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    KR102226991B1 - Fire fighter drone employing launching device grenade-shaped extinguisher for emergency fire suppression
    51.
    发明专利
    KR102226991B1 - Fire fighter drone employing launching device grenade-shaped extinguisher for emergency fire suppression 有权

    公开(公告)号：KR102226991B1

    公开(公告)日：2021-03-12

    申请号：KR1020190103766A

    申请日：2019-08-23

    Applicant: 주식회사 유시스

    Inventor： 안성호

    IPC: B64C39/02 ,  A62C3/02 ,  B64D1/06

    CPC classification number: B64C39/024 ,  A62C3/025 ,  B64D1/06 ,  B64C2201/121

    Abstract: 실시예는 긴급화재진압을 위한 소화탄 발사기를 적용한 소방용 드론에 관한 것이다.
    구체적으로, 이러한 드론은 화재가 발생될 시, 상기 드론의 일단에 구비되어 압축 가스의 밸브로부터 개폐를 수행함으로써 압축 가스에 의해 장전된 소화탄을 선택적으로 타켓 위치에 발사하는 소화탄 발사기를 구비한다.
    그리고, 상기 압축 가스의 밸브에 대한 개폐가 수행될 시, 드론 기체의 배터리로부터 전원을 선택적으로 상기 압축 가스의 밸브에 공급함으로써 상기 소화탄 발사기의 압축 가스에 의해 장전된 소화탄 발사가 되도록 하는 전원부를 구비한다.
    그래서, 제어유닛이 GCS의 소화탄 발사 제어 신호에 따라 상기 전원부의 전원을 선택적으로 공급하도록 함으로써 사용자가 원하는 바에 따라 상기 소화탄 발사기의 압축 가스에 의해 장전된 소화탄 발사가 이루어지도록 하는 것을 특징으로 한다.
    따라서, 이를 통해 기존의 유인 대응체계가 가진 소방현장에서의 상황정보 획득 한계를 극복하기 위한 첨단장비인 드론이 영상정보 획득뿐만 아니라 화재 현장에서의 소화 능력까지 갖춘다.

    ADMINISTRATION OF SUBSTANCES TO ANIMALS
    55.
    发明申请
    ADMINISTRATION OF SUBSTANCES TO ANIMALS 审中-公开
    对动物的管理

    公开(公告)号：WO2018033812A1

    公开(公告)日：2018-02-22

    申请号：PCT/IB2017/054434

    申请日：2017-07-21

    Applicant: UAS FLIGHTEC SYSTEMS (PROPRIETARY) LIMITED ,  VISAGIE, Pieter, Johan

    Inventor： SMIT, Jacobus, Petrus ,  SMIT, Timo

    IPC: B64C39/02 ,  B64C99/00

    CPC classification number: B64C39/024 ,  A61D7/00 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/146

    Abstract: An unmanned aerial vehicle substance administration payload (10) includes a mounting (12) configured to mount to an unmanned aerial vehicle capable of hovering (a UAV). A magazine (14) is configured to hold at least one unguided free-fall projectile (16) configured to administer a substance to an animal upon impact with the animal. The magazine (14) is carried by the mounting (12). A release mechanism (18) is provided to release the unguided free-fall projectile (16) from the magazine (14) so that the projectile (16) can drop under the force of gravity from the magazine (14) to a target animal directly below the magazine (14). Aiming means (20) is associated with the magazine (14) to determine whether the magazine (14) is vertically directly above the target animal. A method of administering a substance to an animal using a UAV is also provided.

    Abstract translation: 无人驾驶飞行器物质管理有效载荷（10）包括配置为安装到能够悬停的无人驾驶飞行器（无人飞行器）的安装件（12）。 杂志（14）被配置成保持至少一个未导引的自由落体射弹（16），该自由落体射弹（16）被配置为在与动物碰撞时向动物施用物质。 杂志（14）由支架（12）携带。 提供释放机构（18）以从钉仓（14）释放非导引自由落体抛射物（16），使得抛射物（16）能够在重力作用下从钉仓（14）直接下落到目标动物 在杂志（14）下面。 瞄准装置（20）与匣子（14）相关联以确定匣子（14）是否竖直地直接在目标动物的上方。 还提供了使用无人机向动物施用物质的方法。

    ROBOTIC SYSTEM AND METHOD FOR COMPLEX INDOOR COMBAT
    56.
    发明申请
    ROBOTIC SYSTEM AND METHOD FOR COMPLEX INDOOR COMBAT 审中-公开
    机动系统和复杂室内机的方法

    公开(公告)号：WO2015029007A1

    公开(公告)日：2015-03-05

    申请号：PCT/IL2014/000043

    申请日：2014-08-28

    Applicant: GABBAY, Ronen Izidor

    Inventor： GABBAY, Ronen Izidor

    IPC: B64C19/00 ,  B64C27/00

    CPC classification number: B64C39/024 ,  B64C2201/121 ,  F41A23/56 ,  F41G3/165 ,  G05D1/0038 ,  G05D1/0044 ,  G05D1/0094

    Abstract: The present invention provides systems and methods for combatting a threat, the system including a motorized apparatus adapted to hover and hold at least one engagement element, at least one detection element adapted to convey detection data, an apparatus location element adapted to convey system location data, an onboard processor adapted to receive and process the detection data from the at least one detection element and the location data from the at least one apparatus location data element, the processor being configured to output at least one command to the at least one engagement element to inactivate the threat; and at least one communication element, and a ground station for monitoring the motorized apparatus and for receiving data from the at least one communication element.

