Air mobility
    1.
    发明授权

    公开(公告)号:US11905011B2

    公开(公告)日:2024-02-20

    申请号:US17378693

    申请日:2021-07-17

    摘要: An air mobility may include a wing portion extending from a fuselage of the air mobility; a folded portion provided at an edge portion of the wing portion, configured to extend from the wing portion to form a part of the wing portion during unfolding of the folded portion, and configured to move to overlap with the wing portion during folding of the folded portion, so that an area of air resistance in a vertical direction of the wing portion is reduced; an actuator connected to the folded portion and configured to provide power to the folded portion, so that the folded portion is unfolded or folded to the wing portion; and a controller connected to the actuator and configured to control the actuator, so that the folded portion is folded during vertical takeoff or landing of the fuselage, and configured to control the actuator to unfold the folded portion during cruising of the fuselage.

    CONTROL APPARATUS AND METHOD OF HYBRID VEHICLE

    公开(公告)号:US20220363237A1

    公开(公告)日:2022-11-17

    申请号:US17473991

    申请日:2021-09-13

    摘要: A control apparatus of a hybrid vehicle includes an input and output module for a driver to select a driving mode, an engine that generates power required for vehicle driving by fuel combustion, a driving motor that generates power required for vehicle driving and operates as a generator, a hybrid starter-generator (HSG) that starts the engine and operates as a generator, and a controller. When the driving mode is inputted to a stopping mode through the input and output module, based on an expected stop time, a current SOC of a battery, a target SOC of the battery, output of the driving motor, and output of the HSG, the controller that performs a first charging mode that charges the power generated by the engine in the battery through the driving motor and a second charging mode that charges the power generated by the engine in the battery through the driving motor and the HSG.

    Propeller apparatus of air mobility

    公开(公告)号:US11845535B2

    公开(公告)日:2023-12-19

    申请号:US17459772

    申请日:2021-08-27

    IPC分类号: B64C11/28

    CPC分类号: B64C11/28

    摘要: A propeller apparatus of an air mobility may include blades configured for being folded or unfolded in a response to flight situation of the air mobility, so that energy efficiency of the air mobility is improved and flight distance is increased by efficient use of the plurality of blades in each flight situation. Furthermore, as a pitching motion of the plurality of blades is performed in addition to a folding or unfolding motion of the plurality of blades, flight performance is improved.

    Tilting system for propeller of aerial vehicle

    公开(公告)号:US11608164B2

    公开(公告)日:2023-03-21

    申请号:US17411962

    申请日:2021-08-25

    IPC分类号: B64C27/52

    摘要: A tilting system for a propeller of an aerial vehicle, may include a propeller provided in front of the opening portion of the housing and configured to be selectively tilted with respect to the housing; a link assembly provided in the internal space of the housing, a first end portion of which is connected to the housing and a second end portion of which is connected to the propeller, and configured to tilt up or tilt down the propeller as the link assembly is extended from the housing or retracted into the housing; and an actuator coupled to the link assembly and configured to provide power for extension or retraction to the link assembly.

    ROTOR-COOLING STRUCTURE OF A DRIVE MOTOR

    公开(公告)号:US20220294295A1

    公开(公告)日:2022-09-15

    申请号:US17516388

    申请日:2021-11-01

    IPC分类号: H02K1/32 H02K5/20 H02K9/19

    摘要: A rotor-cooling structure is for a drive motor including an inner shaft, a rotor shaft surrounding the inner shaft, a rotor connected to the rotor shaft, and a stator disposed to be spaced apart from the rotor. The rotor-cooling structure includes: a first flow passage formed in the inner shaft; a second flow passage formed in the rotor shaft to receive oil through the first flow passage; a third flow passage formed in a plate disposed at an end of a rotor core, constituting the rotor, to be connected to the second flow passage; and a fourth flow passage formed to be connected to the third flow passage and to penetrate the rotor core in the direction in which core plates constituting the rotor core are stacked.

    LIGHTING SYSTEM FOR AIR MOBILITY
    10.
    发明申请

    公开(公告)号:US20220185500A1

    公开(公告)日:2022-06-16

    申请号:US17379828

    申请日:2021-07-19

    IPC分类号: B64D47/06 F21S43/19

    摘要: A lighting system for air mobility may include a light emitting unit provided on a boom or a propeller of the air mobility and configured to emit light toward a ground surface so that the light is projected onto a point directed toward the ground surface from the propeller or the boom; and a control unit electrically connected to the light emitting unit and configured to control light emitting modes of the light, emitted by the light emitting unit, based on operating modes of the air mobility or operating modes of the propeller.