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    • 1. 发明公开
      EP4177173A1 A DEVICE FOR UNMANNED AERIAL VEHICLE TO INSTALL RAINFALL CATALYTIC BOMB 审中-实审
    • A DEVICE FOR UNMANNED AERIAL VEHICLE TO INSTALL RAINFALL CATALYTIC BOMB
    • EP4177173A1
    • 2023-05-10
    • EP22206045.1
    • 2022-11-08
    • Shanghai Autoflight Co., Ltd.
    • TIAN, Yu
    • B64U10/20 , B64U10/25 , A01G15/00 , F42B12/36 , F42B15/01 , F42B15/08 , B64U101/18 , B64U101/35
    • The invention belongs to the technical field of unmanned aerial vehicle application and artificial rainfall, and discloses a device for unmanned aerial vehicle to install rainfall catalytic bomb which comprises an unmanned aerial vehicle, a cannonball for artificial precipitation and a cylinder, wherein the unmanned aerial vehicle is connected with the cannonball for artificial precipitation through a soft lock, the cannonballs for artificial precipitation are multiple and are wrapped in the cylinders, a second sensor is arranged in the cylinder, wing surfaces are arranged on the outer side of the cylinder, the wing surfaces are multiple and are arranged at one end of the cylinder in the long shaft direction, and one end of the soft lock is connected to the other end of the cylinder in the long shaft direction. The unmanned aerial vehicle carries the cannonball for artificial precipitation to carry out rainfall, the unmanned aerial vehicle does not need to enter a cloud layer, the unmanned aerial vehicle can safely run to reduce the accident rate, the operation is simple, and the rainfall cost is low. The position of the cannonball for artificial precipitation can be accurately monitored in real time, so that it can be conveniently and accurately thrown in and detonated. The wing surface is arranged, so that the stability and the posture adjustment of the cannonball for artificial precipitation can be controlled conveniently.
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
    • 4. 发明公开
      EP2411758A1 BESTIMMUNG DER MÜNDUNGSGESCHWINDIGKEIT EINES GESCHOSSES 有权
    • BESTIMMUNG DER MÜNDUNGSGESCHWINDIGKEIT EINES GESCHOSSES
    • BESTIMMUNG DERMÜNDUNGSGESCHWINDIGKEITEINES GESCHOSSES
    • EP2411758A1
    • 2012-02-01
    • EP10710318.6
    • 2010-03-23
    • Dynamit Nobel Defence GmbH
    • FURCH, Benjamin , RÜDIGER, Manfred
    • F42B15/08 , F42C17/04 , G01P3/66 , F41A21/32
    • F42C17/04 , F41A21/325 , F42B15/08 , G01P3/665
    • The invention relates to a method for determination of the muzzle velocity of a projectile (2) when it emerges from the firing barrel (1) of a shoulder-held weapon. In order not to weaken the firing barrel, it is proposed that a transmitter (3) for transmission of signals be arranged on the end face of the firing barrel (1) and that two sensors (9, 10), which are arranged at a distance d from one another, be arranged in or on the projectile (2) in order to detect the signals transmitted by the transmitter (3) and that these sensors (9, 10) detect a pulse on flying past the transmitter (3), and that the muzzle velocity for the projectile (2) be determined from the time difference between the pulses detected by the two sensors (9, 10).
    • 本发明涉及一种用于确定射弹（2）从肩扛武器的射击筒（1）出射时的枪口速度的方法。 为了不削弱射击筒，提出了用于传输信号的发射器（3）布置在击发筒（1）的端面上，并且两个传感器（9,10）被布置在 彼此之间的距离d被布置在射弹（2）中或其上，以便检测由发射器（3）发射的信号，并且这些传感器（9,10）检测飞过发射器（3）的脉冲， 并且从两个传感器（9,10）检测的脉冲之间的时间差确定射弹（2）的枪口速度。
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
    • 7. 发明公开
      EP1878661A3 System for attaching an instrument or apparatus to a load carried by an aircraft 有权
    • System for attaching an instrument or apparatus to a load carried by an aircraft
    • 用于将仪器或设备连接到由飞机运载的负载的系统
    • EP1878661A3
    • 2008-03-05
    • EP07112269.1
    • 2007-07-11
    • Alenia Aeronautica S.p.A.
    • Spensatellu, Tonino
    • B64D47/08 , F42B15/08 , G03B15/00
    • B64D47/08 , F42B10/00 , F42B15/08 , G03B15/006
    • The system comprises an attachment device (14) including a support structure (18, 20) and at least one band member (22) for releasably connecting the support structure (18, 20) to a load (12), such as a missile, carried by an aircraft, and an aerodynamic element (32) associated to the attachment device (14). The support structure (18, 20) of the attachment device (14) includes a support bracket (18) which is open upwards and an intermediate member (20) which is adapted to be attached to the support bracket (18) to close the support bracket (20) from above. The intermediate member (20) is arranged in the assembled condition between the instrument or apparatus (10) and the load (12). The aerodynamic element (32) is releasably attached to the load (12) in front of the instrument or apparatus (10).
    • 该系统包括包括支撑结构（18,20）和用于将支撑结构（18,20）可释放地连接至负载（12）（例如导弹）的至少一个带构件（22）的附接装置（14） 由飞机携带，以及与附接装置（14）相关联的空气动力学元件（32）。 附接装置（14）的支撑结构（18,20）包括向上敞开的支撑托架（18）和适于附接到支撑托架（18）以关闭支撑件的中间构件（20） 从上方支架（20）。 中间构件（20）布置在仪器或设备（10）和负载（12）之间的组装状态中。 气动元件（32）可释放地附接到仪器或装置（10）前方的负载（12）。
    • 基本信息 添加关注 加入工作空间 PDF全文 PDF下载 全文下载 相似专利 双屏查看 权利要求书 说明书全文 Global Dossier Espacenet 法律信息 同族专利 专利引用
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