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公开(公告)号:US20190186520A1
公开(公告)日:2019-06-20
申请号:US16306381
申请日:2017-05-31
申请人: RUAG SCHWEIZ AG
CPC分类号: F16B13/141 , F16B5/01 , F16B13/144
摘要: The invention is directed to an insert system comprising an insert with a base and an outer skirt extending from the base, thereby forming a chamber. The outer skirt is provided with a first inner skirt surface and a first outer skirt surface. The insert system further comprises a panel with a core structure and a first cover sheet that at least partially covers the core structure. The first cover sheet defines a first outer panel surface and has an opening. At least one piston is arranged in the opening and beneath the first outer panel surface. According to the invention the piston during mounting of the insert sweeps into the chamber to discharge an adhesive agent from the chamber into the core structure via at least one pathway.
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公开(公告)号:US20190171191A1
公开(公告)日:2019-06-06
申请号:US16272828
申请日:2019-02-11
申请人: THE BOEING COMPANY
发明人: Aaron Coon , Chris G. McInelly , Bret Hoeksema , Ryan Lillibridge , Tom Allen , Steve Solack , Kevin Bowe , Gary K. Allen
CPC分类号: G05B19/41805 , B23P19/001 , B23P19/04 , B29C65/483 , B29C65/542 , B29C65/564 , B29C65/7802 , B29C66/30321 , B29C66/30325 , B29C66/474 , B29C66/72525 , B29C66/863 , B29L2031/3076 , B32B3/06 , B32B3/266 , B32B7/08 , B32B2305/024 , B32B2607/00 , F16B5/01 , G05B2219/40111
摘要: An automated fastener insert installation system for composite panels is provided. A first module receives and secures a composite panel with respect to an origin of a first coordinate system, wherein the composite panel has opposed major surfaces and defines an insert-receiving orifice extending through one of the major surfaces, and is secured such that one of the major surfaces is externally accessible. A second module engages each of a plurality of fastener inserts with an installation aide. Third module determines a configuration of the orifice defined by the composite panel, selects a corresponding one of the fastener inserts engaged with the installation aide, inserts the selected fastener insert into the orifice, and dispenses an adhesive material through the installation aide and into the orifice about selected fastener insert such that the adhesive material secures the selected fastener insert within the orifice. Associated systems are also provided.
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公开(公告)号:US10018209B2
公开(公告)日:2018-07-10
申请号:US14676552
申请日:2015-04-01
申请人: B/E Aerospace, Inc.
CPC分类号: F16B5/02 , F16B5/01 , F16B11/006 , F16B33/00 , F16B37/048 , Y10T29/49622 , Y10T29/4981 , Y10T29/49948
摘要: In an illustrative embodiment, an insert apparatus for creating an attachment point in an aircraft panel includes a flange insert configured for bonding against an inner surface of a skin of the aircraft panel such that a portion of a load from a component mounted to the attachment point is distributed through the skin. The flange insert may include a wide flange, a bore, and a central opening through the wide flange and the bore, and a nut including an enlarged end and a shaft, where the nut is disposed in the central opening of the flange such that the enlarged end is proximate the wide flange and the shaft extends along the bore. Upon bonding to the aircraft panel, the bore may extend from an underside of the wide flange to proximate an outer surface of the skin of the aircraft panel.
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公开(公告)号:US10016955B2
公开(公告)日:2018-07-10
申请号:US15132697
申请日:2016-04-19
申请人: The Boeing Company
发明人: Christopher Mills
CPC分类号: B32B7/08 , B32B3/06 , B32B3/12 , B32B5/18 , B32B5/245 , B32B5/26 , B32B27/065 , B32B27/08 , B32B27/12 , B32B27/28 , B32B27/42 , B32B2250/03 , B32B2250/40 , B32B2260/023 , B32B2260/046 , B32B2262/106 , B32B2266/0221 , B32B2266/0257 , B32B2266/0285 , B32B2307/50 , B32B2307/546 , B32B2307/718 , B32B2307/72 , B32B2605/18 , B64C1/12 , B64C1/1407 , B64C1/18 , F16B5/01
摘要: A panel apparatus is described that includes a first sandwich panel and a second sandwich panel arranged substantially parallel to each other, and the first sandwich panel and the second sandwich panel each include a core material inserted between at least two skin layers. The panel apparatus also includes at least one mechanical fastener mechanically embedded into the first sandwich panel and the second sandwich panel. The at least one mechanical fastener at least extends through one skin layer and into the core material of the first sandwich panel and at least extends through one skin layer and into the core material of the second sandwich panel, and the at least one mechanical fastener is configured to accept insertion of an item. Methods of assembling the panel apparatus are also described.
