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公开(公告)号：US12110092B2
公开(公告)日：2024-10-08
申请号：US18310971
申请日：2023-05-02
申请人： Duplicent, LLC
发明人： Curren Krasnoff
IPC分类号： B64C27/52 , B64C29/00 , B64C37/00 , B64U30/16 , B64U30/26 , B64U50/19 , B64U50/31 , B64D27/353 , B64U10/13
CPC分类号： B64C27/52 , B64C29/0033 , B64C37/00 , B64U30/16 , B64U30/26 , B64U50/31 , B64D27/353 , B64U10/13 , B64U50/19
摘要： An aircraft includes a body defining an interior compartment configured to hold at least one of a passenger and a payload, a battery system, a plurality of arms coupled to and extending from the body, and a plurality of propulsion devices configured to provide thrust to fly the aircraft. Each of the plurality of propulsion devices is coupled to a respective one of the plurality of arms. The plurality of propulsion devices are powered by the battery system. Each of the plurality of propulsion devices is selectively pivotable about at least one axis. The plurality of propulsion devices include at least one of (i) counter rotating ducted fans and (ii) ionizing electrode engines.
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公开(公告)号：US12017766B2
公开(公告)日：2024-06-25
申请号：US17829822
申请日：2022-06-01
申请人： Jimmy Sherwood Myer
发明人： Jimmy Sherwood Myer
CPC分类号： B64C37/00 , B60F5/02 , B64C29/0083
摘要： A flying car that does not require complex transformation between a car and an aircraft, the flying car can quickly take off from a land, such as road or parking, and can land on the road or parking. The flying car is of triangular shape having a broad front and narrow rear. Three motorized members are coupled to three corners of a frame of the flying car. Each of the three motorized members includes a wheel assembly that includes a wheel and a wheel frame, an inner ring and an outer ring coupled to each other, and both mounted to the wheel frame. A fan mounted on the inner ring and one or more turbines mounted on the outer ring.
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公开(公告)号：US20230186779A1
公开(公告)日：2023-06-15
申请号：US17548911
申请日：2021-12-13
发明人： Joseph Soryal , Naila Jaoude , Christina Cacioppo
IPC分类号： G08G7/00 , G08G1/0965 , G08G1/0968 , G01C21/36 , B64C37/00 , B60F5/02
CPC分类号： G08G7/00 , G08G1/0965 , G08G1/096855 , G01C21/365 , B64C37/00 , B60F5/02 , G05D1/101
摘要： A processing system including at least one processor executing a traffic management application may detect a proximity to a traffic zone for vehicular traffic, the dual-mode vehicle having two modes of operation, the two modes of operation comprising a surface mode of operation and an aerial mode of operation, and may verify a rule set for vehicular operations within the traffic zone. The processing system may then identify a leader traffic management application from among a plurality of traffic management applications of a plurality of dual-mode vehicles within or near the traffic zone, obtain at least one navigation instruction from the leader traffic management application, and perform at least one of: executing a navigation action in accordance with the at least one navigation instruction, or displaying at least a portion of a permitted route that is in conformance with the at least one navigation instruction.
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公开(公告)号：US20230115625A1
公开(公告)日：2023-04-13
申请号：US17829822
申请日：2022-06-01
申请人： Jimmy Sherwood Myer
发明人： Jimmy Sherwood Myer
摘要： A flying car that does not require complex transformation between a car and an aircraft, the flying car can quickly take off from a land, such as road or parking, and can land on the road or parking. The flying car is of triangular shape having a broad front and narrow rear. Three motorized members are coupled to three corners of a frame of the flying car. Each of the three motorized members includes a wheel assembly that includes a wheel and a wheel frame, an inner ring and an outer ring coupled to each other, and both mounted to the wheel frame. A fan mounted on the inner ring and one or more turbines mounted on the outer ring.
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公开(公告)号：US11618548B2
公开(公告)日：2023-04-04
申请号：US17165186
申请日：2021-02-02
发明人： Umesh N. Gandhi , Ryohei Tsuruta
摘要： A reinforced, foldable component for an aircraft is provided, configured to stabilize a high frequency aeroelastic fluttering movement. The reinforced component may include a frame structure defining at least one air chamber, and a plurality of sealed compartments. A shear thickening fluid is disposed in at least one of the sealed compartments, exhibiting a decreasing viscosity responsive to an impact force. The frame structure may define one of an inflatable wing structure, a fairing structure, an aileron structure, and a stabilizer structure, and the like. The foldable component may include an exterior layer with an exterior surface exposed to an external environment and an interior layer adjacent the at least one air chamber, wherein the plurality of sealed compartments are disposed between the exterior layer and the interior layer. The exterior layer or the interior layer may include an impact-resistant fabric layer including a shear thickening material.
