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1.发明申请公开(公告)号：US20230086129A1
公开(公告)日：2023-03-23
申请号：US17909021
申请日：2020-03-05
摘要： The invention relates to an airborne platform comprising a main body configured for flying over a region of interest and an electrical charging system fixed to the main body and located outside of the main body. The electrical charging system comprising at least one induction coil intended to remotely charge at least one battery of at least one apparatus.
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公开(公告)号：US20230069643A1
公开(公告)日：2023-03-02
申请号：US17794556
申请日：2020-06-08
申请人： AERONEXT INC.
发明人： Yoichi SUZUKI
摘要： The present disclosure relates to a flying body. The flying body includes a mounting space for mounting an object, a loading port for loading the object in the mounting space, and a take-out port for taking out the object loaded in the mounting space, wherein the loading port and the take-out port are provided at least partially at different positions. According to such a configuration, even a person without specialized knowledge can operate it easily and safely.
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公开(公告)号：US11573566B2
公开(公告)日：2023-02-07
申请号：US16926914
申请日：2020-07-13
申请人： NAVICO HOLDING AS
发明人： Jeremiah Clark , Andrew Corbett , Mark N. Harnett , Alan Islas Cital , Thomas E. H. Isaacson , Matthew Laster , William B. Newberry, Jr. , Shauna Reed , Kristopher C. Snyder
IPC分类号： G05D1/00 , B64D1/02 , B64D47/08 , B64C39/02 , B63G8/00 , G01S15/89 , G01S15/88 , G01S13/88 , G01S7/00 , G01S15/96 , B64D47/02 , G01S7/62 , G05D1/02 , B63B34/00 , B63B35/00 , B63B21/66
摘要： Many different types of systems are utilized and tasks are performed in a marine environment. The present invention provides various configurations of castable devices that can be operated and/or controlled for such systems or tasks. One or more castable devices can be integrated with a transducer assembly, such as a phased array, that emits sonar beams and receives sonar returns from the underwater environment. Processing circuitry may receive the sonar returns, process the sonar returns, generate an image, and transmit the image to a display.
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公开(公告)号：US20220406067A1
公开(公告)日：2022-12-22
申请号：US17889897
申请日：2022-08-17
发明人： Rene SEEBER , Ingo Seebach , Henning Meyer , Markus Schoeler , Kai Baumgart , Christian Scheibe , David Prantl
摘要： Systems, methods, and apparatus for performing an action when an aggregated confidence measure. Data is received from a first sensor proximate to a particular air space. Data is also received from a second sensor and a third sensor proximate to the particular air space. The data from the first sensor, second sensor, and third sensor are each analyzed to determine respective confidence measures that a UAV is within the particular air space. The first sensor corresponds to a first type of data, the second sensor corresponds to a second type of data, and the third sensor corresponds to a third type of data. The confidence measures from each sensor are aggregated together to generate a combined confidence measure indicating a possible presence of the UAV within in the particular air space. When the combined confidence measure exceeds a threshold, an action is taken.
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公开(公告)号：US11531050B2
公开(公告)日：2022-12-20
申请号：US16723858
申请日：2019-12-20
申请人： DISH Network L.L.C.
摘要： A drone deployable power line fault detection sensor. The sensor can include a clamp mechanism having a clamp ring with first and second ring portions movably connected to each other and a resilient member positioned to urge the first and second ring portions toward a closed configuration. A latch can be positioned to retain the first and second ring portions in an open configuration whereby the sensor can be positioned on a power transmission line with a drone. A trigger can be coupled to the latch and operative, under the weight of the sensor, to disengage the latch thereby releasing the first and second ring portions to close around the transmission line under the force of the resilient member. One or more sensors are carried by the clamp mechanism and positioned to detect a line fault on the power transmission line, which is reported to a power station control system to de-energize the power transmission line.
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公开(公告)号：US11488385B2
公开(公告)日：2022-11-01
申请号：US16864854
申请日：2020-05-01
发明人： Alexander Morrow , Zachary Schmid , Joe Price , Mitch Meverden , Rene Seeber
摘要： Systems, methods, and apparatus for identifying, tracking, and disrupting UAVs are described herein. Sensor data can be received from one or more portable countermeasure devices or sensors. The sensor data can relate to an object detected proximate to a particular airspace. The system can analyze the sensor data relating to the object to determine a location of the object and determine that the object is flying within the particular airspace based at least in part on location data. A portable countermeasure device can be identified that corresponds to the location of the object. The system can transmit information about the object to the identified portable countermeasure device. The portable countermeasure device can transmit additional data relating to the object to the system.
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公开(公告)号：US11465745B1
公开(公告)日：2022-10-11
申请号：US17127542
申请日：2020-12-18
摘要： An air delivery barrel system is described, the air delivery barrel system includes a strap system that provides line stretch of the strap system when a force is exerted on the strap system, the strap system including a continuous strap, a first barrel, the first barrel being formed out of a cylindrically shaped wall and the cylindrically shaped wall including a channel that the strap system passes through, an end cap, the end cap being detachably connectable to a bottom end of the first barrel, the end cap protecting a bottom portion of the strap system, a lid, the lid being detachably connectable to a top end of the first barrel, the lid including a recess through which the strap system passes through, and a second barrel that can be situated within the first barrel and the cylindrically shaped wall of the first barrel protects the second barrel.
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公开(公告)号：US20220299296A1
公开(公告)日：2022-09-22
申请号：US17641573
申请日：2020-08-19
摘要： The invention provides an airborne passive decoy system for use in the radio waveband, the system comprising a controllable aerial propulsion unit and one or more retroreflectors, wherein the one or more retroreflectors are mounted on, contained within or otherwise borne by the controllable propulsion unit, and wherein the system is configured such that the one or more retroreflectors can be deployed as a decoy at a desired location and/or time. The system is an integral system which does not rely on tethers, cables or suchlike. Related methods and uses are also provided.
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公开(公告)号：US20220289375A1
公开(公告)日：2022-09-15
申请号：US17631893
申请日：2020-07-28
发明人： Henrik SCHÄFER , Florian BECKER
摘要： A method for autonomous in-flight transfer of a load from a first Aerial Vehicle, AV, to a second AV is provided. Each of the first AV and the second AV includes a frame with a vertical opening for receiving the load. A plurality of rotors are attached to the frame. The method comprising autonomously performing the following in-flight: fastening means of the first AV hold the load in the vertical opening of the first AV such that a bottom end of the load is accessible by the second AV; the second AV approaches the first AV from below in order to couple a fastening means of the second AV to the bottom end of the load; the fastening means of the first AV releases the load after the fastening means of the second AV couples to the bottom end of the load; and the fastening means of the second AV lower the load with respect to the frame of the second AV in order to move the load into a flight position.
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公开(公告)号：US11370543B2
公开(公告)日：2022-06-28
申请号：US16835684
申请日：2020-03-31
发明人： Yoav Herzig
摘要： A pylon for mounting to a bottom surface of an aircraft and for carrying an external payload is provided. The pylon comprises a body spanning along a vertical axis between an upper face and a lower face, the upper face comprising one or more mounting arrangements configured to facilitate mounting the pylon to the bottom surface of the aircraft, the lower face comprising at least one suspension mechanism configured to facilitate selective attachment of the payload to the pylon. The pylon further comprises a covering arrangement configured for selective shifting between a closed position in which it covers the suspension mechanism and an open position in which the suspension mechanism is uncovered. The width of the body varies smoothly along the vertical axis between, inclusively, the upper and lower faces.
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