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公开(公告)号：US20130255986A1
公开(公告)日：2013-10-03
申请号：US13848753
申请日：2013-03-22
Applicant: ICON POLYMER GROUP LIMITED
Inventor： Timothy Denzil Price , Calvin Tan
IPC: F16L11/22
CPC classification number: F16L11/22 , B60L3/0046 , B60L3/0069 , B60L3/04 , B60L53/16 , B60L53/18 , B60L2200/10 , B60L2240/36 , B60L2240/662 , B64C39/024 , B64C2201/063 , B64C2201/066 , B64D39/00 , B64D39/06 , F16L11/127 , H01R12/77 , H01R13/005 , H01R13/6683 , H01R2201/26 , Y02T10/7005 , Y02T10/7088 , Y02T10/7291 , Y02T90/121 , Y02T90/14 , Y02T90/16
Abstract: A hose is disclosed for conveying fluids. The hose has a wall defining a fluid carrying tube and a power and/or data transmission cable is integrated into said wall. Also disclosed is a user definable module that is removably attachable to the distal end of a fluid conveying hose. The hose being releasably connectable to a fluid receiving entity to provide fluid to said entity. The fluid conveying hose has a wall defining a fluid carrying tube and a power and/or data transmission cable integrated into that wall. The user definable module is connectable to the cable and has components to measure at least one measurable parameter at the end of the hose and/or provide electrical connection between the cable and said fluid receiving entity for the transmission of data and/or power along the hose via said user definable interface. Also disclosed is a method of configuring a hose for fluid transfer. The method includes the step of selecting a user definable module and attaching the selected module to a distal end of the hose prior to connecting said hose to a fluid receiving entity.
Abstract translation: 公开了用于输送流体的软管。 软管具有限定流体输送管的壁，并且将功率和/或数据传输电缆集成到所述壁中。 还公开了可拆卸地附接到流体输送软管的远端的用户可定义的模块。 软管可释放地连接到流体接收实体以向所述实体提供流体。 流体输送软管具有限定流体输送管和集成到该壁中的电力和/或数据传输电缆的壁。 用户可定义的模块可连接到电缆，并且具有测量软管端部的至少一个可测量参数的组件和/或在电缆和所述流体接收实体之间提供电连接，用于沿着所述电缆传输数据和/或电力 软管通过用户可定义的界面。 还公开了一种配置用于流体转移的软管的方法。 该方法包括在将所述软管连接到流体接收实体之前，选择用户可定义模块并将所选模块附接到软管的远端的步骤。
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公开(公告)号：US20240194081A1
公开(公告)日：2024-06-13
申请号：US18077371
申请日：2022-12-08
Applicant: Wing Aviation LLC
Inventor： Marcus Hammond
CPC classification number: G08G5/0069 , B64C39/024 , G06V20/17 , B64C2201/066 , B64C2201/18
Abstract: In an example embodiment, a method carried out by an uncrewed aerial vehicle (UAV) may involve receiving a reference map of a cluster of charging pads from a server. The cluster may include a layout of charging pads and fiducial markers distributed across the layout, the reference map representing the layout and fiducial markers. The UAV may fly to the cluster and acquire an image of charging pads and observed fiducial markers near the charging pads. The image may capture an observed constellation of fiducial markers at apparent positions and orientations relative to the charging pads. A reference constellation of fiducial markers at reference positions and orientations relative to reference charging pads may be identified in the reference map. Identities of the reference charging pads and a match of the reference constellation to the observed constellation may be used to disambiguate a particular charging pad from among the charging pads.
