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.

    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.

    LIGHTING SYSTEM FOR AIR MOBILITY
    4.
    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.

    AIR MOBILITY
    6.
    发明申请

    公开(公告)号:US20220194550A1

    公开(公告)日:2022-06-23

    申请号:US17378693

    申请日:2021-07-17

    IPC分类号: B64C3/54

    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.

    Retractable propeller apparatus of air mobility vehicle

    公开(公告)号:US11661174B2

    公开(公告)日:2023-05-30

    申请号:US17317143

    申请日:2021-05-11

    IPC分类号: B64C11/28

    CPC分类号: B64C11/28

    摘要: A retractable propeller apparatus of an air mobility vehicle has a structure enabling a propeller to be exposed or hidden depending on whether the air mobility vehicle is in a high-speed flight or a parking position. In particular, the retractable propeller apparatus includes: a base having a mount provided with a space; a propeller unit disposed on the mount and configured to generate a flow of air; a cover configured to close the space and be movable in the top-bottom direction with respect to the mount; and a lift unit disposed on the mount connected to the cover, and configured to move the cover. The cover selectively closes or opens the space based on an operation of the lift unit such that the propeller unit is operable.

    PROPELLER APPARATUS OF AIR MOBILITY

    公开(公告)号:US20220185450A1

    公开(公告)日:2022-06-16

    申请号:US17459772

    申请日:2021-08-27

    IPC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.