公开(公告)号：WO2015135523A1

公开(公告)日：2015-09-17

申请号：PCT/DE2015/000113

申请日：2015-03-13

Applicant: GAßMANN, Uwe

Inventor： GAßMANN, Uwe

IPC: G05D1/06 ,  G05D1/00 ,  B64C19/02 ,  G05D1/08 ,  G05D1/10 ,  B64C39/02

CPC classification number: G05D1/0676 ,  B64C2201/066 ,  G05D1/0858

Abstract: Die Erfindung betrifft ein Verfahren zur vollautomatischen Anflugsteuerung von Landestationen für Fluggeräte (2), insbesondere batteriebetriebene Flugdrohnen mit einer GPS- (24) und Gyroskopsteuerung (42). Um eine zielsichere Ansteuerung der Fiuggeräte (2) zu ermöglichen, ist erfindungsgemäß vorgesehen, dass durch ein Flugleitsystem der Landestation die vorhandene GPS-Steuerung (42) des Fluggerätes (2) in der Nähe einer Landestation durch ein Transpondersignal ausgeschaltet wird und das Fluggerät (2) durch die Gyroskopsteuerung (42) an die Landestation herangeführt wird. Die Gyroskopsteuerung (42) wird zu diesem Zweck aus der ursprünglichen Lageposition ausgelenkt, um einen seitlichen Drift des Fluggerätes (2) zu erzeugen und diese Steuerungsmöglichkeit zum exakten Ansteuern der Landestation zu verwenden. Die Landestation selbst ist für den Austausch oder die Ladung der an Bord des Fluggerätes (2) befindlichen Batterie (7) vorgesehen.

Abstract translation: 本发明涉及一种用于着陆台的全自动接近飞行控制飞机（2），尤其是电池供电的无人机与GPS（24）和Gyroskopsteuerung（42）的方法。 在为了使Fiuggeräte（2）的更安全的控制，本发明提供的是，在到达站，飞行器的现有的GPS控制器（42）的飞行管理系统（2）是在着陆台的附近通过一个转发器信号和所述飞行器（2关闭 ）由Gyroskopsteuerung（42）引导到陆地站。 所述Gyroskopsteuerung（42），以便产生所述飞行器（2）的横向漂移，并使用该控制可能性精确控制的到达站偏转从所述原点位置这一目的。 着陆台本身设置为位于的在飞行器（2）的电池（7）的板更换或充电。

公开(公告)号：WO2015057832A1

公开(公告)日：2015-04-23

申请号：PCT/US2014/060681

申请日：2014-10-15

Applicant: ELWHA LLC ,  HYDE, Roderick A. ,  WOOD, Lowell L., Jr.

Inventor： HYDE, Roderick A. ,  WOOD, Lowell L., Jr. ,  DUNCAN, William David ,  KARE, Jordin T. ,  MALASKA, Stephen L. ,  MYHRVOLD, Nathan P. ,  PETROSKI, Robert C. ,  WEAVER, Thomas Allan

IPC: B62D63/02 ,  B62D63/04 ,  B64F3/02 ,  B64D39/00

CPC classification number: B64C39/024 ,  B64C39/022 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/046 ,  B64C2201/063 ,  B64C2201/066 ,  B64C2201/12 ,  B64C2201/127 ,  B64C2201/145 ,  B64C2201/146 ,  B64C2201/208 ,  B64F1/00 ,  G05D1/0094

Abstract: A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.

Abstract translation: 机动车辆系统包括包括飞行器着陆部分的机动车辆和被配置为被支撑在飞行器着陆部分上的主动推进无人飞行器。 车辆和飞行器构造成使得当飞行器被支撑在飞行器着陆部分上时，车辆能够向飞机提供燃料和电能中的至少一种。

公开(公告)号：WO2014013270A1

公开(公告)日：2014-01-23

申请号：PCT/GB2013/051945

申请日：2013-07-19

Applicant: ELSON, Andrew, Charles

Inventor： DAVIDSON, Peter

IPC: B64C39/02 ,  B64D27/24

CPC classification number: B64D5/00 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/162 ,  B64C2201/187 ,  B64D2211/00

Abstract: A method of flying an unmanned aerial vehicle (50) at an elevated altitude comprising at least two wings (53) comprising solar-energy collectors (not shown), the method involving flying the vehicle (50) for an extended period of time with the wings (53), and therefore the solar collectors, angled towards the sun, so that the glancing angle of sunlight is greater than it would be if the vehicle (50) was flying with its wings (53) in a horizontal orientation, the vehicle (50) comprising means to reduce or eliminate the rate of change of compass bearing during flight.

