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71. 发明申请

WO2008091287A2 CARGO TRANSPORT SYSTEM AND METHOD 审中-公开
标题翻译：货物运输系统和方法
公开(公告)号：WO2008091287A2
公开(公告)日：2008-07-31
申请号：PCT/US2007/016375
申请日：2007-07-18
申请人： THE BOEING COMPANY , SANFORD, William, C. , LAIB, Trevor , MITCHELL, Brad , SANCHEZ, Jesus , FLETCHER, Henry, V. , CALLAHAN, Kevin, S.
发明人： SANFORD, William, C. , LAIB, Trevor , MITCHELL, Brad , SANCHEZ, Jesus , FLETCHER, Henry, V. , CALLAHAN, Kevin, S.
CPC分类号： B64D9/00 , B64D2009/006 , Y02T50/46
摘要： A system for loading cargo containers into a storage hold, and offloading cargo containers from the storage hold, especially of a vehicle, such as an aircraft. The system includes at least one guide rail and a motorized platform, onto which cargo containers are loaded, cooperating mechanically with the guide rail. The guide rail guides the cargo laden motorized platform into the storage hold, and the motorized platform deposits the cargo upon remote command. The motorized platform has a chassis; a power source; a control module controlling drive motors of the wheels of the platform; and means for reciprocating at least a portion of an upper surface of the platform sufficient to elevate a load placed thereon above the guide rail height.
摘要翻译：一种用于将货物集装箱装载到储存架中的装置，以及从储存架，特别是诸如飞机的车辆卸载货物集装箱的系统。该系统包括至少一个导轨和电动平台，货物集装箱在其上装载有与导轨机械地配合的电动平台。导轨将货物装载的电动平台引导到储存架中，并且电动平台在远程命令时存放货物。电动平台有底盘; 电源; 控制所述平台车轮的驱动马达的控制模块; 以及用于使所述平台的上表面的至少一部分往复移动的装置，其足以使其上方的载荷提升到所述导轨高度之上。

72. 发明申请

WO2008057385A1 REMOTE NONDESTRUCTIVE INSPECTION SYSTEMS AND METHODS 审中-公开
标题翻译：远程非导体检查系统和方法
公开(公告)号：WO2008057385A1
公开(公告)日：2008-05-15
申请号：PCT/US2007/023072
申请日：2007-10-31
申请人： THE BOEING COMPANY , KOLLGAARD, Jeffrey, R. , GEORGESON, Gary, E. , BERTRAND, Blake, A. , BOSSI, Richard, H.
发明人： KOLLGAARD, Jeffrey, R. , GEORGESON, Gary, E. , BERTRAND, Blake, A. , BOSSI, Richard, H.
IPC分类号： G06F11/273
CPC分类号： G06F11/2294
摘要： Systems and methods are disclosed for providing nondestructive inspection (NDI) services. For example in accordance with an embodiment of the invention, a system for remote inspection includes a nondestructive inspection (NDI) system configured to examine a structure and provide NDI data related to a damage condition of the structure, the NDI system being configured to communicate the NDI data to a remote location; and a remote computer disposed at the remote location, the remote computer being configured to receive the NDI data and provide the received NDI data for a review, the remote computer being configured to communicate an analytical result based on the review to the NDI system, the analytical result including a repair disposition decision corresponding to the damage condition.
摘要翻译：公开了用于提供无损检测（NDI）服务的系统和方法。例如，根据本发明的实施例，用于远程检查的系统包括被配置为检查结构并提供与结构的损坏状况相关的NDI数据的非破坏性检查（NDI）系统，NDI系统被配置为将 NDI数据到远程位置; 以及设置在所述远程位置的远程计算机，所述远程计算机被配置为接收所述NDI数据并提供所接收的NDI数据以进行审查，所述远程计算机被配置为将基于所述审查的分析结果传达到所述NDI系统，分析结果包括对应于损坏状况的修复处置决定。

