公开(公告)号：US06805842B1

公开(公告)日：2004-10-19

申请号：US09976628

申请日：2001-10-12

申请人： Kevin S. Bodner ,  Tyler A. Palmer ,  Pejman Ghanouni

发明人： Kevin S. Bodner ,  Tyler A. Palmer ,  Pejman Ghanouni

IPC分类号： B01L300

CPC分类号： B01L3/505 ,  B01L3/0217 ,  B01L3/50825 ,  B01L3/5085 ,  B01L2200/142 ,  B01L2300/044 ,  B01L2300/047 ,  B01L2300/0672 ,  B01L2300/0854 ,  B01L2400/0478

摘要： A sample container for minimizing evaporation of a contained volume of sample includes a container housing, a repuncturable self-sealing membrane, and a collapsible sample bag. The container housing includes an open end and a hollow interior region. The repuncturable self-sealing membrane configured to self-seal after repeated punctures is engaged in the open end of the container housing and includes an exterior surface exposed to the external environment and an interior surface oriented toward the hollow interior region of the container housing. The collapsible sample bag includes a proximate end that is permanently attached to the interior surface of the repuncturable self-sealing membrane.

摘要翻译： 用于最小化容纳体积的样品的蒸发的样品容器包括容器壳体，可重复的自密封膜和可折叠样品袋。 容器壳体包括开口端和中空的内部区域。 构造为在重复穿刺之后自密封的可重复使用的自密封膜被接合在容器壳体的开口端中，并且包括暴露于外部环境的外表面和朝向容器壳体的中空内部区域定向的内表面。 可折叠的样品袋包括永久地附着到可再次自密封膜的内表面的近端。

公开(公告)号：US06308919B1

公开(公告)日：2001-10-30

申请号：US09558444

申请日：2000-04-25

申请人： Tyler A. Palmer ,  Varouj G. Baghdasarian

发明人： Tyler A. Palmer ,  Varouj G. Baghdasarian

IPC分类号： B64G122

CPC分类号： H01Q1/1207 ,  B64G1/222 ,  B64G1/645 ,  B64G1/66 ,  H01Q1/288

摘要： A spacecraft having nested reflectors that are released and deployed during a single release event using one or more dual reflector holddowns. The nested reflectors are held in place prior to release by the holddowns and are released during the single release event. The nested reflectors are secured to the body of the spacecraft by hinges attached to respective reflector backup structures and are releasably secured to the body using the one or more dual reflector holddowns. The reflector backup structures are secured by reflector interface brackets of the respective holddowns. An exemplary holddown has a separable tubular housing that is longitudinally secured together between an end cap and a release device. A threaded shaft 28 extends through the tubular housing, the end cap and the release device. A retraction spring is disposed around the exterior of the housing. The reflector interface brackets are secured to the outer and inner housings that attach the plurality of reflectors to the holddown.

摘要翻译： 具有嵌套反射器的航天器，其在单个释放事件期间使用一个或多个双反射器按压来释放和部署。 嵌套的反射器在通过压缩释放之前保持原位，并在单次发布事件期间释放。 嵌套的反射器通过连接到相应的反射器支撑结构的铰链固定到航天器的主体，并且使用一个或多个双反射器按压可释放地固定到主体。 反射器支撑结构由相应的压盖的反射器接口支架固定。 示例性的压紧具有可分离的管状壳体，其在端盖和释放装置之间纵向地固定在一起。 螺纹轴28延伸穿过管状壳体，端盖和释放装置。 退避弹簧设置在壳体的外部周围。 反射器接口支架固定到将多个反射器连接到压紧件的外壳体和内壳体上。