公开(公告)号：US07874091B2

公开(公告)日：2011-01-25

申请号：US12165071

申请日：2008-06-30

Applicant: Jyun-Horng Fu ,  Robert James Howard ,  John W. Rapp ,  Antonio Paulic

Inventor： Jyun-Horng Fu ,  Robert James Howard ,  John W. Rapp ,  Antonio Paulic

IPC: F41C9/06

CPC classification number: F41C9/06 ,  F41A21/32 ,  F41F3/08 ,  F41F3/10

Abstract: An apparatus for sealing the barrel of an underwater gun between firings is disclosed. The apparatus comprises a magnetically-attractable water-impermeable disk. Via operation of a drive system, the disk is movable between a sealing position, wherein it prevents water from entering the barrel by moving into alignment with the first bore, and a firing position, wherein the first water-impermeable disk moves out of alignment with the first bore.

Abstract translation: 公开了一种用于在发射之间密封水下枪的枪管的装置。 该装置包括可吸引不透水的盘。 通过驱动系统的操作，盘可以在密封位置之间移动，密封位置通过与第一孔对准而防止水进入筒体，以及击发位置，其中第一不透水盘移动不对准与 第一个孔。

公开(公告)号：US07523714B1

公开(公告)日：2009-04-28

申请号：US11499972

申请日：2006-08-02

Applicant: Michael T. Ansay ,  Michael D. Wray ,  George M. Duarte

Inventor： Michael T. Ansay ,  Michael D. Wray ,  George M. Duarte

IPC: B63G8/28

CPC classification number: B63G8/30 ,  B63G8/32 ,  F41A17/00 ,  F41F3/08 ,  F41F3/10

Abstract: A hydraulic circuit for prevention of inadvertent weapons launches in which a hydraulic firing valve provides hydraulic pressure to a backup select valve rather than the backup select valve receiving hydraulic pressure directly from a ship supply header. This hydraulic pressure shifts the backup select valve to allow hydraulic pressure to pass to a mode select control valve that actuates a controllable air-firing valve, until a hydraulic firing valve for the weapon is opened. The backup select valve actuation can only occur with the initiation of the hydraulic firing valve. Only after the hydraulic firing valve is open, does the backup select valve initiate hydraulic pressure to the mode select control valve thereby preventing hydraulic actuation of the backup select valve.

Abstract translation: 一种用于防止意外武器发射的液压回路，其中液压点火阀向备用选择阀提供液压，而不是直接从船舶供应头接收液压的备用选择阀。 这种液压压力使备用选择阀移动，以允许液压通过模式选择控制阀，该模式选择控制阀致动可控制的空气启动阀，直到用于武器的液压点火阀打开。 备用选择阀致动只能在液压启动阀的启动时才会发生。 仅在液压点火阀打开之后，备用选择阀是否向模式选择控制阀启动液压，从而防止备用选择阀的液压致动。

公开(公告)号：US07506570B1

公开(公告)日：2009-03-24

申请号：US12001595

申请日：2007-12-10

Applicant: Samuel R. Koski

Inventor： Samuel R. Koski

IPC: F41F3/052

CPC classification number: F41F3/052 ,  F41F3/08 ,  F42B39/22

Abstract: A device is provided for holding and releasing a missile within a canister. The device includes a housing attached to the canister, a latch mechanism extending from the housing into the canister, a tension applier disposed in the housing to restrain the missile in the canister, a release mechanism disposed on the housing, an interface mechanism and a compression applier. The tension applier forces the latch mechanism against the housing to withdraw from the missile. The interface mechanism initially couples the release mechanism and the tension applier. The compression applier anchors to the interface mechanism and forces the latch mechanism against the housing to engage the missile and counteract said tension applier. On command, the release mechanism disengages from the housing to release the compression applier from the interface mechanism. This action enables the tension applier to withdraw the latch mechanism from the missile.

