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公开(公告)号：US20150285165A1
公开(公告)日：2015-10-08
申请号：US14439502
申请日：2013-10-22
Applicant: EADS DEUTSCHLAND GMBH
Inventor： Juergen Steinwandel , Florian Stagliano , Jan Van Toor
CPC classification number: F02D29/02 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/044 , B64C2201/066 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/16 , B64D27/02 , B64D27/24 , B64D31/00 , B64D41/00 , B64D2027/026 , Y02T50/44 , Y02T50/64
Abstract: An unmanned aircraft includes a propulsion system having a diesel or kerosene internal combustion engine and a charger device for engine charging. The propulsion system can be a hybrid propulsion system or a parallel hybrid propulsion system.
Abstract translation: 无人机包括具有柴油或煤油内燃机的推进系统和用于发动机充气的充电装置。 推进系统可以是混合推进系统或并联混合推进系统。
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公开(公告)号：US20150259078A1
公开(公告)日：2015-09-17
申请号：US14658183
申请日：2015-03-14
Applicant: Zlatko Aurelio Filipovic , Guan-Wu Wang , Weiping Wang
Inventor： Zlatko Aurelio Filipovic , Guan-Wu Wang , Weiping Wang
CPC classification number: H04W88/08 , B64C39/024 , B64C2201/066 , B64C2201/146 , F21K9/20 , F21S9/022 , F21V33/0056 , F21V33/0076 , F21Y2115/10 , G05D1/0011 , H01J61/56 , H01K1/62
Abstract: A Handy Base Station (HBS) which is capable of connecting through a base portion into a power socket (e.g., lamp socket). The HBS may have a plurality of functional modules capable of being detachably mounted in a housing. One of the functional modules may be a light emitter such as a light emitting diode (LED). Another rmodule may be a communication module which may communicate using a wire line or wirelessly using standard wireless communication protocols. Further disclosed is a combination unit which has the HBS located on a pole such as a utility pole with a landing pad for an unmanned aerial vehicle (UAV) to allow the UAV a recharging location between deliveries and to allow the HBS to guide the UAV on its flight.
Abstract translation: 便携式基站（HBS），其能够通过基座部分连接到电源插座（例如，灯座）中。 HBS可以具有能够可拆卸地安装在壳体中的多个功能模块。 功能模块之一可以是诸如发光二极管（LED）的发光体。 另一个模块可以是可以使用有线线路或使用标准无线通信协议无线地进行通信的通信模块。 进一步公开的是具有HBS的组合单元，其位于诸如具有用于无人机（UAV）的着陆垫的电线杆的杆上，以允许UAV在递送之间的充电位置，并允许HBS引导UAV 它的航班
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公开(公告)号：US20150097079A1
公开(公告)日：2015-04-09
申请号：US13856892
申请日：2013-04-04
Applicant: Sunlight Photonics Inc.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , ALLAN J. BRUCE
CPC classification number: B64D33/00 , B64C39/024 , B64C2201/042 , B64C2201/066 , B64C2201/141 , B64D27/24 , B64D41/00 , B64D41/007 , B64D47/00 , B64D2041/002 , F03D9/007 , F03D9/11 , F03D9/25 , F03D9/30 , G05D1/0005 , G05D1/101 , H02S10/12 , Y02T50/53 , Y02T50/64
Abstract: Methods and apparatus to harvest renewable energy are provided herein. In some embodiments, a method to harvest renewable energy includes providing an aircraft suitable for untethered flight in an open airspace and an airborne kinetic energy conversion system attached to the airframe, the airborne kinetic energy conversion system comprising a turbine, a generator connected to the turbine, and electrical storage means connected to the generator; flying the aircraft; gaining excess kinetic energy; and converting excess kinetic energy into electricity using the kinetic energy conversion system.
