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1. 发明申请

WO2016116841A1 GUIDANCE SYSTEM OF A DRONE 审中-公开
标题翻译：指导制度
公开(公告)号：WO2016116841A1
公开(公告)日：2016-07-28
申请号：PCT/IB2016/050192
申请日：2016-01-15
申请人： PARADOX ENGINEERING SAGL , SUPSI (SCUOLA UNIVERSITARIA DELLA SVIZZERA ITALIANA)
发明人： GIUSTI, Alessandro , GAMBARDELLA, Luca Maria , MINETTI, Giovanni , GUZZI, Jérôme
IPC分类号： G05D1/00
CPC分类号： G08G5/0069 , B60L11/1822 , B60L11/1838 , B60L2200/10 , B64C39/024 , B64C2201/042 , B64C2201/128 , B64C2201/146 , B64F1/02 , G01S1/68 , G05D1/0011 , G05D1/0202 , G08G5/0013 , G08G5/0026 , G08G5/0052 , G08G5/045 , H04W84/18
摘要： A guidance system (1) for a drone (100) is described, said system comprising: a plurality of poles (2-10) fixed to the ground and associated with a private or public electric power grid; a plurality of devices (12-20) fixed to the poles and powered by the electric power grid, said devices being interconnected in a wireless network (40) and comprising a radio communication module (22-30) for communicating with the drone; a controller (35) connected to the wireless network (40) and intended to program a flight path (P) of the drone (100) between two or more poles (2, 3, 4, 10) by transmitting configuration commands to the respective devices (12, 13, 14, 20) of the wireless network (40), for configuring the radio communication modules (22, 23, 24, 30), wherein the radio communication module (33) of one pole (3) in the flight path (P) is configured to guide the drone (100) towards the radio communication module (34) of a following pole (4) in the flight path (P).
摘要翻译：描述了用于无人机（100）的引导系统（1），所述系统包括：固定到地面并与私人或公共电网相关联的多个极点（2-10）; 固定到所述电极并由所述电网供电的多个设备（12-20），所述设备在无线网络（40）中互连，并且包括用于与所述无人机通信的无线电通信模块（22-30）连接到无线网络（40）并且旨在通过将配置命令发送到相应的两个或多个极（2,3,4,10）来对无人机（100）的飞行路径（P）进行编程的控制器（35）用于配置无线电通信模块（22,23,24,36）的无线网络（40）的设备（12,13,14,20），其中所述无线网络（40）中的一个极（3）的无线电通信模块（33）飞行路径（P）被配置为朝向飞行路径（P）中的随后的极点（4）的无线电通信模块（34）引导无人机（100）。

2. 发明申请

WO2016007275A1 ENHANCED ACCURACY FOR TRACKING TETHERED AIRBORNE VEHICLES 审中-公开
标题翻译：用于跟踪机载AIRBORNE车辆的增强精度
公开(公告)号：WO2016007275A1
公开(公告)日：2016-01-14
申请号：PCT/US2015/036922
申请日：2015-06-22
申请人： GOOGLE INC.
发明人： HALLAMASK, Kurt , HACHTMANN, Brian , NELSON, Rob , HARDHAM, Corwin , JENSEN, Kenny , PATTEN, Elias, Wolfgang
IPC分类号： F03D11/00 , F03D7/04 , F03D1/02 , B64F3/00
CPC分类号： G06T7/004 , B64C39/022 , B64F1/02 , B64F3/00 , B64F3/02 , G06T7/70
摘要： Wind energy systems, such as an Airborne Wind Turbine ("AWT"), may be used to facilitate conversion of kinetic energy to electrical energy. An AWT may include an aerial vehicle that flies in a path to convert kinetic wind energy to electrical energy. The aerial vehicle may be tethered to a ground station with a tether that terminates at a tether termination mount system. In one aspect, the tether termination mount system may include a tether termination unit configured in one or more gimbals that allow for the tether termination unit to rotate about one or more axes while tracking the aerial vehicle in flight. In a further aspect, the tether termination mount system may include an imaging device configured for imaging the aerial vehicle during flight in order to enhance tracking accuracy over that which is performed by angular motion of the tether termination unit.
摘要翻译：诸如空降风力发电机（“AWT”）等风能系统可用于促进将动能转换为电能。 AWT可以包括在将动能风能转换成电能的路径中飞行的空中飞行器。航空器可以连接到具有终止于系绳终端安装系统的系绳的地面站。在一个方面，系绳终端安装系统可以包括配置在一个或多个万向节中的系绳终端单元，其允许系绳终端单元围绕一个或多个轴线旋转，同时跟踪飞行中的空中飞行器。在另一方面，系绳终端安装系统可以包括被配置为在飞行期间对飞行器进行成像的成像装置，以便提高跟踪系统终端单元的角运动执行的追踪精度。

