公开(公告)号：US20190382104A1

公开(公告)日：2019-12-19

申请号：US16484830

申请日：2018-02-12

Applicant: Singapore University Of Technology And Design

Inventor： Jun En LOW ,  Thura Win Luk SOE ,  Chee How TAN ,  Danial Sufiyan Bin SHAIFUL ,  Shaohui FOONG ,  Gim Song SOH

IPC: B64C27/22 ,  B64C39/02

Abstract: An aircraft including: a pair of wings rotatably coupled to opposing lateral sides of the fuselage and being rotatable relative to each other; a pair of servo motors, each connected to a corresponding wing and configured to rotate the corresponding wing in two rotational directions; a pair of thrust motors, each of which mounted on a corresponding wing; and a flight controller connected to the servo motors and to the thrust motors, and configured to control each servo motor and each thrust motor, such that the aircraft can be selectively operated in a cruising mode, such that the pair of wings are in a non-permanent-rotation-state about a yawing axis which extends at least substantially through the center of gravity, and a monocopter mode, in which the pair of thrust motors provide thrust in opposite directions so that the pair of wings are in a permanent-rotation-state about the yawing axis.