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公开(公告)号：US20210172710A1
公开(公告)日：2021-06-10
申请号：US16708012
申请日：2019-12-09
Applicant: The Boeing Company
Inventor： John N. Harris
Abstract: A ballistic panel is described including a core layer having a first major surface and a second major surface, the core layer including a ballistic gel. The first layer of ballistic resistant material is on the first major surface of the core layer. A second layer of ballistic resistant material is on the second major surface of the core layer.
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公开(公告)号：US09683362B2
公开(公告)日：2017-06-20
申请号：US13913641
申请日：2013-06-10
Applicant: The Boeing Company
Inventor： John N. Harris , Daniel B. Slaton
CPC classification number: E04B1/7662 , C08K7/08 , D21H13/46 , D21H17/20 , Y02T50/43 , Y10T428/237 , Y10T428/238 , Y10T428/24124 , Y10T442/20 , Y10T442/2631 , Y10T442/668 , Y10T442/696
Abstract: A composite structure includes a resin and a plurality of titanium dioxide fibers provided in the resin.
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公开(公告)号：US08689447B2
公开(公告)日：2014-04-08
申请号：US13663040
申请日：2012-10-29
Applicant: The Boeing Company
Inventor： John N. Harris
IPC: B21D53/88
CPC classification number: B64F5/0009 , B64C1/1484 , B64F5/10 , E04B1/942 , Y10T29/49622 , Y10T428/25 , Y10T428/256 , Y10T428/2913 , Y10T428/31507 , Y10T428/31511
Abstract: A fire retardant, transparent panel and method of making the panel, that is especially well suited for use on mobile platforms, and particularly on aircrafts. The panel is a composite of a transparent matrix and a plurality of fire-retardant nanoparticles. The nanoparticles have a diameter less than the visible spectrum of light, and in one form between about 0.1 nm to about 400 nm in diameter. The nanoparticles may be arranged randomly or in predetermined patterns within the matrix during manufacturing of the panel. The panel is lightweight, transparent and yet highly fire retardant.
Abstract translation: 阻燃，透明面板和制造面板的方法，特别适用于移动平台，特别是飞机上。 面板是透明基质和多种阻燃纳米粒子的复合物。 纳米颗粒的直径小于可见光光谱，直径在约0.1nm至约400nm之间。 在制造面板期间，纳米颗粒可以随机地或以矩阵内的预定图案布置。 该面板重量轻，透明，阻燃性好。
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公开(公告)号：US20130295809A1
公开(公告)日：2013-11-07
申请号：US13913641
申请日：2013-06-10
Applicant: The Boeing Company
Inventor： John N. Harris , Daniel B. Slaton
IPC: E04B1/76
CPC classification number: E04B1/7662 , C08K7/08 , D21H13/46 , D21H17/20 , Y02T50/43 , Y10T428/237 , Y10T428/238 , Y10T428/24124 , Y10T442/20 , Y10T442/2631 , Y10T442/668 , Y10T442/696
Abstract: A composite structure includes a resin and a plurality of titanium dioxide fibers provided in the resin.
Abstract translation: 复合结构包括设置在树脂中的树脂和多个二氧化钛纤维。
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5.发明公开公开(公告)号：US20230407121A1
公开(公告)日：2023-12-21
申请号：US18326355
申请日：2023-05-31
Applicant: THE BOEING COMPANY
Inventor： John N. Harris , Stephanie I. Metting
Abstract: Described herein are phosphor-containing ink compositions for disinfecting surfaces and improving the photostability of synthetic polymers. Methods for preparing the ink compositions are additionally described.
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Patent Agency Ranking
公开(公告)号：US20230405158A1
公开(公告)日：2023-12-21
申请号：US18326338
申请日：2023-05-31
Applicant: THE BOEING COMPANY
Inventor： John N. Harris
CPC classification number: A61L2/0076 , C09K11/77064 , C09K11/02
Abstract: Described herein are methods for disinfecting surfaces using a photon-emitting inorganic phosphor-doped substrate material. Methods for preparing the photon-emitting inorganic phosphor-doped substrate materials are additionally described.
