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公开(公告)号：US08458979B2
公开(公告)日：2013-06-11
申请号：US12407023
申请日：2009-03-19
申请人： James E. Ebner , Greg A. Tubbs
发明人： James E. Ebner , Greg A. Tubbs
CPC分类号： F16B21/09 , B64C1/066 , B64C1/403 , F16B2/06 , F16B5/123 , Y10T24/44026 , Y10T24/45105 , Y10T24/45812 , Y10T24/45995
摘要： An attachment system for coupling together two airplane sections includes an attachment section securing one of the airplane sections and a mount section affixed to the other section. The attachment section includes a top, a bottom, a first end, and a second end. Coupled to the top are two clamp sections, whereby at least one of the clamp sections is moveable. Coupled to the bottom is a pair of buttons. The mount section includes a top and a bottom, such that the mount bottom couples to the second airplane section. The mount section further includes a track coupled to the mount top, wherein the track includes an open end having outwardly tapered edges and a closed end. The one of the buttons slides into the track for coupling the attachment section to the mount section.
摘要翻译： 用于将两个飞机部分联接在一起的附接系统包括固定飞机部分中的一个和附接到另一部分的安装部分的附接部分。 附接部分包括顶部，底部，第一端和第二端。 连接到顶部的是两个夹紧部分，由此夹紧部分中的至少一个可移动。 结合底部是一对按钮。 安装部分包括顶部和底部，使得安装底部联接到第二飞行器部分。 安装部分还包括耦合到安装顶部的轨道，其中轨道包括具有向外渐缩的边缘和闭合端的开口端。 其中一个按钮滑入轨道，用于将连接部分连接到安装部分。
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公开(公告)号：US20120241559A1
公开(公告)日：2012-09-27
申请号：US13071823
申请日：2011-03-25
CPC分类号： B64C1/14 , B21D53/92 , B64C1/1492 , Y10T29/49826 , Y10T29/49876
摘要： An aircraft window has an inner window assembly retained on an outer window assembly by a plurality of interlocking clips and receptacles positioned around the perimeter of the window. The interlocking clips and receptacles produce a retention force that compresses a seal against an outer structural the window to seal an internal cavity between the inner and outer window assemblies.
摘要翻译： 飞机窗具有通过多个互锁夹和保持在外窗组件上的内窗组件，所述多个互锁夹和定位在窗的周边周围。 联锁夹和容器产生保持力，该保持力将窗口的外部结构压缩密封，以密封内窗组件和外窗组件之间的内腔。
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3.发明授权Method and apparatus for attaching electrically powered seat track cover to through hole seat track design 有权用于将电动座椅轨道盖连接到通孔座轨道设计的方法和装置公开(公告)号：US08033501B2
公开(公告)日：2011-10-11
申请号：US11150578
申请日：2005-06-10
IPC分类号： B64D11/06
CPC分类号： H02G3/00 , B64C1/20 , H01R13/62933 , H02G11/00
摘要： A system for communicating electrical signals between two spaced apart seat assemblies on a mobile platform, for example an aircraft. The seat assemblies are secured to seat tracks mounted on a floor of the aircraft cabin. The seat tracks have a plurality of spaced apart holes that enable seat assembly mounting. A seat track cover is snap-fit onto one or more seat track mount devices. Each of the seat track mount devices includes one or more cleats or knobs that can be snap fit into the openings in the seat track to quickly and easily secure the seat track cover to the seat track. The seat track cover and mount devices enable a simple, planar seat track having spaced apart holes to be employed, rather than a C-shaped seat mounting track.
摘要翻译： 用于在移动平台（例如飞行器）上的两个间隔开的座椅组件之间传递电信号的系统。 座椅组件被固定到安装在飞机机舱地板上的座椅轨道上。 座椅轨道具有能够使座椅组件安装的多个间隔开的孔。 座椅导轨盖卡扣配合到一个或多个座椅轨道安装装置上。 座椅轨道安装装置中的每一个包括一个或多个夹板或旋钮，其可以卡扣配合到座椅轨道中的开口中，以快速且容易地将座椅轨道盖固定到座椅轨道。 座椅导轨盖和安装装置使得能够使用具有间隔开的孔的简单的平面座椅轨道，而不是C形座椅安装轨道。
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公开(公告)号：US08944381B2
公开(公告)日：2015-02-03
申请号：US13071823
申请日：2011-03-25
IPC分类号： B64C1/14
CPC分类号： B64C1/14 , B21D53/92 , B64C1/1492 , Y10T29/49826 , Y10T29/49876
摘要： An aircraft window has an inner window assembly retained on an outer window assembly by a plurality of interlocking clips and receptacles positioned around the perimeter of the window. The interlocking clips and receptacles produce a retention force that compresses a seal against an outer structural the window to seal an internal cavity between the inner and outer window assemblies.
摘要翻译： 飞机窗具有通过多个互锁夹和保持在外窗组件上的内窗组件，所述多个互锁夹和定位在窗的周边周围。 联锁夹和容器产生保持力，该保持力将窗口的外部结构压缩密封，以密封内窗组件和外窗组件之间的内腔。
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公开(公告)号：US20090283640A1
公开(公告)日：2009-11-19
申请号：US12120948
申请日：2008-05-15
申请人： James E. Ebner
发明人： James E. Ebner
CPC分类号： F16B33/006 , F16B37/041 , Y10T403/7092
摘要： An attachment system includes a dual sleeve nut comprising at least two spaced-apart nut housings; at least two interiorly-threaded fastener openings extending through the nut housings, respectively; and a nut base connecting the nut housings. At least two threaded fasteners extend through the fastener openings, respectively, of the nut housings. A method of attaching a bracket to a composite structure is also disclosed.
