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91. 发明申请

WO2010025413A3 OPTIMIZING THE SHAPE OF A COMPOSITE STRUCTURE 审中-公开
标题翻译：优化复合结构的形状
公开(公告)号：WO2010025413A3
公开(公告)日：2010-05-20
申请号：PCT/US2009055433
申请日：2009-08-28
申请人： BOEING CO , HUNTER ETHAN W , FALASCO THOMAS J , SWANSON KURT M
发明人： HUNTER ETHAN W , FALASCO THOMAS J , SWANSON KURT M
IPC分类号： G06F17/50 , B29C70/00
CPC分类号： B29C70/00 , G06F17/5095 , G06F2217/08 , G06F2217/44 , Y02T50/43 , Y02T50/433
摘要： The shape of a laminated composite structure is optimized using finite element analysis. The optimized shape minimizes the weight of the structure while satisfying minimum strength and stiffness requirements.
摘要翻译：使用有限元分析优化层压复合结构的形状。优化的形状使结构的重量最小化，同时满足最小强度和刚度要求。

92. 发明申请

WO2008091713A3 THERMAL INSULATION ASSEMBLIES AND METHODS FOR FABRICATING THE SAME 审中-公开
标题翻译：热绝缘组件及其制造方法
公开(公告)号：WO2008091713A3
公开(公告)日：2010-05-20
申请号：PCT/US2008050018
申请日：2008-01-02
申请人： BOEING CO , HENG VANN , DICHIARA JR ROBERT A , CHU ELIZABETH , ZORGER DAVID
发明人： HENG VANN , DICHIARA JR ROBERT A , CHU ELIZABETH , ZORGER DAVID
IPC分类号： B32B18/00 , C04B35/117 , C04B35/185 , C04B35/80
CPC分类号： B32B18/00 , C04B35/117 , C04B35/185 , C04B35/803 , C04B41/009 , C04B41/5031 , C04B41/87 , C04B2111/00982 , C04B2235/3217 , C04B2235/3463 , C04B2235/3826 , Y10T29/49826 , Y10T428/166 , Y10T428/24033 , Y10T428/24942 , Y10T428/24999 , C04B41/4539 , C04B41/5037 , C04B35/00 , C04B35/80
摘要： Thermal insulation assemblies and methods for fabricating thermal insulation assemblies are provided. In an exemplary embodiment, a thermal insulation assembly comprises a ceramic tile having a surface coated with an alumina-mullite slurry. A ceramic matrix composite is disposed on the coated surface. The ceramic matrix composite comprises a first ply of a ceramic fiber impregnated with a ceramic matrix.
摘要翻译：提供隔热组件和制造隔热组件的方法。在示例性实施例中，绝热组件包括具有涂覆有氧化铝 - 莫来石浆料的表面的陶瓷砖。陶瓷基复合材料设置在涂层表面上。陶瓷基复合材料包括浸渍有陶瓷基体的陶瓷纤维的第一层。

93. 发明申请

WO2010053808A2 MULTI-ENERGY RADIOGRAPHY USING MONOENERGETIC PULSED SOURCE 审中-公开
标题翻译：使用单一脉冲源的多能量射线照相
公开(公告)号：WO2010053808A2
公开(公告)日：2010-05-14
申请号：PCT/US2009062438
申请日：2009-10-28
申请人： BOEING CO , GORDON CLARENCE L , BOSSI RICHARD H , ADAMSKI JOHN L
发明人： GORDON CLARENCE L , BOSSI RICHARD H , ADAMSKI JOHN L
IPC分类号： G01N23/04 , G01N23/18 , G01V5/00
CPC分类号： G01N23/043 , G01N23/18
摘要： A method and apparatus for multi -energy object inspection using a brilliant x-ray source. A first mono -energetic x-ray image of an object at a first selected energy is generated. A second mono-energetic x-ray image of the object at a second selected energy is generated. The first selected energy is different than the second selected energy. Additional mono- energetic x-ray images may be generated at energies different than previous energies up to n selected energies. The mono- energetic x-ray images are mathematically combined and processed to form a result. The result of processing the mono-energetic x-ray images is presented. The result comprises processed mono- energetic x-ray image data describing materials in the object with greater sensitivity, identifying the layers, and identifying the material composition than in the first image or the second image.
摘要翻译：一种使用明亮的X射线源进行多能量物体检测的方法和设备。产生处于第一选定能量的物体的第一单能量X射线图像。生成第二选定能量的物体的第二单能X射线图像。第一选择的能量不同于第二选择的能量。额外的单能X射线图像可以以与先前的能量不同的能量生成，直到n个选定的能量。单能x射线图像在数学上被组合并处理以形成结果。介绍了处理单能X射线图像的结果。结果包括处理的单能X射线图像数据，该数据以比第一图像或第二图像更高的灵敏度描述对象中的材料，识别层并识别材料成分。

