公开(公告)号：US20190161178A1

公开(公告)日：2019-05-30

申请号：US16206988

申请日：2018-11-30

Applicant: Coretronic Intelligent Robotics Corporation

Inventor： SHIH-HANG LIN ,  YING-CHIEH CHEN

IPC: B64C27/00 ,  B64C27/473 ,  B64C39/02

Abstract: An unmanned aerial vehicle includes a body, a plurality of cantilevers and a plurality of driving components. Each cantilever has a first end and a second end. Each first end is opposite to the corresponding second end. The first ends are connected to the body. The driving components are respectively connected to the second ends of the cantilevers. Each driving component includes a motor and a plurality of paddles. The motor has a shaft. The propeller is connected to the shaft and includes a balance disc and a plurality of paddles. The balance disc is connected to the motor. The paddles are connected to the balance disc. The balance disc has a plurality of counterweight holes. The counterweight holes are used to be disposed with the at least one counterweight block. A propeller is also provided.

公开(公告)号：US20190100330A1

公开(公告)日：2019-04-04

申请号：US15721003

申请日：2017-09-29

Applicant: Coretronic Intelligent Robotics Corporation

Inventor： HSU-CHIH CHENG ,  YING-CHIEH CHEN ,  CHI-TONG HSIEH

IPC: B64F1/00 ,  B64C39/02

Abstract: A platform, adapted to accommodate a UAV (Unmanned Aerial Vehicle), includes a base and a cover. The base includes a first connection port and a power source, and the power source is coupled to the first connection port including a first connection electrode and a second connection electrode. The cover includes at least one fan and a second connection port corresponding to the first connection port of the base, the at least one fan is coupled to the second connection port, and the second connection port includes a first contact electrode and a second contact electrode. The cover is connected to the base and moves between an open position and a closed position relative to the base. The first connection port is connected to the second connection port when the cover is at the closed position, and the power source provides power to the at least one fan.

公开(公告)号：US20240150017A1

公开(公告)日：2024-05-09

申请号：US18386612

申请日：2023-11-03

Applicant: Coretronic Intelligent Robotics Corporation

Inventor： TAI-YUAN WANG ,  I-TA YANG ,  YING-CHIEH CHEN

IPC: B64D1/22

CPC classification number: B64D1/22

Abstract: A hanging structure applicable to an unmanned aerial vehicle includes a hook-shaped body and at least one hook claw. The hook-shaped body has a bottom, at least one pivoting end, and an abutting portion. A hook opening is provided between the at least one pivoting end and the abutting portion and is opposite to the bottom. In addition, the at least one hook claw has a pivoting portion, and a first claw portion and a second claw portion that extend from the pivoting portion, respectively. The pivoting portion is pivoted to the at least one pivoting end. The second claw portion is heavier than the first claw portion. When the hanging structure is in a hanging state, a first end of the first claw portion abuts against the abutting portion, and the hook opening is closed. An unmanned aerial vehicle hanging system including the above hanging structure is further provided.

公开(公告)号：US20190315463A1

公开(公告)日：2019-10-17

申请号：US16276587

申请日：2019-02-14

Applicant: Coretronic Intelligent Robotics Corporation

Inventor： YING-CHIEH CHEN ,  I-TA YANG ,  HSU-CHIH CHENG ,  CHI-TONG HSIEH

IPC: B64C39/02 ,  F24H9/20 ,  G05D23/20 ,  B64F1/22

Abstract: A temperature control equipment, adapted to control the temperature of a docking station for a UAV, wherein a cover of the docking station includes a first and a second vents. The temperature control equipment includes a first and a second temperature control devices. The first temperature control device includes a first and a second airflow openings, and the second temperature control device includes a third and a fourth airflow openings. The first, second, third, and fourth airflow openings, and the first and second vents form a first airflow path; or the first and second airflow openings, the first vent, and a third vent of the cover form a second airflow path; or the first, second, third, and fourth airflow openings, the first, second, and third vents, a fourth vent of the cover form a third airflow path. A heater is located on the first, second or third airflow path.

公开(公告)号：US20190152620A1

公开(公告)日：2019-05-23

申请号：US16172682

申请日：2018-10-26

Applicant: Coretronic Intelligent Robotics Corporation

Inventor： YING-CHIEH CHEN ,  LIN-CHING WU ,  CHUANG-YUAN CHENG ,  KAI-CHUNG CHAN

IPC: B64D45/00 ,  B64C39/02 ,  G08B21/18

Abstract: An unmanned aerial vehicle, an unmanned aerial vehicle control center and an unmanned aerial vehicle alarm method are provided. The unmanned aerial vehicle includes a motor and a control circuit board. The control circuit board is adapted to read a real-time drive current value and/or a real-time rotational speed value of the motor and transmitting warning related information. The unmanned aerial vehicle control center is adapted to conduct a warning according to the warning related information and adapted to a backup and storage of data. The unmanned aerial vehicle alarm method includes that the unmanned aerial vehicle is made to read the real-time drive current value and/or the real-time rotational speed value at the time of a motor operation and to transmit the warning related information to the unmanned aerial vehicle control center.

公开(公告)号：US20200001995A1

公开(公告)日：2020-01-02

申请号：US16396795

申请日：2019-04-29

Applicant: Coretronic Intelligent Robotics Corporation

Inventor： I-TA YANG ,  YING-CHIEH CHEN ,  CHI-TONG HSIEH ,  HSU-CHIH CHENG

IPC: B64C39/02 ,  B64C27/473

Abstract: A rotorcraft includes a body and a plurality of rotary-wing parts. The body has a front-end portion, a rear-end portion, two side portions, and a reference plane passing through the front-end portion, the rear-end portion, and the two side portions. The plurality of rotary-wing parts are disposed to the body. Each of the rotary-wing parts includes at least one blade and a shaft coupled to the at least one blade. The at least one blade is rotated around an axis of the shaft. An angle between the axis of the shaft and a normal line of the reference plane is between 5 and 30 degrees. The rotorcraft can provide additional lift force, to help reduce the weight of the rotorcraft.

公开(公告)号：US20180127086A1

公开(公告)日：2018-05-10

申请号：US15807461

申请日：2017-11-08

Applicant: Coretronic Intelligent Robotics Corporation

Inventor： YING-CHIEH CHEN ,  SHIH-HANG LIN ,  PEI-RONG WU

IPC: B64C11/18

CPC classification number: B64C11/18 ,  B64C27/467 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108

Abstract: An aerial vehicle and a propeller thereof are provided. The propeller includes a hub and at least one blade. The hub is rotatable about a shaft, and the blade is mounted to the hub. The blade extends from the hub to a tip along a first direction and has a leading edge and a tailing edge opposite to the leading edge. The blade has a section along a second direction in an arbitrary position along the first direction. The second direction is perpendicular to the first direction. A section of the blade in a first position along the first direction has a first peak value of chord length, and a section of the blade in a second position along the first direction has a second peak value of chord length. The second position is between the first position and the tip.