公开(公告)号：US20240118695A1

公开(公告)日：2024-04-11

申请号：US17961562

申请日：2022-10-07

申请人： Honda Motor Co., Ltd.

发明人： Ryuta SUZUKI ,  Takashi HASHIZUME

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

CPC分类号： G05D1/0094 ,  B64C39/024 ,  G05D1/0038 ,  G05D1/106 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/127 ,  B64C2201/146

摘要： 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：US20230367380A1

公开(公告)日：2023-11-16

申请号：US17663434

申请日：2022-05-16

申请人： CHENGDU QINCHUAN IOT TECHNOLOGY CO., LTD.

发明人： Zehua SHAO ,  Bin LIU ,  Yaqiang QUAN ,  Yong LI ,  Xiaojun WEI

IPC分类号： G06F1/26 ,  G08G1/095 ,  G08G1/01 ,  B64C39/02

CPC分类号： G06F1/26 ,  G08G1/095 ,  G08G1/0133 ,  G08G1/0145 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/12 ,  B64C2201/141

摘要： The embodiments of the present disclosure provide a method, system, and medium for traffic management in a smart city based on Internet of Things (IoT). The method is implemented on the traffic management platform, comprising: obtaining power supply detection information of traffic indication device through a sensor network platform; predicting a congestion degree at a location of the traffic indication device in a target time period when the power supply detection information is in a power-off state; and determining whether a temporary power supply is needed to be provided to the traffic indication device based on the congestion degree.

公开(公告)号：US20230343101A1

公开(公告)日：2023-10-26

申请号：US17659851

申请日：2022-04-20

申请人： Ford Global Technologies, LLC

发明人： Stuart C. Salter ,  Brendan Diamond ,  John Robert Van Wiemeersch ,  Tarik Safir ,  Sam Harris

IPC分类号： G06V20/52 ,  G06V20/17 ,  G06V20/58 ,  G08G5/00 ,  B64C39/02 ,  B60L58/12

CPC分类号： G06V20/52 ,  G06V20/17 ,  G06V20/58 ,  G08G5/0034 ,  B64C39/024 ,  B60L58/12 ,  B64C2201/127 ,  B64C2201/208 ,  B64C2201/042

摘要： The disclosure generally pertains to systems and methods for providing a vehicle-and-drone-based security service. In an example method, a first area of interest and a second area of interest associated with a structure may be determined. The first area of interest may then be determined to be monitored at the vehicle. The second area of interest may also be determined to be monitored at a drone associated with the vehicle. A route may be identified for the drone to travel along, where the route is configured for the drone to monitor the second area of interest. The drone may then be launched via the vehicle to travel along the route to monitor the second area of interest.

公开(公告)号：US20230264833A1

公开(公告)日：2023-08-24

申请号：US17652357

申请日：2022-02-24

申请人： Microavia International Limited

发明人： Ivan Biriuk ,  Denis Kotov

IPC分类号： B64F1/00 ,  B64C39/02 ,  B64F1/22

CPC分类号： B64F1/007 ,  B64C39/024 ,  B64F1/222 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/201

摘要： A packaging system for a plurality of drones is disclosed herein. The packaging system is designed for drones, which include a plurality of downward facing propellers and a drone body configured operatively below the plurality of downward facing propellers in a downwardly extending configuration. The packaging system comprises a primary container; and a plurality of secondary containers for holding ten of the drones therein, wherein the secondary containers have dimensions for facilitating accommodation of nine of the secondary containers in the primary container.

公开(公告)号：US20230227157A1

公开(公告)日：2023-07-20

申请号：US17852101

申请日：2022-06-28

申请人： Hyundai Motor Company ,  Kia Corporation

发明人： Jung Hun CHOI ,  Dong Hyun Ha ,  Jae Wung Jung

IPC分类号： B64C39/02 ,  F03D9/32 ,  B64B1/62 ,  B64C3/56 ,  B64D27/24 ,  B64D47/00 ,  B64C13/28 ,  B64C11/18 ,  H02K7/18

CPC分类号： B64C39/024 ,  F03D9/32 ,  B64B1/62 ,  B64C3/56 ,  B64D27/24 ,  B64D47/00 ,  B64C13/28 ,  B64C11/18 ,  H02K7/183 ,  F05B2220/706 ,  B64C2201/042 ,  B64C2201/022

摘要： An aero wind power generation apparatus includes: a drone unit including drone wings configured to make the aero wind power generation apparatus move and hover and a sensor unit configured to detect information for controlling the aero wind power generation apparatus; a buoyancy generation unit connected to the drone unit and including a side cover configured to open or close and a balloon provided inside the side cover, wherein the buoyancy generation unit is configured to enable injection of gas into or release of the gas from the balloon; and a power generation unit connected to the buoyancy generation unit and including a rotating unit with a plurality of blades, a blade control unit of adjusting the state of the blades, and a motor unit of converting kinetic energy transferred from the rotating unit into electrical energy.

