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Development of a Coanda-Drone with Built-in Propellers

Zejing ZHAO, Bin ZHANG, Hun-ok LIM

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Summary :

In this study, a Coanda-drone with length, width, and height of 121.6, 121.6, and 191[mm] was designed, and its total mass was 1166.7[g]. Using four propulsion devices, it could produce a maximum of 5428[g] thrust. Its structure is very different from conventional drones because in this study it combines the design of the jet engine of a jet fixed-wing drone with the fuselage structure layout of a rotary-wing drone. The advantage of jet drone's high propulsion is kept so that it can output greater thrust under the same variation of PWM waveform output. In this study, the propulsion device performs high-speed jetting, and the airflow around the propulsion device will also be jetted downward along the direction of the airflow.

Publication
IEICE TRANSACTIONS on Information Vol.E107-D No.2 pp.180-190
Publication Date
2024/02/01
Publicized
2023/11/10
Online ISSN
1745-1361
DOI
10.1587/transinf.2023EDP7053
Type of Manuscript
PAPER
Category
Artificial Intelligence, Data Mining

Authors

Zejing ZHAO
  Kanagawa University
Bin ZHANG
  Kanagawa University
Hun-ok LIM
  Kanagawa University

Keyword