94. 发明申请

WO2009148660A3 IMAGING AN ANOMALY USING BACKSCATTERED WAVES 审中-公开
标题翻译：使用后置波形成像异常
公开(公告)号：WO2009148660A3
公开(公告)日：2010-05-06
申请号：PCT/US2009036188
申请日：2009-03-05
申请人： BOEING CO , IHN JEONG-BEOM
发明人： IHN JEONG-BEOM
IPC分类号： G01N29/06 , G01N29/07 , G01N29/44
CPC分类号： G01N29/07 , G01N29/069 , G01N29/4427 , G01N2291/044 , G01N2291/2694
摘要： A method for generating an image of an anomaly may include generating a pulse wave into a structure being evaluated from each of a plurality of sensors and collecting scattered wave data caused by the pulse wave impacting an anomaly. The scattered wave data may be collected by the same sensor that generated the pulse wave or by a different sensor. The method may also include identifying backscattered wave data from a distal edge or border of the anomaly relative to a location of the sensor collecting the scattered wave data. The method may additionally include processing the backscattered wave data from each of the sensors collecting the scattered wave data to generate a two dimensional image of the anomaly. The method may further include presenting the two dimensional image of the anomaly.
摘要翻译：用于产生异常的图像的方法可以包括将脉搏波生成到从多个传感器中的每一个估计的结构中，并收集由脉冲波引起的影响异常的散射波数据。散射波数据可以由产生脉冲波的相同传感器或不同的传感器收集。该方法还可以包括从相对于收集散射波数据的传感器的位置的异常的远端边缘或边界识别反向散射波数据。该方法可以另外包括处理来自收集散射波数据的每个传感器的后向散射波数据以产生异常的二维图像。该方法还可以包括呈现异常的二维图像。

95. 发明申请

WO2010002518A3 SYSTEMS AND METHODS FOR ALLEVIATING AIRCRAFT LOADS WITH PLASMA ACTUATORS 审中-公开
标题翻译：用等离子体驱动器对飞机载荷进行跟踪的系统和方法
公开(公告)号：WO2010002518A3
公开(公告)日：2010-04-29
申请号：PCT/US2009045086
申请日：2009-05-22
申请人： BOEING CO , DROUIN-JR DONALD V , SCHWIMLEY SCOTT L
发明人： DROUIN-JR DONALD V , SCHWIMLEY SCOTT L
IPC分类号： B64C23/00 , F15D1/12 , H05H1/54
CPC分类号： B64C23/005 , B64C2230/12 , H05H1/2406 , Y02T50/166
摘要： Systems (100) and methods for alleviating aircraft loads with plasma actuators are disclosed. A method for operating an aircraft in accordance with a particular embodiment includes receiving an input corresponding to an aircraft component structural response to an aerodynamic load. The method can further include, based at least in part on the input corresponding to the aircraft component's structural response, reducing the structural response to the aerodynamic load by activating at least one plasma actuator carried by the aircraft, in accordance with one or more activation parameters.
摘要翻译：公开了使用等离子体致动器来减轻飞行器负载的系统（100）和方法。根据特定实施例的用于操作飞行器的方法包括接收对应于飞行器部件对空气动力学负载的结构响应的输入。该方法可以进一步包括至少部分地基于对应于飞行器部件的结构响应的输入，通过根据一个或多个激活参数激活由飞行器携带的至少一个等离子体致动器来减小对空气动力学负载的结构响应。

