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    METHOD OF USING A DEVICE CAPABLE OF CONTROLLED FLIGHT
    71.
    发明申请
    METHOD OF USING A DEVICE CAPABLE OF CONTROLLED FLIGHT 审中-公开
    使用可控制飞行器的装置的方法

    公开(公告)号：WO2015169931A9

    公开(公告)日：2016-01-21

    申请号：PCT/EP2015060128

    申请日：2015-05-07

    Applicant: IMP INNOVATIONS LTD

    Inventor： KOVAC MIRKO ,  ALHINAI TALIB MUHAMMAD TALIB

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C25/00 ,  B64C39/02 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/146 ,  B64C2201/18 ,  B64D2211/00 ,  G05D1/104

    Abstract: There is provided a method of using a device capable of controlled flight in a surrounding environment, the device comprising: lifting means for providing lift to the device; object-retaining means for holding an object to be affixed to a target site; and a dispensing assembly for dispensing an adhesive, wherein the method comprises: controlling the lifting means so as to controllably fly the device in the surrounding environment; and using the device to affix an object held by the object-retaining means to a target site in the surrounding environment by dispensing an adhesive from the dispensing assembly. Thus, an aerial device, for example a robotic device, may be used to fly to a desired location and affix an object at the desired location, by dispensing, ejecting or otherwise applying an adhesive.

    Abstract translation: 提供了一种使用能够在周围环境中控制飞行的装置的方法，该装置包括：提升装置，用于向装置提供电梯; 用于保持待贴在目标地点上的物体的物体保持装置; 以及用于分配粘合剂的分配组件，其中所述方法包括：控制所述提升装置，以便在所述周围环境中可控地飞行所述装置; 并且使用该装置通过从分配组件分配粘合剂来将由对象保持装置保持的对象附加到周围环境中的目标位置。 因此，例如机器人装置的空中装置可以用于飞行到期望的位置，并通过分配，喷射或以其它方式施加粘合剂将物体附着在所需位置。

    METHODS FOR LAUNCHING AND LANDING AN UNMANNED AERIAL VEHICLE
    72.
    发明申请
    METHODS FOR LAUNCHING AND LANDING AN UNMANNED AERIAL VEHICLE 审中-公开
    启动和着陆无人驾驶飞机的方法

    公开(公告)号：WO2015085598A1

    公开(公告)日：2015-06-18

    申请号：PCT/CN2013/089443

    申请日：2013-12-13

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： WANG, Ming-yu

    IPC: B64C13/18

    CPC classification number: G05D1/0669 ,  A63H27/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/08 ,  G05D1/0011 ,  G05D1/0676

    Abstract: Methods and apparatus are provided for launching and landing unmanned aerial vehicles (UAVs) including multi-rotor aircrafts. The methods and apparatus disclosed herein utilize positional change of the UAV, visual signal, or other means to effect the launch or landing. The methods and apparatus disclosed herein are user friendly, particularly to amateur UAV users lacking practice of operating a UAV.

    Abstract translation: 提供了包括多转子飞机在内的无人机（UAV）发射和着陆的方法和装置。 本文公开的方法和装置利用无人机，视觉信号或其他方式的位置变化来实现发射或着陆。 本文公开的方法和装置是用户友好的，特别是对于没有操作无人机的操作的业余无人机的用户。

    UNMANNED AERIAL SYSTEMS
    73.
    发明申请
    UNMANNED AERIAL SYSTEMS 审中-公开
    无人机系统

    公开(公告)号：WO2014058510A2

    公开(公告)日：2014-04-17

    申请号：PCT/US2013/051959

    申请日：2013-07-25

    Applicant: BYE UAS, INC. ,  BYE, George ,  BICKEL, Matt

    Inventor： BYE, George ,  BICKEL, Matt

    IPC: B64C19/02

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/126 ,  B64C2201/165 ,  B64C2201/167 ,  B64C2201/185 ,  B64C2211/00

    Abstract: The present invention provides an Unmanned Aircraft System, including an integrated unmanned aerial vehicle and all related components and subsystems that can be packaged and transported as a kit, and customized to fit desired mission profiles, and easily repaired by replacement of damaged components or subsystems. The present invention further provides unmanned aircraft system components and subsystems that facilitate low power and low noise operation, and extended flight times.

