The original paper is in English. Non-English content has been machine-translated and may contain typographical errors or mistranslations. ex. Some numerals are expressed as "XNUMX".
Copyrights notice
The original paper is in English. Non-English content has been machine-translated and may contain typographical errors or mistranslations. Copyrights notice
Neste estudo, foi projetado um drone Coanda com comprimento, largura e altura de 121.6, 121.6 e 191[mm], e sua massa total foi de 1166.7[g]. Usando quatro dispositivos de propulsão, ele poderia produzir um empuxo máximo de 5428[g]. Sua estrutura é muito diferente dos drones convencionais porque neste estudo combina o design do motor a jato de um drone de asa fixa a jato com o layout da estrutura da fuselagem de um drone de asa rotativa. A vantagem da alta propulsão do drone a jato é mantida para que ele possa produzir maior empuxo sob a mesma variação da saída da forma de onda PWM. Neste estudo, o dispositivo de propulsão realiza jatos de alta velocidade, e o fluxo de ar ao redor do dispositivo de propulsão também será lançado para baixo ao longo da direção do fluxo de ar.
Zejing ZHAO
Kanagawa University
Bin ZHANG
Kanagawa University
Hun-ok LIM
Kanagawa University
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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},}
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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 -