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    드론을 이용한 지뢰탐지 및 제거방법
    61.
    发明申请
    드론을 이용한 지뢰탐지 및 제거방법 审中-公开

    公开(公告)号：WO2019050298A1

    公开(公告)日：2019-03-14

    申请号：PCT/KR2018/010424

    申请日：2018-09-06

    Applicant: 오병후

    Inventor： 오병후

    IPC: F41H11/136 ,  B64C39/02 ,  B64D1/06

    CPC classification number: B64C39/024 ,  B64C2201/121 ,  B64D1/06 ,  F41H11/136

    Abstract: 본 발명은 무인방식의 드론을 이용하여 지상이나 지하에 매설된 지뢰를 탐지하고 제거하는 방법에 관한 것으로서, 보다 상세하게는 지뢰를 탐지하는 탐지드론과 탐지드론에 의해 탐지된 지뢰를 제거하는 제거드론이 한 조로 이루어져, 지뢰탐지와 제거 등 인간이 직접 수행하기 위험한 작업을 대신하도록 하며, 군사경계선 등 전쟁이 발발할 수 있는 위험한 지역에 투입하여 지뢰를 탐지하고 제거할 수 있는 드론을 이용한 지뢰탐지 및 제거방법이다.

    SPACE COMBAT DRONE
    62.
    发明申请
    SPACE COMBAT DRONE 审中-公开
    空间战斗无人机

    公开(公告)号：WO2017131823A2

    公开(公告)日：2017-08-03

    申请号：PCT/US2016/052091

    申请日：2016-09-16

    Applicant: WILKINSON, Christopher

    Inventor： WILKINSON, Christopher

    IPC: B64C13/24 ,  A63H30/04

    CPC classification number: B64C39/024 ,  B64C2201/02 ,  B64C2201/046 ,  B64C2201/082 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/206 ,  B64C2201/22

    Abstract: An unmanned aerial combat vehicle system is disclosed. The system provides for an unmanned aerial combat vehicle that is capable of performing reconnaissance, disrupting enemy communications, or delivering a weaponized payload. The unmanned aerial combat vehicle may also be equipped with a cloaking mechanism, where it can mask it' s heat signature, or simulate an image on its outer surface.

    Abstract translation: 公开了一种无人空中作战车辆系统。 该系统提供了一种无人驾驶的空中作战车辆，能够执行侦察，破坏敌方通信或发射武器化的有效载荷。 无人驾驶飞行器也可以配备隐形装置，它可以掩盖它的热特征，或者在其外表面模拟图像。

    TRAILER FOR AUTONOMOUS VEHICLE
    63.
    发明申请
    TRAILER FOR AUTONOMOUS VEHICLE 审中-公开
    自动车辆拖车

    公开(公告)号：WO2015038697A3

    公开(公告)日：2015-10-29

    申请号：PCT/US2014055075

    申请日：2014-09-11

    Applicant: SILICIS TECHNOLOGIES INC

    Inventor： STIGLER MICHAEL J ,  SETAR NICHOLAS JAMES

    IPC: B64F1/12

    CPC classification number: B60P3/11 ,  B60P7/06 ,  B60P7/0876 ,  B64B1/10 ,  B64B1/50 ,  B64B1/58 ,  B64B1/66 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/06 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/125 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/208 ,  B64F1/14 ,  B64F3/02 ,  G08C17/02

    Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.

    Abstract translation: 所公开的实施例包括用于由命令和控制接口控制的自主车辆的拖车。 拖车包括拖车主体，其构造成将自主车辆保持在未部署的构造中。 拖车还以部署的配置锚定自主车辆。 提供了系绳，其具有联接到拖车主体的第一端和被配置为联接到自主车辆的第二端。 使用绞盘来调节系绳的长度以在未部署的配置和部署配置之间移动自主车辆。 此外，通信系统与命令和控制界面以及自主车辆进行通信，以控制自动车辆在未部署配置和部署配置之间的移动。

    INTERCEPTION MISSILE AND WARHEAD THEREFOR
    64.
    发明申请
    INTERCEPTION MISSILE AND WARHEAD THEREFOR 审中-公开
    拦截失误和战争

    公开(公告)号：WO2015102001A1

    公开(公告)日：2015-07-09

    申请号：PCT/IL2015/050012

    申请日：2015-01-01

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： ROVINSKY, Jacob

    IPC: F42B12/22 ,  F42B12/00

    CPC classification number: F42B12/22 ,  B64C39/024 ,  B64C2201/121 ,  F41G7/001 ,  F41G7/20 ,  F42B10/26 ,  F42B12/202 ,  F42B12/32 ,  F42C19/095

    Abstract: A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.

    Abstract translation: 提供了能够安装在载体车辆中的分裂弹头，该弹头具有纵向轴线。 在至少一个示例中，弹头包括沿着纵向轴线延伸的壳体。 壳体包括固定壳体部分和碎裂部分，并且在其间限定用于在其中容纳炸药的空腔。 碎裂部分包括在碎裂部分中以相应的串联连续关系的至少一组串联相邻碎片，并且相对于纵向轴线呈大致螺旋关系。 还提供了相应的载体车辆和相应的导弹。

    VEHICLE CAPABLE OF STABILIZING A PAYLOAD WHEN IN MOTION
    65.
    发明申请
    VEHICLE CAPABLE OF STABILIZING A PAYLOAD WHEN IN MOTION 审中-公开
    在运动中能够稳定有效载荷的车辆