73. 发明申请

WO2008039643A1 THERMAL PROCESSING METHOD FOR IMPROVED MACHINABILITY OF TITANIUM ALLOYS 审中-公开
标题翻译：用于改善钛合金机械性能的热处理方法
公开(公告)号：WO2008039643A1
公开(公告)日：2008-04-03
申请号：PCT/US2007/078198
申请日：2007-09-11
申请人： THE BOEING COMPANY , COTTON, James, D. , MERRICK, William, L. , WATTS, Michael, L.
发明人： COTTON, James, D. , MERRICK, William, L. , WATTS, Michael, L.
IPC分类号： C22F1/18 , C22C14/00
CPC分类号： C22C14/00 , C22F1/183
摘要： A method is provided for improving the machinability of a titanium alloy includes heating the alloy at a temperature and time period that imparts to the alloy a microstructure having between about 10 and 15 vol.% alpha phase in a beta phase matrix. According to one embodiment, the alloy is thereafter annealed at a temperature lower than the temperature for the initial heating step, and for a duration that is longer than the time period for the initial heating step.
摘要翻译：提供了一种用于提高钛合金的机械加工性的方法，包括在赋予合金的温度和时间周期内加热合金，在β相基体中具有约10至15体积％的α相之间的微结构。根据一个实施方案，然后在低于初始加热步骤的温度的温度下退火合金，并且持续时间长于初始加热步骤的时间段。

74. 发明申请

WO2007078408A2 APPARATUS AND METHODS FOR INSPECTING A COMPOSITE STRUCTURE FOR DEFECTS 审中-公开
标题翻译：用于检查缺陷的复合结构的装置和方法
公开(公告)号：WO2007078408A2
公开(公告)日：2007-07-12
申请号：PCT/US2006/042717
申请日：2006-10-31
申请人： THE BOEING COMPANY , ENGELBART, Roger, W. , HANNEBAUM, Reed , POLLOCK, Tim , ORR, Sam , RECTOR, Eric , PUTNAM, Jeff
发明人： ENGELBART, Roger, W. , HANNEBAUM, Reed , POLLOCK, Tim , ORR, Sam , RECTOR, Eric , PUTNAM, Jeff
CPC分类号： G01N21/88 , B29C70/382 , B29C70/386 , G01N2021/8472 , G01N2021/8867 , G01N2201/0635 , G01N2201/0636
摘要： A system and method of inspecting material laid by a material placement machine. Light is directed onto the material in a direction essentially normal to the material to illuminate a section of the material. Laser energy is projected onto the section at an angle predetermined to reveal imperfections in the section. This system provides improved illumination for material widths exceeding six inches and is scalable for inspecting various material widths.
摘要翻译：一种材料放置机器放置材料的检查系统和方法。光以基本上垂直于材料的方向被引导到材料上以照射材料的一部分。激光能量以预定的角度投影到部分上，以显示该部分中的缺陷。该系统为超过6英寸的材料宽度提供改进的照明，并且可扩展以用于检查各种材料宽度。

75. 发明申请

WO2015020721A1 BLADE COVER 审中-公开
标题翻译：刀片盖
公开(公告)号：WO2015020721A1
公开(公告)日：2015-02-12
申请号：PCT/US2014/041298
申请日：2014-06-06
申请人： THE BOEING COMPANY
发明人： GINGRICH, Thomas, A.
IPC分类号： B26B29/02
CPC分类号： B26B29/025 , B26B29/02 , Y10T83/04
摘要： A blade cover (10) may include a cover body (32) defining an interior volume (46), the cover body being configured to receive a cutting implement (12) within the interior volume, a recess (56) is disposed in the cover body, and a slot (44) is disposed through the recess, the slot defining an opening into the interior volume, wherein the slot is configured to receive at least a portion of a blade (14) of the cutting implement and the recess is configured to expose at least a portion of the blade of the cutting implement.
摘要翻译：刀片盖（10）可以包括限定内部容积（46）的盖主体（32），所述盖主体被构造成在所述内部容积内容纳切割工具（12），凹部（56）设置在所述盖主体和槽（44）穿过所述凹槽设置，所述狭槽限定到所述内部容积中的开口，其中所述狭槽被构造成容纳所述切割工具的刀片（14）的至少一部分并且所述凹部被配置以暴露切割工具的刀片的至少一部分。