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公开(公告)号:US09976583B2
公开(公告)日:2018-05-22
申请号:US15090146
申请日:2016-04-04
申请人: The Boeing Company
发明人: Karina R. Lopez , Hayden S. Osborn
CPC分类号: F16B5/01 , B32B7/08 , B32B2250/40 , B32B2605/18 , F16B5/02
摘要: A threaded adjustable-height insert may be installed in a bore of a sandwich panel, such that the insert may be configured to transfer a load to the sandwich panel. The threaded adjustable-height insert may include a first insert part and a second insert part that may be selectively operatively positioned with respect to each other. The overall height of the threaded adjustable-height insert may be adjusted by longitudinally sliding the second insert part with respect to the first insert part and rotating the second insert part with respect to the first insert part. Presently disclosed threaded adjustable-height inserts may be configured for flush installation in a sandwich panel. Methods of installing such threaded adjustable-height inserts and adjusting the height of the same are also disclosed.
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公开(公告)号:US20180003211A1
公开(公告)日:2018-01-04
申请号:US15634370
申请日:2017-06-27
申请人: SFS intec Holding AG
发明人: Sascha Costabel
CPC分类号: F16B37/122 , F16B5/01 , F16B5/125 , F16B37/043 , F16B37/044 , F16B37/12
摘要: A lightweight fastener includes a threaded body with at least one torque support, a housing, which receives the threaded body at least in part, and a counter support for at least one torque support. In accordance with the invention a wire nut or threaded wire nut is used as thread body. A lightweight fastener of this type is used in clips or inserts, i.e. fastening elements that are used in particular in the interior design of vehicles and aircraft.
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公开(公告)号:US09810251B2
公开(公告)日:2017-11-07
申请号:US14635508
申请日:2015-03-02
申请人: THE BOEING COMPANY
CPC分类号: F16B5/0614 , B64D11/00 , B64D11/003 , B64D11/02 , B64D11/04 , F16B5/01 , F16B5/0635 , F16B21/075 , Y10T24/44 , Y10T24/44026
摘要: A panel system includes a tab panel having at least one tab extending therefrom. The tab panel has a core and a facesheet adjacent the core. The panel system includes a slot panel having at least one slot receiving the corresponding tab of the tab panel therein. The slot panel has a core and a facesheet adjacent the core. The slot is formed in the facesheet and at least a portion of the core. The panel system includes a clip positioned between the tab panel and the slot panel. The clip is at least partially received in the slot. The clip has a tab panel securing member being secured to the tab panel and the clip has a slot panel securing member being secured to the slot panel. The clip securely joins the tab panel to the slot panel.
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公开(公告)号:US20170297301A1
公开(公告)日:2017-10-19
申请号:US15132697
申请日:2016-04-19
申请人: The Boeing Company
发明人: Christopher Mills
摘要: A panel apparatus is described that includes a first sandwich panel and a second sandwich panel arranged substantially parallel to each other, and the first sandwich panel and the second sandwich panel each include a core material inserted between at least two skin layers. The panel apparatus also includes at least one mechanical fastener mechanically embedded into the first sandwich panel and the second sandwich panel. The at least one mechanical fastener at least extends through one skin layer and into the core material of the first sandwich panel and at least extends through one skin layer and into the core material of the second sandwich panel, and the at least one mechanical fastener is configured to accept insertion of an item. Methods of assembling the panel apparatus are also described.
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公开(公告)号:US20170253006A1
公开(公告)日:2017-09-07
申请号:US15062927
申请日:2016-03-07
申请人: The Boeing Company
发明人: Karina Lopez , Lee James Keetle
CPC分类号: B32B3/266 , B32B3/12 , B32B2250/03 , B32B2605/08 , B32B2605/18 , B62D33/08 , B64C1/12 , B64D11/00 , F16B5/01
摘要: A two-part adjustable-height insert may be installed in a bore of a sandwich panel, such that the adjustable-height insert may be configured to transfer a load to the sandwich panel. The adjustable-height insert may include a first insert part and a second insert part that may be selectively operatively positioned with respect to each other. The adjustable-height insert may be configured such that an interference fit between the first insert part and the second insert part may be engaged by moving a second flange of the second insert part towards a first flange of the first insert part, which may thereby reduce the overall height of the adjustable-height insert to a selected height. Presently disclosed adjustable-height inserts may be configured for flush installation in a sandwich panel. Methods of installing such adjustable-height inserts and adjusting the height of the same are also disclosed.
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公开(公告)号:US09732778B2
公开(公告)日:2017-08-15
申请号:US14825044
申请日:2015-08-12
发明人: Samuel Dale Frias
CPC分类号: F16B5/0208 , F16B1/00 , F16B3/005 , F16B5/01 , F16B11/006 , F16B2001/0035 , Y10S428/90 , Y10T24/32 , Y10T403/56
摘要: A panel insert comprising an external body having an open end, said body having a central bore, a magnet received in said bore and having a smooth surface facing said open end of the body, said magnet being affixed to said body.
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