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    SYSTEM AND METHOD FOR DEFINING AND PREDICTING AIRCRAFT TRAJECTORIES
    1.
    发明申请
    SYSTEM AND METHOD FOR DEFINING AND PREDICTING AIRCRAFT TRAJECTORIES 审中-公开
    用于定义和预测飞机轨道的系统和方法

    公开(公告)号：WO2015101848A3

    公开(公告)日：2016-05-12

    申请号：PCT/IB2014066292

    申请日：2014-11-24

    Applicant: BOEING CO

    Inventor： NAVARRO FRANCISCO ,  VALLS HERNÁNDEZ ERNESTO ,  VILAPLANA MIGUEL ,  CHESSA PIERO ,  QUEREJETA MASSAVEU CARLOS

    IPC: G01C21/20 ,  G06Q10/04 ,  G06Q50/30 ,  G08G5/00

    CPC classification number: G08G5/0052 ,  G01C21/20 ,  G06Q10/047 ,  G06Q50/30 ,  G08G5/0034 ,  G08G5/0091 ,  G08G5/0095

    Abstract: The method of the present invention comprises acquiring input data of both aircraft performance characteristics and atmospheric data, and defining trajectory parameters to which the aircraft trajectory must be subjected, the method further comprising defining aircraft trajectory parameters; acquiring a plurality of atmospheric forecast ensembles; calculating a predicted trajectory from each atmospheric forecast of an atmospheric forecast ensemble, said predicted trajectory having associated information regarding a certain figure of merit of the aircraft trajectory, wherein an ensemble of predicted trajectories is obtained from each atmospheric forecast ensemble, each predicted trajectory of the ensemble of predicted trajectories having an associated probability derived from the probability of each atmospheric forecast within an atmospheric forecast ensemble; the system of the present disclosure comprising all the necessary equipment to carry out the method of the present disclosure.

    Abstract translation: 本发明的方法包括获取飞机性能特征和大气数据两者的输入数据，以及定义飞机轨迹必须经受的轨迹参数，该方法还包括定义飞机轨迹参数; 获取多个大气预报组合; 计算大气预报集合的每个大气预报的预测轨迹，所述预测轨迹具有关于飞机轨迹的某个品质因数的相关信息，其中从每个大气预报集合获得每个预测轨迹的集合，每个预测轨迹 具有相关概率的预测轨迹的集合从大气预报集合内的每个大气预报的概率导出; 本公开的系统包括执行本公开的方法的所有必要设备。

    SYSTEMS AND METHODS FOR GROUND COLLISION AVOIDANCE
    2.
    发明申请
    SYSTEMS AND METHODS FOR GROUND COLLISION AVOIDANCE 审中-公开
    用于避免地面碰撞的系统和方法

    公开(公告)号：WO2015134078A3

    公开(公告)日：2015-12-17

    申请号：PCT/US2014069163

    申请日：2014-12-08

    Applicant: BOEING CO

    Inventor： BAER JOSHUA J ,  THOREEN ADAM M ,  WYCKOFF PETER N

    IPC: G08G5/04 ,  G01C23/00 ,  G08G5/00 ,  G08G5/06

    CPC classification number: G08G5/065 ,  G01C23/00 ,  G08G5/0021 ,  G08G5/045

    Abstract: A system for displaying guidance aids to a crew for ground obstacle avoidance, particularly wingtip clearance. Perspective areas are drawn representing the current locations of the wingtips over the ground and predicted locations out into the future for a specified time or a specified distance. A flight crew may use these displayed guidance aids to determine the proximity of any perceived threat to the airplane. This capability addresses the costly problem of wingtip/airplane ground collisions. The disclosed graphical cue systems are specifically targeted toward aircraft that have a large wing span/size and/or folding wingtips.

    Abstract translation: 用于向机组人员显示辅助地面障碍避免特别是翼尖间隙的辅助系统。 透视区域被绘制，表示在地面上的翼尖的当前位置以及在特定时间或指定距离内未来的预测位置。 飞行机组人员可以使用这些显示的辅助工具来确定任何感知到的威胁与飞机的距离。 这种能力解决了翼尖/飞机地面碰撞的昂贵问题。 所公开的图形提示系统专门针对具有大翼展/尺寸和/或折叠翼尖的飞机。

    SYSTEM AND METHOD FOR MEASURING PARAMETERS AT AIRCRAFT LOC1
    3.
    发明申请
    SYSTEM AND METHOD FOR MEASURING PARAMETERS AT AIRCRAFT LOC1 审中-公开
    用于在飞机LOC1上测量参数的系统和方法

