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1. 发明申请

WO2017069331A1 수소 리싸이클 비행시스템 및 비행방법 审中-公开
标题翻译：氢回收飞行系统和飞行方法
公开(公告)号：WO2017069331A1
公开(公告)日：2017-04-27
申请号：PCT/KR2015/013121
申请日：2015-12-03
申请人： 서울시립대학교 산학협력단
发明人： 유병덕 , 민현수 , 전준진
IPC分类号： B64B1/00 , B64B1/06 , B64B1/24 , B64B1/58 , B64B1/40 , C01B3/04 , B64D41/00 , B64D47/00 , F17C5/00 , B64B1/36
CPC分类号： B64B1/00 , B64B1/06 , B64B1/24 , B64B1/36 , B64B1/40 , B64B1/58 , B64D41/00 , B64D47/00 , C01B3/04 , F17C5/00
摘要： 본 발명은 수소 리싸이클 비행 시스템 및 비행방법에 관한 것으로, 몸체의 양측에 적어도 한 쌍의 날개를 갖는 비행동체와, 상기 비행동체에 기밀 연결되는 수소가스벌룬과, 상기 수소가스벌룬과 연결되고, 상기 비행동체 외부 또는 내부에 설치되는 수소연료전지와, 상기 수소연료전지로부터 생산된 전기 또는 비행동체 외주부에 구비된 태양전지로부터 생산된 전기 또는 외부 전력망 전기로 충전되는 2차전지를 포함하며, 스위치 전환으로 수소연료전지를 물전기분해장치로 또는 물전기분해장치를 수소연료전지로 전환하고, 상기 수소연료전지로부터 생성된 물을 저장하는 물탱크, 상기 저장된 물을 전기분해하는 상기 물전기분해장치와, 수소연료전지와 물전기분해장치의 기능전환을 위한 스위치 제어장치와, 물전기분해장치에서 생산된 수소가스와 산소가스를 고압저장하기 위한 고압가스통과, 비행체의 부양동력인 상기 수소가스벌룬의 부피가 상기 수소연료전지의 작동 또는 상기 고압가스통에 의해 제어되어 비행하는 것을 특징으로 한다.
摘要翻译：
本发明涉及一种氢气循环飞行系统和飞行方法，和氢气气球是在飞行中，与具有至少在主体的任一侧上的一对翼，气密联接到飞行体的主体，其中 2与氢气气球相连，并充入电或从设置在从氢燃料电池所产生的外周部的电或飞行体的太阳能电池产生的外部电网的电力，氢燃料电池被安装在外部或内部的飞行体的腿包括是否氢燃料电池的一个开关转换为水电解槽或作为水的电解的氢的燃料电池装置，和水箱，储存的水，电的分解，其存储由所述氢燃料电池所产生的水一种用于切换氢燃料电池和水电解装置功能的开关控制装置，其特征在于，所述高压气瓶，车辆到高压储存氢气和氧气飞由操作或氢燃料电池的高压气体流路控制的氢气气球的体积的相关功率。

2. 发明申请

WO2015026732A1 LONG ENDURANCE AIRSHIP OPERATIONS USING A FREE-FLYING TETHERED AIRSHIP SYSTEM 审中-公开
标题翻译：使用自由飞行的空中飞行系统的长寿命航空运行
公开(公告)号：WO2015026732A1
公开(公告)日：2015-02-26
申请号：PCT/US2014/051515
申请日：2014-08-18
申请人： HEPPE, Stephen B.
发明人： HEPPE, Stephen B.
IPC分类号： B64B1/54 , B64B1/58 , B64B1/60
CPC分类号： B64B1/54 , B64B1/02 , B64B1/06 , B64B1/58 , B64B2201/00 , B64C37/02
摘要： In one example, a free-flying tethered airship system includes an upper airship adapted to tailor its lift and drag, a lower airship adapted to tailor its lift and drag, and a tether connecting the upper airship to the lower airship such that the upper airship is at least one kilometer above the lower airship. The upper airship is configured to be equiliberally buoyant, while carrying the tether, in a first altitude range. The lower airship is configured to be equiliberally buoyant in a second altitude range, the first altitude range being higher than the second altitude range. A method for stationkeeping of a free-flying tethered airship system is also provided.
摘要翻译：在一个例子中，一个自由飞行的系留式飞艇系统包括适合于调整其升降机的上部飞艇，适于调整其升降机的下部飞艇，以及将上部飞艇连接到下部飞艇的系绳，使得上部飞艇距离下游飞艇至少一公里。上部飞艇构造成在第一高度范围内平衡地浮起，同时携带系绳。下部飞艇被配置为在第二高度范围内平衡地浮起，第一高度范围高于第二高度范围。还提供了一种用于维持自由飞行的系留式飞艇系统的方法。