Abstract translation: 提供一种用于在罐内保持和释放导弹的装置。 该装置包括附接到罐的壳体，从壳体延伸到罐中的闩锁机构，设置在壳体中的张力施加器以将导弹限制在罐中，设置在壳体上的释放机构，接口机构和压缩 应用者 紧张施加器迫使闩锁机构抵靠壳体从导弹退出。 接口机构最初将释放机构和张力施加器联接起来。 压缩施加器锚固到接口机构并且迫使闩锁机构抵靠壳体接合导弹并抵消所述张力施加器。 按照命令，释放机构与壳体脱离接合机构释放压缩施加器。 该动作使紧张施加器能够从导弹中撤出闩锁机构。

公开(公告)号：US06577990B1

公开(公告)日：2003-06-10

申请号：US09606114

申请日：2000-06-12

Applicant: Dominik A. Kotlow ,  Peter R. Witting ,  James W. Coleman

Inventor： Dominik A. Kotlow ,  Peter R. Witting ,  James W. Coleman

IPC: H04B1500

CPC classification number: F41F3/08

Abstract: A method is provided to process system test data to determine certification parameters of the system based on the test data. For a torpedo launch system, the velocity data is generated by a Pressure/Velocity/Displacement housing interfaced with a computer based data acquisition system and known launch system and test parameters, such as sample rate, muzzle exit length, time of acquisition, decimation factor and low pass cutoff frequency are provided as inputs. The method forces assigns a value of zero to any data less than a predetermined threshold in order to eliminate non-zero levels contributed by ambient noise. The method then passes the data through a filter chosen to agree with hand fit smoothing methods, so as to obtain a smoothed velocity profile. The smoothed data is processed to obtain and display an acceleration profile and a displacement profile, as well as data points for peak acceleration, time at peak, acceleration pulse width, muzzle exit velocity and time at exit.

Abstract translation: 提供了一种处理系统测试数据以根据测试数据确定系统的认证参数的方法。 对于鱼雷发射系统，速度数据由与基于计算机的数据采集系统接口的压力/速度/位移壳体产生，已知的发射系统和测试参数，例如采样率，枪口出口长度，采集时间，抽取因子 并提供低通截止频率作为输入。 为了消除由环境噪声引起的非零电平，方法力将零值分配给小于预定阈值的任何数据。 然后，该方法将数据通过选择的滤波器来与手拟合平滑方法一致，以便获得平滑的速度分布。 对平滑的数据进行处理，以获得和显示加速度曲线和位移曲线，以及峰值加速度，峰值时间，加速度脉冲宽度，枪口出口速度和出口时间的数据点。

公开(公告)号：US06367307B1

公开(公告)日：2002-04-09

申请号：US09267916

申请日：1999-03-02

Applicant: Christa M. Reise ,  James C. Butts

Inventor： Christa M. Reise ,  James C. Butts

IPC: G01N330

CPC classification number: F41F3/08 ,  G01N3/30 ,  G01P15/123

Abstract: A calibrated stop bolt is provided for measuring the dynamic load transmitted to the calibrated stop bolt during a shock test. The stop bolt includes an anterior extension and a posterior extension, for restraining a torpedo bearing plate therebetween, and also includes a plurality of strain gauges mounted at the top portion of each extension. In one embodiment, eight strain gauges are utilized, with two strain gauges placed on each side of the two extensions, i.e., in a full bridge arrangement. The calibrated stop bolt is preferably mounted to a base plate and bolted at each end to a longitudinal test fixture. The calibrated stop bolt can be utilized with a conventional longitudinal shock test fixture, torpedo shape and heavy weight shock machine.

Abstract translation: 提供了一个校准的止动螺栓，用于测量在冲击试验期间传递到校准止动螺栓的动态载荷。 止动螺栓包括前延伸部和后延伸部，用于在其间限制鱼雷支承板，并且还包括安装在每个延伸部的顶部的多个应变计。 在一个实施例中，使用八个应变计，其中两个应变计放置在两个延伸部的每一侧，即全桥布置。 校准的止动螺栓优选地安装到基板并且在每个端部处螺栓连接到纵向测试夹具。 校准的止动螺栓可以与传统的纵向冲击试验夹具，鱼雷形状和重型冲击机一起使用。

