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公开(公告)号：US10598251B2
公开(公告)日：2020-03-24
申请号：US15487603
申请日：2017-04-14
申请人： The Boeing Company
摘要： A vibration damper including a frame having at least a first cavity, a frame first end and a frame second end spaced from the frame first end; a shaft slidably coupled to and extending into the frame where the shaft extends through the first cavity; a first vibration isolator disposed within the first cavity where the shaft extends through the first vibration isolator so as to capture the first vibration isolator within the first cavity where the first vibration isolator interfaces with the frame second end; and a second vibration isolator disposed on the shaft, where the shaft extends through the second vibration isolator so as to capture the second vibration isolator on the shaft where the second vibration isolator interfaces with the frame second end opposite the first vibration isolator, where the first vibration isolator and the second vibration isolator act only in compression.
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公开(公告)号：US20170173896A1
公开(公告)日：2017-06-22
申请号：US15450832
申请日：2017-03-06
申请人： THE BOEING COMPANY
CPC分类号： B29C70/30 , B29C33/0011 , B29C33/38 , B29C33/3842 , B29C33/40 , B29C33/76 , B29C41/40 , B29C53/82 , B29C70/32 , B29C70/38 , B29K2079/085 , B29K2879/085 , B29K2905/02 , B29K2995/0017 , B29L2031/3076 , B29L2031/3082 , B33Y10/00 , B33Y80/00 , Y02T50/43 , Y10T29/49842
摘要： One example of the present disclosure relates to a tool for laying up composite material to form a workpiece having a target contour. The tool includes a support structure including an elongated member having a longitudinal axis, and support plates connected to the elongated member and spaced apart from each other along the longitudinal axis. The elongated member includes a metallic material. The tool also includes a non-metallic backing structure connected to the support plates, the non-metallic backing structure comprising a working surface that includes a backing contour complementary to the target contour.
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公开(公告)号：US09597843B2
公开(公告)日：2017-03-21
申请号：US14278205
申请日：2014-05-15
申请人： THE BOEING COMPANY
IPC分类号： B33Y10/00 , B33Y80/00 , B29C70/30 , B29C33/38 , B29C33/40 , B29C70/32 , B29C33/00 , B29C33/76 , B29K79/00
CPC分类号： B29C70/30 , B29C33/0011 , B29C33/38 , B29C33/3842 , B29C33/40 , B29C33/76 , B29C41/40 , B29C53/82 , B29C70/32 , B29C70/38 , B29K2079/085 , B29K2879/085 , B29K2905/02 , B29K2995/0017 , B29L2031/3076 , B29L2031/3082 , B33Y10/00 , B33Y80/00 , Y02T50/43 , Y10T29/49842
摘要： One example of the present disclosure relates to a tool for laying up composite material to form a workpiece having a target contour. The tool includes a support structure including an elongated member having a longitudinal axis, and support plates connected to the elongated member and spaced apart from each other along the longitudinal axis. The elongated member includes a metallic material. The tool also includes a non-metallic backing structure connected to the support plates, the non-metallic backing structure comprising a working surface that includes a backing contour complementary to the target contour.
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公开(公告)号：US11167848B2
公开(公告)日：2021-11-09
申请号：US15933928
申请日：2018-03-23
申请人： The Boeing Company
摘要： System and method for loading cargo onto an unmanned aerial vehicle (UAV). One embodiment is a cargo pod for an unmanned aerial vehicle (UAV). The cargo pod includes a hollow body that forms a section of a fuselage of the UAV, and further includes a latching mechanism that releasably secures the hollow body with the fuselage of the UAV.
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公开(公告)号：US20190291626A1
公开(公告)日：2019-09-26
申请号：US15933928
申请日：2018-03-23
申请人： The Boeing Company
摘要： System and method for loading cargo onto an unmanned aerial vehicle (UAV). One embodiment is a cargo pod for an unmanned aerial vehicle (UAV). The cargo pod includes a hollow body that forms a section of a fuselage of the UAV, and further includes a latching mechanism that releasably secures the hollow body with the fuselage of the UAV.
