AN AIRFRAME LEADING EDGE
    41.
    发明申请
    AN AIRFRAME LEADING EDGE 审中-公开
    空中飞行器领先

    公开(公告)号:US20150298787A1

    公开(公告)日:2015-10-22

    申请号:US14646028

    申请日:2012-11-20

    Applicant: SAAB AB

    CPC classification number: B64C1/062 B64C1/12 B64C3/28 B64D2045/0095

    Abstract: An airframe leading edge part designed to be replaceable fixed to a structural portion which during use moves through the air. The airframe leading edge part includes first and second longitudinal joint edges adapted to fit the structural portion. At least one joint is provided between the structural portion and at least one of the longitudinal joint edges. The joint is adapted to break in the event of a object strikes and deforms the airframe leading edge part during use. The joint is designed to break at beforehand determined maximum joint strength of the joint. Also a repair method for exchanging a damaged leading edge.

    Abstract translation: 设计为可更换的机身前缘部分固定到结构部分,在使用过程中移动通过空气。 机身前缘部分包括适于装配结构部分的第一和第二纵向接合边缘。 在结构部分和纵向接合边缘中的至少一个之间提供至少一个接头。 在使用时,关节适于在物体撞击的情况下破裂并使机身前缘部分变形。 接头设计为预先确定接头的最大接头强度。 也是用于更换损坏前缘的修复方法。

    A POROUS COATING APPLIED ONTO AN AERIAL ARTICLE
    42.
    发明申请
    A POROUS COATING APPLIED ONTO AN AERIAL ARTICLE 审中-公开
    适用于某一专利文献的多孔涂料

    公开(公告)号:US20150292074A1

    公开(公告)日:2015-10-15

    申请号:US14439929

    申请日:2012-10-31

    Applicant: SAAB AB

    Abstract: An aerial article including a composite skin, a leading edge facing an airflow during use of the aerial article, an erosion resistant coating including a metallic material, and an aerodynamic surface. The coating at least partly covers the composite skin of the aerial article. The coating has a porosity sufficiently high to provide an open area, diffusion passage way, so as to permit moisture transportation from the composite skin to the aerodynamic surface of the coating. A method of applying an erosion resistant coating including a metallic material to a composite skin of an aerial article. An erosion resistant coating material is provided onto the composite skin over a selected area of the article. The coating is porous. The outer surface of the coating is polished to achieve a smooth aerodynamic surface.

    Abstract translation: 包括复合皮肤的空中物品,在使用空中物品期间面向气流的前缘,包括金属材料的抗侵蚀涂层和空气动力学表面。 该涂层至少部分地覆盖空中物品的复合皮肤。 涂层具有足够高的孔隙以提供开放区域,扩散通道的方式,以便允许水分从复合表皮输送到涂层的空气动力学表面。 将包含金属材料的耐侵蚀涂层施加到空中物品的复合表皮的方法。 在制品的选定区域上的复合皮肤上提供抗侵蚀涂层材料。 涂层是多孔的。 抛光涂层的外表面以实现平滑的空气动力学表面。

    METHOD AND A SYSTEM FOR BUILDING A THREE-DIMENSIONAL MODEL FROM SATELLITE IMAGES
    43.
    发明申请
    METHOD AND A SYSTEM FOR BUILDING A THREE-DIMENSIONAL MODEL FROM SATELLITE IMAGES 有权
    用于从卫星图像建立三维模型的方法和系统

