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公开(公告)号:US20190194943A1
公开(公告)日:2019-06-27
申请号:US16311430
申请日:2018-04-23
申请人: Rigidcore Group LLC
发明人: Robert J. Bingham
摘要: A one-piece component comprising a tetrahedral-octahedral honeycomb lattice is disclosed herein, along with a mold, a system and methods of making the component. A one-piece component comprising a truncated tetrahedral-octahedral honeycomb lattice also is disclosed, along with corresponding molds, systems and methods.
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公开(公告)号:US20170254087A1
公开(公告)日:2017-09-07
申请号:US15602571
申请日:2017-05-23
申请人: PN II, Inc.
IPC分类号: E04D11/00 , E04D13/17 , E04C2/38 , E04D1/28 , E04C2/36 , E04D3/32 , E04D3/35 , E04B7/22 , E04D1/36
CPC分类号: E04D11/005 , E04B7/22 , E04C2/365 , E04C2/384 , E04C2/386 , E04C2/388 , E04D1/28 , E04D1/36 , E04D3/32 , E04D3/351 , E04D3/357 , E04D13/17 , Y10T428/236 , Y10T428/239 , Y10T428/24149 , Y10T428/24157 , Y10T428/24165 , Y10T428/24777 , Y10T428/31504 , Y10T442/3423 , Y10T442/3854 , Y10T442/3943
摘要: A self supporting panel system used to fabricate ceilings, floors, walls, or roofs. The panel system is assembled from a plurality of panels, each having a core that is sandwiched between opposing plate members. In a preferred embodiment, the core of each panel includes a unifying material to enhance the load bearing capacity of the panel.
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公开(公告)号:US09688050B2
公开(公告)日:2017-06-27
申请号:US13292686
申请日:2011-11-09
申请人: David Carlson , Brandon Madaus , Matthew Harthcock , Kearney Barton , Charles L. Taylor , Jason Walker
发明人: David Carlson , Brandon Madaus , Matthew Harthcock , Kearney Barton , Charles L. Taylor , Jason Walker
IPC分类号: B32B37/02 , B32B37/26 , B32B37/06 , B32B3/12 , B29C44/12 , B29C44/18 , B32B5/18 , B32B5/20 , B32B7/02 , E04C2/36 , B29L31/00
CPC分类号: B32B3/12 , B29C44/1228 , B29C44/186 , B29K2995/0002 , B29L2031/776 , B32B5/18 , B32B5/20 , B32B7/02 , B32B2250/40 , B32B2262/0261 , B32B2262/101 , B32B2262/106 , B32B2307/102 , B32B2307/304 , B32B2307/732 , B32B2419/00 , B32B2439/00 , B32B2479/00 , B32B2509/00 , B32B2605/00 , E04C2/365 , Y10T428/24157
摘要: A panel structure and a method of forming the panel structure are disclosed. The panel structure typically includes at least one panel associated with a material. The panel structure has been found particularly advantageous for use as an interior panel of an airplane.
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公开(公告)号:US09586363B2
公开(公告)日:2017-03-07
申请号:US14505892
申请日:2014-10-03
申请人: Zephyros, Inc.
发明人: Patrick Siboni , John Blancaneaux
IPC分类号: A41H37/00 , A44B19/00 , B29C65/00 , B32B37/00 , C09J163/00 , B32B3/12 , B29C65/48 , C09J5/06 , E04C2/36 , F16B5/01 , B32B7/00 , B32B7/02 , B32B7/12 , B32B27/38 , F16B37/04 , B29C65/54 , B32B37/14 , B29K63/00 , F16B11/00
CPC分类号: B29C65/4815 , B29C65/542 , B29C66/474 , B29C66/72525 , B29K2063/00 , B32B3/12 , B32B7/00 , B32B7/02 , B32B7/12 , B32B27/38 , B32B37/146 , B32B2250/40 , B32B2605/00 , B32B2605/18 , C09J5/06 , C09J2463/00 , E04C2/365 , F16B5/01 , F16B11/006 , F16B37/048
摘要: The present invention contemplates a method for the attachment of a component to a honeycomb structure comprising forming a cavity in the honeycomb structure whereby the cavity is formed within one or more honeycomb cells; placing an insert adapted to enable the attachment of the component to the honeycomb structure whereby a reformable epoxy resin adhesive is injected about the insert or an expandable reformable epoxy resin adhesive is overmolded onto the insert; heating the reformable epoxy resin adhesive; and hardening and adhering the reformable epoxy resin adhesive to one or more interior walls of the cavity upon cooling.
