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    Systems and methods for automated fleet management for aerial vehicles
    4.
    发明授权
    Systems and methods for automated fleet management for aerial vehicles 有权

    公开(公告)号：US11804138B2

    公开(公告)日：2023-10-31

    申请号：US17528597

    申请日：2021-11-17

    申请人： BETA AIR, LLC

    发明人： Steven J. Foland ,  Lochie Ferrier ,  Nick Warren ,  John Palombini

    IPC分类号： G08G5/00 ,  B64C29/00

    CPC分类号： G08G5/0008 ,  B64C29/00 ,  G08G5/0039

    摘要： In an aspect of the present disclosure is a system of automated fleet management for aerial vehicles, including a first aerial vehicle, the aerial vehicle comprising: a first sensor configured to measure an external metric and generate external datum based on the external metric; and a second sensor configured to measure an aircraft metric and generate aircraft datum based on the aircraft metric; and a computing device operating on the first aerial vehicle, the computing device communicatively connected to a network including at least a second aerial vehicle, the computing device configured to: receive the external datum from the first sensor of the first aerial vehicle and the aircraft datum from the second sensor of the first aerial vehicle; and transmit at least a flight plan update element to the network based on the external datum and the aircraft datum.

    Methods and systems for orienting a thrust propulsor in response to a failure event of a vertical take-off and landing aircraft
    8.
    发明授权
    Methods and systems for orienting a thrust propulsor in response to a failure event of a vertical take-off and landing aircraft 有权

    公开(公告)号：US11584534B2

    公开(公告)日：2023-02-21

    申请号：US17673031

    申请日：2022-02-16

    申请人： BETA AIR, LLC

    发明人： Nicholas Moy ,  Riley Griffin ,  Lochie Ferrier ,  Collin Freiheit

    IPC分类号： B64D31/10 ,  B64C29/00 ,  B64C11/00

    摘要： Aspects relate to systems and methods for orienting a thrust propulsor in response to a failure event of a vertical take-off and landing (VTOL) aircraft. An exemplary system includes a plurality of lift propulsors mechanically connected to a VTOL aircraft, wherein each of the plurality of lift propulsors are configured to produce lift, a plurality of sensors, wherein at least a sensor is configured to detect a failure of at least a lift propulsor, and transmit a failure datum, a thrust propulsor mechanically attached to the VTOL aircraft with an orientable joint, wherein the thrust propulsor is configured to produce thrust and orient the thrust propulsor as a function of a thrust orientation datum, and a flight controller configured to receive the failure datum, generate a thrust orientation datum as a function of the failure datum, and transmit the thrust orientation datum to the orientable joint.