公开(公告)号：US11691761B2

公开(公告)日：2023-07-04

申请号：US16876203

申请日：2020-05-18

申请人： FlyFocus Sp. z.o.o.

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

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

CPC分类号： 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

摘要： 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：US20230205197A1

公开(公告)日：2023-06-29

申请号：US17564430

申请日：2021-12-29

申请人： BETA AIR, LLC

发明人： Timothy Gerard Richter ,  Sean Donovan

IPC分类号： G05D1/00 ,  B64C39/02 ,  G07C5/00

CPC分类号： G05D1/0005 ,  B64C39/024 ,  G07C5/008 ,  B64C2201/042 ,  B64C2201/12

摘要： A system for redistributing electrical load in an electric aircraft. The system includes a ring bus and a controller communicatively connected to the ring bus. The ring bus includes a plurality of bus sections including a first bus section and a second bus section. The controller is configured to receive a fault datum indicative of a fault associated with one of a first energy source and a second energy source, actuate, as a function of the fault datum, at least a switch to electrically connect the first bus section and the second bus section so as to form an electrical merger of the first bus section and the second bus section, and redistribute the electrical load to compensate for the fault associated with one of the first energy source and the second energy source. A method of redistributing electrical load in an electric aircraft is also provided.

公开(公告)号：US20230202680A1

公开(公告)日：2023-06-29

申请号：US17561765

申请日：2021-12-24

申请人： ABDALLAH YEHYA

发明人： ABDALLAH YEHYA

IPC分类号： B64F1/00 ,  B64C39/02 ,  B60L53/51

CPC分类号： B64F1/007 ,  B64C39/024 ,  B60L53/51 ,  B64C2201/021 ,  B64C2201/088 ,  B64C2201/201 ,  B64C2201/042 ,  B64C2201/123

摘要： The present disclosure provides a versatile drone and nest launching system. A hybrid UAV drone having fixed wings in addition to vertical take-off and landing capabilities is used to enable the launching nest to remain compact and of simple design with few moving parts, while also housing a drone capable of travelling long distances. The entire system is configured function autonomously, utilising a solar-powered charging pad installed on the nest to repeatedly recharge and relaunch depleted drones. Novel mounting systems for situating the nest in a variety of terrains are also disclosed.

公开(公告)号：US20230202652A1

公开(公告)日：2023-06-29

申请号：US17645752

申请日：2021-12-23

申请人： OCTOFAN SAS

发明人： Pierre Convert

IPC分类号： B64C29/00 ,  B64C3/54 ,  B64C11/00 ,  B64C11/48 ,  B64C39/02 ,  B64C39/08

CPC分类号： B64C29/0033 ,  B64C3/54 ,  B64C11/001 ,  B64C11/48 ,  B64C39/024 ,  B64C39/08 ,  B64C2201/088 ,  B64C2201/042 ,  B64C2201/102 ,  B64C2201/162

摘要： The aircraft comprises a fuselage defining a fuselage main axis. The fuselage comprises a docking system for fixing removable nacelles. The aircraft has wings equipped with tilting actuators for rotating wings about rotation axes parallel to the fuselage main axis and at least six propellers mechanically connected to the fuselage. The aircraft also has at least one cryo-hydrogen tank and at least one fuel cell for supplying power to the propellers, and
A capacitor for supplying power to the propellers, charged by at least one fuel cell. This capacitor stores electrical energy greater than the energy needed by all the propellers for ten seconds of hovering flight. Each propeller is equipped with a tilting actuator for rotating the propeller about a rotation axis making an angle of less than 45 degrees with a plane perpendicular to the fuselage main axis. The fuselage having a forward and a rear portion defining a forward to rear order of the propellers, in cruise flight, the two forward propellers are activated to provide vertical thrust, the intermediate propellers between the forward and rearmost propellers are not activated and the two rearmost propellers are activated to provide horizontal thrust.

公开(公告)号：US20230150662A9

公开(公告)日：2023-05-18

申请号：US17490942

申请日：2021-09-30

申请人： William C. Peterson

发明人： William C. Peterson

IPC分类号： B64C39/02 ,  B64D9/00 ,  B64C35/00 ,  B64D27/24 ,  B64C3/16

CPC分类号： B64C39/024 ,  B64D9/003 ,  B64C35/005 ,  B64C35/001 ,  B64C35/006 ,  B64D27/24 ,  B64C3/16 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/128 ,  B64C2201/146 ,  B64C2201/141

摘要： An unmanned Wing In Ground Effect vessel (UWIG) for transporting the cargo with internal cargo hold contained in a seaworthy fuselage. The UWIG is autonomous or semi-autonomous. A pair of wings are attached to the fuselage. An on-board controller controls lift sufficient lift to travel in ground effect. The controller also controls UWIG surface maneuvering, taxiing and flying. The UWIG may be autonomous or semi-autonomous.