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1. 发明公开

CN106275363A 一种超小型系留气球系统有权
公开(公告)号：CN106275363A
公开(公告)日：2017-01-04
申请号：CN201610879143.3
申请日：2016-10-08
申请人：中国科学院光电研究院
发明人：祝榕辰 , 杨燕初 , 张冬辉
IPC分类号： B64B1/50 , B64B1/42 , B64B1/58
CPC分类号： B64B1/50 , B64B1/42 , B64B1/58
摘要：本发明公开了一种超小型系留气球，涉及系留气球领域，其包括球体系统、绞盘系统、充气系统、地面控制与接收系统、缆绳系统、载荷系统和收纳背负系统。其中球体系统中球体为扁圆形回转球体，不仅抗风效果好、稳定性好，且收放便捷，占据空间小。其中绞盘系统中动力系统为收放手动摇把或收放电机，携带方便。本发明提出的超小型系留气球操作简便，所需操作人员少，可快速部署、灵活机动；对场地要求低，可在城市、乡村或偏远地区展开及发放。

2. 发明公开

CN106741808A 一种空中作业的农药喷洒方法无效
公开(公告)号：CN106741808A
公开(公告)日：2017-05-31
申请号：CN201510833630.1
申请日：2015-11-25
申请人：重庆田瓜瓜农业科技开发有限公司
发明人：李昌林
IPC分类号： B64B1/20 , B64B1/24 , B64B1/14 , B64C39/02 , B64B1/60 , B64B1/62 , B64B1/42
CPC分类号： B64B1/20 , B64B1/14 , B64B1/24 , B64B1/42 , B64B1/60 , B64B1/62 , B64C39/02
摘要：本发明公开了一种空中作业的农药喷洒方法，包括气囊装置、飞艇机舱，所述的飞艇机舱上方固定设置气囊装置，所述气囊装置两侧的飞艇机舱上分别设置有艇翼，所述的艇翼下方设置有电动推进器，所述的电动推进器连接有蓄电池。所述的气囊装置连接氦气充气系统，所述的气囊装置的气囊采用内层膜和外层膜双层结构，所述的内层膜和外层膜双层结构内设置有相互独立的若干个气囊圈。所述的飞艇机舱上设置喷雾装置和遥感影像机。

3. 发明公开

EP1772374A2 Direct mounted propulsion for non-rigid airship 有权
标题翻译： Nicht-starres Luftschiff mit direkt angebrachtem Antrieb
公开(公告)号：EP1772374A2
公开(公告)日：2007-04-11
申请号：EP06255086.8
申请日：2006-09-30
申请人： Lockheed Martin Corporation
发明人： Marimon, Thomas L. , Peritt, Jonathan , Houmard, James E.
IPC分类号： B64B1/30
CPC分类号： B64B1/32 , B64B1/02 , B64B1/42
摘要： A propulsion assembly (20) for attachment to the enclosing material (14) of an airship (10) includes a base (21) which is positioned proximate to the enclosing material. An extension member (40) having opposed ends projects away from the base (21) and includes opposed ends. A motor assembly (50) is attached to the end of the extension member (40) opposed to the base (21). A mounting assembly (70) is attached to the enclosing material and a plurality of pre-tensioned guy cables (60) connect the mounting assembly (70) to the extension member (40).
摘要翻译：用于附接到飞艇（10）的封闭材料（14）的推进组件（20）包括靠近封闭材料定位的基座（21）。具有相对端的延伸构件（40）远离基部（21）突出并且包括相对的端部。马达组件（50）附接到与基座（21）相对的延伸构件（40）的端部。安装组件（70）附接到封闭材料，并且多个预张紧的铠装电缆（60）将安装组件（70）连接到延伸构件（40）。

4. 发明公开

EP2879950A1 LIGHTER-THAN-AIR CRAFT FOR ENERGY-PRODUCING TURBINES 审中-公开
标题翻译：轻于空气车辆涡轮机发电
公开(公告)号：EP2879950A1
公开(公告)日：2015-06-10
申请号：EP13826340.5
申请日：2013-08-02
申请人： Altaeros Energies Inc.
发明人： GLASS, Benjamin, W.
IPC分类号： B64B1/02 , B64B1/50 , F03D9/00
CPC分类号： F03D3/0427 , B64B1/42 , B64B1/50 , B64B2201/00 , F03D13/20 , F05B2240/922 , Y02E10/728 , Y02E10/74
摘要： A wind-based power generating system provides a wind energy converter for converting wind energy into another form of energy using a lighter-than-air craft configured to produce a positive net lift. The net lift includes both a net aerodynamic lift and a net buoyant lift. A tethering mechanism is configured to restrain the lighter-than-air craft with respect to the ground. The lighter-than-air craft defines an interior volume for containing a lighter-than-air gas, and the lighter-than-air craft has a fore section and an aft section. The tethering system has at least one attachment point on the fore section of the lighter-than-air craft and at least one attachment point on the aft section of the lighter-than-air craft. The lighter-than-air craft provides a stable aerodynamic moment with respect to a yaw axis about a center-of-mass of the lighter-than-air craft. The craft can be formed in a variety of aerodynamic profiles/shapes.

