公开(公告)号：US06193535B1

公开(公告)日：2001-02-27

申请号：US09502027

申请日：2000-02-10

申请人： James E. Ayers ,  Shohreh Sedighi ,  John D. Kisch ,  David J. Hernandez, Jr.

发明人： James E. Ayers ,  Shohreh Sedighi ,  John D. Kisch ,  David J. Hernandez, Jr.

IPC分类号： H01R1362

CPC分类号： F41F3/04 ,  H01R13/533 ,  H01R13/633 ,  Y10S439/933

摘要： A connector assembly which includes conventional components that are well known in the connector assembly field but which includes within it an improved ceramic deadface which is located at a front face plate on an interior portion of the connector assembly. If the connector is separated so that the deadface is exposed, then in the event that location with the deadface exposed faces an area of extreme high temperature, the deadface preserves the connector assembly and prevents internal components including plugs and wires from being destroyed or melted. The connector assembly involves the incorporation of a novel ceramic deadface on the interior portion of the connector assembly which is able to withstand extreme high temperatures.

摘要翻译： 一种连接器组件，其包括在连接器组件领域中众所周知的常规部件，但在其内部包括改进的陶瓷死体，其位于连接器组件内部的前面板上。 如果连接器被分开以使得暴露出来，那么在暴露暴露的位置的位置面临极高温度的区域的情况下，死角保留连接器组件，并且防止包括插头和电线的内部部件被破坏或熔化。 连接器组件包括在连接器组件的内部部分上并入新颖的陶瓷底面，其能够承受极高的温度。

公开(公告)号：US06679177B1

公开(公告)日：2004-01-20

申请号：US10131903

申请日：2002-04-24

申请人： Jui-Yu Wu ,  Matthew B. Dalton ,  John D. Kisch

发明人： Jui-Yu Wu ,  Matthew B. Dalton ,  John D. Kisch

IPC分类号： F42B1510

CPC分类号： F42B15/36 ,  Y10T403/581

摘要： A hold-down and release apparatus for a flight termination system having a terminal portion for holding-down and releasing a structural object which has an arrangement for attaching to the flight termination system. The hold-down and release apparatus includes several movable clamping segments provided on the terminal portion of the flight termination system that are engageable in a complimentary fashion with the attachment arrangement on the structural object for releasably attaching the structural object to the flight termination system. The hold-down and release apparatus also includes springs for biasing the movable clamping segments means in a disengaging direction that causes the clamping segments to disengage from the attachment arrangement on the structural object to release the structural object from the flight termination system. The hold-down and release apparatus further includes a release band attached to the movable clamping segments for preventing the disengaging movement of the movable clamping segments such that they remain engaged to the attachment arrangement of the structural object for releasably attaching the structural object to the flight termination system. The release band is held in position by two non-explosive actuators (NEAs), such that either one or both actuators may initiate the release and loosen the release band which allows the movable clamping segments to move under the urge of the biasing, springs to disengage the complimentary attachment arrangement from the attachment arrangement of the structural object, to release the structural object from the flight termination system.

摘要翻译： 一种用于飞行终点系统的按压和释放装置，具有用于按压和释放具有用于附接到飞行终点系统的装置的结构物体的终端部分。 压紧和释放装置包括设置在飞行终端系统的终端部分上的多个可移动的夹紧段，其能够以与结构物体上的附接装置互补的方式接合，以将结构物体可释放地附接到飞行终点系统。 压紧和释放装置还包括弹簧，用于使分离方向偏置可动夹紧段装置，使得夹紧段与结构物体上的附接装置分离，以将结构物体从飞行终端系统释放。 压紧和释放装置还包括附接到可动夹紧段的释放带，用于防止可动夹紧段的分离运动，使得它们保持接合到结构物体的附接装置，以将结构物件可释放地附接到飞行 终止系统。 释放带由两个非爆炸致动器（NEAs）保持就位，使得一个或两个致动器可以启动释放并松开释放带，其允许可动夹紧段在偏压的推动下移动，弹簧到 将互补的附接装置与结构物体的附接装置分离，以将结构物体从飞行终点系统释放。