3. 发明申请

WO2012012275A3 SYSTEM AND METHOD FOR SOLAR-POWERED AIRSHIP 审中-公开
标题翻译： SOLAR-POWERED AIRSHIP的系统和方法
公开(公告)号：WO2012012275A3
公开(公告)日：2012-04-19
申请号：PCT/US2011044102
申请日：2011-07-15
申请人： LTA CORP , GOELET JOHN
发明人： GOELET JOHN
IPC分类号： B64B1/00 , B64B1/08 , B64B1/10 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/34 , B64B1/58
CPC分类号： B64B1/06 , B64B1/005 , B64B1/08 , B64B1/10 , B64B1/16 , B64B1/20 , B64B1/22 , B64B1/28 , B64B1/30 , B64B1/58 , B64D9/00
摘要： A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply system including solar panels operatively coupled to the electric motors and configured to supply power to the electric motors. The power supply system may also include batteries operatively coupled to the solar panels and configured to receive and store electrical energy supplied by the solar panels, the batteries being further operatively coupled to the electric motors and configured to supply power to the electric motors. The batteries may each be located within an outer envelope of the airship defined by the hull of the airship in a position selected to provide ballast. The solar-powered airship may also include a cargo system configured to contain passengers or freight.
摘要翻译：具有被配置为容纳气体的船体的太阳能飞艇以及具有推进装置和配置成驱动推进装置的电动机的至少一个推进组件。飞艇还可以包括电力供应系统，该电力供应系统包括可操作地耦合到电动机并且被配置为向电动机供电的太阳能面板。电源系统还可以包括可操作地连接到太阳能电池板并配置为接收和存储由太阳能电池板供应的电能的电池，电池进一步可操作地连接到电动机并且配置为向电动机供电。每个电池可以位于由飞艇的船体限定的飞艇的外壳内，其位置被选择为提供压载物。太阳能飞艇还可以包括配置为容纳乘客或货物的货物系统。

4. 发明申请

WO2010051088A1 APPARATUS AND METHOD FOR WIDESPREAD COMMERCIALIZATION OF HYDROGEN AS AN ALTERNATIVE FUEL SOURCE 审中-公开
标题翻译：作为替代燃料来源的氢气商业化的装置和方法
公开(公告)号：WO2010051088A1
公开(公告)日：2010-05-06
申请号：PCT/US2009/053339
申请日：2009-08-11
申请人： BRUTOCO, Rinaldo
发明人： BRUTOCO, Rinaldo
IPC分类号： B64B1/06
CPC分类号： B64B1/62 , B64B1/00 , B64B1/06 , B64B1/12 , B64B1/20 , B64B1/32 , B64B1/66 , B64F1/02 , F42B15/00 , Y10T137/6906
摘要： A system for efficiently transporting hydrogen from where it can be economically made to where it is most needed using specially designed airships. Technologies such as geothermal, wind, solar, wave tidal or hydropower can be used to generate electricity in-situ or very near to the primary energy sources. This electricity can then be used to produce hydrogen directly from water through various methods known in the art. Hydrogen can be delivered from the place where it is produced to the place where it is needed using an airship in which the hydrogen gas can also be used for generating lift, providing propulsion energy and serving ancillary needs. In other embodiments of the invention, the airship of the present invention can be used to dramatically reduce the cost of transportation of freight, the cost of passenger transportation, and to save on the area required for landing at the points of loading/unloading and embarkation/debarkation. And in another embodiment, the airship of the present invention can be used for transporting water and food to areas where needed. A unique docking system can use a remotely piloted unmanned aircraft flown from the mother craft to carry a guide line into a receiving attachment point.
摘要翻译：一种能够经济地运输氢气的系统，使用专门设计的飞艇最需要的地方。诸如地热，风能，太阳能，波浪潮汐或水电等技术可用于原地或非常接近主要能源的电力。然后可以通过本领域已知的各种方法将该电直接用于从水中产生氢气。氢气可以从生产地点运送到需要的地方，使用其中氢气也可以用于产生升降机的飞艇，提供推进能量和服务辅助需求。在本发明的其他实施例中，本发明的飞艇可用于显着降低货物运输成本，乘客运输成本，并节省在装卸点和登船点上着陆所需的面积 /登陆。在另一个实施例中，本发明的飞艇可用于将水和食物运送到需要的区域。独特的对接系统可以使用从母机飞行的遥控无人驾驶飞机将引导线运送到接收附件点。