Abstract translation: 本文提供了收获可再生能源的方法和设备。 在一些实施例中，一种收获可再生能源的方法包括提供适用于开放空域中的无螺旋飞行的飞行器以及连接到机身的机载动能转换系统，该机载动能转换系统包括涡轮机，连接到涡轮机的发电机 和连接到发电机的电存储装置; 飞机飞行 获得过量的动能; 并使用动能转换系统将过量的动能转化为电能。
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公开(公告)号：US20140319272A1
公开(公告)日：2014-10-30
申请号：US14264636
申请日：2014-04-29
Applicant: The Boeing Company
Inventor： Enrique Juan Casado Magaña , David Esteban-Campillo , David Scarlatti Jiménez , Ivan Maza , Fernando Caballero
IPC: B64F1/00
CPC classification number: B64C39/024 , B60L3/0046 , B60L3/12 , B60L11/1805 , B60L11/1816 , B60L11/1822 , B60L11/1824 , B60L2200/10 , B60L2220/42 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/18 , B64C2201/20 , B64F1/04 , Y02T10/646 , Y02T10/7005 , Y02T10/7072 , Y02T90/121 , Y02T90/124 , Y02T90/14
Abstract: An autonomous battery replacement station for an unmanned aerial vehicle (UAV) is provided. The UAV includes a replaceable battery. The station includes (a) a landing platform configured to receive the UAV, (b) a storage location configured to store a replacement battery for the UAV, and (c) a means for swapping the replaceable battery on the UAV with a replacement battery from the storage location.
Abstract translation: 提供了一种用于无人机（UAV）的自主电池更换站。 无人机包括可更换的电池。 该车站包括：（a）配置成接收无人机的着陆平台，（b）配置为存储UAV的替换电池的存储位置，以及（c）用UA替换可更换电池的替换电池， 存储位置。
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公开(公告)号：US08794566B2
公开(公告)日：2014-08-05
申请号：US13565654
申请日：2012-08-02
Applicant: Donald B. Hutson
Inventor： Donald B. Hutson
CPC classification number: B64D47/08 , B64C27/006 , B64C27/10 , B64C27/20 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/042 , B64C2201/066 , B64C2201/108 , B64C2201/121 , B64C2201/126 , B64C2201/127 , B64C2201/182 , B64D9/00 , F16M11/123 , F16M11/18 , F16M13/00 , F16M13/02 , F16M2200/041
Abstract: In specific embodiments, a vehicle propellable through fluids comprises a main work section and a plurality of propulsion units. The main work section includes a payload support hub, a payload support structure rotatable in 360° about the payload support hub in at least one axis, and a core including at least one microprocessor, the core at least partially nested within the payload support hub. The at least one microprocessor is adapted to substantially maintain an orientation of the payload support structure relative to a horizon line as the vehicle is propelled. One or more payloads are mountable on the rotatable payload support structure.
Abstract translation: 在具体实施例中，通过流体推进的车辆包括主工作部分和多个推进单元。 主工作部分包括有效载荷支撑轮毂，在至少一个轴线上围绕有效载荷支撑轮毂360°旋转的有效载荷支撑结构，以及包括至少一个微处理器的核心，至少部分地嵌套在有效载荷支撑轮毂内。 所述至少一个微处理器适于在车辆被推进时基本上保持有效载荷支撑结构相对于水平线的取向。 一个或多个有效载荷可安装在可旋转的有效载荷支撑结构上。
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Patent Agency Ranking
公开(公告)号：US20140034775A1
公开(公告)日：2014-02-06
申请号：US13565654
申请日：2012-08-02
Applicant: DONALD B. HUTSON
Inventor： DONALD B. HUTSON
CPC classification number: B64D47/08 , B64C27/006 , B64C27/10 , B64C27/20 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/042 , B64C2201/066 , B64C2201/108 , B64C2201/121 , B64C2201/126 , B64C2201/127 , B64C2201/182 , B64D9/00 , F16M11/123 , F16M11/18 , F16M13/00 , F16M13/02 , F16M2200/041
Abstract: In specific embodiments, a vehicle propellable through fluids comprises a main work section and a plurality of propulsion units. The main work section includes a payload support hub, a payload support structure rotatable in 360° about the payload support hub in at least one axis, and a core including at least one microprocessor, the core at least partially nested within the payload support hub. The at least one microprocessor is adapted to substantially maintain an orientation of the payload support structure relative to a horizon line as the vehicle is propelled. One or more payloads are mountable on the rotatable payload support structure.
Abstract translation: 在具体实施例中，通过流体推进的车辆包括主工作部分和多个推进单元。 主工作部分包括有效载荷支撑轮毂，在至少一个轴线上围绕有效载荷支撑轮毂360°旋转的有效载荷支撑结构，以及包括至少一个微处理器的核心，至少部分地嵌套在有效载荷支撑轮毂内。 所述至少一个微处理器适于在车辆被推进时基本上保持有效载荷支撑结构相对于水平线的取向。 一个或多个有效载荷可安装在可旋转的有效载荷支撑结构上。
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公开(公告)号：US20230166615A1
公开(公告)日：2023-06-01
申请号：US17893546
申请日：2022-08-23
Applicant: HYUNDAI MOBIS Co., Ltd.
