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：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：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.