公开(公告)号：US20190185161A1

公开(公告)日：2019-06-20

申请号：US16323704

申请日：2017-08-08

Applicant: CLEO ROBOTICS INC.

Inventor： Omar ELERYAN ,  Szymon CZARNOTA

IPC: B64C39/02 ,  B64C13/16 ,  B64D47/08

CPC classification number: B64C39/024 ,  B64C13/16 ,  B64C27/08 ,  B64C29/00 ,  B64C39/00 ,  B64C39/02 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/18 ,  B64C2201/20 ,  B64D47/08

Abstract: A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a duct. The UAV further comprises a motor for rotating a fan that directs air into and out of the duct enabling the UAV to take flight. The UAV comprises a flight-control system that comprises at least two flight control surfaces that can alter the directed air as it flows through the duct for controlling the roll and pitch and optionally the yaw of the UAV during flight. The flight control system may be controlled by a microprocessor controller. The UAV further comprises a payload, with at least a wireless transmitter and receiver unit.

公开(公告)号：US20230150664A1

公开(公告)日：2023-05-18

申请号：US18089175

申请日：2022-12-27

Applicant: CLEO ROBOTICS INC.

Inventor： Omar ELERYAN ,  Szymon CZARNOTA

IPC: B64C39/02 ,  B64C13/16

CPC classification number: B64C39/024 ,  B64C13/16 ,  B64C39/028 ,  B64U10/13

Abstract: A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a duct. The UAV further comprises a motor for rotating a fan that directs air into and out of the duct enabling UAV to take flight. The UAV comprises a flight-control system that comprises at least two flight control surfaces that can alter the directed air as it flows through the duct for controlling the roll and pitch and optionally the yaw of the UAV during flight. The flight control system may be controlled by a microprocessor controller. The UAV further comprises a payload, with at least a wireless transmitter and receiver unit.