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31. 发明申请

US20160297546A1 Self Transportable Aerostat System 有权
标题翻译：自动运输气动系统
公开(公告)号：US20160297546A1
公开(公告)日：2016-10-13
申请号：US15185740
申请日：2016-06-17
申请人： TCOM, L.P.
发明人： Edward Cunningham , Han Dinh Phan
IPC分类号： B64F1/14 , B64D47/08 , B64B1/58 , B64B1/66 , B64B1/50
CPC分类号： B64F1/14 , B64B1/50 , B64B1/58 , B64B1/66 , B64D47/08 , B64F1/12
摘要： A self transportable aerostat system comprising: a first motorized mooring truck; a mooring tower removable attached to a base assembly of the first mooring truck, generally vertically arranged in relation to the bed of the first mooring truck; a proximal and distal boom deck removably attached to the base assembly; a flying sheave for redirecting a tether carried by the base assembly and attachable to an aerostat; a second motorized mooring truck attachable to the outer edge of the distal boom; and, an aerostat truck having an electrical connection for connecting to the first mooring truck and having an aerostat storage compartment for storing the aerostat is a retracted configuration.
摘要翻译：一种可自行运送的空气净化系统，包括：第一电动系泊车; 一个可移动的系泊塔，可连接到第一系泊车的基座组件上，大致垂直地布置成相对于第一系泊车的床; 可拆卸地附接到基座组件的近侧和远侧臂架甲板; 用于重新定向由基座组件承载的系绳并可附接到空气净化器的飞轮; 第二电动系泊车可附接到远端吊杆的外缘; 并且具有用于连接到第一系泊卡车的电气连接并且具有用于存储空气净化器的空气净化器储藏室的空气净化器卡车是缩回构型。

32. 发明申请

US20160288895A1 FILLING APPARATUS FOR HIGH-ALTITUDE BALLOONS 有权
公开(公告)号：US20160288895A1
公开(公告)日：2016-10-06
申请号：US15161613
申请日：2016-05-23
申请人： Google Inc.
发明人： Kyle Brookes
IPC分类号： B64B1/58 , B64B1/40
CPC分类号： B64B1/58 , B64B1/40 , B64F5/00 , Y10T137/3584
摘要： High-altitude balloons and apparatuses for filling such high-altitude balloons are provided. As an example, an apparatus for filling a high-altitude balloon includes a tube extending through envelope material of the balloon is provided. The apparatus also includes a flange connected to a first end of the tube. The flange is connected to an interior surface of the balloon. A fitting is connected to a second end of the tube. The fitting is configured for attachment with an apparatus for filling the balloon with lift gas. In addition, methods of filling high-altitude balloons with lift gas and methods of manufacturing balloons are also provided.

33. 发明申请

US20160263815A1 SYSTEM FOR CONSTRUCTING BALLOON ENVELOPES 有权
标题翻译：构建气球包装系统
公开(公告)号：US20160263815A1
公开(公告)日：2016-09-15
申请号：US15160140
申请日：2016-05-20
申请人： Google Inc.
发明人： Kevin Roach , Jeffrey Neri , Daniel Henry Fourie
IPC分类号： B29C65/18 , B64B1/58
CPC分类号： B29C65/18 , B29C65/226 , B29C65/30 , B29C65/4825 , B29C65/50 , B29C65/743 , B29C65/7802 , B29C65/7847 , B29C66/0044 , B29C66/1122 , B29C66/133 , B29C66/244 , B29C66/3452 , B29C66/474 , B29C66/71 , B29C66/836 , B29C66/86533 , B29C66/9672 , B29K2623/06 , B29L2022/022 , B64B1/58 , B29K2011/00 , B29K2023/06 , B29K2067/003
摘要： An assembly for use during manufacture of a balloon envelope that includes a table having first and second levels, an indicator disposed on the first level and a sealing component. The first level is arranged to receive a first sheet portion of material. The indicator is arranged along a lengthwise axis of the table to indicate a position for attaching a tendon to the first sheet portion. The second level is arranged to receive assembled gore portions of the envelope comprising the first sheet portion, the tendon and a second sheet portion of material. The sealing component is configured to move along the table and to apply a heat seal to bond together the first and second sheet portions disposed thereon in order to form at least part of a gore portion of the envelope, such that the tendon is arranged proximate to a centerline of the gore.
摘要翻译：一种用于制造球囊的组件，包括具有第一和第二层的工作台，设置在第一层上的指示器和密封部件。第一级布置成接收材料的第一片材部分。指示器沿着桌子的纵向轴线布置以指示用于将腱附接到第一片部分的位置。第二级布置成接收包围第一片部分，腱和材料的第二片部分的封套的组装的部分。密封部件被构造成沿着工作台移动并且施加热密封以将布置在其上的第一和第二片部分结合在一起，以便形成包封部分的至少一部分，使得腱布置成靠近戈尔的中心线。