摘要翻译： 附接系统包括双套筒螺母，其包括至少两个间隔开的螺母壳体; 分别延伸穿过螺母壳体的至少两个内螺纹紧固件开口; 以及连接螺母外壳的螺母基座。 至少两个螺纹紧固件分别延伸穿过螺母壳体的紧固件开口。 还公开了一种将托架附接到复合结构的方法。
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公开(公告)号：US20090179111A1
公开(公告)日：2009-07-16
申请号：US12407023
申请日：2009-03-19
申请人： James E. Ebner , Greg A. Tubbs
发明人： James E. Ebner , Greg A. Tubbs
IPC分类号： B64C1/00
CPC分类号： F16B21/09 , B64C1/066 , B64C1/403 , F16B2/06 , F16B5/123 , Y10T24/44026 , Y10T24/45105 , Y10T24/45812 , Y10T24/45995
摘要： An attachment system for coupling together two airplane sections includes an attachment section securing one of the airplane sections and a mount section affixed to the other section. The attachment section includes a top, a bottom, a first end, and a second end. Coupled to the top are two clamp sections, whereby at least one of the clamp sections is moveable. Coupled to the bottom is a pair of buttons. The mount section includes a top and a bottom, such that the mount bottom couples to the second airplane section. The mount section further includes a track coupled to the mount top, wherein the track includes an open end having outwardly tapered edges and a closed end. The one of the buttons slides into the track for coupling the attachment section to the mount section.
摘要翻译： 用于将两个飞机部分联接在一起的附接系统包括固定飞机部分中的一个和附接到另一部分的安装部分的附接部分。 附接部分包括顶部，底部，第一端和第二端。 连接到顶部的是两个夹紧部分，由此夹紧部分中的至少一个可移动。 结合底部是一对按钮。 安装部分包括顶部和底部，使得安装底部联接到第二飞行器部分。 安装部分还包括耦合到安装顶部的轨道，其中轨道包括具有向外渐缩的边缘和闭合端的开口端。 其中一个按钮滑入轨道，用于将连接部分连接到安装部分。
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公开(公告)号：US07527223B2
公开(公告)日：2009-05-05
申请号：US11400398
申请日：2006-04-06
申请人： James E. Ebner , Greg A. Tubbs
发明人： James E. Ebner , Greg A. Tubbs
IPC分类号： B64C1/06
CPC分类号： F16B21/09 , B64C1/066 , B64C1/403 , F16B2/06 , F16B5/123 , Y10T24/44026 , Y10T24/45105 , Y10T24/45812 , Y10T24/45995
摘要： An attachment system for coupling together two airplane sections includes an attachment section securing one of the airplane sections and a mount section affixed to the other section. The attachment section includes a top, a bottom, a first end, and a second end. Coupled to the top are a two clamp sections, whereby at least one of the clamp sections is moveable. Coupled to the bottom is a pair of buttons. The mount section includes a top and a bottom, such that the mount bottom couples to the second airplane section. The mount section further includes a track coupled to the mount top, wherein the track includes an open end having outwardly tapered edges and a closed end. The one of the buttons slides into the track for coupling the attachment section to the mount section.
摘要翻译： 用于将两个飞机部分联接在一起的附接系统包括固定飞机部分中的一个和附接到另一部分的安装部分的附接部分。 附接部分包括顶部，底部，第一端和第二端。 耦合到顶部的是两个夹紧部分，其中至少一个夹持部分是可移动的。 结合底部是一对按钮。 安装部分包括顶部和底部，使得安装底部联接到第二飞行器部分。 安装部分还包括耦合到安装顶部的轨道，其中轨道包括具有向外渐缩的边缘和闭合端的开口端。 其中一个按钮滑入轨道，用于将连接部分连接到安装部分。
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公开(公告)号：US07448822B2
公开(公告)日：2008-11-11
申请号：US11376682
申请日：2006-03-15
IPC分类号： F16B21/06
CPC分类号： F16B5/07 , B60R13/0206 , B60R13/0237 , Y10T24/45089 , Y10T24/45099 , Y10T403/60 , Y10T403/606
摘要： A retaining component for securing an external structure or panel to a seat track within a mobile platform, such as an aircraft. The retaining component includes a pair of flexible flanges that are adapted to engage an external component or panel, in one example a seat track in a commercial aircraft cabin area. The retaining component also includes a base portion having a flexible portion with at least one locking tab protruding therefrom. One or more hook-shaped engaging tabs also protrude from the base portion. The engaging tabs and the locking tab enable the retaining component to be secured to a flange of a seat track having a plurality of spaced apart holes in a manner that does not require any external threaded or rivet style fastening elements, or the use of separate assembly tools. The retaining component, in one form, is a single piece, lightweight, integrally formed component that is ideally suited for use in mobile platforms such as commercial aircraft where assembly time and costs are important considerations in the manufacture of a commercial aircraft.
摘要翻译： 用于将外部结构或面板固定到诸如飞行器的移动平台内的座椅轨道的保持部件。 保持部件包括一对柔性凸缘，其适于接合外部部件或面板，在一个示例中是商用飞机机舱区域中的座椅轨道。 保持部件还包括具有柔性部分的基部部分，其中至少一个锁定突片从其突出。 一个或多个钩形接合突片也从基部突出。 接合突片和锁定突舌使得保持部件能够以不需要任何外部螺纹或铆钉式紧固元件的方式固定到具有多个间隔开的孔的座椅轨道的凸缘上，或者使用单独的组件 工具 一种形式的保持部件是单件，重量轻，整体形成的部件，其理想地适用于诸如商用飞机的移动平台，其中组装时间和成本是制造商用飞机的重要考虑因素。
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