纳米管（CNT）的生长导致基板无连续化学气相沉积（CVD）工艺中的电路公开(公告)号：US09544998B1
公开(公告)日：2017-01-10
申请号：US14853004
申请日：2015-09-14
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld
IPC: H01L33/62 , H05K1/09 , H05K3/46 , H01L25/075
CPC classification number: H01L33/62 , H01L25/0753 , H01L51/0048 , H01L2221/1094 , H05K1/09 , H05K1/097 , H05K3/1275 , H05K2201/026 , H05K2201/0323
Abstract: A method and structure for an electrical device and a plurality of electrical circuits including a plurality of carbon nanotubes (CNTs). The method can include forming a first CNT catalyst layer including a plurality of first CNT catalyst plugs, a plurality of electrical circuits electrically coupled to the first CNT catalyst layer, and a second CNT catalyst layer including a plurality of second CNT catalyst plugs electrically coupled to the second CNT catalyst layer. CNTs may be simultaneously formed on the plurality of first and second CNT catalyst plugs within a chemical vapor deposition (CVD) furnace.
Abstract translation: 一种电气装置和包括多个碳纳米管（CNT）的多个电路的方法和结构。 该方法可以包括形成第一CNT催化剂层，其包括多个第一CNT催化剂塞，电耦合到第一CNT催化剂层的多个电路，以及包括多个第二CNT催化剂塞的第二CNT催化剂层，该第二CNT催化剂层电耦合到 第二CNT催化剂层。 可以在化学气相沉积（CVD）炉内的多个第一和第二CNT催化剂塞上同时形成CNT。
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Patent Agency Ranking
公开(公告)号：US09434826B2
公开(公告)日：2016-09-06
申请号：US14589057
申请日：2015-01-05
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld
CPC classification number: C08J5/06 , C01B32/194 , C08J5/042 , C08J5/24 , C08J2300/00 , C08K7/06 , D01F9/12 , D02G3/38 , D10B2101/12 , D10B2505/02
Abstract: Composite materials with graphene-augmented carbon reinforcement fibers having a graphene film wrapped about one or more carbon fiber filaments. The graphene film is wrapped about the carbon fiber filaments in a spiral orientation and has amine groups formed on an outer surface of the graphene film and epoxide groups formed on at least one edge of the graphene film. The amine groups are formed in a functionalized area on the outer surface of the graphene film that is within about 10 microns from the at least one edge of the graphene film. The graphene film may also have holes formed through the graphene film. The graphene film may be wrapped around a single carbon fiber filament, a substantially cylindrical bundle of about 19 carbon fiber filaments, or a substantially rectangular bed of carbon fiber filaments formed from a plurality of carbon fiber tows.
Abstract translation: 具有石墨烯增强碳增强纤维的复合材料，其具有缠绕在一个或多个碳纤维长丝上的石墨烯膜。 石墨烯膜以螺旋取向缠绕在碳纤维长丝上，并且在石墨烯膜的外表面上形成有胺基，在石墨烯膜的至少一个边缘上形成环氧基。 在石墨烯膜的外表面上的功能化区域中形成胺基，其距离石墨烯膜的至少一个边缘在约10微米内。 石墨烯膜也可以具有通过石墨烯膜形成的孔。 石墨烯膜可以缠绕在单个碳纤维长丝上，大致圆柱形的约19个碳纤维长丝的束或由多个碳纤维丝束形成的大致矩形的碳纤维长丝床。
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公开(公告)号：US20160194463A1
公开(公告)日：2016-07-07
申请号：US14589057
申请日：2015-01-05
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld
CPC classification number: C08J5/06 , C01B32/194 , C08J5/042 , C08J5/24 , C08J2300/00 , C08K7/06 , D01F9/12 , D02G3/38 , D10B2101/12 , D10B2505/02
Abstract: Composite materials with graphene-augmented carbon reinforcement fibers having a graphene film wrapped about one or more carbon fiber filaments. The graphene film is wrapped about the carbon fiber filaments in a spiral orientation and has amine groups formed on an outer surface of the graphene film and epoxide groups formed on at least one edge of the graphene film. The amine groups are formed in a functionalized area on the outer surface of the graphene film that is within about 10 microns from the at least one edge of the graphene film. The graphene film may also have holes formed through the graphene film. The graphene film may be wrapped around a single carbon fiber filament, a substantially cylindrical bundle of about 19 carbon fiber filaments, or a substantially rectangular bed of carbon fiber filaments formed from a plurality of carbon fiber tows.