3. 发明申请

WO2015160394A3 ASYMMETRIC AIRCRAFT AND THEIR LAUNCH AND RECOVERY SYSTEMS FROM SMALL SHIPS 审中-公开
标题翻译：不平衡飞机及其小型起重机和恢复系统
公开(公告)号：WO2015160394A3
公开(公告)日：2015-12-10
申请号：PCT/US2015011149
申请日：2015-01-13
申请人： ADVANCED PRODUCT DEV LLC
发明人： MCDONNELL WILLIAM RANDALL
IPC分类号： B64C3/10 , B64F1/04 , B64F3/00
CPC分类号： B64C3/10 , B63H9/0685 , B64C39/024 , B64C2201/028 , B64C2201/082 , B64C2201/182 , B64C2201/205 , B64C2201/208 , B64F1/02 , B64F1/04 , B64F1/222 , Y02T50/12 , Y02T50/826
摘要： An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).
摘要翻译：一架不对称的飞机（1）和一架可从小型船只运行的飞机（1），并在一架直升机机库（107）内以三个或更多的飞机高密度存储，无需起落架或机翼折叠。这些飞机在计算机上像电路板一样滑入和移出机库（90）的机库，并使用大型拖缆机（6）发射和恢复。

4. 发明申请

WO2015099846A1 AIRCRAFT RETRIEVAL DEVICE 审中-公开
标题翻译：飞机检索装置
公开(公告)号：WO2015099846A1
公开(公告)日：2015-07-02
申请号：PCT/US2014/055354
申请日：2014-09-12
申请人： CHAVEZ, Jose, Cruz
发明人： CHAVEZ, Jose, Cruz
IPC分类号： B64F1/12 , B64F1/02
CPC分类号： B64F1/02 , B64C39/024 , B64C2201/021 , B64C2201/182
摘要： A retrieval device for an unmanned aircraft. The retrieval device may include a frame that supports a flexible material. The flexible material may form a receptacle portion shaped to receive the unmanned aircraft. The flexible material may absorb at least a portion of the energy exerted by the aircraft landing within the receptacle portion. Wheels may be connected to the frame to further control and absorb energy from the landing.
摘要翻译：无人机的检索装置。检索装置可以包括支撑柔性材料的框架。柔性材料可以形成成形为接收无人驾驶飞行器的接收器部分。柔性材料可以吸收飞机着陆在容器部分内施加的能量的至少一部分。轮可以连接到框架以进一步控制和吸收来自着陆的能量。

5. 发明申请

WO2014014136A1 동체 이착륙이 가능한 항공기 및 이 항공기의 이착륙 시스템 审中-公开
标题翻译：飞机可以通过其飞机起飞或着陆，飞机起飞/着陆系统
公开(公告)号：WO2014014136A1
公开(公告)日：2014-01-23
申请号：PCT/KR2012/005698
申请日：2012-07-17
申请人： 양후영 , 양현영 , 양동규
发明人： 양동규
IPC分类号： B64C25/04 , B64C1/06 , B64C25/68 , B64F1/00
CPC分类号： B64C25/32 , B64C25/04 , B64C25/14 , B64C25/62 , B64F1/02 , B64F1/04 , Y02T50/82
摘要： 본 발명에 의한 동체 이착륙이 가능한 항공기 및 이 항공기의 이착륙 시스템은, 저면에 강착면(landing surface)이 형성되는 항공기 동체가 안착되어 활주방향으로 미끄러지면서 이착륙되도록 다수 개의 이착륙용 롤러가 활주방향으로 배열됨으로써, 별도의 랜딩기어 없이 항공기 동체가 활주면체에 접촉되어 이착륙될 수 있다. 이를 통해 항공기 중량을 낮출 수 있을 뿐만 아니라 항공기의 연료 소모량을 줄일 수 있으며 항공기 내 유효 공간을 넓힐 수 있고 이착륙 장치의 마찰력을 이용하여 활주로의 길이를 줄일 수 있고 항공기의 이착륙 안전성을 높일 수 있다.
摘要翻译：根据本发明的能够通过其机身起飞/着陆的飞行器和飞行器的起飞/着陆系统被构造成使得多个起飞/着陆滚轮沿滑动方向布置，使得具有着陆面的飞机机身形成在其底部可以安全地滑动并滑动方向，从而使飞机机身能够接触运行的表面，起飞/着陆，而无需单独的起落架。因此，不仅可以减少飞机的重量，还可以减少飞机的燃料消耗，从而可以扩大飞机的有用空间，由于产生的摩擦力可以缩短跑道的长度通过起飞/着陆装置，可以提高飞机起飞/着陆期间的安全性。

