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公开(公告)号:US20240294280A1
公开(公告)日:2024-09-05
申请号:US18495549
申请日:2023-10-26
申请人: Ryan Joseph Bohm , Daniel Garrett
发明人: Ryan Joseph Bohm , Daniel Garrett
CPC分类号: B64U20/40 , B60L50/60 , B64U10/16 , B64U30/29 , B64U50/30 , B64U80/86 , B60L2200/10 , B64U2101/61
摘要: A flying vehicle that is compact and portable and can be carried over the roof rack of a passenger car. The flying vehicle includes an upper chassis and a lower chassis removably mounted to the upper chassis. The lower chassis is positioned below the upper chassis. Eight rotors, a battery pack, and a control unit are mounted to the upper chassis. A seat for the rider is mounted to the lower chassis directly below the battery pack. Such a position of the seat allows a rider to egress from the vehicle safely without requiring the vehicle to land and turn off the rotors.
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公开(公告)号:US20240166385A1
公开(公告)日:2024-05-23
申请号:US18228943
申请日:2023-08-01
申请人: Darkhive, Inc.
发明人: Steven Turner , John Goodson , David Moroniti
IPC分类号: B64U30/299 , B64U30/26 , B64U50/30
CPC分类号: B64U30/299 , B64U30/26 , B64U50/30
摘要: An uncrewed aerial vehicle (UAV) configured and operable for controllable flight, including autonomous flight. A generally planar body defining opposing front and back planar surfaces includes a plurality of circular duct openings provided in the planar body extending between the opposing front and back surfaces. A plurality of rotor guard assemblies are provided wherein each respective rotor guard assembly is configured for detachable engagement with a respective duct opening. A rotor is respectively rotatably mounted in each respective duct opening of the plurality of duct openings whereby each rotor is configured for providing propulsion of the UAV planar body. An electronic controller is operatively coupled to each rotor for controlling rotation of each rotor wherein the electronic controller is configured to enable flight of the UAV via a single hand-throw from a user operator of the UAV.
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3.
公开(公告)号:US20230382570A1
公开(公告)日:2023-11-30
申请号:US17824382
申请日:2022-05-25
申请人: BETA AIR, LLC
发明人: Steven J. Foland , Thomas Henck , Herman Wiegman
摘要: An apparatus for determining a resource remaining datum of an electric aircraft is disclosed. The apparatus includes a processor and a memory communicatively connected to the processor. The memory contains instructions configuring the processor to receive aircraft data from at least a sensing device, wherein the at least a sensing device is configured to measure at least a parameter of a battery pack of the electric aircraft and generate aircraft data as a function of the at least a parameter of the battery pack of the electric aircraft. The memory contains instructions configuring the processor to determine a reserve energy as a function of a flight mode of the electric aircraft and determine a resource remaining datum as a function of the aircraft data and the reserve energy, wherein the resource remaining datum is related to the battery pack of the electric aircraft.
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4.
公开(公告)号:US20230344054A1
公开(公告)日:2023-10-26
申请号:US18344327
申请日:2023-06-29
发明人: Fanggui PENG , Zhifei HUANG , Ying WANG
IPC分类号: H01M50/242 , H01M50/298 , H01M50/249 , H01M50/262 , H01M50/507 , H01M50/296 , H01M50/271 , B64U50/30
CPC分类号: H01M50/242 , H01M50/298 , H01M50/249 , H01M50/262 , H01M50/507 , H01M50/296 , H01M50/271 , B64U50/30 , H01M2220/20
摘要: A method for manufacturing a battery module, including: disposing an adapting plate on a battery cell assembly, and connecting the adapting plate to tabs of the battery cell assembly; providing a fastening frame, where the fastening frame is provided with an accommodating cavity, and the accommodating cavity accommodates the adapting plate and at least part of the battery cell assembly; and providing a filler in a gap between the inner side of the accommodating cavity and the battery cell assembly and a gap between the inner side of the accommodating cavity and the adapting plate.
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公开(公告)号:US20230322424A1
公开(公告)日:2023-10-12
申请号:US18297129
申请日:2023-04-07
发明人: Haruhisa KAMIYA , Toshio IWAHARA
CPC分类号: B64U40/20 , B64U20/70 , B64U50/30 , B64U2101/66
摘要: Provided is an apparatus or a method that can stabilize flight of an unmanned aerial vehicle after package receiving or package passing. A port as a package receiving or passing apparatus includes: a landing portion on which an aerial vehicle lands; a slider for horizontally moving the landed aerial vehicle to an indoor area; an elevating/lowering portion on which a package-chamber tray taken down from the aerial vehicle in the indoor area is to be placed; a movement control portion for elevating/lowering an elevating/lowering portion; a package moving portion for moving a package between a package storage portion and the package-chamber tray placed on the elevating/lowering portion; and a center of gravity adjustment portion for adjusting the center of gravity position of the aerial vehicle after package receiving or package passing.
