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    SUB-MUNITION UNIT
    1.
    发明申请
    SUB-MUNITION UNIT 审中-公开
    辅助单元

    公开(公告)号：US20100229752A1

    公开(公告)日：2010-09-16

    申请号：US12669400

    申请日：2008-06-27

    Applicant: Alexander Paesch ,  Martin Rybol

    Inventor： Alexander Paesch ,  Martin Rybol

    IPC: F42B12/58

    CPC classification number: F42B10/56 ,  F42B10/58 ,  F42C11/002 ,  F42C13/006

    Abstract: The invention relates to a sub-munition unit (1) having a warhead (2) that comprises an antenna (3) on the bow side, as seen in the direction of flight, for target acquisition, and is connected on the aft side to a releasably attached parachute cartridge (4). In order to protect the antenna (3) sufficiently against both mechanical loads and aerodynamic stresses using a simple protective device, and without thereby negatively affecting the function of the antenna (3), an antenna protection cover (5) is releasably disposed on the warhead in front of the antenna (3) so as to protect the antenna (3), and the warhead (2) comprises an operating mechanism causing the antenna protection cover (5) to be ejected when the parachute cartridge (4) is released from the warhead (2).

    Abstract translation: 本发明涉及一种具有弹头（2）的子弹单元（1），其包括在飞行方向上的弓侧上的天线（3），用于目标采集，并且在后侧连接到 可释放地附接的降落伞筒（4）。 为了使用简单的保护装置充分抵御机械负载和空气动力学应力来保护天线（3），并且不会对天线（3）的功能产生负面影响，天线保护盖（5）可释放地设置在弹头 在天线（3）的前面，以便保护天线（3），并且弹头（2）包括一个操作机构，当伞形弹药筒（4）被释放时，导致天线保护罩（5）被弹出 弹头（2）。

    Flexible wing
    2.
    发明授权
    Flexible wing 失效
    柔性翼

    公开(公告)号：US5067410A

    公开(公告)日：1991-11-26

    申请号：US632211

    申请日：1990-12-21

    Applicant: James F. Murnane, III ,  William G. Kuhnle

    Inventor： James F. Murnane, III ,  William G. Kuhnle

    IPC: F42B10/58

    CPC classification number: F42B10/58

    Abstract: A flexible wing which is connected to a submunition provides a substantia vertical descent and provides torque which power submunition electronics. The flexible wing is deployed in a low drag configuration to avoid collision with other submunitions. The flexible wing is canted to allow rotation of the wing.

    Abstract translation: 连接到子弹药的柔性翼片提供基本垂直的下降并提供对子弹药电子设备的扭矩。 柔性机翼以低阻力配置部署，以避免与其他子弹药的碰撞。 柔性翼片倾斜以允许翼的旋转。

    INTELLIGENT MULTI-ROTOR RESCUE THROWER AND CONTROL METHOD THEREOF
    6.
    发明公开
    INTELLIGENT MULTI-ROTOR RESCUE THROWER AND CONTROL METHOD THEREOF 审中-公开

    公开(公告)号：US20230204331A1

    公开(公告)日：2023-06-29

    申请号：US17927902

    申请日：2022-02-15

    Applicant: JIANGSU UNIVERSITY

    Inventor： Yue SHEN ,  Yicen LI ,  Dewei WANG ,  Xiuli WANG ,  Zhixiang SHI ,  Yayun SHEN

    IPC: F42B10/58 ,  F42B12/56 ,  B63C9/26 ,  F42B10/56

    CPC classification number: F42B10/58 ,  F42B12/56 ,  B63C9/26 ,  F42B10/56

    Abstract: In an intelligent multi-rotor rescue thrower, a throwing projectile head is located at a foremost end of the thrower, a parachute storage bin is mounted at a center of a front end of the throwing projectile head, a rear end of the throwing projectile head is connected to a projectile body shell through threads, and a first splitter plate, a second splitter plate, and a third splitter plate are directly connected to the projectile body shell through slide grooves built in the projectile body shell to equally divide a space in a cavity of the projectile body shell; connecting flanges tightly connect the projectile body shell to motors, a rotor is connected to an upper end of each of the motors, and three rotors are provided in the space in the cavity of the projectile body shell.

    Method and apparatus for imparting to an airborne warhead a desired pattern of movement
    7.
    发明授权
    Method and apparatus for imparting to an airborne warhead a desired pattern of movement 失效
    赋予机载弹头所需运动模式的方法和装置

    公开(公告)号：US5679919A

    公开(公告)日：1997-10-21

    申请号：US525734

    申请日：1995-12-05

    Applicant: Anders Holm ,  Jan Axinger ,  Kenneth Jarnryd

    Inventor： Anders Holm ,  Jan Axinger ,  Kenneth Jarnryd

    IPC: F42B10/48 ,  F42B10/30 ,  F42B10/58 ,  F42B12/58

    CPC classification number: F42B10/58 ,  F42B10/30

    Abstract: A method and apparatus is for imparting, in a continuous sequence, a predetermined rotational movement to a warhead releasably housed in a protective canister and ejected out in ballistic ejection trajectories from the canister. The canister is spun to the desired rotational speed by flow of combustion gases through gas outlet nozzles discharging in the outer periphery of the canister and supplied from a central combustion chamber in which a propellant powder charge is combusted. The combustion gases are then led from the combustion chamber, in the final phase of the propellant charge combustion, through gas outlets facing towards the warhead and initially covered by the propellant charge and exposed as a result of the combustion, for ejecting the warhead out of the canister.

    Abstract translation: PCT No.PCT / SE94 / 00232 Sec。 371 1995年12月5日第 102（e）日期1995年12月5日PCT 1994年3月17日PCT公布。 公开号WO94 / 23265 日期1994年10月13日一种方法和装置用于连续顺序地将预定的旋转运动传递给可释放地容纳在保护罐中的弹头，并从弹出的弹道弹出轨迹中弹出。 通过燃烧气体的流动通过在罐的外周排出并从其中燃烧有推进剂粉末装料的中心燃烧室供给的气体出口喷嘴将罐旋转到所需的转速。 燃烧气体然后在推进剂充气燃烧的最后阶段通过面向弹头的气体出口从燃烧室引出，并且最初被推进剂装料覆盖并作为燃烧而暴露，以将弹头从 罐。

    Fuse assembly
    8.
    发明授权
    Fuse assembly 失效
    保险丝总成

    公开(公告)号：US4662278A

    公开(公告)日：1987-05-05

    申请号：US712676

    申请日：1985-03-18

    Applicant: William N. Lillios

    Inventor： William N. Lillios

    IPC: F42B10/58 ,  F42C15/184 ,  F42B25/02 ,  F42C15/22

    CPC classification number: F42B10/58 ,  F42C15/184

    Abstract: A fuse assembly embodying a detonator movable by centrifugal force into alignment with a firing pin held retracted by a drogue and drag line and movable forwardly into engagement with the detonator by impact, the fuse assembly being attached to a grenade which, in turn, is attached to a projectile, for firing the grenade upon impact of the projectile with a target.

    Abstract translation: 一种保险丝组件，其包括雷管，所述雷管可以通过离心力移动，与由棘爪和牵引线缩回的撞针对准，并通过冲击向前与所述雷管接合，所述保险丝组件附接到手榴弹，所述手榴弹又附接 射弹，用弹射弹射击目标后发射手榴弹。

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