6. 发明申请

WO2014007705A1 LANDING ARRESTING SYSTEM FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AERIAL VEHICLES, LANDING AND TAKE-OFF PLATFORM FOR VTOL AERIAL VEHICLES AND VTOL LOCKING MEMBER FOR AERIAL VEHICLES 审中-公开
标题翻译：用于垂直起落架的垂直起落架系统（垂直起落架）空中客车，起重机和起落架平台，用于空中客车和垂直起落架的空中客车
公开(公告)号：WO2014007705A1
公开(公告)日：2014-01-09
申请号：PCT/SE2012/050790
申请日：2012-07-05
申请人： SAAB AB , CARDELL, Per-Erik , STENBOM, Kjell
发明人： CARDELL, Per-Erik , STENBOM, Kjell
IPC分类号： B64F1/12 , B64C25/68 , E01F3/00
CPC分类号： B64F1/02 , B64C25/52 , B64C25/68 , B64C2025/325 , B64C2201/182 , B64F1/007 , B64F1/125 , E01F3/00 , Y02T50/82
摘要： The present invention relates to a landing arresting system for vertical take-off and landing (VTOL) aerial vehicles(1) comprising a landing and take-off platform(6) and at least one VTOL locking member (4) having a projecting portion (32) arranged at a lower portion of the vehicle (1). The landing and take-off platform(6) comprises a plurality of individually displaceable rolls (12),arranged substantially in a horizontal direction, and moveable back and forth, such that the projecting portion (32) of the VTOL locking member (4) can be entered, retained and released between two adjacent rolls (12). The present invention also relates to a landing and take-off platform for VTOL aerial vehicles and a VTOL locking member for aerial vehicles.
摘要翻译：本发明涉及一种用于垂直起飞和降落（VTOL）空中飞行器（1）的降落停止系统，其包括着陆和起飞平台（6）和至少一个具有突出部分的垂直起落架锁定构件（4） 32）布置在车辆（1）的下部。着陆和起飞平台（6）包括基本上沿水平方向布置并可前后移动的多个单独可移动的辊（12），使得垂直起落架锁定构件（4）的突出部分（32）可以在两个相邻的辊（12）之间进入，保持和释放。本发明还涉及用于垂直起降飞机的着陆和起飞平台以及用于飞行器的垂直起落架锁定构件。

7. 发明申请

WO2011015679A3 METHOD AND SYSTEM TO ASSIST CONVENTIONAL FIXED-WING AIRCRAFT LANDING, WITHOUT A RUNWAY 审中-公开
标题翻译：方法和系统来协助常规固定翼飞机着陆，无跑道
公开(公告)号：WO2011015679A3
公开(公告)日：2011-03-31
申请号：PCT/ES2010000311
申请日：2010-07-16
申请人： UNIV MADRID POLITECNICA , GOMEZ PEREZ JOSE PATRICIO , GOMEZ PEREZ IGNACIO , MONTEAGUDO LOPEZ DE SABANDO ANTONIO
发明人： GOMEZ PEREZ JOSE PATRICIO , GOMEZ PEREZ IGNACIO , MONTEAGUDO LOPEZ DE SABANDO ANTONIO
IPC分类号： B64F1/02
CPC分类号： B64F1/02
摘要： The present system allows conventional, unprepared fixed-wing aircrafts to land safely on unprepared, small zones, enabling an aerodynamic capacitance in which the airplanes can fly in a controlled manner against coherent airflow, assisted by a combined system including both the airflow control mechanisms and the automatic flight control system of the aircraft.
摘要翻译：本系统允许传统的无准备的固定翼飞机在没有准备的小区域安全着陆，从而实现空气动力学电容，在该空气动力学电容中，飞机可以以受控的方式飞行以抵抗相干气流，并且通过包括气流控制机构和飞机的自动飞行控制系统。

