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    공간영상도화용 이미지를 확보하는 드론 시스템
    32.
    发明授权
    공간영상도화용 이미지를 확보하는 드론 시스템 有权
    Dron系统保护图像进行空间图像映射

    公开(公告)号：KR101833920B1

    公开(公告)日：2018-04-13

    申请号：KR1020170137587

    申请日：2017-10-23

    Applicant: (주)지스페이스코리아

    Inventor： 김태연

    IPC: B64C39/02 ,  B64B1/40 ,  B64B1/62

    CPC classification number: B64C39/024 ,  B64B1/40 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/024 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/145

    Abstract: 본발명은기촬영된항공촬영이미지와연결되기위한국소적인촬영이미지를드론을통해공중에서효율적으로획득할수 있으며, 해당드론이촬영시에는추력을정지시켜떨림없이보다정확하고선명한촬영이미지를획득할수 있는공간영상도화용이미지를확보하는드론시스템에관한것으로서, 본발명에따른공간영상도화용이미지를확보하는드론시스템은드론및 무추력촬영서포트장치를포함하여구성되며, 드론은영상도화작업을위한촬영이미지를공중에서획득하는기능을하고, 무추력촬영서포트장치는드론을통한촬영이미지의획득작업이드론의추력이정지된상태에서진행될수 있게하는기능을하는것으로서, 이러한무추력촬영서포트장치는드론을통한촬영이미지의획득을위해사전에정해지는여러위치에각각설치된다.

    Abstract translation: 本发明是基于，并且可以获得一个集中式的图像要被记录在有效地通过所述无人驾驶飞机的空气连接到所记录的图像的空气，无人驾驶飞机能够获得没有一个更精确和锐利记录的图像，颤动阻止推力拍摄 根据本发明的用于保护用于空间图像映射的图像的dron系统包括无人驾驶飞机和无推力拍摄支持装置。无人驾驶飞机用于图像绘制操作 无推力拍摄支持设备具有通过无人机获取拍摄图像的功能，使得无人机的宝座能够以停止状态进行。 安装在各种预定位置以便通过无人机获取拍摄的图像。

    BUOYANT FLYING BODY
    39.
    发明公开
    BUOYANT FLYING BODY 审中-公开
    SCHWIMMFÄHIGERFLUGKÖRPER

    公开(公告)号：EP3150483A4

    公开(公告)日：2017-09-20

    申请号：EP16811654

    申请日：2016-06-15

    Applicant: NAKAMURA KOHEI

    Inventor： NAKAMURA KOHEI

    IPC: B64B1/30 ,  B64B1/58 ,  B64C25/06 ,  B64C27/08 ,  B64C39/02

    CPC classification number: B64B1/30 ,  B64B1/58 ,  B64C25/06 ,  B64C27/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/127

    Abstract: Provided is a buoyant aerial vehicle which can secure high safety by reducing the risk of crashing, and which can facilitate control of movement by suppressing the influence of wind and exhibit high mobility capability. The buoyant aerial vehicle is configured by including: a buoyant vehicle body in which gas having a specific gravity smaller than air is hermetically filled; a vertical propulsion propeller which provides vertical propulsive force to the buoyant vehicle body; and a horizontal propulsion propeller which provides horizontal propulsive force to the buoyant vehicle body, and is configured such that the buoyant vehicle body has horizontal wind passages formed in at least two directions, and has outer peripheral edges each formed into an acute angle in side view.

    Abstract translation: 本发明提供一种浮力飞行器，其能够通过降低碰撞风险来确保较高的安全性，并且能够通过抑制风的影响来促进对运动的控制，并且具有高运动能力。 所述浮力飞行器通过包括：浮力车体，在所述浮力车体中气密地填充比重小于空气的气体; 向浮力车体提供垂直推进力的垂直推进螺旋桨; 以及向浮力车体提供水平推进力的水平推进螺旋桨，并且浮力车体具有形成在至少两个方向上的水平风道，并且具有在侧视图中形成为锐角的外周边缘 。

    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM
    40.
    发明公开
    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM 审中-公开
    图像和/或无线电信号捕获平台

    公开(公告)号：EP3169974A2

    公开(公告)日：2017-05-24

    申请号：EP15757339.5

    申请日：2015-07-17

    Applicant: Altec S.p.A.

    Inventor： MUSSO, Ivano

    IPC: G01C11/02 ,  G03B15/00 ,  G01W1/08

    CPC classification number: G01W1/08 ,  B63B35/00 ,  B64C2201/022 ,  B64C2201/125 ,  B64C2201/127 ,  B64D1/12 ,  B64D47/08 ,  G01C11/02 ,  G01S13/953 ,  G01S13/956 ,  G03B15/006 ,  G03B17/08 ,  G03B17/561 ,  H04N5/2252 ,  H04N5/23238 ,  H04N7/18

    Abstract: Platform (100; 200, 200′, 200″) configured to acquire images and/or radio signals and to be carried by lightweight aviation aircrafts, characterised in that it comprises housing means (1, 3; 22, 201, 202, 203, 31) that houses one or more acquisition sensors selected from the group comprising or consisting of cameras (5; 51; 32) configured to acquire still and/or moving images and radio signal receivers (62; 34) configured to acquire radio signals, said housing means (1, 3; 22, 201, 202, 203, 31) being configured to be coupled to a light aviation aircraft (540), said one or more acquisition sensors (5; 51; 32; 62; 34) being connected to processing means (6; 23) configured to receive sensing data from a position and motion sensing unit (10; 230) coupled to said one or more acquisition sensors (5; 51; 32; 62; 34), said processing means (6; 23) being configured to control and/or program, on the basis of the received sensing data, each acquisition sensor (5; 51; 32; 62; 34) so as to enable the same to acquire images and/or radio signals when such acquisition sensor (5; 51; 32; 62; 34) is in a determined position and is subject to oscillations having a velocity that is not larger in absolute value than a maximum oscillation velocity value, whereby a rate of variation of an actual aiming of such acquisition sensor (5; 51; 32; 62; 34) is not larger in absolute value than a respective maximum value of rate of variation of offset with respect to an ideal aiming at a target, so as to ensure focusing of such acquisition sensor (5; 51; 32; 62; 34) on an aimed area.

    Abstract translation: 被配置为获取图像和/或无线电信号并由轻型航空飞机携带的平台（100; 200,200'，200“），其特征在于，所述平台包括壳体装置（1,3; 31），其容纳从被配置为获取静止和/或运动图像的摄像机（5; 51; 32）或被配置为获取无线电信号的无线电信号接收器（62; 34）组成的组中选择的一个或多个采集传感器，所述 所述一个或多个采集传感器（5; 51; 32; 62; 34）被连接到所述轻型航空飞行器（540），所述一个或多个采集传感器（5; 51; 32; 62; 34） （6; 23），所述处理装置被配置为从耦合到所述一个或多个采集传感器（5; 51; 32; 62; 34）的位置和运动感测单元（10; 230）接收感测数据，所述处理装置 ; 23）被配置为基于所接收的感测数据来控制和/或编程每个获取传感器（5; 51; 32; 62; 34）以便启用 当这样的采集传感器（5; ...）获取图像和/或无线电信号时， 51; 32; 62; 34）处于确定的位置并且受到具有绝对值不大于最大振荡速度值的速度的振动，由此这种获取传感器（5; 51; 32; 62）的实际瞄准的变化率 ; 34）的绝对值不大于相对于理想瞄准目标的偏移量变化率的相应最大值，以确保这种采集传感器（5; 51; 32; 62; 34）的聚焦， 在目标区域。

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