公开(公告)号：US20170297445A1

公开(公告)日：2017-10-19

申请号：US15132255

申请日：2016-04-19

Applicant: SHENZHEN FLYEAH INTELLIGENT TECHNOLOGY CO., LTD.

Inventor： Junxiong ZHENG ,  Daniel Yin LIU ,  Hongyu RAN

IPC: B60L11/18 ,  B64F1/36 ,  B64C39/02 ,  B64D5/00

CPC classification number: B64D5/00 ,  B60L53/14 ,  B60L53/37 ,  B64C37/02 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/182 ,  B64C2201/206 ,  B64D2203/00

Abstract: A cone shaped docking and releasing mechanism provides rigid connection between a parent UAV and a sub UAV to form a spliced double unmanned aerial vehicle system with improved cruising duration ability by providing sub UAV battery with charging function. It comprises a parent UAV, a sub UAV and a docking mechanism with charging ports. The parent UAV and the sub UAV are connected with each other through the docking mechanism to form a double UAV system, the docking mechanism is a cone structure and comprises a charging output component connected with the parent UAV internal control system, a charging circuit connected with a sub UAV control system and a charging input component connected with the charging circuit.