8. 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。

9. 发明申请

WO2008015663A1 AN UNMANNED AERIAL VEHICLE LAUNCHING AND LANDING SYSTEM 审中-公开
标题翻译：一个无人驾驶的民用航空器起飞和登陆系统
公开(公告)号：WO2008015663A1
公开(公告)日：2008-02-07
申请号：PCT/IL2007/000488
申请日：2007-04-18
申请人： ELBIT SYSTEMS ELECTRO-OPTICS ELOP LTD. , KARIV, Amnon
发明人： KARIV, Amnon
IPC分类号： B64F1/02 , B64F1/04 , B64F1/08
CPC分类号： B64F1/06 , B64C2201/084 , B64C2201/182 , B64F1/02
摘要： A system for landing UAV's comprising a slingshot structure (25) that includes a central arm (26) and an axis means (45) installed along the central arm of the structure and wherein it enables the central arm to move around it in addition, the system comprises base means (50) connecting the axis means to a platform (20) at which the system is installable. The system also include a controlled pulling and braking means (55) that connects between lower end of the central arm of the structure and the platform upon which the system is installable and an assembly (35), essentially formed as a substantially "Y" shape part that is installable unto the top end of the central arm of the structure and a stretchable elastic means (30) installed in a stretched manner at a gap formed between the two arms of the assembly and set to connect with a landing UAV(15). At the landing phase, the controlled pulling and braking means of the system, essentially brakes the motion of the central arm of the structure that is propelled to revolve around the system's axis means, from a time that the UAV forms contact with the elastic means and with it propels the structure to move around the axis means.
摘要翻译：一种用于着陆UAV的系统，其包括弹弓结构（25），该弹弓结构包括中心臂（26）和沿着所述结构的中心臂安装的轴线装置（45），并且其中使得所述中央臂能够围绕其运动，系统包括将轴装置连接到可安装系统的平台（20）的基座装置（50）。该系统还包括可控制的拉动和制动装置（55），其连接该结构的中心臂的下端和该系统可安装的平台以及基本上形成为基本上“Y”形的组件（35）该部分可安装到该结构的中央臂的顶端，以及可拉伸的弹性装置（30），该伸缩弹性装置（30）以形成在组件的两个臂之间的间隙的方式安装，并设置成与着陆UAV（15）连接，。在着陆阶段，从无人机与弹性装置形成接触的时间起，系统的受控牵引和制动装置基本上制动被推进围绕系统轴装置旋转的结构的中心臂的运动，随着它推动结构围绕轴线移动。

10. 发明申请

WO2007055709A2 UAV RECOVERY SYSTEM 审中-公开
标题翻译：无人机恢复系统
公开(公告)号：WO2007055709A2
公开(公告)日：2007-05-18
申请号：PCT/US2005/046378
申请日：2005-12-21
申请人： LOCKHEED MARTIN CORPORATION , WATTS, Michael, A. , ROOT, George, Raymond , ADAMSKI, David, M.
发明人： WATTS, Michael, A. , ROOT, George, Raymond , ADAMSKI, David, M.
CPC分类号： B64F1/02 , B64C2201/182
摘要： A UAV capture system is disclosed. In the illustrative embodiment, the UAV capture system is coupled to the deck of a sea-faring vessel. The UAV capture system includes a single arresting line that is supported by a stanchion. In the illustrative embodiment, the stanchion is disposed on a rotatable boom.
摘要翻译：公开了一种无人机捕获系统。在说明性实施例中，UAV捕获系统耦合到海上船只的甲板。 UAV捕获系统包括由支柱支撑的单个拦截线。在说明性实施例中，支柱设置在可旋转的吊杆上。

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