21-06-2018 дата публикации
Номер: WO2018108148A1
Автор:
HUANG, Li,
WU, Han,
WANG, Gang,
WANG, Xiaojie,
GU, Xing,
LIU, Huabin
Принадлежит:
An unmanned aerial vehicle, comprising a fuselage (1) and multiple arms (2) disposed at left and right sides of the fuselage (1), said unmanned aerial vehicle also comprising a sliding mechanism; open grooves (3,11) are provided on the fuselage (1); the sliding mechanism comprises: slides (5, 7, 13, 15) provided in the open grooves (3, 11); when the unmanned aerial vehicle is in operation, the arms (2) slide along the slides (5, 7, 13, 15) and thereby extend out of the open grooves (3, 11) of the fuselage (1); when the unmanned aerial vehicle is not in operation, the arms (2) slide along the slides (5, 7, 13, 15) and thereby retract within the open grooves (3, 11) of the fuselage. The present unmanned aerial vehicle has a a compact structure and takes up little space, and can greatly decrease volume when in a non-operating state, facilitating a user storing, holding, carrying and transporting the unmanned aerial vehicle.
Подробнее