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    MISSILE CABLE CUTTING SYSTEM
    1.
    发明申请
    MISSILE CABLE CUTTING SYSTEM 审中-公开

    公开(公告)号：US20180347942A1

    公开(公告)日：2018-12-06

    申请号：US15989422

    申请日：2018-05-25

    申请人： AGENCY FOR DEFENSE DEVELOPMENT

    发明人： Minji BAE ,  Sanghwa KIM ,  Jonghwan KIM ,  Hajun LEE

    IPC分类号： F41F3/055

    摘要： A missile cable cutting system includes a tubular housing opened at one end and allowing a missile to be loaded therein, a cable housing fixed to and installed on one surface of the tubular housing and accommodating an umbilical cable protruding from the inside of the missile, a fixing plate installed in the cable housing and allowing the umbilical cable to be inserted between the fixing plate and the cable housing, and a cable cutter installed to be adjacent to the umbilical cable and cutting one side of the umbilical cable when the missile is fired and moved in a traveling direction.

    Umbilical cable disconnect
    3.
    发明授权
    Umbilical cable disconnect 有权
    脐带断线

    公开(公告)号：US09074842B2

    公开(公告)日：2015-07-07

    申请号：US13675925

    申请日：2012-11-13

    申请人： Raytheon Company

    发明人： Paul A. Merems

    IPC分类号： F41F3/055

    CPC分类号： F41F3/055

    摘要： An umbilical cable disconnect device is disclosed. The umbilical cable disconnect device includes a base having an opening configured to receive an umbilical cable, a cutter extending into the opening of the base, and a spacer component disposed in the opening between the cutter and the umbilical cable. The spacer component maintains separation of the cutter and the umbilical cable prior to disconnect of the umbilical cable. The cutter is operable to penetrate the spacer component in response to displacement of the disconnect device relative to the umbilical cable to facilitate cutting of the umbilical cable by the cutter to disconnect the umbilical cable.

    摘要翻译： 公开了一种脐带缆断开装置。 脐带电缆断开装置包括具有构造成接收脐带电缆的开口的基座，延伸到基座的开口中的切割器以及设置在切割器和脐带缆线之间的开口中的间隔件部件。 间隔件组件在断开脐带缆之前保持切割器和脐带缆的分离。 切割器可操作以响应于断开装置相对于脐带缆线的位移而穿透间隔件部件，以便于切割器切割脐带缆以断开脐带缆。

    Device for separating the two portions of a launcher refueling module
    4.
    发明授权
    Device for separating the two portions of a launcher refueling module 有权
    用于分离发射器加油模块的两部分的装置

    公开(公告)号：US08505429B2

    公开(公告)日：2013-08-13

    申请号：US13262304

    申请日：2010-03-30

    申请人： Aliénor Malapel ,  Mickaël Deschamps ,  Georges Verdier ,  Jean-Luc Pattyn

    发明人： Aliénor Malapel ,  Mickaël Deschamps ,  Georges Verdier ,  Jean-Luc Pattyn

    IPC分类号： F41F3/055

    CPC分类号： B64G5/00 ,  B64G1/402

    摘要： The invention relates to a separator device for separating the on-board and ground portions of a launcher fueling module, the device comprising: a locking system having a locking finger (50) mounted on the ground portion (22) and having a blocking portion (523), and a locking pin (42) on the on-board portion (21) co-operating by engaging with the blocking portion (523) in order to hold the on-board portion (21) and the ground portion (22) in a locking position. The separator system further comprises an actuation system that, under vertical movement of the launcher (10), enables the blocking portion (523) to be disengaged from the locking pin (42), whereby the on-board portion (21) is suitable for being separated from the ground portion (22). The invention also provides a method of separating the on-board and ground portions of a launcher fueling module, which method is implemented by means of such a separator device.

    摘要翻译： 本发明涉及一种用于分离发射器燃料供给模块的车载和接地部分的分离器装置，该装置包括：锁定系统，其具有安装在接地部分（22）上并具有阻挡部分（22）的锁定指（50） 523）和通过与阻挡部分（523）接合来协同工作的板上部分（21）上的锁定销（42），以便保持板上部分（21）和接地部分（22） 处于锁定位置。 分离器系统还包括致动系统，其在发射器（10）的垂直运动下使得阻挡部分（523）能够与锁定销（42）脱离接合，由此板上部分（21）适于 与地面部分（22）分离。 本发明还提供了一种分离发射器加油模块的车载和接地部分的方法，该方法通过这种分离装置实现。

