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1. 发明申请

US20140124616A1 AEROSTAT DEPLOYMENT SYSTEM AND METHODS FOR THE SAME 审中-公开
标题翻译： AEROSTAT部署系统及其相关方法
公开(公告)号：US20140124616A1
公开(公告)日：2014-05-08
申请号：US13795158
申请日：2013-03-12
申请人： Michael Alan Greco , Eric Jon Baack , Patrick Adam Thies , Bradley Roger Jensen , Justin Lee Marsh , Frank Louis Raymond, III
发明人： Michael Alan Greco , Eric Jon Baack , Patrick Adam Thies , Bradley Roger Jensen , Justin Lee Marsh , Frank Louis Raymond, III
IPC分类号： B64B1/40
CPC分类号： B64B1/40 , B64B1/58 , Y10T29/49826
摘要： An aerostat deployment system includes fore and aft envelope housings with respective folded fore and aft portions of an inflatable aerostat envelope therein. A support frame is interposed between the fore and aft envelope housings, and a payload is coupled with the inflatable aerostat envelope between the fore and aft envelope housings at the time of deployment inflation. One or more of the fore or aft envelope housings includes a brake configured to control unrolling of the folded fore or aft portions. In one example, the folded aft portion of the inflatable aerostat envelope including a tail portion is inflated prior to inflation of the folded fore portion.
摘要翻译：一种空气净化器部署系统包括前后信封壳体，其内部具有可膨胀的空气净化器信封的各自折叠的前部和后部。在前后信封壳体之间插入支撑框架，并且在展开充气时，有效载荷与前后信封壳体之间的可充气式空气净化器外壳联接。前部或后部信封外壳中的一个或多个包括构造成控制展开折叠的前部或后部的制动器。在一个示例中，包括尾部的可充气式空气净化器外壳的折叠后部部分在折叠的前部充气之前被充气。

2. 发明申请

US20160207605A1 HIGH ALTITUDE BALLOON APEX ASSEMBLY 审中-公开
标题翻译：高海拔巴勒斯坦APEX大会
公开(公告)号：US20160207605A1
公开(公告)日：2016-07-21
申请号：US14995629
申请日：2016-01-14
申请人： Brad Jensen , Josh McQuade , Derek Jensen , Eric Jon Baack
发明人： Brad Jensen , Josh McQuade , Derek Jensen , Eric Jon Baack
IPC分类号： B64B1/58 , B64B1/40
CPC分类号： B64B1/58 , B64B1/40
摘要： An atmospheric balloon comprises a membrane surrounding a chamber and extending between an upper and lower apex. An apex plate coupled to the membrane comprises a plate body including a termination opening with a portion of the membrane spread across the termination opening and a cutting device coupled to the plate body to cut the membrane to forma flight-termination opening. A fill port assembly is coupled to the plate body and in communication with the chamber. An adhesive assembly comprises one or more bridging panels that span between a first coupling interface coupled to the apex plate and a second coupling interface coupled to the membrane, and adhesive between the membrane and the apex plate, between the one or more bridging panels and the apex plate at the first coupling interface, and between the one or more bridging panels and the membrane at the second coupling interface.
摘要翻译：大气气球包括围绕室并且在上顶点和下顶点之间延伸的膜。联接到膜的顶板包括板主体，其包括终止开口，其中膜的一部分跨过终止开口延伸，以及切割装置，其联接到板体以切割膜以形成飞行终止开口。填充端口组件联接到板体并与腔室连通。粘合剂组件包括一个或多个桥接面板，其跨越耦合到顶点板的第一耦合界面和耦合到膜的第二耦合界面，以及膜和顶板之间的粘合剂，位于一个或多个桥接面板和在第一耦合界面处的顶点板，以及在第二耦合界面处的一个或多个桥接面板和膜之间。

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