Abstract translation: 一种在升高的高度上飞行无人驾驶飞行器（50）的方法，包括包括太阳能收集器（未示出）的至少两个翼部（53），所述方法包括使车辆（50）延长一段时间， 因此太阳能收集器朝向太阳倾斜，使得阳光的扫视角度大于如果车辆（50）以其水平方向与其翼（53）一起飞行的那样，则车辆（53） （50）包括用于减少或消除飞行中的罗盘方位变化率的装置。

公开(公告)号：WO2014013268A1

公开(公告)日：2014-01-23

申请号：PCT/GB2013/051942

申请日：2013-07-19

Applicant: ELSON, Andrew Charles

Inventor： ELSON, Andrew Charles

IPC: B64D5/00 ,  B64C39/02

CPC classification number: B64D5/00 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/162 ,  B64C2201/187 ,  B64D2211/00

Abstract: A method of launching a powered unmanned aerial vehicle (10), the method comprising lifting the vehicle (10) by attachment to a lighter- than-air carrier (12) from a substantially ground-level location to an elevated altitude, wherein the vehicle (10) is prevented from entering its flight mode during ascent, causing the vehicle (10) to detach from the carrier (12) while the velocity of the vehicle (10) relative to the carrier (12) is substantially zero, the vehicle (10) thereafter decreasing in altitude as it accelerates to a velocity where it is capable of preventing any further descent and can begin independent sustained flight.

Abstract translation: 一种发射供电的无人驾驶飞行器（10）的方法，所述方法包括通过从基本上地面等级的位置附近到升高的高度的轻于空气的载体（12）来提升所述车辆（10），其中所述车辆 （10）在上升期间被阻止进入其飞行模式，使得车辆（10）相对于运载器（12）的速度基本上为零，车辆（10）从托架（12）脱离，车辆 10）此后随着其高度减小，其速度能够防止任何进一步的下降并且可以开始独立的持续飞行。

公开(公告)号：WO2014011255A2

公开(公告)日：2014-01-16

申请号：PCT/US2013034420

申请日：2013-03-28

Applicant: MORRISON CONSULTING GROUP INC W

Inventor： YATES WILLIAM M ,  USSERY ROBERT ,  YOUNG BRYON

IPC: G01C21/34 ,  B60W10/18 ,  B60W40/04 ,  B60W40/06

CPC classification number: B64D39/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/104 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/187 ,  B64D5/00 ,  B64D27/24

Abstract: Electric aircraft, including in-flight rechargeable electric aircraft, and methods of operating electric aircraft, including methods for recharging electric aircraft in-flight, through the use of unmanned aerial vehicle (UAV) packs flying independent of and in proximity to the electric aircraft.

Abstract translation: 电动飞机，包括飞行中可充电电动飞机，以及运行电动飞机的方法，包括通过使用独立于飞机和飞机附近飞行的无人驾驶飞行器（UAV）组件，在飞行中为电动飞机充电的方法。

公开(公告)号：US20240123843A1

公开(公告)日：2024-04-18

申请号：US18047303

申请日：2022-10-18

Applicant: International Business Machines Corporation

Inventor： Sarbajit K. Rakshit ,  Satyam Jakkula ,  Sudheesh S. Kairali ,  Sudhanshu Sekher Sar

IPC: B60L53/126 ,  B60L53/36 ,  B60L53/66 ,  B64C39/02

CPC classification number: B60L53/126 ,  B60L53/36 ,  B60L53/66 ,  B64C39/024 ,  B60L2200/10 ,  B64C2201/066 ,  B64C2201/128

Abstract: Computer-implemented methods for wireless power transfer among multiple vehicles are provided. Aspects include identifying a group of vehicles, from a plurality of vehicles, that require charging and identifying a wireless charging capability of each vehicle of the group of vehicles. Aspects also include deploying wireless power chargers to the vehicles of the group of vehicles that do not have wireless charging capability and charging each vehicle of the group of vehicles using a wireless power transfer module. The charging of the group of vehicles is performed while the vehicles are in motion.

公开(公告)号：US20240118695A1

公开(公告)日：2024-04-11

申请号：US17961562

申请日：2022-10-07

Applicant: Honda Motor Co., Ltd.