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公开(公告)号:US20240350879A1
公开(公告)日:2024-10-24
申请号:US18136691
申请日:2023-04-19
申请人: Matthew Zdunich
发明人: Matthew Zdunich
IPC分类号: A63B55/60 , A63B24/00 , A63B71/06 , B62B3/10 , B62B5/00 , B64U10/14 , B64U50/20 , B64U50/30 , G05D1/02 , G05D1/10 , G06T7/70 , G06V20/17 , G06V20/40 , G06V40/20 , G10L15/22 , H04N5/91 , H04N23/57 , H04R1/02
CPC分类号: A63B55/61 , A63B24/0006 , A63B24/0021 , A63B71/0622 , B62B3/102 , B62B5/00 , B62B5/004 , B62B5/0043 , B62B5/0069 , B64U10/14 , B64U50/20 , B64U50/30 , G06T7/70 , G06V20/17 , G06V20/42 , G06V40/23 , G10L15/22 , H04N5/91 , H04N23/57 , H04R1/028 , A63B2024/0028 , A63B2071/0625 , A63B2220/05 , A63B2220/806 , A63B2225/50 , B62B2202/406 , B64U2101/30 , G06T2207/10016 , G06T2207/10032 , G06T2207/30224 , G10L2015/223
摘要: A golf caddy system for autonomously carrying a golf bag across a golf course, recording video of golf swings, and providing golfing advice to a user includes an autonomous motorized cart. The cart includes a processor with map data of the golf course in a memory of the processor and a global positioning system receiver for determining a current location of the cart. The cart also includes a camera which is configured to capture video of a golf swing.
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公开(公告)号:US20240327044A1
公开(公告)日:2024-10-03
申请号:US18620932
申请日:2024-03-28
发明人: Dmytro Silin , Albert Pegg , Martin Fleury
摘要: Systems and methods directed to suspended propulsion systems for an unmanned aerial vehicle (UAV) are provided. A system may include a UAV having a body and a center of gravity (CG), and a suspended propulsion system coupled to the UAV. The suspended propulsion system may include a power source for the UAV, and a harness coupled to the UAV to suspend at least a portion of the power source under the CG of the UAV. The harness may be a rigid or flexible harness configured to decouple an inertia of the suspended propulsion system from an inertia of the UAV. Additional systems and related methods are also provided.
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8.
公开(公告)号:US11970294B2
公开(公告)日:2024-04-30
申请号:US17824382
申请日:2022-05-25
申请人: BETA AIR, LLC
发明人: Steven J. Foland , Thomas Henck , Herman Wiegman
摘要: An apparatus for determining a resource remaining datum of an electric aircraft is disclosed. The apparatus includes a processor and a memory communicatively connected to the processor. The memory contains instructions configuring the processor to receive aircraft data from at least a sensing device, wherein the at least a sensing device is configured to measure at least a parameter of a battery pack of the electric aircraft and generate aircraft data as a function of the at least a parameter of the battery pack of the electric aircraft. The memory contains instructions configuring the processor to determine a reserve energy as a function of a flight mode of the electric aircraft and determine a resource remaining datum as a function of the aircraft data and the reserve energy, wherein the resource remaining datum is related to the battery pack of the electric aircraft.
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公开(公告)号:US20230373668A1
公开(公告)日:2023-11-23
申请号:US18318434
申请日:2023-05-16
申请人: Skydio, Inc.
发明人: Yevgeniy Kozlenko , Benjamin Scott Thompson , Jack Zi Qi Ye , Christopher Brian Grasberger , Gareth Benoit Cross , Jack Louis Zhu , Abraham Galton Bachrach , Adam Parker Bry , Hayk Martirosyan
摘要: A battery configured to power an unmanned aerial vehicle. The battery includes an enclosure configured to house a power module of the battery. The battery also includes one or more conducting contacts located on the enclosure configured to contact one or more pogo pins of a battery charger located on a docking station of the unmanned aerial vehicle.
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公开(公告)号:US20230170702A1
公开(公告)日:2023-06-01
申请号:US17916039
申请日:2021-03-17
IPC分类号: H02J3/32 , H02J3/38 , H02J3/00 , B64C39/02 , B64D9/00 , B64U50/30 , B64U20/87 , B60L50/00 , B60L3/00 , G05D1/10
CPC分类号: H02J3/322 , H02J3/381 , H02J3/004 , H02J3/003 , B64C39/024 , B64D9/00 , B64U50/30 , B64U20/87 , B60L50/00 , B60L3/0023 , G05D1/101 , B64U2101/60
摘要: An energy supply system, which is a system constituting a regional power system in a target region, includes a power transmission system including a first power generation facility and a second power generation facility, a power transmission and distribution system that supplies power to each consumer, a management system, and an unmanned flying object. The unmanned flying object has a transport function of transporting a cargo and a power supply function of supplying power to an outside. When the amount of power supplied by the power transmission system is less than the amount of power required by the power transmission and distribution system, the management system performs a power adjustment process of supplying power from the unmanned flying object to the power transmission and distribution system by using the power supply function of the unmanned flying object.
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