76. 发明申请

WO2014088704A2 JOINING COMPOSITE COMPONENTS USING LOW TEMPERATURE THERMOPLASTIC FILM FUSION 审中-公开
标题翻译：使用低温热塑性膜熔合加工复合组件
公开(公告)号：WO2014088704A2
公开(公告)日：2014-06-12
申请号：PCT/US2013/065238
申请日：2013-10-16
申请人： THE BOEING COMPANY
发明人： WONG, Sharon , RUBIN, Alexander M. , HEINZ, Stephen R.
IPC分类号： B29C65/02
CPC分类号： B29C65/02 , B29C65/1412 , B29C65/18 , B29C65/44 , B29C65/4815 , B29C65/5057 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/41 , B29C66/43441 , B29C66/474 , B29C66/49 , B29C66/524 , B29C66/63 , B29C66/71 , B29C66/712 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/73117 , B29C66/73752 , B29C66/73771 , B29C66/73772 , B29C66/73773 , B29C66/73774 , B29C66/7392 , B29C66/73921 , B29C66/7394 , B29C66/73941 , B29C66/742 , B29C66/7461 , B29C66/81463 , B29C66/8322 , B29C66/919 , B29C66/91935 , B29C70/026 , B29C70/086 , B29C70/40 , B29K2063/00 , B29K2071/00 , B29K2081/06 , B29K2105/0872 , B29K2307/04 , B29K2995/004 , B29K2995/0097 , B29L2031/3076 , B32B27/08 , B32B37/04 , B32B2305/076 , B32B2398/20 , B32B2605/18 , C09J5/00 , B29K2081/04 , B29K2309/08
摘要： Composite components are joined together by an amorphous thermoplastic film forming a fused thermoplastic joint between the components. Fusion of the film may be achieved at relatively low temperatures that are sufficient to cure thermoset composite components, but are below the melting point of semi-crystalline thermoplastic components.
摘要翻译：复合部件通过在组件之间形成熔融热塑性接头的无定形热塑性薄片连接在一起。膜的融合可以在足以固化热固性复合组分但低于半结晶热塑性组分的熔点的相对低的温度下实现。

77. 发明申请

WO2014055187A1 METHOD AND APPARATUS FOR FABRICATING AN ULTRA-HIGH MOLECULAR WEIGHT POLYMER STRUCTURE 审中-公开
标题翻译：制备超高分子量聚合物结构的方法和装置
公开(公告)号：WO2014055187A1
公开(公告)日：2014-04-10
申请号：PCT/US2013/057499
申请日：2013-08-30
申请人： THE BOEING COMPANY
发明人： CLEMEN, Mark, J., Jr.
IPC分类号： B29C63/00 , B29C35/08 , B29C70/38 , B32B37/16 , B32B38/18 , B29C65/00
CPC分类号： B29C35/08 , B29C65/1403 , B29C66/1122 , B29C66/45 , B29C66/8362 , B29C70/386 , B29C70/388 , B29C2035/085 , B29C2035/0877 , B29K2023/0683 , B32B37/16 , B32B38/0008 , B32B2038/0076 , B32B2038/1891 , B32B2310/0875 , B32B2310/0887 , B32B2323/04 , Y10T156/10
摘要： A polymer laminate is fabricated by laying down layers (22) of an ultra-high molecular weight polymer material (34) on top of each other, and fusing the layers (22) to each other by cross-linking (25) molecular chains of adjoining layers (22).
摘要翻译：通过将超高分子量聚合物材料（34）的层（22）铺放在彼此的顶部上并通过交联（25）分子链将层（22）彼此熔合来制造聚合物层压体邻接层（22）。

