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公开(公告)号：US20120055321A1
公开(公告)日：2012-03-08
申请号：US12875758
申请日：2010-09-03
申请人： Mark A. Angeloff
发明人： Mark A. Angeloff
摘要： Systems and methods for launching munitions are provided. In some embodiments, the system may include a cover for use with a munitions launcher including a housing with a face. The cover may include a lid, a defined passage through the lid, and an actuator. The lid may be configured to mount to the face of the munitions launcher. The defined passage through the lid may be sized to allow a munition to pass through the lid when launched by the launcher and to substantially cover any other munitions disposed at least partially within the munitions launcher. The actuator may be configured to operate the lid in a manner that moves the defined passage in relation to the face of the munitions launcher. Movement of the defined passage in relation to the face of the munitions launcher may uncover at least one munition that was substantially covered prior to the movement of the defined passage and substantially cover any other munitions disposed at least partially within the munitions launcher.
摘要翻译： 提供了发射弹药的系统和方法。 在一些实施例中，系统可以包括用于与包括具有面部的壳体的弹药发射器一起使用的盖。 盖可以包括盖，通过盖的限定通道和致动器。 盖可以被配置成安装在弹药发射器的面上。 通过盖子的限定通道的大小可以被设计成允许弹药在发射器发射时通过盖子，并且基本上覆盖至少部分地设置在弹药发射器内的任何其他弹药。 致动器可以被配置为以相对于弹药发射器的面移动限定的通道的方式操作盖子。 关于弹药发射器面的限定通道的运动可能会发现至少一个在定义的通道移动之前基本覆盖的弹药，并且基本上覆盖至少部分在弹药发射器内部的任何其他弹药。
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公开(公告)号：US08087336B2
公开(公告)日：2012-01-03
申请号：US12266445
申请日：2008-11-06
CPC分类号： F41F3/077 , E05D15/58 , E05F15/60 , E05F15/63 , E05Y2900/50 , E05Y2900/504 , E06B7/16
摘要： A system and method for actuating a hatch door. One embodiment includes a vertical launcher system that has a hatch door disposed in a plane at the top of a hold. The hatch door includes a leading edge and a trailing edge at opposite ends of the hatch door. When an actuator arm for maneuvering the hatch door is extended, the leading edge is lifted away from the plane by the actuator arm while the trailing edge remains in the plane and slides across the top of the plane toward the point where the leading edge was first lifted away. Such a sliding hatch mechanism allows for quick opening and closing of a hatch door while providing more efficient use of mechanical energy for breaking ice build up or prevent intrusion.
摘要翻译： 一种用于启动舱门的系统和方法。 一个实施例包括垂直发射器系统，其具有设置在保持件顶部的平面中的舱门。 舱口门包括前缘和后缘在舱口门的相对端。 当用于操纵舱口门的致动器臂被延伸时，前缘被致动器臂提升离开平面，而后缘保持在平面中并且滑过平面的顶部朝向前缘首先的点 解除了 这种滑动舱口机构允许快速打开和关闭舱门，同时提供更有效地使用机械能来破坏积冰或防止入侵。
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公开(公告)号：US20110126474A1
公开(公告)日：2011-06-02
申请号：US12628849
申请日：2009-12-01
申请人： John Snediker , Daniel Skurdal
发明人： John Snediker , Daniel Skurdal
CPC分类号： F41F3/073 , F16H1/14 , F41F3/052 , F41F3/077 , F42B39/00 , F42B39/20 , Y10T74/1966 , Y10T74/19665 , Y10T403/52 , Y10T403/7005 , Y10T403/7009 , Y10T403/76
摘要： A reversible sealing mechanism for sealing a bulkhead having a first central aperture defined along a central axis and disposed between first and second compartments includes a cover member having a recess defined therein by a substantially cylindrical sidewall and adapted to cover the first central aperture. A wedge ring having a generally cylindrical body is accommodated by the first and second central apertures and is configured to operatively engage the cover member. A mechanical input is operative to reversibly rotate the wedge ring about the central axis such that a rotation of the wedge ring in a first direction urges the cover member in the axial direction into a sealed position.
