MODE ADJUSTMENT METHOD FOR DRONE BASE STATION, ADJUSTMENT APPARATUS, AND DRONE BASE STATION

    公开(公告)号:US20240268067A1

    公开(公告)日:2024-08-08

    申请号:US18431421

    申请日:2024-02-02

    Inventor: Dianlin FU

    CPC classification number: H05K7/20209 B64F1/362 H05K7/20145

    Abstract: This disclosure discloses a mode adjustment method for a drone base station. The mode adjustment method includes: acquiring a current temperature of an upper compartment; determining whether the current temperature is equal to or higher than a preset high temperature; when the current temperature is equal to or higher than the preset high temperature, controlling a temperature adjustment component to execute a refrigeration and heat dissipation mode; when the current temperature is lower than the preset high temperature, determining whether the current temperature is lower than or equal to a preset low temperature; when the current temperature is lower than or equal to the preset low temperature, controlling the temperature adjustment component to execute a heating and temperature maintaining mode; and when the current temperature is higher than the preset low temperature, controlling the temperature adjustment component to execute a standard operating mode.

    Camera with gimbal
    84.
    外观设计

    公开(公告)号:USD1034404S1

    公开(公告)日:2024-07-09

    申请号:US29849405

    申请日:2022-08-10

    Designer: Zhengli Zhang

    Abstract: FIG. 1 is a front, right and top perspective view of a camera with gimbal, showing my design.
    FIG. 2 is a rear, left and bottom perspective view thereof.
    FIG. 3 is a front, right and bottom perspective view thereof.
    FIG. 4 is a front elevation view thereof.
    FIG. 5 is a rear elevation view thereof.
    FIG. 6 is a left side elevation view thereof.
    FIG. 7 is a right side elevation view thereof.
    FIG. 8 is a top plan view thereof.
    FIG. 9 is a bottom plan view thereof.
    FIG. 10 is a partial enlarged view of an area labeled 10 in FIG. 1; and,
    FIG. 11 is a partial enlarged view of an area labeled 11 in FIG. 1.
    The broken lines shown in the drawings are included for the purpose of illustrating portions of the camera with gimbal that form no part of the claimed design.
    In addition, the dot-dash broken lines in FIGS. 1 and 10-11 are for the purpose of annotating the enlargements only and form no part of the claimed design.

    Aerial vehicle
    85.
    外观设计

    公开(公告)号:USD1034313S1

    公开(公告)日:2024-07-09

    申请号:US29886885

    申请日:2023-03-14

    Designer: Boming Lu

    Abstract: FIG. 1 is a front, right and top perspective view of an aerial vehicle, showing my design.
    FIG. 2 is a rear, left and bottom perspective view thereof.
    FIG. 3 is a front elevation view thereof.
    FIG. 4 is a rear elevation view thereof.
    FIG. 5 is a left side elevation view thereof.
    FIG. 6 is a right side elevation view thereof.
    FIG. 7 is a top plan view thereof.
    FIG. 8 is a bottom plan view thereof.
    FIG. 9 is an enlarged view of detail 9 in FIG. 1.
    FIG. 10 is an enlarged view of detail 10 in FIG. 1.
    FIG. 11 is an enlarged view of detail 11 in FIG. 2.
    FIG. 12 is an enlarged view of detail 12 in FIG. 2.
    FIG. 13 is another front, right and top perspective view of the aerial vehicle of FIG. 1 in another state.
    FIG. 14 is a rear, left and bottom perspective view of the aerial vehicle of FIG. 13.
    FIG. 15 is a front elevation view of the aerial vehicle of FIG. 13.
    FIG. 16 is a rear elevation view of the aerial vehicle of FIG. 13.
    FIG. 17 is a left side elevation view of the aerial vehicle of FIG. 13.
    FIG. 18 is a right side elevation view of the aerial vehicle of FIG. 13.
    FIG. 19 is a top plan elevation view of the aerial vehicle of FIG. 13.
    FIG. 20 is a bottom plan elevation view of the aerial vehicle of FIG. 13; and,
    FIG. 21 is an enlarged view of detail 21 in FIG. 13.
    The broken lines depict portions of the aerial vehicle that form no part of the claimed design. The dot-dash broken lines in FIGS. 1, 2, 9-13, and 21 depict the boundaries of the enlargements that form no part of the claimed design.

    Wing detachment assembly and aerial vehicle

    公开(公告)号:US12030613B2

    公开(公告)日:2024-07-09

    申请号:US17653522

    申请日:2022-03-04

    Inventor: Yuanyuan Du

    CPC classification number: B64C1/26 F16B39/28

    Abstract: Embodiments of the present invention discloses a wing detachment assembly and an aerial vehicle. The wing detachment assembly includes a first connecting portion and a second connecting portion, one of the first connecting portion and the second connecting portion being fixed on a wing and the other being fixed on a vehicle body. The second connecting portion includes a thumb wheel, the thumb wheel being provided with a threaded hole and being rotatably mounted on the vehicle body or the wing. The first connecting portion is threadedly connected to a threaded hole of the thumb wheel, the first connecting portion and the thumb wheel being fastened or detached when the thumb wheel is rotated. The aerial vehicle includes the foregoing wing detachment assembly. The wing detachment assembly and the aerial vehicle have the advantage of being convenient to detach and mount the wing.

    HEAT DISSIPATION STRUCTURE AND UNMANNED AERIAL VEHICLE

    公开(公告)号:US20240196558A1

    公开(公告)日:2024-06-13

    申请号:US18527516

    申请日:2023-12-04

    Inventor: Xiaode LI

    CPC classification number: H05K7/20163 B64U20/98 H05K7/20336

    Abstract: Embodiments of the present disclosure relate to the field of unmanned aerial vehicle technologies, and disclose a heat dissipation structure and an unmanned aerial vehicle including same. The heat dissipation structure includes: a first structure body, where a heat dissipation channel is provided in the first structure body for a cooling medium to flow through; and a second structure body, where the second structure body is arranged in the heat dissipation channel, and configured to divide the heat dissipation channel to form at least two channel branches, where a sealed cavity configured to accommodate a heating device is provided in the second structure body. Through a design of heat dissipation channel branches arranged in a cascading manner, a required sealed space can be formed conveniently between channel branches, providing sufficient sealing to satisfy requirements of components for waterproofing/dustproofing.

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