    公开(公告)号：WO2008118633A8

    公开(公告)日：2015-11-12

    申请号：PCT/US2008056534

    申请日：2008-03-11

    Applicant: BOEING CO ,  MCNERNEY MARK A ,  YEELES CHRISTOPHER J ,  MCGHEHEY MARK J ,  HOLLAND MARK J

    Inventor： MCNERNEY MARK A ,  YEELES CHRISTOPHER J ,  MCGHEHEY MARK J ,  HOLLAND MARK J

    IPC: B64D43/00 ,  G01M9/06

    CPC classification number: H04Q9/00

    Abstract: A system (12) for measuring parameters at a plurality of loci associated with an aircraft includes: (a) a central unit (14); (b) a plurality of communicating nodes (16n) coupled with the central unit; and (c) a respective plurality of sensing units (18m, 20m, 22m, 24m) associated with each respective communicating node of the plurality of communicating nodes; at least one selected sensing unit of at least one respective plurality of sensing units being a remote sensing unit. The at least one remote sensing unit communicates wirelessly with the respective communicating node.

    Abstract translation: 用于测量与飞行器相关联的多个轨迹的参数的系统（12）包括：（a）中央单元（14）; （b）多个通信节点耦合与中央单元（16N）的; 和（c）各自的多个与所述多个通信节点中的每个各自的通信节点相关联的感测单元（18米，20M，22M，24M）的; 至少一个选择的至少一个相应的多个感测单元是远程感测单元的感测单元。 所述至少一个远程传感单元与各自的通信节点进行无线通信。

    SYSTEMS AND METHODS FOR ROBOTIC MEASUREMENT OF PARTS
    4.
    发明申请
    SYSTEMS AND METHODS FOR ROBOTIC MEASUREMENT OF PARTS 审中-公开
    用于机械测量零件的系统和方法

    公开(公告)号：WO2014200653A3

    公开(公告)日：2015-04-09

    申请号：PCT/US2014038088

    申请日：2014-05-15

    Applicant: BOEING CO

    Inventor： VASQUEZ CHRISTINA M ,  BOYL-DAVIS THEODORE M ,  VALENZUELA DARIO I ,  JONES DARRELL D

    IPC: G05B19/401 ,  B25J9/16 ,  G01B5/008 ,  G01B11/03

    CPC classification number: G05B19/402 ,  G05B19/401 ,  G05B2219/40298 ,  G05D1/021 ,  Y10S901/44

    Abstract: Systems and methods for robotic measurement of parts are provided. One system includes one or more omni-directional ground vehicles configured to move within a facility defined work zone to a setup calibration station and an engineering defined work space, wherein the engineering defined work space includes a part to be measured. The system also includes a multi-axis robot removably coupled to each of the omni-direction ground vehicles and configured to move a laser scanner, wherein the laser scanner of each of the multi-axis robots is configured to move in at least two linear directions and one rotational direction. The system further includes a processor configured to automatically generate a surface ready output file from measurement data received from the laser scanners, wherein the surface ready output file is configured to command a machine to manufacture a mating component to the part.

    Abstract translation: 提供了用于机器人测量零件的系统和方法。 一个系统包括一个或多个全方位地面车辆，其被配置为在设施定义的工作区域内移动到安装校准站和工程定义的工作空间，其中工程定义的工作空间包括待测量的部件。 该系统还包括可移除地联接到每个全向地面车辆并且被配置为移动激光扫描器的多轴机器人，其中每个多轴机器人的激光扫描器被配置成在至少两个直线方向上移动 和一个旋转方向。 该系统还包括处理器，其被配置为根据从激光扫描器接收的测量数据自动生成表面就绪输出文件，其中表面就绪输出文件被配置为命令机器制造到部件的配合部件。

    BARCODE ACCESS TO ELECTRONIC RESOURCES FOR COMPLEX SYSTEM PARTS
    6.
    发明申请
    BARCODE ACCESS TO ELECTRONIC RESOURCES FOR COMPLEX SYSTEM PARTS 审中-公开
    条形码访问复杂系统部件的电子资源

    公开(公告)号：WO2014175979A3

    公开(公告)日：2014-12-31

    申请号：PCT/US2014031173

    申请日：2014-03-19

    Applicant: BOEING CO

    Inventor： FLOYD JOSEPH F ,  HADLEY BRENT L ,  EAMES PATRICK J

    IPC: G06F17/00 ,  G06F7/10 ,  G06Q30/00

    CPC classification number: G06F17/30002 ,  G06F17/30879

    Abstract: A system (100) is provided for access to system-related resources for complex-system parts. The system (100) includes a barcode reader (202) and front-end engine (204) coupled thereto. The barcode reader (202) is configured to scan a barcode located on a complex-system part. The barcode encodes links to respective system-related resources for the complex-system part, including software-based systems and/or electronic documents. The barcode reader (202), then, is configured to decode the links from the barcode. The front-end engine (204) is in turn configured to generate a portal that identifies the complex-system part, and that includes the links decoded from the barcode. The front-end engine (204) is also configured to cause display of the portal in a graphical user interface through which the links are navigable to access the respective system-related resources for the complex-system part.