78. 发明申请

WO2013133831A1 METHOD AND ASSEMBLY FOR MOUNTING COMPONENTS ON BEAMS 审中-公开
标题翻译：用于安装组件的方法和组件
公开(公告)号：WO2013133831A1
公开(公告)日：2013-09-12
申请号：PCT/US2012/028220
申请日：2012-03-08
申请人： THE BOEING COMPANY , TIAN, Yuri , GOTTWALD, Robert Pratt
发明人： TIAN, Yuri , GOTTWALD, Robert Pratt
IPC分类号： F16B2/08 , F16L3/24 , H02G3/32 , B64C1/40 , G09F7/18 , B64D27/26
CPC分类号： B64D27/00 , B64D27/26 , B64D2027/264 , F16B2/08 , H02G3/32
摘要： A mounting assembly (50) allows components (48) to be mounted on a beam (38) having a rectangularly shaped cross section and flat sides (64). The mounting assembly (50) includes a plurality of adapter members (52-58) and a strap (70). Each of the adapter members (52-58) has a generally flat inner face (60) engaging one of the flat sides (64) of the beam (38) and a generally curved outer face (62). Drawing the strap (70) against the curved outer faces (62) of the adapter members (52-58) clamps the adapter members (52-58) on the beam (38). One or more components (48) may be attached to each of the adapter members (52-58) at a location inboard of the strap (70).
摘要翻译：安装组件（50）允许组件（48）安装在具有矩形横截面和平坦侧面（64）的梁（38）上。安装组件（50）包括多个适配器构件（52-58）和带子（70）。每个适配器构件（52-58）具有接合梁（38）的平坦侧面（64）中的一个的大致平坦的内表面（60）和大致弯曲的外表面（62）。将绑带（70）拉到适配器构件（52-58）的弯曲外表面（62）上时，夹紧梁（38）上的适配器构件（52-58）。一个或多个部件（48）可以在带子（70）的内侧的位置处附接到每个适配器部件（52-58）。

79. 发明申请

WO2012082280A1 COMPOSITES HAVING DISTORTIONAL RESIN COATED FIBERS 审中-公开
标题翻译：具有折射树脂涂层纤维的复合材料
公开(公告)号：WO2012082280A1
公开(公告)日：2012-06-21
申请号：PCT/US2011/060472
申请日：2011-11-11
申请人： THE BOEING COMPANY , SCHNEIDER, Terry L. , CHRISTENSEN, Stephen , GOSSE, Jonathan H.
发明人： SCHNEIDER, Terry L. , CHRISTENSEN, Stephen , GOSSE, Jonathan H.
IPC分类号： C08J5/06
CPC分类号： C08J5/06 , C08J2300/00
摘要： A fiber reinforced resin composite includes a coating on the fibers that improves load transfer between the fibers and the surrounding resin matrix.
摘要翻译：纤维增强树脂复合材料包括纤维上的涂层，其改善纤维与周围树脂基质之间的载荷转移。

80. 发明申请

WO2011068592A1 SANDWICH STRUCTURE HAVING ARRESTMENT FEATURE AND METHOD OF MAKING THE SAME 审中-公开
标题翻译：具有制作特征的三维结构及其制作方法
公开(公告)号：WO2011068592A1
公开(公告)日：2011-06-09
申请号：PCT/US2010/052343
申请日：2010-10-12
申请人： THE BOEING COMPANY , SAFF, Charles R. , FOGARTY, John H. , GU, Haozhong , RICHARDSON, Terry D. , RETZ, Kevin M.
发明人： SAFF, Charles R. , FOGARTY, John H. , GU, Haozhong , RICHARDSON, Terry D. , RETZ, Kevin M.
IPC分类号： B32B3/06 , B32B3/12
CPC分类号： B32B3/18 , B23B3/04 , B29C65/00 , B29C66/01 , B29C66/05 , B29C66/10 , B29C66/11 , B29C66/112 , B29C66/1122 , B29C66/114 , B29C66/1142 , B29C66/118 , B29C66/1182 , B29C66/122 , B29C66/128 , B32B3/04 , B32B3/06 , B32B3/12 , B32B3/14 , B32B2250/03 , B32B2307/718 , B32B2605/18 , Y10T29/49622 , Y10T29/49982 , Y10T156/10 , Y10T156/1002 , Y10T156/1034 , Y10T156/1093 , Y10T428/239 , Y10T428/24174 , Y10T428/24752 , Y10T428/24777 , Y10T428/249923
摘要： A composite sandwich structure comprises a core sandwiched between composite laminate facesheets. The core includes a plurality of core sections spliced together at joints that incorporate integral features for arresting the propagation of irregularities in the facesheets.
摘要翻译：复合夹层结构包括夹在复合层压板之间的芯。芯包括在接头处拼接在一起的多个芯部分，其包含用于阻止面板中的凹凸的传播的整体特征。

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