    Lost-fluid hydraulic actuation system
    5.
    发明授权
    Lost-fluid hydraulic actuation system 失效
    液压液压驱动系统

    公开(公告)号：US4757960A

    公开(公告)日：1988-07-19

    申请号：US844966

    申请日：1986-03-27

    申请人： Francois Paris ,  Claude Johnson ,  Albert Lecrivain

    发明人： Francois Paris ,  Claude Johnson ,  Albert Lecrivain

    IPC分类号： B64G1/26 ,  B64G5/00 ,  F02K9/80 ,  F02K9/84 ,  F41F3/055

    CPC分类号： B64G1/26 ,  B64G5/00 ,  F02K9/805 ,  F02K9/84

    摘要： Lost-fluid hydraulic actuation system.This system makes it possible to control for a short time an element (168) in an autonomous working unit, particularly a rocket, with an onboard means (100) connected to the unit. Hydraulic fluid under pressure is introduced into the element (168) by a delivery pipe (141). A tank (130) supplies the hydraulic fluid used during the autonomous working, a helium bottle (110) puts the hydraulic fluid under pressure, and an evacuation pipe (171) evacuates the hydraulic fluid out of the autonomous unit after it has actuated the element (168).

    摘要翻译： 液压液压驱动系统。 该系统使得可以在自动工作单元（特别是火箭）中短时间地控制元件（168），其中机载装置（100）连接到该单元。 在压力下的液压流体通过输送管道（141）引入到元件（168）中。 储罐（130）供应在自主工作期间使用的液压流体，氦气瓶（110）将液压流体置于压力下，抽真空管（171）在其启动元件之后将其排出自主单元 （168）。

    Missile launcher
    6.
    发明授权
    Missile launcher 失效
    导弹发射器

    公开(公告)号：US4475436A

    公开(公告)日：1984-10-09

    申请号：US141962

    申请日：1980-04-21

    申请人： Dennis R. Campbell

    发明人： Dennis R. Campbell

    IPC分类号： F41A9/27 ,  F41F3/055 ,  F41F3/06

    CPC分类号： F41A9/27 ,  F41F3/055 ,  F41F3/06

    摘要： A rotatable support mounts a plurality of missile carrying missile launchers for rotation about a center axis. Each launcher mounts a plurality of missiles for rotation about an axis. The rotatable support is rotated to successively bring each missile launcher into a launch position. Each such launcher is rotated to successively bring each missile carried by it into a launch position.

    摘要翻译： 可旋转支撑件安装多个导弹携带导弹发射器以围绕中心轴线旋转。 每个发射器安装多个用于围绕轴旋转的导弹。 旋转的支撑件被旋转以连续地使每个导弹发射器进入发射位置。 每个这样的发射器被旋转以连续地将其携带的每个导弹发射到发射位置。

    Fin clip and connector mount
    8.
    发明授权
    Fin clip and connector mount 失效
    翅片和连接器安装

    公开(公告)号：US3921498A

    公开(公告)日：1975-11-25

    申请号：US47310474

    申请日：1974-05-24

    申请人： US NAVY

    发明人： KONGELBECK SVERRE

    IPC分类号： F41F3/04 ,  F41F3/055 ,  F42B13/32

    CPC分类号： F41F3/055 ,  F41F3/04 ,  F42B10/14

    摘要： The invention is a mounting capable of holding retracted missile fins and an umbilical electrical connector in a magazine-type launcher during long periods of storage and handling under adverse conditions without damage to the fins or connectors. The present mounting comprises a ''''wishbone'''' member having transversely extending yoke-like clips on each arm of the wishbone member, the clips holding the missile fins in a folded, retracted position prior to launch of the missile. The center of the wishbone member is pivoted at its center, the center thereof being the point of connection of the mounting to the launcher and being located at a point above the axis of the missile to minimize the effects of missile movement which act to ''''work'''' the fins in the clips and the electrical connector seated in the missile itself.

    摘要翻译： 本发明是一种能够在不利条件下在长时间的储存和处理期间将收回的导弹翅片和脐带电连接器保持在匣式发射器中而不损坏翅片或连接器的安装件。 本安装件包括在叉骨构件的每个臂上具有横向延伸的轭状夹子的“叉骨”构件，夹子在发射导弹之前将导弹翼片保持在折叠的缩回位置。 叉骨构件的中心在其中心枢转，其中心是安装件与发射器的连接点，并且位于导弹轴线上方的点处，以最小化导弹运动的作用“作用”的作用 “夹子中的翅片和位于导弹本身的电气连接器。