公开(公告)号：US20160122012A1

公开(公告)日：2016-05-05

申请号：US14805803

申请日：2015-07-22

Applicant: LG ELECTRONICS INC.

Inventor： ZHIMIN CHOO ,  Chulbae LEE

IPC: B64C27/50 ,  B64D47/08 ,  B64C27/10

CPC classification number: B64C39/028 ,  A63H27/12 ,  B64C27/50 ,  B64C29/0025 ,  B64C39/02 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127

Abstract: There is disclosed a drone including a main body comprising a motor, a shaft inserted in the main body vertically, a wing unit rotatable on the shaft by a power generated from the motor, the wing unit comprising a propeller unfolded horizontally and folded vertically, wherein the motor comprises a first motor and a second motor, and the shaft comprises an upper shaft inserted in the main body from a top vertically and a lower shaft inserted in the main body from a bottom vertically, and the wing unit comprises a first wing unit rotated on the upper shaft in a first direction by a power generated from the first motor, and a second wing unit rotated on the lower shaft in a second direction, which is the reverse of the first direction, by a power generated from the second motor.

Abstract translation: 公开了一种无人机，包括：主体，包括电动机，垂直插入主体的轴;翼单元，其通过由电动机产生的动力在轴上旋转，所述翼单元包括水平地折叠并垂直折叠的螺旋桨，其中 所述电动机包括第一电动机和第二电动机，并且所述轴包括从垂直方向从底部插入主体的顶部垂直插入主体中的上轴，并且所述机翼单元包括第一翼单元 通过从第一马达产生的动力沿第一方向在上轴上旋转，并且第二翼单元通过从第二马达产生的动力沿与第一方向相反的第二方向在下轴上旋转 。