    公开(公告)号:US20150243072A1

    公开(公告)日:2015-08-27

    申请号:US14188454

    申请日:2014-02-24

    Applicant: SAAB AB

    Abstract: The invention relates to a method for building a 3D model of an area of interest on the surface of a planet. The method comprises providing a plurality of 2D images from satellites, where each 2D image out of the plurality of 2D images at least partly covers the area of interest. Also, each subarea of the area of interest is covered by at least two images, taken from different angles, out of the plurality of 2D images. Bundle adjustments are performed for the plurality of 2D images and the area of interest is divided into parts. For each part of the area of interest at least one combination and preferably all possible combinations out of two images covering that part of the area of interest are taken. Said two images are taken from the at least two images, taken from at least two different angles, out of the plurality of 2D images. Further, for each part of the area, point matching correspondence is established for a set of points for each such combination of two images. The sets of points are combined if more than one set of points exists. Even further, for each part of the area, a 3D model of said part of the area of interest is built based on the combined set of points. The 3D models from each part of the area of interest are combined to a 3D model of the whole area of interest. The invention also relates to a system, a computer program and a computer program product.

    Abstract translation: 本发明涉及一种在行星表面上建立感兴趣区域的3D模型的方法。 该方法包括从卫星提供多个2D图像,其中多个2D图像中的每个2D图像至少部分地覆盖感兴趣的区域。 此外,感兴趣区域的每个子区域由多个2D图像中的不同角度的至少两个图像覆盖。 对多个2D图像执行束调整,并且将感兴趣的区域分成多个部分。 对于感兴趣区域的每个部分至少一个组合,并且优选地采用覆盖感兴趣区域的那部分的两个图像中的所有可能的组合。 从多个2D图像中的至少两个不同的角度取出所述两个图像。 此外,对于该区域的每个部分,针对两个图像的每个这样的组合的一组点建立点匹配对应。 如果存在多个点集合,则组合点组合。 更进一步地,对于该区域的每个部分,基于组合的点来构建所述感兴趣区域的所述部分的3D模型。 来自感兴趣区域的每个部分的3D模型被组合到感兴趣的整个区域的3D模型。 本发明还涉及一种系统,计算机程序和计算机程序产品。

    CALCULATING TIME TO GO AND SIZE OF AN OBJECT BASED ON SCALE CORRELATION BETWEEN IMAGES FROM AN ELECTRO OPTICAL SENSOR
    44.
    发明申请
    CALCULATING TIME TO GO AND SIZE OF AN OBJECT BASED ON SCALE CORRELATION BETWEEN IMAGES FROM AN ELECTRO OPTICAL SENSOR 有权
    基于来自电光传感器的图像之间的尺度相关的计算对象的大小和尺寸

    公开(公告)号:US20140278048A1

    公开(公告)日:2014-09-18

    申请号:US14289201

    申请日:2014-05-28

    Applicant: SAAB AB

    Inventor: Jimmy Jonsson

    CPC classification number: G08G5/045 G06K9/00805 G08G5/0021

    Abstract: A method for calculating a Time To Go value between a vehicle and an intruding object. First and second images of the object are retrieved at first and second points of time. A scaling factor is selected and the second image scaled with the scale factor. The scaled image is resampled to a set position. Correlation values are calculated between the first image and the resampled scaled image for different horizontal displacements and/or different vertical displacements for the resampled scaled image. A maximum correlation value is found based on the correlation values. Selecting the scaling factor, resampling, calculating the correlation values, and finding the maximum correlation values are repeated a second predetermined number of times. A largest maximum correlation value is found among the maximum correlation values and the scale factor associated with the largest maximum correlation value. The Time To Go is calculated based on the associated scale factor.

    Abstract translation: 一种用于计算车辆和入侵物体之间的“到达时间”值的方法。 在第一和第二时间点检索对象的第一和第二图像。 选择缩放因子,第二个图像用比例因子缩放。 缩放图像被重新采样到设置位置。 对于不同的水平位移和/或重采样的缩放图像的不同垂直位移,在第一图像和重采样的缩放图像之间计算相关值。 基于相关值找到最大相关值。 选择缩放因子,重采样,计算相关值和找到最大相关值重复第二预定次数。 在最大相关值和与最大最大相关值相关联的比例因子之间找到最大最大相关值。 Time to Go是根据相关的比例因子计算的。

