NOISE REDUCTION SYSTEM FOR AIR MOBILITY

    公开(公告)号:US20220194566A1

    公开(公告)日:2022-06-23

    申请号:US17378444

    申请日:2021-07-16

    Abstract: A noise reduction system for air mobility, may include a plurality of propeller modules provided on the air mobility and each including an inverter, a motor electrically connected to the inverter, and a propeller mounted to the motor; and a control unit configured to perform PWM control of power to be provided to the inverters to reduce noise attributable to carrier frequencies generated by the plurality of inverters or reduce noise attributable to fundamental frequencies generated by the plurality of motors.

    Magnetic gear
    7.
    发明授权

    公开(公告)号:US11705769B2

    公开(公告)日:2023-07-18

    申请号:US17382929

    申请日:2021-07-22

    CPC classification number: H02K3/12 H02K1/16 H02K3/48 H02K7/003

    Abstract: A magnetic gear may include a stator, having a stator core having a plurality of teeth extending toward a rotation shaft and a plurality of coils wound around the plurality of teeth, a rotor, having a rotor core disposed inside the stator and fixed to the rotation shaft and a plurality of permanent magnets attached to the external surface of the rotor core, and a pole-piece unit, having a plurality of first pole pieces and a plurality of second pole pieces arranged radially about the rotation shaft between the stator core and the rotor core such that the plurality of first pole pieces and the plurality of second pole pieces are alternately arranged in a circumferential direction thereof.

    Apparatus for generating thrust for air transport

    公开(公告)号:US11591082B2

    公开(公告)日:2023-02-28

    申请号:US17307721

    申请日:2021-05-04

    Abstract: An apparatus for generating thrust for air transport includes a main thrust device, and an auxiliary thrust device configured to generate auxiliary thrust so as to enable an aircraft to vertically take off and land. The apparatus further includes: wings fixed to left and right sides of a fuselage of the aircraft, rotors installed on the wings and configured to generate thrust. In particular, the main thrust device provides driving force to the rotors using motors and an engine, and the auxiliary thrust device is installed in the fuselage and has a center of gravity configured to coincide with a center of gravity of the aircraft.

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