-
公开(公告)号：US10746503B2
公开(公告)日：2020-08-18
申请号：US16415059
申请日：2019-05-17
摘要： A launcher device for launching ammunition or weapons provided with primers, contains a plurality of launch tubes combined so as to form a launcher battery. Each of the launch tubes is loaded with ammunition or a weapon, and each of the launch tubes is closed off by a cover. A device is provided for detecting damage to the covers closing off the launch tubes.
-
公开(公告)号：US09841256B2
公开(公告)日：2017-12-12
申请号：US15403717
申请日：2017-01-11
发明人： James W. Teetzel , Gary M. Lemire
摘要： A dual purpose missile storage and launch tube device includes a tubular housing and a front cover removably covering a first end of the tubular housing, the first end defining an opening for firing a missile. A rear cover assembly removably covers a second end of the tubular housing opposite the first end. A safety mechanism is attached to the tubular housing and includes a sliding member extending through a longitudinal passageway formed in the safety mechanism. A forward portion of the sliding member engages the front cover. A rearward portion of the sliding member engages a fastener locking the rear cover assembly onto the tubular housing. The rearward portion of the sliding member is disengaged from the fastener when the front cover is removed from the first end of the tubular housing for unlocking the rear cover assembly from the tubular housing.
-
公开(公告)号：US09612085B2
公开(公告)日：2017-04-04
申请号：US14605397
申请日：2015-01-26
申请人： Sparton Corporation
发明人： David Powell , Earl Mark , Keith Huber , Taylor Durrance , Tanner Sizemore , Charles M. Nowell, Jr.
摘要： A payload launch system includes a launch tube, payload, rocket tube, pressurized motor assembly, and control system. The motor assembly has a launch actuator and an accumulator housing containing compressed gas. The accumulator housing defines a vent opening having a closure. The control system transmits an actuation signal to the actuator in response to a launch request signal to open the closure and cause a discharge of pressure into the launch tube. This causes the rocket tube to launch from the launch tube to a threshold altitude in a single gaseous thrust phase. A method includes deploying a launch system, transmitting a launch actuation signal to the launch actuator via a control system, and opening a closure to allow compressed gas to enter the launch tube, thereby launching the rocket tube from the launch tube to a threshold altitude in the single gaseous thrust phase.
-
公开(公告)号：US08851786B2
公开(公告)日：2014-10-07
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。
-
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。
-
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。
-
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。
-
公开(公告)号：US5162605A
公开(公告)日：1992-11-10
申请号：US821159
申请日：1992-01-16
申请人： Edward T. Piesik
发明人： Edward T. Piesik
CPC分类号： F41F3/077 , F41F3/0413
摘要： A structural arrangement is provided in conjunction with the upper closure of a missile cell which, upon launch of the missile, generates a rarefaction wave which assists in closing the bottom closure of the missile cell. As a result, reverse flow of exhaust gases back up into the missile chamber from an associated plenum chamber is prevented or minimized.
-
公开(公告)号：US4970937A
公开(公告)日：1990-11-20
申请号：US354416
申请日：1989-05-19
申请人： Norman R. Ward
发明人： Norman R. Ward
IPC分类号： F41F3/077
CPC分类号： F41F3/077
摘要： This invention relates to an anti-ice protector for use on open-ended projectile launch tubes. The protector is made of resiliently deformable material and is hinged to permit the protector being removed by the emerging projectile.
摘要翻译： 本发明涉及一种用于开放式射弹发射管的防冰保护器。 保护器由可弹性变形的材料制成，并被铰接以允许保护器被新出现的射弹移除。
-
公开(公告)号：US4455917A
公开(公告)日：1984-06-26
申请号：US357933
申请日：1982-03-15
申请人： Richard G. Shook
发明人： Richard G. Shook
CPC分类号： F41F3/077
摘要： A missile launch cannister end cap removal device utilizing the pressure pulse of a traveling shock wave within the cannister is disclosed. A pressure chamber, the interior of which is separated from the interior of the cannister by a diaphragm having a selected rupture pressure. Gas pressure is generated in the chamber by the firing of an explosive charge at the appropriate time in the missile launch sequence. The diaphragm is ruptured by the pressure developed in the chamber introducing a traveling shock wave into the interior of the missile cannister. The pressure pulse of the shock wave removes the end caps fitted over the open ends of the cannister.
摘要翻译： 公开了一种利用枪管内行进的冲击波的压力脉冲的导弹发射罐端盖去除装置。 压力室，其内部通过具有选定的破裂压力的隔膜与罐的内部分离。 在导弹发射序列中的适当时间通过点燃爆炸物在腔室中产生气体压力。 隔膜由室内产生的压力破裂，将行进的冲击波引入导弹罐的内部。 冲击波的压力脉冲去除了安装在罐的开口端上的端盖。
-
-
-
-
-
-
-
-
-
搜索结果
83 条记录 (耗时 0.02 秒)
