公开(公告)号：US20240417114A1

公开(公告)日：2024-12-19

申请号：US18691352

申请日：2022-09-13

Applicant: ORTHODRONE GMBH

Inventor： Juri Niklas KLUSAK ,  Nils LIECKFELDT ,  Mirko Jesper DENECKE ,  Max-Christoph GURGEL ,  Sebastian SCHOCK ,  Christine Elizabeth AVERY ,  Julian Ärwin TEEGE ,  Clara Andrea DRUMMER

IPC: B64U30/296 ,  B64U10/14 ,  B64U30/24

Abstract: Described is an aircraft, in particular a drone, with a supporting body (2) and at least two propulsion arrangements (4, 8) arranged at a distance from one another on the supporting body (2), which are designed to generate a propulsive thrust in a direction of propulsion (8b). According to a first aspect of the invention, the propulsion arrangements (4, 8) on the supporting body (2) are each mounted so as to be pivotable independently of one another about a first axis of pivoting (6) extending at an angle to the direction of propulsion (8b) and a first actuating drive (10) is provided and designed to pivot the propulsion arrangements (4, 8) independently of one another about the first axis of pivoting (6). According to a second aspect of the invention, in which a trunk body (20) is provided, this trunk body (20) is mounted on the supporting body (2) so as to be pivotable about a second axis of pivoting (22) and a second actuating drive (24) is provided and designed to pivot the supporting body (2) relative to the trunk body (20).