Inventor： Ryuta SUZUKI ,  Takashi HASHIZUME

IPC: G05D1/00 ,  B64C39/02 ,  G05D1/10

CPC classification number: G05D1/0094 ,  B64C39/024 ,  G05D1/0038 ,  G05D1/106 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/127 ,  B64C2201/146

Abstract: A terminal device, adapted to control a drone to support navigation of a boat, the terminal device including a control unit and a display unit. The control unit including a processor, configured to obtain a speed of the boat, and receive an image that is imaged by the drone. The display unit including a display for displaying the image that is imaged by the drone, wherein the terminal device is configured to control an altitude of the drone based on the speed of the boat.

公开(公告)号：US20230302933A1

公开(公告)日：2023-09-28

申请号：US17700538

申请日：2022-03-22

Applicant: STRIX DRONES LTD

Inventor： Niv Aharoni ,  Maoz Klein

IPC: B60L53/35 ,  B60L53/10 ,  B64C39/02

CPC classification number: B60L53/35 ,  B60L53/10 ,  B64C39/024 ,  B64C2201/12 ,  B64C2201/066

Abstract: An electrical communication system for unmanned aerial vehicle that includes conductive contact surfaces with magnets that are attached to a landing platform, and conductive pin systems that are attached to the vehicle. Each conductive pin system includes a conductive pin that its lower end is made of a magnetizing material, and its upper end is connected to the controller and the battery of the vehicle. The conductive pin systems includes a main body, that is attached to the vehicle, with a hole inside which the conductive pin is penetrated, a nut assembled on the upper end of the pin, a spring that is wounded on the pin between the nut and the main body so that the spring pushes upwards the pin, and a cable connector that is connected to the upper end of the pin to enable electrical connection with the controller and the battery.

公开(公告)号：US11691761B2

公开(公告)日：2023-07-04

申请号：US16876203

申请日：2020-05-18

Applicant: FlyFocus Sp. z.o.o.

Inventor： Kacper Antoni Dolata ,  Igor Jan Skawinski ,  Bartlomiej Mateusz Zawada ,  Julian Daniel Zyromski

IPC: B64F3/02 ,  B64C39/02 ,  B64D47/08 ,  B60L53/16 ,  B60L53/20 ,  B60L53/66

CPC classification number: B64F3/02 ,  B60L53/16 ,  B60L53/20 ,  B60L53/66 ,  B64C39/022 ,  B64D47/08 ,  B60L2200/10 ,  B60L2210/10 ,  B60L2210/30 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/127

Abstract: A surveillance drone system is provided herein generally including an UAV, a base power station, and, a tether for connecting the UAV to the base power station to provide electrical power to the UAV when airborne. The base power station may include a cable take-up assembly for releasing and taking up the tether. A plug or power module is provided at the free end of the tether configured to be detachably coupled with the UAV, to transmit electrical power to, and, possibly, data to and from, the UAV. With the plug or power module being detached, the UAV is free to fly unrestricted. This arrangement allows for the UAV to be airborne for prolonged periods to allow for monitoring a region and for release to allow the UAV to investigate anomalies in the monitored region.

公开(公告)号：US20190237999A1

公开(公告)日：2019-08-01

申请号：US15886362

申请日：2018-02-01

Applicant: The Boeing Company

Inventor： Brian J. Tillotson ,  Teiyuri Aoshima

IPC: H02J50/12 ,  H02J50/90 ,  B64C3/32 ,  H02J7/02 ,  H01F38/14

CPC classification number: H02J50/12 ,  B64C3/32 ,  B64C2201/066 ,  H01F38/14 ,  H02J7/025 ,  H02J50/90

Abstract: Systems and methods for recharging the battery onboard an aircraft (hereinafter “receiving aircraft”) via resonant inductive coupling. In accordance with some embodiments, wireless power transfer to the receiving aircraft is effected by means of a second aircraft (hereinafter “transmitting aircraft”). The receiving and transmitting aircraft are both equipped with respective LC circuits. The aircraft fly in a formation such that transmit coils onboard the transmitting aircraft and receive coils onboard the receiving aircraft are separated by a distance within a resonant inductive coupling range. During the recharge procedure, each transmit coil is driven by an alternating current source having a frequency equal to the resonant frequency of the LC circuit onboard the receiving aircraft. The receive coils then feed the induced alternating current to a rectifier for supplying direct current to the onboard battery charger.