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公开(公告)号：US20230271701A1
公开(公告)日：2023-08-31
申请号：US17682736
申请日：2022-02-28
Applicant: Saudi Arabian Oil Company
Inventor： Khaled F. Abusalem , Soliman A. Al-Walaie , Osama Bakur Bahwal
CPC classification number: B64C39/022 , B64C39/024 , B60L53/53 , B60L58/12 , B64C2201/066 , B64C2201/088
Abstract: An unmanned aerial vehicle (UAV) system energized by power lines includes a UAV, a charging mechanism and an electric circuit. The charging mechanism is operatively coupled to a body of the UAV. The charging mechanism can connect to power transmission lines deployed near an air space in which the UAV is airborne and operating. The charging mechanism can draw power from the power transmission lines to power a flight of the UAV. The electric circuit is onboard the UAV. The electric circuit can generate charging currents based on the power drawn from the power transmission lines to power the flight of the UAV while the UAV is airborne.
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公开(公告)号：US20230150383A1
公开(公告)日：2023-05-18
申请号：US17526432
申请日：2021-11-15
Inventor： Yanghe Liu , Shailesh N. Joshi
CPC classification number: B60L53/38 , B60L53/12 , H02J50/005 , B64C39/024 , B64C29/0025 , B60L2200/10 , B64C2201/066
Abstract: A panel for wireless charging of an electric vehicle includes a metamaterial panel with a first shape and a second shape different than the first shape. The metamaterial panel is configured to be positioned between a transmitter coil of a wireless power transfer station (WPTS) and a receiver coil of the electric vehicle during wireless charging of the electric vehicle and change between the first shape and the second shape as a function of at least one of a size of the transmitter coil, a size of the receiver coil, and a distance between the transmitter coil and the receiver coil. A robot with at least one of a robotic arm and a robotic buggy can be included and the metamaterial panel can be coupled to the robot. And the robot is configured to position the metamaterial panel between the transmitter coil of the WPTS and the receiver coil of the electric vehicle during wireless charging of the electric vehicle.
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公开(公告)号：US20190185159A1
公开(公告)日：2019-06-20
申请号：US16210413
申请日：2018-12-05
Applicant: Iain Matthew Russell
Inventor： Iain Matthew Russell
IPC: B64C39/02
CPC classification number: B64C39/024 , B64C2201/042 , B64C2201/066 , B64C2201/08 , B64C2201/141 , B64C2201/18 , B64C2201/205 , B64C2201/206 , B64C2201/208 , G06Q10/00
Abstract: Various measures (for example methods, UAVs, controllers and computer programs) are provided in relation to controlling a UAV. The UAV is caused to provide energy to and receive energy from a given vehicle. The received energy is used to provide power to at least one component of the UAV.
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Patent Agency Ranking
公开(公告)号：US20180277000A1
公开(公告)日：2018-09-27
申请号：US15762877
申请日：2016-08-04
Inventor： Mitsuru UESUGI , Tsuyoshi OSATO
CPC classification number: G08G5/0078 , B64C39/024 , B64C2201/066 , B64C2201/122 , B64C2201/127 , B64C2201/141 , B64D47/08 , B64F1/222 , B64F1/362 , G08C17/02 , G08C2201/40 , G08G1/00 , H04B7/18504 , H04N5/247
Abstract: Observing an observation area wider than a cruising distance of a drone, an acquiring observation data of all observation sections and analyzing all the observation area, even when it is impossible for the operator to go to the observation base due to a failure of a traffic infrastructure and when a failure of a communication infrastructure occurs. The drone flies through the observation section from the observation base, where the drone is on standby, to a next observation base to observe, to transmit all observation data after a first observation section stored in the drone to the next drone on standby at the observation base when the drone lands at the next observation base, and to deliver observation data of all observation sections to the observation base, which is a destination, by sequentially repeating the performance of the transmitting of data between the drones in all observation sections.
