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公开(公告)号：US20240346939A1
公开(公告)日：2024-10-17
申请号：US18645983
申请日：2024-04-25
申请人： Joby Aero, Inc.
CPC分类号： G08G5/0043 , B64C29/00 , G06N20/00 , G08G5/02
摘要： A vertiport system dynamically updates configuration of a vertiport based on predicted usage of the vertiport during a given time frame. The vertiport system predicts vertiport usage using flight data and estimated passenger demands and determines a desired number of parking pads and a desired number of final approach and takeoff (FATO) pads for the vertiport during the time frame. Based on the desired number of parking pads and the desired number of FATO pads for the vertiport, the vertiport system determines an updated configuration of the vertiport. According to the updated configuration, the vertiport system updates the configuration of the vertiport for at least a portion of the time frame.
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2.发明公开公开(公告)号：US20240321120A1
公开(公告)日：2024-09-26
申请号：US18405250
申请日：2024-01-05
申请人： Joby Aero, Inc.
IPC分类号： G08G5/00 , B64C17/08 , B64C29/00 , G05D1/652 , G05D1/695 , G06Q10/0631 , G06Q50/40 , G08G5/02
CPC分类号： G08G5/0043 , B64C17/08 , B64C29/00 , G05D1/652 , G05D1/695 , G06Q10/06315 , G06Q50/40 , G08G5/0013 , G08G5/0065 , G08G5/025
摘要： A request for transport services that identifies a rider, an origin, and a destination is received from a client device. Eligibility of the request to be serviced by a vertical take-off and landing (VTOL) aircraft is determined based on the origin and the destination. The client device is sent an itinerary for servicing the transport request including a leg serviced by the VTOL aircraft. Confirmation is received that the rider has boarded the VTOL aircraft and determination made as to whether the VTOL aircraft should wait for additional riders. Instruction are sent to the VTOL aircraft to take-off if one or more conditions are met.
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公开(公告)号：US12084177B2
公开(公告)日：2024-09-10
申请号：US17744040
申请日：2022-05-13
申请人： Santh Sathya
发明人： Santh Sathya
CPC分类号： B64C37/00 , B60F5/02 , B64C29/00 , G05D1/0088
摘要： An air and road vehicle system includes a road vehicle having a chassis, a plurality of wheels, an engine, and a cabin area. A flight vehicle having a main body, wings, flight control surfaces, and a plurality of propulsion devices is removably coupled to the road vehicle by a plurality of docking mechanisms. In the connected orientation, the top end of the road vehicle is connected to the bottom surface of the wings, and the back end of the road vehicle is connected to the main body via an elongated catch tongue. Controllers on the flight vehicle and road vehicle are communicatively linked wirelessly or via hardwire receptacles. In the disconnected orientation, the road vehicle is functional as a road motor vehicle, and in the connected orientation, the flight vehicle and the road vehicle are functional for flight in a vertical or horizontal orientation.
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公开(公告)号：US20240286759A1
公开(公告)日：2024-08-29
申请号：US18174821
申请日：2023-02-27
发明人： Gang He
摘要： Systems and methods are provided for displaying horizontal situational indicator (HSI) for a vertical takeoff and landing (VTOL) aircraft. The system includes an aircraft control panel in a cockpit of the VTOL aircraft and a HSI digital display that is located on the aircraft control panel. The HSI digital display shows a fixed target symbol representing an intended landing point, a speed vector indicator that represents an approach direction and a predicted hover point relative to the fixed target symbol that is calculated based on the speed, acceleration and turn rate of the VTOL aircraft, and a dynamic target symbol representing a positional change in the predicted hover point in response to instantaneous dynamic changes in flight conditions for the VTOL aircraft.
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公开(公告)号：US20240253775A1
公开(公告)日：2024-08-01
申请号：US18426956
申请日：2024-01-30
发明人： Paul C. Collado , Tatiana Arends , Sean Michael Killingsworth , Justin Birkey , Steven G. Hagerott
摘要： A landing gear system for an aerial device includes a mounting structure and a main landing gear. The mounting structure is configured to be attached relative to a fuselage of the aerial device. The main landing gear includes a pair of aft swept struts and wheels mounted on each of the aft swept struts. The pair of aft swept struts is attached relative to the mounting structure and extends downwardly and rearwardly relative thereto.
