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1. 发明公开

EP4402049A1 SYSTEMS AND METHODS FOR MEASURING LIFT OF A GAS CELL 审中-公开
公开(公告)号：EP4402049A1
公开(公告)日：2024-07-24
申请号：EP22881599.9
申请日：2022-10-07
申请人： LTA Research And Exploration, LLC
发明人： VERNYI, Kyle , CARTER, Dennis, L. , WITTMER, Jonathan
IPC分类号： B64B1/62 , B64D45/00
CPC分类号： B64B1/06 , B64B1/62 , G01B5/0021 , G01B11/24

2. 发明公开

EP3390217A1 LIGHTER-THAN-AIR PLATFORM 审中-公开
公开(公告)号：EP3390217A1
公开(公告)日：2018-10-24
申请号：EP16876247.4
申请日：2016-11-02
申请人： Skycom Corporation
发明人： MICHAELIS IV, Max, G. , BENNETT, John, H. H.
IPC分类号： B64B1/00 , B64B1/02 , B64B1/40 , B64B1/44 , B64B1/58 , B64B1/62
CPC分类号： H02S20/32 , B64B1/12 , B64B1/30 , B64B1/58 , B64B1/62 , B64C2201/022 , B64C2201/122 , B64C2201/208 , H02S10/40 , H02S30/20
摘要： Techniques are disclosed relating lighter-than-air aircraft. Such aircraft may be used for various purposes, such as providing network connectivity to areas that would otherwise lack such connectivity. For example, in some embodiments, a lighter-than-air aircraft according to this disclosure may include various types of antennas (directional or non-directional) for communicating with ground-based electronics or with other lighter-than-air aircraft.

3. 发明授权

EP2873166B1 GEO-FENCING 有权
标题翻译：地理围栏
公开(公告)号：EP2873166B1
公开(公告)日：2017-10-18
申请号：EP13816293.8
申请日：2013-05-09
申请人： X Development LLC
发明人： TELLER, Eric , DEVAUL, Richard, Wayne , WEAVER, Joshua , BIFFLE, Clifford, L. , RHODES, Bradley , STAAF, Anton
IPC分类号： H04B7/185 , H04W4/00 , H04W84/02 , H04B10/112 , G05D1/10 , B64D1/02 , B64B1/40 , B64B1/62
CPC分类号： B64B1/40 , B64B1/62 , B64D1/02 , G05D1/105 , H04B10/1129 , H04W84/02

4. 发明授权

EP2864194B1 BALLON STRATOSPHÉRIQUE À TENUE À LA COMPRESSION AMÉLIORÉE 有权
标题翻译：采用改善的压缩强度平流层气球
公开(公告)号：EP2864194B1
公开(公告)日：2016-08-10
申请号：EP13730849.0
申请日：2013-06-14
申请人： Airbus Group SAS
发明人： GENESTE, Jean-François
IPC分类号： B64B1/40 , B64B1/62 , B64B1/60 , B64B1/58
CPC分类号： B64B1/58 , B64B1/40 , B64B1/60 , B64B1/62

5. 发明授权

EP2619083B1 "MOMOHELI II" LIFTING MODULE AND VEHICLES 有权
标题翻译： “MOMOHELI II”提升模及车辆“
公开(公告)号：EP2619083B1
公开(公告)日：2016-04-27
申请号：EP10765983.1
申请日：2010-09-23
申请人： Monsch, Daniel , Monsch, Hans
发明人： Monsch, Daniel , Monsch, Hans
IPC分类号： B64B1/08 , B64B1/14 , B64B1/62 , B64B1/40 , B64B1/30 , B64B1/22 , B64B1/02
CPC分类号： B64B1/62 , B64B1/02 , B64B1/08 , B64B1/14 , B64B1/22 , B64B1/30 , B64B1/40