5. 发明申请

WO2008051175A2 SEMI-RIGID AIR VEHICLE 审中-公开
标题翻译：半刚性空气车
公开(公告)号：WO2008051175A2
公开(公告)日：2008-05-02
申请号：PCT/US2005045424
申请日：2005-12-16
申请人： ALMAN JAMES
发明人： ALMAN JAMES
IPC分类号： B64B1/02
CPC分类号： B64B1/06 , B64B1/32
摘要： A lighter than air semi-rigid air vehicle utilizing two or more spherical chambers with composite fairings in between to reduce drag. The vehicle also may utilize a reverse ballonet or conventional ballonet system for the lift gas control (Helium, Hot Air, Hydrogen or any other lift gas). The power plants may use reversible pitch propellers to enhance maneuverability.
摘要翻译：比空气半刚性的空气车辆更轻，利用两个或多个具有复合整流罩的球形腔，以减少阻力。车辆还可以使用用于提升气体控制（氦气，热空气，氢气或任何其它提升气体）的反向气球或常规气球系统。发电厂可以使用可逆螺距螺旋桨来提高机动性。

6. 发明申请

WO2007037932A2 AIRSHIP HAVING A CENTRAL FAIRING TO ACT AS A STALL STRIP AND TO REDUCE LIFT 审中-公开
标题翻译：航空公司有一个中央公路作为一个阶梯，并减少提升
公开(公告)号：WO2007037932A2
公开(公告)日：2007-04-05
申请号：PCT/US2006/034789
申请日：2006-09-08
申请人： LTAS HOLDINGS, LLC , HEAVEN, JR., George H.
发明人： HEAVEN, JR., George H.
IPC分类号： B64B1/02
CPC分类号： B64B1/06 , B64B1/42
摘要： An airship including a hull having a lenticular shape and a fairing attached to the hull to act as a stall strip and reduce the lift generated by the hull. The hull is symmetrical along a central horizontal plane and the fairing may be positioned along the central horizontal plane. The fairing may have a triangular shape, a semi-circular shape or any other shape capable of disrupting the flow of air over the hull.
摘要翻译：飞艇包括具有透镜形状的船体和附接到船体的整流罩，用作失速条并减少船体产生的升力。船体沿中心水平面对称，整流罩可沿中心水平面定位。整流罩可以具有三角形，半圆形或能够破坏船体上空气流的任何其他形状。

7. 发明申请

WO2006119056A2 LIGHTER THAN AIR SUPERSONIC VEHICLE 审中-公开
标题翻译：比空中超级车辆亮
公开(公告)号：WO2006119056A2
公开(公告)日：2006-11-09
申请号：PCT/US2006/016336
申请日：2006-04-29
申请人： GENERAL ORBITAL CORPORATION , DIFFER, Alfred
发明人： DIFFER, Alfred
IPC分类号： B64B1/06
CPC分类号： B64B1/06 , B64C30/00
摘要： The present invention comprises a lighter than air space vehicle which is optimized for supersonic speeds and altitudes from 30,000 feet to space.
摘要翻译：本发明包括比空中飞行器更轻的车辆，其针对超音速速度和从30,000英尺到空间的高度进行了优化。