34. 发明授权

US09399506B2 Self transportable aerostat system 有权
标题翻译：自动运输航空器系统
公开(公告)号：US09399506B2
公开(公告)日：2016-07-26
申请号：US13735728
申请日：2013-01-07
申请人： TCOM, LP
发明人： Edward Cunningham , Han Dinh Phan
IPC分类号： B64F1/14 , B64B1/66 , B64B1/58 , B64F1/12 , B64B1/50
CPC分类号： B64F1/14 , B64B1/50 , B64B1/58 , B64B1/66 , B64D47/08 , B64F1/12
摘要： A self transportable aerostat system comprising: a first motorized mooring truck; a mooring tower removably attached to a base assembly of the first mooring truck, generally vertically arranged in relation to the bed of the first mooring truck; a proximal and distal boom deck removably attached to the base assembly; a flying sheave for redirecting a tether carried by the base assembly and attachable to an aerostat; a second motorized mooring truck attachable to the outer edge of the distal boom; and, an aerostat truck having an electrical connection for connecting to the first mooring truck and having an aerostat storage compartment for storing the aerostat is a retracted configuration.
摘要翻译：一种可自行运送的空气净化系统，包括：第一电动系泊车; 系泊塔可移除地附接到第一系泊车的基座组件，其大致垂直地布置成相对于第一系泊车的床; 可拆卸地附接到基座组件的近侧和远侧臂架甲板; 用于重新定向由基座组件承载的系绳并可附接到空气净化器的飞轮; 第二电动系泊车可附接到远端吊杆的外缘; 并且具有用于连接到第一系泊卡车的电气连接并且具有用于存储空气净化器的空气净化器储藏室的空气净化器卡车是缩回构型。

35. 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。

36. 发明授权

US09352820B2 Device mount for an inflatable structure 有权
标题翻译：用于充气结构的设备安装
公开(公告)号：US09352820B2
公开(公告)日：2016-05-31
申请号：US13466415
申请日：2012-05-08
申请人： Robert B. Williams , Kyle W. Maxhimer , Larry L. Lai , Thomas Brennan
发明人： Robert B. Williams , Kyle W. Maxhimer , Larry L. Lai , Thomas Brennan
IPC分类号： B64B1/00 , B64B1/58 , B64B1/14 , H01Q1/12
CPC分类号： B64B1/58 , B64B1/14 , H01Q1/1292
摘要： An inflatable structure mount is used for mounting a device to an inflatable structure. An example is mounting of radar panels to an inflatable structure within an airship. The mount includes the device, and inserts coupled to the back side of the device, which mechanically couple to flexures mounted on the inflatable structure. Some of the flexures may have slotted holes, used in positioning the inserts on the inflatable structure at positions that will allow the flexures to mate with the inserts. A jig or tool may be used as part of the installation process, to locate the flexures at points where they will properly engage the inserts. The flexures may also each face a center point that is underneath the device to be mounted. The flexures may engage the inserts in ways that allow for quick installation and de-installation of devices, and may allow for visual inspection of proper installation.
摘要翻译：可充气结构安装座用于将装置安装到可充气结构上。一个例子是将雷达面板安装到飞艇内的可充气结构中。该安装件包括该装置，以及联接到该装置的后侧的插入件，其机械地联接到安装在该可充气结构上的挠曲件。一些弯曲部可以具有开槽孔，用于将插入件定位在可膨胀结构上的位置，以允许挠曲件与插入件配合。可以使用夹具或工具作为安装过程的一部分，以便在将它们正确接合插入件的位置处定位挠曲件。挠曲件也可以各自面向要安装的装置下方的中心点。挠曲件可以以允许快速安装和拆卸设备的方式接合插入件，并且可以允许目视检查正确的安装。