Abstract translation: 具有石墨烯增强碳增强纤维的复合材料，其具有缠绕在一个或多个碳纤维长丝上的石墨烯膜。 石墨烯膜以螺旋取向缠绕在碳纤维长丝上，并且在石墨烯膜的外表面上形成有胺基，在石墨烯膜的至少一个边缘上形成环氧基。 在石墨烯膜的外表面上的功能化区域中形成胺基，其距离石墨烯膜的至少一个边缘在约10微米内。 石墨烯膜也可以具有通过石墨烯膜形成的孔。 石墨烯膜可以缠绕在单个碳纤维长丝上，大致圆柱形的约19个碳纤维长丝的束或由多个碳纤维丝束形成的大致矩形的碳纤维长丝床。
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68.发明申请COMPOSITE MATERIALS WITH IMPROVED ELECTRICAL CONDUCTIVITY AND METHODS OF MANUFACTURE THEREOF 审中-公开具有改善电导率的复合材料及其制造方法公开(公告)号：US20160055930A1
公开(公告)日：2016-02-25
申请号：US14468227
申请日：2014-08-25
Applicant: THE BOEING COMPANY
Inventor： Keith Daniel Humfeld
CPC classification number: H01B1/22 , B29C70/14 , B29C70/62 , B29C70/882 , B29D99/001 , B29L2031/3076 , B32B3/12 , B32B5/024 , B32B5/26 , B32B2260/021 , B32B2262/101 , B32B2262/106 , B32B2264/105 , B32B2307/202 , B32B2307/208 , B32B2309/025 , B32B2419/00 , B32B2605/00 , B64D45/02
Abstract: A method of manufacturing a composite material may include providing one or more layers of reinforcement material penetrated with viscous matrix material that is doped with electrically conductive particles. The method may further include applying a magnetic field to arrange the particles into one or more electrically conductive pathways, and curing the matrix material to secure the pathways in position relative to the reinforcement material.
Abstract translation: 制造复合材料的方法可以包括提供一个或多个穿透了掺有导电颗粒的粘性基质材料的增强材料层。 该方法可以进一步包括施加磁场以将颗粒排列成一个或多个导电路径，以及固化基质材料以将通道固定在相对于增强材料的适当位置。
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公开(公告)号：US20150343483A1
公开(公告)日：2015-12-03
申请号：US14293092
申请日：2014-06-02
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld , Mark Stewart Wilenski
CPC classification number: B05C3/02 , B05D1/18 , B05D1/28 , B82Y30/00 , C01B32/168 , C01B2202/08
Abstract: A system for use in producing a nanotube mesh structure is provided. The system includes a first nanotube collection apparatus including a first substrate configured to collect a plurality of nanotubes substantially aligned in a first orientation on an attachment surface thereof, and a second nanotube collection apparatus including a second substrate configured to collect a plurality of nanotubes substantially aligned in a second orientation on an attachment surface thereof. The first and second nanotube collection apparatuses are configured to combine the pluralities of nanotubes at an interface. The system also includes a first energy source configured to direct energy towards the interface between the pluralities of nanotubes, wherein the energy is configured to join the pluralities of nanotubes to form the nanotube mesh structure.
Abstract translation: 提供了一种用于制造纳米管网状结构的系统。 该系统包括第一纳米管收集装置，该第一纳米管采集装置包括：第一基板，被配置为收集在其附接表面上以第一取向基本上对准的多个纳米管;以及第二纳米管收集装置，其包括第二基板，其被配置为收集多个基本上对准 在其附接表面上的第二取向。 第一和第二纳米管收集装置被配置为在界面处组合多个纳米管。 该系统还包括被配置为将能量引导到多个纳米管之间的界面的第一能量源，其中能量被配置为连接多个纳米管以形成纳米管网状结构。
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公开(公告)号：US11578432B2
公开(公告)日：2023-02-14
申请号：US16663055
申请日：2019-10-24
Applicant: The Boeing Company
Inventor： Keith Daniel Humfeld , Gwen Marie Lanphere Gross
Abstract: Systems and methods are provided for fabrication of enhanced carbon fiber laminates that utilize encapsulated catalyst. One embodiment is a method that includes acquiring a batch of dry fibers, and acquiring a batch of catalyst capsules that each comprise catalyst that accelerates polymerization of monomers of a resin, and a shell that encapsulates the catalyst and liquefies at a curing temperature. The method further includes interspersing the catalyst capsules among the dry fibers, and impregnating the fibers with the resin after interspersing the catalyst capsules with the fibers.
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