96. 发明申请

WO2009058454A3 METHOD AND APPARATUS FOR CLOSING A SWING TAIL ON AN AIRCRAFT 审中-公开
标题翻译：用于关闭飞机上的摇尾的方法和装置
公开(公告)号：WO2009058454A3
公开(公告)日：2009-11-26
申请号：PCT/US2008072933
申请日：2008-08-12
申请人： BOEING CO , NAKAMURA DARRYL HITOSHI , POECHLAUER KURT , VYESON CRAIG ALAN , PROBERT-BAKER ROGER , PIETERSEN QUENTIN THEODOR
发明人： NAKAMURA DARRYL HITOSHI , POECHLAUER KURT , VYESON CRAIG ALAN , PROBERT-BAKER ROGER , PIETERSEN QUENTIN THEODOR
IPC分类号： B64C1/14
CPC分类号： B64C1/22 , B64C1/1415
摘要： A method and apparatus for aligning a swing tail cargo door (416). An alignment system comprises an alignment ramp (700), a set of pull-in hook mechanisms (720,722), and a set of lock trains (958). The alignment ramp (700) may be configured for initial alignment between a swing tail cargo door (416) and an aircraft fuselage (406) during closing of the swing tail cargo door. The set of pull-in hook mechanisms (720, 722) may be disposed along an interface between the swing tail cargo door and the aircraft fuselage and may be capable of a final alignment between the swing tail cargo door and the aircraft fuselage during the closing of the swing tail cargo door. The set of lock trains (958) may be disposed along the interface and may be capable of locking a plurality of latch actuators (912, 950) in the latched position.
摘要翻译：一种用于对齐摆尾货舱门（416）的方法和装置。对准系统包括对准斜面（700），一组拉入钩机构（720,722）和一组锁定列（958）。对准斜面（700）可以被配置为在关闭摇摆尾货门期间在摆尾货舱门（416）和飞行器机身（406）之间的初始对准。该组牵引钩机构（720,722）可以沿着摆尾货物门和飞行器机身之间的界面设置，并且可以在关闭期间在摆尾货物门和飞机机身之间最终对准的秋千尾货门。锁组件（958）可以沿着界面布置，并且可以将多个闩锁致动器（912,950）锁定在锁定位置。

97. 发明申请

WO2007064856A3 METHODS AND SYSTEMS FOR MANAGING AIRCRAFT MAINTENANCE AND MATERIAL SUPPLY 审中-公开
标题翻译：管理飞机维护和材料供应的方法和系统
公开(公告)号：WO2007064856A3
公开(公告)日：2009-08-27
申请号：PCT/US2006045953
申请日：2006-11-30
申请人： BOEING CO , AVERY ROBERT L , LEONHARDI DAVID R , CRONIE WENDY A , NOMI MARGARET L , RHODES PATRICIA L , MALONEY JAY P , BUESER MATTHEW C , THACKER GRANT H , FROMM ERIK , KHERA CHERYL , KIRKISH PAULA M
发明人： AVERY ROBERT L , LEONHARDI DAVID R , CRONIE WENDY A , NOMI MARGARET L , RHODES PATRICIA L , MALONEY JAY P , BUESER MATTHEW C , THACKER GRANT H , FROMM ERIK , KHERA CHERYL , KIRKISH PAULA M
IPC分类号： G06Q10/00
CPC分类号： G06Q10/087 , G06Q10/20
摘要： Methods and systems for managing aircraft maintenance and material supply by a business entity for at least one customer are provided. The method includes managing a plurality of maintenance activities for an aircraft by the business entity wherein the plurality of maintenance activities are performed by at least one maintenance entity separate from the business entity and the at least one customer. The method further includes managing a supply of aircraft parts to the maintenance entity from a plurality of parts suppliers by the business entity and outputting at least one maintenance activity to be performed by the maintenance entity.
摘要翻译：提供了用于管理至少一个客户的业务实体的飞机维护和材料供应的方法和系统。该方法包括由业务实体管理飞机的多个维护活动，其中多个维护活动由与业务实体和至少一个客户分开的至少一个维护实体执行。该方法还包括由业务实体从多个零件供应商管理向维护实体提供飞机零件的供应，并且输出由维护实体执行的至少一个维护活动。

98. 发明申请

WO2008106585A3 ADHERENDS WITH ENHANCED SURFACES 审中-公开
标题翻译：与增强表面贴合
公开(公告)号：WO2008106585A3
公开(公告)日：2009-07-30
申请号：PCT/US2008055251
申请日：2008-02-28
申请人： BOEING CO , MACK JULIA J
发明人： MACK JULIA J
IPC分类号： C23C18/08 , B32B7/12 , B32B15/04 , B64C1/14
CPC分类号： C23C18/08 , B82Y30/00 , Y10S977/81 , Y10T428/12493 , Y10T428/12569 , Y10T428/12736 , Y10T428/1275 , Y10T428/12931 , Y10T428/12944 , Y10T428/26 , Y10T428/28 , Y10T428/31678
摘要： Metallic substrates have a surface for receiving application of an adhesive that includes a precipitated coating of metallic nanoparticulates. A first portion of the nanoparticulates is adhered to the surface and a second portion is in contact with the first portion. Also provided are adhered constructs. These constructs include a first substrate with a first surface that has a metallic precipitated coating of nanoparticulates. A first portion of the nanoparticulates is adhered to the surface and a second portion contacts the first portion. The constructs include a second substrate that has a second surface; and an adhesive is applied between the first surface and the second surface.
摘要翻译：金属基底具有用于接收包括金属纳米颗粒的沉淀涂层的粘合剂的表面。纳米颗粒的第一部分粘附到表面，第二部分与第一部分接触。还提供了粘附构造。这些构建体包括具有第一表面的第一基底，其具有纳米颗粒的金属沉淀涂层。纳米颗粒的第一部分粘附到表面，第二部分接触第一部分。构建体包括具有第二表面的第二基底; 并且在第一表面和第二表面之间施加粘合剂。