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公开(公告)号：US20240250585A1
公开(公告)日：2024-07-25
申请号：US18292434
申请日：2022-07-15
摘要： Aircraft electric propulsion system including: a motor including a hollow rotor, and a power and control electronics device, in which the power and control electronics device includes at least two ring-shaped electrical tracks each including at least two inverters, the inverters being connected to each other in parallel, wherein the electrical tracks delimit a hollow circular part of the power and control electronics device, the hollow circular part being placed in the axis of the hollow rotor of the motor.
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公开(公告)号：US11990647B2
公开(公告)日：2024-05-21
申请号：US18206610
申请日：2023-06-06
发明人： Michael Raymond Hull , Steven Loveland , Yue Fan
IPC分类号： H02P1/00 , B60L50/64 , B60L58/10 , B64C29/00 , B64D27/24 , H01M10/42 , H01M50/209 , H01M50/249 , H01M50/512
CPC分类号： H01M50/512 , B60L50/64 , B60L58/10 , B64C29/00 , B64D27/24 , H01M10/4207 , H01M10/425 , H01M50/209 , H01M50/249 , B60L2200/10 , B64D2221/00 , H01M2010/4271 , H01M2220/20
摘要： A modular battery system includes an array of battery modules arranged in at least one stack. Each battery module includes a plurality of battery cells, a first side having positive and negative receptacles and a second side, that is opposite of the first side, having positive and negative plugs. The receptacles and plugs are configured such that adjacent battery modules in a side-by-side relationship are electrically coupled together via plug and receptacle connections and such that the battery modules are electrically coupled together in parallel. An interconnection electrically couples each stack of battery modules together via plug and receptacle connections with one of the battery modules in each stack such that the stacks of battery modules are electrically coupled together in parallel. Each of the battery modules includes a thermal conditioning system configured to thermally isolate the battery module from the other battery modules.
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公开(公告)号：US11990050B2
公开(公告)日：2024-05-21
申请号：US18321289
申请日：2023-05-22
申请人： Joby Aero, Inc.
CPC分类号： G08G5/0043 , B64C29/00 , G06N20/00 , G08G5/02
摘要： A vertiport system dynamically updates configuration of a vertiport based on predicted usage of the vertiport during a given time frame. The vertiport system predicts vertiport usage using flight data and estimated passenger demands and determines a desired number of parking pads and a desired number of final approach and takeoff (FATO) pads for the vertiport during the time frame. Based on the desired number of parking pads and the desired number of FATO pads for the vertiport, the vertiport system determines an updated configuration of the vertiport. According to the updated configuration, the vertiport system updates the configuration of the vertiport for at least a portion of the time frame.
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公开(公告)号：US11941925B2
公开(公告)日：2024-03-26
申请号：US17852783
申请日：2022-06-29
申请人： BETA AIR, LLC
CPC分类号： G07C5/0825 , B64D45/00 , B64D47/00 , G06N20/00 , B64C29/00 , B64D2045/0085
摘要： An aircraft monitoring system for an electric aircraft is disclosed. The monitoring system may include at least a sensor configured to generate a failure datum. The failure datum includes a datum regarding a condition of an electric motors. An electronic checklist may include a crew alerting system (CAS). A CAS may be in electronic communication a sensor, wherein the CAS is comprised of at least a computing device. A CAS may generate a plurality of remedy data as a function of the failure datum. A CAS then may display the plurality of remedy data using a pilot display. A pilot may be prompted to apply the remedy datum using a pilot display as a function of the plurality of remedy data. The CAS provides an indication of the condition of the electric motor using a pilot display as a function of the application of the plurality of remedy data.
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10.发明公开公开(公告)号：US20240094729A1
公开(公告)日：2024-03-21
申请号：US18516038
申请日：2023-11-21
申请人： AeroVironment, Inc.
发明人： Quentin Lindsey , Henry Thome Won
CPC分类号： G05D1/0202 , B64C29/00 , B64C39/024 , B64D47/08 , G08G5/0034 , B64U2101/30 , G08G5/003
摘要： Systems, devices, and methods for receiving, by a processor having addressable memory, data representing a geographical area for imaging by one or more sensors of an aerial vehicle; determining one or more straight-line segments covering the geographical area; determining one or more waypoints located at an end of each determined straight-line segment, where each waypoint comprises a geographical location, an altitude, and a direction of travel; determining one or more turnarounds connecting each of the straight-line segments, where each turnaround comprises one or more connecting segments; and generating, by the processor, a flight plan for the aerial vehicle comprising: the determined one or more straight-line segments and the determined one or more turnarounds connecting each straight-line segment.
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