    Abstract translation: 本发明提供了用于对抗威胁的系统和方法，所述系统包括适于悬停和保持至少一个接合元件的机动设备，适于传送检测数据的至少一个检测元件，适于传送系统位置数据的装置位置元件 适于接收并处理来自所述至少一个检测元件的检测数据和来自所述至少一个装置位置数据元素的位置数据的车载处理器，所述处理器被配置为将至少一个命令输出到所述至少一个接合元件 灭绝威胁; 以及至少一个通信元件，以及用于监视机动化装置并用于从所述至少一个通信元件接收数据的地面站。

    UNMANNED VEHICLE
    57.
    发明申请
    UNMANNED VEHICLE 审中-公开
    未经规定的车辆

    公开(公告)号：WO2005123502A3

    公开(公告)日：2007-03-29

    申请号：PCT/US2004041583

    申请日：2004-12-13

    Applicant: ADVANCED CERAMICS RES INC ,  MULLIGAN ANTHONY C ,  TROUDT CHRISTOPHER D ,  DOUGLAS JASON MICHAEL K

    Inventor： MULLIGAN ANTHONY C ,  TROUDT CHRISTOPHER D ,  DOUGLAS JASON MICHAEL K

    IPC: G01S19/48 ,  G05D1/02 ,  B64C15/00 ,  B64C39/02 ,  G01S13/76 ,  G06F17/12

    CPC classification number: G05D1/0094 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/044 ,  B64C2201/104 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/205 ,  B64C2201/208

    Abstract: Methods and apparatuses provide surveillance of a convoy (12). At least one unmanned aerial vehicle (UAV) (10) obtains images around the convoy's position to provide information about potential hostile activity while th UAV follows a generally curvilinear path around the convoy as instructed by one of the convoy vehicles. Path planner algorithm software is executed by the controlling convoy vehicle in which position and velocity information regarding the unmanned aerial vehicle and the convoy are processed to determine values of control variables. The determined values are sent to the unmanned aerial vehicle over a wireless communications channel. The path of the surveillance vehicle may be changed in order to provide evasive measures to avoid an attack on the surveillance vehicle by an adversary.

    Abstract translation: 方法和设备对车队进行监视（12）。 至少一架无人机（UAV）（10）获得围绕车队位置的图像，以提供关于潜在敌对行为的信息，而无人机遵循车队之一的指示，沿着车队周围的大致曲线路径。 路径规划器算法软件由控制车队车辆执行，其中处理关于无人机和车队的位置和速度信息以确定控制变量的值。 所确定的值通过无线通信信道发送到无人驾驶飞行器。 监视车辆的路径可能会改变，以便提供回避措施，以避免对手对监控车辆的攻击。

    STOWABLE DESIGN FOR UNMANNED AERIAL VEHICLE
    58.
    发明申请
    STOWABLE DESIGN FOR UNMANNED AERIAL VEHICLE 审中-公开
    可持续的空中客车设计

    公开(公告)号：WO2006073750A3

    公开(公告)日：2006-12-28

    申请号：PCT/US2005045715

    申请日：2005-12-16

    Applicant: ALMAN JAMES

    Inventor： ALMAN JAMES

    IPC: B64C3/38

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203

    Abstract: An unmanned aerial vehicle (UAV) having a design for optimum stowability and low cost. The UAV having a collapsible wing section which can be easily removed from the fuselage, allowing for quick assembly and disassembly and ease of portability. The unmanned aerial vehicle includes a primary wing assembly, a fuselage, a means for propelling the unmanned aerial vehicle , and means for remotely controlling the unmanned aerial vehicle. The primary wing assembly includes a wing having a center spar and two outwardly diverging side spars. The wing also has a pliable flexible material supported by the center spar and the at least two outwardly diverging side spars. The pylon is connected to the wing and supports the wing. The fuselage is connected to the pylon such that the pylon extends away from the fuselage and spaces the wing a distance from the fuselage. The fuselage includes a tail having a rudder located along a trailing edge and elevators located along the trailing edge.