公开(公告)号：US5174236A

公开(公告)日：1992-12-29

申请号：US907760

申请日：1992-06-29

Applicant: Paul E. Moody

Inventor： Paul E. Moody

IPC: B63G8/32 ,  F41F3/08

CPC classification number: B63G8/32 ,  F41F3/08

Abstract: A positioning assembly for a torpedo having a projection thereon including support mounted on the torpedo tube adjacent the projection, and a control member movable on the support transversely of the torpedo tube. The control member has a control surface with a series of abutment surfaces for the projection to limit motion of the torpedo within the tube. A first transverse abutment surface limits movement of the torpedo towards the muzzle end of the tube during loading, and a second transverse abutment surface cooperates with a portion of the first abutment surface to limit movement of the torpedo in either direction axially in the tube. The control member is movable on the support to (i) a first position wherein the projection is engageable with only the first abutment surface, (ii) a second position wherein the projection is disposed between the first and second abutment surfaces, and (iii) a third position wherein the projection is free from the first abutment surface so that the torpedo is movable towards the muzzle end of the tube.

Abstract translation: 一种用于鱼雷的定位组件，其上具有突出部，其上包括安装在与鱼雷管相邻的突起的鱼雷管上的支撑;以及控制构件，其可在鱼雷管的横向上在支架上移动。 控制构件具有控制表面，该控制表面具有用于突出物的一系列邻接表面，以限制鱼雷在管内的运动。 第一横向邻接表面限制在加载期间鱼雷向管口的运动，并且第二横向邻接表面与第一邻接表面的一部分配合以限制鱼雷在管中沿任一方向的运动。 控制构件可在支撑件上移动（i）第一位置，其中突起仅与第一邻接表面接合，（ii）第二位置，其中突起设置在第一和第二邻接表面之间，和（iii） 第三位置，其中所述突起远离所述第一邻接表面，使得所述鱼雷能够朝向所述管的所述枪口端移动。

公开(公告)号：US3962951A

公开(公告)日：1976-06-15

申请号：US563993

申请日：1975-04-01

Applicant: Jan M. Schenk

Inventor： Jan M. Schenk

IPC: F41F3/077 ,  F41F3/08 ,  F41F3/04

CPC classification number: F41F3/08 ,  F41F3/077 ,  Y10T403/60 ,  Y10T403/69

Abstract: The missile launching assembly includes a mount tube having a circumferenl tapered continuous groove, a launch tube within the mount tube, a shatterable end closure on the end of the launch tube adapted to be shattered when the missile is launched, a locking device in the form of a single split ring or a plurality of arcuate-shaped ring segments with a cross-section to match the groove taper positioned within the groove and between the mount tube and the flange of the end closure, and one or more circumferentially oriented spreading elements, such as expanding jackscrews fitted into the ring or ring segments for increasing the ring circumference to bring pressure to bear on the closure flange. The launch tube is designed to contain therein in a lengthwise direction the missile to be fired.The mount tube is a permanent part of the vehicle such as a submarine, from which the missile is to be launched.

Abstract translation: 导弹发射组件包括具有周向锥形连续槽的安装管，安装管内的发射管，发射管端部上的可破碎的端盖，适于在发射导弹时被破碎;形式的锁定装置 具有横截面以匹配定位在凹槽内的凹槽锥形以及安装管与端盖的凸缘之间以及一个或多个圆周定向的扩展元件的多个弧形环段， 例如安装在环或环段中的膨胀式螺旋桨，用于增加环形周长以使压力承受在封闭法兰上。 发射管设计成在其长度方向上容纳待发射的导弹。

公开(公告)号：US3109343A

公开(公告)日：1963-11-05

申请号：US57330656

申请日：1956-03-22

Applicant: GONDEK JOHN T

Inventor： GONDEK JOHN T

IPC: F41F3/08

CPC classification number: F41F3/08

公开(公告)号：US3106905A

公开(公告)日：1963-10-15

申请号：US65264257

申请日：1957-03-29

Applicant: GONDEK JOHN T

Inventor： GONDEK JOHN T

IPC: F41F3/08

CPC classification number: F41F3/08

公开(公告)号：US2342996A

公开(公告)日：1944-02-29

申请号：US37905241

申请日：1941-02-15

Applicant: HUBERT SCOTT PAINE

Inventor： NETHERWOOD BARKER STUART ,  SIDNEY SELMAN GEORGE

IPC: F41F3/08

CPC classification number: F41F3/08