Multiple missile carriage and launch guidance module
    3.
    发明授权
    Multiple missile carriage and launch guidance module 有权
    多导弹运载和发射指导模块

    公开(公告)号:US09360277B2

    公开(公告)日:2016-06-07

    申请号:US13970865

    申请日:2013-08-20

    IPC分类号: F41F3/04 F41F3/073 F41F3/077

    摘要: A multiple missile carriage and launch guidance module comprising a plurality of missile launch rails that are each configured to carry and guide the launch of a missile and are carried on a common missile carriage wall in respective positions and orientations allowing for missile carriage and launch from the rails.

    摘要翻译: 一个多导弹托架和发射指导模块,其包括多个导弹发射轨道,每个导弹发射轨道被配置为携带和引导导弹的发射,并且在各自的位置和方位上承载在共同导弹托架壁上,从而允许导弹运载和发射 轨道

    MISSILE CONTAINER AND METHOD OF OPERATING A MISSILE CONTAINER
    4.
    发明申请
    MISSILE CONTAINER AND METHOD OF OPERATING A MISSILE CONTAINER 有权
    容器和操作容器的方法

    公开(公告)号:US20140174283A1

    公开(公告)日:2014-06-26

    申请号:US14138340

    申请日:2013-12-23

    发明人: HAGEN KEMPAS

    IPC分类号: F41F3/042

    摘要: A missile container has a container housing, a container roof, at least one canister for holding a missile which, in a storage position, is disposed on the container housing, and a movement mechanism for moving the canister from the storage position into an operating position. The elements arranged in the interior of the container housing are protected against external weather influences. In the operating position, the canister is held at least partially outside the container housing by the movement mechanism and the container roof is closed and shields a container interior against the outside.

    摘要翻译: 导弹容器具有容器壳体,容器屋顶,至少一个罐,用于保持在存放位置上设置在容器壳体上的导弹;以及移动机构,用于将罐从储存位置移动到操作位置 。 布置在容器壳体内部的元件被保护免受外部天气影响。 在操作位置,罐通过移动机构至少部分地保持在容器壳体外部,并且容器屋顶被封闭并且将容器内部屏蔽在外部。

    Rocket launcher
    5.
    发明授权
    Rocket launcher 有权
    火箭发射器

    公开(公告)号:US08720340B1

    公开(公告)日:2014-05-13

    申请号:US13590408

    申请日:2012-08-21

    IPC分类号: F42B4/00

    CPC分类号: F42B4/20 F41F3/045 F41F3/077

    摘要: The rocket launcher includes a launching tube that extends vertically from a flat base. The launching tube is of an undefined length and includes an opening adjacent to the bottom distal end where the flat base attaches. The flat opening includes a hinged door that opens to enable insertion of a rocket or firework therein. The door includes a plurality of small holes thereon so as to enable air to pass there through along with a fuse if applicable. A handle is also attached to and extends from the exterior surface of the launching tube, and enables the rocket launcher to be carried between uses.

    摘要翻译: 火箭发射器包括从平底座垂直延伸的发射管。 发射管具有未定义的长度,并且包括与平底部附接的底部远端相邻的开口。 平开口包括铰接的门,其打开以使得能够插入火箭或烟火。 该门在其上包括多个小孔,以便如果适用的话,空气能够与保险丝一起通过。 手柄也附接到发射管的外表面并从发射管的外表面延伸,并且使火箭发射器能够在使用之间传送。

    Shell restraining device for an anti-armour weapon
    6.
    发明授权
    Shell restraining device for an anti-armour weapon 失效
    防护装甲装甲防弹武器

    公开(公告)号:US07757596B1

    公开(公告)日:2010-07-20

    申请号:US11651578

    申请日:2007-01-10

    申请人: Kenneth Sundvall

    发明人: Kenneth Sundvall

    IPC分类号: F41A9/00

    CPC分类号: F42B39/22 F41F3/042 F41F3/077

    摘要: A device for restraining a shell in a barrel of a disposable anti-armour weapon being stored in a compartment of a transport box. A stopper member is configured to be placed in the barrel in front of and adjacent to a shell loaded therein. The stopper member has at least three radially expandable legs, which are distributed circumferentially and configured to face and engage a tapered front surface of the shell in the barrel. The legs are provided with gripping elements on radially outermost surfaces thereof and configured to cut into the barrel wall upon a forward movement of the shell in the barrel.

    摘要翻译: 一种用于限制在一次性防铠装武器的枪管中的壳体被存储在运输箱的隔室中的装置。 止动构件被构造成在装在其中的壳体的前面和后面放置在筒体中。 止动构件具有至少三个可径向伸缩的腿部,其沿周向分布并且构造成面向并接合筒体中壳体的锥形前表面。 腿部在其径向最外表面上设置有夹紧元件,并且构造成在壳体在筒体中向前移动时切割成筒壁。

    Article comprising a missile canister cover
    7.
    发明申请
    Article comprising a missile canister cover 有权
    文章包括导弹筒盖

    公开(公告)号:US20060207416A1

    公开(公告)日:2006-09-21

    申请号:US11072482

    申请日:2005-03-04

    IPC分类号: F41F5/00

    CPC分类号: F41F3/077

    摘要: The illustrative embodiment of the present invention is a launch system that includes a missile canister cover that, in use, is attached to a missile canister. The cover is capable of being blown off of the canister before there is any contact between the nose of the missile and the cover and is further capable of withstanding a higher ambient pressure than internal canister pressure. These capabilities are achieved based on an attention to material mechanics and the prevailing geometry of the system.

    摘要翻译: 本发明的说明性实施例是一种发射系统,其包括在使用中附接到导弹筒的导弹盖罩。 在导弹的鼻子和盖子之间存在任何接触之前,盖子能够从罐子吹出,并且能够承受比内部罐压力更高的环境压力。 这些功能是基于对材料力学和系统主流几何学的注意而实现的。

    Rocket launcher tube post-launch rear closure
    9.
    发明授权
    Rocket launcher tube post-launch rear closure 失效
    火箭发射管后发射后关闭

    公开(公告)号:US4134327A

    公开(公告)日:1979-01-16

    申请号:US860039

    申请日:1977-12-12

    申请人: Edward T. Piesik

    发明人: Edward T. Piesik

    IPC分类号: F41F3/04 F41F3/077

    CPC分类号: F41F3/077 F41F3/0413

    摘要: A rear door for a rocket launch tube provided to prevent rocket exhaust gas flow into an empty launch tube from an associated multiple-rocket plenum chamber. The door is maintained in a stored position while a missile is in the launch tube and is activated when the missile leaves the launcher. The door may be latched open and released by a sensor device at a selected position of the missile as it is leaving the launch tube. Preferably, gases from the launching missile power closure of the door, once the door is released from its open latched position. Once the door closes, a second latch locks it in place to seal off the launch tube from the plenum chamber.

    摘要翻译: 用于火箭发射管的后门,用于防止火箭废气从相关联的多火箭增压室流入空的发射管。 当导弹在发射管中时,门保持在存储位置,并且当导弹离开发射器时被激活。 当导弹离开发射管时,门可以被锁定在导弹的选定位置处由传感器装置释放。 优选地,一旦门从其打开的锁定位置释放,来自门的发射导弹动力闭合的气体。 一旦门关闭,第二个闩锁将其锁定就位,以将发射管从增压室密封。