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公开(公告)号：US20180140878A1
公开(公告)日：2018-05-24
申请号：US15860791
申请日：2018-01-03
Applicant: The Boeing Company
Inventor： Scott M. Livingston , Jack W. Mauldin , Robert P. Lotter , Paul B. Philipp , Khalid S. Alshobber , John N. Harris
CPC classification number: A62C3/08 , A62C2/06 , A62C99/009 , B64C1/10 , B64C1/16 , B64D27/00 , B64D45/00 , B64D2045/009 , F02K1/78 , F16J15/027 , F16J15/065 , F16L55/10 , F16L55/1026
Abstract: A fire seal end cap including a cap portion and a plug portion, wherein the plug portion protrudes from the cap portion, and wherein the cap portion and the plug portion are formed from a fire-resistant material.
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公开(公告)号：US09889323B2
公开(公告)日：2018-02-13
申请号：US13975797
申请日：2013-08-26
Applicant: The Boeing Company
Inventor： Scott M. Livingston , Jack W. Mauldin , Robert P. Lotter , Paul B. Philipp , Khalid S. Alshobber , John N. Harris
IPC: F16L55/10 , A62C3/08 , F16J15/16 , F02F11/00 , B64C1/10 , B64C1/16 , B64D27/00 , B64D45/00 , F16J15/02 , F16J15/06
CPC classification number: A62C3/08 , A62C2/06 , A62C99/009 , B64C1/10 , B64C1/16 , B64D27/00 , B64D45/00 , B64D2045/009 , F02K1/78 , F16J15/027 , F16J15/065 , F16L55/10 , F16L55/1026
Abstract: A multi-member assembly including a first structural member, a second structural member opposed from the first structural member, a crossover seal positioned between the first and second structural members, wherein the crossover seal defines a bore, and an end cap including a cap portion and a plug portion protruding from the cap portion, wherein the plug portion is at least partially received in the bore such that the cap portion bridges the first and second structural members.
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公开(公告)号：US20160359154A1
公开(公告)日：2016-12-08
申请号：US14616817
申请日：2015-02-09
Applicant: The Boeing Company
Inventor： John N. Harris , Daniel B. Slaton
IPC: H01M2/10 , H01M10/625 , H01M10/659 , H01M10/658 , H01M8/02 , H01G11/14 , H01M8/0662 , H01M2/02 , H01G11/78 , H01G11/08 , H01G11/18 , H01M10/0525 , H01M8/04007
CPC classification number: H01M2/1094 , H01G11/08 , H01G11/14 , H01G11/18 , H01G11/78 , H01G11/82 , H01M2/0262 , H01M2/0287 , H01M2/1072 , H01M8/02 , H01M8/04067 , H01M8/0662 , H01M8/2475 , H01M10/052 , H01M10/0525 , H01M10/48 , H01M10/625 , H01M10/658 , H01M10/659 , H01M2220/20 , H01M2250/20 , Y02E60/122 , Y02T90/32
Abstract: A containment system including a primary containment layer at least partially defining a primary containment volume, the primary containment layer including a thermal material, a secondary containment layer at least partially defining a secondary containment volume, the secondary containment layer including a gas capturing material, wherein the primary containment layer is positioned in the secondary containment volume, and a tertiary containment layer at least partially defining a tertiary containment volume, the tertiary containment layer including a ballistic material, wherein the secondary containment layer is positioned in the tertiary containment volume.
Abstract translation: 一种包含系统，包括至少部分地限定主要容纳体积的主容纳层，所述主容纳层包括热材料，至少部分限定二次容纳体积的次级容纳层，所述二级容纳层包括气体捕获材料，其中 主容纳层位于次级容纳体积中，并且三级容纳层至少部分地限定第三容纳体积，所述第三容纳层包括防弹材料，其中所述第二容纳层位于所述第三容纳体积中。
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公开(公告)号：US09500593B2
公开(公告)日：2016-11-22
申请号：US14217478
申请日：2014-03-18
Applicant: The Boeing Company
Inventor： John N. Harris , Finley Miller , Michael R. Swift
CPC classification number: G01N21/78 , G01M3/04 , G01M3/042 , G01N21/783 , G01N31/225
Abstract: A device indicates the location of an air leak in a vacuum bag used to process composite parts. The device includes a layer of material on the inner face of the bag that changes in appearance due to an oxidation-reduction reaction in areas of the layer exposed to oxygen caused by a leak in the bag.
Abstract translation: 设备表示用于处理复合部件的真空袋中的空气泄漏的位置。 该装置包括在袋的内表面上的一层材料，其由于在袋中泄漏而暴露于氧的层的区域中由于氧化还原反应而在外观上变化。
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