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    SYSTEMS AND METHODS FOR SCALING LAG BASED ON FLIGHT PHASE OF AN ELECTRIC AIRCRAFT
    3.
    发明公开
    SYSTEMS AND METHODS FOR SCALING LAG BASED ON FLIGHT PHASE OF AN ELECTRIC AIRCRAFT 审中-公开

    公开(公告)号：US20230205232A1

    公开(公告)日：2023-06-29

    申请号：US17880172

    申请日：2022-08-03

    申请人： BETA AIR, LLC

    发明人： Alexander Hoekje List ,  Vincent Moeykens

    IPC分类号： G05D1/10 ,  B64D27/24 ,  B64C29/00

    CPC分类号： G05D1/102 ,  B64D27/24 ,  B64C29/00

    摘要： A system for scaling lag based on flight phase of an electric aircraft is presented. The system include a sensor connected to an electric aircraft configured to detect measured aircraft data, identify a flight phase of the electric aircraft, and generate a flight datum. The system further comprises a computing device communicatively connected to the sensor, wherein the computing device is configured to receive the flight datum and the flight phase, identify an input latency as a function of the flight datum, select a lag frame as a function of the input latency, wherein the lag frame further comprises a lag threshold, and transmit the flight datum to a user device as a function of the lag frame. The system further includes a remotely located user device configured to receive the flight datum.

    IN-FLIGHT STABILIZATION OF AN AIRCRAFT
    5.
    发明申请
    IN-FLIGHT STABILIZATION OF AN AIRCRAFT 有权

    公开(公告)号：US20210371123A1

    公开(公告)日：2021-12-02

    申请号：US17113647

    申请日：2020-12-07

    申请人： BETA AIR, LLC

    发明人： Alexander Hoekje List ,  Lochie Ferrier

    IPC分类号： B64D45/00 ,  G05D1/08 ,  B64C39/02

    摘要： A system for in-flight stabilization including a plurality of flight components mechanically coupled to an aircraft, wherein the plurality of flight components includes a first flight component and a second flight component opposing the first flight component. The system further comprises a sensor mechanically coupled to the aircraft, wherein the sensor is configured to detect a failure event of a first flight component. The system comprises a vehicle controller communicatively connected to the sensor and is configured to receive the failure datum of the first flight component from the sensor, initiate an automatic response as a function of the failure datum. Initiating the automatic response further includes determining an autorotation inducement action for the second flight component to perform and commanding the second flight component to perform the autorotation inducement action.

    AIRCRAFT FOR SELF-NEUTRALIZING FLIGHT
    9.
    发明申请
    AIRCRAFT FOR SELF-NEUTRALIZING FLIGHT 有权

    公开(公告)号：US20220315236A1

    公开(公告)日：2022-10-06

    申请号：US17222539

    申请日：2021-04-05

    申请人： BETA AIR, LLC

    发明人： Alexander Hoekje List ,  David L. Churchill

    IPC分类号： B64D31/10 ,  B64D31/12

    摘要： An aircraft for self-neutralizing flight comprising a fuselage, at least a power source, a plurality of laterally extending elements attached to the fuselage, a plurality of downward directed propulsors attached to the plurality of laterally extending elements and electrically connected to at least a power source, wherein the plurality of downward directed propulsors have a rotational axis offset from a vertical axis by a yaw-torque-cancellation angle.

    AIRCRAFT FOR NEUTRALIZING VERTICAL FLIGHT
    10.
    发明申请
    AIRCRAFT FOR NEUTRALIZING VERTICAL FLIGHT 有权

    公开(公告)号：US20220315207A1

    公开(公告)日：2022-10-06

    申请号：US17349269

    申请日：2021-06-16

    申请人： BETA AIR, LLC

    发明人： Alexander Hoekje List ,  David L. Churchill

    IPC分类号： B64C15/02 ,  B64C29/00 ,  B64D27/24

    摘要： An aircraft for neutralizing flight comprising a fuselage, at least a power source, a plurality of laterally extending elements attached to the fuselage, a plurality of downward directed propulsors attached to the plurality of laterally extending elements and electrically connected to at least a power source, wherein the plurality of downward directed propulsors have a rotational axis offset from a vertical axis by a yaw-torque-cancellation angle, and a flight controller configured to include a notification unit.