摘要翻译: 本发明涉及一种用于将部件附接到蜂窝结构体的方法,包括在蜂窝结构体中形成空腔,由此在一个或多个蜂窝单元内形成空腔; 放置适于使部件附着到蜂窝状结构上的插入件,由此将可重整的环氧树脂粘合剂注入到插入件周围,或者可膨胀的可重整环氧树脂粘合剂被包覆模制到插入物上; 加热可重整环氧树脂粘合剂; 并且在冷却时将可重整环氧树脂粘合剂硬化并粘附到腔的一个或多个内壁。
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公开(公告)号:US09421731B2
公开(公告)日:2016-08-23
申请号:US14379188
申请日:2013-02-19
发明人: Akira Furutani , You Gotou
IPC分类号: B32B3/00 , B32B3/12 , E04C2/32 , B32B7/04 , B32B7/12 , B32B37/24 , E04C2/36 , B32B7/14 , B32B15/04 , B32B15/08 , B32B3/30 , E04C2/34 , B32B37/12 , B32B37/00 , B32B37/14
CPC分类号: B32B3/12 , B32B3/30 , B32B7/045 , B32B7/12 , B32B7/14 , B32B15/043 , B32B15/08 , B32B37/0076 , B32B37/12 , B32B37/1292 , B32B37/144 , B32B37/24 , B32B2250/02 , B32B2250/03 , B32B2305/08 , B32B2307/718 , B32B2307/734 , B32B2311/00 , B32B2315/08 , B32B2398/00 , B32B2419/00 , B32B2457/12 , B32B2457/20 , B32B2551/08 , B32B2605/00 , E04C2/324 , E04C2/365 , E04C2002/3422 , Y10T428/24149
摘要: A panel structure includes a plate-like flat panel and a reinforcement panel in which a criterion plate portion and a plurality of truncated conic protrusions protruding from the criterion plate portion are formed. Apex portions of the plurality of truncated conic protrusions in the reinforcement panel are joined to the flat panel by an adhesive.
摘要翻译: 面板结构包括板状平板和加强板,其中形成有标准板部分和从标准板部分突出的多个截头圆锥突起。 加强板中的多个截头圆锥突起的尖端部分通过粘合剂接合到平板。
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6.
公开(公告)号:US20160160501A1
公开(公告)日:2016-06-09
申请号:US14955773
申请日:2015-12-01
申请人: Jeffrey M. Taraba , Emil M. Taraba
发明人: Jeffrey M. Taraba , Emil M. Taraba
CPC分类号: E04B5/48 , E04B5/12 , E04C2/34 , E04C2/3405 , E04C2/365 , E04C2/50 , E04C2/521 , E04C2/523 , E04C2/525 , E04F15/02038 , E04F15/102 , E04F15/107 , F24D3/142 , F24D2220/006 , Y02B30/24
摘要: A structural flooring panel comprises an upper sheet, a lower sheet and a plurality of longitudinally extending ribs between the sheets. The ribs are laterally spaced to define at least one longitudinally extending, internal channel within the panel.
摘要翻译: 结构地板面板包括上片,下片和在片之间的多个纵向延伸的肋。 肋横向间隔开以限定面板内的至少一个纵向延伸的内部通道。
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公开(公告)号:US09205616B2
公开(公告)日:2015-12-08
申请号:US14052256
申请日:2013-10-11
申请人: The Boeing Company
CPC分类号: B29C53/04 , B23C3/34 , B26D3/06 , B26D3/065 , B26D5/20 , B29C53/063 , B29C70/02 , B29C2793/0009 , B29D99/001 , B29K2105/06 , B29K2105/256 , B29L2009/00 , B29L2031/3076 , B29L2031/608 , B32B3/02 , B32B3/12 , B32B3/28 , B32B3/30 , B32B5/26 , B32B2260/023 , B32B2260/046 , B32B2262/101 , B32B2305/024 , B32B2605/18 , E04C2/00 , E04C2/24 , E04C2/365 , Y02T50/43 , Y10T29/49801 , Y10T156/1026 , Y10T156/1044 , Y10T409/30 , Y10T428/24479 , Y10T428/24612
摘要: A method and apparatus for forming a bend in composite panel. A method for forming a bend in a composite panel comprises forming a slot having a curved flange in the composite panel, inserting a sheet into the curved flange, and bending the composite panel with the slot and the sheet within the curved flange about a longitudinal axis of the slot to form the bend.
