Magnetic spring inceptor
    21.
    发明授权

    公开(公告)号:US10761557B2

    公开(公告)日:2020-09-01

    申请号:US15863592

    申请日:2018-01-05

    Applicant: Wisk Aero LLC

    Abstract: A magnetic spring input device is disclosed. In various embodiments, an input device as disclosed includes a manual input structure movably coupled to a base assembly; and a non-stationary magnet fixedly coupled to the manual input structure; a stationary magnet coupled to the base assembly in a manner that is fixed with respect to at least a first input axis of the input device, the stationary magnet being coupled to the base assembly with a first magnetic pole having a first magnetic polarity is oriented opposite a corresponding magnetic pole of the non-stationary magnet having the first magnetic polarity, in a position that is adjacent to but offset from the non-stationary magnet when the manual input structure is in a neutral position. The non-stationary magnet is coupled to the manual input structure in a position such that movement of the manual input structure about or along the first input axis of the input device brings said poles have said first magnetic polarity within sufficient proximity to generate a repulsive magnetic force.

    COMPACT VERTIPORT WITH EFFICIENT SPACE UTILIZATION

    公开(公告)号:US20250051034A1

    公开(公告)日:2025-02-13

    申请号:US18930966

    申请日:2024-10-29

    Applicant: Wisk Aero LLC

    Abstract: Embodiments provide a compact vertiport system. The vertiport system may be efficient and compact by combining, into one space and time period, multiple activities that typically take place in different spaces and different times. For example, when an aircraft is being moved from a landing zone to a takeoff zone, the aircraft may also be charged simultaneously. Also, passenger exchange may take place while the aircraft is being moved. As a result, compact vertiport systems may fit into smaller spaces (e.g., tops of buildings, or smaller plots of land).

    COMPACT VERTIPORT WITH EFFICIENT SPACE UTILIZATION

    公开(公告)号:US20250051033A1

    公开(公告)日:2025-02-13

    申请号:US18930963

    申请日:2024-10-29

    Applicant: Wisk Aero LLC

    Abstract: Embodiments provide a compact vertiport system. The vertiport system may be efficient and compact by combining, into one space and time period, multiple activities that typically take place in different spaces and different times. For example, when an aircraft is being moved from a landing zone to a takeoff zone, the aircraft may also be charged simultaneously. Also, passenger exchange may take place while the aircraft is being moved. As a result, compact vertiport systems may fit into smaller spaces (e.g., tops of buildings, or smaller plots of land).

    Compact vertiport with efficient space utilization

    公开(公告)号:US12162625B2

    公开(公告)日:2024-12-10

    申请号:US17520006

    申请日:2021-11-05

    Applicant: Wisk Aero LLC

    Abstract: Embodiments provide a compact vertiport system. The vertiport system may be efficient and compact by combining, into one space and time period, multiple activities that typically take place in different spaces and different times. For example, when an aircraft is being moved from a landing zone to a takeoff zone, the aircraft may also be charged simultaneously. Also, passenger exchange may take place while the aircraft is being moved. As a result, compact vertiport systems may fit into smaller spaces (e.g., tops of buildings, or smaller plots of land).

    Aircraft with pusher propeller
    27.
    发明授权

    公开(公告)号:US11975830B2

    公开(公告)日:2024-05-07

    申请号:US17173133

    申请日:2021-02-10

    Applicant: Wisk Aero LLC

    Abstract: Embodiments provide an electric aircraft with a plurality of lift fan assemblies that are configured to provide vertical lift, and one or more pusher propellers that are configured to provide forward thrust. The lift fan assemblies may be coupled to the wings of the aircraft via one or more support structures, and the wings may be coupled to an upper region of the fuselage. The pusher propeller(s) may be coupled to a tailing end of the fuselage. The lift fan assemblies and the pusher propeller(s) may provide thrust and movement in directions that are orthogonal to one another. A control system coupled to the aircraft may control the lift fan assemblies and the one or more pusher propellers to activate, increase in power, and decrease in power. The lift fan assemblies and the one or more pusher propellers may be operated separately, and may be active at different times.

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