公开(公告)号：USD903573S1

公开(公告)日：2020-12-01

申请号：US29681933

申请日：2019-02-28

Applicant: JAPAN AEROSPACE EXPLORATION AGENCY

Designer： Eiji Shima

公开(公告)号：USD885298S1

公开(公告)日：2020-05-26

申请号：US29681929

申请日：2019-02-28

Applicant: JAPAN AEROSPACE EXPLORATION AGENCY

Designer： Eiji Shima

公开(公告)号：US11794891B2

公开(公告)日：2023-10-24

申请号：US17413896

申请日：2019-07-19

Applicant: JAPAN AEROSPACE EXPLORATION AGENCY

Inventor： Eiji Shima ,  Seiji Tsutsumi ,  Keiichiro Fujimoto

IPC: B64C29/00 ,  B64C9/00 ,  B64D27/24

CPC classification number: B64C29/0033 ,  B64C9/00 ,  B64D27/24 ,  B64C2009/005

Abstract: An aerial vehicle includes a propulsion unit and a fuselage unit. The propulsion unit includes a rotary shaft extending in a first direction and thrust producing mechanisms provided at both ends of the rotary shaft and produces a propulsion force for flying in air. The fuselage unit is suspended from the propulsion unit below the rotary shaft, has a center of gravity at a position below the rotary shaft, is configured to freely rotate around the rotary shaft, and is capable of storing an article.