摘要翻译： 用于密封具有沿着中心轴线限定并且设置在第一和第二隔室之间的第一中心孔的隔板的可逆密封机构包括盖构件，该盖构件具有由基本上圆柱形的侧壁限定在其中的适于覆盖第一中心孔的凹部。 具有大致圆柱形主体的楔形环由第一和第二中心孔容纳，并且构造成可操作地接合盖构件。 机械输入可操作以使楔环围绕中心轴线可逆地旋转，使得楔形环在第一方向上的旋转将轴向的盖构件推动到密封位置。
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公开(公告)号：US07891281B2
公开(公告)日：2011-02-22
申请号：US11400017
申请日：2006-04-07
申请人： Bruno Baldi , Roberto De Girolamo , Teodoro Andrea Dragani , Sandro Mazzuca , Gian Fabrizio Venarucci
发明人： Bruno Baldi , Roberto De Girolamo , Teodoro Andrea Dragani , Sandro Mazzuca , Gian Fabrizio Venarucci
IPC分类号： F41F3/042
摘要： In a ground launcher, two or more housing-transportation-launch assemblies for respective missiles are placed one on top of the other and connected releasably and interchangeably to each other; each housing-transportation-launch assembly has a respective outer casing, which in turn has longitudinal end walls breakable from inside the casing, and a deflecting body for deflecting the exhaust gas of the engine of the missile; a guide and protection assembly being interposed between the casing and the missile to guide the missile in the set launch direction, and to protect the missile against shock or vibration.
摘要翻译： 在地面发射器中，用于各个导弹的两个或多个外壳运输发射组件一个放置在另一个的顶部上，并且彼此可释放地和互换地相连; 每个壳体运输发射组件具有相应的外壳，其又具有可从壳体内部破裂的纵向端壁和用于偏转导弹发动机的排气的偏转体; 引导和保护组件插入在外壳和导弹之间以在发射方向上引导导弹，并保护导弹免受冲击或振动。
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公开(公告)号：US07389717B1
公开(公告)日：2008-06-24
申请号：US11111077
申请日：2005-04-21
IPC分类号： F41F3/04
CPC分类号： F41F3/077 , F41F3/0413
摘要： A missile launch system is disclosed that allows for the rapid reloading of missiles in support of missions (e.g., littoral warship missions, etc.) that require a high-volume assault of one or more targets. In particular, the illustrative embodiment of the present invention uses a munitions module that is capable of launching missiles and is able to fit inside a warship. In addition to accommodating multiple missiles, the munitions module accommodates one or more missile types. The munitions module is configured with a door at a breech end to provide access to multiple launch cells for the rapid reloading of missiles. The door is physically configured to define a plenum that couples the launch cells to an exhaust duct for the purpose of venting exhaust gases. The munitions module mitigates some of the problems associated with launch systems in the prior art.
摘要翻译： 公开了一种导弹发射系统，其允许快速重新加载导弹，以支持需要大量攻击一个或多个目标的任务（例如沿海战舰任务等）。 特别地，本发明的说明性实施例使用能够发射导弹并且能够装配在军舰内的弹药模块。 除了容纳多枚导弹之外，弹药模块还可容纳一种或多种导弹类型。 弹药模块在后膛配置有门，以提供对多个发射单元的访问，以便快速重新加载导弹。 门被物理地配置成定义将发射室耦合到排气管道的通风室，以排气。 弹药模块减轻了与现有技术中的发射系统相关的一些问题。
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公开(公告)号：US07207254B2
公开(公告)日：2007-04-24
申请号：US10106530
申请日：2002-03-20
摘要： A missile launcher comprising a canister for housing a missile and piston based launcher, the piston being arrested in the tube after launch of the missile.
摘要翻译： 一种导弹发射器，包括用于容纳基于导弹和活塞的发射器的罐，活塞在发射导弹之后被阻塞在管中。
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公开(公告)号：US20060107828A1
公开(公告)日：2006-05-25
申请号：US10106530
申请日：2002-03-20
申请人： Alan Veitch , Anthony Machell , John Winter , Roger Harriss
发明人： Alan Veitch , Anthony Machell , John Winter , Roger Harriss
IPC分类号： F41F3/00
摘要： A missile launcher comprising a canister for housing a missile and piston based launcher, the piston being arrested in the tube after launch of the missile.