Inventor： Young Soo DOW
CPC classification number: B60L53/36 , H02J50/12 , B60L53/12 , B60L53/37 , B64C39/024 , B60L2200/10 , B64C2201/042 , B64C2201/066 , B64C2201/127
Abstract: The present disclosure relates to an in-place alignment method for wireless charging of an urban air mobility and a device and a system therefor. A wireless charging method in an urban air mobility includes acquiring location information of a supply device for supplying wireless power, moving to the supply device based on the location information, performing a horizontal alignment based on a distance to the supply device, performing a longitudinal alignment based on completion of the horizontal alignment, and performing the wireless charging after the urban air mobility stops based on completion of the longitudinal alignment. Therefore, the present disclosure has an advantage of maximizing a wireless charging efficiency and minimizing a power waste by quickly and accurately aligning wireless power transmitting/receiving pads of the urban air mobility and the supply device with each other in place.
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48.发明公开公开(公告)号：US20230147814A1
公开(公告)日：2023-05-11
申请号：US17519683
申请日：2021-11-05
Applicant: AT&T Intellectual Property I, L.P.
Inventor： Paul Carver , Abhigyan Sharma Abhigyan , John Craig , Andrew Kell , James Pratt , David Plunkett, JR. , James Carlton Bedingfield, SR. , Michael Albrecht , Michael L. Hunter , Virginia S. Ng
CPC classification number: B64C39/024 , G08G5/0034 , G08G5/0069 , G08G5/0008 , G01C21/20 , B60L53/30 , H04L63/0428 , G06F9/547 , H04W12/63 , B64C2201/066
Abstract: Aspects of the subject disclosure may include, for example, identifying an uncrewed aerial vehicle (UAV) for route planning and power management, obtaining information regarding the UAV, a present location of the UAV, a destination location for the UAV, or a combination thereof, determining, based on the information, a need for the UAV to recharge a power source of the UAV as part of a journey of the UAV from the present location of the UAV to the destination location for the UAV, responsive to the determining the need, identifying a recharging station associated with a network for recharging the power source of the UAV, and calculating a flight path for the UAV in accordance with the identifying the recharging station. Other embodiments are disclosed.
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公开(公告)号：US20190245365A1
公开(公告)日：2019-08-08
申请号：US16344590
申请日：2016-10-28
Applicant: Telefonaktiebolaget LM Ericsson (publ)
Inventor： Fereydoun FARRAHI MOGHADDAM , Reza FARRAHI MOGHADDAM , Yves LEMIEUX , Denis MONETTE
CPC classification number: H02J7/0044 , B64C39/00 , B64C39/024 , B64C2201/066 , H02J7/0018 , H02J7/0027 , H02J7/0042 , H02J7/0045
Abstract: A drone charging station configured to charge at least one drone, the charging station including at least one charging stack comprised of a plurality of base blocks, the at least one charging stack including a first conductor block having a first polarity for electrically engaging with a corresponding first electrode of the at least one drone, and a first drone guiding portion, a second conductor block having a second polarity different from the first polarity for electrically engaging with a corresponding second electrode of the at least one drone, the second conductor block having a second drone guiding portion, and an insulator block positioned between the first conductor block and the second conductor block and having a third drone guiding portion. The first drone guiding portion, the second drone guiding portion and the third drone guiding portion arranged to provide a drone guiding path along the charging stack.
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50.发明申请公开(公告)号：US20190204856A1
公开(公告)日：2019-07-04
申请号：US16214463
申请日：2018-12-10
Applicant: Cheng-Ying Weng
Inventor： Cheng-Ying Weng , Hsiang-Tien Wu
CPC classification number: G05D1/101 , B64C39/024 , B64C2201/066 , B64C2201/128 , B64D1/02 , G06Q10/08355 , Y02P90/02
Abstract: A goods transporting system with aerial machines utilizes instantaneous collection of location information and future moving path planning information of multiple ground and/or surface vehicles to pair with the delivery path of the goods. The aerial machine can be parked on the selected ground and/or the surface vehicle in the path of taking and transporting the goods, thereby saving power consumption of the aerial machine and effectively extending the transport distance for the goods.
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