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公开(公告)号:US20180305004A1
公开(公告)日:2018-10-25
申请号:US15576799
申请日:2016-05-25
Applicant: DOTTEREL TECHNOLOGIES LIMITED
Inventor: Samuel Seamus ROWE , Shuan Taggart Pentecost
CPC classification number: B64C27/20 , B64C27/08 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2220/00
Abstract: A shroud for an aircraft having a noise reducing material on or in an inner surface of the shroud adjacent to one or more tips of the propeller. The noise reducing material is preferably an electrospun nanomaterial, particularly a ridged composite acoustic nanofibre. The interior surface of the shroud may be provided with a plurality of sound deflectors configured to dissipate sound by reflection and refraction, and absorb sound into the shroud body. The sound deflectors may be ribs or arrangements of discrete reflector elements.
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公开(公告)号:US20180292223A1
公开(公告)日:2018-10-11
申请号:US15573978
申请日:2015-07-07
Applicant: Halliburton Energy Services, Inc.
Inventor: Nathan P. Leach
CPC classification number: G01C21/3469 , B64C39/02 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/123 , B64C2201/127 , B64C2201/146 , B64D47/08 , B64F5/10 , G01C21/20 , G01C21/3415 , G01C21/3461 , G05D1/0094 , G05D1/0214 , G05D1/0225 , G05D1/101 , G05D2201/0207 , H04N5/23203 , H04N5/23216 , H04N5/23296 , H04N7/185
Abstract: A monitoring system may include a semi-autonomous mobile monitoring device capable of determining whether it has a sufficient power level to perform a monitoring task based on the distance between the position of the mobile monitoring device and a task area corresponding to the monitoring task. Upon determining a sufficient power level to perform the monitoring task, the mobile monitoring device may calculate a path to a task area corresponding to the monitoring task based on map information stored in a memory of the mobile monitoring device. The mobile monitoring system may automatically avoid known obstacles in the monitoring area between the position of the mobile monitoring device and the task area without using a remote control.
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公开(公告)号:US20180281935A1
公开(公告)日:2018-10-04
申请号:US16005309
申请日:2018-06-11
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor: Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
IPC: B64C27/08 , B64C25/06 , B64C25/32 , B64C27/00 , B64D43/00 , G01V3/16 , B64C27/54 , B64C1/30 , B64C39/02 , G05D1/00 , G01R33/00
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
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24.
公开(公告)号:US20180279105A1
公开(公告)日:2018-09-27
申请号:US15504518
申请日:2015-08-19
Applicant: AERYON LABS INC.
Inventor: Scott HUBER , Nevin MCCALLUM , Sean MCCABE , Ian MCDONALD , Thomas Charles NAGY
CPC classification number: H04W4/90 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/128 , H04L63/08 , H04W4/021 , H04W4/025 , H04W4/04 , H04W4/12 , H04W12/06 , H04W48/12 , H04W76/10 , H04W76/50
Abstract: Embodiments described herein relate to an autonomous emergency system (EMS) for UAVs and UMVs. The autonomy of the emergency system enables the vehicle to self-detect that it is in an emergency state (autonomous detection). When vehicle detects the emergency state the vehicle is configured to implement an improved autonomous emergency system process. The vehicle triggers autonomous state change, and controls its operation (auxiliary, power levels, and so on). The vehicle has beacons to emit pulses over time intervals to communicate with specific vehicles. For example, when known, friendly, other vehicles come into a specific radius, the EMS detects the friendly vehicle(s) and sends safe signals. The EMS implements a pairing communication process based on pre-establish configurations and protocols.
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25.
公开(公告)号:US20180275685A1
公开(公告)日:2018-09-27
申请号:US15918660
申请日:2018-03-12
Applicant: Samsung Electronics Co., Ltd.
Inventor: Jongho KIM , Yun Woo Lee , Kyonggon Choi
CPC classification number: G05D1/12 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/141 , B64D47/08 , G05D1/0016 , G05D1/0094 , G06T7/248 , G06T7/70 , G06T2207/30241
Abstract: An electronic device may include a communication module, a memory storing instructions, and one or more processors coupled to the communication module. The one or more processors may be configured to execute the instructions to receive information related to a movement of an external electronic device from the external electronic device by using the communication module, determine a range of moving the electronic device, at least on the basis of the information related to the movement, determine a location to which the electronic device is moved, at least on the basis of the range, and move the electronic device to the location.