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公开(公告)号：US11603197B2
公开(公告)日：2023-03-14
申请号：US16331736
申请日：2017-09-11
发明人： Ron Bublitsky
摘要： A modular vehicle system includes at least one body module having at least one body connection interface, and a kit. The kit includes a plurality of utility modules including at least one first utility module (in the form of a fixed-wing utility module) and at least one second utility module (in the form of a rotor-wing utility module). Each first utility module includes at least one utility module connection interface in the form of a first utility module connection interface for coupling with the body connection interface. Each second utility module includes at least one utility module connection interface in the form of a second utility module connection interface, distinct from the first utility module connection interface, for coupling with the body connection interface. Each body connection interface is configured for selective reversible coupling at least with respect to any one of the utility module connection interfaces while concurrently excluding coupling of another utility module connection interface thereto, to provide an air vehicle.
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公开(公告)号：US20230058202A1
公开(公告)日：2023-02-23
申请号：US17445367
申请日：2021-08-18
发明人： Fadl Abdellatif , Jeff S. Shamma , Sultan Shaqaq , Abdullah Arab , Abdullah A. Alkhder , Sahejad Patel
IPC分类号： B64C39/02 , B64D27/24 , B64C37/00 , B60F5/02 , B64D31/00 , B64D35/02 , G05D1/10 , G05D1/00 , G01N29/04 , G01N29/265 , G01N29/22
摘要： An unmanned aerial vehicle (UAV) has a flight-only mode with a motor only rotating propellers and not rotating on-board wheels to configure the UAV to fly away from a surface of a structure, and a crawling-only mode in which the UAV is configured to crawl on the surface due to the motor only rotating the wheels while not rotating the propellers. In the flight-only mode, a clutch disengages a motor from the wheels so that the motor only engages the propellers to fly to lift from the surface. In the crawling-only mode, the clutch disengages the motor from the propellers so that the motor only engages the wheels to move the UAV on the surface.
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公开(公告)号：US20230034488A1
公开(公告)日：2023-02-02
申请号：US17744040
申请日：2022-05-13
申请人： Santh Sathya
发明人： Santh Sathya
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：US20230017708A1
公开(公告)日：2023-01-19
申请号：US17686864
申请日：2022-03-04
发明人： David Wayne Russell
摘要： Unmanned Aerial Vehicles also known as UAVs or Drones, either autonomous or remotely piloted, are classified as drones by the US Federal Aviation Administration (FAA) as weighing under 212 pounds. The system described herein details Autonomous Flight Vehicles (AFV) which weigh over 212 pounds but less than 1,320 pounds which may require either a new classification or a classification such as Sport Light Aircraft, but without the requirement of a pilot due to the safe autonomous flight system such as the Safe Temporal Vector Integration Engine or STeVIE. Safe Autonomous Light Aircraft (SALA) are useful as drone carriers, large scale air package or cargo transport, and even human transport depending on the total lift capability of the platform.
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公开(公告)号：US20230001756A1
公开(公告)日：2023-01-05
申请号：US17698183
申请日：2022-03-18
发明人： Jin Ho HWANG , Dong Eun Cha , Sang Heon Lee
摘要： A mobility vehicle hub configured to function as a terminal for an air mobility vehicle, a ground mobility vehicle, or a water mobility vehicle, includes a plurality of layers through a combination of: a water layer connected to the surface of water and having an entrance for a water mobility vehicle; a port layer having a take-off and landing pad for an air mobility vehicle; or a ground layer configured to be connected to a ground and having an entrance for a ground mobility vehicle, wherein an elevation passage is provided between the layers, the elevation passage has an internal space extending in an up-down direction of the mobility vehicle hub, the internal space is connected to each of the water, port and ground layers, and the air mobility vehicle, the ground mobility vehicle, or the water mobility vehicle is lifted or lowered through the internal space.
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