    Abstract translation: 无人飞行器（UAV）具有最佳的可收藏性和低成本的设计。 无人机具有可折叠的机翼部分，可以方便地从机身中移除，从而实现快速组装和拆卸，便于携带。 无人飞行器包括主翼组件，机身，用于推动无人驾驶飞行器的装置，以及用于远程控制无人驾驶飞行器的装置。 主翼组件包括具有中心翼梁和两个向外发散的侧翼的翼。 机翼还具有由中心翼梁和至少两个向外发散的侧翼支撑的柔韧的柔性材料。 塔架连接到机翼并支撑机翼。 机身连接到挂架，使得吊架远离机身延伸，并将机翼与机身隔开一段距离。 机身包括尾部，尾部沿着后缘设有方向舵，沿着后缘设有电梯。

    MICRO-ROTOCRAFT SURVEILLANCE SYSTEM
    59.
    发明申请
    MICRO-ROTOCRAFT SURVEILLANCE SYSTEM 审中-公开
    MICRO-ROTOCRAFT监控系统

    公开(公告)号：WO03059735A2

    公开(公告)日：2003-07-24

    申请号：PCT/US0241280

    申请日：2002-12-19

    Applicant: ARLTON PAUL E ,  ARLTON DAVID J

    Inventor： ARLTON PAUL E ,  ARLTON DAVID J

    IPC: B64C27/10 ,  B64C39/02 ,  B64C

    CPC classification number: G08B13/19621 ,  B64C27/10 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2201/208 ,  G08B13/19619 ,  G08B13/1963

    Abstract: A flying micro-rotorcraft unit is provided for remote tactical and operational missions. The unit includes an elongated body having an upper and a lowe end. The body defines a vertical axis. The unit further includes a navigation module including means for determining a global position of the elongated body during flight of the unit. Rotor means of the unit is coupled to the upper end of the elongated body for generating a thrust force that acts in a direction parallel to the verical axis to lift the elongated body into the air. The rotor means is located between the elongated body and the navigation module.

    Abstract translation: 提供了一个飞行的微型旋翼航空器，用于远程战术和作战任务。 该单元包括具有上端和下端的细长体。 身体定义垂直轴。 该单元还包括导航模块，其包括用于在单元飞行期间确定细长主体的全局位置的装置。 该单元的转子装置联接到细长主体的上端，用于产生一个推力，该推力作用在平行于虚拟轴线的方向上，以将细长主体提升到空气中。 转子装置位于细长主体和导航模块之间。

    CIRCULAR VERTICAL TAKE-OFF AND LANDING AIRCRAFT
    60.
    发明申请
    CIRCULAR VERTICAL TAKE-OFF AND LANDING AIRCRAFT 审中-公开
    圆形垂直起落架和飞机

    公开(公告)号：WO2002070342A1

    公开(公告)日：2002-09-12

    申请号：PCT/GB2002/000863

    申请日：2002-02-26

    Applicant: WALMSLEY, Eric, Ronald

    Inventor： WALMSLEY, Eric, Ronald

    IPC: B64C39/00

    CPC classification number: B64C27/20 ,  B64C39/001 ,  B64C39/024 ,  B64C39/06 ,  B64C39/062 ,  B64C2201/027 ,  B64C2201/046 ,  B64C2201/048 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/162

    Abstract: A circular VTOL aircraft with a central vertically mounted turboprop engine (14), driving contra-rotating co-axial propellers (24), above a central jet engine, or engines (12), horizontally mounted on a turntable (11) and steerable through 360 degrees. The turboprop provides vertical thrust from propellers compressing air from an upper circular intake (5) downward through a circular funnel-shaped rotor-chamber (6), to a circular vent (10) at the base of the aircraft. The resulting column of compressed air gives lift for VTOL operations and a cushion of air in flight. The horizontally mounted turbine provides acceleration, retro-thrust and directional control for horizontal flight and vectored thrust for VTOL. An alternative engine configuration (Figure 9), replaces the turboprop and propellers with a vertical turbojet or rocket-engine system providing direct vertical thrust via four control vents (12/14), with an optional horizontal vectored thrust vent (15/37).he aircraft. Fuel-tanks are installed around the central engines. The flight-deck is at the top-centre of the craft above the engines, which are detachable for maintenance.

    Abstract translation: 一种具有中心垂直安装的涡轮螺旋桨发动机（14）的圆形垂直起降飞机，在中心喷气发动机上方驱动反向旋转的同轴推进器（24），或水平安装在转盘（11）上并可导向 360度。 涡轮螺旋桨发动机从螺旋桨提供垂直推力，将来自上部圆形进气口（5）的空气向下压缩通过圆形漏斗形转子室（6），到飞机底部的圆形通风口（10）。 由此产生的压缩空气柱可提供垂直起落架作用的升降机和飞行中的空气缓冲。 水平安装的涡轮机为垂直起落架的垂直飞行和向心推力提供加速度，逆向推力和方向控制。 另一种发动机配置（图9）用垂直涡轮喷气发动机或火箭发动机系统代替涡轮螺旋桨发动机和螺旋桨系统，通过四个控制通风口（12/14）提供直接垂直推力，并具有可选的水平向心推力通风口（15/37）。 他的飞机。 燃油箱安装在中央发动机周围。 飞行甲板位于发动机上方的工艺的顶部中心，可拆卸以进行维护。

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