公开(公告)号：US20170253331A1

公开(公告)日：2017-09-07

申请号：US15383375

申请日：2016-12-19

Applicant: FUTABA CORPORATION ,  O.S.ENGINES MFG. CO., LTD.

Inventor： Shuichiro NAKASHIMA

IPC: B64C39/02 ,  B64C27/08

CPC classification number: B64C39/024 ,  B64C27/08 ,  B64C2201/027 ,  B64C2201/044 ,  B64C2201/108 ,  B64D35/04

Abstract: A multicopter is provided which includes an engine configured to generate rotation by burning fuel in the engine, a plurality of propellers configured to generate a lift by rotating, a rotation transmission path configured to distribute and transmit the rotation generated by the engine to the propellers.