    公开(公告)号：WO2014062276A3

    公开(公告)日：2014-06-26

    申请号：PCT/US2013053006

    申请日：2013-07-31

    Applicant: NEUROSCIENCES RES FOUND

    Inventor： HUTSON DONALD B

    IPC: B64C25/36

    CPC classification number: B64D47/08 ,  B64C27/006 ,  B64C27/10 ,  B64C27/20 ,  B64C39/024 ,  B64C2025/325 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/182 ,  B64D9/00 ,  F16M11/123 ,  F16M11/18 ,  F16M13/00 ,  F16M13/02 ,  F16M2200/041

    Abstract: In specific embodiments, a vehicle propellable through fluids comprises a main work section and a plurality of propulsion units. The main work section includes a payload support hub, a payload support structure rotatable in 360 about the payload support hub in at least one axis, and a core including at least one microprocessor, the core at least partially nested within the payload support hub. The at least one microprocessor is adapted to substantially maintain an orientation of the payload support structure relative to a horizon line as the vehicle is propelled. One or more payloads are mountable on the rotatable payload support structure.

    Abstract translation: 在特定实施例中，可通过流体推进的车辆包括主工作区段和多个推进单元。 主工作部分包括有效负载支撑集线器，在至少一个轴线上围绕有效负载支撑集线器360旋转的有效负载支撑结构以及包括至少一个微处理器的核心，核心至少部分地嵌套在有效负载支撑集线器内。 所述至少一个微处理器适于在车辆被推进时基本上保持有效载荷支撑结构相对于水平线的取向。 一个或多个有效载荷可安装在可旋转有效载荷支撑结构上。

    UNMANNED AERIAL VEHICLE ANGULAR REORIENTATION
    66.
    发明申请
    UNMANNED AERIAL VEHICLE ANGULAR REORIENTATION 审中-公开
    不定期的空中客车航向转向

    公开(公告)号：WO2012119132A2

    公开(公告)日：2012-09-07

    申请号：PCT/US2012/027619

    申请日：2012-03-02

    Applicant: AEROVIRONMENT, INC. ,  MIRALLES, Carlos

    Inventor： MIRALLES, Carlos

    IPC: G06F19/00

    CPC classification number: B64C13/16 ,  B64B2201/00 ,  B64C39/024 ,  B64C2201/04 ,  B64C2201/121 ,  B64C2201/141 ,  B64C2201/165 ,  F41G7/2253 ,  F41G7/2286 ,  F41G7/2293 ,  G05D1/12

    Abstract: A system comprising an unmanned aerial vehicle (UAV) (100) having wing elements (141, 142) and tail elements (143, 144) configured to roll to angularly orient the UAV (100) by rolling so as to align a longitudinal plane of the UAV, in its late terminal phase, with a target. A method of UAV body re-orientation comprising: (a) determining by a processor (940) a boresight angle error correction value (850) bases on distance between a target point (812) and a boresight point (820) of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point (812) to a re-oriented target point (814) in the body-fixed frame, to maintain the offset angle via (850) the offset angle correction value.

    Abstract translation: 一种包括具有翼元件（141,142）和尾部元件（143,144）的无人驾驶飞行器（UA）（100）的系统，所述尾部元件（143,144）被配置成滚动以通过滚动角度地定向所述UAV（100） 无人机在其末期阶段有一个目标。 一种UAV身体重新定位的方法，包括：（a）基于处理器（940）确定基于目标点（812）和身体 - 角度（820）的视轴点（820）之间的距离的视轴角度误差校正值（850） 固定框架 和（b）进行无人机操作，其包括将所述目标点（812）转换为所述身体固定框架中的重定向目标点（814）的角度角色分量，以通过（850）偏移角度 校正值。

    POWER SAFETY INSTRUMENT SYSTEM
    67.
    发明申请
    POWER SAFETY INSTRUMENT SYSTEM 审中-公开
    电力安全仪表系统

    公开(公告)号：WO2012087303A1

    公开(公告)日：2012-06-28

    申请号：PCT/US2010/061701

    申请日：2010-12-22

    Applicant: BELL HELICOPTER TEXTRON INC. ,  MCCOLLOUGH, James, M. ,  OLTHETEN, Erik ,  LAPPOS, Nicholas

    Inventor： MCCOLLOUGH, James, M. ,  OLTHETEN, Erik ,  LAPPOS, Nicholas

    IPC: G01C21/00

    CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

    Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

    Abstract translation: 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个指示器位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。

    INTERCEPTION MISSILE AND WARHEAD THEREFOR
    69.
    发明公开
    INTERCEPTION MISSILE AND WARHEAD THEREFOR 审中-公开
    ABFANGRAKETE UND GEFECHTSKOPFDAFÜR

    公开(公告)号：EP3071925A4

    公开(公告)日：2017-07-19

    申请号：EP15733090

    申请日：2015-01-01

    Applicant: ISRAEL AEROSPACE IND LTD

    Inventor： ROVINSKY JACOB

    IPC: F42B12/22 ,  F42B12/00 ,  F42B12/20 ,  F42B12/32 ,  F42C19/095

    CPC classification number: F42B12/22 ,  B64C39/024 ,  B64C2201/121 ,  F41G7/001 ,  F41G7/20 ,  F42B10/26 ,  F42B12/202 ,  F42B12/32 ,  F42C19/095

    Abstract: A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.

    Abstract translation: 提供碎片弹头，能够安装在运载工具上，弹头具有纵向轴线。 在至少一个示例中，弹头包括沿着纵向轴线延伸的壳体。 壳体包括固定壳体部分和碎裂部分，并且在壳体之间限定用于在其中容纳炸药的空腔。 碎裂部分包括至少一组串联相邻的碎片，碎片部分中相应的串行连续关系并且相对于纵向轴线大致呈螺旋关系。 还提供相应的运载车辆和相应的导弹。

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