37. 发明授权

US09327844B2 Methods and mechanisms for balloon launching 有权
标题翻译：气球发射的方法和机制
公开(公告)号：US09327844B2
公开(公告)日：2016-05-03
申请号：US14179710
申请日：2014-02-13
申请人： Google Inc.
发明人： Daniel Ratner
IPC分类号： B64B1/40 , B64F1/04 , B64B1/58
CPC分类号： B64B1/005 , B64B1/40 , B64B1/58 , B64F1/04
摘要： A method for balloon launching may include loading a pre-packaged balloon and payload into a shell structure. The pre-packaged balloon may be pulled out of its packaging in a vertical direction, for instance using a gantry crane. The gantry crane may be configured to inflate the balloon from the top of the envelope. The balloon may be inflated while substantially within the shell structure, which may provide protection from wind gusts. A vehicle, such as a heavy forklift, may provide mobility and support for the balloon and shell. Once the balloon is inflated, the vehicle may move the balloon/shell combination at a rate and direction substantially matching the current wind direction/speed. Furthermore, after reaching a zero-velocity condition relative to the wind, the vehicle may assist and/or initiate the opening of the shell. A tether connecting the balloon to the shell structure may be disconnected, allowing the balloon to launch.
摘要翻译：用于气球发射的方法可以包括将预先包装的气囊和有效载荷装载到壳结构中。预包装的气囊可以在垂直方向从其包装中拉出，例如使用龙门式起重机。龙门式起重机可以被配置成从信封的顶部使气囊膨胀。气囊可以在基本上在壳结构内充气，这可以提供防风阵风的保护。诸如重型叉车的车辆可以为气球和壳提供移动性和支撑。一旦气囊膨胀，车辆可以以基本上与当前风向/速度相匹配的速率和方向移动气囊/壳组合。此外，在相对于风达到零速度状态之后，车辆可以辅助和/或启动壳体的打开。将气球连接到壳结构的系绳可能会断开，从而允许气球发射。

38. 发明申请

US20160096612A1 SUPER-PRESSURE BALLOON 审中-公开
标题翻译：超压气球
公开(公告)号：US20160096612A1
公开(公告)日：2016-04-07
申请号：US14870288
申请日：2015-09-30
申请人： Aether Industries, LLC.
发明人： Benjamin Longmier , John Mark Guthery , John Patrick Sheehan
IPC分类号： B64B1/44 , B64B1/58
CPC分类号： B64B1/44 , B64B1/58
摘要： A payload delivery and recovery system, having a payload including a data collection device arranged to collect data, and a controllable ascent vehicle comprising a controllable lighter than air (LTA) mechanism detachably coupled to the payload and used during an ascent phase to deliver the payload to a pre-determined altitude. The LTA mechanism includes low cost super-pressure balloons.
摘要翻译：一种有效载荷递送和恢复系统，其具有包括布置成收集数据的数据收集装置的有效载荷，以及包括可拆卸地耦合到有效载荷并在上升阶段期间用于传递有效载荷的空气（LTA）机构的可控的轻量级车辆到一个预定的高度。 LTA机制包括低成本超压气球。