8. 发明申请

WO2004074091A2 AIRCRAFT 审中-公开
标题翻译：飞机
公开(公告)号：WO2004074091A2
公开(公告)日：2004-09-02
申请号：PCT/GB2004/000742
申请日：2004-02-24
申请人： LUFFMAN, Charles, Raymond
发明人： LUFFMAN, Charles, Raymond
IPC分类号： B64B
CPC分类号： B64B1/22 , B64B1/06 , B64B1/34 , B64B1/58 , B64B2201/00
摘要： An aircraft comprising an envelope (6) that is inflatable with a lifting gas that is lighter than air that, at least when inflated has curved upper and lower surfaces. The aircraft has a payload carrying means (5), and an aerodynamic lifting means (8) for creating a vertical annular flow of air that induces a flow of air over the respective upper or lower surface (12, 14) of the envelope (6.). One form of aerodynamic generator (8) comprises a plurality of aerofoil blades (20) mounted for rotation around a periphery of the envelope (6).
摘要翻译：一种飞机，其包括可以与至少在充气时具有弯曲的上表面和下表面的空气轻于空气的提升气体充气的外壳（6）。飞行器具有有效载荷装置（5）和用于产生垂直环形空气流的空气动力提升装置（8），该空气动力提升装置（8）在外壳（6）的相应上表面或下表面（12,14）上引起空气流）。一种形式的空气动力发电机（8）包括多个安装用于围绕外壳（6）的周边旋转的翼型叶片（20）。

9. 发明申请

WO99047414A1 AEROSTAT 审中-公开
标题翻译：浮空器
公开(公告)号：WO99047414A1
公开(公告)日：1999-09-23
申请号：PCT/PL1999/000009
申请日：1999-03-18
IPC分类号： B64B1/06
CPC分类号： B64B1/06
摘要： Vacuum aerostat made of foamed polystyrene.
摘要翻译：由泡沫聚苯乙烯制成的真空空气净化器。

10. 发明申请

WO98051568A1 AERIAL COMMUNICATIONS NETWORK 审中-公开
标题翻译：航空通信网络
公开(公告)号：WO98051568A1
公开(公告)日：1998-11-19
申请号：PCT/US1998/010074
申请日：1998-05-15
IPC分类号： B64B1/06 , B64G1/10 , H04B7/185 , B64G1/24 , H04B1/185
CPC分类号： H04B7/18504 , B64B1/06 , B64G1/1007 , B64G1/1085
摘要： A global communications network comprises a plurality of aerial platforms or vehicles (220) deployed at an altitude in or near the stratosphere and permitted to drift in a controlled manner such that each platform (220-300) adjusts its position relative to other aerial platforms (220-300). Each aerial platform has a propulsion system (16) and control surfaces (14) and preferably includes a lighter-than-air component (10) to maintain lift in an economical manner. Each aerial platform (220-300) also includes a payload, means for communicating with other aerial platforms and a control system including location-finding equipment (700) and a processor (70) adapted for directing the platform's propulsion system (16) and control surfaces (14) to effectuate changes in the aerial platform's position relative to other aerial platforms (220-300) based on position information. The communications network provides a self-adjusting network for creating and maintaining a global communications link optionally capable of interoperating with one or more orbiting communications satellites (58) or with ground, air or sea-based equipment.
摘要翻译：全球通信网络包括多个高空作业平台或车辆（220），其部署在平流层中或其附近的高度，并允许以受控的方式漂移，使得每个平台（220-300）相对于其他高空作业平台调整其位置（ 220-300）。每个空中平台具有推进系统（16）和控制表面（14），并且优选地包括以比经济方式维持升降机的轻于空气的部件（10）。每个空中平台（220-300）还包括有效载荷，用于与其他高空作业平台通信的装置和包括定位设备（700）和适于引导平台的推进系统（16）的控制系统（70）的控制系统和控制（14）根据位置信息来实现空中平台相对于其他高空作业平台（220-300）的位置的变化。通信网络提供用于创建和维护全球通信链路的自调整网络，其可选地能够与一个或多个轨道通信卫星（58）或地面，空中或海上设备进行互操作。

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