6. 发明公开

EP2885204A4 BALLOON POWER SOURCES WITH A BUOYANCY TRADE-OFF 有权转让
标题翻译： BALLONSTROMQUELLEN MIT EINEMSCHWIMMFÄHIGKEITSAUSGLEICH
公开(公告)号：EP2885204A4
公开(公告)日：2016-04-13
申请号：EP13830352
申请日：2013-08-12
申请人： GOOGLE INC
发明人： DEVAUL RICHARD WAYNE , TELLER ERIC , BIFFLE CLIFFORD L , WEAVER JOSHUA
IPC分类号： B64B1/44 , B64B1/40 , B64B1/62 , H04W16/18
CPC分类号： G05D1/042 , B64B1/40 , B64B1/62 , C25B1/04 , H02S20/30 , Y02E60/366 , Y02E70/10 , Y02P20/134
摘要： Example embodiments may facilitate altitude control by a balloon in a balloon network. An example method involves: (a) causing a balloon to operate in a first mode, wherein the balloon comprises an envelope, a high-pressure storage chamber, and a solar power system, (b) while the balloon is operating in the first mode: (i) operating the solar power system to generate power for the balloon and (ii) using at least some of the power generated by the solar power system to move gas from the envelope to the high-pressure storage chamber such that the buoyancy of the balloon decreases; (c) causing the balloon to operate in a second mode; and while the balloon is operating in the second mode, moving gas from the high-pressure storage chamber to the envelope such that the buoyancy of the balloon increases.
摘要翻译：示例性实施例可以促进气球网络中的气球的高度控制。示例性方法包括：（a）使气球以第一模式操作，其中气囊包括外壳，高压储存室和太阳能发电系统，（b）当气囊以第一模式操作时（i）操作太阳能发电系统以产生用于气球的电力，以及（ii）使用由太阳能发电系统产生的至少一些功率将气体从壳体移动到高压储存室，使得浮力气球减少; （c）使气球以第二模式操作; 并且当气囊在第二模式下操作时，将气体从高压储存室移动到外壳，使得气球的浮力增加。

7. 发明公开

EP2739527A2 AUTONOMOUS INTELLIGENCE SURVEILLANCE RECONNAISSANCE AND PAYLOAD DELIVERY SYSTEM AND METHOD OF USING SAME 有权
标题翻译：自动化ÜBERWACHUNGS-UND ERKENNUNGS- SOWIE NUTZLASTABGABESYSTEM MITFLUIDBEFÜLLUNGSSYSTEM
公开(公告)号：EP2739527A2
公开(公告)日：2014-06-11
申请号：EP12866919.9
申请日：2012-08-06
申请人： Silicis Technologies Inc.
发明人： STIGLER, Michael, J. , SETAR, Nicholas, James
IPC分类号： B64B1/00
CPC分类号： B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
摘要： An intelligence, surveillance, and reconnaissance system and associated operating method is disclosed including a ground station and one or more autonomous aerial vehicles. Each automomous vehicle is adapted to a) self-monitor a plurality of environment data; b) calculate, based at least in part upon the environment data, a soft wall radius from which it can return to the command and control interface station; c) receive a destination position to which it is commanded to fly; d) determine if the destination position is beyond the soft wall radius; and e) communicate an alert to the command and control interface station if the destination position is beyond the soft wall radius.
摘要翻译：披露了一个智能，监视和侦察系统，包括地面站和一个或多个空中飞行器。飞行器是能够将情报数据传送到地面站的自主系统，并用作导弹发射包的一部分。多个飞行器可以被配置为在地面上的大面积上施放广泛的侦察网，包括由多个飞行器中的每一个提供的较小的重叠侦察区域。

8. 发明授权

EP2132087B1 AIRCRAFT CONFIGURED FOR VERTICALLY ASCENDING AND LANDING 有权
标题翻译：的垂直上升和-LANDUNG配置飞机
公开(公告)号：EP2132087B1
公开(公告)日：2010-10-06
申请号：EP08723889.5
申请日：2008-03-10
申请人： Van Helden Industrie B.V.
发明人： VAN HELDEN, Aalbert Adrianus
IPC分类号： B64B1/60 , B64B1/62
CPC分类号： B64B1/60 , B64B1/62 , B64B2201/00

