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    SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE
    53.
    发明公开
    SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE 有权
    VerstärktesRohr zum katapultieren von Drohnen

    公开(公告)号：EP2475578A2

    公开(公告)日：2012-07-18

    申请号：EP10833731.2

    申请日：2010-09-09

    Applicant: AeroVironment, Inc.

    Inventor： MIRALLES, Carlos Thomas ,  SU, Guan H. ,  ANDRYUKOV, Oleksandr ,  MCNEIL, John

    IPC: B64F1/04 ,  F41F3/04 ,  B64C13/20

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/146 ,  B64C2201/201 ,  B64F1/06 ,  F41A21/02 ,  F41F1/00 ,  F41F3/042 ,  F42B39/14

    Abstract: An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505).

    Abstract translation: 一种无人驾驶飞行器（UAV）发射管（100），其包括围绕右平行六面体孔（305）设置的至少一个预浸料衬底内层（370），至少一个围绕右侧设置的预浸料衬底（380）外层 平行六面体孔和设置在至少一层预浸料衬底（340）的内层与至少一层预浸料衬底（380）之间的一个或多个结构面板（341-344）。 一种无人驾驶飞行器（UAV）发射管（100），其包括被构造成与在内壁限定的发射器体内接合无人机的拴系的膛体（700,740），所述拴系的炮（700,740）的尺寸设置成在内部提供压力密封 并且其中所述系绳式突破（700,740）是中空的，具有朝向高压容积定向的开口端和连接在所述破坏物（700）的中空部（910）内的系绳（740），并且附接到 所述内壁保持高压容积或附接到所述内底壁（1013）。 包括通信节点（1500-1505）和发射器（1520）的系统，其包括处于预发射状态的无人驾驶飞行器（UAV），其被配置为接收并响应来自通信节点（1500-1505）的命令输入。

    무인 비행체용 이륙 보조장치
    56.
    发明公开
    무인 비행체용 이륙 보조장치 有权

    公开(公告)号：KR1020180063616A

    公开(公告)日：2018-06-12

    申请号：KR1020160163572

    申请日：2016-12-02

    Applicant: 김성남

    Inventor： 김성남

    IPC: B64F1/04 ,  B64C39/02

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/08

    Abstract: 본발명은무인비행체용이륙보조장치에관한것으로, 그주된목적은무인비행체이륙시필요한양력(Lift, 위로들어올리는힘)과측면에서바람을받는측풍에영향받지않고안정적인이륙이이루어지도록함과동시에이륙이개시되는시점까지무인비행체의동체및 날개를확실하게고정함으로써비행체의안정된이륙을도모하는것이다. 이러한목적으로이루어진본 발명에따른무인비행체용이륙보조장치는, 견인차에피견인되며운행될수 있도록양측에바퀴를갖춘주행부와; 상기주행부의후방에무인비행체의몸체하부를고정할수 있도록구비되는고정장치와; 상기고정장치의선단양측에대칭형수직방향으로상기무인비행체의몸체상부를고정하도록구비되는록킹장치를포함한다. 이에따라, 본발명에따른무인비행체용이륙보조장치에의하면, 무인비행체이륙시필요한양력(Lift, 위로들어올리는힘)과측면에서바람을받는측풍에영향받지않고안정적인이륙이이루어지도록함과동시에이륙이개시되는시점까지무인비행체의동체및 날개를확실하게고정함으로써비행체의안정된이륙을도모하는이점이있다.

    드론 이륙 보조 시스템 및 이에 적용되는 분리장치
    57.
    发明公开
    드론 이륙 보조 시스템 및 이에 적용되는 분리장치 有权

    公开(公告)号：KR20180051246A

    公开(公告)日：2018-05-16

    申请号：KR20160148316

    申请日：2016-11-08

    Applicant: 한국항공우주연구원

    Inventor： AHN SEOK MIN ,  KIM JAE EUN ,  RYU HYEOK

    IPC: B64F1/08 ,  B64C39/02 ,  B64F3/00

    CPC classification number: B64F1/08 ,  B64C39/024 ,  B64C2201/08 ,  B64F3/00

    Abstract: 본발명의실시예에따른드론이륙보조시스템은드론(drone)의이륙단계시 상기드론을계류(繫留)하여상기드론의비정상적인비행을예방하는드론이륙보조시스템으로서, 이륙장소에설치되고, 외측으로연결부재가연장되는계류부, 그리고상기연결부재와상기드론을서로연결하고, 미리설정된조건에따라상기연결부재와상기드론을서로분리시키는분리장치를포함한다. 본발명에의하면, 드론이지면에대해수직으로이륙하고있고, 연결부재에일정크기이상의장력이걸릴경우에만연결부재와드론이서로분리되도록함으로써, 드론의이륙단계시 드론이설정위치를벗어나거나, 비정상적으로비행하는것을예방하고, 나아가드론의추락및 파손을방지하여드론에의한 2차적인피해발생을예방할수 있다.

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