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    ICING DETECTOR PROBE AND ICING DETECTOR WITH THE SAME
    4.
    发明公开
    ICING DETECTOR PROBE AND ICING DETECTOR WITH THE SAME 有权
    VEREISUNGSDETEKTORSONDE UND VEREISUNGSDETEKTOR DAMIT

    公开(公告)号：EP2594486A1

    公开(公告)日：2013-05-22

    申请号：EP11806272.8

    申请日：2011-06-30

    申请人： Commercial Aircraft Corporation Of China Ltd ,  Commercial Aircraft Corporation Of China Ltd Shanghai Aircraft Design and Research Institute ,  Huazhong University of Science and Technology

    发明人： CHEN, Yingchun ,  YE, Lin ,  ZHANG, Miao ,  GE, Junfeng ,  FENG, Lijuan ,  LIU, Tiejun ,  ZHOU, Feng

    IPC分类号： B64D15/20 ,  G08B19/02

    CPC分类号： B64D15/20

    摘要： An icing detector probe includes three sections arranged sequentially along the direction of air flow, namely, a first section (I), a second section (II) and a third section (III). Wherein, the shape of the outer surface of the first section (I) is suitable for collecting droplets in the air flow; the shape of the outer surface of the second section (II) is suitable for full decelerating and releasing latent heat of large droplets during their movements; the outer surface of the third section (III) is suitable for icing of large droplets. The probe could distinguish and identify large droplets icing, thus effectively detecting it. Furthermore, it could effectively detect types of traditional icing, thus being helpful for exact detection of icing thickness. An icing detector including said icing detector probe is also provided.

    摘要翻译： 结冰检测器探头包括沿空气流方向依次布置的三个部分，即第一部分（I），第二部分（II）和第三部分（III）。 其中，第一部分（I）的外表面的形状适合于在空气流中收集液滴; 第二部分（II）的外表面的形状适用于在大液滴运动期间完全减速和释放大液滴的潜热; 第三部分（III）的外表面适用于大液滴的结冰。 该探头可以区分和识别大型液滴结冰，从而有效地检测它。 此外，它可以有效地检测传统结冰的类型，从而有助于精确检测结冰厚度。 还提供了包括所述结冰探测器探头的结冰探测器。

    AIRCRAFT COCKPIT VIEW ENHANCING SYSTEM AND METHOD
    6.
    发明公开
    AIRCRAFT COCKPIT VIEW ENHANCING SYSTEM AND METHOD 审中-公开
    飞机驾驶舱查看增强系统和方法

    公开(公告)号：EP3291170A1

    公开(公告)日：2018-03-07

    申请号：EP16863620.7

    申请日：2016-11-09

    申请人： Commercial Aircraft Corporation Of China Ltd ,  Commercial Aircraft Corporation Of China Ltd Shanghai Aircraft Design and Research Institute

    发明人： JIN, Ding

    IPC分类号： G06T3/00

    摘要： An aircraft cockpit view enhancing system and method. The aircraft cockpit view enhancing system comprises: a central camera device (CC), a left camera device (LC), and a right camera device (RC), the central camera device (CC) being arranged between a driver eye site (E) and an aircraft windshield force column and having the shooting angle directly facing the aircraft windshield force column, and the left camera device (LC) and the right camera device (RC) being respectively arranged at the left side and the right side of the aircraft windshield force column and having the shooting angles respectively pointed and deflected to the right side and the left side of the aircraft windshield force column; an image processing device, used for performing image synthesis and image matching on a correct image, a left image and a right image shot by the central camera device (CC), the left camera device (LC) and the right camera device (RC), and acquiring an image of a shielding zone of the aircraft windshield force column; and a display device, used for displaying the image of the shielding zone of the aircraft windshield force column. The aircraft cockpit view enhancing system and method are able to accurately display an image of a shielding zone of a windshield force column and eliminate the defect of shielding the view of a cockpit by the windshield force column.