摘要翻译： 一种导弹发射器，包括用于容纳基于导弹和活塞的发射器的罐，活塞在发射导弹之后被阻塞在管中。
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公开(公告)号：US06311604B1
公开(公告)日：2001-11-06
申请号：US07516405
申请日：1990-04-30
申请人： Victor G. Foris , Takeshi Tokiyama
发明人： Victor G. Foris , Takeshi Tokiyama
IPC分类号： F41F304
CPC分类号： F41F3/077
摘要： A missile launch system is described in which a missile launch tube has the launch end thereof protected by a hollow launch tube cover. The launch tube cover is divided into a plurality of segments which are frangible and are dispersed during launch of a missile 62. The surfaces of the individual segments are coated with water repellant material such as tetrafluoroethylene or silicone to prevent ice buildup. Moreover the outer surface of the head of the launch tube cover can be coated with a layer of metallic material to prevent electro magnetic interference or radio frequency interference. The launch tube cover is constructed of a light weight, water proof material such as an expanded closed cell foam including polyurethane foam.
摘要翻译： 描述了一种导弹发射系统，其中导弹发射管的发射端由空心发射管盖保护。 发射管盖被分成多个段，这些段在导弹62的发射期间是易碎的并分散的。各个段的表面涂覆有防水材料，例如四氟乙烯或硅树脂，以防止积冰。 此外，发射管盖的头部的外表面可以涂覆有一层金属材料，以防止电磁干扰或射频干扰。 发射管盖由重量轻，防水的材料构成，例如膨胀的闭孔泡沫，包括聚氨酯泡沫。
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公开(公告)号：US6123005A
公开(公告)日：2000-09-26
申请号：US649395
申请日：1984-09-11
CPC分类号： F41F3/077
摘要： A cover closes off the open end of a missile launch canister. The cover isesigned so as to seal off the interior compartment of the canister to protect the missile or the like contained within it from moisture, contaminants and the conflagration created by nearby fired missiles. The cover is designed to maintain a minimum vapor pressure within the canister for storage purposes and to burst prior to contact by the nose of the missile contained within the canister upon the occurrence of a predetermined accumulation of vapor pressure within the canister after firing of the missile or the like. The cover is formed of a laminate of fiberglass cloths having an electromagnetic interference shield and vapor barrier adhered to the interior surface of the cover. A layer of rubber protects the fiberglass laminate from scratching or puncturing and a polyurethane layer over the rubber layer provides a moisture seal as well as insulation from other contaminants. An aluminum ring is used to secure the cover to the canister.
摘要翻译： 一个盖子关闭了导弹发射罐的开口端。 盖被设计成密封罐的内部隔间，以保护其中包含的导弹等免受潮湿，污染物和由附近的发射导弹产生的火焰。 盖被设计成在罐内保持最小的蒸汽压力用于存储目的，并且在发射预定的聚集釜内的蒸汽压力之后，在发射导弹之前在罐内的导弹的鼻子接触之前爆裂 或类似物。 盖由具有电磁干扰屏蔽和粘附在盖的内表面上的蒸汽屏障的玻璃纤维布层压制成。 一层橡胶保护玻璃纤维层压板免受划伤或刺穿，橡胶层上的聚氨酯层提供湿气密封以及与其他污染物的绝缘。 使用铝环将盖固定到罐。
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公开(公告)号：US5239909A
公开(公告)日：1993-08-31
申请号：US838458
申请日：1992-03-11
IPC分类号： F41F3/077
摘要： A missile is housed in a launcher from which it is launched by efflux gases from a thrust motor of the missile. A closure device is secured by retaining screws in a position in which it closes off the rear end of the missile and embodies a thrust generating cartridge which is fired to propel the device clear of the rear end of the missile. The closure device comprises a demand cap and base plate and the cartridge generates thrust first to release the cap and plate from the screws and then to displace the domed cap relative to the base plate to bring them to a disposition in which the momentum of the domed cap is imparted to the complete closure device thereby to propel the cap and the plate together at velocity determined by the motion of the domed cap relative to the base plate.
摘要翻译： 一枚导弹安置在发射器上，由导弹的推力马达排出的气体发射。 闭合装置通过将螺钉固定在其从导弹的后端封闭的位置而被固定，并且包括一个推力发生筒，该推进发生筒被驱动以推动该装置远离导弹的后端。 闭合装置包括需求帽和基板，并且料筒首先产生推力以从螺钉释放盖和板，然后相对于基板移动圆顶帽以使它们处于拱顶的动量 帽被赋予完整的封闭装置，从而以由圆顶盖相对于基板的运动确定的速度推动盖和板一起。
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