    Abstract translation: 本发明提供了一种无人驾驶飞机系统，其包括集成的无人驾驶飞行器以及可以作为套件来包装和运输的所有相关部件和子系统，并且定制以适应期望的任务轮廓并且易于修理 通过更换损坏的部件或子系统。 本发明还提供了有助于低功率和低噪音操作以及延长飞行时间的无人驾驶飞机系统部件和子系统。

    LAUNCH TUBE RESTRAINT SYSTEM FOR UNMANNED AERIAL VEHICLE (UAV)
    74.
    发明申请
    LAUNCH TUBE RESTRAINT SYSTEM FOR UNMANNED AERIAL VEHICLE (UAV) 审中-公开
    无人机（UAV）发射管约束系统

    公开(公告)号：WO2013126111A2

    公开(公告)日：2013-08-29

    申请号：PCT/US2012/067086

    申请日：2012-11-29

    Applicant: AEROVIRONMENT, INC. ,  SU, Guan ,  RODRIGUEZ, Marcos

    Inventor： SU, Guan ,  RODRIGUEZ, Marcos

    IPC: B64C1/22

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/084 ,  B64C2201/088 ,  B64C2201/201 ,  B64F1/06 ,  F41B11/80 ,  F41F3/00 ,  F41F3/042 ,  F41F3/052 ,  F41F3/073

    Abstract: An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV (400) having an exterior surface, an aerial vehicle (AV) tab (510) extending from the exterior surface, a tube (440) containing the UAV (400), the tube (440) including a tab stop (515) configured to controllably hinder travel of the AV tab (510) past the tab stop (515), and a pair of opposing tab guides (700, 705) configured to position the AV tab (510) for travel over the tab stop (515).

    Abstract translation: 公开了一种无人驾驶飞行器（UAV）发射设备，其包括具有外表面的UAV（400），从外表面延伸的飞行器（AV）突片（510），管 （440），所述管（440）包括配置成可控制地阻碍所述AV突片（510）经过所述突片止挡件（515）的行程的突片止挡件（515），以及一对相对的突片引导件 700），其被配置为定位AV标签（510）以在标签止挡（515）上行进。

    NOISE SUPPRESSION DEVICE FOR A DRONE LAUNCH TUBE
    76.
    发明授权
    NOISE SUPPRESSION DEVICE FOR A DRONE LAUNCH TUBE 有权

    公开(公告)号：EP3133019B1

    公开(公告)日：2018-12-05

    申请号：EP16179915.0

    申请日：2010-09-09

    Applicant: AeroVironment, Inc.

    Inventor： Miralles, Carlos Thomas ,  Andryukov, Alexander ,  Su, Guan H. ,  McNeil, John

    IPC: B64F1/04 ,  F41F3/04 ,  F41F1/06

    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).

    SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE
    79.
    发明公开
    SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE 审中-公开
    用于远程操作的无人机空中车辆报告的系统和装置 - 具有便携式射频透明发射管的压载式发射机

    公开(公告)号：EP3133019A1

    公开(公告)日：2017-02-22

    申请号：EP16179915.0

    申请日：2010-09-09

    Applicant: AeroVironment, Inc.

    Inventor： Miralles, Carlos Thomas ,  Andryukov, Alexander ,  Su, Guan H. ,  McNeil, John

    IPC: B64F1/04 ,  F41F3/04 ,  B64C13/20 ,  F42B39/14 ,  F41F1/00

    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: 一种无人飞行器（UAV）发射管（100），其包括围绕直角平行六面体孔（305）布置的至少一个预浸料坯基底（370）的内层，至少一个预浸料坯基底 （305）以及设置在所述至少一个预浸料坯衬底（340）的内层和所述至少一个预浸料坯衬底（380）的外层之间的一个或多个结构面板（341-344）。 1。一种无人驾驶飞行器（UAV）发射管（100），其包括被配置成在由内壁限定的发射器体积内接合UAV的系留弹底（700,740），所述系留弹壳（700,740）的尺寸被设计成在内部提供压力密封 （700,740）是中空的，具有朝向高压容积的开口端和连接在弹壳（700）的中空部（910）内并连接到所述内壁的系绳（740） 内壁保持高压容积或附接到内部基壁（1013）。 一种包括通信节点（1500-1505）和启动器（1520）的系统，所述通信节点（1500-1505）和启动器（1520）包括处于预启动状态的无人飞行器（UAV），其被配置为接收并响应来自通信节点（1500-1505）的命令输入。

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