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公开(公告)号:US20180273194A1
公开(公告)日:2018-09-27
申请号:US15571258
申请日:2016-04-29
Applicant: Intelligent Energy Limited
Inventor: David Edgar , Henri Winand
CPC classification number: B64D27/24 , B64C39/024 , B64C2201/021 , B64C2201/027 , B64C2201/042 , B64C2201/104 , B64C2201/108 , B64C2201/165 , B64D2041/005 , B64D2211/00 , H01M8/1007 , H01M2250/20 , Y02T50/55 , Y02T50/62 , Y02T90/32 , Y02T90/36
Abstract: The disclosure relates to an unmanned aerial vehicle, wherein the fuel cell provides a structural component of the vehicle.
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公开(公告)号:US20180265222A1
公开(公告)日:2018-09-20
申请号:US15781498
申请日:2016-12-06
Applicant: Kunio TAKAGI
Inventor: Noriko TAKAGI
IPC: B64F1/32 , B64C13/18 , B64C13/20 , B64C27/08 , B64C39/02 , B64D47/08 , B65D25/02 , B65G61/00 , G05D1/10
CPC classification number: B64F1/32 , B64C13/18 , B64C13/20 , B64C27/08 , B64C39/02 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/128 , B64C2201/141 , B64C2201/182 , B64C2201/208 , B64D47/08 , B65D25/02 , B65D88/14 , B65G61/00 , G05D1/0676 , G05D1/102
Abstract: A transport system using an unmanned aerial vehicle that overcomes restrictions on distance, time, and the like, thereby expanding a deliverable range for improved convenience. A transport system using an unmanned aerial vehicle that is capable of performing three-dimensional movement using electric power supplied thereto. The unmanned aerial vehicle is mounted with a container for storing a cargo to be transported and is flown by means of relay stations that cover the shipment source with the shipment destination of the cargo. The container is provided with a power storage unit for storing electric power to be supplied to the unmanned aerial vehicle, and the power storage unit of the container is charged at the relay station when the container is not being moved.
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公开(公告)号:US20180265191A1
公开(公告)日:2018-09-20
申请号:US15921881
申请日:2018-03-15
Applicant: Hideomi SAKUMA
Inventor: Hideomi SAKUMA
CPC classification number: B64C29/02 , B64C11/46 , B64C39/024 , B64C2201/021 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/104 , B64C2201/108 , B64C2201/146 , B64C2201/165 , G05D1/0808
Abstract: An aircraft includes propellers at a center of the airframe; a first power source; a pitch adjuster to change pitch angles of the propellers; a plurality of attitude control propellers; a second power source lower in output than the first power source; and a control circuit to control attitude of the airframe. The control circuit includes a first yaw rotation generation control unit to control first yaw rotation generated by torques of the propellers with the pitch adjuster; and a second yaw rotation generation control unit to control a second yaw rotation generated by torques generated by a difference in rotation speed between the attitude control propellers. The control circuit is configured to control the first yaw rotation generation control unit and the second yaw rotation generation control unit in accordance with a magnitude of a command value of yaw rotation.
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公开(公告)号:US20180257502A1
公开(公告)日:2018-09-13
申请号:US15761311
申请日:2016-09-29
Applicant: LG INNOTEK CO., LTD.
Inventor: Sung Soo PARK
CPC classification number: B60L11/1829 , B60L53/12 , B60L53/36 , B60L53/38 , B60L53/60 , B60L2200/10 , B64C25/32 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/108 , B64C2201/145 , B64F1/007 , H02J7/025 , H02J50/10 , H02J50/12 , H02J50/40 , H02J50/50 , H02J50/80 , H02J50/90 , Y02T10/7005
Abstract: A driving method of an unmanned aerial vehicle according to an embodiment may include moving, by the unmanned aerial vehicle, based on GPS information, receiving a wireless signal including position information about a charging apparatus from the charging apparatus, determining whether the GPS information matches the position information included in the wireless signal and landing based on the GPS information and the wireless signal, transferring a reception packet including power information about the unmanned aerial vehicle to the charging apparatus, and receiving precise position information including position coordinates of the charging apparatus generated based on the reception packet.
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公开(公告)号:US20180245365A1
公开(公告)日:2018-08-30
申请号:US15752901
申请日:2016-08-17
Applicant: H3 Dynamics Holdings Pte. Ltd.
Inventor: Taras Wankewycz
CPC classification number: E04H6/44 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/148 , B64C2201/201 , B64F1/007 , B64F1/222 , E04H6/04 , H02J7/00 , H02J7/0042 , H02J7/025
Abstract: The application provides a storage unit for an Unmanned Aerial Vehicle (UAV). The storage unit includes a container, a UAV landing platform, and a receptacle. The container is provided for enclosing the UAV. The receptacle is positioned above the UAV landing platform and it includes at least one inclined surface for guiding a landing UAV to a predetermined UAV landing position on the UAV landing platform.
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