9. 发明公开

EP1283162A1 Balloon 有权
标题翻译：巴隆
公开(公告)号：EP1283162A1
公开(公告)日：2003-02-12
申请号：EP02002348.7
申请日：2002-01-31
申请人： The Director-General of the Institute of Space and Astronautical Science,a Japanese Government Agency
发明人： Naoki, Izutsu , Yajima, Nobuyuki
IPC分类号： B64B1/40 , B64B1/58 , B64G1/10
CPC分类号： B64B1/58 , B64B1/40 , B64B1/62 , B64G1/105 , B64G2001/224
摘要： A balloon (10, 20) comprising an envelope (11, 21), wherein the envelope (11, 21) has a multilayered structure comprising a gas-impervious sheet (15, 25), and a liquid absorbent sheet (16, 26) overlaid on the inner surface of the gas-impervious sheet (15, 25).
摘要翻译： 1.一种包括外壳（11,21）的气囊（10,20），其中所述外壳（11,21）具有包括不透气性片（15,25）的多层结构和吸液性片（16,26）覆盖在不透气片材（15,25）的内表面上。

10. 发明公开

EP0671322A1 Improvements in the generation and control of inflatable balloons 失效
标题翻译： Verbesserungen zum Erzeugen und Steuern aufblasbarer Ballone。
公开(公告)号：EP0671322A1
公开(公告)日：1995-09-13
申请号：EP95301575.7
申请日：1995-03-10
申请人： KAVANAGH BALLOONS PTY LIMITED
发明人： Kavanagh, Phillip Robert
IPC分类号： B64B1/62
CPC分类号： B64B1/62
摘要： A thermal aircraft, such as a hot air load-carrying balloon (1) which includes a balloon envelope (2) having a deflation aperture (3) therein and a venting valve or operculum (16) designed to removably cover and seal the aperture and to be opened and/or closed rapidly so as to assist in the control of the balloon, forming both a deflation panel and a manoeuvring port for the balloon. The venting valve (16) is removably and releasably secured to the balloon envelope adjacent the periphery of the aperture (3), and means (17, 21, 23, 28) are provided for controllably and selectively positioning the valve in the aperture for open and closed dispositions thereof. Separate controls are provided firstly (17, 17a, 17b, 21) to extend the valve (16) to its maximum surface area, at which point it removably covers and seals the aperture and/or to allow controlled venting of hot air therefrom, and secondly (23, 28) to allow reefing of the valve (16) from the aperture (3) for rapid deflation of the envelope (2). This provides the pilot with a great deal of control over the flight of the balloon, especially during final landing procedures and especially during such procedures in gusty or windy conditions, contributing significantly to control and safety.
摘要翻译：一种热飞机，例如包括其中具有放气孔（3）的气囊（2）的热空气承载气囊（1），以及设计成可移除地覆盖和密封孔的排气阀或操纵器（16）被快速地打开和/或关闭，以帮助气球的控制，形成气囊的通风面板和操纵口。通气阀（16）可移除地和可释放地固定到邻近孔（3）的周边的气囊外壳，并且提供装置（17,21,23,28），用于可控地和选择性地将阀定位在孔中以用于打开及其封闭配置。首先提供独立的控制（17,17a，17b，21）以将阀（16）延伸到其最大表面积，此时可拆卸地覆盖和密封孔口和/或允许从其中控制热空气排出，第二（23,28），以允许阀（16）从孔（3）中取出，用于使信封（2）快速收缩。这为飞行员提供了对气球飞行的大量控制，特别是在最终着陆程序期间，尤其是在这种风风雨雨的程序中，对控制和安全性作出了重大贡献。

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