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公开(公告)号：US09895836B2
公开(公告)日：2018-02-20
申请号：US14487422
申请日：2014-09-16
申请人： The Boeing Company
发明人： Matthew S. Stauffer
IPC分类号： B29C47/00 , B32B5/12 , B32B3/28 , B32B5/02 , B32B5/22 , B32B5/26 , B32B7/00 , B32B27/08 , B32B27/36 , B32B3/14 , B32B3/18 , B29C64/106 , B29C64/386 , B29L31/30 , B33Y10/00 , B33Y50/02 , B33Y80/00
CPC分类号： B29C47/0045 , B29C64/106 , B29C64/386 , B29L2031/3076 , B32B3/14 , B32B3/18 , B32B3/28 , B32B5/022 , B32B5/12 , B32B5/22 , B32B5/26 , B32B7/005 , B32B27/08 , B32B27/365 , B32B2250/20 , B32B2262/02 , B32B2307/50 , B32B2605/18 , B33Y10/00 , B33Y50/02 , B33Y80/00 , Y02T50/43
摘要： Technologies for fused filament fabrication using multi-directional layering are disclosed herein. According to aspects of the disclosure, a component may be strengthened using a multi-directional layering manufacturing technique. In some implementations, one or more portions of the component are manufactured in different orientations. In still further implementations, one layer of a component is laid down in a first orientation and a second layer of the component is laid down in a second orientation.
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公开(公告)号：US10118347B2
公开(公告)日：2018-11-06
申请号：US15450832
申请日：2017-03-06
申请人： THE BOEING COMPANY
IPC分类号： B29C33/00 , B29C70/30 , B29C70/32 , B29C70/38 , B29C53/82 , B29C33/76 , B29C41/40 , B29L31/30
摘要： A tool for laying up composite material to form a workpiece having a target contour is disclosed. The tool includes a support structure including an elongated member having a longitudinal axis, and support plates connected to the elongated member and spaced apart from each other along the longitudinal axis. The elongated member includes a metallic material. The tool also includes a non-metallic backing structure connected to the support plates, the non-metallic backing structure comprising a working surface that includes a backing contour complementary to the target contour.
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公开(公告)号：US09500249B2
公开(公告)日：2016-11-22
申请号：US14641586
申请日：2015-03-09
申请人： The Boeing Company
IPC分类号： F16F7/12
CPC分类号： F16F7/12
摘要： An apparatus and method for a composite structural aircraft transmission support link having an integral energy-absorbing feature is disclosed. The link is a two-force member that can carry structural loads up an ultimate load. When loaded beyond ultimate load the design allows sections of the link to fail in a controlled and progressive manner, so that energy is absorbed over a defined stroking distance.
摘要翻译： 公开了一种具有整体能量吸收特征的复合结构飞行器传动支撑连杆的装置和方法。 该连杆是一个双力部件，可承受最大载荷的结构载荷。 当加载超过极限负载时，设计允许链路的部分以受控和渐进的方式失效，使得能量在规定的行程距离上被吸收。
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公开(公告)号：US20160333960A1
公开(公告)日：2016-11-17
申请号：US14711199
申请日：2015-05-13
申请人： The Boeing Company
摘要： An energy absorbing fitting is constructed to absorb tension, shear and compression loads at a joint between two composite material beams of a composite material frame. The fitting is constructed with a band of composite material having an inverted U-shape, a panel of composite material having a U-shaped cross-section configuration that is assembled into the inverted U-shaped configuration of the band, and a sheet of composite material having an inverted L-shape configuration that is secured to the band and to the panel. The fitting is positioned at the intersection of the beams and is secured to the joint between the beams, thereby reinforcing the joint against tension, shear and compression loads.
摘要翻译： 构造能量吸收配件以吸收复合材料框架的两个复合材料梁之间的接头处的张力，剪切和压缩载荷。 该配件由具有倒U形的复合材料带构成，具有U形横截面构造的复合材料面板组装成带的倒置U形构造，以及复合材料片 具有固定到带和面板的倒L形构造的材料。 该配件定位在梁的交叉处并且被固定到梁之间的接合处，从而加强接头以抵抗张力，剪切和压缩载荷。
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公开(公告)号：US20160265613A1
公开(公告)日：2016-09-15
申请号：US14641586
申请日：2015-03-09
申请人： The Boeing Company
IPC分类号： F16F7/12
CPC分类号： F16F7/12
摘要： An apparatus and method for a composite structural aircraft transmission support link having an integral energy-absorbing feature is disclosed. The link is a two-force member that can carry structural loads up an ultimate load. When loaded beyond ultimate load the design allows sections of the link to fail in a controlled and progressive manner, so that energy is absorbed over a defined stroking distance.
摘要翻译： 公开了一种具有整体能量吸收特征的复合结构飞行器传动支撑连杆的装置和方法。 该连杆是一个双力部件，可承受最大载荷的结构载荷。 当加载超过极限负载时，设计允许链路的部分以受控和渐进的方式失效，使得能量在规定的行程距离上被吸收。
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