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公开(公告)号:US20180216912A1
公开(公告)日:2018-08-02
申请号:US15749409
申请日:2016-07-20
申请人: MBDA FRANCE
发明人: Bertrand Leroy , Pascal Herquel
CPC分类号: F41F3/077 , B32B15/043 , B32B15/14 , B32B25/02 , B32B2250/40 , B32B2260/023 , B32B2260/048 , B32B2262/02 , B32B2262/10 , B32B2307/51 , B32B2307/7242 , B32B2319/00 , B32B2435/02 , B32B2581/00 , F16J15/064 , F16J15/067 , F16J15/122
摘要: A flexible cover comprising at least one, so-called composite, layer, formed from a composite material consisting of at least one fabric and at least one elastomer and a flat metal blade secured to the composite layer by elastomer and comprising pre-cut lines for fragilisation of the flexible cover, the pre-cut lines being arranged so as to create areas in the form of petals, the composite layer and the metal blade being designed so as to return to an initial position once the flexible cover has been opened.
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公开(公告)号:US09567107B2
公开(公告)日:2017-02-14
申请号:US14642720
申请日:2015-03-09
申请人: QUICKLAUNCH, INC.
发明人: Harry E. Cartland
IPC分类号: B64G1/00 , F41F3/04 , F41F1/00 , F41B11/723 , F41A1/02 , F41B11/60 , F41F3/077 , B64G5/00 , F41B11/68 , F42B10/26 , F42B10/66 , F42B14/06 , F42B15/00
CPC分类号: B64G1/002 , B64G5/00 , F41A1/02 , F41B11/60 , F41B11/68 , F41B11/723 , F41F1/00 , F41F3/04 , F41F3/0413 , F41F3/077 , F42B10/26 , F42B10/66 , F42B14/06 , F42B15/00
摘要: A gas gun launcher has a pump tube and a launch tube with a first end of the launch tube slidably inserted into a second end of the pump tube. The pump tube may hold a heat exchanger to heat a light gas used to launch a vehicle. A sliding seal can be employed to manage recoil and to retain the gas within the launch tube and the pump tube. A fast-closing muffler at the second end of the launch tube can conserve the light gas utilized for launching a vehicle, enabling the light gas to be recycled. A launch tube alignment system is preferably automatic, ensuring the survival of the launch vehicle.
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公开(公告)号:US09360277B2
公开(公告)日:2016-06-07
申请号:US13970865
申请日:2013-08-20
CPC分类号: F41F3/0406 , F41F3/0413 , 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
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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
CPC分类号: F41F3/042 , B65D88/126 , F41A23/20 , F41F3/077
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。
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公开(公告)号:US08720340B1
公开(公告)日:2014-05-13
申请号:US13590408
申请日:2012-08-21
申请人: Henry Edward Kendrix
发明人: Henry Edward Kendrix
IPC分类号: F42B4/00
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。
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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
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。
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公开(公告)号:US20060207416A1
公开(公告)日:2006-09-21
申请号:US11072482
申请日:2005-03-04
申请人: Brian Bohs , William Everitt
发明人: Brian Bohs , William Everitt
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。
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公开(公告)号:US5823469A
公开(公告)日:1998-10-20
申请号:US663308
申请日:1996-06-26
申请人: Ivan Ivanovitch Arkhangelsky , Eugene Gueorguevitch Bolotov , Vladimir Sergueevitch Philippov , Vladimir Yakovlevitch Mizrokhi , Vladimir Grigorievitch Svetlov , Gregory Andreevitch Stanevsky , Serge Grigorievitch Khitenkov , Victor Leonidovitch Gaidoukevitch , Eugene Afanassievitch Chmikov
发明人: Ivan Ivanovitch Arkhangelsky , Eugene Gueorguevitch Bolotov , Vladimir Sergueevitch Philippov , Vladimir Yakovlevitch Mizrokhi , Vladimir Grigorievitch Svetlov , Gregory Andreevitch Stanevsky , Serge Grigorievitch Khitenkov , Victor Leonidovitch Gaidoukevitch , Eugene Afanassievitch Chmikov
CPC分类号: F42B10/663 , F41F3/04 , F41F3/077 , F42B10/66
摘要: This invention concerns a missile launching system, and particularly a missile launching and orientation system. It can be used to modernize missiles with an inclined launch at an angle by transforming them into missiles controlled for circular defense, avoids ejection of the passive mass within the launching area. In order to do this, the launching system comprises launching means, aerodynamic control surfaces with drive and means of orientation including at least one gas generator and nozzles connected to it. Orientation means are located in an annular body rigidly connected to the rear part of the missile body. The outside surface of the annular body is cone-shaped and is covered with a thermal insulating material forming a gas pipe, the profile of which is a continuation of the profile of the nozzle of the missile cruise engine.
摘要翻译: PCT No.PCT / FR95 / 01423 Sec。 371日期:1996年6月26日 102(e)日期1996年6月26日PCT提交1995年10月27日PCT公布。 出版物WO96 / 13694 日期1996年5月9日本发明涉及导弹发射系统,特别是导弹发射和导向系统。 通过将导弹转化为控制循环防御的导弹,可以用倾斜发射方式将导弹现代化,避免在发射区域内弹出被动质量。 为了做到这一点,发射系统包括发射装置,具有驱动的空气动力学控制表面和取向装置,其包括至少一个气体发生器和连接到其上的喷嘴。 定向装置位于刚性地连接到导弹体的后部的环形体中。 环形体的外表面是锥形的并且被形成气体管道的绝热材料覆盖,其形状是导弹巡航发动机的喷嘴轮廓的延续。
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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
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。
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公开(公告)号:US3974774A
公开(公告)日:1976-08-17
申请号:US194837
申请日:1971-11-02
CPC分类号: F42B12/50 , F41F3/0455 , F41F3/077
摘要: A projectile for use in a multishot portable weapon system containing a voelastic solution of high molecular weight polyisobutylene in triethylaluminum to be delivered to a target site to inflict casualties and/or produce a conflagration.
摘要翻译: 一种用于多重便携式武器系统的弹丸,包含三乙基铝中高分子量聚异丁烯的粘弹性溶液,以传送到目标地点,造成人员伤亡和/或产生爆燃。
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