99. 发明申请

WO2008018902A8 SYSTEM AND METHOD FOR DETECTING SECURITY VIOLATION 审中-公开
标题翻译：用于检测安全隐患的系统和方法
公开(公告)号：WO2008018902A8
公开(公告)日：2009-07-09
申请号：PCT/US2007000824
申请日：2007-01-12
申请人： BOEING CO , ROYALTY CHARLES D
发明人： ROYALTY CHARLES D
IPC分类号： H04L29/06 , H04L12/22
CPC分类号： H04L63/0209 , H04L63/10
摘要： A system and a method for ensuring that the initiation of mobile platform operations using maintenance terminals or other tools is prohibited when maintenance activities are not intended to be performed. The solution involves the incorporation of a manual interlock switch (accessible only to authorized personnel) that blocks activation of certain functions during times when such activation would be hazardous and when no properly authorized person has authorized such activation. No system for performing such a function will respond to a request unless the interlock is enabled. Should such a request be received, the system is required to report a fault, so that an investigation can be made as to the cause of the invalid request.
摘要翻译：当不打算执行维护活动时，确保使用维护终端或其他工具启动移动平台操作的系统和方法被禁止。该解决方案涉及将手动互锁开关（仅限授权的人员）结合在一起，在这种激活是有害的时候，以及当没有正当授权的人授权这种激活时，阻止某些功能的激活。没有执行此功能的系统将响应请求，除非互锁已启用。如果收到这样的请求，系统需要报告错误，以便对无效请求的原因进行调查。

100. 发明申请

WO2008134151A3 LAMINAR FLOW SURFACES WITH SELECTED ROUGHNESS DISTRIBUTIONS, AND ASSOCIATED METHODS 审中-公开
标题翻译：具有选择的粗糙度分布的层间流动表面和相关方法
公开(公告)号：WO2008134151A3
公开(公告)日：2009-06-11
申请号：PCT/US2008057984
申请日：2008-03-24
申请人： BOEING CO , CROUCH JEFFREY D , NG LIAN L , SUTANTO MARY I
发明人： CROUCH JEFFREY D , NG LIAN L , SUTANTO MARY I
IPC分类号： B64C21/10 , F15D1/12
CPC分类号： B64C21/10 , B64C2230/26 , Y02T50/166
摘要： Laminar flow surfaces with selected roughness distributions, and associated methods are disclosed. A representative method for designing an airfoil includes selecting a parameter that includes a flow behavior distribution and/or a surface shape (221) for an airflow surface. Based at least in part on the selected parameter, the method can include (a) selecting a target roughness value and determining a chordwise location forward of which surface roughness is at or below the target roughness value (223) and/or (b) selecting a target chordwise location and determining a roughness value for a region forward of the chordwise location, with the surface roughness at or below the roughness value (224). In particular embodiments, a percentage of a local chord length of the airfoil over which the roughness is below a target value decreases in a spanwise direction. In another embodiment, the roughness at a particular spanwise location can increase over at least three values, continuously, in a step manner, or otherwise.
摘要翻译：公开了具有选定的粗糙度分布的层流表面和相关方法。用于设计翼型的代表性方法包括选择包括用于气流表面的流动行为分布和/或表面形状（221）的参数。至少部分地基于所选择的参数，该方法可以包括（a）选择目标粗糙度值并确定表面粗糙度等于或低于目标粗糙度值（223）和/或（b）选择的向前位置目标和弦位置，并且确定弦向位置向前的区域的粗糙度值，其中粗糙度等于或小于粗糙度值（224）。在特定实施例中，粗糙度低于目标值的翼型的局部翼弦长度的百分比在翼展方向上减小。在另一个实施例中，特定翼展方向位置处的粗糙度可以连续地，以逐步方式或以其他方式增加至少三个值。

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