Modular Autonomous Air and Road Vehicle

    公开(公告)号:US20220402604A1

    公开(公告)日:2022-12-22

    申请号:US17354739

    申请日:2021-06-22

    申请人: Santh Sathya

    发明人: Santh Sathya

    IPC分类号: B64C37/00 B64C29/00 B60F5/02

    摘要: The modular autonomous air and road mobility (AARM) vehicle with Vertical Take-off and Landing (VTOL) capability provides combined air and road mobility solution.
    AARM is clean energy powered, modular vehicle, which can be undocked and redocked into road module and air module, providing uninterrupted autonomous mobility between air and road. In addition, the modular design enables: Easy navigation through highly populated areas without the need to accommodate fixed wing aircraft on urban roads. Reduced energy consumption and noise levels in urban roads by not having to carry the air propulsion system into urban areas. The road and air modules dock with each other through a sensor guided docking and load carrying mechanism (SGDMS), allowing connectivity, command and control. The vehicle can be scaled appropriately to serve: personal mobility, shared car, air taxis, regional air transport, cargo and shipping, defense missions, medical evacuations and air ambulances.

    WALKING VTOL DRONE AND RELATED SYSTEMS AND METHODS

    公开(公告)号:US20220339983A1

    公开(公告)日:2022-10-27

    申请号:US17728760

    申请日:2022-04-25

    申请人: Aigen, Inc.

    发明人: Richard Wurden

    摘要: Walking VTOL vehicles and related systems and methods are disclosed. A representative system can include one or more vertical thrust propulsion systems for providing vertical thrust for the vehicle, one or more horizontal thrust propulsion systems for providing horizontal thrust for the vehicle, and leg elements that are rotatable between a first configuration in which each leg element extends downwardly and a second configuration different from the first configuration. A representative method of operating a vehicle includes using vertical thrust to raise the vehicle upward, rotating a leg element forward, lowering the vehicle, and then rotating the leg element rearward to propel the vehicle forward.

    Transportation systems for hybrid vehicles

    公开(公告)号:US11434611B2

    公开(公告)日:2022-09-06

    申请号:US17534581

    申请日:2021-11-24

    申请人: Ahmad Abu Elreich

    发明人: Ahmad Abu Elreich

    摘要: A transportation system for hybrid vehicles. The transportation system may include pillars and a raised pathway. Further, the pillars configured to be vertically mounted on the ground. Further, a first pillar of the pillars may include a first lower portion and a first upper portion. Further, a second pillar of the pillars may include a second lower portion and a second upper portion. Further, the raised pathway supported by the pillars. Further, a raised pathway of the raised pathway may include a first end and a second end. Further, the first end may be supported by the first upper portion of the first pillar. Further, the second end may be supported by the second upper portion of the second pillar. Further, the raised pathway may include a raised transportation surface configured to facilitate transportation of a hybrid vehicle.

    MULTI-MODAL VEHICLE
    15.
    发明申请

    公开(公告)号:US20220242182A1

    公开(公告)日:2022-08-04

    申请号:US17612860

    申请日:2020-05-20

    摘要: The present invention relates to a multi-modal vehicle operable in a first mode as a fixed wing aircraft and reconfigurable to be operable in a second mode as a ground vehicle. The vehicle comprises first and second ends configured to operate in a first direction, with the first end leading the second end, in the first mode and in a second direction, with the second end leading the first end, in normal operation in the second mode.

    Aircraft having a folding system
    16.
    发明申请

    公开(公告)号:US20220227477A1

    公开(公告)日:2022-07-21

    申请号:US17614065

    申请日:2020-05-20

    申请人: Friedrich GRIMM

    发明人: Friedrich GRIMM

    IPC分类号: B64C3/56 B64C39/06 B60F5/02

    摘要: An aircraft has an empennage and a folding system. The folding system has aerofoils and node bodies which are connected to one another. The aerofoils have at least two nose-side aerofoils and at least two tail-side aerofoils, of which one of the nose-side aerofoils and one of the tail-side aerofoils are port-side aerofoils and one of the nose-side aerofoils and one of the tail-side aerofoils are starboard-side aerofoils. The node bodies have fuselage-side node bodies and outer node bodies. The nose-side aerofoils and tail-side aerofoils are each articulated at a first end to an associated fuselage-side node body, and the nose-side aerofoils and tail-side aerofoils are each articulated at a second end to an outer node body. The tail-side node bodies are displaceable at least partially along an associated translation axis. The folding system functions as the empennage during flight.

    Method for transformation of motor transportation vehicle for ground and air transport, motor transportation vehicle

    公开(公告)号:US11230363B2

    公开(公告)日:2022-01-25

    申请号:US16610047

    申请日:2018-05-10

    申请人: Stefan Klein

    发明人: Stefan Klein

    摘要: A system and method for transformation of motor transportation vehicle for ground and air transport, motor transportation vehicle are disclosed. The motor transportation vehicle consists of the body with the cabin, the front and rear axles, an actuation system, wings, covers, and tail including the support and the tail surfaces, and for transformation of the motor transportation vehicle for air transport to the motor transportation vehicle for ground transport the following transformation steps are preformed: minimization of the wings footprint area by turning the wings around their horizontal axes, which axes run through the halves or near the halves of the wing widths; opening two body covers; turning the folded wings into the vertical position; turning the folded wings from the vertical position towards rear position around the horizontal axis perpendicular to the length of the motor transportation vehicle, followed by closing the body covers; tilting the support cover/covers out; retracting the support/supports of the tail surfaces under the opened support covers; closing the support cover/covers.

    FOLDING BEAM FOR SWINGING WING
    20.
    发明申请

    公开(公告)号:US20210237849A1

    公开(公告)日:2021-08-05

    申请号:US17234251

    申请日:2021-04-19

    摘要: Some embodiments described herein relate to a wing that is coupled to a body of a vehicle and configured to rotate forward from a deployed configuration, in which the wing extends from the body to a retracted configuration in which a tip portion of the wing is closer to a nose portion of the body than a root portion of the wing is to the nose portion. A hinged beam having a first portion pivotably coupled to a second portion is configured to transmit loads associated with flight from the wing to the body.