    Abstract translation: 提供系统（100）用于访问用于复杂系统部件的系统相关资源。 系统（100）包括与其耦合的条形码读取器（202）和前端引擎（204）。 条形码读取器（202）被配置为扫描位于复合系统部件上的条形码。 条形码将针对复合系统部件的相应系统相关资源的链接编码，包括基于软件的系统和/或电子文档。 然后，条形码读取器（202）被配置为对来自条形码的链接进行解码。 前端引擎（204）又被配置为生成识别复合系统部分并且包括从条形码解码的链接的门户。 前端引擎（204）还被配置为使得门户在图形用户界面中显示，通过该图形用户界面，链接可以通过该界面访问用于复合系统部分的相应的系统相关资源。

    GAS SEPARATION MODULES AND METHODS FOR FORMING
    7.
    发明申请
    GAS SEPARATION MODULES AND METHODS FOR FORMING 审中-公开
    气体分离模块及其形成方法

    公开(公告)号：WO2014143336A3

    公开(公告)日：2014-12-31

    申请号：PCT/US2013077205

    申请日：2013-12-20

    Applicant: BOEING CO

    Inventor： CAO TUAN Q

    IPC: B01D63/02 ,  B01D53/22

    CPC classification number: B01D53/22 ,  B01D63/022 ,  B01D63/043 ,  B01D2053/224 ,  B01D2256/10 ,  B01D2257/104 ,  B01D2259/4575 ,  B01D2313/13 ,  B64D37/32 ,  B82Y30/00 ,  Y10S977/773 ,  Y10S977/833 ,  Y10T156/1052 ,  Y10T156/1064

    Abstract: A gas separation module includes at least one inlet port, a plurality of outlet ports, and a plurality of hollow fiber membranes. Individual fibers have a feed end and a product end with a retentate interior side and a permeate exterior side. The module includes a feed tubesheet within the shell segregating the at least one inlet port and the permeate side of the fibers. The feed tubesheet includes a matrix and at least one segment joint. The segment joint separates segments of the feed tubesheet from one another. A formation method includes positioning a hollow fiber membrane material in association with at least one tubesheet segment joint and applying a matrix. The method includes forming a feed tubesheet from cured matrix and the segment joint and forming a plurality of hollow fiber membranes from the fiber material. The segment joint separates segments of the feed tubesheet from one another.

    Abstract translation: 气体分离模块包括至少一个入口端口，多个出口端口和多个中空纤维膜。 单个纤维具有进料端，产物末端具有滞留物内侧和渗透物外侧。 该模块包括壳体内的进料管板，其分离纤维的至少一个入口端口和渗透侧。 进料管板包括基体和至少一个段接头。 节段接头将进料管板的段彼此分开。 形成方法包括将中空纤维膜材料定位成与至少一个管板段接头相关联并施加基质。 该方法包括从固化基质和片段接头形成进料管片，并从纤维材料形成多个中空纤维膜。 节段接头将进料管板的段彼此分开。

    AIRCRAFT PART CONTROL SYSTEM
    8.
    发明申请
    AIRCRAFT PART CONTROL SYSTEM 审中-公开
    飞机零件控制系统

    公开(公告)号：WO2012166545A3

    公开(公告)日：2014-12-31

    申请号：PCT/US2012039429

    申请日：2012-05-24

    Applicant: BOEING CO ,  XU ALEKZANDER ,  LI WINFENG ,  AYYAGARI ARUN ,  KUMAR ANIL ,  BLACKWELL DAVID B

    Inventor： XU ALEKZANDER ,  LI WINFENG ,  AYYAGARI ARUN ,  KUMAR ANIL ,  BLACKWELL DAVID B

    IPC: G06K7/00 ,  G06K7/08 ,  H04B5/00

    CPC classification number: B64F5/60 ,  G06Q10/06 ,  G06Q10/087

    Abstract: A method and apparatus for managing parts. Location information is displayed for a part on an aircraft on a mobile device. A determination is made as to whether the part is present in a location using a sensor system in the mobile device when the mobile device is in a zone including the location. A presence of the part in the location is indicated in response to the part being present in the location.

    Abstract translation: 一种用于管理零件的方法和装置。 在移动设备上的飞机上的零件显示位置信息。 当移动设备在包括该位置的区域中时，确定该部件是否存在于使用移动设备中的传感器系统的位置中。 响应于位置中存在的部分来指示该部位在该位置中的存在。

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