    摘要翻译： 飞机驾驶舱视图增强系统和方法。 所述飞机驾驶舱视野增强系统包括：中央摄像装置（CC），左侧摄像装置（LC）和右侧摄像装置（RC），所述中央摄像装置（CC）布置在驾驶员眼部位置（E） 和飞机挡风玻璃力柱，并且具有直接面向飞机挡风玻璃力柱的拍摄角度，并且左侧摄像机装置（LC）和右侧摄像机装置（RC）分别布置在飞机挡风玻璃的左侧和右侧 并将拍摄角度分别指向并偏转至飞机风挡力柱的右侧和左侧; 图像处理装置，用于对中央摄像装置（CC），左侧摄像装置（LC）和右侧摄像装置（RC）拍摄的正确图像，左侧图像和右侧图像进行图像合成和图像匹配， 并且获取所述飞机挡风玻璃推力柱的屏蔽区域的图像; 和显示装置，用于显示飞机挡风玻璃力柱的屏蔽区域的图像。 该飞机驾驶舱视野增强系统和方法能够准确地显示挡风玻璃受力柱的遮蔽区域的图像，并消除由挡风玻璃受力柱遮挡驾驶舱视野的缺陷。

    AIRPLANE WING ASSEMBLY
    10.
    发明公开
    AIRPLANE WING ASSEMBLY 审中-公开
    FLUGZEUGFLÜGELANORDNUNG

    公开(公告)号：EP3130534A1

    公开(公告)日：2017-02-15

    申请号：EP15846306.7

    申请日：2015-09-29

    申请人： Commercial Aircraft Corporation Of China Ltd ,  Commercial Aircraft Corporation Of China Ltd Shanghai Aircraft Design and Research Institute ,  Shanghai Aircraft Manufacturing Co., Ltd

    发明人： LIAN, Wei ,  LI, Ming ,  LIU, Jiangang ,  WENG, Chentao ,  SHEN, Dehong ,  LIU, Yankai ,  HE, Rui ,  ZHANG, Yuanqing ,  XU, Mengmeng

    IPC分类号： B64C3/52

    CPC分类号： B64C23/069 ,  B64C3/187 ,  B64C3/52 ,  B64F5/00 ,  Y02T50/164

    摘要： The present disclosure provides an aircraft wing assembly, comprising: an aircraft wing having a wing box; a winglet disposed at a wing tip of the aircraft wing, the winglet being connected to the aircraft wing through the wing box; a connection comprises a joint rib for assembling with the wing box and a central joint for assembling with the winglet, wherein the joint rib has a first shearing pin's hole and a second shearing pin's hole, for being pressed into corresponding first and second shearing pins to form an interference fit, respectively; the central joint has a first bushing hole and a second bushing hole, for being pressed into corresponding first and second bushings to form an interference fit; a positional relationship between the first shearing pin's hole and the second shearing pin's hole is identical to a positional relationship between the first bushing hole and the second bushing hole, such that when the winglet assembled with the central joint moves towards the wing box assembled with the joint rib, and when the first and second shearing pins are inserted into the first bushing hole and the second bushing hole on the center joint, respectively, small clearance fit is achieved between the first and second shearing pins and between the first and second bushings, respectively.

    摘要翻译： 本公开提供了一种飞机机翼组件，包括：具有翼盒的飞机机翼; 设置在飞行器机翼的翼尖处的小翼，小翼通过翼盒连接到飞机机翼; 连接件包括用于与翼盒组装的接合肋和用于与小翼组装的中心接头，其中所述接合肋具有第一剪切销孔和第二剪切销孔，用于压入相应的第一和第二剪切销 分别形成干涉配合; 中心接头具有第一衬套孔和第二衬套孔，用于压入相应的第一和第二衬套以形成过盈配合; 第一剪切销孔和第二剪切销孔之间的位置关系与第一衬套孔和第二衬套孔之间的位置关系相同，使得当与中心接合件组装的小翼朝向与组件 并且当第一和第二剪切销分别插入中心接头上的第一衬套孔和第二衬套孔中时，在第一和第二剪切销之间以及在第一和第二衬套之间实现小的间隙配合， 分别。