公开(公告)号：US20190009901A1

公开(公告)日：2019-01-10

申请号：US16129115

申请日：2018-09-12

Applicant: AUTEL ROBOTICS CO., LTD.

Inventor： Dongdong LUO ,  Marc SCHWARZBACH ,  Wenbing SU

IPC: B64C29/00 ,  B64C27/26

Abstract: A tilt driving mechanism comprises a housing fixedly mounted on the aircraft, a driving mechanism mounted in the housing, and a mounting seat flexibly mounted on the housing. A power unit is fixedly mounted on the mounting seat, and the driving mechanism is fixedly connected to the mounting seat, so as to drive the mounting seat to rotate with respect to the housing. The tilt driving mechanism is disposed on the aircraft, and a rotation angle of the tilt driving mechanism is controlled with high precision to change a direction of the power unit, so that the power unit switches between a lift force providing position and a thrust providing position. Meanwhile, the driving mechanism is disposed in the tilt driving mechanism, thereby significantly reducing a torque of the driving mechanism, facilitating miniaturization design of the tilt driving mechanism, and improving stability and safety of the tilt driving mechanism.

公开(公告)号：US20190092447A1

公开(公告)日：2019-03-28

申请号：US16051726

申请日：2018-08-01

Applicant: AUTEL ROBOTICS CO., LTD.

Inventor： Marc SCHWARZBACH ,  Jian WANG ,  Thomas RAFFLER

IPC: B64C1/28 ,  B64C27/08 ,  B64C39/02

Abstract: A multirotor aircraft is provided. The multirotor aircraft comprises a body comprising a main body and a camera assembly with a camera coupled to the main body; a frame connected to the body, comprising a multirotor propulsion system; and a drive system coupled with the body and the frame, for driving the body to rotate against the frame. With the multirotor aircraft, full unobstructed 360° yaw field of view of the camera in the upper or lower hemisphere can be obtained and the camera is in a safe position at takeoff and landing.

公开(公告)号：US20190047706A1

公开(公告)日：2019-02-14

申请号：US16158899

申请日：2018-10-12

Applicant: AUTEL ROBOTICS CO., LTD.

Inventor： Marc SCHWARZBACH ,  Jian WANG

IPC: B64C39/02 ,  G01C23/00 ,  G05D1/00 ,  H04N7/18

Abstract: The present disclosure relates to aircraft technologies, and in particular, to a flight direction display method and apparatus, and an unmanned aerial vehicle. The method includes the following steps: obtaining a flight direction indication of an aircraft sent by a camera system, where the flight direction indication is determined by the camera system according to a relative angle between a camera apparatus and the aircraft; and displaying the flight direction indication of the aircraft on a shooting preview screen. In the present disclosure, the flight direction indication of the aircraft sent by the camera system is obtained, where the flight direction indication is determined by the camera system according to the relative angle between the camera apparatus and the aircraft, and the flight direction indication of the aircraft is displayed in the shooting preview screen. In addition, a flight direction of the aircraft is controlled according to the flight direction indication, so that in a shooting process, a flight direction of a fuselage of the aircraft is the same as a rotation direction of the camera apparatus, so as to shoot content wanted by the camera apparatus, thereby improving user experience.