39. 发明授权

US09193480B2 High altitude balloon system 有权
标题翻译：高空气球系统
公开(公告)号：US09193480B2
公开(公告)日：2015-11-24
申请号：US13827779
申请日：2013-03-14
申请人： Raven Industries, Inc.
发明人： Michael Smith , Kurt Sehnert , Randy Scott , Justin Lee Marsh , Mark L. West
IPC分类号： B64B1/02 , B64D45/02 , B64B1/44 , B64B1/70 , B64B1/30 , B64B1/42 , B64B1/58
CPC分类号： B64B1/08 , B64B1/30 , B64B1/42 , B64B1/44 , B64B1/58 , B64B1/70 , B64D45/02 , Y10T156/10
摘要： A high altitude balloon system includes a dual chamber balloon extending from an upper apex to a lower apex with a circumferential edge between the upper and lower apexes. A deflectable diaphragm is within the dual chamber balloon and coupled along the circumferential edge. The deflectable membrane divides the dual chamber balloon into a lift gas chamber formed by an interior surface of the dual chamber balloon and the deflectable diaphragm, and a ballast chamber formed by the interior surface of the dual chamber balloon and the deflectable diaphragm. Optionally, the dual chamber balloon is constructed by interposing the deflectable diaphragm between an upper and lower balloon panels. Each of the upper and lower balloon panels and the deflectable diaphragm are then coupled together along the circumferential edge to form both the lift gas chamber and the ballast chamber.
摘要翻译：高空气球系统包括从上顶点延伸到下顶点的双室气囊，其中上和下顶点之间具有圆周边缘。可偏转隔膜位于双室气囊内并且沿圆周边缘连接。可偏转膜将双室气囊分成由双室气囊和可偏转隔膜的内表面形成的提升气室，以及由双室气囊的内表面和可偏转膜片形成的镇流室。可选地，双室气囊通过将可偏转隔膜插入在上气囊面板和下气囊面板之间来构造。上，下气囊板和可偏转隔膜中的每一个然后沿着圆周边缘连接在一起以形成提升气室和镇流器室。

40. 发明申请

US20150203184A1 SAIL-EQUIPPED AMPHIBIOUS AEROSTAT OR DIRIGIBLE 审中-公开
标题翻译：安全的大型航空航天或可靠的
公开(公告)号：US20150203184A1
公开(公告)日：2015-07-23
申请号：US14157798
申请日：2014-01-17
申请人： JOSEPH NILO SARMIENTO
发明人： JOSEPH NILO SARMIENTO
IPC分类号： B64B1/24 , B64B1/36 , B64B1/10 , B64B1/58 , B64B1/70 , B64B1/66 , B64B1/68 , B64B1/02 , B64B1/20
CPC分类号： B64B1/24 , B64B1/02 , B64B1/10 , B64B1/20 , B64B1/36 , B64B1/66 , B64B1/68 , B64B1/70
摘要： A highly maneuverable craft or airship with aerostatic lift which may be manned or operated autonomously and remotely consists, in particular, a sail or similar device for main propulsion; the aerostat or dirigible sustains lift from gasbags containing helium or hydrogen or other similar lighter-than-air gas. Further, said aerostat may be mounted with a wind turbine for electrical power generation and mechanical operation; and, ballast tanks and landing gear to enable amphibious capability.
摘要翻译：具有空气静力升降机的高度机动的飞艇或飞艇可以自主和远程地进行人员操作或操作，特别是用于主推进的帆或类似装置; 空气稳定器或气体可以从包含氦气或氢气或其他类似轻型空气气体的气囊中维持升力。此外，所述空气净化器可以安装有用于发电和机械操作的风力涡轮机; 以及压载舱和起落架，以实现两栖能力。

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