摘要翻译: 一种用于在复合板中形成弯曲的方法和装置。 一种用于在复合板中形成弯曲的方法包括在复合板中形成具有弯曲凸缘的槽,将板插入弯曲凸缘中,并将复合板与槽和弯曲凸缘中的板弯曲成纵向轴线 的槽形成弯曲。
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8.
公开(公告)号:US09114591B2
公开(公告)日:2015-08-25
申请号:US13724257
申请日:2012-12-21
发明人: Randy B. Williams
IPC分类号: B32B3/12 , B29C70/86 , B29C70/88 , B32B3/28 , B32B5/26 , B32B15/02 , B32B15/14 , B64D43/00 , E04C2/36
CPC分类号: B32B3/12 , B29C70/865 , B29C70/885 , B32B3/28 , B32B5/26 , B32B15/02 , B32B15/14 , B32B2250/40 , B64D43/00 , E04C2/365 , Y02T50/43 , Y10T29/49826 , Y10T156/10 , Y10T428/1234 , Y10T428/24149 , Y10T428/24157 , Y10T428/24165 , Y10T428/24661
摘要: A honeycomb core includes a first wall secured to a second wall and a conductor disposed therebetween. A honeycomb cell is formed between the first wall and the second wall and the conductor is configured to extend through the cell and a point where the first wall and the second wall are secured together.
摘要翻译: 蜂窝芯包括固定到第二壁的第一壁和布置在其间的导体。 蜂窝单元形成在第一壁和第二壁之间,并且导体被构造成延伸通过电池和第一壁和第二壁固定在一起的点。
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公开(公告)号:US09021705B2
公开(公告)日:2015-05-05
申请号:US12679080
申请日:2008-09-17
申请人: Valter Naldi
发明人: Valter Naldi
CPC分类号: E04C2/365 , B32B3/22 , B32B21/042 , B32B2307/50 , B32B2479/00 , E04C2/296 , Y10T29/49629 , Y10T29/49787 , Y10T156/10 , Y10T156/1052 , Y10T156/1062 , Y10T156/1082 , Y10T428/13 , Y10T428/24612 , Y10T428/24752
摘要: A fully or partly edged panel (10; 200) of wood or wood fiber. The panel (10; 200) includes a sandwich blank (10*; 200*) having outer layers (11) of solid consistency, and at least one supple inner layer (12) with a lightweight, possibly “honeycomb” or supple foam material, structure. The panel (10; 200) is characterized by having at least one spacer (13; 213) inserted between the two outer layers (11) of the blank (10*; 200*) at at least one corner thereof. The peripheral outer faces (15) of the blank (10*; 200*) may be edged with an adhesive edging strip (16). Also described are methods (100; 1000) for manufacturing the panel (10; 200).
摘要翻译: 完全或部分边缘的木材或木纤维板(10; 200)。 面板(10; 200)包括具有固体稠度的外层(11)的三明治坯料(10 *; 200 *)和至少一个柔软的内层(12),其具有轻质的,可能的“蜂窝状”或柔软泡沫材料 , 结构体。 面板(10; 200)的特征在于在其至少一个角部处具有插入坯料(10 *; 200 *)的两个外层(11)之间的至少一个间隔件(13; 213)。 坯料(10 *; 200 *)的周边外表面(15)可以用粘合剂边缘条(16)边缘。 还描述了用于制造面板(10; 200)的方法(100; 1000)。
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公开(公告)号:US20150030806A1
公开(公告)日:2015-01-29
申请号:US14338733
申请日:2014-07-23
发明人: Axel FINK
CPC分类号: B32B3/12 , B29D99/0014 , B32B3/30 , B32B5/028 , B32B15/046 , B32B15/14 , B32B2250/03 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/102 , B32B2307/542 , B32B2605/18 , E04C2/365 , G10K11/168 , Y10T428/24149
摘要: A sandwich type load bearing panel (1) with a transversely shear stiff core (3) and a plurality of individual unidirectional plies respectively for a first and a second composite layer (2, 4), bonded each to one of the main surfaces of the core (3). The first composite layer (2) is a continuous and monolithic assembly and the second layer (4) is an open net of intercrossing strips (4a, 4b, 4c) running along at least three directions and being laid up of said plurality of individual unidirectional plies.
摘要翻译: 一种具有横向剪切刚性芯(3)和分别用于第一和第二复合层(2,4)的多个单个单向层的夹层型承载面板(1),每个层叠结合到所述第一和第二复合层的主表面之一 核心(3)。 第一复合层(2)是连续且整体的组件,第二层(4)是沿着至少三个方向延伸并且由所述多个单独的单向排列的交叉条(4a,4b,4c)的开放网 层
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