IEICE TRANSACTIONS on Information
Development of a Coanda-Drone with Built-in Propellers
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
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Zejing ZHAO, Bin ZHANG, Hun-ok LIM, "Development of a Coanda-Drone with Built-in Propellers" in IEICE TRANSACTIONS on Information,
vol. E107-D, no. 2, pp. 180-190, February 2024, doi: 10.1587/transinf.2023EDP7053.
Abstract: 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.
URL: https://global.ieice.org/en_transactions/information/10.1587/transinf.2023EDP7053/_p
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@ARTICLE{e107-d_2_180,
author={Zejing ZHAO, Bin ZHANG, Hun-ok LIM, },
journal={IEICE TRANSACTIONS on Information},
title={Development of a Coanda-Drone with Built-in Propellers},
year={2024},
volume={E107-D},
number={2},
pages={180-190},
abstract={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.},
keywords={},
doi={10.1587/transinf.2023EDP7053},
ISSN={1745-1361},
month={February},}
Copy
TY - JOUR
TI - Development of a Coanda-Drone with Built-in Propellers
T2 - IEICE TRANSACTIONS on Information
SP - 180
EP - 190
AU - Zejing ZHAO
AU - Bin ZHANG
AU - Hun-ok LIM
PY - 2024
DO - 10.1587/transinf.2023EDP7053
JO - IEICE TRANSACTIONS on Information
SN - 1745-1361
VL - E107-D
IS - 2
JA - IEICE TRANSACTIONS on Information
Y1 - February 2024
AB - 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.
ER -
English