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公开(公告)号：US10053213B1
公开(公告)日：2018-08-21
申请号：US15589409
申请日：2017-05-08
Applicant: Pinnacle Vista, LLC
Inventor： Haofeng Tu
CPC classification number: B64C27/26 , B64C27/82 , B64C29/0025 , B64C39/024 , B64C39/12 , B64C2027/8236 , B64C2201/021 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/128 , B64C2201/165 , G05D1/0202 , G05D1/042 , G05D1/0858
Abstract: A multi-copter lift body aircraft has a push or pull propeller and a lift body that has a first airfoil shape on a front to rear cross-section and a second airfoil shape on a left to right cross-section. The lift body is made from a top shell and a bottom shell. The lift body has a nose and a tail. Multi-copter propellers are attached to the lift body. The multi-copter propellers provide a lift at low speeds and the lift body provides a lift at high speeds. Avionics can be stored in a hollow cavity of the lift body. The avionics may include a control circuit, batteries, and a radio receiver. The multi-copter has a lift body made from an upper shell and a lower shell. The lift body has an optimum attack angle at a cruising speed, and the lift body provides a combined lift mode.
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公开(公告)号：US20180222339A1
公开(公告)日：2018-08-09
申请号：US15943581
申请日：2018-04-02
Applicant: Asylon, Inc.
Inventor： Damon C. HENRY , Adam I. MOHAMED , Brent MCLAUGHLIN , David DONES
CPC classification number: B60L11/1822 , B60L53/35 , B60L53/36 , B60L53/80 , B60L2200/10 , B64C39/024 , B64C2201/042 , B64C2201/066 , B64C2201/141 , B64C2201/18 , B64D45/08 , B64F1/007 , B64F1/12 , B64F1/20 , B64F1/362 , G05D1/0027 , G05D1/0676 , G05D1/101 , Y02T10/7005 , Y02T10/7072 , Y02T90/121 , Y02T90/124 , Y02T90/125 , Y02T90/14
Abstract: A reconfigurable system capable of autonomously exchanging material from unmanned vehicles of various types and sizes. The system comprises an environmental enclosure, a landing area, a universal mechanical system to load and unload material from the unmanned vehicle, and a central processor that manages the aforementioned tasks. The landing area may comprise a one or more visible or non-visible markers/emitters capable of generating composite images to assist in landing the unmanned vehicle upon the reconfigurable, autonomous system.
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209.发明申请公开(公告)号：US20180194466A1
公开(公告)日：2018-07-12
申请号：US15913406
申请日：2018-03-06
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor： Kaiyong ZHAO , Mingxi WANG , Xiangyu CHEN
CPC classification number: B64C39/024 , B64C2201/042 , B64C2201/066 , B64C2201/123 , B64C2201/141 , G05D1/0088 , G05D1/0676 , G05D1/102 , G05D1/104
Abstract: An unmanned aerial vehicle (UAV) includes a detection device configured to generate a supplement demand signal in response to a need of the UAV for resource supplement, a wireless communication device configured to establish a wireless communication connection with at least one aerial platform and communicate with the at least one aerial platform in response to the supplement demand signal being generated, and a flight control device configured to determine a target aerial platform from the at least one aerial platform, generate a flight control signal based upon communication information of the target aerial platform received by the wireless communication device, and adjust a spatial distance between the UAV and the target aerial platform based upon the flight control signal to enable an airborne replenishment to the UAV by the target aerial platform.
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210.发明申请公开(公告)号：US20180178899A1
公开(公告)日：2018-06-28
申请号：US15391700
申请日：2016-12-27
Inventor： Dongsoo HAR , Celso MORAES , Dongsuk KUM
CPC classification number: B64D27/24 , B64C3/385 , B64C5/02 , B64C11/001 , B64C13/50 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/162 , B64C2201/165 , Y02T50/62
Abstract: An aircraft includes: a fuselage having opposing leading and trailing extremities along a vertical axis; a fixed wing airframe having opposed at least two main wings connected to the fuselage and extending on a horizontal axis; at least two electric coplanar main wing motors respectively attached to the main wings; a duct frame attach to the trailing extremity of the fuselage; at least two horizontal stabilizers connected to the duct frame and extending on the horizontal axis; an electric tail motor fitted an inner side of the duct frame; multiple battery packs installed inside the fuselage and suitable for supply power to the main wing motors and the tail motor; and support beams suitable for connecting the duct frame to the fuselage.
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