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    AIRCRAFT WITH DETACHABLE WINGS
    161.
    发明公开
    AIRCRAFT WITH DETACHABLE WINGS 有权
    FLUGZEUG MIT ABNEHMBARENFLÜGELN

    公开(公告)号：EP2903892A1

    公开(公告)日：2015-08-12

    申请号：EP13763040.6

    申请日：2013-09-13

    Applicant: Sensefly S.A.

    Inventor： BEYELER, Antoine ,  KLAPTOCZ, Adam ,  ROBERTS, James F. ,  ZIMMERMANN, Loic ,  ZUFFEREY, Jean-Christophe ,  LAZZARATTO-PINÖSCH, Andreas

    IPC: B64C1/26

    CPC classification number: B64C1/26 ,  B64C39/024 ,  B64C39/10 ,  B64C2201/028 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/162 ,  B64C2201/187 ,  B64C2201/20

    Abstract: This invention relates to a connection set that is used to attach and transfer force and torque between a wing (2a, 2b), comprising a lifting surface and a control surface (9) connected together by a hinge, and the central body (1) of an aircraft, which contains a servo-motor (10) used for actuating said control surface (9). The wing (2a, 2b) is connected to the central body (1) using a connection set comprised of two components. First, an attachment mechanism (3, 4, 5, 6) is used to align the wings (2a, 2b) relative to the central body (1) and to transfer the aerodynamic forces acting on the wing (2a, 2b) to the central body (1), preventing the wing (2a, 2b) from bending at its connection point. Second, a torque coupling mechanism (7, 8) is used to actuate the control surfaces that are present on the wings using servomotors (10) that are embedded within the central body (1). The connection set is engaged and disengaged using a single motion and does not require additional connection of electrical cables or mechanical fixations.

    Abstract translation: 本发明涉及一种用于在包括提升表面和通过铰链连接在一起的控制表面（9）的翼（2a，2b）之间附接和传递力和扭矩的连接组，以及中心体（1） 其包含用于致动所述控制表面（9）的伺服电动机（10）。 翼（2a，2b）使用由两个部件组成的连接组件连接到中心体（1）。 首先，使用附接机构（3,4,5,6）来相对于中心体（1）对准翼（2a，2b）并将作用在机翼（2a，2b）上的空气动力传递到 中心体（1），防止机翼（2a，2b）在其连接点处弯曲。 第二，扭矩联接机构（7,8）用于使用嵌入在中心体（1）内的伺服电动机（10）致动存在于机翼上的控制表面。 连接组使用单一动作进行接合和分离，不需要额外连接电缆或机械固定。

    UNMANNED AERIAL VEHICLE AND METHOD OF LAUNCHING
    162.
    发明公开
    UNMANNED AERIAL VEHICLE AND METHOD OF LAUNCHING 有权
    UNBEMANNTES LUFTFAHRZEUG UND ABSCHUSSVERFAHRENDAFÜR

    公开(公告)号：EP2874875A1

    公开(公告)日：2015-05-27

    申请号：EP13742690.4

    申请日：2013-07-19

    Applicant: Elson, Andrew Charles

    Inventor： Elson, Andrew Charles

    IPC: B64D5/00 ,  B64C39/02

    CPC classification number: B64D5/00 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/162 ,  B64C2201/187 ,  B64D2211/00

    Abstract: A method of launching a powered unmanned aerial vehicle, the method comprising lifting the vehicle by attachment to a lighter-than-air carrier from a substantially ground-level location to an elevated altitude, wherein the vehicle is prevented from entering its flight mode during ascent, causing the vehicle to detach from the carrier while the velocity of the vehicle relative to the carrier is substantially zero, the vehicle thereafter decreasing in altitude as it accelerates to a velocity where it is capable of preventing any further descent and can begin independent sustained flight.

    Abstract translation: 一种在至少13000米的高度上发射供电的无人驾驶飞行器的方法，所述方法包括通过将空载承载器从基本上地平面的位置附近提升到升高的高度，使得车辆 当车辆相对于承运人的速度基本上为零时，车辆离开载体，然后车辆随着其高度减小到能够防止任何进一步下降并且可以开始独立的持续飞行的速度。

    GROUND-BASED VIDEOMETRICS GUIDING METHOD FOR AIRCRAFT LANDING OR UNMANNED AERIAL VEHICLES RECOVERY
    166.
    发明公开
    GROUND-BASED VIDEOMETRICS GUIDING METHOD FOR AIRCRAFT LANDING OR UNMANNED AERIAL VEHICLES RECOVERY 审中-公开
    陆基视频梅特赖克领导程序飞机的着陆或回从无人驾驶飞机

    公开(公告)号：EP2413096A1

    公开(公告)日：2012-02-01

    申请号：EP09842038.3

    申请日：2009-03-27

    Applicant: Yu, Qifeng

    Inventor： LEI, Zhihui ,  ZHANG, Xiaohu ,  SHANG, Yang ,  ZHANG, Heng ,  ZHOU, Xiang

    IPC: G01C11/00 ,  G01C21/00 ,  G01C11/04 ,  G01C21/10

    CPC classification number: G01C11/00 ,  B64C2201/187 ,  G01C21/10 ,  G01S5/16 ,  G05D1/0676 ,  G08G5/0026 ,  G08G5/025

    Abstract: The present invention provides a ground-based camera surveying and guiding method for aircraft landing and unmanned aerial vehicle recovery based on the camera surveying technology, which is a ground-based camera surveying and guiding system mainly including several video cameras arranged near the landing areas of an aircraft or an unmanned aerial vehicle. During the approaching process of the aircraft or the unmanned aerial vehicle, the system performs imaging of the aircraft in real time and detects movement parameters such as the track, velocity, acceleration, attitude and the offset relative to the glide slope of the aircraft or the unmanned aerial vehicle in real time by analyzing images and applying camera surveying method and technology, so as to provide guidance for aircraft landing or unmanned aerial vehicle recovery. The method is an autonomic guiding survey without interferences from others, which has high accuracy and reliability. The hardware devices are mature, simple and have low cost. The devices are moveable and versatile, and can be used in aircraft landing aid, unmanned aerial vehicle recovery and the like.

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