5. 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。

6. 发明授权

US09067666B1 Superpressure balloon envelope cage structure and rigging technique 有权
标题翻译：超压球囊信封笼结构和索具技术
公开(公告)号：US09067666B1
公开(公告)日：2015-06-30
申请号：US13941674
申请日：2013-07-15
申请人： Google Inc.
发明人： Kevin Roach , Pamela Desrochers
IPC分类号： B64B1/02 , B64B1/40 , B64B1/42
CPC分类号： B64B1/40 , B64B1/42
摘要： A balloon apparatus is provided having (1) a cage structure that includes (a) a plurality of vertical tendons, where each of the vertical tendons includes a first end and second end, where the first ends of the vertical tendons are all connected to one another and where the second ends of the vertical tendons are all connected to one another and (b) one or more horizontal tendons, where each horizontal tendon is attached to each of the vertical tendons at a corresponding level of the cage structure and (2) a balloon envelope, where the balloon envelop is arranged inside the cage structure and inflatable within the cage structure.
摘要翻译：提供了一种气球装置，其具有（1）笼结构，其包括（a）多个垂直筋，其中每个垂直筋包括第一端和第二端，其中垂直筋的第一端全部连接到一个另一个并且其中垂直腱的第二端全部彼此连接并且（b）一个或多个水平腱，其中每个水平腱在笼结构的相应水平处附接到每个垂直腱，以及（2）一个气球外壳，其中气球信封布置在笼结构内部并且可在笼结构内充气。

7. 发明授权

US3521836A Inflated buoyant wing 失效
标题翻译：充气ANT ANT
公开(公告)号：US3521836A
公开(公告)日：1970-07-28
申请号：US3521836D
申请日：1968-08-06
申请人： STRUBLE ARTHUR D JR
发明人： STRUBLE ARTHUR D JR
IPC分类号： B64C3/30 , B64B1/50 , B64B1/42 , B64F1/12
CPC分类号： B64B1/52 , B64B1/42 , B64F1/14 , Y10S244/90

8. 发明公开

EP2879950A4 LIGHTER-THAN-AIR CRAFT FOR ENERGY-PRODUCING TURBINES 审中-公开
标题翻译：轻于空气车辆涡轮机发电
公开(公告)号：EP2879950A4
公开(公告)日：2016-03-23
申请号：EP13826340
申请日：2013-08-02
申请人： ALTAEROS EN INC
发明人： GLASS BENJAMIN W
IPC分类号： B64B1/02 , B64B1/50 , F03D1/02 , F03D1/04 , F03D9/00
CPC分类号： F03D3/0427 , B64B1/42 , B64B1/50 , B64B2201/00 , F03D13/20 , F05B2240/922 , Y02E10/728 , Y02E10/74
摘要： A wind-based power generating system provides a wind energy converter for converting wind energy into another form of energy using a lighter-than-air craft configured to produce a positive net lift. The net lift includes both a net aerodynamic lift and a net buoyant lift. A tethering mechanism is configured to restrain the lighter-than-air craft with respect to the ground. The lighter-than-air craft defines an interior volume for containing a lighter-than-air gas, and the lighter-than-air craft has a fore section and an aft section. The tethering system has at least one attachment point on the fore section of the lighter-than-air craft and at least one attachment point on the aft section of the lighter-than-air craft. The lighter-than-air craft provides a stable aerodynamic moment with respect to a yaw axis about a center-of-mass of the lighter-than-air craft. The craft can be formed in a variety of aerodynamic profiles/shapes.

9. 发明公开

EP1772374A3 Direct mounted propulsion for non-rigid airship 有权
标题翻译：对非刚性飞艇直接连接驱动器
公开(公告)号：EP1772374A3
公开(公告)日：2008-02-20
申请号：EP06255086.8
申请日：2006-09-30
申请人： Lockheed Martin Corporation
发明人： Marimon, Thomas L. , Peritt, Jonathan , Houmard, James E.
IPC分类号： B64B1/30
CPC分类号： B64B1/32 , B64B1/02 , B64B1/42
摘要： A propulsion assembly (20) for attachment to the enclosing material (14) of an airship (10) includes a base (21) which is positioned proximate to the enclosing material. An extension member (40) having opposed ends projects away from the base (21) and includes opposed ends. A motor assembly (50) is attached to the end of the extension member (40) opposed to the base (21). A mounting assembly (70) is attached to the enclosing material and a plurality of pre-tensioned guy cables (60) connect the mounting assembly (70) to the extension member (40).

10. 发明专利

JP2002544064A Equipment to reduce the degree of unwanted movement of the weather balloon with a local irregularities 审中-公开
公开(公告)号：JP2002544064A
公开(公告)日：2002-12-24
申请号：JP2000618752
申请日：2000-05-18
申请人：バラット,ジャン
发明人：バラット，ジャン
IPC分类号： B64B1/40 , B64B1/42 , B64C21/10 , F15D1/12 , G01W1/08
CPC分类号： B64B1/42 , B64C21/10 , F15D1/12 , G01W1/08 , Y02T50/166
摘要： (57)【要約】膨張可能な気のうを設けかつＧＰＳ型ゾンデをはめ込んだ気象用気球によって上昇段階の間に行なわれる風の測定の品質を向上させるための装置であって、装置は、前記気球（４）の壁の部分にしっかりと固定されたスポイラー（Ａｓ）を含み、スポイラーは上昇の間に前記気球（４）の上半球に位置付けられ、その態様により、前記スポイラー（Ａｓ）はそれに作用するいかなる空力的力も前記気球（４）に伝達し、前記スポイラー（Ａｓ）は前記気球の外側表面に従う空気の流れ（ＦＡｓ）を変えて、前記空気の流れ（ＦＡｓ）が上昇の間に前記気球（４）の下半球の表面に付着するのを防止することを特徴とする。

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