公开(公告)号：US12187467B2

公开(公告)日：2025-01-07

申请号：US17660257

申请日：2022-04-22

Applicant: AUTEL ROBOTICS CO., LTD.

Inventor： Qiang Liu ,  Gang Chen ,  Kangli Wang ,  Shenglong Wang ,  Maxwell Lee ,  Wenzhong He ,  Xiangxi Pan

IPC: B64U20/40 ,  B64U10/14 ,  B64U10/20 ,  B64U30/14 ,  B64U30/291 ,  B64U30/40

Abstract: The embodiments is an unmanned aerial vehicle. The unmanned aerial vehicle includes: an airframe; and a fixed-wing assembly and a rotor assembly, both replaceably connected to the airframe. The fixed-wing assembly is connected to the airframe to form a vertical take-off and landing fixed-wing unmanned aerial vehicle and the rotor assembly is connected to the airframe to form a multi-rotor unmanned aerial vehicle, thereby implementing an unmanned aerial vehicle that can switch between the vertical take-off and landing fixed-wing unmanned aerial vehicle and the multi-rotor unmanned aerial vehicle.

公开(公告)号：US20220242563A1

公开(公告)日：2022-08-04

申请号：US17660251

申请日：2022-04-22

Applicant: AUTEL ROBOTICS CO., LTD.

Inventor： Shenglong WANG ,  Maxwell Lee

IPC: B64C39/02 ,  B64C1/06 ,  B64C1/16

Abstract: The embodiment is an unmanned aerial vehicle. The unmanned aerial vehicle includes: an airframe, including first mounting portions, where the first mounting portion includes a first mounting body and connecting rods formed on the first mounting body, the connecting rods extending in a pitch axis direction; and a power assembly, including a first assembling body and eccentric wheels mounted on the first assembling body, where the eccentric wheel is rotatable between a first rotation position and a second rotation position of the first assembling body around a rotation axis of the first assembling body, the rotation axis being perpendicular to the pitch axis direction.

公开(公告)号：US12065241B2

公开(公告)日：2024-08-20

申请号：US17660251

申请日：2022-04-22

Applicant: AUTEL ROBOTICS CO., LTD.

Inventor： Shenglong Wang ,  Maxwell Lee

IPC: B64C39/02 ,  B64C1/06 ,  B64C1/16 ,  B64U10/20 ,  B64U30/14

CPC classification number: B64C39/024 ,  B64C1/061 ,  B64C1/16 ,  B64U10/20 ,  B64U30/14

Abstract: The embodiment is an unmanned aerial vehicle. The unmanned aerial vehicle includes: an airframe, including first mounting portions, where the first mounting portion includes a first mounting body and connecting rods formed on the first mounting body, the connecting rods extending in a pitch axis direction; and a power assembly, including a first assembling body and eccentric wheels mounted on the first assembling body, where the eccentric wheel is rotatable between a first rotation position and a second rotation position of the first assembling body around a rotation axis of the first assembling body, the rotation axis being perpendicular to the pitch axis direction.