    VALIDITY CHECK OF VEHICLE POSITION INFORMATION
    45.
    发明申请
    VALIDITY CHECK OF VEHICLE POSITION INFORMATION 审中-公开
    车辆位置信息的有效性检查

    公开(公告)号:US20140070979A1

    公开(公告)日:2014-03-13

    申请号:US14078061

    申请日:2013-11-12

    Applicant: SAAB AB

    Abstract: A method for validating received positional data in vehicle surveillance applications. A signal carrying a Mode S ES message including positional data indicating an alleged position of a vehicle, transmitted from a radio source is received with a radio direction finding antenna of a receiver. A bearing from the receiver to the radio source is estimated utilizing the radio direction finding antenna and received signal. A distance between the receiver and radio source based on a time of flight for a signal travelling between the receiver and radio source at known speed is estimated with a distance measurer including primary radar, laser detector and ranger, and/or secondary surveillance radar. An estimated position of the radio source is calculated based on the estimated bearing and distance. A deviation value indicating a deviation/coincidence between the alleged position is determined according to the received and estimated position of the radio source.

    Abstract translation: 一种在车辆监控应用中验证接收到的位置数据的方法。 使用接收机的无线电测向天线接收携带包括从无线电源发送的指示车辆的位置的位置数据的模式S ES消息的信号。 使用无线电测向天线和接收信号来估计从接收机到无线电源的方位。 基于用于以已知速度在接收机和无线电源之间行进的信号的飞行时间的接收器和无线电源之间的距离通过包括主雷达,激光检测器和巡航器和/或次级监视雷达的距离测量器来估计。 根据估计的方位和距离计算无线电源的估计位置。 根据无线电源的接收和估计位置确定指示所述位置之间的偏差/重合的偏差值。

    Vehicle track block signal apparatus
    46.
    发明授权
    Vehicle track block signal apparatus 失效
    车辆跟踪块信号装置

    公开(公告)号:US3638014A

    公开(公告)日:1972-01-25

    申请号:US3638014D

    申请日:1969-09-22

    Applicant: SAAB AB

    CPC classification number: B61L13/047

    Abstract: The condition of a signal for each block of vehicle track corresponds to that of a bistable memory unit placed in one condition by momentary output of an arrival detector and in its other condition by momentary output of a departure detector. All detectors are actuated by a single type of vehicle-carried exciter. An arrival detector is located near each end of each block. A departure detector is spaced along the track from each arrival detector, in the direction away from the other arrival detector.

    Abstract translation: 车辆轨道的每个块的信号的条件对应于通过到达检测器的瞬时输出置于一个状态的双稳态存储器单元的条件,并且在其它条件下通过离场检测器的瞬时输出。 所有检测器都由单一类型的车载激励器启动。 到达检测器位于每个块的每一端附近。 离开检测器沿着远离另一到达检测器的方向沿着轨道从每个到达检测器间隔开。

    Forming apparatus for hydraulic press
    48.
    发明授权
    Forming apparatus for hydraulic press 失效
    液压机成型设备

    公开(公告)号:US3635061A

    公开(公告)日:1972-01-18

    申请号:US3635061D

    申请日:1969-12-05

    Applicant: SAAB AB

    CPC classification number: B21D22/205

    Abstract: In a hydraulic forming tool of the diaphragm type, the punch and the work holder or die member are rigidly mounted on separate pistons that move in communicated cylinders, so that downward movement of one effects upward movement of the other by reason of displacement of fluid from the bottom of one of said cylinders to the bottom of the other. Adequate forming force is assured by metering outflow of fluid from the upper portion of the cylinder having the upgoing piston.

    Abstract translation: 在隔膜式的液压成形工具中,冲头和工件保持器或模具构件刚性地安装在在连通的气缸中移动的单独的活塞上,使得一个的向下运动由于流体从 一个所述气缸的底部到另一个的底部。 通过计量流体从具有上活塞的气缸的上部流出来确保足够的成形力。

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